foreword

This Flight Crew Training Manual is an essential tool to learn the ATR standard operating
procedures. It has been conceived as the standard baseline for all ATR flight crew training.
To facilitate the learning process, procedures are presented in a pedagogical and user-
friendly way, with, when necessary, a visualization of cockpit flows and schematics of flight
patterns.

This manual is a comprehensive document that efficiently complements FCOM procedures.

It is divided into two volumes:
Normal Procedures and Emergency & Abnormal Procedures.

In the Normal Procedures manual, procedures are presented with detailed task sharing
and include standard call outs. Additional procedures relating to specific operations and to
equipments uses are part of this manual.

In the Emergency & Abnormal Procedures manual, the general management of abnormal
situations is explained. Then, a detailed presentation of the procedures to apply per specific
situation is made.

This latest revision encompasses all the changes agreed in 2008 during a comprehensive
review of the ATR operational documentation (AFM, FCOM & QRH).
NB: Should you find any discrepancy in the emergency procedures between the FCTM and the AFM,
please follow the AFM procedures.

The Training and Flight Operations support team.

 NORMAL PROCEDURES
ORGANIZATION JUN 09
OF THE MANUAL

TOP OF PAGE

1 2 4
NORMAL PROCEDURES 01.01
5 Page 4 01 6
STANDARD OPERATING
PROCEDURES
3 7 SEPT 08

1 ATC logo
2 Part title
3 Chapter title
4 Chapter & sections numbers
5 Page numbering for the section
6 Sequence number
7 Date of issue

LATERAL BOOKMARK
42 not PEC
72 not PEC

ALL ATR
42 PEC
72 PEC

shows aircraft type for which page is effective: please refer to it before study.
72 PEC refers to 72-500
42 PEC refers to 42-500
72 not PEC refers to 72-200/210
42 not PEC refers to 42-300/320

FOR TRAINING ONLY

 NORMAL PROCEDURES
CONTENTS JUN 09

Introduction to normal procedures...................................................... 01

1. Definitions............................................................................................................................... 01.01
1.1. Crew.................................................................................................................................. 01.01 1
1.2. Flight phase....................................................................................................................... 01.01 1
1.3. Procedure......................................................................................................................... 01.01 1
1.4. Checklist........................................................................................................................... 01.01 1
2. Crew coordination................................................................................................................. 01.02
2.1. Crew function.................................................................................................................... 01.02 1
2.2. Safety recommendations.................................................................................................. 01.02 2
2.3. Cross control..................................................................................................................... 01.02 3
2.4. Procedure methodology.................................................................................................... 01.02 4
2.5. Checklist methodology / Challenge and reply.................................................................... 01.02 7
2.6. Task sharing...................................................................................................................... 01.02 8
3. Specific procedures.............................................................................................................. 01.03
3.1. Auto Flight Control System (AFCS).................................................................................... 01.03 1
3.2. Flaps use.......................................................................................................................... 01.03 16
3.3. Landing gear use.............................................................................................................. 01.03 17
3.4. Altimeter and radioaltimeter setting................................................................................... 01.03 18
3.5. Speed bugs...................................................................................................................... 01.03 20
3.6. Torque bugs...................................................................................................................... 01.03 25
3.7. Data card........................................................................................................................... 01.03 28
3.8. Briefing............................................................................................................................. 01.03 36
3.9. Navigation policy............................................................................................................... 01.03 39
3.10. Radio-communication..................................................................................................... 01.03 43
3.11. Lights policy..................................................................................................................... 01.03 44

Standard operating procedures. ................................................................ 02

1. Presentation........................................................................................................................... 02.01
2. Pre-flight preparation procedure........................................................................................ 02.02
3. Procedures and associated flows....................................................................................... 02.03
3.1. Long and short transit........................................................................................................ 02.03 1
3.2. Internal inspection............................................................................................................. 02.03 2
3.3. External inspection............................................................................................................ 02.03 4
3.4. Preliminary cockpit preparation......................................................................................... 02.03 16
3.5. Final cockpit preparation................................................................................................... 02.03 24
3.6. Before propeller rotation.................................................................................................... 02.03 26
3.7. Before taxi......................................................................................................................... 02.03 31
3.8. Taxi................................................................................................................................... 02.03 35
3.9. Before take-off.................................................................................................................. 02.03 37
3.10. Take-off........................................................................................................................... 02.03 39
3.11. Climb sequence............................................................................................................... 02.03 41
3.12. After take-off.................................................................................................................... 02.03 43
3.13. FL 100 during climb......................................................................................................... 02.03 44
3.14. Cruise.............................................................................................................................. 02.03 44
3.15. Before descent................................................................................................................ 02.03 46
3.16. FL 100 during descent..................................................................................................... 02.03 48
3.17. Approach......................................................................................................................... 02.03 48
3.18. Before landing................................................................................................................. 02.03 48

FOR TRAINING ONLY

 NORMAL PROCEDURES
CONTENTS JUN 09

3.19. Circle to land................................................................................................................... 02.03 54

3.20. Visual flight patterns........................................................................................................ 02.03 56
3.21. Landing........................................................................................................................... 02.03 58
3.22. Go-around...................................................................................................................... 02.03 59
3.23. After landing.................................................................................................................... 02.03 61
3.24. Parking............................................................................................................................ 02.03 63
3.25. Leaving the aircraft.......................................................................................................... 02.03 65

NORMAL SYSTEM USE...................................................................................................... 03

1. Global Navigation Satellite System (GNSS)....................................................................... 03.01
1.1. Policy................................................................................................................................. 03.01 1
1.2. Pre-flight............................................................................................................................ 03.01 2
1.3. User waypoints................................................................................................................. 03.01 11
1.4. Flight in progress............................................................................................................... 03.01 13
2. Aircraft Performance Monitoring (APM)............................................................................ 03.02
2.1. APM cockpit interface........................................................................................................ 03.02 1
2.2. Normal procedures........................................................................................................... 03.02 2

Additional standard operating procedures................................... 04

1. Hotel mode use...................................................................................................................... 04.01
1.1. Start up without GPU during long transit............................................................................ 04.01 1
1.2. Start up without GPU during short transit.......................................................................... 04.01 6
1.3. Ramp arrival without GPU................................................................................................. 04.01 6
2. Noise abatement procedures.............................................................................................. 04.02
3. Icing conditions..................................................................................................................... 04.03
4. Operations on wet and contaminated runways................................................................. 04.04
5. Push-back operation............................................................................................................. 04.05
5.1. Power back....................................................................................................................... 04.05 1
5.2. Push-back with Tug........................................................................................................... 04.05 1
6. Start up engine n 1 during taxiing...................................................................................... 04.06
7. Operating minima.................................................................................................................. 04.07
7.1. Definitions.......................................................................................................................... 04.07 1
7.2. Approach minima.............................................................................................................. 04.07 2
7.3. RVR / visibility.................................................................................................................... 04.07 4
7.4. Flight preparation............................................................................................................... 04.07 6
7.5. Airport approach facilities.................................................................................................. 04.07 7

Schematics........................................................................................................................... 05
1. Take-off................................................................................................................................... 05.01
2. ILS 2 Engines.......................................................................................................................... 05.02
3. Non precision approach....................................................................................................... 05.03
4. Circling approach.................................................................................................................. 05.04
5. Go-around 2 engines............................................................................................................. 05.05
6. Standard visual pattern 1500 ft AAL................................................................................... 05.06

FOR TRAINING ONLY

 01.01
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PROCEDURES

1. Definitions

1.1. Crew
CM1 refers to the crew member in the left hand seat.

CM2 refers to the crew member in the right hand seat.

The captain always makes the final decision.

PF is the crew member who flies the aircraft and performs the navigational tasks.

PNF is the crew member who deals with radio communication, performs the mechanical tasks
(Condition Levers), and monitors flight path.

Cabin crew has to take care of passengers and to ensure the communication between the cabin
and the cockpit. Cabin crew is in charge of passenger safety.

For any additional explanation on task sharing, please refer to Introduction to the Emergency and
Abnormal Procedures Manual.

1.2. Flight phase

ALL ATR
A flight is divided into several flight phases.

Each flight phase is associated with a procedure and eventually followed by a checklist.

A procedure allows crew members to perform all actions. Checklist permits to check they have
been correctly done.

1.3. Procedure
Each flight phase complies with a specific chronological action list which the crew performs from
memory.

Note: n A procedure is performed before checklist reading.

n It is triggered by the word procedure. (e.g. Before take-off procedure).
n All procedures contained in this manual are in compliance with FCOM & QRH.

1.4. Checklist (C/L)

Normal checklists are used to verify that main procedures with impact on flight management
have been correctly performed and checked.

To be efficient, checklist reading must be preceeded with all actions performed from memory.

Note: All checklists in this manual are in compliance with QRH.

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2. Crew coordination

2.1. Crew function

FLIGHT PHASES CM1 CM2

ON THE GROUND < 70Kt PF PNF

1st
ON THE GROUND PF PNF
situation*
> 70Kt

or
2nd
IN FLIGHT PNF PF
situation*
ALL ATR

* decided during the captain's briefing.

For all procedures, the general task sharing stated below is applicable:

PF is in charge of: PNF is in charge of:

Flight path and power levers Checklist reading

Navigation Communication
Aircraft configuration Mechanic and conditions levers
Procedure initiation Monitoring PF and flight path

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Pilot flying transfer

The PF function may be transfered, due to to external factors, with the following announcement:

YOUR CONTROL or YOU HAVE CONTROL

The pilot who receives the PF function announces:

MY CONTROL or I HAVE CONTROL

After PF / PNF function change, the crew must change and check that the coupling is set to the new
PF side.

Whenever possible and prior to the transfer, the PF should remind the main flight parameters to the
PNF.

2.2. Safety recommendations

ALL ATR
Execution of given orders

Crew members must inform each other of any task done.

PF orders and PNF executes and announces when complete.

Anti collision monitoring

Crew should avoid paper work (flight log, technical log,...) between ground and Flight Level 100 (except
for ATC clearance).

Anti collision monitoring must be done by both crew members (outside by visual check and inside by
ATC frequency listening and TCAS).

Communication in the cockpit

Talks, requests and call outs must be limited to a minimum during the critical flight phases (take-off,
approach, landing or missed approach).

Technical communications between both pilots must comply with the standard announcements and
call outs explained in this manual.

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Headset

The crew must wear headset: n Before engine start and up to FL 100.
n From FL 100 to engine shut down.
n On Captains decision.

Cabin crew

Pilots must inform the cabin crew of all significant flight phase changes.

Take-off.

Service beginning.

Turbulence area.

Descent.

Before landing.

Technical problem impacting cabin procedure.

Following an announcement, the cabin crew must:

Secure servicing materials, and stay at service seat.

Start a technical or commercial action.

ALL ATR

Apply a specific procedure.

2.3. Cross control

Cross control is a safety factor, using CROSS CHECKS.

Control must be done by clear messages and information.

To allow an efficient cross check:

Each pilot should know the other crew member procedures.

The procedure should be entirely and accurately followed.

If an indication is not in compliance with the executed action, crew members must check that the
relevant system is correctly set and/or take any necessary action to correct the situation.

Any pilot action, wich modifies the flight parameters (flight path, speed or a system status), should be
announced by a pilot and cross-checked by the other one (cross check efficiency is necessary to flight
safety).

PNF can be briefly busy (ATC message, weather listening, operating manual reading, procedure action,
etc). Any mode changed by PF concerning ADU, system or any noticeable items must be reported to
PNF when his attention becomes available again.

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2.4. Procedure methodology

A procedure always precedes a checklist for the considered flight phase.

Procedures must be executed in full, calmly, and precisely.

Every pilot must know the other pilot's procedure items.

Procedures are triggered by:

On the ground: In flight:

Procedures are triggered by Procedures are triggered by

CM1 or specific flight event PF or specific flight event

PF and PNF task sharing must comply with the following orders and announcements:
Example: Taxi procedure

Flight events CM1 CM2

ALL ATR
READY TO TAXI ORDER DO
REQUEST TAXI CLEARANCE TAXI CLEARANCE...........REQUESTED

TAXI CLEARANCE ANNOUNCE

GROUND FROM COCKPIT, READY TO TAXI,
RECEIVED
YOU CAN REMOVE CHOCKS AND
DISCONNECT

WHEN GROUND DO DO
STAFF IN SIGHT ON COCKPIT COM HATCH.....CLOSED
CAPTAINS SIDE BLOCK TIME..................ANNOUNCED
SECURITY ....................CHECK LEFT SIDE SECURITY..................CHECK RIGHT SIDE
TAXI & T/O LIGHT............ON
PARKING BRAKE............RELEASED

BRAKES CHECK: for passengers comfort, the following procedure can be used:
set taxi power
parking brake handle from ON to EMER position
then CM2 checks brakes (parking brake released)
then CM1 checks brakes (CM2 releases) and CM1 starts to taxi.

ORDER DO
TAXI PROCEDURE INSTRUMENT................CHECK
ON TAXIWAY HDG MODE...................SELECTED
DO
INSTRUMENTS............. CHECK* LOW BANK....................SELECTED
IAS MODE.....................SELECTED
IAS...............................V2 + 5 kt SET
COUPLING....................PF SIDE
* CHECK HEADING, BEARINGS, HORIZON / RMI T/O CONFIG TEST...........PERFORMED

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Flight events CM1 CM2

When PF and PNF

ready PF

DO
T/O BRIEFING...............PERFORMED
Refer to 01.03 p. 37, take-off briefing

After PF take-off ANNOUNCE

briefing TAXI PROCEDURE COMPLETE

ANNOUNCE AND READ

when taxi REQUEST AND ANSWER TAXI CHECKLIST
procedure TAXI CHECKLIST Refer to QRH 6.01
complete
ANNOUNCE
C/L COMPLETE

REMARKS:

In some flight phases, the procedure achievement is triggered by events and is automatically
done in a chronological way.
ALL ATR

It is not necessary to order the procedure because all the actions are already achieved. PF will
directly ask for the checklist.
Example:
After take-off, the procedure is triggered by the CLIMB SEQUENCE.
For approach phase, the procedure is triggered by QNH SETTING.
Before landing, the procedure is triggered by the FLAPS SET FOR LANDING.

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There are 2 ways to execute a procedure:

SCANS enable the checking of all PBs,

switches and lights on the panel.

They are executed:

from memory

following a logical way (upward).

Example:
Preliminary cockpit preparation

ALL ATR
FLOWS enable a predetermined order for
actions.

They are executed:

from memory

following a specific order.

A flow is a reminder of the task sequence.

Example:
Climb sequence flow

FOR TRAINING ONLY

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2.5. Checklist Methodology / Challenge and Reply

CHALLENGE AND REPLY concept: PNF reads C/L, PF answers.
Checklist use:

On the ground In flight

C/L is requested by CM1 C/L is requested by PF

C/L is read by CM2 C/L is read by PNF

PNF announces C/L title, reads the C/L, asking questions.

When C/L is completed, PNF announces C/L complete
The answer must be in compliance with the C/L and adapted to the present situation.
PNF must receive the correct answer before reading the next item. If not, PNF must repeat the
same item.
If and when a checklist is interrupted, reading must be resumed one step before the last read
item.
PF and PNF task sharing must comply with following orders and announcement:
ALL ATR

Flight events PNF PF

APPROACH REQUEST AND ANSWER

procedure APPROACH CHECKLIST
complete ANNOUNCE AND READ
APPROACH CHECKLIST

Approach checklist 6.01

SEAT BELTS............................ON
ALTIMETERS........SET AND CHECK
CABIN ALTITUDE.................CHECK

ANNOUNCE
CHECKLIST COMPLETE

REMARKS:
To have a standard documentation common to all ATR series, some C/L items in QRH are stated
in a general way and identified by SET
Example: FLAPS..........SET
To ensure good crew coordination and communication, it is necessary to announce the exact
value of the setting.
Example: FLAPS...........15
Values or conditions must be announced as and when changes occur.

FOR TRAINING ONLY

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2.6. Task sharing

A flight is divided into several flight phases. For each phase, the crew tasks are explained in the
procedures hereafter.

TRIGGERED
FLIGHT EVENTS PROCEDURES CHECKLIST
BY

Arrival at the aircraft Flight preparation procedure CM1 / CM2

CM2 enters the cockpit Internal inspection procedure CM2

Internal inspection External inspection

CM1
complete procedure

Internal inspection Preliminary cockpit

CM2
complete preparation procedure
Preliminary
Preliminary cockpit preparation cockpit
procedure complete preparation CM1 / CM2
checklist

ALL ATR
Preliminary cockpit preparation C/L Final cockpit preparation
CM1
complete procedure

Final cockpit
Final cockpit preparation procedure
preparation CM1
complete
checklist

Ready to start engine 2 in hotel

Before propeller rotation CM1
mode
Before propeller
Before propeller rotation procedure
rotation CM1
complete
checklist

Start up clearance receive Before taxi procedure CM1

Before taxi
Before taxi procedure complete CM1
checklist

On taxiway Taxi procedure CM1

Taxi procedure complete Taxi checklist CM1

Approaching holding point and

Before take-off procedure CM1
"cabin ok" received

Before take-off
Before take-off procedure complete CM1
checklist

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TRIGGERED
FLIGHT EVENTS PROCEDURES CHECKLIST
BY

Reaching acceleration altitude Climb sequence PF

After take-off
Altimeters setting performed PF
checklist

Crossing FL 100 FL 100 procedure No C/L PF

Reaching cruise speed Cruise procedure No C/L PF

10 minutes before T.O.D Before descent procedure PF

Arrival briefing complete Descent checklist PF

Crossing FL 100 FL 100 procedure No C/L PF

When cleared to an altitude or

Approach procedure PF
ALL ATR

passing transition level

Approach procedure complete Approach checklist PF

Clear for approach Before landing procedure PF

Before landing
Landing configuration PF
checklist

Runway vacated After landing procedure CM1

After landing
When engine 1 is stopped CM1
checklist

Marshaller in sight Parking procedure CM1

Parking procedure complete Parking checklist CM1

Leaving the aircraft

All documentation filled CM1
procedure

Leaving the aircraft Leaving the aircraft

CM1
procedure complete checklist

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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3. Specific procedures

3.1. Auto Flight Control System (AFCS)

ADU (Advisory Display Unit)

ADVISORIES SELECT ALT

TCS ENG ALT SEL ---------FT
CAT 1 ALT SEL 3000 FT
CAT 2

ADVISORIES SELECT ALT

MESSAGES
ARMED MODE
LATERAL MODES CAPTURED MODE VERTICAL MODES
ARMED and CAPTURED ARMED and CAPTURED
MODES MODES

HDG SEL LO ALT ALT* ALT

HDG SEL HI IAS --- KTS
VOR VOR* VOR IAS 160 KTS
LNAV LNAV VS ---- FPM
LOC LOC* LOC VS - 600 FPM
HDG HOLD GS GS* GS

ALL ATR
BC BC* BC GA

NAV (VOR, LOC and LNAV) and APP modes must be associated with High Bank speeds.

Mode selection is achieved by acting on the corresponding PB on the AFCS control panel except
for ALT SEL mode and GO-AROUND mode.

Note: Simultaneously armed modes are limited to one lateral mode and two vertical modes.
Therefore vertical armed modes are working in the following priority sequence:

1. ILS GS ARMED

2. ALT SEL ARMED

Any change on ADU from an armed mode (white) to a capturing mode (star) or from a capturing
mode (star) to a captured mode (green) must trigger a crew cross control on the FMA (Flight Mode
Announciator).

Flight director modes are

displayed on the FMA

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3.1.1. With AP engaged

AP may be set by PF or by order to PNF.

AP ENGAGED
PF acts on AFCS

All track and navigational changes on the AFCS are performed by the PF with the following
method:

When the PF has completed his action, he informs the PNF by using the word SET at
the end of his call out.
ALL ATR

PNF checks the displayed mode and announces CHECK.

GENERAL PHILOSOPHY:

Any ...SET is done via ADU by PF if autopilot ON, or PNF if not.

Any CHECK is done via FMA. Any FMA status change must be announced.

REMARK:

If the PF is busy, he can request the setting from the PNF.

Note:

A climb or descend action must be done with the entire following sequence:
1) Select ALT SEL
2) Select and adjust vertical mode (usually IAS for climb and VS for descent)
3) Adjust Np and power as needed.
4) Change altimeter barometric setting and compare (please refer to 01.03 p.18, altimeter
setting)
5) Select speed bug.

The IAS mode must be used during climb (to avoid any stall due to high altitude and low aircraft
performance). During descent, the VS mode is mainly used (except in emergency descent where
IAS mode is used). The basic (pitch) mode may be used in accordance with the commercial
company policy in effect.

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Climb mode (AP ON)

ALL ATR
HDG ALT HDG ALT IAS HDG ALT* HDG ALT

Flight events PNF PF

DO
CLeared to FL 180 ALT SEL......................... 18000 SELECTED
IAS . .......................... 160/170 SELECTED
TORQUE / NP.................... CLIMB SETTING

ANNOUNCE
FL 180, IAS 160 (/170) SET ALT WHITE*
ANNOUNCE
CHECK

alt star ANNOUNCE

ALT STAR

ANNOUNCE
CHECK
alt green ANNOUNCE
ALT GREEN
ANNOUNCE
CHECK

* ALT white appears only when a vertical mode is armed and the aircraft is climbing or descending
towards the preselected altitude / FL.

Note: In a simultaneous setting situation, only one announcement can be made.

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Descent mode (AP ON)

ALL ATR

HDG ALT HDG ALT VS HDG ALT* HDG ALT

Flight events PNF PF

DO
CLeared to FL 060 ALT SEL.......................... 6000 SELECTED
VS . ...............................-1500 SELECTED
TORQUE / NP................. TORQUE SETTING
ANNOUNCE
FL 60 SET
ALT WHITE, VS -1500 SET
ANNOUNCE
CHECK

alt star ANNOUNCE

ALT STAR
ANNOUNCE
CHECK
alt green ANNOUNCE
ALT GREEN

ANNOUNCE
CHECK

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NAV mode (AP ON)

ALL ATR
HDG ALT VOR HDG ALT VOR* ALT VOR ALT

Flight events PNF PF

DO
CLeared to HDG BUG................................... SET 045
INTERCEPT RADIAL
270 ANNOUNCE
HDG BUG LEFT 045 SET
ANNOUNCE
CHECK
DO
ESTABLISHED ON NAV MODE.............................. SELECTED
INTERCEPTION
HEADING
ANNOUNCE
NAV MODE SET, VOR WHITE
ANNOUNCE
CHECK

VOR STAR ANNOUNCE

VOR STAR
ANNOUNCE
CHECK

VOR GREEN ANNOUNCE

VOR GREEN
ANNOUNCE
CHECK

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HDG mode (AP ON)

ALL ATR

VOR ALT HDG ALT

Flight events PNF PF

CLeared to DO
HEADING 130 HDG MODE...............................SELECTED

ANNOUNCE
HDG MODE LO (or HI) BANK SET*

ANNOUNCE *HI or LO according to flight conditions.

CHECK

HEADING SELECTION
DO
HDG BUG.......................... 130 SELECTED

ANNOUNCE
HDG BUG RIGHT 130 SET
ANNOUNCE
CHECK

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APP mode (AP ON)

LOC HDG GS ALT LOC* GS ALT LOC GS* LOC GS

ALL ATR
Flight events PNF PF

CLeared to DO
perform an ils APP MODE...........................SELECTED
approach
ANNOUNCE
LOC AND GS WHITE
ANNOUNCE
CHECK

localiser star
ANNOUNCE
ANNOUNCE LOC STAR
CHECK

localiser green ANNOUNCE

ANNOUNCE LOC GREEN
CHECK

glide slope star ANNOUNCE

ANNOUNCE GS STAR
CHECK

glide slope green ANNOUNCE

ANNOUNCE GS GREEN
CHECK

FOR TRAINING ONLY

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GA mode (AP ON)

FD / AP displays are the same
for all ATRs.
The shown procedure applies
to 42 not PEC. For others,
please refer to 2.03 p. 59,
go-around.

When GA PB depressed,
autopilot is automatically
disconnected

LOC GS HHLD GA HDG ALT IAS

Flight events PNF PF

FULLY established ANNOUNCE
LOC GREEN, GS GREEN
ANNOUNCE
CHECK
ORDER
at da or mda GO-AROUND, SET POWER, FLAPS ONE NOTCH

DO
DO GA PB ON PL.........................DEPRESSED
TQs..............................CHECK/ADJUST GA ROTATE............... GA PITCH (+8 NOSE UP)
FLAPS 15..................................SELECTED PLs...............ADVANCED TO WHITE MARK
when flaps at CAVALRY CHARGE..................................CANCEL
15 on the flaps ANNOUNCE
indicaTor FLAPS 15, POWER SET

when positive ANNOUNCE ORDER

climb on the vsi POSITIVE RATE GEAR UP, SET HEADING, LOW BANK, IAS
VGA
DO
GEAR LEVEL......................................... UP
42 not PEC

HDG MODE................................SELECTED
LO BANK...................................SELECTED
IAS.................................... VGA SELECTED
TAXI & T/O LIGHT..................................OFF

ANNOUNCE ANNOUNCE
IAS XXX SET CHECK

when all lights ANNOUNCE

extinguished on GEAR UP
the ldg gear panel

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3.1.2. With AP disengaged (flying manually following FD bars)

AP DISENGAGED
PNF acts on AFCS on PF request

All track and navigation changes on AFCS are performed by the PNF, at the PF's request.

To avoid repetition, heading or altitude clearance are set and announced by the PNF without a PF
order. All flight parameters (speed bug, altimeter setting) are set by both pilots after PFs request.

1. PF orders the action by starting his sentence with the word SET

2. PNF informs PF after performing the action, concluding his sentence by SET

3. PF announces CHECK after checking the FMA and/or ADU

ALL ATR

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Climb mode (AP OFF)

ALL ATR

HDG ALT HDG ALT IAS HDG ALT* HDG ALT

Flight events PNF PF

ORDER
CLeared to FL 180 SET FL 180, IAS 160
DO
ALT SEL......................... FL 180 SELECTED
IAS............................ 160 / 170 SELECTED

ANNOUNCE ANNOUNCE
FL 180, IAS 160/170 SET, ALT WHITE CHECK
CHECK OR ADJUST PWR LEVER TO AMBER TQ BUGS

alt star
ANNOUNCE ANNOUNCE
ALT STAR
CHECK
ANNOUNCE
alt green ALT GREEN
ANNOUNCE
CHECK

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

Descent mode (AP OFF)

ALL ATR
HDG ALT HDG ALT VS HDG ALT* HDG ALT

Flight events PNF PF

ORDER
CLeared to FL 60 DO SET FL 60, VS - 1500
ALT SEL........................ FL 060 SELECTED
VS.................................. 1500 SELECTED

ANNOUNCE
FL 60, VS - 1500 SET, ALT WHITE
ANNOUNCE
CHECK

alt star ANNOUNCE

ALT STAR
ANNOUNCE
CHECK
alt green ANNOUNCE
ALT GREEN
ANNOUNCE
CHECK

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

NAV mode (AP OFF)

ALL ATR

HDG ALT VOR HDG ALT IAS VOR* ALT VOR

Flight events PNF PF

ORDER
CLeared to SET HEADING BUG LEFT 045
INTERCEPT RADIAL DO
270 HDG BUG........................................... 045

ANNOUNCE
HEADING BUG 045 SET
ANNOUNCE
CHECK

ESTABLISHED ON ORDER
INTERCEPTION SET NAV MODE
HEADING
DO
NAV MODE................................SELECTED

ANNOUNCE
NAV MODE SET, VOR WHITE
ANNOUNCE
CHECK

VOR STAR
ANNOUNCE ANNOUNCE
VOR STAR
CHECK

VOR GREEN
ANNOUNCE ANNOUNCE
VOR GREEN
CHECK

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

HDG mode (AP OFF)

ALL ATR
VOR ALT HDG ALT

Flight events PNF PF

CLeared to ORDER
HEADING 130 SET HEADING MODE
DO
HDG MODE................................SELECTED

ANNOUNCE
HEADING LOW (or HI) BANK SET* ANNOUNCE
*HI or LO according to flight conditions. CHECK

ORDER
SET HEADING BUG RIGHT 130
DO
HDG MODE.........................130 SELECTED

ANNOUNCE
HEADING BUG 130 SET

ANNOUNCE
CHECK

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

APP mode (AP OFF)

LOC HDG GS ALT LOC* GS ALT LOC GS* LOC GS

ALL ATR

Flight events PNF PF

ORDER
CLeared to SET APPROACH MODE
perform an ils DO
approach APP MODE................................SELECTED

ANNOUNCE
APPROACH MODE SET, LOC AND GS WHITE ANNOUNCE
CHECK

loc star ANNOUNCE

LOC STAR
ANNOUNCE
CHECK
loc green ANNOUNCE
LOC GREEN
ANNOUNCE
CHECK
gs star ANNOUNCE
GS STAR
ANNOUNCE
CHECK
gs green ANNOUNCE
GS GREEN
ANNOUNCE
CHECK

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

GA mode (AP OFF)

LOC GS HHLD GA HDG ALT IAS

ALL ATR
Flight events PNF PF
FULLY established ANNOUNCE
LOC GREEN, GS GREEN
ANNOUNCE
CHECK
ORDER
at da or mda GO-AROUND, SET POWER, FLAPS ONE NOTCH

DO
DO GA PB ON PL.........................DEPRESSED
TQs............................. CHECK/ADJUST GA ROTATE............... GA PITCH (+8 NOSE UP)
FLAPS 15................................. SELECTED PLs...............ADVANCED TO WHITE MARK
when flaps at CAVALRY CHARGE..................................CANCEL
XX on the flaps
indicaTor ANNOUNCE
FLAPS XX, POWER SET
Note: ATR 42-500 SEE 02.02.03 page 96

when positive ANNOUNCE

climb on the vsi POSITIVE RATE ORDER
GEAR UP, HEADING, LOW BANK, IAS VGA
DO
GEAR LEVEL......................................... UP
HDG MODE............................... SELECTED
LOW BANK............................... SELECTED
IAS.................................... VGA SELECTED
TAXI & T/O LIGHT................................. OFF

ANNOUNCE
IAS XXX SET ANNOUNCE
CHECK
when all lights
ANNOUNCE
extinguished on
the ldg gear panel
GEAR UP ANNOUNCE
CHECK

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

3.2. Flaps use

For system use in normal operations, any setting change shall be performed through the cross
control concept:

PF: orders system action.

PNF: performs the action and announces the configuration when the setting is in
compliance with the system indicator

Flaps manoeuvers are always performed by the PNF under PF order. PNF checks the speed
before each configuration change then performs the task and announces the new configuration.

Example:
ALL ATR

Flight events PNF PF

flaps extension ORDER
FLAPS XX
ANNOUNCE
SPEED CHECK

DO
FLAPS LEVER............................SELECTED

FLAPS AT XX ON THE
FLAPS INDICATOR ANNOUNCE
FLAPS XX
ANNOUNCE
CHECK

Note: Select new speed only when the new configuration is obtained, during deceleration.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

3.3. Landing gear use

For system use in normal operations, any setting change shall be performed through the cross
control concept:

PF: orders system action.

PNF: performs the action and announces the configuration when the setting is in
compliance with the system indicator

Gear manoeuvers are always performed by the PNF under PF order. PNF checks the speed
before each configuration change then performs the task and announces the new configuration.

Example:

ALL ATR
Flight events PNF PF
landing gear ORDER
extension GEAR DOWN
ANNOUNCE
SPEED CHECK

DO
LANDING GEAR LEVEL.....................DOWN
PWR MGT...................................TAKE-OFF
TAXI & T/O LIGHTS................................ ON

3 GREEN LIGHTS ON ANNOUNCE

THE LANDING GEAR GEAR DOWN
INDICATOR ANNOUNCE
CHECK

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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PROCEDURES JUN 09

3.4. Altimeter and radioaltimeter setting

3.4.1. Altimeter setting

PF and PNF altimeter settings must be identical. Any change shall be performed with a specific
call and cross control.
Example: cleared down to an altitude with QNH 1015

Flight events PNF PF

QNH setting ORDER
SET QNH

DO DO
QNH 1015...........................................SET QNH 1015..........................................SET

ANNOUNCE
1015 SET
desired altitude
ANNOUNCE
XXXX FT, NOW
CHECK
CHECK
If difference less than 50 feet
or
XX FT
ALL ATR

If difference more than 50 feet

* XXXX is the altimeter value: expressed in feet for QNH setting.

expressed in Flight Level for standard setting.

For each flight phase, the altimeter setting must be in compliance with the following table.

Note: Settings may vary, depending on prevailing local regulations.

ALTIMETERS

FLIGHT PHASE
CAPTAIN STANDBY FIRST OFFICER

From ground till QNH QNH QNH

cleared to FL (departure airport) (departure airport) (departure airport)

From climb to FL till STANDARD QNH STANDARD

cleared down to altitude Regional

Cleared to altitude QNH QNH QNH

(arrival airport) (arrival airport) (arrival airport)

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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PROCEDURES JUN 09

Altimeter bugs (if installed)

Bug setting must be the same on the captain's and the first officer's side.

Take-off

Example: Acceleration altitude = 1000 ft (white bug)

Airport elevation = 500 ft (red bug)

Acceleration altitude

Airport elevation

ALL ATR
Landing

Example: - DA or MDA = 700 ft (white bug)

- Airport elevation = 500 ft (red bug)
Decision altitude (DA) or (MDA)

3.4.2. Radioaltimeter Setting Airport elevation

DH policy
Used for CAT II approach.
May be set under CAT I approach, by both the PNF and PF together, and for information only (i.e.
not to be used as a reference).
Never used for non precision approach.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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PROCEDURES JUN 09

3.5. Speed bugs

Setting

The PF and PNF speed bug settings must be identical.

Any setting change shall be performed with a specific call out and cross control.
Example: After filling the landing data card, ready to set speed bug.

Flight events PNF PF

Landing data card ANNOUNCE
proceeding VGA 103

DO DO
YELLOW BUG............................SELECTED YELLOW BUG...........................SELECTED

ANNOUNCE
103 SET ANNOUNCE
WHITE BUG 131

DO DO
WHITE BUG...............................SELECTED WHITE BUG..............................SELECTED

ANNOUNCE
131 SET ANNOUNCE
RED BUG 145
ALL ATR

DO DO
RED BUG...................................SELECTED RED BUG..................................SELECTED

ANNOUNCE
145 SET

Speed bug

When aircraft configuration is obtained, PF orders new speed bug setting according to flight phase,
on both sides. Speed bug manages Fast / Slow speed scale and must be considered also as
a cross-check tool.

Example:

Flight events PNF PF

ACCELERATING TO ANNOUNCE
160 KT SPEED BUG 160

DO DO
SPEED BUG...............................SELECTED SPEED BUG............................. SELECTED

ANNOUNCE
SET

FOR TRAINING ONLY

 Green bug V1 Set when V1 = VR (When runway limited (set at 12 o'clock when not used))

Yellow bug VR When limiting runway

V1/VR When non limiting runway

3.5.1. Take-off bugs

V2
Speed bug

Normal conditions Icing conditions

White bug FLAPS RETRACTION SPEED (VmLB0)

Single engine climb
Best climb angle speed Flaps 0 speed Flaps 15
Single engine climb speed Flaps 0 (VmLB15)

White bug + 10 kt

FOR TRAINING ONLY

HIGH BANK (VmHB0)
PROCEDURES
NORMAL PROCEDURES

Best climb rate speed Flaps 0

FLAPS
Red bug RETRACTION
SPEED (VmLB0)
INTRODUCTION TO NORMAL

Red bug + 10 kt HIGH BANK

VmLB: minimum speed LOW BANK (HDG SEL LO on ADU)
Page 21

VmHB: minimum speed HIGH BANK (HDG SEL HI on ADU)

01.03

JUN 09
01

ALL ATR
 ALL ATR

Normal conditions Icing conditions

DRIFT DOWN
3.5.2. Cruise bugs

DRIFT DOWN SPEED Flaps 0

White bug SPEED Flaps 15
MINI EN ROUTE (VmLB0)
(VmLB15)

MINI EN ROUTE
PROCEDURES
NORMAL PROCEDURES

Red bug
Flaps 0 (VmLB0)

FOR TRAINING ONLY

INTRODUCTION TO NORMAL
Page 22

Speed bug Cruise speed

01.03

JUN 09
01
 VGA = Greatest:
Yellow bug VAPP no wind + 5 kt
or
1,1 Vmca

VAPP= VAPP no wind +

Speed bug
wind factor
3.5.3. Approach bugs

Normal conditions Icing conditions

FLAPS RETRACTION SPEED (VmLB0) Single engine climb

White bug
Best climb angle speed Flaps 0 speed Flaps 15
Single engine climb speed Flaps 0 (VmLB15)

White bug +10 kt HIGH BANK (VmHB0)

FOR TRAINING ONLY

Best climb rate speed Flaps 0
PROCEDURES
NORMAL PROCEDURES

FLAPS
Red bug RETRACTION
SPEED (VmLB0)
INTRODUCTION TO NORMAL

Red bug +10 kt HIGH BANK

VmLB: minimum speed LOW BANK (HDG SEL LO on ADU)
Page 23

VmHB: minimum speed HIGH BANK (HDG SEL HI on ADU)

01.03

JUN 09
01

ALL ATR
 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
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3.5.4. Best angle and best rate speed

2 ENGINES 1 ENGINE
BEST ANGLE:
WHITE BUG

NORMAL WHITE BUG

CONDITIONS FLAPS

BEST RATE: 0 0
WHITE BUG +10

0 15

ICING
RED BUG WHITE BUG
CONDITIONS
ALL ATR

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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3.6. Torque bugs

3.6.1. Take-off bugs

Take-off torque bug (TO)

(Manually set)

Reserve take-off torque bug (RTO)

(set by FDAU)

Example: Airport pressure altitude is 1000 ft and OAT is 10C.

ALL ATR

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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3.6.2. Cruise bugs OPS DATA

4.41
Eng : PW120
MAR 98 001

16 t
Speeds Normal Icing
NON LIMITING RWY
V1 = VR 100 109
TAKEOFF
V2 106 115
FLAPS 15 Cruise torque bug, automatically
127 computed127by the FDAU.
FINAL TAKE OFF
(Flaps 0) (Flaps 15)
127
DRIFT DOWN
127 (Flaps 15)
VmLB
(Flaps 0) 148
MINI EN ROUTE
(Flaps 0)
FINAL VmHB
The FDAU torque is checked in the cruise performance 102
chart. 120
APPROACH (Flaps 30)
MAX CRUISE 2 ENGINES
FLIGHT ISA
LEVEL 10 5 0 +5 +10 +15 +20
90.0 90.0 90.0 90.0 90.0 90.0 84.8 90.0 79.5 88.7 74.4 83.0 69.4 77.5
343 317 343 317 343 318 328 318 313 314 298 299 283 283
80
ALL ATR

235 225 234 224 233 223 227 222 220 220 213 213 206 206
259 248 260 249 261 250 257 252 252 251 246 245 240 239
90.0 90.0 90.0 90.0 87.3 90.0 82.0 90.0 77.1 86.0 72.2 80.5 67.5 75.3
336 312
100 233 223
337
231
312
222
329
228
313
221
314
221
313
220
300
215
302
215
286
208
287
208
272
201
273
201
264 253 265 254 263 256 258 257 253 253 248 247 242 241
90.0 90.0 89.5 90.0 84.5 90.0 79.2 88.3 74.4 83.0 69.9 77.9 65.5 73.0
120 330
230
307
221
329
229
307
220
315
222
308
219
300
216
304
216
287
209
289
209
273
203
275
202
261
196
262
195
269 259 270 260 265 261 260 260 254 255 249 248 243 242
90.0 90.0 85.9 90.0 81.2 90.0 76.5 85.3 71.6 79.9 67.4 75.1 63.2 70.5
325 302 313 303 300 303 287 291 273 276 261 263 249 250
140 228 218 222 217 216 216 210 210 203 204 197 197 191 190
274 263 271 264 266 266 261 261 255 255 250 249 243 242
86.8 90.0 82.1 90.0 77.4 86.3 73.0 81.3 68.5 76.4 64.0 71.3 60.1 66.9
160 311
222
298
216
297
216
299
214
284
210
289
210
272
203
276
204
259
197
262
197
246
190
248
189
235
183
236
182
276 268 271 269 266 266 261 261 255 255 248 247 242 240
81.5 90.0 77.2 86.0 73.0 81.4 69.0 76.9 65.1 72.6 61.1 68.1 57.2 63.7
290 295 278 284 266 271 255 259 245 248 233 235 222 223
180 214 213 208 208 202 202 196 196 190 189 183 181 175 174
274 273 270 269 265 264 259 259 254 253 247 245 239 238
76.8 85.5 73.0 81.3 69.1 77.0 65.3 72.8 61.6 68.6 58.1 64.7 54.5 60.7
273 279 262 267 250 255 240 244 230 233 220 222 210 211
200 206 206 200 200 195 194 188 188 182 181 175 174 167 166
272 272 268 268 263 263 258 257 251 250 244 243 236 234
72.0 80.3 68.5 76.3 65.0 72.4 61.5 68.4 58.1 64.6 54.7 60.9 51.5 57.3
256 262 245 250 235 240 225 229 216 219 206 209 197 199
220 197 197 191 191 186 185 179 179 173 171 165 164 157 156
270 270 265 265 260 259 254 253 247 245 239 237 230 228
65.9 73.4 63.9 71.2 60.6 67.5 57.5 63.9 54.3 60.3 51.2 56.8 48.0 53.2
235 240 229 234 219 224 210 214 201 204 192 194 183 185
240 186 186 182 182 176 175 169 168 162 160 154 152 143 139
263 263 260 260 255 254 248 246 240 237 231 227 216 211
62.9 70.0 61.1 68.0 58.4 65.0 55.3 61.5 52.3 58.1 49.2 54.5
224 229 219 224 211 216 202 206 193 196 184 186
250 180 180 176 176 170 169 163 162 156 154 146 142
259 259 256 256 251 250 243 241 235 232 223 217
TQ % NP = 86 % TQ % NP = 77 %
KG/H/ENG KG/H/ENG NP 77 %
IAS IAS NOT MECH. LIMITED
TAS TAS

Mod :

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

3.6.3. Torque preset

For the following conditions, this table shows the best torque presets.

Precise torque values will vary depending on aircraft weight and outside conditions but differences
will be very minimal.

Do not forget that Np modifies the torque for a given PL angle.

Approach
NP = 86/82% Level flight
3

Speed 180 160 140 120 VAPP

Gear UP UP DOWN DOWN DOWN

Flaps 0 0 15 30/35 30/35

All engine torque 50% 40% 40% 50% 25%

All engine pitch +1 +1 +2 +2 1

ALL ATR
Single engine torque 90% 75% 75% 90% 50%

Single engine pitch +1 +1 +2 +2 1

For profiles other than ILS and level flight, use the following equivalence:

3% Torque <=> 1 percent slope

or

5% Torque <=> 1 degree slope

or

5% Torque <=> 10 Kt of wind component

(to be able to maintain a constant ground descent gradient, the vertical speed must be adjusted
and so the speed).

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
Page 28 01
INTRODUCTION TO NORMAL
PROCEDURES JUN 09

3.7. Data card

3.7.1. Take-off data card

Data card filling

CM2 fills in take-off data card:
during "final cockpit preparation" procedure: purple labels
prior to the "before propeller rotation" procedure: green labels.

All operational data shall be cross checked by the crew on relevant documentation (QRH, FOS,
load and trim sheet...)

1 2 3 4

3
7 A 10

5
8 B
ALL ATR

C
9 11
G
D

6
12

E F

FLT N
1 Write the flight number.

2 FROM
Write the ICAO departure airport code.

3 TO
Write the ICAO arrival airport code.

DATE
4
Write the present date.

5 ATIS
Write the ATIS data.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
Page 29 01
INTRODUCTION TO NORMAL
PROCEDURES JUN 09

ICING
6 Tick the box when icing conditions prevail at take-off.

W LIM
7 Write the lowest limitation value.

OBJ TQ
8 Write the objective torque read in the QRH (page 4.11) according to the outside air
temperature and the pressure altitude.

RTO TQ
9 Write the reserve take-off torque read in the QRH (page 4.12) according to both the
outside air temperature and the pressure altitude.

ACC
10 Write the acceleration altitude for take-off.
The minimum figure must be 400 feet above airport level (AAL).

11 SINGLE ENGINE PROCEDURE

Write the single engine procedure read on the FOS chart (at least the first turn).

HDG
12 Write runway in use for take-off.

ALL ATR
After load and trim sheet proceeding:

TOW
A
Write the TOW read on the load and trim sheet and compare with W LIM

V1
B Write V1 read on the FOS if taking off on a limiting runway, or in the QRH, according to
the actual TOW, if the runway is NL.

VR
C Write VR read on the FOS if taking off on a limiting runway, or in the QRH, according
to the actual TOW, if the runway is NL.

V2
D Write V2 read on the FOS if taking off on a limiting runway, or in the QRH, according to
the actual TOW, if the runway is NL.

FINAL TO (WB)
E Write the value of Final take-off speed read in the QRH according to the normal
(VmLB0) or icing conditions prevailing (VmLB 15)

VmLB 0 (RB)
F Write the value of VmLB0 in icing conditions read in the QRH.

CG% TRIM
G Write the value of the trim setting according to the CG location in percentage of MAC
given on the load and trim sheet.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

Data card proceeding

Information proceeding from the take-off data card permits crew members to prepare the
departure and take-off briefings.

The card must be read from up to down and from left to right by the PF (5 columns), and set when
necessary (QNH, OBJ TQ, speed bugs, trim, altimeters bugs): "are you ready to proceed?".

1 2 3 4

7 10 17

5
8 11

12
9 18
16
ALL ATR

13

6
19

14 15

FLT N

1 Announce the flight number and check the FDEP.

2 FROM
Announce the ICAO departure airport code.

3 TO
Announce the ICAO arrival airport code.

DATE
4
Announce the present date.

5 ATIS
Read the ATIS data and check:
the possibility to take-off according to present RVR/Visibility and value read on the
Jeppesen chart.
the possibility to fly back to departure airport in case of engine failure. (if an
alternate airport is necessary, it must be indicated on the load and trim sheet).
wind limitations for take-off and hotel mode use.
set QNH on the 3 altimeters and cross-check the elevation readings.
temperature and moisture to determine if normal or icing conditions are prevailing.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
Page 31 01
INTRODUCTION TO NORMAL
PROCEDURES JUN 09

ICING
6 If the box is ticked, remember icing conditions prevail.

W LIM
7 Announce W LIM

OBJ TQ
8 Announce the objective torque value and set the white bugs on the torques gauges.

RTO TQ
9 Announce the reserve take-off torque value and check that amber bugs on the torque
gauges are facing the above-mentioned value.

TOW
10 Check that TOW is less than or equal to your W LIM

V1
11 Set the yellow bug on both airspeed indicators according to that value and cross-check.

VR
12 Memorize the value (if V1 and VR are different, use the green bug for V1 and the yellow
bug for VR).

V2
13 Set the amber bug on both airspeed indicators according to that value and cross-
check.

ALL ATR
14 FINAL TO (WB)
Set white bug on both airspeed indicators according to that value and cross-check.

VmLB 0 (RB) (Icing)

15 Set red bug on both airspeed indicators according to that value and cross-check.

16 CG% TRIM
Set the pitch trim and check it remains inside the green arc.

17 ACC
Set the white bug on both altimeters according to that value.

18 SINGLE ENGINE PROCEDURE

Confirm the single engine procedure according to weather conditions.

HDG
19 Check the runway in use given on ATIS.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

3.7.2. Landing data card

Data card filling-in

The landing data card must be filled in by the PF prior to the arrival briefing.

it is done from up to down and from left to right.

1 2 3 4

7 11 17

5
8 12

18
13
9
ALL ATR

10 14

6
19

15 16

FLT N

1 Write the flight number.

2 DESTINATION
Write the ICAO destination airport code.

3 ALT
Write the destination airport elevation.

ALTERNATE
4
Write the ICAO alternate airport code.

ATIS

5 Write the ATIS data.

ICING

6 Tick the box if icing conditions are prevailing at landing.

W LIM
7 Write the limiting weight for landing.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
Page 33 01
INTRODUCTION TO NORMAL
PROCEDURES JUN 09

GA TQ

8 Write the value of the GA TQ read in the QRH (page 4.13).

9 1.1 VMCA
Write the value read in the QRH (page 4.64).

10 VGA
Write the VGA value: highest value between: - 1.1 VMCA, or
- VAPP no wind + 5 Kt.
LW
11
Write the calculated LDG weight and compare with W LIM

12 FLAPS
Write the flaps value.

13 VAPP no wind
Write the value of VAPP no wind read in the QRH (on the final approach speed line).

14 VAPP
Write the value of VAPP=VAPP no wind + wind factor.
Wind factor = the highest value between: - 1/3 of reported headwind, or
- the gust in full.

}
Max. correction: 15 kt
15 VmLB (WB)
Write the value found in the QRH: - VmLB 0 in normal conditions

ALL ATR
- VmLB 15 in icing conditions.

16 VmLB 0 (RB) (Icing)
Write the value found in the QRH: - VmLB 0 in icing conditions.

17 ACC
Write the acceleration altitude for the go-around procedure.
The highest value between: - 1000 feet AAL, or
- the value specified on Jeppesen chart, or
- a specific computation.

GO-AROUND
18 PROCEDURE
Draw the first segment of the go-around procedure (first heading, first altitude, first turn).

19 HDG
Write the runway in use on the destination airport.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
Page 34 01
INTRODUCTION TO NORMAL
PROCEDURES JUN 09

Data card proceeding

The landing data card must be proceeded by the PF prior to the arrival briefing: "Are you ready
to proceed?".

It is done from up to down and from left to right.

1 2 3 4

7 11
17
5
8 12

18
13
9

10 14
ALL ATR

6
19

15 16

1 FLT N
Announce the flight number.
2 DESTINATION
Announce the ICAO destination airport code.
ELEV
3 Set the red bugs on PF and PNF altimeters.
4 ALTERNATE
Write the ICAO alternate airport code.
5 ATIS
Read the ATIS data and check:
- visibility or RVR value to determine airport's accessibility
- instrument approach in use
- wind limitations for landing
- QNH and set it on the standby altimeter
- temperature to determine if normal or icing conditions are prevailing.
6 ICING
If the box is ticked, remember icing conditions prevail for landing.
W LIM

7 Announce W LIM value.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
Page 35 01
INTRODUCTION TO NORMAL
PROCEDURES JUN 09

GA TQ

8 Announce the go-around torque value and set white bugs on torque gauges.

1.1 VMCA
9 Announce the value of 1.1 VMCA

VGA
10 Set yellow bugs on the airspeed indicators according to that value.

LW
11 Check that LW is less or equal than W LIM..

FLAPS
12 Announce flaps setting for landing.

VAPP no wind
13 Announce the value of VAPP no wind.

VAPP
14 Announce and memorize the value of VAPP.

VmLB (WB)
15 Set white bugs on airspeed indicators according to that value and crosscheck.

VmLB 0 (RB) (Icing)

16 Set red bugs on airspeed indicators according to that value and crosscheck.

ALL ATR
ACC
17 Set white bugs on main altimeters according to that value.

GO-AROUND PROCEDURE
18 Describe the first segment of the go-around procedure.

RWY
19 Announce and set ALTI BUGS (if installed): red on threshold elevation, white on MDA

Example: First-officer will be PF in flight, so he performs the data card proceeding:

We'll be landing at xxxx, elevation xxx ft, alternate is xxxx. Information x (if ATIS received) recorded at
xx.xx, runway in use xx, wind is xxx/xx kt (check wind limitation), ceiling xxx and visibility xx (check pro-
cedure minima), temperature is xx , QNH is xxxx hPa set on stand by altimeter, normal/icing condi-
tions, MLW is xx,x tons, LW is xx, x t (check LW<MLW), GA TQ xxx% set (set on torque indicator), VGA is
xxx kt, white bug is xxx kt, red bug isxxx kt (set on both ASI, CPT and FO), with flaps XX Vapp is xxxkt.
Missed approach procedure is reported, and acceleration altitude is xxxx ft

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

3.8. Briefing

3.8.1. Departure briefing

All departure settings must be ready before performing briefing.

"Are you ready for the departure briefing?"

Status

Weather conditions (icing, thunderstorm, wind...)

Aircraft technical situation (technical concern, MEL restriction...)

Specific flight items (NOTAMs, de-icing...)

Taxi

Taxi out description

Specifics (contamination, taxiway closed...)

Runway in use and expected holding point

Runway
1
Limitations, specifications, bleed, anti-icing
ALL ATR

(fluid type...)
3
SID (Standard Instrument Departure)
2

5
1 Jeppesen chart N __ & date __

2 SID name

3 MSA

4 Flight path description:
1 - routing
2 - first FL or altitude
3 - climb gradient
4
5 Radio navigation setting

Active frequency + associated course
Standby frequency (if necessary)
DME hold (if necessary)
RMI: VOR and / or ADF

6 RNAV setting:
If equipped (HT 1000 or certified GPS
receiver) check SID inserted in FPL for cross
check operation.

"If no question, departure briefing complete"

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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3.8.2. Departure clearance

When clearance departure is received from ATC, you must check it is in compliance with the
expected SID:

a - Is actual SID in compliance with the prepared one?

b - Is altitude clearance in compliance with MSA / SID climb instruction?

c - Set squawk code.

If clearance is amended, reorganize and describe new radio-navigation setting and limitations.

If clearance is not amended, PF announces: "no change".

3.8.3. Take-off briefing

"Take-off RWY _____, Weight _____, V1 ______

If failure before _____ kt, I (you) stop the aircraft.

If failure at or after _____ kt, we continue HDG _____, acceleration altitude is _____, MSA is

ALL ATR
_____"

The single engine flight path shall be read on FOS chart.

Example: First officer will be PF in flight, so he performs the take-off briefing:

"Are you ready for take-off briefing?... Take-off runway 32L, weight 16 tons, V1 100 kt , normal/
icing condition
If failure before V1, you call STOP and stop the aircraft
If failure at or after V1, we continue runway heading until 1000 ft, acceleration altitude, then right
turn TOE climbing 4000 ft, MSA is 3000 ft,
If no question, briefing complete".

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

3.8.4. Arrival briefing

Top of descent (TOD)

expressed in distance (time for information) and MSA.

Particularities:

Icing or normal conditions

NOTAM
3
Airport equipment failure...

Etc...
2
Alternate & holding time:

Holding time before diversion

Weather at destination: 8

4
1 Visi / RVR compared to minima: 5
ALL ATR

airport accessible or not and icing or normal speeds.

Approach procedure:

2 Jeppesen chart N __ & date __

3 Type of approach

4 MSA according to the arrival sector.

5 Flight path and description

6 Descend interception: 6
- altitude
- distance
- stabilization point
7 Minima

8 Go-around procedure 7

Radio-navigation setting:

for the final approach.

Example
"Are you ready for arrival briefing?... Top of descent is 50 DME from BMC at 1456, MEA is 5000 ft.
Landing in Bordeaux in normal conditions, without Approach Lights. Holding time before diverting
to LFBA is 20'. We have the minima for an ILS runway 23, chart 11-1 of November 14th, effective
27th. MSA is 2100ft within 25 NM of BMC. From LIBRU, standard arrival to reach 3000 ft to inter-

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

cept localizer. We leave 3000 ft at D9 to pass D4 DB at 1420 ft Stabilization altitude is 1200 ft

Decision altitude is 360 ft (set on alti bug) and decision height is 200 ft (set at DH) "SET RIGHT" /
"SET LEFT". In case of a go-around we climb straight ahead D4 DME DB, then right turn heading
042 following standard track up to 4000 ft. (check frequencies), NAV 2 ILS active, VOR stand-by,
both ADF on BE frequency (check), RMI keys on ADF. After landing we vacate second left (and
etc... if needed). If no question, briefing complete.

3.9. Navigation policy

3.9.1. Definitions

En route navigation airspaces are now widely organized on the basis of the RNAV (Area Navigation)
concept.

RNAV can be defined as a method of navigation that permits aircraft operation on any desired
course within the coverage of station-referenced navigation signals or within the limits of a self
contained system capability, or a combination of these.

RNAV navigation is now commonly used for departure and arrival flight phases with more stringent
procedures and a better level of accuracy.

RNAV operations permit flight in any airspace without the need to fly directly over ground-based
aids.

ALL ATR

Area Navigation Route

Flying in RNAV airspaces require additional navigational aircraft capabilities in terms of performance
monitoring and alerting.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

ATR aircraft have different levels of performance and capabilities depending on their RNAV
navigation system equipment and level of certification.
ATR navigation systems (KLN 90 and HT1000) are based on GPS signals or GPS + DME signals.
Latest HT1000 installations allow to fly departure, en route, arrival track in RNAV designated area
and to conduct non-precision approach on specific GNSS RNAV procedure. Refer to the aircraft
AFM to check RNAV capabilities.
Crew qualification is required to conduct RNAV procedures.
Example of local specifications:
B-RNAV for enroute navigation / P-RNAV for TMA departure and arrival procedures

B-RNAV: The Basic Area Navigation (B-RNAV) was introduced to enable en route capacity gains
to be achieved with minimal aircraft capacity. It requires aircraft conformance to a track-keeping
accuracy of 5NM for at least 95% of flight time.

P-RNAV: The Precision Area Navigation (P-RNAV) was introduced for RNAV applications in terminal
airspace. It requires aircraft conformance to a track-keeping accuracy of 1NM for at least 95% of
flight time.

In this chapter:
conventional radio navigation equipment or method refers to the use of VOR/LOC,DME and ADF
RNAV navigation refers to the use of HT1000 GNSS or KLN 90 GPS receiver or any other RNAV
ALL ATR

equipment.

3.9.2. General
CM2 initiates power up, set up and verifications of the navigation equipments during the preliminary
cockpit preparation procedure.

PF performs flight plan and performance data insertion in RNAV system, and VOR, DME, ADF
settings during final cockpit preparation procedure. Flight crew crosscheck is performed during
departure briefing.

PF shall perform every new navigation entries, waypoints selection applying cross check procedure.

PF is responsible for the selection of the appropriate sources (RNAV or V/L) and the application of the
navigation display policy (MAP or ARC/ROSE) for each flight phase.

3.9.3. Navigation within RNAV airspace: Departure / En Route / Arrival

Flight crews must ensure that they are properly qualified, and verify the aircraft certification for
relevant RNAV operations.
RNAV track is displayed on PF side on EHSI using MAP setting and RNAV source.
On PNF side, radio aid navigation source is selected on EHSI with V/L setting, so as to allow
immediate cross-checking or reversion in the event of loss of RNAV navigation capability.

Note: MAP/RNAV setting on both sides generates RNAV amber message on both EHSI. The LNAV
mode must be engaged when High Bank speeds are reached. Indeed, in LNAV, the bank angle
order (within a 30 limit) is computed independantly from the current speed of the aircraft. Thus
there is no protection against stall if the aircraft is in LNAV at Low Bank speeds.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

The flight crew check RAIM integrity and legs sequence throughout the flight plan.

In addition, the flight crew continuously check aircraft position, and in case of uncertainty or
detected failure, must notify ATC and revert to conventional means.

Furthermore, on aircraft with limited RNAV capabilities, the flight crew must inform ATC:

Unable P-RNAV
Unable B-RNAV in terminal area

Each time airspace or navigation procedure specifications exceed GPS/GNSS aircraft certification
or crew qualification.

In this case, the flight crew apply navigation outside RNAV airspace method.

3.9.4. Navigation by means of conventional radio-navigation: Departure /

En Route / Arrival

General

Navigation using conventional methods must be applied:

When flying outside RNAV or RNP airspace or,

When aircraft certification or crew qualification cannot meet airspace specifications.

ALL ATR
Radio means are selected and set on both sides on PF orders.

VOR or ADF frequency setting requires flight crew callouts to identify:

Radio navigation station Name and frequency,

Course selected (VOR and ILS),

Radio identification listening is conducted by PNF after each new frequency setting. The VOR
mode must be engaged when High Bank speeds are reached. Indeed, in VOR, the bank angle
order (within a 30 limit) is computed independantly from the current speed of the aircraft. Thus
there is no protection against stall if the aircraft is in VOR at Low Bank speeds.

Conventional Radio navigation method

On PF side: set radio aid frequency and course for the current leg.
set next radio aid frequency on stand by

On PNF side: set radio aid frequency and course for the next leg.
set next radio aid frequency on stand by

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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PROCEDURES JUN 09

Classic:

In this example, CM2 is PF

TOU

PPG

PNF PNF

Then
ALL ATR

TOU frequency PPG frequency

(to be changed) (expected track)

PNF PF
REQUEST
SET NAV 1 PPG, COURSE 135

DO
NAV 1.................. PPG FREQUENCY SET
COURSE 1............................... 135 SET

ANNOUNCE
NAV 1 116.25, COURSE 135 SET
ANNOUNCE
CHECK

ADF / VOR policy: set useful ADF for departure, en route (alternate), and arrival.

Check the RMI pointers to the required setting.

RMI pointers:
On RMI indicator: VOR / VOR
On EHSI: ADF / ADF

Note: These settings can be modified according to type of approach / departure.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

3.10. Radio-communication
The PNF is responsible for radio-communications.

Radio-communication may be transferred to PF (if available), on PNF request:

Example: The PNF listens to the latest ATIS and fills in the data card.

PNF PF
REQUEST
MONITOR VHF 1
WITH TOULOUSE CONTROL ANNOUNCE
RADIO IS RIGHT (LEFT) SIDE

RESUMING NORMAL TASK SHARING

ANNOUNCE
COMING BACK, I HAVE VHF 1 ANNOUNCE
WE ARE NOW WITH PARIS CONTROL
INBOUND TO XXX, RADIO IS LEFT (RIGHT) SIDE"

Listen before transmitting, write down the newly assigned frequency.

VHF receivers standard setting:

ALL ATR
VHF 1 VHF 2

ACTIVE ATC FREQUENCY ATIS / 121.5 MHz (cruise)

STBY NEXT ATC FREQUENCY OPS FREQUENCY

Audio control panel policy:

Headset not used:

VHF 1 key depressed, volume adjusted.
VHF 2 volume adjusted on request.
LOUDSPEAKER knob: 3 o'clock.
INT / RAD switch in neutral position.
Handmike used to transmit.
If INT key depressed, adjust INT volume: interphone function enabled (flight attendant or
mechanic).
Headset used:
VHF 1 key depressed, volume adjusted.
VHF 2 volume adjusted on request.
LOUDSPEAKER knob: minimum.
INT / RAD switch in INT position.
Boomset used: to transmit, press PTT on control wheel or select INT / RAD switch on
RAD position.
INT key must remain in up position.

FOR TRAINING ONLY

 NORMAL PROCEDURES 01.03
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INTRODUCTION TO NORMAL
PROCEDURES JUN 09

3.11. Lights policy

NAV Airplane electrically suplied.

WINGS Engine 2 running in hotel mode.

BEACON Propeller rotating.

TAXI & T/O Airplane taxiing.

LAND Line up to FL 100.

FL 100 to runway vacated.

STROBES Lining up and flight up to runway vacated.

LOGO Company advertisement.

ALL ATR

FOR TRAINING ONLY

 02.01
NORMAL PROCEDURES Page 1 01
STANDARD OPERATING JUN 09
PROCEDURES

1. Presentation

PROCEDURES COCKPIT PANEL

Information for: Information for:

Task sharing Task explanation

Announcements and callouts Flows or scans
Guidelines and checklists System use
Triggering event for procedures Documentation

NORMAL

ALL ATR
STANDARD
norMal proCedUres 02.03 PROC
page 2 02
STANDARD OPERATING INTERNAL INSPECTION FLOW
PROCEDURES Mar 09
CARGO DOOR CTL panel cover: CLOSED 7
72 PEC
72 PEC If opened, only self test of MFC 1B,2B when the battery C
is switched ON.
3.2. Internal inspection 42
42 PEC
PEC
72 not PEC 2 2 8

72 not PEC EMERGENCY EQUIPMENT : CHECK C

The following procedures are based on operations with GPU available*. 19
Check :
72 PEC

exit hatch closed, handle locked and safetied, 9

This procedure will be performed prior to powering the aircraft, either by maintenance or CM2, 13
18 escape rope stowed. Sh
as appropriate completion ensures there will be no damage to aircraft and danger to personnel 17 life jackets stowed (if installed).
when powering up the systems.
axe, flashlights, smoke goggles and oxygen masks 10

12 16 stowed. C
14 15 12 portable fire extinguisher safetied and pressure within
Flight events CM1 CM2 EC
the green area.
CM2 DO L/G emergency handle stowed, cover closed. 11
enters the COCkpit Cargo door Control
panel Cover .............................. Closed protective gloves. C
eMergenCY eQUIpMent ................ CHeCK
gear pIns ............................... on Board
doCUMentatIon ..................... on Board
GEAR PINS : ON BOARD 12
C/B ................................................. CHeCK Check the 3 gear pins stowed behind the F/O seat.
stBY HorIZon ereCtIon
13
KnoB ................................................pUll
DOCUMENTATION : ON BOARD Ch
42 PEC

and MaIntaIned
BatterY .............................................. on PB
MFC ............................................... CHeCK
stBY HorIZon ereCtIon 10 COCKPIT C
KnoB ....................................... released FA
vHF 1 ................................................... on 3
BraKe Handle ........................... parKIng 11
pl1 and 2 ..............................................gI 14
gUst loCK........................................... on 1 C/B PANELS: CHECK
Cl 1 and 2 ................................ FUel s/o Check all C/B panels. Reset as applicable.
Flaps lever ................................. CHeCK 15
eeC 1 and 2 .................................... CHeCK C
landIng gear lever.....................doWn 2 STANDBY HORIZON ERECTION KNOB:
WIpers ...............................................oFF
dC eXt poWer pB ............................... on
PULLED AND MAINTAINED
16
no sMoKIng / seat Belts....................... on
eMer eXIt lIgHts ..............................arM
To
2 BATTERY: ON
BeaCon, nav, logo, WIng .................. on su
Pull Stby Horizon prior to switch battery on.
72 not PEC

FUel pUMps .on For 2 seCond tHen oFF

aIr panel...WHIte lIgHts eXtIngUIsHed Check both amber arrows are illuminated. 17
ovBd valve ..................................... aUto
HYd aUX pUMp pB ................. depressed Check the UNDV amber light is extinguished. SE
To
* Should no GPU be available, please refer to 4.01 p. 1, Hotel mode use. 2 AUTO TEST MFC: CHECKED du
7 9 Check auto test: MFC 1A, 2A flashing (only if cargo door
5 control panel is closed), then MFC 1B, 2B. 18
C
20 3 STANDBY HORIZON ERECTION KNOB: PB
6 RELEASED
19
8 Check no flag.
C
4 In
4 VHF 1: ON
or
In case of any emergency situation.
20
5 BRAKE HANDLE: PARKING
To
Check the brake accumulator pressure. du
Use HYD AUX PUMP PB if necessary.
1
Circuit 6 PL 1 & 2: GI
Breakers Check both PLs are in Ground Idle position.

FOR TRAINING ONLY FOR TRAINING

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.02
Page 1 01
STANDARD OPERATING
PROCEDURES JUN 09

2. Pre-flight preparation procedure

Crew members shall check the following items:

1 Aircraft condition.
2 NOTAMs.
3 Weather briefing.
4 Airport infrastructure (at destination).
5 Specifics.
6 Flight planning.
7 Fuel planning.
8 Flight presentation.
9 Flight attendant briefing.
ALL ATR

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 1 01
STANDARD OPERATING
PROCEDURES JUN 09

3. Procedures and associated flows

3.1. Long and short transit
It is the Captain's responsiblity to determine wether to perform long or short transit regarding the
criteria described hereafter:

Flight crew
YES change NO

Communication between Crew has left the

leaving crew and new crew
NO LONG TRANSIT YES aircraft

YES SHORT TRANSIT NO

ALL ATR
Long transit:

The flight crew must perform:

Internal inspection 02.02.03 page 2
External inspection 02.02.03 page 4
Preliminary cockpit preparation (long transit) 02.02.03 page 16
Final cockpit preparation 02.02.03 page 22

Short transit:

The flight crew must perform:

External inspection 02.02.03 page 4
Preliminary cockpit preparation (short transit) 02.02.03 page 16
Final cockpit preparation 02.02.03 page 22

For external inspection, please refer to the "Walk around" software.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 2 01
STANDARD OPERATING
PROCEDURES JUN 09

3.2. Internal inspection

The following procedures are based on operations with GPU available*.

This procedure will be performed prior to powering the aircraft, either by maintenance or CM2,
as appropriate completion ensures there will be no damage to aircraft and danger to personnel
when powering up the systems.

Flight events CM1 CM2

CM2 DO
enters the cockpit Cargo door control
panel cover............................... closed
Emergency equipment................. check
Gear pins................................ on board
Documentation...................... on board
C/B.................................................. CHECK
STBY HORIZON ERECTION KNOB.........PULL
AND MAINTAINED
BATTERY............................................... ON
STBY HORIZON
ERECTION KNOB........................ RELEASED
VHF 1.................................................... ON
BRAKE HANDLE............................ PARKING
PL1 AND 2...............................................GI
GUST LOCK........................................... ON
CL 1 AND 2................................. FUEL S/O
FLAPS LEVER.................................. CHECK
ECU 1 AND 2................................... CHECK
LANDING GEAR LEVER.....................DOWN
WIPERS................................................OFF
DC EXT POWER PB................................ ON
NO SMOKING / SEAT BELTS........................ ON
EMER EXIT LIGHTS...............................ARM
BEACON, NAV, LOGO, WING................... ON
FUEL PUMPS.....ON FOR 2 SECOND THEN OFF
AIR PANEL.....WHITE LIGHTS EXTINGUISHED
OVBD VALVE...................................... AUTO
HYD AUX PUMP PB.................. DEPRESSED

* Should no GPU be available, please refer to 4.01 p. 1, Hotel mode use.

42 not PEC

FOR TRAINING ONLY

PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 2 02
STANDARD OPERATING
PROCEDURES JUN 09

3.2. Internal inspection

The following procedures are based on operations with GPU available*.
72 PEC

This procedure will be performed prior to powering the aircraft, either by maintenance or CM2,
as appropriate completion ensures there will be no damage to aircraft and danger to personnel
when powering up the systems.

Flight events CM1 CM2

CM2 DO
enters the cockpit Cargo door control
panel cover............................... closed
EMERGENCY EQUIPMENT................. CHECK
GEAR PINS................................ ON BOARD
DOCUMENTATION...................... ON BOARD
C/B.................................................. CHECK
STBY HORIZON ERECTION
KNOB.................................................PULL
42 PEC

AND MAINTAINED
BATTERY............................................... ON
MFC................................................ CHECK
STBY HORIZON ERECTION
KNOB........................................ RELEASED
VHF 1.................................................... ON
BRAKE HANDLE............................ PARKING
PL1 AND 2...............................................GI
GUST LOCK........................................... ON
CL 1 AND 2................................. FUEL S/O
FLAPS LEVER.................................. CHECK
EEC 1 and 2..................................... CHECK
LANDING GEAR LEVER.....................DOWN
WIPERS................................................OFF
DC EXT POWER PB................................ ON
NO SMOKING / SEAT BELTS........................ ON
EMER EXIT LIGHTS...............................ARM
BEACON, NAV, LOGO, WING................... ON
72 not PEC

FUEL PUMPS....ON FOR 2 SECOND THEN OFF

AIR PANEL...WHITE LIGHTS EXTINGUISHED
OVBD VALVE...................................... AUTO
HYD AUX PUMP PB.................. DEPRESSED

* Should no GPU be available, please refer to 4.01 p. 1, Hotel mode use.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 3 01
STANDARD OPERATING
PROCEDURES JUN 09

INTERNAL INSPECTION FLOW

CARGO DOOR CTL panel cover: CLOSED 7 GUST LOCK: ON
72 PEC
72 PEC If opened, only self test of MFC 1B,2B when the battery Check it is fully engaged.
is switched ON.
42
42 PEC
PEC
2 2 8 CL 1 & 2: FUEL S/O
72 not PEC EMERGENCY EQUIPMENT : CHECK
72 not PEC 19 Check both CLs are in Fuel Shut off position.
Check :
exit hatch closed, handle locked and safetied, 9 FLAPS LEVER: CHECK POSITION
13
18 escape rope stowed. Should be at 0.
17 life jackets stowed (if installed).
axe, flashlights, smoke goggles and oxygen masks 10 ECU/EEC 1 & 2: PB DEPRESSED IN

12 16 stowed. Check FAULT amber lights are illuminated, only for

14 15 12 portable fire extinguisher safetied and pressure within ECU.
the green area.
L/G emergency handle stowed, cover closed. 11 LANDING GEAR LEVER: DOWN
protective gloves. Check it is in down position, no red light illuminated.

GEAR PINS : ON BOARD 12 CAPTAIN & F/O WIPERS: OFF

Check the 3 gear pins stowed behind the F/O seat.
13 DC EXT PWR: ON
DOCUMENTATION : ON BOARD Check the AVAIL green light is illuminated, then depress the
PB.
10 COCKPIT Check the MAIN ELEC PWR panel: only DC GEN 1 & 2
FAULT amber lights are illuminated.
3
11
14 NO SMKG & SEAT BELTS SIGNS: ON

ALL ATR
1 C/B PANELS: CHECK
Check all C/B panels. Reset as applicable.
15 EMER EXIT LT: ARM

Check the DISARM amber light is extinguished.

2 STANDBY HORIZON ERECTION KNOB:
PULLED AND MAINTAINED
16 NAV, LOGO (AT NIGHT): ON
To advise ground staff that the aircraft is electrically
2 BATTERY: ON
supplied.
Pull Stby Horizon prior to switch battery on.
Check both amber arrows are illuminated. 17 FUEL PUMPS 1 & 2: ON FOR A FEW
Check the UNDV amber light is extinguished. SECONDS, THEN OFF
To pressurize the system and check possible leakage
2 AUTO TEST MFC: CHECKED during the following external inspection.
7 9 Check auto test: MFC 1A, 2A flashing (only if cargo door
5 control panel is closed), then MFC 1B, 2B. 18 AIR PANEL: EXTINGUISH ALL WHITE LIGHTS
Check the FAULT amber lights on ENG 1 & 2 BLEED
20 3 STANDBY HORIZON ERECTION KNOB: PBs and on PACK VALVE 1 & 2 PBs.
6 RELEASED
Check no flag. 19 OVBD VALVE: AUTO
8 Check the FAULT amber light is extinguished.
4 In cold weather operation, FULL CLOSED can be set in
4 VHF 1: ON
order to warm the cabin more quickly.
In case of any emergency situation.
20 HYD AUX PUMP PB: DEPRESSED
5 BRAKE HANDLE: PARKING To pressurize the system and check possible leakage
Check the brake accumulator pressure. during the following external inspection.
Use HYD AUX PUMP PB if necessary.
1
Circuit 6 PL 1 & 2: GI
Breakers Check both PLs are in Ground Idle position.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 4 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.3. External inspection
During this inspection, the CM1 must perform and check the following:

Cabin inspection (safety device, emergency exit, holds, smoke detector, door).
Overall condition of the aircraft.
Visible components.
Flight equipment.
Aircraft clear of frost, ice, and snow.
Memorization of surfaces position to compare with command levers position.
Hydraulic, oil or fuel leaks (especially puddles on the ground).
Tyres condition, brakes and shock absorbers.
Access doors closed and latched.

Upon completion of inspection:

PNF returns to the cockpit

10
9

ALL ATR
8
12
11
7

13

5 1
14
4

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 5 01
STANDARD OPERATING
PROCEDURES JUN 09

1 Main left landing gear and fairing

Park brake accumulator

pressure 6 maintenance doors
(check minimum (closed)
1600psi)

Gear door (check, fixed,

no impact)

Beacon (condition,
window not broken) and
flashing if selected ON

ALL ATR
Landing gear
structure (check,
no crack, no oil)
Hydraulic lines
(check, no leak)
Wheel and tires
(condition, no
crack, inflation)

Brake wear detector

Brake temperature
(check indicator out of
sensor (check plugging in)
bolt)

Safety pin removed

Uplock (open)
Wheel well (condition,
no leak)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 6 01
STANDARD OPERATING
PROCEDURES JUN 09

Free fall assister (check

the red marker of the
pressure indicator is
not visible)

Landing light (condition, Pack ram air inlet

window not broken) (check unobstructed)

42 PEC
TAT prob (check)
Magnetic fuel level (in) 72 PEC
72 not PEC
ALL ATR

2 Left wing trailing edge

Banana seal (check

unobstructed) and not
damaged

Exhaust nozzle
(unobstructed)

Inner/outer flaps
uncoupling control
system (check indicator
visible)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 7 01
STANDARD OPERATING
PROCEDURES JUN 09

Flaps position (check

the position in Flaps (condition, fixed,
accordance with the no impact)
flaps lever)

5 static dischargers
Aileron and tab (check,
(check they are
fixed, no impact)
in place, not broken)

3 Left wing leading edge

Nav and strobe lights

Horn (condition) (condition, window
not broken) and
illuminated if ON

ALL ATR
Magnetic fuel level in,
wing de-icing boots Fuel vent NACA inlet
(no tear, no blister, (clear, unobstructed)
no peeling)

Wing de-icing boots

Ice detector
(no tear, no blister,
(check, in place)
no peeling, varnish)

4 - Left engine

Left cowls
(closed, latched)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 8 01
STANDARD OPERATING
PROCEDURES JUN 09

Engine de icing boots Engine air intake (clear,

(no tear, no oil) unobstructed)

Oil cooler air intake

(clear, unobstructed)

Propeller (feathered, Spinner (secure, spinner

condition, free rotation, indicator aligned with propeller
no impact, no oil, de-icer) indicator, no impact)
ALL ATR

Inner wing leading edge

and fairing (condition)

5 Left forward fuselage

Emergency exit
(check closed)

Wing light (condition, window

not broken)
Emergency light
(condition, window not
broken)

Avionics vent overboard

valve (open)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 9 01
STANDARD OPERATING
PROCEDURES JUN 09

Antennae (check in
place, no impact)

Cargo door (closed, Cargo door operating

latched) panel (closed)

Bottle overboard
discharge indicator
(green in normal status)

ALL ATR
Cockpit communication Angle of attack
hatch (closed) (condition)

Icing evidence probe

(condition)
Pitot probes and covers
(check, removed)
Static ports (clear)

6 Nose

Static dischargers
(check)
Wipers (condition, in
place, position)
Radome and latches
(check, fixed, no impact)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 10 01
STANDARD OPERATING
PROCEDURES JUN 09

Nose wheel steering Nose gear structure (check,

(condition) no crack)

Nose gear wheels and

tyres (condition, no crack, 2 nose gear doors (closed,
inflation) fixed, no impact)

Taxi and T/O lights

Hydraulic lines (condition,
(condition, window not
no leak)
broken)

Wheel well (condition,

Safety pin (removed)
no leak)

7 Right forward fuselage

Angle of attack (condition) Pilot probes and covers

(check, removed)

TAT probe (check)

Static ports (clear)
ALL ATR

42 not PEC

Ext DC and AC elect power

access doors (check)

Emergency exit
(check closed)
Emergency light (check,
window not broken)
Wing light (condition,
window not broken)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 11 01
STANDARD OPERATING
PROCEDURES JUN 09

8 Right engine

Right cowls (closed, Inner wing leading edge

latched) and fairing (condition)

Engine de-icing boots Engine air intake

(no tear, no oil) (clear, unobstructed)

Oil cooler air intake

(clear, unobstructed)

ALL ATR
Spinner (secure, spinner
Propeller (feathered condition, indicator aligned with
free rotation, no impact, propeller indicator,
no oil, de-icer) no impact)

Right cowls (closed,

latched)

9 Right wing leading edge

Refuelling point access

Wing de-icing boots
door (closed)
(no tear, no blister,
42 not PEC no peeling, varnish)
42 PEC

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 12 01
STANDARD OPERATING
PROCEDURES JUN 09

Fuel vent NACA inlet

Magnetic fuel level in
(clear, unobstructed)

Nav and strobe lights

(condition, window
Horn (condition)
not broken) and
illuminated if ON

10 Right wing trailing edge

5 static dischargers
Aileron and tab (check,
(check in place, not
fixed, no impact)
broken)
ALL ATR

Flaps position
(check position is in Flaps (condition, fixed,
accordance with the no impact)
flaps lever)

Inner/outer flaps
uncoupling control
system (check indicator
visible)

Banana seal (check

Exhaust nozzle
unobstructed) and
(unobstructed)
not damaged

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 13 01
STANDARD OPERATING
PROCEDURES JUN 09

11 Main right landing gear and fairing

Refuelling point access

door (closed) Air conditionning ground
access door (closed)
72 PEC
72 not PEC
Pack ram air inlet (check
Landing light (condition, unobstructed)
window not broken)

Refuelling control
access door

Wheel and tires

Gear doors (check,
(condition, no creek,
fixed, no impact)
inflation)

ALL ATR
Landing gear
structure (check, Hydraulic lines
no creek, no oil) (check, no leak)

Safety pin removed

Uplock (open)
Wheel well (condition,
no leak)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 14 01
STANDARD OPERATING
PROCEDURES JUN 09

Check the red marker of the

Free fall assister pressure indicator is not
visible

Brake temperature Brake wear detector (check

sensor (check plugging in) indicator out of bolt)

12 Right aft fuselage

VHF antennae (check in Emergency exit light

place, planning) (condition, window not broken)
ALL ATR

Service door (closed,

fixed, no impact)

2 outflow valves
Tail skid (check)
(unobtructed)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 15 01
STANDARD OPERATING
PROCEDURES JUN 09

13 Tail

Flight controls access

door (closed)

Horn (condition)
Logo light (condition,
window not broken)

Stabilizers, elevators
8 static dischargers
and trims (check,
(check, in place,
fixed, no impact)
no break, no burn)

Stabilizer de-icing boots (condition, no

tear, no blister, no peeling, varnish) 5 static dischargers, fin, rudder, tab
(check fixed, no impact)

VOR antenna (check in place, no impact)

2 static dischargers, nav and strobe
lights (condition, window not broken)

ALL ATR
Vortex generator (check no impact)

14 Left aft fuselage

Toilet service door

(closed)

Drinkable water service door

Cabin door (check closed, fixed, (closed)
no impact)

Entry emergency light

(condition, window not broken) 72 PEC
Tail prop (check) 72 not PEC

FOR TRAINING ONLY

PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 16 01
STANDARD OPERATING
PROCEDURES JUN 09

3.4. Preliminary cockpit preparation (1/2)

Preliminary cockpit preparation is done by CM2 with a GPU connected.
In case of preliminary cockpit preparation with engine 2 in hotel mode, apply the additional standard
operating procedure Hotel mode use 02.04.01 pages 01 to 06.
There are two procedures: for long or for short transits.
The main approach is to extinguish all white lights, to test all systems and to prepare the cockpit
for the flight.

3.4.1. Long transit

CM1 CM2
DO DO
EXTERNAL INSPECTION SCAN ON OVERHEAD PANEL
ANNUNCIATOR LIGHT......................... TEST
DOME LIGHT......................... AS REQUIRED
STANDBY COMPASS LIGHT.................. OFF
STORM LIGHT...................................... OFF
ENG 1 PUMP........................................ ON
FUEL X-FEED...................................CHECK
ENG 2 PUMP........................................ ON
FUEL X-FEED TEST: DOORS.............................................. TEST
SPOILER LIGHTS................. EXTINGUISHED
LDG GEAR INDICATOR......................CHECK
ENG 1 PUMP ON: FEED LO PR 1
TLU...................................................AUTO
Extinguished ; FEED LO PR 2 Illuminated ENG 1 FIRE..................................... 3 TEST
EXTERNAL LIGHTS............... AS REQUIRED
FUEL X-FEED in line: FEED LO PR 1 and 2 PROP BRAKE........................................ ON
Extinguished DC/AC PANEL..................................CHECK
CVR................................................... TEST
FUEL X-FEED closed: FEED LO PR 1 SIGN PANEL....................................CHECK
DE-ICING/ANTI-ICING................ LIGHTS OFF
Extinguished ; FEED LO PR 2 Illuminated
PROBES HEATING................................. ON
WINDSHIELD HEATING.......................... ON
ENG 2 PUMP ON: FEED LO PR 1 and 2 ACW PANEL....................................CHECK
Extinguished HYD PANEL.....................................CHECK
EMER LOC XTMR...............................AUTO
AIR COND PANEL.............................CHECK
AVIONICS VENT..................................AUTO
OXYGEN..........................................CHECK
COMPT SMK...................................... TEST
EXHAUST MODE.............................. RESET
ENG 2 FIRE..................................... 3 TEST
SCAN ON PEDESTRAL
LIGHTS................................. AS REQUIRED
FDEP (If installed)....FLIGHT NUMBER+DATE
TRIMS....................TEST AND SET NEUTRAL
ATPCS.......................................... 2 TESTS
TCAS.........................................TEST/STBY
VHF..............................................ON/ TEST
ADF..............................................ON/ TEST
TRANSPONDER.........................STBY/ TEST
IDLE GATE.....................................PULLED
EMER AUDIO CANCEL.................GUARDED
ATC RECOMMENDATION: PL.......................................................... GI
In case of dual installation check both CL................................................FUEL SO
42 not PEC

systems using: GUST LOCK.......................................... ON

RADAR.............................................. STBY
system 1 for odd days.
ECP.............................................TEST/SET
system 2 for even days. GPS..................................................... ON
MCDU (If installed with the MPC).......... SET
Example: TRANSPONDER, IGNITION, ADC CDLS........................................Daily check
SWITCH (IF INSTALLED)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 17 01
STANDARD OPERATING
PROCEDURES JUN 09

3.4. Preliminary cockpit preparation (2/2)

Flight events CM1 CM2

AFTER PEDESTAL DO
PANEL SCAN
SCAN ON CENTRAL PANEL
FUEL QTY............................... TEST / CHECK
TAT/SAT............................................ CHECK
CAP..................................................... CLR
STBY INSTRUMENTS........................ .CHECK
PWR MGT..............................................T/O
SYNCHROPHASER.................................. ON
FUEL USED....................................... RESET
ENGINE INDICATORS............... TEST / CHECK
ENG PANEL...................................... CHECK
CAB PRESS PANEL........................... CHECK
AUTO PRESS...... TEST / LANDING ELEVATION
TRIM INDICATOR............................... CHECK
FLAPS INDICATOR............................. CHECK
STICK PUSHER......................... DEPRESSED
HYDRAULIC...................................... CHECK

SCAN ON GLARE SHIELD

fD BARS............................................... ON
NAV 1 AND 2............................... ON / TEST
ADU.....................................................BRT

SCAN ON LEFT LATERAL PANEL

COCKPIT COM HATCH.......................... OPEN
nW STEERING........................ ON/GUARDED
OXYGEN MASK.................................... TEST
MARKERS.....................................TEST / LO
AHRS.............................................. CHECK
AUDIO1 SEL.................................... Check
CAPT SWITCHING PANEL................... CHECK
(E)GPWS......................................GUARDED

SCAN ON LEFT INSTRUMENT PANEL

CLOCK..................................................SET
AIR SPEED INDICATOR...................... CHECK
RMI/EHSI......................................... CHECK
EADI................................................ CHECK
(E)GPWS............................................. TEST
ATC RECOMMENDATION: ALTIMETER............................................SET
RMI set with VOR bearing VERTICAL AIR SPEED........................ CHECK
EHSI set with ADF bearing*
SCAN ON RIGHT LATERAL PANEL
could be selected according to PF
EXTRACT AIR FLOW............................ OPEN
decision. OXYGEN MASK.................................... TEST
AHRS.............................................. CHECK
* 1 needle recommended. F/O SWITCHING PANEL..................... CHECK
AUDIO 2 SEL................................... CHECK

SCAN ON RIGHT INSTRUMENT PANEL

(E)GPWS............................................. TEST
VERTICAL AIR SPEED........................ CHECK
ALTIMETER............................................SET
EADI................................................ CHECK
RMI/EHSI......................................... CHECK
42 not PEC

AIR SPEED INDICATOR...................... CHECK

CLOCK..................................................SET

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 16 02
STANDARD OPERATING
PROCEDURES JUN 09

3.4. Preliminary cockpit preparation (1/2)

Preliminary cockpit preparation is done by CM2, with a GPU connected.
In case of preliminary cockpit preparation with engine 2 in hotel mode, apply the additional 01.03.1

72 PEC
standard operating procedure Hotel mode use 02.04.01 pages 01 to 06.
There are two procedures: for long or for short transits.
The main approach is to extinguish all white lights, to test all systems and to prepare the cockpit
for the flight.

3.4.1. Long transit

CM1 CM2
DO DO
EXTERNAL INSPECTION SCAN ON OVERHEAD PANEL
ANNUNCIATOR LIGHT......................... TEST
DOME LIGHT......................... AS REQUIRED

42 PEC
STANDBY COMPASS......... CHECK AND OFF
STORM LIGHT................... CHECK AND OFF
ENG 1 PUMP........................................ ON
FUEL X-FEED...................................CHECK
ENG 2 PUMP........................................ ON
FUEL X-FEED TEST: DOORS.............................................. TEST
SPOILER LIGHTS................. EXTINGUISHED
LDG GEAR INDICATOR......................CHECK
ENG 1 PUMP ON: FEED LO PR 1
TLU...................................................AUTO
Extinguished ; FEED LO PR 2 Illuminated ENG 1 FIRE..................................... 3 TEST
EXTERNAL LIGHTS............... AS REQUIRED
FUEL X-FEED in line: FEED LO PR 1 and 2 PROP BRAKE........................................ ON
Extinguished DC/AC PANEL..................................CHECK
CVR................................................... TEST
FUEL X-FEED closed: FEED LO PR 1 SIGN PANEL....................................CHECK
DE-ICING/ANTI-ICING................ LIGHTS OFF
Extinguished ; FEED LO PR 2 Illuminated
PROBES HEATING................................. ON

72 not PEC
WINDSHIELD HEATING.......................... ON
ENG 2 PUMP ON: FEED LO PR 1 and 2 ACW PANEL....................................CHECK
Extinguished HYD PANEL.....................................CHECK
EMER LOC XTMR...............................AUTO
AIR COND PANEL.............................CHECK
AVIONICS VENT..................................AUTO
OXYGEN..........................................CHECK
COMPT SMK...................................... TEST
EXHAUST MODE.............................. RESET
ENG 2 FIRE..................................... 3 TEST
SCAN ON PEDESTRAL
LIGHTS................................. AS REQUIRED
FDEP (If installed)....FLIGHT NUMBER+DATE
TRIMS....................TEST AND SET NEUTRAL
ATPCS.......................................... 2 TESTS
TCAS.........................................TEST/STBY
VHF..............................................ON/ TEST
ADF..............................................ON/ TEST
TRANSPONDER.........................STBY/ TEST
IDLE GATE.....................................PULLED
EMER AUDIO CANCEL.................GUARDED
ATC RECOMMENDATION: PL.......................................................... GI
In case of dual installation check both CL................................................FUEL SO
systems using: GUST LOCK.......................................... ON
AIL LOCK LIGHT.................. EXTINGUISHED
system 1 for odd days.
RADAR.............................................. STBY
system 2 for even days. ECP.............................................TEST/SET
GPS..................................................... ON
Example: TRANSPONDER, IGNITION, ADC MCDU (If installed with the MPC).......... SET
SWITCH (IF INSTALLED) CDLS........................................Daily check

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 17 02
STANDARD OPERATING
PROCEDURES JUN 09

3.4. Preliminary cockpit preparation (2/2)

72 PEC

Flight events CM1 CM2

AFTER PEDESTAL DO
PANEL SCAN
SCAN ON CENTRAL PANEL

FUEL QTY............................... TEST / CHECK

TAT/SAT............................................ CHECK
CAP..................................................... CLR
72 PEC STBY INSTRUMENTS........................ .CHECK
PWR MGT..............................................T/O
42 PEC PEC 1 & 2.............................................. ON
SYNCHROPHASER.................................. ON
72 not PEC FUEL USED....................................... RESET
ENGINE INDICATORS............... TEST / CHECK
ENG PANEL...................................... CHECK
CAB PRESS PANEL........................... CHECK
AUTO PRESS...... TEST / LANDING ELEVATION
TRIM INDICATOR............................... CHECK
FLAPS INDICATOR............................. CHECK

42 PEC

STICK PUSHER......................... DEPRESSED
HYDRAULIC...................................... CHECK

SCAN ON GLARE SHIELD

fD BARS............................................... ON
NAV 1 AND 2............................... ON / TEST
ADU.....................................................BRT

SCAN ON LEFT LATERAL PANEL

ATC RECOMMENDATION:
COCKPIT COM HATCH.......................... OPEN
In case of dual installation check both nW STEERING........................ ON/GUARDED
systems using: OXYGEN MASK.................................... TEST
- System 1/a for odd days. MARKERS.....................................TEST / LO
- System 2/b for even days. AHRS.............................................. CHECK
Example: TRANSPONDER, IGNITION, ADC AUDIO1 SEL.................................... Check
SWITCH (IF INSTALLED) CAPT SWITCHING PANEL................... CHECK
(E)GPWS......................................GUARDED
72 not PEC

SCAN ON LEFT INSTRUMENT PANEL

CLOCK..................................................SET
AIR SPEED INDICATOR...................... CHECK
RMI/EHSI......................................... CHECK
EADI................................................ CHECK
ATC RECOMMENDATION: (E)GPWS............................................. TEST
- RMI set with VOR bearing ALTIMETER............................................SET
VERTICAL AIR SPEED........................ CHECK
- EHSI set with ADF bearing*
adc switch.................................... 1 or 2

could be selected according to PF SCAN ON RIGHT LATERAL PANEL

decision.
EXTRACT AIR FLOW............................ OPEN
OXYGEN MASK.................................... TEST
* 1 needle recommended.
AHRS.............................................. CHECK
F/O SWITCHING PANEL..................... CHECK
AUDIO 2 SEL................................... CHECK

SCAN ON RIGHT INSTRUMENT PANEL

APM (IF INSTALLED)................... DAILY TEST
(E)GPWS............................................. TEST
VERTICAL AIR SPEED........................ CHECK
ALTIMETER............................................SET
EADI................................................ CHECK
RMI/EHSI......................................... CHECK
AIR SPEED....................................... CHECK
CLOCK..................................................SET

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 18 01
STANDARD OPERATING
PROCEDURES JUN 09
PRELIMINARY COCKPIT PREPARATION SCAN (long transit) (1/4)

72 PEC
PEC 11 15 21
72 OVERHEAD PANEL 12 EXTERNAL LIGHTS: AS REQUIRED
42
42 PEC
PEC 1 Set NAV lights ON and LOGO lights ON if during night
10 ANNUNCIATOR LIGHT: TEST
72 not PEC operation.
72 not PEC Check all lights are illuminated (except fuel LO LEVEL
and engine gauges). 13 PROP BRK: ON
2 Check the PROP BRK blue light is illuminated.
DOME LIGHT: AS REQUIRED
If not, depress HYD AUX PUMP PB on the pedestal.
3 STANDBY COMPASS: CHECK AND OFF When the READY green light illuminates, select PROP
Check lights off. BRK ON.
Check the UNLK red light is extinguished.
4 STORM LIGHT: CHECK AND OFF
2 12 16 1 14 DC / AC PANEL: CHECK
Check storm light OFF.
No amber light, except both DC GEN FAULT lights.
5 ENG 1 PUMP: ON
15 CVR: TEST
Check the RUN green light is illuminated, FEED LO PR
extinguished and LP VALVE in-line Can be performed with GPU, only by depressing the
RCDR PB on the pedestal.
6 FUEL X-FEED : CHECK Check the ON blue light illuminates on the PB.
Set X-FEED VALVE in-line and check FEED LO PR is Depress the TEST PB. Check the needle in the green
extinguished for ENG 2. Then close the X-FEED VALVE. arc.
Stop the CVR by depressing the RESET PB on the
7 ENG 2 PUMP: ON
pedestal.
Check the RUN green light is illuminated, FEED LO PR
extinguished and LP VALVE in-line. 16 SIGNS PANEL: ON
Select the NO SMKG and SEAT BELTS switches to ON.
8 DOORS: TEST
Check NO SMK and SEAT BELTS on the memo panel.
Depress TEST SW. Check CAB OK and SVCE OK lights Select EMER EXIT Light to ARM

ALL ATR
illuminate, provided associated doors are opened.
17 DE-ICING / ANTI-ICING PANEL: CHECK
9 SPOILER LIGHTS: EXTINGUISHED Check all lights are extinguished.
10 LANDING GEAR INDICATORS: CHECK
18 PROBES / WINDSHIELD HTG PANEL: CHECK
Check the control lever is down and that there are 3 Check all white lights are extinguished.
green lights.
19 ACW PANEL: CHECK
10 TLU AUTO: CHECK Extinguish any white light.
Check the toggle switch is in AUTO position, no amber
light. 20 HYD PANEL: CHECK

11 ENG 1 FIRE PROTECTION: TEST

Extinguish any white light.
Check the BLUE and GREEN PUMP LO PR lights are
Check ENG 1 fire handle IN and latched.
illuminated and other lights are extinguished.
Extinguish any white light.
Select the EMER EXIT Light to ARM.
Depress SQUIB TEST PB and check both AGENT
SQUIB lights illuminate. 21 EMER LOC XMTR: AUTO
Select TEST switch on FIRE and check: Check the toggle switch is in AUTO position, guarded
ENG FIRE red light illuminates into associated fire and lockwired.
handle.
CCAS is activated (CRC + MW + ENG 1 FIRE on
CAP)
FUEL SO red light illuminates in CL 1 if temporarily
selected out of FUEL SO.
Select TEST switch on FAULT and check:
both LOOP A & B FAULT lights illuminate.

COCKPIT + OVERHEAD PANEL

FOR TRAINING ONLY

PERSONAL NOTES PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 19 01
STANDARD OPERATING
PROCEDURES JUN 09

PRELIMINARY COCKPIT PREPARATION SCAN (long transit) (2/4)

OVERHEAD PANEL (Cont'd) Reset trims as required for take-off.

26 Before each flight:
22 AIR COND PANEL: CHECK Check PITCH, ROLL and YAW trim operation.
Extinguish any white light Check STBY PITCH trim operation, check guarded in
Select COMP TEMP selectors as required. OFF position.

23 AVIONIC VENT: AUTO 4 ATPCS: TEST

Check the OVBD VALVE CTL guarded switch is in Turn ATPCS to the left / right and select ARM.
AUTO position. Check the ATPCS ARM green light illuminates.
Check there is no amber nor white light on. Set the ATPCS selector to ENG 1 / ENG 2.
Check the ENG 2 / ENG 1 UPTRIM light illuminates
24 OXYGEN PANEL: CHECK and the ARM light extinguishes after 2.15 seconds.
22 Check oxygen high pressure indication.
Check the oxygen duration chart in the 2.01.05 to 5 TCAS: TEST / STBY
determine there is sufficient quantity for the scheduled
flight. 6 VHF 1 AND VHF 2: ON & TEST
Select MAIN SUPPLY ON: check the PB light is
7 ADF 1 AND ADF 2: ON & TEST
extinguished.
Check PAX SUPPLY OFF. 8 TRANSPONDER: STANDBY & TEST

25 COMPT SMK: TEST (if installed)

FID: ATC flight identification inserted (if equipped)
Depress the SMK TST PB to check smoke detectors. 9 IDLE GATE: CHECK
When testing is over, reset the AVIONICS VENT Select the flight ID (If Installed)
EXHAUST MODE PB to restart the extract fan. Check the IDLE GATE FAIL amber light is extinguished
26 ENG 2 FIRE PROTECTION: CHECK
and the amber band is visible on the lever.
Check ENG 2 fire handle IN and latched. 10 EMER AUDIO CANCEL: CHECK GUARDED
Extinguish any white light:

ALL ATR
Check the switch is guarded and lockwired.
Depress the SQUIB TEST PB and check both AGENT
SQUIB lights illuminate. 11 PLs: GI
Select TEST switch on FIRE and check: Check both PLs in ground idle position.
ENG FIRE red light illuminates into associated fire
handle. 12 CLs: FUEL S.O.

18 CCAS is activated (CRC + MW + ENG 1 FIRE on Check both CLs in fuel shut-off position.
CAP)
13 GUST LOCK: ON
FUEL SO red light illuminates in CL 2 if temporarily
selected out of FUEL SO. Check gust lock is engaged.
Select TEST switch on FAULT and check: AIL LOCK LIGHT (If installed): CHECK EXTINGUISHED
both LOOP A & B FAULT lights illuminate.
14 EFIS CONTROL PANEL(ECP): TEST / SET
Select EADI ON, check composite mode, select EADI
PEDESTAL OFF.
1 LIGHTS: AS REQUIRED
Select EHSI ON, check composite mode.
Select EADI ON.
Adjust lights as required.
Test DH by depressing DH TEST PB.
2 FDEP (If installed): SET FLIGHT NUMBER +
15 WEATHER RADAR: STBY
DATE
Set standby.
Check FDAU time base, adjust if necessary.
16 GPS: ON (if installed)
3 TRIM: TEST AND SET NEUTRAL
Daily check, for the first flight of the day. 17 MCDU (If installed with the MPC): SET
Check PITCH, ROLL and YAW trim operation as follows: Set the flight number and and check FDAU time base,
Check the normal TRIM activation in both directions adjust if necessary.
by simultaneously depressing both control rocker
switches. 18 COCKPIT DOOR DAILY CHECK (If installed)
For a few seconds, depress each single control rocker Refer to QRH - Normal Procedure - 3.02A
switch independently and check the non-activation of
1 the corresponding trim in both directions.

OVERHEAD PANEL (contd) + PEDESTAL

FOR TRAINING ONLY

PERSONAL NOTES PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 20 01
STANDARD OPERATING
PROCEDURES JUN 09
PRELIMINARY COCKPIT PREPARATION SCAN (long transit) (3/4)

CENTRAL PANEL 14 STICK PUSHER: CHECK

1 FUEL QTY PANEL: TEST Check no light is illuminated.

Depress TEST PB and check:
15 HYDRAULIC GAUGES: CHECK
MC + SC + FUEL on CAP
all lights and displays Check brake accumulator pressure at 3000 PSI.
both LO LVL amber lights illuminated
both RUN green lights illuminated on pumps PB.

2 TAT / SAT / TAS PANEL: CHECK GLARESHIELD

3 CAP: CLR 1 FD BARS: ON

Check amber lights are extinguished. Check the FD BARS switch in the ON position.

4 STBY INSTRUMENTS: CHECK 2 NAV 1 & 2: TEST / ON

Check there is no flagging.
3 ADU: BRT
5 PWR MGT: TO Adjust ADU brightness as required.
Check the rotary selector is on TO.

6 SYNPHR: ON
Check the synchrophaser is OFF, white light extinguished.

6 PEC 1 & 2: ON
Check no amber light is illuminated.

7 FUEL USED: RESET

72 PEC Pull the reset knob to reset the fuel used value.

ALL ATR
42 PEC 6 8 ENG 1 & 2 INSTRUMENTS: CHECK AND TEST
Check: oil press = 0
oil temp = realistic indication
FF / FU = 0
NH = 0
ITT = realistic indication
NP = 0
TQ = 0.

9 ENG PANEL: CHECK

EEC / ECU 1 & 2 PBs and ATPCS PB depressed in.
10 CAB PRESS PANEL: CHECK
Check no light is illuminated.
Check the rotary selector is facing the green mark.

11 AUTO PRESS PANEL: TEST / CHECK

Depress the TEST PB and check:
MC + SC + AIR on CAP
FAULT amber light illuminated in MODE SEL PB
display cycling between -8800 and 18800.
12 TRIM INDICATOR: CHECK
Check neutral setting for roll and yaw axis.
13 FLAPS INDICATOR: CHECK
Check the position according to the flaps lever position
and to the position noticed during the external
inspection.

CENTRAL PANEL + GLARESHIELD

FOR TRAINING ONLY

PERSONAL NOTES PERSONAL NOTES

FOR TRAINING ONLY FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 21 01
STANDARD OPERATING
PROCEDURES JUN 09
PRELIMINARY COCKPIT PREPARATION SCAN (long transit) (4/4)

CAPT LATERAL PANEL 4 EADI: CHECK

1 COCKPIT COM HATCH: OPEN
5 EGPWS: TEST
Refer to FCOM 1.15.40 for test procedure.
Must be kept open until engine 1 start, in order to avoid
pressurization shocks. 6 ALTIMETER: CHECK

2 N/W STEERING: CHECK Check no flag.

Check N/W steering guarded switch on N/W steering 7 VSI: CHECK
position. Check no flag and pointer indicates zero.
3 OXYGEN MASK : TEST (once a day)
8 ADC SWITCH (If installed):
Set the audio control panel INT/RAD selector to INT
SET TO ADEQUATE ADC
and adjust the volume.
Depress and hold the PRESS TO TEST AND RESET
PB (hose and mask charged with oxygen): observe the
blinker momentarily turn yellow and must turn dark if F/O LATERAL PANEL
there is no leak.
Hold the PRESS TO TEST AND RESET PB and press
the red clips on each side of the hose (oxygen pressure 1 EXTRACT AIRFLOW: OPEN
inflates the harness): observe the blinker momentarily 2 OXYGEN MASK: TEST
turns yellow and must turn dark if there is no leak. Same as on the captain side.
Hold the PRESS TO TEST AND RESET PB and select
the EMERGENCY knob (emergency flow is tested): 3 AHRS: CHECK
observe the blinker turn yellow during the oxygen flow Check the AHRS 2 light is extinguished.
and must turn dark when the knob is released.
4 F/O SWITCHING: CHECK
Note: In these three cases, check that the oxygen Check ATT/HDG, VOR/ILS and EFIS SG: depress then
reset, check lights are extinguished.
flow sounds through the loudspeakers.
5 AUDIO: CHECK

ALL ATR
Check the OXY LO PR light is extinguished on the Check the AUDIO 2 SEL light is extinguished.
overhead panel.
Set N/100% rocker lever to 100%.
F/O INSTRUMENT PANEL
4 MKR: LO
Set MKR switch to LO.. 1 APM (If installed): TEST

5 AHRS: CHECK Daily check must be performed

Check the AHRS 1 light is extinguished. Push and maintain the APM PTT PB
for the test duration
6 AUDIO: CHECK
Check the AUDIO 1 SEL light is extinguished. 2 (E)GPWS: TEST
7 CAPT SWITCHING: CHECK 3 VSI: CHECK
Check the ATT/HDG, VOR/ILS, and EFIS SG lights are Check there is no flagging and that the pointer
extinguished. indicates zero.
8 EGPWS: CHECK
4 ALTIMETER: CHECK
Check the EGPWS switch is guarded in normal position Check there is no flagging.
and the GPWS light is not illuminated on CAP.
5 EADI: CHECK
CAPT INSTRUMENT PANEL 6 RMI / EHSI: CHECK
Crosscheck heading information.
1 CLOCK: CHECK
Select RMI on VOR 1 and VOR 2.
Check the time, adjust if necessary.
7 ASI: CHECK
2 ASI: CHECK Check: no flagging
Check: no flag airspeed pointer indicates zero
airspeed pointer indicates zero VMO pointer indicates 250kt.
VMO pointer indicates 250kt.
8 CLOCK: CHECK
3 RMI / EHSI: CHECK Check the time, adjust if necessary.
Crosscheck heading information.
Select RMI on VOR 1 and VOR 2.

CAPT LATERAL & INSTRUMENT PANELS + F/O LATERAL & INSTRUMENT PANELS

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 22 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.4.2. Short transit

Flight events CM1 CM2

DO DO

EXTERNAL INSPECTION ENG 1 FIRE.................................... 3 TESTS

ENG 2 FIRE.................................... 3 TESTS
FDEP (If installed)..... FLIGHT NUMBER+DATE
MCDU (If installed).................................SET
FUEL QTY................................. TEST/CHECK
FUEL USED....................................... RESET
AUTOPRESS......... TEST/LANDING ELEVATION
COCKPIT COM HATCH......................... OPEN

ALL ATR

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 23 01
STANDARD OPERATING
PROCEDURES JUN 09
PRELIMINARY COCKPIT PREPARATION FLOW (SHORT TRANSIT)

1 2 1 ENG 1 FIRE PROTECTION: TEST 3 FDEP (If installed): SET FLIGHT NUMBER +
Check the ENG 1 fire handle is IN and latched. DATE
Extinguish any white light. Check FDAU time base, adjust if necessary.
Depress the SQUIB TEST PB and check both AGENT
SQUIB lights illuminate. 4 MCDU (If installed with the MPC): SET

Select TEST switch on FIRE and check: Set the flight number and check FDAU time base,
ENG FIRE red light illuminates into associated fire adjust if necessary.
handle.
CCAS is activated (CRC + MW + ENG 1 FIRE on 5 FUEL QTY PANEL: TEST and CHECK

CAP) Depress the TEST PB and check:

MC + SC + FUEL on CAP
FUEL SO red light illuminates in CL 1 if temporarily
all lights and displays
selected out of FUEL SO. both LO LVL amber lights illuminated
Select TEST switch on FAULT and check: both RUN green lights illuminated on pumps PB
both LOOP A & B FAULT lights illuminate. check quantity.
2 ENG 2 FIRE PROTECTION: CHECK 6 FUEL USED: RESET
Check the ENG 2 fire handle is IN and latched. Pull reset knob to reset fuel used value.
Extinguish any white light:
Depress the SQUIB TEST PB and check both AGENT 7 AUTO PRESS PANEL: TEST / CHECK
SQUIB lights illuminate. Depress TEST PB and check:
Select TEST switch on FIRE and check: MC + SC + AIR on CAP
ENG FIRE red light illuminates into associated fire FAULT amber light illuminated in MODE SEL PB
handle. display cycling between -8800 and 18800.
CCAS is activated (CRC + MW + ENG 1 FIRE on
8 COCKPIT COM HATCH: OPEN
CAP)
Must be kept open until engine 1 start, in order to avoid
FUEL SO red light illuminates in CL 2 if temporarily pressurization shocks.
selected out of FUEL SO.

ALL ATR
Select TEST switch on FAULT and check:
both LOOP A & B FAULT lights illuminate.
7

5 6

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 24 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.5. Final cockpit preparation

Flight events CM1 CM2

preliminary cockpit ANNOUNCE

preparation FINAL COCKPIT PREPARATION PROCEDURE
complete DO DO
PARKING BRAKE.............. ON & PRESSURE ATIS /WEATHER.............................. NOTED
FUEL QUANTITY..............................CHECK TAKE-OFF DATA CARD...1st part FILLED (1)
MEMO PANEL................................CHECK QNH..................... SET (OWN) AND CHECK
QNH........... SET (own & STBY) AND CHECK

PF
(1) Take-off data card 1ST PART:
Flight number, FROM, TO, date, weather, WLIM,
T/O TQ, RTO TQ, acceleration altitude, single DO
engine flight path, RWY heading. RADIO NAV & RNAV................................SET
(according to expected SID)
VHF 1 & 2..............................................SET

Flight events PNF PF

CREW READY FOR TAKE- READ AND DO

OFF DATA CARD WEATHER........................................ CHECK

ALL ATR
1st PART PROCCEEDING OBJ TORQUE........................................SET
RTO TORQUE...............CHECK AMBER BUGS
ALTIMETERS BUGSSET & CROSSCHECK ALTIMETERS BUGS....... SET & CROSSCHECK
LANDING ELEVATION..SET

CREW READY TO
PERFORM THE
Refer to 01.03 p. 36, departure briefing
DEPARTURE BRIEFING
ANNOUNCE
FINAL COCKPIT PREPARATION PROCEDURE
COMPLETE

Flight events CM1 CM2

FINAL COCKPIT REQUEST AND ANSWER

PREPARATION FINAL COCKPIT PREPARATION C/L
COMPLETE
ANNOUNCE AND READ
FINAL COCKPIT PREPARATION C / L
Refer to QRH normal C/L
C/L COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 25 01
STANDARD OPERATING
FINAL COCKPIT PREPARATION FLOW
PROCEDURES JUN 09

CM1 CM2
1 PARKING BRAKE: ON 1 ATIS/WEATHER: NOTED
Set parking brake ON and check brake accumulator
pressure. 2 TAKE-OFF DATA CARD: 1st PART FILLED
Fill the weather, Wlim (FOS), acceleration altitude and
2 FUEL QUANTITY: CHECK single engine flight path parts.
Check both tanks are symetrically loaded and that the
total matches the flight plan block fuel 3 QNH: SET (own altimeter)
Check and cross-check with CM1.
3 MEMO PANEL: CHECK
Check NO SMKG, SEAT BELTS and PROP BRK blue
lights illuminated. PF
4 QNH: SET (own & STBY altimeters) A NAV 1 & 2: SET (GNSS filled, if equipped,
Check and cross-check with CM2. please refer to 03.01 p. 2, Preflight.)
A A Set NAV 1 & 2, ADF 1 & 2 , GNSS (or GPS receiver)
according to the expected SID.

B VHF 1 & 2: SET

Set VHF 1 & 2 according to the frequencies read on
A Jeppesen chart.
D E 3
4 C TAKE-OFF DATA CARD: 1st PART PROCESSED

D OBJECTIVE TORQUES: SET

ALL ATR
F Set white bugs on the torque gauges.

E ALTIMETER BUGS: SET and cross check

2 3
PNF Set altimeter bugs as per the process described in
01.03 p 18, altimeter setting.
A ALTIMETER BUGS: SET and cross check
Set altimeter bugs as per the process described in F LANDING ELEVATION: SET
section 01.03 p 18, altimeter setting.

B B
1 2
C

FOR TRAINING ONLY

PERSONAL NOTES PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 26 01
STANDARD OPERATING
PROCEDURES JUN 09

3.6. Before propeller rotation (1/2)

Engine 2 start in Hotel mode is decided in accordance with operational requirements and limitations. It is
the Captain decision; at the very least the PRELIMINARY COCKPIT PREPARATION PROCEDURE for
short or long transit shall be completed and the weather recorded and checked.

Flight events CM1 CM2

READY TO START ANNOUNCE

ENGINE 2 IN HOTEL GROUND FROM COCKPIT
MODE READY TO START ENG 2 IN HOTEL MODE, DO
CONFIRM SERVICE DOOR CLOSED SERVICE DOOR............................ CLOSED
AND AREA CLEAR WING LIGHTS...................................... ON
PROP BRAKE......... ON/PROP BRK blue light
ENGINE START SELECT.... A+B (or A or B)*
*A+B for the first starting of the day, then for the
next starting, A for odd days and B for even
days, to detect ignition system hidden failure
ANNOUNCE
RIGHT SIDE CLEAR,
READY TO START ENG 2?
ANNOUNCE
I AM READY

After OUTSIDE DO
VISUAL CHECK START 2 PB........................... DEPRESSED

DO ANNOUNCE
TIMING*............................................START STARTER ON
START 2..................................... CHECK ON
* For starter limitation time,
30 s maxi when starter off (45%NH)
NH=10% DO AND ANNOUNCE
(UNTIL NH=19% if CL 2.......................................... FEATHER
ITT>200C) TIMING*..........................................START
FUEL OPEN
*For ignition time, it should rise within 10 seconds
DO
ENGINE PARAMETERS.....................CHECK

ITT increasING DO ANNOUNCE

ENGINE PARAMETERS.......................CHECK IGNITION
TIMING............................................. STOP

NH=25% DO ANNOUNCE
ENGINE PARAMETERS.......................CHECK When FAULT amber light extinguished
ECU

NH INCREASING DO
ENGINE PARAMETERS.......................CHECK DO AND ANNOUNCE
ENGINE PARAMETERS.....................CHECK
OIL PRESS

NH=45% ANNOUNCE
ANNOUNCE 45%
STARTER OFF
*If not, select rotary selector OFF/START ABORT DO
DO ITT MAX..........................................CHECK
TIMING............................................... STOP
ANNOUNCE
ITT XXX C
42 not PEC

NH = 61.5% ANNOUNCE
PARAMETERS STABILIZED

PARAMETERS
STABILIZED DO
DO ENGINE START............... OFF/START ABORT
DC GEN 2 VOLTAGE..........................CHECK DC EXT PWR................OFF / DISCONNECT
DC GEN 2 FAULT.................EXTINGUISHED
DC BTC............................ CHECK CLOSED
ANNOUNCE
BLEED / PACKS / X VALVE................. OPEN
GROUND FROM COCKPIT, YOU CAN
DISCONNECT GPU

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 27 01
STANDARD OPERATING
PROCEDURES JUN 09

3.6. Before propeller rotation (2/2)

The data card 2nd part proceeding, can be performed during final cockpit preparation, if the load and trim
sheet has been received.

Flight events CM1 CM2

LOAD AND TRIM DO
SHEET ON BOARD LOAD................................................. CHECK

ANNOUNCE DO
TOW .., TRIM SETTING.. CM2 crosschecks TOW and TRIM value before
filling DATA CARD 2nd part
DO TAKE-OFF DATA CARD..2nd PART FILLED
CROSSCHECK............. T/O SPEEDS AND TRIM

Flight events PNF PF

CREW READY FOR DO READ AND DO
TAKE-OFF DATA CARD SPEED BUGS................................ SET AND SPEED BUGS................................ SET AND
2nd PART CROSSCHECK CROSSCHECK
PROCEEDING TRIM..................................... CROSSCHECK TRIM.....................................................SET

Flight events CM1 CM2

PASSENGERS AND DO DO
CARGO ON BOARD CABIN ATTENDANT REPORT.............RECEIVED REQUEST START UP CLEARANCE FROM ATC
CABIN ANNOUNCE...............................DONE

DOORS................................. CHECK CLOSED

CDLS (IF INSTALLED................................. ON
SEAT BELTS ............................................ ON
BEACON.................................................. ON

REQUEST AND ANSWER

BEFORE PROPELLER ROTATION C/L ANNOUNCE AND READ
BEFORE PROPELLER ROTATION C/L
Refer to QRH normal C/L

C/L COMPLETE
42 not PEC

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 26 02
STANDARD OPERATING
PROCEDURES JUN 09

3.6. Before propeller rotation (1/2)

Engine 2 start in Hotel mode is decided in accordance with operational requirements and limitations. It is
the Captain decision; at the very least the PRELIMINARY COCKPIT PREPARATION PROCEDURE for

72 PEC
short or long transit shall be completed and the weather recorded and checked.

Flight events CM1 CM2

READY TO START ANNOUNCE

ENGINE 2 IN HOTEL GROUND FROM COCKPIT
MODE READY TO START ENG 2 IN HOTEL MODE, DO
CONFIRM SERVICE DOOR CLOSED SERVICE DOOR............................ CLOSED
AND AREA CLEAR WING LIGHTS...................................... ON
PROP BRAKE......... ON/PROP BRK blue light
ENGINE START SELECT.... A+B (or A or B)*
*A+B for the first start of the day, then for the
next start, A for odd days and B for even
days, to detect ignition system hidden failure
ANNOUNCE
RIGHT SIDE CLEAR,
READY TO START ENG 2?
ANNOUNCE
I AM READY

42 PEC
After OUTSIDE
VISUAL CHECK DO
START 2 PB........................... DEPRESSED
DO ANNOUNCE
TIMING*............................................START STARTER ON
START 2..................................... CHECK ON
* For starter limitation time,
30 s maxi when starter off (45%NH)
NH=10% DO AND ANNOUNCE
(UNTIL NH=19% if CL 2.......................................... FEATHER
ITT>200C) TIMING*..........................................START
FUEL OPEN
*For ignition time, it should rise within 10 seconds
DO

72 not PEC
ENGINE PARAMETERS.....................CHECK

ITT increasING DO ANNOUNCE

ENGINE PARAMETERS.......................CHECK IGNITION
TIMING............................................. STOP

NH INCREASING DO
ENGINE PARAMETERS.......................CHECK DO AND ANNOUNCE
ENGINE PARAMETERS.....................CHECK
OIL PRESS

NH=45% ANNOUNCE
ANNOUNCE 45%
STARTER OFF
DO
*If not, select rotary selector OFF/START ABORT ITT MAX..........................................CHECK
DO
TIMING............................................... STOP ANNOUNCE
ITT XXX C

NH=61.5% ANNOUNCE
PARAMETERS STABILIZED

PARAMETERS
STABILIZED DO
DO ENGINE START............... OFF/START ABORT
DC GEN 2 VOLTAGE..........................CHECK DC EXT PWR................OFF / DISCONNECT
DC GEN 2 FAULT.................EXTINGUISHED
DC BTC............................ CHECK CLOSED
ANNOUNCE BLEED / PACKS / X VALVE................. OPEN
GROUND FROM COCKPIT, YOU CAN
DISCONNECT GPU

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 27 02
STANDARD OPERATING
PROCEDURES JUN 09

3.6. Before propeller rotation (2/2)

The data card 2nd part proceeding, can be performed during final cockpit preparation, if the load and trim
sheet has been received.
72 PEC

Flight events CM1 CM2

LOAD AND TRIM DO
SHEET ON BOARD LOAD................................................. CHECK

ANNOUNCE DO
TOW .., TRIM SETTING.. CM2 crosschecks TOW and TRIM value before
filling DATA CARD 2nd part
DO TAKE-OFF DATA CARD..2nd PART FILLED
CROSSCHECK............. T/O SPEEDS AND TRIM

Flight events PNF PF

CREW READY FOR DO READ AND DO
TAKE-OFF DATA CARD SPEED BUGS................................ SET AND SPEED BUGS................................ SET AND
42 PEC

2nd PART CROSSCHECK CROSSCHECK

PROCEEDING TRIM..................................... CROSSCHECK TRIM.....................................................SET

Flight events CM1 CM2

PASSENGERS AND DO DO
CARGO ON BOARD CABIN ATTENDANT REPORT.............RECEIVED REQUEST START UP CLEARANCE FROM ATC
CABIN ANNOUNCE...............................DONE

DOORS................................. CHECK CLOSED

CDLS (IF INSTALLED................................. ON
SEAT BELTS ............................................ ON
BEACON.................................................. ON

REQUEST AND ANSWER

BEFORE PROPELLER ROTATION C/L ANNOUNCE AND READ
BEFORE PROPELLER ROTATION C/L
72 not PEC

Refer to QRH normal C/L

C/L COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 28 01
STANDARD OPERATING
PROCEDURES JUN 09

BEFORE PROPELLER ROTATION FLOW (1/3)

CM1 CM2
1 MECHANICAL CALL: PERFORMED 1 U CHECK: PERFORMED
Start timing when CM2 announces Starter ON. DOORS: CLOSED
Check the UNLK amber light is extinguished.
2 TIMING: START WING LIGHTS: ON, to visually inform that start is in Hotel
1 9 Start timing when CM2 announces Starter ON. Mode.
1 3 Fuel Pump N2: RUN
2
7 5 8 3 STARTER 2: CHECK ON PROPELLER BRAKE : ON
If no AC GPU, press HYD AUX PUMP, in order to get the
10 4 ENGINE PARAMETERS: MONITOR READY green light, then place the propeller brake switch
According to the CM2 callouts. to ON.
ENGINE START ROTARY SELECTOR: A+B
5 START OFF: CHECK
At 45% NH, check the Start ON light is extinguished 2 START PB: DEPRESSED
and announce STARTER OFF and stop timing. START 2 PB: ON
Depress START 2 PB after a visual check on right side.
6 DC GEN 2 VOLTAGE: CHECK Announce: STARTER ON.

7 MECH CALL: PERFORMED 3 CL2: FEATHER

When CM2 switches off the external pwr, CM1 ask Advance CL 2 to feather when NH reaches 10% and
the mechanic to disconnect the GPU. announce: FUEL OPEN.
6
4 TIMING: START
4
2 5 ENGINE PARAMETERS: MONITOR
When ITT needle increases, announce: IGNITION. ITT

ALL ATR
must increase within 10 sec on CM1 Timing. Otherwise
5 CL2 shut off.
7
4 6 ECU FAULT LIGHT: EXTINGUISH
At 25% NH, check ECU fault light exinguishes, announce
ECU ON.

7 ENGINE PARAMETERS: MONITOR

OIL PRESS needle increases, announce OIL PRESS
At 45% NH, announce 45%.

8 ENGINE START ROTARY SELECTOR: OFF

When engine parameters are stabilised, announce
PARAMETERS STABLISED, then turn the rotary
selector to OFF/START ABORT.

9 DC EXTERNAL POWER: OFF / DISCONNECT

When OFF check that the DC GEN 2 FAULT light
extinguishes and BTC still closed.
3
10 BLEED 2 / PACKS 1+2 / X VALVE: OPEN
When only one BLEED is on OPEN on ground, X VALVE is
6 opened to supply both packs.

FOR TRAINING ONLY

PERSONAL NOTES PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 29 01
STANDARD OPERATING
PROCEDURES JUN 09

BEFORE PROPELLER ROTATION FLOW (2/3)

CM1 CM2
1 LOAD AND TRIM SHEET: CHECK 1 TAKE-OFF DATA CARD: 2ND PART FILLED
Check and announce TOW and Trim setting. Fill TOW, speeds and trim setting parts.

PNF PF
A SPEED BUGS: SET DATA CARD 2ND PART PROCEEDING
Set speed bugs and cross-check.
A SPEED BUGS: SET

B TRIM: CROSSCHECK Set speed bugs and cross-check.

B TRIM: SET

A
A

ALL ATR
B B

1
1

FOR TRAINING ONLY

PERSONAL NOTES PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 30 01
STANDARD OPERATING
PROCEDURES JUN 09

BEFORE PROPELLER ROTATION FLOW (3/3)

CM1
1 DOORS: CLOSED
Check the UNLK amber light extinguished.

2 CDLS (if installed): ON

The control switch located behind the first officer is
1 ON.
On the cockpit door control panel (pedestal), the
toggle switch is in the close position and the
Open light is off.
4 3
3 SEAT BELTS: ON

4 BEACON LIGHT: ON
As propellers will rotate, beacon lights must be
switched ON.

ALL ATR
2

FOR TRAINING ONLY

PERSONAL NOTES PERSONAL NOTES

FOR TRAINING ONLY FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 31 01
STANDARD OPERATING
PROCEDURES JUN 09

3.7. Before taxi (1/2)

Flight events CM1 CM2

START UP CLEARANCE ORDER

RECEIVED BEFORE TAXI PROCEDURE
ANNOUNCE
GROUND FROM COCKPIT
PARKING BRAKE IS ON, READY TO
RELEASE PROPELLER BRAKE,
CONFIRM CHOCKS ON, DOORS CLOSED,
AIRCRAFT CLEAR

ANNOUNCE
RIGHT SIDE CLEAR? ANSWER
DO RIGHT SIDE CLEAR!
HYD AUX PUMP.............................. DEPRESS
PROP BRAKE............ CHECK READY LIGHT ON

DO
PROP BRAKE...........................................OFF
ANNOUNCE (AFTER VISUAL CHECK)
NP STABILIZED................................... CHECK ROTATION

ORDER
CL 2 MAX RPM

DO
CL 2.............................................. MAX RPM

ANNOUNCE
LOW PITCH

WHEN NP STABILIZED DO
AROUND 71 % ACW GEN 2 FAULT.................. EXTINGUISHED
ACW BTC......................................... CLOSED
HYDRAULIC PANEL..............NO AMBER LIGHT
ANTI ICING............................ ON if icing cond.
HYD INDICATORS........................3 X 3000PSI
ANTISKID.............................................. TEST
FLAPS..................................................... 15

72 not PEC
ENG 1 START: FOR TRAINING PURPOSE ENG 1 START ON APRON IS DEPICTED. Please refer to 04.06 p.1, Start up engine n1 during
taxiing.

Flight events CM1 CM2

ENGINE 1 START ANNOUNCE

GROUND FROM COCKPIT DO (U CHECK)
PARKING BRAKE IS ON, READY TO DOORS............................................ CLOSED
START ENG 1, CONFIRM CHOCKS ON, DOORS ENGINE START SELECT......... A+B (or A or B)*
CLOSED, AIRCRAFT CLEAR *A+B for the first start of the day, then for the next
start, A for odd days and B for even days, to
detect ignition system hidden failure.

ANNOUNCE
CONFIRM LEFT SIDE CLEAR,
ANNOUNCE
READY TO START ENG N 1?
LEFT SIDE CLEAR,
42 not PEC

I AM READY
DO
START 1 PB................................ DEPRESSED

ANNOUNCE
STARTER ON
DO
TIMING*.............................................. START
START 1........................................CHECK ON
* For starter limitation time , 30 s maxi
when starter off (45% NH)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 32 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

3.7. Before taxi (2/2)

Flight events CM1 CM2

NH = 10% DO AND ANNOUNCE

(UNTIL NH=19% if CL 1............................................. FEATHER
ITT>200C) TIMING*............................................ START
FUEL OPEN
*For ignition time, ITT should rise within 10 seconds

ITT increasING DO ANNOUNCE

ENGINE PARAMETERS...................... CHECK IGNITION
TIMING...............................................STOP

NH = 25% DO ANNOUNCE When FAULT amber light extinguished

ENGINE PARAMETERS...................... CHECK ECU
42 not PEC
NH INCREASING DO DO AND ANNOUNCE
ENGINE PARAMETERS...................... CHECK ENGINE PARAMETERS...................... CHECK
OIL PRESS

NH = 45% ANNOUNCE
45%
ANNOUNCE
STARTER OFF DO
* If not, rotary selector OFF/START ABORT ITT MAX........................................... CHECK
DO
TIMING...............................................STOP
ANNOUNCE
DO ITT XXX C
ENGINE PARAMETERS...................... CHECK

NH = 61.5% ANNOUNCE
PARAMETERS STABILIZED

PARAMETERS DO
STABILIZED ENGINE START...............OFF &START ABORT
DC GEN 1 FAULT.................. EXTINGUISHED
DC BTC..................... CHECK EXTINGUISHED
BLEED / PACKS......... lights extinguished
ORDER
CL 1 MAX RPM DO
CL 1............................................ MAX RPM
72 not PEC

ANNOUNCE
LOW PITCH

WHEN NP STABILIZED DO
AROUND 71 % COCKPIT COM HATCH......................CLOSE CHECK
ACW GEN 1................................... ON LINE
OVERHEAD PANEL DARK (EXCEPTED THE FAULT
LIGHT ON EXHAUST MODE P/B FOR 2 MINUTES)

PROCEDURE COMPLETE ANNOUNCE

BEFORE TAXI PROCEDURE COMPLETE
REQUEST AND ANSWER
BEFORE TAXI CHECKLIST
ANNOUNCE AND READ
BEFORE TAXI CHECKLIST

Refer TO QRH 6.01

ANNOUNCE
C/L COMPLETE
42 not PEC

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 31 02
STANDARD OPERATING
PROCEDURES JUN 09

3.7. Before taxi (1/2)

Flight events CM1 CM2

72 PEC
START UP CLEARANCE ORDER
RECEIVED BEFORE TAXI PROCEDURE
ANNOUNCE
GROUND FROM COCKPIT
PARKING BRAKE IS ON, READY TO
RELEASE PROPELLER BRAKE,
CONFIRM CHOCKS ON, AIRCRAFT CLEAR

ANNOUNCE ANSWER
"RIGHT SIDE CLEAR"
RIGHT SIDE CLEAR?
DO
HYD AUX PUMP........................... DEPRESS
PROP BRAKE.....................READY LIGHT ON

DO ANNOUNCE (AFTER VISUAL CHECK)

PROP BRAKE........................................OFF ROTATION
NP STABILIZED................................. CHECK

42 PEC
ORDER
CL 2 AUTO DO
CL 2.................................................. AUTO

ANNOUNCE
SINGLE CHANNEL LOW PITCH

WHEN NP STABILIZED DO
AROUND 71% ACW GEN 2 FAULT................ EXTINGUISHED
ACW BTC....................................... CLOSED
HYDRAULIC PANEL............NO AMBER LIGHT
ANTI ICING.......................... ON if icing cond.
HYD INDICATORS......................3 X 3000PSI
ANTISKID............................................ TEST
FLAPS................................................... 15

ENG 1 START: FOR TRAINING PURPOSE ENG 1 START ON APRON IS DEPICTED. Please refer to 04.06 p.1, Start up engine n1
during taxiing.

Flight events CM1 CM2

ENGINE 1 START
ANNOUNCE
GROUND FROM COCKPIT DO (U CHECK)
PARKING BRAKE IS ON, READY TO DOORS.......................................... CLOSED
START ENG 1, CONFIRM CHOCKS ON, DOORS ENGINE START SELECT....... A+B (or A or B)*
CLOSED, AIRCRAFT CLEAR *A+B for the first starting of the day, then for the next
starting, A for odd days and B for even days, to detect
ignition system hidden failure

ANNOUNCE
ANNOUNCE CONFIRM LEFT SIDE CLEAR,
LEFT SIDE CLEAR, I AM READY READY TO START ENG N 1?

DO
STARTER 1 PB.......................... DEPRESSED

DO ANNOUNCE
TIMING*............................................ START STARTER ON

START 1......................................CHECK ON
* For starter limitation time , 30 s maxi
when starter off (45%NH)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 32 02
STANDARD OPERATING
PROCEDURES JUN 09

3.7. Before taxi (2/2)

Flight events CM1 CM2
72 PEC

NH = 10% DO AND ANNOUNCE

(UNTIL NH=19% if CL 1............................................. FEATHER
ITT>200C) TIMING*............................................ START
FUEL OPEN
*For ignition time, ITT should rise within 10 seconds

ITT increasING DO ANNOUNCE

ENGINE PARAMETERS...................... CHECK IGNITION
TIMING...............................................STOP
NH INCREASING
DO DO AND ANNOUNCE
ENGINE PARAMETERS...................... CHECK ENGINE PARAMETERS...................... CHECK
OIL PRESS

NH = 45% ANNOUNCE
ANNOUNCE 45%
STARTER OFF DO
*If not, select rotary selector OFF/START ABORT ITT MAX........................................... CHECK
DO
42 PEC

TIMING...............................................STOP ANNOUNCE
ITT XXX C
DO
ENGINE PARAMETERS...................... CHECK
NH = 61.5% ANNOUNCE
PARAMETERS STABILIZED

PARAMETERS DO
STABILIZED ENGINE START...............OFF &START ABORT
DC GEN 1 FAULT.................. EXTINGUISHED
DC BTC..................... CHECK EXTINGUISHED
BLEED / PACKS......... lights extinguished
ORDER
CL 1 AUTO DO
CL 1.................................................. AUTO
ANNOUNCE
SINGLE CHANNEL LOW PITCH

WHEN NP STABILIZED DO CHECK

COCKPIT COM HATCH......................CLOSE ACW GEN 1................................... ON LINE
AROUND 71%
OVERHEAD PANEL DARK (EXCEPTED THE FAULT
LIGHT ON EXHAUST MODE PB FOR 2 MINUTES)

PROCEDURE ANNOUNCE
COMPLETE BEFORE TAXI PROCEDURE COMPLETE
REQUEST AND ANSWER
BEFORE TAXI CHECKLIST
ANNOUNCE AND READ
BEFORE TAXI CHECKLIST

Refer TO QRH 6.01

ANNOUNCE
C/L COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 33 01
STANDARD OPERATING
PROCEDURES JUN 09

BEFORE TAXI FLOW (1/2)

CM1 CM2
1 HYD AUX PUMP PB: DEPRESSED 1 CL 2: MAX RPM (4NP, 7NP) / AUTO (4P, 7P)
5 Press PB to get the PROP BRK READY light on.
1 PEC SINGLE CHANNEL TEST: CHECK
4 Check SGL CH is illuminated then extinguished.
2 PROP BRK SWITCH: OFF
After outside visual check. 2 LO PITCH LIGHT: ILLUMINATED
6 Check the ready light
PROP BRK SWITCH set to OFF
2 Check UNLOCK extinguished after maximum
15 seconds.

3 ENGINE PARAMETERS: MONITOR

NP stabilized 3 ENGINE PARAMETERS: MONITOR

4 ACW GEN 2: ON LINE

When parameters stabilised, check ACW GEN 2 on line
BTCs closed.

5 HYDRAULIC PANEL: DARK

6 ANTI-ICING: ON
2 7 When icing conditions prevail on take-off

7 ACCUMULATORS GAUGES : 3 x 3000 PSI

3 8

ALL ATR
3
8 ANTISKID: TEST
1 Check MC + SC + WHEELS and FFFF appearing
72 PEC
during 6 seconds.
42 PEC
9 FLAPS 15: SELECTED

1
1

FOR TRAINING ONLY

PERSONAL NOTES PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 34 01
STANDARD OPERATING
PROCEDURES JUN 09

BEFORE TAXI FLOW (2/2)

CM1 CM2
1 MECH CALL: PERFORMED 1 U CHECK: PERFORMED
Check ground clearance with the mechanic. Check doors closed, ELEC FUEL PUMP 1 runs,
BEACON on.
1 11 2 LEFT SIDE CLEAR
Left visual check. 2 ENGINE START ROTARY SELECTOR: A+B (or

2 A or B) START 1 PB: ON
3 TIMING: START Depress START 1 PB after a visual check on right side.
8
Start timing when CM2 depress.
1 START PB. 3 CL 1: FEATHER
Advance CL 1 to feather when NH reaches 10%.
4 TIMING: STOP
Stop timing when STARTER 1 extinguish. 4 TIMING: START
Start timing when CL1 is set to FEATHER and stop
5 COCKPIT COM HATCH when ignition is confirmed, in order to monitor ignition
CLOSE. time, maximum 10 sec.

2 5 ENGINE PARAMETERS: MONITOR

When ITT needle increases, announce: IGNITION.
42 not PEC
6 ECU FAULT LIGHT: EXTINGUISH
At 25% NH, check ECU fault light exinguishes,
10 6 announce ECU ON.
3 4 7 ENGINE PARAMETERS: MONITOR
4 42 PEC

ALL ATR
OIL PRESS needle increases, announce OIL PRESS
72 PEC 9 5 At 45% NH, announce 45%
Stop timing, if STARTER OFF call out has been
7 received.

8 ENGINE START ROTARY SELECTOR: OFF

When engine parameters are stabilized, announce
PARAMETERS STABILIZED, then turn the rotary
selector to OFF/START ABORT.

9 CL 1: MAX RPM/AUTO

9 PEC SINGLE CHANNEL TEST: CHECK

9
Check SGL CH illuminated then extinguished.

10 LO PITCH LIGHT: ILLUMINATED

11 ACW GEN 1: ON LINE

3 Check ACW BTCs OPEN.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 35 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.8. Taxi

Flight events CM1 CM2

READY TO TAXI ORDER

REQUEST TAXI CLEARANCE DO
TAXI CLEARANCE...................... REQUESTED

TAXI CLEARANCE ANNOUNCE

RECEIVED GROUND FROM COCKPIT, READY TO TAXI,
YOU CAN REMOVE CHOCKS AND DISCONNECT

WHEN GROUND
STAFF IN SIGHT ON DO DO
CAPTAINS SIDE BLOCK TIME............................ ANNOUNCED
SAFETY.............................CHECK LEFT SIDE SAFETY...............................CHECK RIGHT SIDE
LEFT SIDE AREA................................CLEAR RIGHT SIDE AREA....................................CLEAR
TAXI & T/O LIGHT.................................... ON
PARKING BRAKE......................... RELEASED

BRAKES CHECK: for passenger comfort, the following procedure can be used:
set taxi power
parking brake handle from ON to EMER position
then CM 2 checks brakes (parking brake released)
then CM 1 checks brakes (CM 2 releases) and CM 1 starts to taxi.

ON TAXIWAY
ORDER

ALL ATR
TAXI PROCEDURE DO
DO INSTRUMENTS................................CHECK*
INSTRUMENTS................................CHECK* HDG MODE................................. SELECTED
Rudder cam............................... Centered LO BANK.................................... SELECTED
IAS MODE................................... SELECTED
IAS........................................V2 + 5 kt SET
COUPLING......................................PF SIDE
* CHECK HEADING, BEARINGS, HORIZON / RMI T/O CONFIG TEST......................PERFORMED

WHEN PF AND PNF PF

READY
DO
T/O BRIEFING..................PERFORMED
Refer to 01.03 p. 37, take-off briefing.

AFTER PF TAKE-OFF ANNOUNCE

BRIEFING TAXI PROCEDURE COMPLETE

WHEN TAXI
PROCEDURE REQUEST AND ANSWER ANNOUNCE AND READ
COMPLETE TAXI CHECKLIST TAXI CHECKLIST

Refer to QRH 6.01

ANNOUNCE
C/L COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 36 01
STANDARD OPERATING
PROCEDURES JUN 09

TAXI FLOW
CM1 CM2
1 BLOCK TIME: ANNOUNCED 1 TAXI CLEARANCE: REQUESTED
CM2 reports block time on the navigation log.
2 RIGHT SIDE AREA: CLEAR CHECK RIGHT
2 LEFT SIDE AREA: CLEAR CHECK LEFT SIDE SIDE

3 TAXI AND T/O LIGHTS: ON 3 BRAKES: CHECK

When on the taxiway the parking brake light has been
turned on, CM1 must switch it off. 4 INSTRUMENTS: CHECK
Check Heading (including STBY compass), Bearings,
3 4 PARKING BRAKE: RELEASED Horizon / RMI.

5 BRAKES: CHECK 5 AFCS: SET

For passenger confort, the following procedure can be Select: HDG LO BANK
used: IAS V2+5
Set Taxi power CPL on PF side
2 Parking brake handle from ON to EMER ALT SEL on first clearance.
position
2 5 6 T/O CONFIG TEST: PERFORMED
Then CM2 checks brakes
Then CM1 checks brakes and CM1 starts to taxi. T/O config test checks aircraft configuration for
take-off and provides an automatic Recall.
6 INSTRUMENTS: CHECK
Check Heading, Bearings, Horizon / RMI.
6 4 7 RUDDER CAM: CENTERED
1

ALL ATR
Center pedals then move the rudder trim to the right
then to the left to center the RCU.

5 3

6
1

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 37 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.9. Before take-off

Flight events CM1 CM2

APPROACHING ORDER
HOLDING POINT AND BEFORE TAKE-OFF PROCEDURE DO
CABIN OK RECEIVED TCAS................................................. AUTO
XPDR.................................................... ALT
GUST LOCK................................ RELEASED

DO DO
FLT CTL.........................SPOILER & RUDDER FLT CTL............................... ROLL / SPOILER
FLT CTL.............................................. PITCH

LINE-UP CLEARANCE DO DO
RECEIVED RECALL PB.............................DEPRESSED* WEATHER RADAR................... AS REQUIRED
TO INHI.................................... DEPRESSED CONT RELIGHT....................... AS REQUIRED
LAND LIGHTS / STROBE.......................... ON BLEED VALVES......................................OFF
AIR FLOW......................................... NORM
* Recall PB may be depressed before T/O INHI PB to APM ROTARY SELECTOR
make sure you will not take-off with degraded sytems. (if installed)................................ TO WEIGHT

DO
DO
LATERAL FD BAR.........................CENTERED
LATERAL FD BAR.........................CENTERED
(CHECK MAGNETIC RWY ORIENTATION)
ANNOUNCE
BEFORE TAKE-OFF PROCEDURE COMPLETE

PROCEDURE REQUEST AND ANSWER

ANNOUNCE AND READ
COMPLETE BEFORE TAKE-OFF CHECKLIST
BEFORE TAKE-OFF CHECKLIST

Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

42 not PEC

FOR TRAINING ONLY

PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 37 02
STANDARD OPERATING
PROCEDURES JUN 09

3.9. Before take-off

Flight
72 PEC

events CM1 CM2

APPROACHING ORDER
HOLDING POINT BEFORE TAKE-OFF PROCEDURE DO
AND CABIN OK TCAS................................................. AUTO
RECEIVED XPDR.................................................... ALT
GUST LOCK................................ RELEASED

DO DO
FLT CTL..................... SPOILER & RUDDER FLT CTL............................... ROLL / SPOILER
` FLT CTL.............................................. PITCH

LINE-UP DO DO
CLEARANCE RECALL PB.................... DEPRESSED* WEATHER RADAR................... AS REQUIRED
RECEIVED TO INHI............................ DEPRESSED BLEED VALVES....................... AS REQUIRED
LAND LIGHTS / STROBE..................ON AIR FLOW......................................... NORM
72 PEC APM ROTARY SELECTOR
* Recall PB may be depressed before T/O INHI PB (if installed)................................ TO WEIGHT
42 PEC to make sure you will not take-off
42 PEC

with degraded sytems.

DO DO
LATERAL FD BAR.................CENTERED LATERAL FD BAR.........................CENTERED
(CHECK MAGNETIC RWY ORIENTATION)
ANNOUNCE
BEFORE TAKE-OFF PROCEDURE COMPLETE

DO
LINE-UP DO WEATHER RADAR................... AS REQUIRED
CLEARANCE RECALL PB.................... DEPRESSED* CONT RELIGHT....................... AS REQUIRED
RECEIVED TO INHI............................ DEPRESSED BLEED VALVES....................... AS REQUIRED
72 not PEC LAND LIGHTS / STROBE..................ON AIR FLOW......................................... NORM
APM ROTARY SELECTOR
* Recall PB may be depressed before T/O INHI PB (if installed)................................ TO WEIGHT
to make sure you will not take-off
72 not PEC

with degraded sytems.

DO
LATERAL FD BAR.........................CENTERED
DO
LATERAL FD BAR.................CENTERED ANNOUNCE
(CHECK MAGNETIC RWY ORIENTATION) BEFORE TAKE-OFF PROCEDURE COMPLETE

ANNOUNCE AND READ

PROCEDURE REQUEST AND ANSWER BEFORE TAKE-OFF CHECKLIST
COMPLETE BEFORE TAKE-OFF CHECKLIST
Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 38 01
STANDARD OPERATING
PROCEDURES JUN 09

BEFORE TAKE-OFF FLOW

CM1 CM2
1 4 1 SPOILERS: CHECK 1 TCAS: AUTO
Look outside if the spoiler deflects, announce It is normal to have TA ONLY on VSI.
SPOILER and check that the blue triangle appears
on the overhead panel, announce BLUE LIGHT. 2 XPDR: ALT
1 It activates the mode S.
2 RECALL PB, THEN T/O INHI PB : DEPRESSED
8
RCL PB has to be depressed before T/O INHI PB. 3 GUST LOCK: RELEASED
6
7 4 Announce Flight Controls ?
3 LAND AND STROBE LIGHTS: ON
7 4 FLT CONTROLS: CHECK
3
Once aligned: Check ROLL / SPOILER and PITCH
72 PEC Look outside if the spoiler deflects, announce
4 FD BARS: CENTERED SPOILER and check that the blue triangle appears
42 PEC To check that runway heading is correct. on the overhead panel, announce BLUE LIGHT.
72 not PEC 5 WEATHER RADAR: STBY or WX
To activate the EGPWS terrain clearance floor mode.

6 CONT RELIGHT: AS REQUIRED (ON 42/72

NO PEC ONLY)
Switch on if icing condition, contaminated runway or
heavy rain.
4 10
7 BLEED VALVES: OFF
9

ALL ATR
7 BLEED VALVES: ON or OFF
2
8 AIR FLOW: AS REQUIRED

Once aligned:
4
5 9 APM ROTARY SELECTOR: TAKE-OFF WEIGHT
Set the TOW on the rotactor
Even if it is the same weight the rotactor should be
moved to take into account the selected weight.
The APM should be selected with both engines
running.
3 Indeed, during start, microcuts on the supplying may
occur and if the selector is moved before engine start,
the TO weight may not be taken into account.

10 LATERAL FD BARS: CENTERED

To check that runway heading is correct.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 39 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.10. Take-off

Flight events CM1 CM2

READY TO TAKE-OFF ANNOUNCE

TAKE-OFF AT XXX OCLOCK,
V1 XXX KT

DO DO
TIMING............................................. START TIMING............................................. START
FUEL USED...................................... CHECK CONTROL WHEEL........HOLD TOWARD WIND
NOSE WHEEL STEERING................ HANDED

DO
PLs.................. ADVANCED TO WHITE MARK

ANNOUNCE
SET POWER
DO
TAKE-OFF TORQUE........................ ADJUST*
ENGINE PARAMETERS................... CHECK**

* TQ: T/O VALUE (white bug)

** NP: 100 %, ITT

ANNOUNCE
ATPCS ARMED
POWER SET

REACHING 70 KT READ ANNOUNCE

ON THE STBY ASI AND 70 KTS
CM 2 ASI ANNOUNCE AND DO
CHECK (on CM 1 ASI)
NOSE WHEEL STEERING............. RELEASED
YOUR CONTROL

Flight events PNF PF

FLIGHT CONTROLS ANNOUNCE

TRANSFER I HAVE CONTROL

REACHING V1 ANNOUNCE
V1

CM1

DO
PLs................................... RELEASED

REACHING VR ANNOUNCE
ROTATE DO
PITCH....ROTATE TO 10 & FOLLOW FD BARS

POSITIVE RATE ANNOUNCE

POSITIVE RATE ORDER
GEAR UP
42 not PEC

DO
LANDING GEAR LEVER............................ UP
YAW DAMPER........................................ ON
TAXI & T/O LIGHT...................................OFF

WHEN ALL LIGHTS

EXTINGUISHED ON THE ANNOUNCE
LDG GEAR PANEL GEAR UP

FOR TRAINING ONLY

PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 39 02
STANDARD OPERATING
PROCEDURES JUN 09

3.10. Take-off
Flight
events CM1 CM2
72 PEC

READY TO ANNOUNCE
TAKE-OFF TAKE-OFF AT XXX OCLOCK,
V1 XXX KT

DO DO
TIMING............................................. START TIMING............................................. START
NOSE WHEEL STEERING................ HANDED CONTROL WHEEL........HOLD TOWARD WIND

DO
PLs................................................. NOTCH

ANNOUNCE
SET POWER
DO
TAKE-OFF TORQUE..........................CHECK*
ENGINE PARAMETERS................... CHECK**
42 PEC

* TQ: T/O VALUE (white bug)

** NP: 100%, ITT

ANNOUNCE
ATPCS ARMED
POWER SET

REACHING 70 ANNOUNCE
KT READ ON 70 KTS
THE STBY ASI ANNOUNCE AND DO
AND CM 2 ASI CHECK (on CM 1 ASI)
NOSE WHEEL STEERING............. RELEASED
YOUR CONTROL

Flight
events PNF PF
72 not PEC

FLIGHT
CONTROLS ANNOUNCE
TRANSFER I HAVE CONTROL

REACHING V1 ANNOUNCE
V1

CM1

DO
PLs................................... RELEASED

REACHING VR ANNOUNCE
ROTATE DO
PITCH....ROTATE TO 10 & FOLLOW FD BARS

POSITIVE RATE ANNOUNCE

POSITIVE RATE ORDER
GEAR UP
DO
LANDING GEAR LEVER............................ UP
YAW DAMPER........................................ ON
TAXI & T/O LIGHT...................................OFF

WHEN ALL
LIGHTS ANNOUNCE
EXTINGUISHED GEAR UP
ON THE LDG
GEAR PANEL

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 40 01
STANDARD OPERATING
PROCEDURES JUN 09

TAKE-OFF FLOW
CM1 CM2
1 TIMING: START 1 TIMING: START
Announce TAKE-OFF AT ___ OCLOCK, V1 ___ Kt.
2 CONTROL WHEEL: HOLD TOWARD WIND
2 FUEL USED: CHECK
3 + 4 TAKE-OFF TORQUES: ADJUSTED/CHECK
3 NOSE WHEEL STEERING: HANDED By acting on PLs, adjust/check torque needles to white
bug, check Np=100%.
4 POWER LEVERS: ADVANCED
Advance PLs to the white mark/notch and order 5 ATPCS LIGHT: ARM ILLUMINATED

C SET POWER. Check ARM green light illuminated.

5 NOSE WHEEL STEERING: RELEASED 6 IAS: MONITOR

At 70 Kt, release nose wheel steering. PF controls At 70 Kt, announce 70 KT. Read on STBY ASI
aircraft through rudder.

6 POWER LEVERS: RELEASED PF

At V1, release PLs.
A FD BARS: FOLLOWED
B
PNF
6 5
A LANDING GEAR LEVER: UP
4 A
1 A 1
B YAW DAMPER: ON

ALL ATR
Check white lights illuminated.

C TAXI & TO. LIGHT: OFF

Control 2
wheel

5 2

3
4
6

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 41 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.11. Climb sequence

Flight events PNF PF

REACHING ANNOUNCE
ACCELERATION ACCELERATION ALTITUDE DO
ALTITUDE RETARD PL......................... WHITE MARKS*

NOTE: Mini 400 ft ORDER

AGL or higher if CLIMB SEQUENCE
requested
DO
IAS............ INCREASED (ABOVE WHITE BUG)
PL.........................CHECK IN WHITE MARKS
PWR MGT......................................... CLIMB
CLs........................................ WHITE MARK
BLEEDS................................................. ON
IAS........................................... 160 KT SET
CL....................................ADJUST NP 86 %
PLs........ ADJUST TORQUE TO AMBER BUGS
CONT RELIGHT....................... AS REQUIRED

ANNOUNCE
CLIMB SEQUENCE COMPLETE

* In order to prevent over torques, PF retards PLs prior to reducing CLs.

42 not PEC

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 41 02
STANDARD OPERATING
PROCEDURES JUN 09

3.11. Climb sequence

Flight events PNF PF

REACHING ANNOUNCE
ACCELERATION ACCELERATION ALTITUDE DO
ALTITUDE
PL............................CHECK IN THE NOTCH*
NOTE: Mini 400 ft
AGL or higher if ORDER
requested CLIMB SEQUENCE
DO
IAS............ INCREASED (ABOVE WHITE BUG)
PL............................. CHECK IN THE NOTCH
PWR MGT......................................... CLIMB
CLs........................................ WHITE MARK
BLEEDS................................SET ON IF NOT
IAS........................................... 170 KT SET
CLs........................................ADJUST 86%
CONT RELIGHT....................... AS REQUIRED

ANNOUNCE
CLIMB SEQUENCE COMPLETE

* In order to prevent over torques, PF checks PL in the notch before moving the PWR MGT. This is to standardize all the ATR
fleet with the go-around and the optional 100% RTO at take-off procedures, which is only available on PW127M engines.

72 not PEC

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 41 03
STANDARD OPERATING
PROCEDURES JUN 09

3.11. Climb sequence

72 PEC

Flight events PNF PF

REACHING ANNOUNCE
ACCELERATION ACCELERATION ALTITUDE DO
ALTITUDE PL............................CHECK IN THE NOTCH*

NOTE: Mini 400 ft

ORDER
AGL or higher if
CLIMB SEQUENCE
requested
DO
IAS............ INCREASED (ABOVE WHITE BUG)
PL............................. CHECK IN THE NOTCH
PWR MGT......................................... CLIMB
BLEEDS................................SET ON IF NOT
IAS.................................... 160 / 170 KT SET

ANNOUNCE
42 PEC

CLIMB SEQUENCE COMPLETE

* In order to prevent over torques, PF checks PL in the notch before moving the PWR MGT. This is to standardize all the ATR
fleet with the go-around and the optional 100% RTO at take-off procedures, which is only available on PW127M engines.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 42 01
STANDARD OPERATING
PROCEDURES JUN 09

CLIMB SEQUENCE FLOW

PNF PF
A ALTIMETER: ACCELERATION ALTITUDE A POWER LEVERS: TQ MINUS 10%
Announce Acceleration altitude Retard PL at Acceleration altitude

B IAS: INCREASED
42 not PEC Increase IAS above white bug by using the pitch wheel
72 not PEC F AFTER PL CHECKED IN THE NOTCH

E C PWR MGT: CLIMB

42 not PEC
D CONDITION LEVERS: WHITE MARK

E BLEEDS: ON

F CONT RELIGHT: AS REQUIRED

G IAS: 160 KT/170 KT

G
H CONDITION LEVERS: ADJUSTED
B
Adjust NP to 86 %

I POWER LEVERS: ADJUSTED

A Adjust TQ needle to amber bug

ALL ATR
C

H
I D
42 not PEC
A

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 43 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.12. After take-off

Flight events PNF PF

REACHING WHITE OR ANNOUNCE

RED BUG (according to WHITE BUG NORMAL CONDITIONS
external conditions) RED BUG ICING CONDITIONS

ORDER
DO FLAPS 0
FLAPS LEVER................................ SET TO 0

WHEN FLAPS AT 0 ON ANNOUNCE

THE FLAPS INDICATOR FLAPS 0

REACHING WHITE OR ANNOUNCE

RED BUG + 10 (according WHITE BUG + 10 NORMAL CONDITIONS
to external conditions) RED BUG + 10 ICING CONDITIONS
ORDER
DO SET HIGH BANK
HI BANK...............................................SET

ANNOUNCE
HIGH BANK SET ANNOUNCE
CHECK

ORDER, DO
SPEED BUG 160 / 170 KT*
DO, ANNOUNCE
SET * 160 kt for 42, 170 kt for 72

ALL ATR
WHEN CLEARED FOR ORDER
A FLIGHT LEVEL OR SET ALTI STANDARD
PASSING TRANSITION
ALTITUDE DO DO
ALTIMETER...........................STANDARD SET ALTIMETER...........................STANDARD SET

ANNOUNCE ANNOUNCE
STANDARD SET PASSING FL XXX, NOW!

ANNOUNCE
CHECK
OR
PLUS OR MINUS XXX

if deviation > 50 Ft check altimeter setting

if deviation < 50 Ft altimeter setting is correct.

AFTER ALTIMETER REQUEST AND ANSWER

STANDARD SETTING OR AFTER TAKE-OFF C/L
AFTER CLIMB ANNOUNCE AND READ
SEQUENCE IF AFTER TAKE-OFF CHECKLIST
ALTIMETERS REMAIN
ON QNH SETTING Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 44 01
STANDARD OPERATING
PROCEDURES JUN 09

3.13. FL100 during climb

Flight events PNF PF

CROSSING FL 100 DO ORDER

CLIMBING PRESSURIZATION............................. CHECK FL 100
(cabin VS, cabin altitude, P) No Checklist for FL 100
LANDING LIGHTS...................................OFF
PAX SEAT BELTS..................... AS REQUIRED

3.14. Cruise

Flight events PNF PF

1000 FT BEFORE DO ORDER

CRUISE FL SAT................................................. CHECK COMPUTE CRUISE PARAMETERS
DELTA ISA....................................COMPUTE
CRUISE PARAMETERS..............DETERMINED
AND NOTED

ALT STAR ON PF EADI ANNOUNCE ANNOUNCE

CHECK ALT STAR read on FMA

ALL ATR
ALT GREEN ANNOUNCE
ON PF EADI ANNOUNCE ALT GREEN read on FMA
CHECK
ORDER AND SET
SPEED BUGKT
DO
SPEED BUG..........................................SET

DO AND ANNOUNCE
TORQUE BUGS......................................SET
SET

REACHING CRUISE ANNOUNCE

SPEED CRUISE PROCEDURE
DO
POWER MANAGEMENT ........................ CRZ
TORQUES.......... ADJUSTED TO AMBER BUG
CRUISE PARAMETERS....................... CHECK
Note: check actual IAS, TAS versus predetermined values.

ANNOUNCE
42 not PEC CRUISE PROCEDURE COMPLETE

REACHING CRUISE ANNOUNCE

SPEED CRUISE PROCEDURE
DO
POWER MANAGEMENT ........................ CRZ
CRZ TQ............................................ CHECK
CRUISE PARAMETERS....................... CHECK
72 not PEC Note: check actual IAS, TAS versus predetermined values.
42 PEC
ANNOUNCE
72 PEC CRUISE PROCEDURE COMPLETE

DURING CRUISE DO DO (as soon as possible)

FILL THE FLIGHT LOG COMPUTE TOP OF DESCENT (TOD)
COMPUTE ESTIMATED TIME OF ARRIVAL
COMPUTE FUEL REMAINING AND HOLDING
TIME
COMPUTE EXPECTED LANDING WEIGHT

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 45 01
STANDARD OPERATING
PROCEDURES JUN 09

CRUISE PARAMETERS

PNF reads SAT by depressing the SAT PB

and determines the ISA deviation.
Example:
Assuming that the aircraft is cruising at FL200, what is the ISA deviation?
In standard ISA conditions, temperature at sea level is 15C and decreases by 2C each
1000ft.
FL200 standard temperature = 15C 20x2C = 25C
In the case described below, the aircraft is flying in ISA conditions.

Take the FCOM or QRH page in compliance with the cruise weight.
Example:
Assuming that your cruise weight is 20T, what are your cruise parameters in 72-500?
ALL ATR

For NP 82% and 20T

TQ = 69.4%
FF = 336 kg/H/eng
IAS = 204 kt
TAS = 273 kt

FLIGHT FUEL MANAGEMENT

1) Fuel used versus distance (in Kg/Nm) = FF / GS
2) FU to DEST (in Kg) = actual FU + (dist. to go x Fuel used versus distance) = X
3) Remaining Fuel at Destination (in Kg) = FOB* - X = RF
4) Holding quantity (in Kg) = RF - (alternate fuel + final reserve) = HF
5) Estimated maxi-holding time (in min) =
HF / 8 for 42-300 (i.e. 480 kg/h fuel consumption**)
HF / 10 for all other ATR type (i.e. 600kg/h**)

* FOB: Fuel On Board before engine start

** please refer to FCOM for exact value.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 46 01
STANDARD OPERATING
PROCEDURES JUN 09

3.15. Before descent

Flight events PNF PF

LANDING DATA DO
AVAILABLE LANDING AIRPORT DATA...............OBTAINED
(approx. 10 min
before tod)
DO
LANDING DATA CARD........................ FILLED
STBY QNH............................................SET DO
LANDING DATA CARD................ PROCESSED
Refer to 01.03 p. 34, data card proceeding.

DO ORDER AND DO
GA TQ BUGS................................ CHECKED GA TQ BUGS.........................................SET
SPEED BUGS........................................SET SPEED BUGS........................................SET
DA or MDA...........................................SET DA or MDA...........................................SET
NAV AIDS.............................................SET
CCAS............................................ RECALL*
Note: Crew review all aircraft status, due to Emer or
Abnormal situation, in preparation for arrival briefing

BEFORE DESCENT DO
(approx. 5 min ARRIVAL BRIEFING..................PERFORMED
before tod) CCAS...............................................CLEAR
Refer to 01.03 p 38, arrival briefing.

ARRIVAL BRIEFING REQUEST AND ANSWER

COMPLETE ANNOUNCE AND READ DESCENT CHECKLIST
(AFTER TOD) DESCENT CHECKLIST

ALL ATR
Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 47 01
STANDARD OPERATING
PROCEDURES JUN 09

LANDING DATA CARD

Filled by PNF and analyzed by PF.

The landing data card information helps the crew to prepare arrival.

Crew must process information. Please refer to 01.03 p34, data card proceeding.

Example: Landing data card

Vapp computation

RWY HDG is 230

- Wind reported 270 / 18kt

- So head wind component is 12kt

Vapp=VmHB 30 + Wind factor *

* Wind factor is the highest value between:

1/3 of reported Head Wind
or
The Gust in full

Wind factor maxi 15 kt

ALL ATR

Vapp=95+1/3(12)=99

Vga computation

Is the highest value between:

1.1 Vmca
or
Normal conditions
Vapp no wind + 5kt
Icing conditions

Vapp computation

RWY HDG is 090

- Wind reported 090 / 20kt gusting 30kt

- So head wind component is 20 kt gusting 30kt

Vapp=VmHB 30 + Wind factor *

* Wind factor is the highest value between:

1/3 of reported Head Wind -> here 20/3 -> 7kt
or
The Gust in full -> here 30-20 -> 10kt

Wind factor maxi 15 kt

Vapp=95+10=105kts

For speed bugs setting please refer to 01.03 p. 20, Speed bugs.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 48 01
STANDARD OPERATING
PROCEDURES JUN 09

3.16. FL 100 during descent

Flight events PNF PF

crosSING fl 100 ORDER

DESCENDING DO FL 100
PRESSURIZATION............................. CHECK No Checklist for FL 100
LANDING LIGHTS.................................... ON
SEAT BELTS........................................... ON

3.17. Approach

Flight events PNF PF

WHEN CLEARED ORDER AND DO

TO AN ALTITUDE OR SET QNH
PASSING TRANSITION DO AND ANNOUNCE
LEVEL XXXX SET
(Check also the standby altimeter setting) ANNOUNCE
PASSING XXXX FT, NOW!
ANNOUNCE
CHECK
OR
PLUS OR MINUS XXXX

if deviation > 50 Ft check altimeter setting

ALL ATR
if deviation < 50 Ft altimeter setting is correct.

PROCEDURE REQUEST AND ANSWER

COMPLETE APPROACH CHECKLIST
ANNOUNCE & READ
APPROACH CHECKLIST
Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

3.18. Before landing

Stabilization policy
STABILIZED means: Aircraft configurated for Landing
Flight Path and Speed appropriate
Checklist before Landing complete

Flight EVENT Flight EVENT PNF ANNOUNCES PF ACTIONS NOTES

STABILIZED XXXX FT, STABILIZED ORDER: WE CONTINUE

1000 FT AGL IMC
NON STABILIZED XXXX FT, NON STABILIZED ORDER: "GO-AROUND" XXXX FT":
ANNOUNCED ALTITUDE
STABILIZED XXXX FT, STABILIZED ORDER: "WE CONTINUE" WILL BE Zx + 1000 FT
500 FT AGL VMC* OR Zx + 500 FT
NON STABILIZED XXXX FT, NON STABILIZED ORDER: "GO-AROUND" OR Zx + 300 FT
ACCORDING TO WEATHER
300 ft AGL Circle STABILIZED XXXX FT, STABILIZED ORDER: "WE CONTINUE" CONDITIONS
to land and
visual patTern NON STABILIZED XXXX FT, NON STABILIZED ORDER: "GO-AROUND"

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 49 01
STANDARD OPERATING
PROCEDURES JUN 09

3.18.1. ILS precision approach (1/2)

Flight events PNF PF
72 PEC

CLEARED FOR DO
APPROACH APP MODE................................. ENGAGED

ANNOUNCE
APPROACH MODE SET
ANNOUNCE LOC WHITE, GS WHITE
CHECK

VOR ALIVE ANNOUNCE

VOR ALIVE

LOC STAR ANNOUNCE

(RWY AXIS IS ANNOUNCE LOC STAR
CONFIRMED WHEN CHECK
VOR IS CENTERED AND RWY AXIS CONFIRMED ORDER
/ OR RMI NEEDLE ON SET RUNWAY HEADING, DUAL ILS
FINAL CRS) DO AND ANNOUNCE
RUNWAY HEADING SET, DUAL ILS SET

G/S ALIVE ANNOUNCE

GLIDE SLOPE ALIVE

ANNOUNCE ORDER
SPEED CHECK FLAPS 15
DO
FLAPS 15.................................. SELECTED

WHEN FLAPS 15 ON ANNOUNCE

FLAPS INDICATOR FLAPS 15
ORDER AND DO
DO AND ANNOUNCE SPEED BUG WHITE BUG + 10
SET

G/S 1 DOT ANNOUNCE

ONE DOT
ANNOUNCE ORDER
SPEED CHECK
72 not PEC

GEAR DOWN
DO
LANDING GEAR LEVEL...................... DOWN
PWR MGT............................................. T/O
TAXI & T/O LIGHTS................................. ON

WHEN 3 GREEN LIGHTS ANNOUNCE

LDG GEAR DOWN

G/S 1/2 DOT ANNOUNCE

42 not PEC HALF DOT

72 not PEC ORDER

ANNOUNCE FLAPS 30
72 PEC SPEED CHECK

DO
FLAPS 30.................................... SELECTED

WHEN FLAPS 30 ON ANNOUNCE

FLAPS INDICATOR FLAPS 30
42 not PEC

42 not PEC DO AND ANNOUNCE ORDER AND DO

72 not PEC SET SPEED BUG V APPROACH
72 PEC

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 49 02
STANDARD OPERATING
PROCEDURES JUN 09

3.18.1. ILS precision approach (1/2)

Flight events PNF PF

CLEARED FOR DO
APPROACH APP MODE................................. ENGAGED

ANNOUNCE
ANNOUNCE APPROACH MODE SET
CHECK LOC WHITE, GS WHITE

VOR ALIVE ANNOUNCE

VOR ALIVE

LOC STAR ANNOUNCE

(RWY AXIS IS ANNOUNCE LOC STAR
CONFIRMED WHEN CHECK
VOR IS CENTERED AND RWY AXIS CONFIRMED
/ OR RMI NEEDLE ON ORDER
FINAL CRS) DO AND ANNOUNCE SET RUNWAY HEADING, DUAL ILS
RUNWAY HEADING SET, DUAL ILS SET

ANNOUNCE
G/S ALIVE GLIDE SLOPE ALIVE ORDER

42 PEC
FLAPS 15
ANNOUNCE
SPEED CHECK
DO
FLAPS 15.................................. SELECTED

WHEN FLAPS 15 ON ANNOUNCE

FLAPS INDICATOR FLAPS 15
ORDER AND DO
DO AND ANNOUNCE SPEED BUG WHITE BUG + 10
SET

G/S 1 DOT ANNOUNCE

ONE DOT
ORDER
ANNOUNCE GEAR DOWN
SPEED CHECK
DO
LANDING GEAR LEVEL...................... DOWN
PWR MGT............................................. T/O
TAXI & T/O LIGHTS................................. ON

WHEN 3 GREEN LIGHTS ANNOUNCE

LDG GEAR DOWN

ANNOUNCE
SPEED CHECK ORDER
DO FLAPS 25
FLAPS 25.................................. SELECTED

WHEN FLAPS 25 ON ANNOUNCE

FLAPS INDICATOR FLAPS 25

G/S 1/2 DOT ANNOUNCE

HALF DOT
ANNOUNCE ORDER
SPEED CHECK FLAPS 35
DO
FLAPS 35.................................... SELECTED
WHEN FLAPS 35 ON ANNOUNCE
FLAPS INDICATOR FLAPS 35
ORDER AND DO
SPEED BUG V APPROACH

DO AND ANNOUNCE
SET

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 50 01
STANDARD OPERATING
PROCEDURES JUN 09

3.18.1. ILS precision approach (2/2)

Flight events PNF PF

G/S STAR ANNOUNCE AND ORDER

DO AND ANNOUNCE GLIDE STAR,
CHECK
72 PEC ORDER
42 PEC DO AND ANNOUNCE SET GO-AROUND ALTITUDE
ADU.............................. G.A. ALTITUDE SET

XXXX FT SET
ANNOUNCE
CHECK''
ANNOUNCE
''TOP OF DESCENT XX DME, CHECK''

G/S STAR
ANNOUNCE AND ORDER
GLIDE STAR,
42 not PEC DO AND ANNOUNCE
72 not PEC CHECK ANNOUNCE
MAX RPM, SET GO-AROUND ALTITUDE

DO AND ANNOUNCE
CL'S.............................ADVANCED TO MAX
ADU.............................. G.A. ALTITUDE SET

MAX RPM, XXXX FT SET

ANNOUNCE
ANNOUNCE CHECK''
''TOP OF DESCENT XX DME, CHECK''

WHEN AIRCRAFT REQUEST AND ANSWER

STABILIZED ANNOUNCE AND READ BEFORE LANDING CHECKLIST
ALL ATR

BEFORE LANDING CHECKLIST

Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

WHEN C/L COMPLETE ANNOUNCE

CENTER HEADING BUG
DO AND ANNOUNCE Apply drift to maintain final track.
HEADING BUG CENTERED

1000 FT AGL IMC ANNOUNCE

"XXXX FT, STABILIZED" ORDER
"WE CONTINUE"
1000 FT AGL IMC ANNOUNCE
"XXXX FT, NON STABILIZED" ORDER
"GO-AROUND"

REACHING ANNOUNCE
DA + 500 FT FIVE HUNDRED ABOVE

REACHING ANNOUNCE
DA + 100 FT ONE HUNDRED ABOVE

REACHING DA ANNOUNCE
MINIMUM ANNOUNCE
LAND OR GO-AROUND

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 51 01
STANDARD OPERATING
PROCEDURES JUN 09

Deviations and limits

Height

General 100 Ft

Beginning of go-around + 50 Ft

At decision height 0 Ft

Tracking

On radial 5

Precision approach half deviation of LOC and GS, according to altitude

Speed

Both engines + 5 Kt / 0 Kt

One engine + 10 Kt / 0 Kt

Aircraft handling when performing a precision approach manually

ALL ATR
LOCALIZER Corrections must be done inside the heading bug.

GLIDE SLOPE Pitch variations should not exceed 2.

Note: PNF calls for any deviation:

SPEED if +10/-0 Kt deviation exceeded.

GLIDE SLOPE if dot deviation exceeded.

LOCALIZER if dot deviation exceeded.

PF answer is:

CORRECTION (and performs correction)

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 52 01
STANDARD OPERATING
PROCEDURES JUN 09

3.18.2. Non precision approach (1/2)

Flight events PNF PF

CLEARED FOR ORDER AND DO

APPROACH
DO AND ANNOUNCE SPEED BUG 160 KT
SET

4 NM BEFORE ORDER
DESCENT POINT OR ANNOUNCE FLAPS 15
2 MINUTES FROM SPEED CHECK
DESCENT POINT (IF NO DO
DME AVAILABLE) FLAPS 15.................................. SELECTED

WHEN FLAPS 15 ON
FLAPS INDICATOR
ANNOUNCE
FLAPS 15 ORDER AND DO
DO AND ANNOUNCE SPEED BUG WHITE BUG + 10
SET
ORDER
GEAR DOWN
ANNOUNCE
SPEED CHECK
DO
LANDING GEAR LEVEL...................... DOWN
PWR MGT............................................. T/O
TAXI & T/O LIGHTS................................. ON

WHEN 3 GREEN LIGHTS

ON AT LEAST ONE LDG ANNOUNCE
LDG GEAR DOWN ORDER
GEAR INDICATOR
FLAPS 30

ANNOUNCE
SPEED CHECK
DO
FLAPS 30.................................. SELECTED

WHEN FLAPS 30 ON
FLAPS INDICATOR
ANNOUNCE
FLAPS 30
ORDER AND DO
72 not PEC

SPEED BUG V APPROACH

DO AND ANNOUNCE
SET
ORDER
DOAND ANNOUNCE MAX RPM, SET GO-AROUND ALTITUDE
MAX RPM,GO-AROUND ALTITUDE SET
* Go-around altitude setting:
Set only if present altitude below GA altitude.
If not set present altitude + 300 ft to avoid ALT*
Set GA altitude when passing GA alt -300 ft
DO AND ANNOUNCE
ANNOUNCE VS 0 FT/MIN SET
CHECK
REQUEST
ANNOUNCE AND READ BEFORE LANDING CHECKLIST
BEFORE LANDING CHECKLIST

Refer to QRH 6.01

42 not PEC

ANNOUNCE
CHECKLIST COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 52 02
STANDARD OPERATING
PROCEDURES JUN 09

3.18.2. Non precision approach (1/2)

Flight events PNF PF

CLEARED FOR DO AND ANNOUNCE ORDER AND DO

APPROACH SPEED BUG 160 KT
SET

ANNOUNCE ORDER
4 NM BEFORE SPEED CHECK FLAPS 15
DESCENT POINT OR DO
2 MINUTES FROM FLAPS 15.................................. SELECTED
DESCENT POINT (IF NO
DME AVAILABLE)

WHEN FLAPS 15 ON ANNOUNCE

FLAPS INDICATOR ORDER AND DO
FLAPS 15
SPEED BUG WHITE BUG + 10

DO AND ANNOUNCE
SET ORDER
GEAR DOWN

42 PEC
ANNOUNCE
SPEED CHECK
DO
LANDING GEAR LEVEL...................... DOWN
PWR MGT............................................. T/O
TAXI & T/O LIGHTS................................. ON

WHEN 3 GREEN ANNOUNCE

LIGHTS ON AT LEAST LDG GEAR DOWN
ONE LDG GEAR ORDER
INDICATOR ANNOUNCE FLAPS 25
SPEED CHECK
DO
FLAPS 25.................................. SELECTED

WHEN FLAPS 25 ON ANNOUNCE

FLAPS INDICATOR ORDER
FLAPS 25
FLAPS 35

ANNOUNCE
SPEED CHECK
DO
FLAPS 35.................................. SELECTED

WHEN FLAPS 35 ON ANNOUNCE

FLAPS INDICATOR FLAPS 35 ORDER AND DO
SPEED BUG V APPROACH
DO AND ANNOUNCE
SET
ORDER
DO AND ANNOUNCE SET GO-AROUND ALTITUDE
GO-AROUND ALTITUDE SET
* Go-around altitude setting:
Set only if present altitude below GA altitude.
If not set present altitude + 300 ft to avoid ALT*
Set GA altitude when passing GA alt -300 ft ORDER
DO AND ANNOUNCE VS 0 FT/MIN SET
CHECK
REQUEST
ANNOUNCE AND READ BEFORE LANDING CHECKLIST
BEFORE LANDING CHECKLIST
Refer to QRH 6.01
ANNOUNCE
CHECKLIST COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 52 03
STANDARD OPERATING
PROCEDURES JUN 09

3.18.2. Non precision approach (1/2)

Flight events PNF PF

72 PEC

CLEARED FOR ORDER AND DO

APPROACH
DO AND ANNOUNCE SPEED BUG 160 KT
SET

4 NM BEFORE
DESCENT POINT OR ANNOUNCE
2 MINUTES FROM SPEED CHECK
DESCENT POINT (IF NO DO ORDER
DME AVAILABLE) FLAPS 15.................................. SELECTED
FLAPS 15
WHEN FLAPS 15 ON
ANNOUNCE
FLAPS INDICATOR
FLAPS 15 ORDER AND DO
DO AND ANNOUNCE SPEED BUG WHITE BUG + 10
SET

ORDER
GEAR DOWN
ANNOUNCE
SPEED CHECK
DO
LANDING GEAR LEVEL...................... DOWN
PWR MGT............................................. T/O
TAXI & T/O LIGHTS................................. ON

WHEN 3 GREEN LIGHTS

ON AT LEAST ONE ANNOUNCE
LDG GEAR DOWN ORDER
LDG GEAR INDICATOR FLAPS 30
AND TLU GREEN LT
ILLUMINATED ANNOUNCE
SPEED CHECK
DO
FLAPS 30.................................. SELECTED

WHEN FLAPS 30 ON ANNOUNCE ORDER AND DO

FLAPS INDICATOR FLAPS 30 SPEED BUG V APPROACH

DO AND ANNOUNCE
SET
ORDER
SET GO-AROUND ALTITUDE
DO AND ANNOUNCE
ADU.............................. G.A. ALTITUDE SET
GO-AROUND ALTITUDE SET
* Go-around altitude setting:
Set only if present altitude below GA altitude.
If not set present altitude + 300 ft to avoid ALT*
Set GA altitude when passing GA alt 300 ft ORDER
VS 0 FT/MIN SET
DO AND ANNOUNCE
CHECK REQUEST
BEFORE LANDING CHECKLIST
ANNOUNCE AND READ
BEFORE LANDING CHECKLIST

Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 53 01
STANDARD OPERATING
PROCEDURES JUN 09

3.18.2. Non precision approach (2/2)

Flight events PNF PF

0.3 NM before the

DESCENT POINT
ORDER
DO AND ANNOUNCE SET VS - XXX FT/MIN
VS - XXX FT/MIN SET

ANNOUNCE
CHECK

STARTING DESCENT
(REFER TO NOTE 1) DO DO
TIMING............................................. START TIMING............................................ START
FLIGHT PATH............................ MONITORED TQ................................... REDUCE TO 25%
FLIGHT PATH........................... MONITORED

WHEN ON FINAL
ANNOUNCE
CENTER HEADING BUG
DO AND ANNOUNCE Apply drift to maintain final track.
HEADING BUG CENTERED

1000 FT AGL IMC ANNOUNCE

"XXXX FT, STABILIZED" ORDER
"WE CONTINUE"

1000 FT AGL IMC ANNOUNCE

"XXXX FT, NON STABILIZED" ORDER
"GO-AROUND"
REACHING ANNOUNCE

ALL ATR
MDA + 500 FT FIVE HUNDRED ABOVE

REACHING ANNOUNCE
MDA + 100 FT ONE HUNDRED ABOVE

MDA ANNOUNCE
MINIMUM ANNOUNCE
LAND
OR
GO-AROUND

Note 1: PNF announces altitude versus distance, and altitude deviation above or below the desired
one.

PF corrects by adjusting VS.

Note 2: When runway in sight, PF announces LAND. No more minima announcement done by
PNF.

Note 3: Go-around may be initiated before MAPT, according to company policy.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 54 01
STANDARD OPERATING
PROCEDURES JUN 09

3.19. Circle to land

For circle to land based on a precision approach, please refer to 02.03 p. 49, ILS precision
approach, for initial configuration.

For circle to land based on a non-precision approach, please refer to 02.03 p. 52, Non precision
approach, for initial configuration.

Then, the following amendments must be taken into account:

Flaps remain at 15, until final descent initiated.

Speed will be White Bug +10 minimum, during all approach, until Flaps 30/35 extended.

Before landing C/L has to be performed during descent, before reaching MDA of the
circle to land procedure.

Reaching MDA, PF orders /or executes:

set ALT, adjust PLs around 40%

set HDG MODE HI, select heading bug 45, start timing.

Established on final, when PF orders FLAPS 30/35, PNF executes and announces

FLAPS 30, MAX RPM, BEFORE LANDING C/L COMPLETE. (42 not PEC / 72 not PEC)
ALL ATR

FLAPS 30/35, BEFORE LANDING C/L COMPLETE. (72 PEC / 42 PEC)

For landing phase, please refer to 02.03 p. 58, Landing.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 55 01
STANDARD OPERATING
PROCEDURES JUN 09

3.19. Circle to land (Contd)

Flight events PNF PF

REACHING MDA
DO
ALT MODE..................................SELECTED

ANNOUNCE
ALT SET, ALT GREEN
ANNOUNCE
CHECK

AT LEVEL OFF DO
PLs........................................ around 40%
HEADING MODE.........................SELECTED
DO HEADING BUG 45..................SELECTED
TIMING............................................. START TIMING............................................ START

ANNOUNCE
HDG MODE SET, HEADING XXX SET,
ANNOUNCE START TIMING
CHECK

30 SEC OUTBOUND DO AND ANNOUNCE

ANNOUNCE HEADING BUG................... ON DOWNWIND
CHECK HDG BUG XXX SET

DOWN WIND - ABEAM DO

THRESHOLD TIMING............................................. START DO
TIMING............................................ START
ANNOUNCE
START TIMING

DO
REACHING HEADING BUG...................... ON BASE LEG
OUTBOUND TIME
ANNOUNCE
HDG BUG XXX SET
ANNOUNCE
CHECK

72 not PEC
END OF BASE LEG DO
HEADING BUG.............................ON FINAL

ANNOUNCE
HDG BUG XXX SET
ANNOUNCE
CHECK
ON FINAL ORDER
FLAPS 30, MAX RPM
ANNOUNCE
SPEED CHECK

DO
FLAPS 30...................................SELECTED
CLs............................................ MAX RPM

ANNOUNCE
FLAPS 30, MAX RPM,
BEFORE LANDING C/L COMPLETE
42 not PEC

300 FT AGL
ANNOUNCE ORDER
"XXXX FT, STABILIZED"
"WE CONTINUE"

300 FT AGL
ANNOUNCE ORDER
"XXXX FT, NON STABILIZED"
"GO-AROUND"

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 55 02
STANDARD OPERATING
PROCEDURES JUN 09

3.19. Circle to land (Contd)

Flight events PNF PF

REACHING MDA DO
ALT MODE..................................SELECTED

ANNOUNCE
ALT SET, ALT GREEN
ANNOUNCE
CHECK

AT LEVEL OFF DO
PLs........................................ around 40%
HEADING MODE.........................SELECTED
DO HEADING BUG 45..................SELECTED
TIMING............................................. START TIMING............................................ START

ANNOUNCE
HDG MODE SET, HEADING XXX SET,
ANNOUNCE START TIMING
CHECK

30 SEC OUTBOUND DO AND ANNOUNCE

42 PEC

ANNOUNCE HEADING BUG................... ON DOWNWIND

CHECK HDG BUG XXX SET

DOWN WIND - ABEAM ANNOUNCE

THRESHOLD FLAPS 25, START TIMING

DO
DO TIMING............................................ START
TIMING............................................. START
FLAPS 25...................................SELECTED

DO AND ANNOUNCE
FLAPS 25

REACHING DO
OUTBOUND TIME HEADING BUG...................... ON BASE LEG

ANNOUNCE
HDG BUG XXX SET
ANNOUNCE
CHECK

END OF BASE LEG DO

HEADING BUG.............................ON FINAL

ANNOUNCE
HDG BUG XXX SET
ANNOUNCE
CHECK

ON FINAL ORDER
FLAPS 35
ANNOUNCE
SPEED CHECK
DO
FLAPS 35...................................SELECTED

ANNOUNCE
FLAPS 35,
BEFORE LANDING C/L COMPLETE

300 FT AGL ANNOUNCE

"XXXX FT, STABILIZED" ORDER
"WE CONTINUE"

300 FT AGL ANNOUNCE

"XXXX FT, NON STABILIZED" ORDER
"GO-AROUND"

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 55 03
STANDARD OPERATING
PROCEDURES JUN 09

3.19. Circle to land (Contd)

72 PEC
Flight events PNF PF

REACHING MDA DO
ALT MODE..................................SELECTED

ANNOUNCE ANNOUNCE
CHECK ALT SET, ALT GREEN

AT LEVEL OFF
DO DO
TIMING............................................. START PLs........................................ around 40%
HEADING MODE.........................SELECTED
HEADING BUG 45..................SELECTED

ANNOUNCE
HDG MODE SET, HEADING XXX SET,
START TIMING
ANNOUNCE
CHECK

30 SEC OUTBOUND DO AND ANNOUNCE

HEADING BUG................... ON DOWNWIND
ANNOUNCE HDG BUG XXX SET
CHECK
DOWN WIND - ABEAM
DO DO
THRESHOLD
TIMING............................................. START
TIMING............................................ START

ANNOUNCE
START TIMING
REACHING
OUTBOUND TIME DO
HEADING BUG...................... ON BASE LEG

ANNOUNCE
HDG BUG XXX SET
ANNOUNCE
CHECK

END OF BASE LEG DO

HEADING BUG.............................ON FINAL

ANNOUNCE
ANNOUNCE HDG BUG XXX SET
CHECK

ON FINAL ORDER
FLAPS 30
ANNOUNCE
SPEED CHECK
DO
FLAPS 30...................................SELECTED

ANNOUNCE
FLAPS 30,
BEFORE LANDING C/L COMPLETE

300 FT AGL ANNOUNCE

"XXXX FT, STABILIZED" ORDER
"WE CONTINUE"

300 FT AGL ANNOUNCE

"XXXX FT, NON STABILIZED" ORDER
"GO-AROUND"

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 56 01
STANDARD OPERATING
PROCEDURES JUN 09

3.20. Visual flight patterns (1/2)

From take-off to 1500 ft AAL, please refer to 02.03 p. 39, Take-off and further.

In this example, the PF flies manually by following FD bars (autopilot OFF).

Flight events PNF PF

REACHING 1500 FT ANNOUNCE

AAL ANNOUNCE ALT STAR
CHECK
ANNOUNCE
ALT GREEN
ANNOUNCE DO
CHECK TQs................................................... 40%

WHEN READY TO TURN ORDER

SET DOWNWIND HEADING
DO AND ANNOUNCE PF has to take into account the crosswind
DOWNWIND HEADING SET component to apply a correct drift.

ANNOUNCE
CHECK

DOWNWIND ORDER
ANNOUNCE FLAPS 15
SPEED CHECK
DO
FLAPS 15...................................SELECTED

ANNOUNCE
FLAPS 15
ORDER
DO AND ANNOUNCE SPEED BUG WHITE BUG +10
SET

WHEN FLAPS SET ORDER

TO 15 GEAR DOWN
ANNOUNCE
72 not PEC

SPEED CHECK
DO
LANDING GEAR LEVER...................... DOWN

ANNOUNCE
GEAR DOWN

ABEAM THRESHOLD DO
DO TIMING............................................ START
TIMING............................................. START
Outbound time = (H / 20) 1 / 1 kt of head/tailwind.
REACHING OUTBOUND
ORDER
TIME
SET RUNWAY HEADING, VS - 700
DO, ANNOUNCE
RUNWAY HEADING SET, VS - 700 SET
ANNOUNCE
CHECK
RUNWAY IN SIGHT
ORDER
FLIGHT DIRECTOR STANDBY
42 not PEC

ON FINAL
ORDER
FLAPS 30, MAX RPM
ANNOUNCE
SPEED CHECK
DO
FLAPS 30...................................SELECTED
CLs............................................ MAX RPM

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 56 02
STANDARD OPERATING
PROCEDURES JUN 09

3.20. Visual flight patterns (1/2)

From take-off to 1500 ft AAL, please refer to 02.03 p. 39, Take-off and further.
In this example, the PF flies manually by following FD bars (autopilot OFF).

Flight events PNF PF

REACHING 1500 FT ANNOUNCE ANNOUNCE

AAL CHECK ALT STAR

ANNOUNCE ANNOUNCE
CHECK ALT GREEN
DO
TQs................................................... 40%

WHEN READY TO TURN ORDER

SET DOWNWIND HEADING
DO AND ANNOUNCE PF has to take into account the crosswind
DOWNWIND HEADING SET component to apply a correct drift.

ANNOUNCE
CHECK

42 PEC
DOWNWIND ORDER
FLAPS 15
ANNOUNCE
SPEED CHECK
DO
FLAPS 15...................................SELECTED

ANNOUNCE
FLAPS 15 ORDER
SPEED BUG WHITE BUG +10
DO AND ANNOUNCE
SET

ABEAM TOWER ORDER

ANNOUNCE GEAR DOWN
SPEED CHECK
DO
LANDING GEAR LEVER...................... DOWN

ANNOUNCE
GEAR DOWN
ANNOUNCE ORDER
SPEED CHECK FLAPS 25
DO
FLAPS 25...................................SELECTED
ANNOUNCE
FLAPS 25

ABEAM THRESHOLD
DO
DO TIMING............................................ START
TIMING............................................. START
Outbound time = (H / 20) 1 / 1 kt of head/tailwind.

REACHING OUTBOUND ORDER

TIME SET RUNWAY HEADING, VS - 700
DO, ANNOUNCE
RUNWAY HEADING SET, VS - 700 SET
ANNOUNCE
CHECK

RUNWAY IN SIGHT ORDER

FLIGHT DIRECTOR STANDBY

ON FINAL ORDER
ANNOUNCE FLAPS 35
SPEED CHECK
DO
FLAPS 35...................................SELECTED

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 56 03
STANDARD OPERATING
PROCEDURES JUN 09

3.20. Visual flight patterns (1/2)

From take-off to 1500 ft AAL, please refer to 02.03 p. 39, Take-off and further.
72 PEC

In this example, the PF flies manually by following FD bars (autopilot OFF).

Flight events PNF PF

REACHING 1500 FT ANNOUNCE

AAL ANNOUNCE ALT STAR
CHECK
ANNOUNCE
ANNOUNCE ALT GREEN
CHECK DO
TQs................................................... 40%

WHEN READY TO TURN ORDER

DO AND ANNOUNCE SET DOWNWIND HEADING
DOWNWIND HEADING SET PF has to take into account the crosswind
component to apply a correct drift.

ANNOUNCE
CHECK

DOWNWIND ANNOUNCE ORDER

SPEED CHECK
DO FLAPS 15
FLAPS 15...................................SELECTED

ANNOUNCE
FLAPS 15

DO AND ANNOUNCE ORDER

SET SPEED BUG WHITE BUG +10

ABEAM TOWER ANNOUNCE ORDER

SPEED CHECK GEAR DOWN
DO
LANDING GEAR LEVER...................... DOWN

ANNOUNCE
GEAR DOWN

ABEAM THRESHOLD DO
DO TIMING............................................ START
TIMING............................................. START Outbound time=(H / 20) 1 / 1 kt of head/tailwind.

REACHING OUTBOUND ORDER

TIME DO, ANNOUNCE SET RUNWAY HEADING, VS - 700
RUNWAY HEADING SET, VS - 700 SET
ANNOUNCE
CHECK

RUNWAY IN SIGHT ORDER

FLIGHT DIRECTOR STANDBY

ON FINAL ANNOUNCE ORDER

SPEED CHECK FLAPS 30
DO
FLAPS 30...................................SELECTED

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 57 01
STANDARD OPERATING
PROCEDURES JUN 09

3.20. Visual flight patterns (2/2)

Flight events PNF PF
WHEN FLAPS AT 30 ANNOUNCE
ON FLAPS INDICATOR FLAPS 30, MAX RPM
ORDER
42 not PEC SPEED BUG VAPP
72 not PEC DO AND ANNOUNCE
SET
REQUEST AND ANSWER
BEFORE LANDING CHECKLIST
ANNOUNCE AND READ
BEFORE LANDING CHECKLIST

Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE''

Flight events PNF PF

WHEN FLAPS AT 35 ANNOUNCE
ON FLAPS INDICATOR FLAPS 35
ORDER
42 PEC DO AND ANNOUNCE SPEED BUG VAPP
SET

REQUEST AND ANSWER

ANNOUNCE AND READ BEFORE LANDING CHECKLIST
BEFORE LANDING CHECKLIST

ALL ATR
Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE''

Flight events PNF PF

WHEN FLAPS AT 30 ANNOUNCE
ON FLAPS INDICATOR FLAPS 30
ORDER
72 PEC DO AND ANNOUNCE SPEED BUG VAPP
SET
REQUEST AND ANSWER
BEFORE LANDING CHECKLIST
ANNOUNCE AND READ
BEFORE LANDING CHECKLIST

Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE''

Flight events PNF PF

300 FT AGL ANNOUNCE
"XXXX FT, STABILIZED" ORDER
"WE CONTINUE"

300 FT AGL ANNOUNCE

"XXXX FT, NON STABILIZED" ORDER
"GO-AROUND"

Note: Flaps 15 have to be kept after T/O when performing a visual pattern below 1500
feet AAL.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 58 01
STANDARD OPERATING
PROCEDURES JUN 09

3.21. Landing
Flight events PNF PF

WHEN PF ANNOUNCE
DISCONNECTS ap AUTOPILOT OFF
(PRESS TWICE TO CANCEL
CAVALRY CHARGE)
Up to 160 ft (CAT I) and 80ft
(CAT II)

RA INFORMATION ANNOUNCE
80
50
20 DO
PL......................................................... FI
DO
FLARE................................PITCH MONITOR

ON RUNWAY DO
(BOTH LOW PITCH PL......................................................... GI
LIGHTS ILLUMINATED) CHECK AND ANNOUNCE DO
2 LOW PITCH PL................................. REVERSE AS RQD

REACHING 70 kt
ANNOUNCE
70 Kt

Note: Use reverse to full stop only if necessary, according to the local noise abatement regulation
(please refer to 04.02 p. 1, Noise abatement procedures.). It is recommended toreturn to GI
position at 40 kt to avoid flight control shaking.
ALL ATR

Reverse policy
ENGINES LO PITCH LIGHTS PNF ANNOUNCES PF ACTION ON REVERSE

TWO ILLUMINATED TWO LOW PITCH NORMAL USE

2 ENGINES
ONLY ONE ILLUMINATED "NO REVERSE" NO USE, MAXI YAW EFFECT

1 ENGINE
ONE ILLUMINATED "ONE LOW PITCH" USE WITH CARE, YAW EFFECT

Flight events CM1 CM2

WHEN PNF CALLS ANNOUNCE
70 kt I HAVE CONTROL

FLIGHT CONTROL DO DO
TRANSFER STEERING CONTROL.......................... HOLD CONTROL WHEEL.....HOLD INTO THE WIND
NORMAL BRAKES......................... APPLIED

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 59 01
STANDARD OPERATING
PROCEDURES JUN 09

3.22. Go-around
Flight events PNF PF

72 PEC
MINIMUM ANNOUNCE
MINIMUM

DA OR MDA ANNOUNCE
(RUNWAY OR RAMP GO-AROUND, SET POWER, FLAPS ONE NOTCH
NOT IN SIGHT)
OR OTHER EVENTS DO DO
UNEXPECTED TQs............................CHECK / ADJUST GA GA PB ON PL......................... DEPRESSED
ROTATE................ GA PITCH (+8 NOSE UP)
42 not PEC FLAPS 15.................................. SELECTED
PLs................ ADVANCED TO WHITE MARK
WHEN FLAPS AT 15 ON CAVALRY CHARGE.........................CANCEL
THE FLAPS INDICATOR ANNOUNCE
FLAPS 15, POWER SET

DA OR MDA ANNOUNCE
(RUNWAY OR RAMP GO-AROUND, SET POWER, FLAPS ONE NOTCH
NOT IN SIGHT)
OR OTHER EVENTS DO DO
UNEXPECTED TQs............................CHECK / ADJUST GA GA PB ON PL......................... DEPRESSED
FLAPS 15.................................. SELECTED ROTATE................ GA PITCH (+8 NOSE UP)
72 not PEC PLs...........................ADVANCED TO RAMP
72 PEC CAVALRY CHARGE.........................CANCEL
ANNOUNCE
WHEN FLAPS AT 15 ON FLAPS 15, POWER SET
THE FLAPS INDICATOR

POSITIVE RATE ANNOUNCE

POSITIVE RATE ORDER
GEAR UP, HEADING, LOW BANK, IAS VGA
DO
GEAR LEVEL......................................... UP
HDG MODE................................ SELECTED
LO BANK................................... SELECTED
IAS..................................... VGA SELECTED
TAXI & T/O LIGHT.................................. OFF

ANNOUNCE

72 not PEC
IAS XXX SET ANNOUNCE
CHECK
ORDER AND DO
DO AND ANNOUNCE SET SPEED BUG VGA
SET

WHEN ALL LIGHTS ANNOUNCE

EXTINGUISHED ON THE GEAR UP
LDG GEAR PANEL

REACHING ANNOUNCE
ACCELERATION ACCELERATION ALTITUDE DO
ALTITUDE PL....................... RETARD TO WHITE MARK
42 not PEC
ORDER
Note: Mini 1000ft CLIMB SEQUENCE
AGL or higher if
requested

REACHING
42 not PEC

ANNOUNCE
ACCELERATION ACCELERATION ALTITUDE
ALTITUDE DO
72 not PEC PL......................... RETARD TO THE NOTCH

72 PEC ORDER
Note: Mini 1000ft CLIMB SEQUENCE
AGL or higher if
requested

CONTINUE THE AFTER TAKE-OFF PROCEDURE - Refer to 02.03 p. 43, After take-off.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 59 02
STANDARD OPERATING
PROCEDURES JUN 09

3.22. Go-around
Flight events PNF PF

MINIMUM ANNOUNCE
MINIMUM

DA OR MDA ANNOUNCE
(RUNWAY OR RAMP GO-AROUND, SET POWER, FLAPS ONE NOTCH
NOT IN SIGHT)
OR OTHER EVENTS DO DO
UNEXPECTED TQs............................CHECK / ADJUST GA GA PB ON PL......................... DEPRESSED
FLAPS 25.................................. SELECTED ROTATE................ GA PITCH (+8 NOSE UP)
PLs...........................ADVANCED TO RAMP
WHEN FLAPS AT 25 ON CAVALRY CHARGE.........................CANCEL
THE FLAPS INDICATOR ANNOUNCE
FLAPS 25, POWER SET

POSITIVE RATE ANNOUNCE

POSITIVE RATE ORDER
GEAR UP, HEADING, LOW BANK, IAS VGA
DO
GEAR LEVEL......................................... UP
42 PEC

HDG MODE................................ SELECTED

LO BANK................................... SELECTED
IAS..................................... VGA SELECTED
TAXI & T/O LIGHT.................................. OFF

ANNOUNCE
IAS XXX SET ANNOUNCE
CHECK
ORDER AND DO
DO AND ANNOUNCE SET SPEED BUG VGA
SET

WHEN ALL LIGHTS ANNOUNCE

EXTINGUISHED ON THE GEAR UP
LDG GEAR PANEL

REACHING ANNOUNCE
ACCELERATION ACCELERATION ALTITUDE DO
ALTITUDE PL......................... RETARD TO THE NOTCH

ORDER
Note: Mini 1000ft CLIMB SEQUENCE
AGL or higher if DO
requested IAS...........INCREASED (ABOVE WHITE BUG)
PWR................................................ CLIMB
BLEEDS............................... SET ON IF NOT
IAS...........................................160 KT SET

REACHING WHITE BUG ANNOUNCE

OR VGA + 15 CLIMB SEQUENCE COMPLETE

ANNOUNCE
WHITE BUG / VGA + 15
Note: PF will order flaps retraction to 15 when speed
reaches VGA + 15kt or white bug, whichever is lower
DO
FLAPS LEVER............................ SET TO 15

WHEN FLAPS AT 15 ON ANNOUNCE

THE FLAPS INDICATOR FLAPS 15

REACHING WHITE OR ANNOUNCE ORDER

RED BUG WHITE BUG NORMAL CONDITIONS FLAPS 0
(ACCORDING TO EXTERNAL RED BUG ICING CONDITIONS
CONDITIONS) DO
FLAPS LEVER............................... SET TO 0
CONTINUE THE AFTER TAKE-OFF PROCEDURE
WHEN FLAPS AT 0 ON ANNOUNCE Refer to 02.03 p. 43, After take-off.
THE FLAPS INDICATOR FLAPS 0

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 60 01
STANDARD OPERATING
PROCEDURES JUN 09

GO-AROUND FLOW

PNF PF
A FLAPS A GO-AROUND PB: DEPRESSED

Select flaps one notch less than actual. GA and HDG HOLD appears on FMA.

A FLAPS: 25 B POWER LEVERS: WHITE MARK/RAMP

When PF orders FLAPS 25, select flaps 25. At the same moment announce:
GO-AROUND, FLAPS ONE NOTCH, SET POWER.
B TORQUE: ADJUSTED/CHECK
Adjust/check torque to GA torque. C PITCH: 8
Follow FD BARS, and cancel AP Cavalry charge.
C LANDING GEAR LEVER: UP
E
Announce POSITIVE RATE. When PF orders
GEAR UP, select landing gear lever up.

D AFCS: SET
Select HDG, LO BANK, IAS VGA.

E TAXI & T/O LIGHTS: OFF

G
C

ALL ATR
A
B B
A 42 PEC

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 61 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.23. After landing

Flight events CM1 CM2

RUNWAY VACATED ORDER

AFTER LANDING PROCEDURE
DO
TRIMS.............................................. RESET
XPDR.................................................. STBY
TCAS.................................................. STBY
FLAPS.....................................................0
GUST LOCK.................................. ENGAGED
RADAR............................................... STBY
ADU......................................... STBY/RESET
LANDING LIGHT..................................... OFF
STROBE LIGHT...................................... OFF
CONT LIGHT.......................................... OFF
ANTI-ICING............................................ OFF
DE-ICING.............................................. OFF

ANNOUNCE
AFTER LANDING PROCEDURE COMPLETE

IF LAST FLIGHT ORDER

OF THE DAY ATPCS TEST
DO
ATPCS TEST.............................PERFORMED

ANNOUNCE
ATPCS TEST PERFORMED

AFTER 1 MINUTE, ORDER

ALL ATR
PL IN GI POSITION CL1 FEATHER, THEN SHUT-OFF
Wait 20 seconds before shut-off DO
for last flight of the day CL1.............................FEATHER, SHUT-OFF
(for oil maintenance check). ACW BTC............................ CHECK CLOSED

WHEN ENG 1 IS REQUEST

STOPPED AFTER LANDING CHECKLIST

READ FOR HIMSELF

AFTER LANDING CHECKLIST

Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 62 01
STANDARD OPERATING
PROCEDURES JUN 09

AFTER LANDING FLOW

CM2
1 TCAS: STBY

2 XPDR: STBY
13
3 FLAPS: 0
9 10
4 GUST LOCK: ENGAGED
8
Pull control column backwards to lock ailerons and elevator.

5 RADAR: STBY

6 TRIMS: RESET

7 ADU: STBY & RESET

7 8 LIGHTS: OFF
Switch off Landing and Strobe lights.

9 CONT RELIGHT: OFF

ALL ATR
10 ANTI-ICING / DE-ICING: OFF
6
11 ATPCS TEST (DYNAMIC): PERFORMED (WHEN NECESSARY)

ARM position: ARM light illuminates green

5 TQ indication increases
NP and NH increase slightly
ENG position: Selected engine TQ decreases below 21%
Opposite engine: TQ does not change, UPTRIM light illuminates,
NP and NH increase slightly.
2.15 seconds later: concerned propeller is automatically feathered,
4 3 ARM green light extinguishes.
Caution: During ATPCS dynamic test, ACW is temporarily lost and
consequently both main hyd pumps are temporarily lost as well.
Do not perform ATPCS test while taxiing if DC HYD PUMP is not
12 operating.
2 If braking is required during test, it will be performed using EMER
brake handle as required.
Wait for 10 minutes if another ATPCS test has to be performed.

12 CONDITION LEVER: FEATHER THEN SHUT-OFF

1 11 Wait for 1 minute in GI position to select CL1 to feather then shut-off (Last flight of the
day, wait for 20 seconds before CL1 shut-off. It enables ground staff to check OIL level).

13ACW BTC: CHECK

CM2 checks ACW BTC is illuminated and ACW BUS 1 fault light is extinguished.

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 63 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.24. Parking

Flight events CM1 CM2

mARSHALLER IN SIGHT DO
TAXI & T/O LIGHT....................................OFF CHECK AND ANNOUNCE
HYDRAULIC PRESS................... 3X3000 PSI
HYDRAULIC CHECK

AT THE GATE DO
DO
PARKING CL2 BRK................................... ON TIMING..............................................START
CL 2.......................................... FEATHERED
READY LT...................................... CHECKED
PROP BRK.............................................. ON PROP 2...............................CHECKED STOP
NP BELLOW 20 %...................... ON/LOCKED
BEACON................................................OFF
SEAT BELT..............................................OFF

WHEN GPU DO
AVAILABLE DC EXT PWR PB........................ DEPRESSED
CL2..................................... FUEL SHUT OFF

PARKING PROCEDURE REQUEST READ FOR HIMSELF

COMPLETE PARKING CHECKLIST PARKING CHECKLIST

Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

ALL ATR

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 64 01
STANDARD OPERATING
PROCEDURES JUN 09

PARKING FLOW
CM1 CM2
1 TAXI AND T.O LIGHT: OFF 1 TIMING: START
Only for last flight of the day, wait 20 seconds before
2 PARKING BRAKE: ON engine 2 shut off (will enable later OIL LEVEL checks).

3 ENG 2: FEATHERED
7
4 PROP BRAKE: ON / LOCKED
Check READY green light illuminated and NP <20%
4 Then switch Prop Brake ON.
1 5
6 5 BEACON LIGHT: OFF

6 SEAT BELTS: OFF

7 DC EXTERNAL PWR: ON
Check voltage first on the lateral panel.

8 CONDITION LEVER 2: SHUT-OFF

Only for last flight of the day, wait 20 seconds before
engine 2 shut off (will enable later OIL LEVEL checks).

ALL ATR
2

3
8

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 65 01
STANDARD OPERATING
PROCEDURES JUN 09

PERSONAL NOTES
3.25. Leaving the aircraft

Flight events CM1 CM2

ALL DOCUMENTATION ORDER

FILLED LEAVING THE AIRCRAFT PROCEDURE
DO
ICE AND RAIN PROTECTION.................. OFF
EXT LTs............................................... OFF
EFIS................................................... OFF
RADAR............................................... OFF
COMs................................................. OFF
FUEL PUMPS...................................... OFF
EMER EXIT LT................................ DISARM
CDLS (if installed)................................ OFF
CDLS CTL Panel FAULT LIGHT............CHECK
EXT POWER........................................ OFF
BAT.................................................... OFF

ANNOUNCE
LEAVING THE AIRCRAFT
PROCEDURE COMPLETE

PROCEDURE READ FOR HIMSELF

COMPLETE LEAVING THE AIRCRAFT CHECKLIST

Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

ALL ATR

FOR TRAINING ONLY

 NORMAL PROCEDURES 02.03
Page 66 01
STANDARD OPERATING
PROCEDURES JUN 09

LEAVING THE AIRCRAFT FLOW

CM2
1 OXYGEN MAIN SUPPLY: OFF
11 2 ICE AND RAIN PROTECTION: OFF
1
3 EXTERNAL LIGHTS OFF
10 2
8 4 CM1 EFIS: OFF

5 CM2 EFIS: OFF

3 9
6 RADAR: OFF

7 COMs / NAVs / XPDR: OFF

8 BOTH FUEL PUMPS: OFF

9 EMER EXIT LIGHT: DISARM

10 EXT PWR: OFF

11 BATTERY: OFF

ALL ATR
4 6 5

FOR TRAINING ONLY

PERSONAL NOTES PERSONAL NOTES

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 1 01
NORMAL SYSTEM USE JUN 09

1. Global Navigation Satellite System (GNSS)

On ATR aircraft, the GNSS on board is the Honeywell HT1000.

1.1. Policy

1.1.1. On the ground:

IDENT page must be displayed. If not, press DATA, then IDENT.

GNSS is filled in by PF, according to known (runway in use, cruise flight level, SID,...) or expected
data.

PNF must crosscheck the LEGS and PERF INIT pages during the PF departure briefing.

Conventional radio navigation means must be set for stand-by use, to assure a safe flight path in
case of GNSS failure.

1.1.2 In flight:
PF manages GNSS with PNF crosscheck when autopilot is engaged.

Below FL100, GNSS is managed by PNF on PF orders.

ALL ATR
Any flight path modification (horizontal or vertical) must be clearly announced and checked by
both crew members.

In case of flight track change due to ATC, the procedures and phraseology hereafter shall be
used:
IF AUTOPILOT ENGAGED:

Flight events PNF PF

NEW WAYPOINT ANNOUNCE
ACKNOWLEDGED DIRECT TO XXXXX, CONFIRM?
ANNOUNCE
CONFIRM DO
EXEC KEY.............................. DEPRESSED
NEW FLIGHT PATH.................. MONITORED

IF AUTOPILOT DISCONNECTED:

Flight events PNF PF

NEW WAYPOINT ORDER
ACKNOWLEDGED SET DIRECT TO XXXXX
DO AND ANNOUNCE
DIRECT TO XXXXX, SET

DO
EXEC KEY............................... DEPRESSED DO
NEW FLIGHT PATH.................. MONITORED

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 2 01
NORMAL SYSTEM USE JUN 09

1.2. Pre-flight

PREFLIGHT PREFLIGHT

LSK 1L LSK 1R

LSK 2L LSK 2R

LSK 3L LSK 3R SV DATA >

LSK 4L < HDG/TAS OVERRIDE

LSK 4R
LSK 5L DEST RAIM >
LSK 5R
LSK 6L POS REF > ROUTE >
LSK 6R

Check aircraft model, engines model and Check present position, time.
navigational database. Depress LSK 6R
Depress LSK 6R (Line Select Key).

PREFLIGHT PREFLIGHT
ALL ATR

USER RTES > USER RTES >

< RTE 2 < RTE 2

Route 1 page on which you insert Enter departure airport ICAO code in
your flight plan. the scratchpad (e.g. LFBO)
Depress LSK 1L to replace the origin
box prompts by LFBO.

PREFLIGHT PREFLIGHT

USER RTES > USER RTES >

< RTE 2 < RTE 2

Check LFBO written under ORIGIN. Enter destination airport ICAO code in the
scratchpad (e.g. LFBD)
Depress LSK 1R

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 3 01
NORMAL SYSTEM USE JUN 09

PREFLIGHT PREFLIGHT

USER USER
RTES > RTES >
< RTE 2 < RTE 2

Check LFBD written under DEST. Enter flight number in the scratchpad
(e.g. ATR 01).
Depress LSK 2R.

PREFLIGHT PREFLIGHT

USER USER
RTES > RTES >
< RTE 2 < RTE 2

ALL ATR
Check ART 01 written under FLT Enter departure runway in the scratch-
NO. pad (e.g. RWY 32R).
Depress LSK 2L.

PREFLIGHT PREFLIGHT

USER USER
RTES > RTES >
< RTE 2 ACTIVATE > < ERASE PERF INIT >

Check RW32R 01 written under RUNWAY. Depress EXEC KEY to execute the
Depress LSK 6R to activate route 1. activation.

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 4 01
NORMAL SYSTEM USE JUN 09

PREFLIGHT PREFLIGHT

USER
< RTE COPY RTES >
< RTE 2 PERF INIT >

Depress LSK 6R to get the PERF INIT

page.

PREFLIGHT PREFLIGHT
ALL ATR

Enter gross weight, in tons, in the Check 16.20 written under GR WT.
scratchpad (e.g. 16.2).
Depress LSK 1L.

PREFLIGHT PREFLIGHT

Enter block fuel, in tons, in the scratch- Check 2.40 CALC written under FUEL.
pad (e.g. 2.4). Check correct zero fuel weight indica-
Depress LSK 2L. tion under ZFW.

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 5 01
NORMAL SYSTEM USE JUN 09

PREFLIGHT PREFLIGHT

Enter fuel reserves, in tons, in the scratch- Check 0.65 written under RESERVES.
pad (e.g. 0.65).
Depress LSK 4L.

PREFLIGHT PREFLIGHT

ALL ATR
< ERASE

Enter cruise FL in the scratchpad (e.g. Check FL160 written under CRZ ALT.
160). Depress EXEC KEY to activate modifications.
Depress LSK 1R.

PREFLIGHT PREFLIGHT

USER RTES >

< RTE COPY

< RTE 2

Check speeds for climb, cruise and des- Depress LSK 5L to copy the route 1 as route 2 to
cent phase. have a second route in case of in flight replanification.
Check speed transition and transition
altitude.
Depress RTE KEY.

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 6 01
NORMAL SYSTEM USE JUN 09

PREFLIGHT PREFLIGHT

USER RTES > USER RTES >

< RTE 2 < RTE 1 ACTIVATE >

Check RTE COPY COMPLETE in LSK 5L. Check route 2 data.

Depress LSK 6L. Depress DEP ARR KEY.

PREFLIGHT PREFLIGHT

< DEP ARR >

ARR >

< DEP ARR >

ARR >

DEP ARR
ALL ATR

< ---- ---- > < INDEX ROUTE >

Depress LSK 1L. Runway 32R is used for departure.

Depress LSK 4R.

PREFLIGHT PREFLIGHT

< ERASE ROUTE > < INDEX ROUTE >

Check <SEL> 32R under RUNWAYS. Check <ACT> 32R under RUNWAYS.
Depress EXEC KEY to activate modifications. AFRIC 5B SID is usual routing.
Depress LSK 1L.

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 7 01
NORMAL SYSTEM USE JUN 09

PREFLIGHT PREFLIGHT

< ERASE ROUTE >

< INDEX ROUTE >

Check AFRIC 5B <SEL> under SIDS. Check AFRIC 5B <ACT> under

Depress EXEC KEY to activate SIDS.
modifications. Depress DEP ARR KEY.

PREFLIGHT PREFLIGHT

< DEP ARR >

ARR >

< DEP ARR >

ARR >

ALL ATR
DEP ARR
< ---- ---- > < INDEX ROUTE >

Depress LSK 2R. ILS 23 is expected on arrival.

Depress LSK 1R.

PREFLIGHT PREFLIGHT

< ERASE ROUTE > < ERASE ROUTE >

Check <SEL> ILS 23 under APPROACHES. Check BGC 4 <SEL> under STARS.
BGC4 STAR is expected. Transition will be done through LIBRU.
Depress LSK 1L. Depress LSK 4R.

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 8 01
NORMAL SYSTEM USE JUN 09

PREFLIGHT PREFLIGHT

< ERASE ROUTE > < INDEX ROUTE >

Check <SEL> LIBRU under TRANS. Check all <SEL> replaced by <ACT>.
Depress EXEC KEY to activate Depress RTE KEY.
modifications.

PREFLIGHT PREFLIGHT
ALL ATR

< RTE 2 < RTE 2

After AFRIC, no waypoint (route discontinuity), Insert MEN VOR/DME between AFRIC and
then BGC. BGC.
Enter MEN in the scratchpad.
Depress LSK 2R.

PREFLIGHT PREFLIGHT

< ERASE

Select MEN VOR/DME located in Check DIRECT MEN in line 2.

France. Depress EXEC KEY to activate modifica-
Depress LSK 1L. tions.

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 9 01
NORMAL SYSTEM USE JUN 09

PREFLIGHT PREFLIGHT

< RTE 2 < RTE 2

Check MOD RTE 1 replaced by ACT RTE 1. Check BGC in the scratchpad.
Route discontinuity has to be cleared. Depress LSK 3R
Depress LSK 4R.

PREFLIGHT PREFLIGHT

ALL ATR
< ERASE < RTE 2

Check discontinuity cleared. Check MOD RTE 1 replaced by ACT RTE

Depress EXEC KEY to activate 1.
modifications. Depress NEXT KEY.

PREFLIGHT PREFLIGHT

< EXECUTE MISSED APPROACH

< RTE 2 < RTE 2 LEGS RTE DATA >

Check ACT RTE 1 page 3/3. Check ACT RTE 1 LEGS page 1/5
Depress LEGS KEY. (track, distance, altitude constraint)
Depress NEXT KEY.

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 10 01
NORMAL SYSTEM USE JUN 09

PREFLIGHT PREFLIGHT

< EXECUTE MISSED APPROACH

< RTE 2 LEGS RTE DATA > < RTE 2 LEGS RTE DATA >

Check ACT RTE 1 LEGS page 2/5 Check ACT RTE 1 LEGS page 3/5
(track, distance, altitude constraint) (track, distance, altitude constraint)
Depress NEXT KEY. Depress NEXT KEY.

PREFLIGHT PREFLIGHT
ALL ATR

< RTE 2 LEGS RTE DATA > < RTE 2 LEGS RTE DATA >

Check ACT RTE 1 LEGS page 4/5 Check ACT RTE 1 LEGS page 5/5
(track, distance, altitude constraint) (holding point).
Depress NEXT KEY.

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 11 01
NORMAL SYSTEM USE JUN 09

1.3. User waypoints

USER WAYPOINTS USER WAYPOINTS

< POS REF NAV DATA >

NEAREST >

FIX >

< USER WPTS

< IDENT MAINTENANCE > < NEW WPT

DATA INDEX page obtained by User waypoints list is empty.

depressing the DATA KEY. Depress LSK 6L.
Depress LSK 5L.

USER WAYPOINTS USER WAYPOINTS

ALL ATR
SAVE USER WPT >

< LIST < LIST

User waypoints can be defined by Enter the waypoint name (e.g. point) in
geographic coordinates or point - the scratchpad.
bearing - distance or Depress LSK 2L.
point - bearing / point - bearing.

USER WAYPOINTS USER WAYPOINTS

SAVE USER WPT > SAVE USER WPT >

< LIST < LIST

Check POINT under IDENT. Enter TOU230/27 in the scratchpad

(point : TOU - bearing : 230 -
distance : 27 Nm).
Depress LSK 4L.

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 12 01
NORMAL SYSTEM USE JUN 09

USER WAYPOINTS USER WAYPOINTS

SAVE USER WPT > SAVE USER WPT >

< LIST < LIST

Check TOU230.0/027.0 under Enter N4323.76E00052.27 in the scrat-

PB/D OR PB/PB. chpad (geographic coordinates).
Check geographic coordinates Depress LSK 3L.
automatically computed.

USER WAYPOINTS USER WAYPOINTS

ALL ATR

SAVE USER WPT >

< LIST < LIST

Check N4323.76 E00052.27 Check USER WPT SAVE

under LAT/LONG. COMPLETE displayed for a couple
Depress LSK 5R. of seconds.
Depress LSK 6L.
USER WAYPOINTS

< NEW DELETE ALL >

WPT

Check POINT inserted in the

user waypoints list..

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 13 01
NORMAL SYSTEM USE JUN 09

1.4. Flight in progress

FLIGHT IN PROGRESS

< POS REPORT POS REF >

ATR01 PROGRESS page obtained by

pressing PROG KEY.
Depress LEGS KEY.

FLIGHT IN PROGRESS FLIGHT IN PROGRESS

ALL ATR
< RTE 2 LEGS RTE DATA > < RTE 2 LEGS RTE DATA >

Inbound FINOT (23.7 Nm to go), you Depress LSK 1L to go direct to MEN.

are cleared direct MEN.
Depress LSK 3L to get MEN in the
scratchpad.

FLIGHT IN PROGRESS FLIGHT IN PROGRESS

ABEAM PTS >

RTE COPY >

< RTE 2 LEGS < RTE 2 LEGS RTE DATA >

Check MEN replaced FINOT. Check MOD RTE 1 LEGS repla-

Depress EXEC KEY to activate modifications. ced by ACT RTE 1 LEGS.

FOR TRAINING ONLY

 03.01
NORMAL PROCEDURES Page 14 01
NORMAL SYSTEM USE JUN 09

FLIGHT IN PROGRESS FLIGHT IN PROGRESS

< RTE 2 LEGS RTE DATA > < RTE 2 LEGS RTE DATA >

Inbound TOU (1.8 Nm to go), you want to remove Depress LSK 3L.
LACOU from your FPL.
Depress CLR KEY to get DELETE in the scratch-
pad.

FLIGHT IN PROGRESS FLIGHT IN PROGRESS

ALL ATR

< ERASE RTE DATA > < ERASE RTE DATA >

Check LACOU removed and Depress LSK 3L to clear the disconti-

route discontinuity displayed. nuity.
Depress LSK 4L.

FLIGHT IN PROGRESS FLIGHT IN PROGRESS

< ERASE RTE DATA > < RTE 2 LEGS RTE DATA >

Check route discontinuity cleared. Check MOD RTE 1 LEGS replaced

Depress EXEC KEY to activate modifica- by ACT RTE 1 LEGS.
tions.

FOR TRAINING ONLY

 03.02
NORMAL PROCEDURES Page 1 01
NORMAL SYSTEM USE JUN 09

2. Aircraft Performance Monitoring (APM)

The APM is an onboard system for detecting ice effects on aircraft, developed to enhance the aircraft
safety and protection. It acquires the aircraft performance parameters in real time and compares
them to the expected values. The monitored performance parameters are the IAS and the drag. Any
abnormal increase on one of those parameters leads to an alarm to alert the flight crew. There are
three different levels of alarms, depending on the severity of the discrepancy found.

2.1. APM cockpit interface

The interface is composed of :
a twelve position rotactor selector
3 indicators placed in front of the captain and co-pilot to display the performance degradation
information
a FAULT/OFF light button to inform the crew of a problem with APM or to select the APM OFF
a Push To Test button to test the APM indicators

ALL ATR

FOR TRAINING ONLY

 03.02
NORMAL PROCEDURES Page 2 01
NORMAL SYSTEM USE JUN 09

2.2. Normal procedures

2.2.1. Take-Off weight Selection

To determine the aircraft theoretical and in flight performance, the aircraft weight must be
known.

As the weight measure is not available, the crew must enter the take-off weight value in the system
with a twelve-position rotary selector.

To take into account the new take-off weight value:

the rotactor must be moved (even if actual weight is the same as the previous flight) to the
minimum TO weight and then back to the nearest TO weight
the selection must be done before the IAS reaches 30 kt
the selection must be done with both engines running. Indeed, some micro cuts can occur on
the DC EMER BUS during the start phase.

If the selected weight is below the real one, the performance of the aircraft will be degraded
compared to the computed one, and spurious alerts may be triggered. Inversely, if a higher
weight is selected, alerts may be hidden, and more specifically, cases of severe icing may be not
detected.
ALL ATR

Note: Any change of the rotary selector in flight will have no effect

If the crew does not select the take-off weight before take-off with the rotactor, the APM will
perform its own take-off weight computation. Computation is performed during the first minutes of
the flight and before the APM begins the drag analysis.

APM calculation is less accurate than the flight crew manual selection: analyses of several hundreds
of revenue flight have shown that the APM maximum deviation is around 1500kg for take-off
weight computation.

2.2.2. APM Testing

APM testing is activated by the crew daily, to check all APM components work properly.

FOR TRAINING ONLY

 04.01
NORMAL PROCEDURES Page 1 01
ADDITIONAL STANDARD JUN 09
OPERATING PROCEDURES

1. Hotel mode use

1.1. Start up without GPU during long transit (1/4)
CM2 alone may start eng 2 if necessary.

Refuel must be complete

CM1 CM2

DO
EMERGENCY EQUIPMENT ...............CHECK
GEARS PINS.............................ON BOARD
FUEL X-FEED TEST:
DOCUMENTATION......................ON BOARD
C/B.................................................CHECK
ENG 1 PUMP ON: FEED LO PR 1 STBY HORIZON
Extinguished ; FEED LO PR 2 Illuminated ERECTION KNOB....PULL AND MAINTAINED
BATTERY.............................................. ON
FUEL X-FEED in line: FEED LO PR 1 and 2 STBY HORIZON
Extinguished ERECTION KNOB...................... RELEASED
VHF 1.................................................. ON
ATPCS...............................................TEST
FUEL X-FEED closed: FEED LO PR 1 COCKPIT COM HATCH........................OPEN
Extinguished ; FEED LO PR 2 Illuminated PARKING BRAKE................................... ON
PL 1 AND 2........................................... GI
ENG 2 PUMP ON: FEED LO PR 1 and 2 GUST LOCK.......................................... ON
Extinguished CL 1 AND 2................................ FUEL S/O
FLAPS LEVER..................................CHECK
LANDING GEAR LEVER..................... DOWN
ECU 1 AND 2 PBs....... CHECK DEPRESSED
WIPERS.............................................. OFF
PROP BRK........................................... ON
FUEL PUMP 2...................................... ON
ENG 2 FIRE TEST.................... PERFORMED
DO
EXTERNAL INSPECTION
READ AND CHECK
Refer to QRH 3.01
(DOWN TO ENG 2 START IN HOTEL MODE)

42 not PEC

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.01
Page 2 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

1.1. Start up without GPU during long transit (2/4)

Flight events CM1 CM2

READY TO START ANNOUNCE

ENGINE 2 IN HOTEL GROUND FROM COCKPIT
MODE READY TO START ENG 2 IN HOTEL MODE, DO
CONFIRM SERVICE DOOR CLOSED SERVICE DOOR............................ CLOSED
AND AREA CLEAR WING LIGHTS...................................... ON
PROP BRAKE......... ON/PROP BRK blue light
ENGINE START SELECT.... A+B (or A or B)*
*A+B for the first start of the day, then for the
next start, A for odd days and B for even
days, to detect ignition system hidden failure
ANNOUNCE
RIGHT SIDE CLEAR,
READY TO START ENG 2?
ANNOUNCE
I AM READY

After OUTSIDE DO
VISUAL CHECK START 2 PB........................... DEPRESSED

DO ANNOUNCE
TIMING*............................................START STARTER ON
START 2..................................... CHECK ON
* For starter limitation time,
30 s maxi when starter off (45%NH)
NH=10% DO AND ANNOUNCE
(UNTIL NH=19% if CL 2.......................................... FEATHER
ITT>200C) TIMING*..........................................START
FUEL OPEN
*For ignition time, it should rise within 10 seconds
DO
ENGINE PARAMETERS.....................CHECK

ITT increasING DO ANNOUNCE

ENGINE PARAMETERS.......................CHECK IGNITION
TIMING............................................. STOP

NH=25% DO ANNOUNCE
ENGINE PARAMETERS.......................CHECK When FAULT amber light extinguished
ECU

NH=45% ANNOUNCE
ANNOUNCE 45%
STARTER OFF
*If not, select rotary selector OFF/START ABORT DO
DO ITT MAX..........................................CHECK
TIMING............................................... STOP
ANNOUNCE
ITT XXX C

NH = 61.5% ANNOUNCE
PARAMETERS STABILIZED

CM1 orders GPU disconnection to ground staff

42 not PEC

PARAMETERS DO
STABILIZED ENGINE START.........................OFF & START
ABORT
DC GEN 2 FAULT...................EXTINGUISHED
DC BTC.............................. CHECK CLOSED
BLEED / PACKS / X VALVE................... OPEN

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.01
Page 3 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

1.1. Start up without GPU (3/4)

Flight events CM1 CM2

AFTER ENG 2
STARTED IN HOTEL DO
MODE SCAN ON OVERHEAD PANEL
ANNUNCIATOR LIGHT......................... TEST
DOME LIGHT.........................AS REQUIRED
STANDBY COMPASS............................OFF
STORM LIGHT......................................OFF
FUEL X-FEED.................................. CHECK
ENG 1 PUMP........................................ON
DOORS.............................................. TEST
SPOILER LIGHTS..................................OFF
LDG GEAR INDICATOR..................... CHECK
ENG 1 FIRE...................................3 TESTS
EXTERNAL LIGHTS...............AS REQUIRED
DC/AC PANEL................................. CHECK
CVR................................................... TEST
SIGN PANEL................................... CHECK
DE-ICING/ANTI-ICING................LIGHTS OFF
PROBES HEATING.................................ON
WINDSHIELD HEATING..........................ON
ACW PANEL................................... CHECK
HYD PANEL.................................... CHECK
EMER LOC XTMR.............................. AUTO
AIR COND PANEL............................ CHECK
AVIONICS VENT................................. AUTO
OXYGEN......................................... CHECK
COMPT SMK...................................... TEST
EXHAUST MODE..............................RESET

SCAN ON PEDESTRAL
LIGHTS.................................AS REQUIRED
ATC recommendation: FDEP (If installed)...FLIGHT NUMBER+DATE
TRIMS....................TEST AND SET NEUTRAL
In case of dual installation check TCAS........................................ TEST/STBY
both system using: VHF............................................. ON/ TEST
System 1 / A for odd days. ADF............................................. ON/ TEST
System 2 / B for even days. TRANSPONDER........................ STBY/ TEST
Example: Transponder, Ignition, IDLE GATE.................................... PULLED
EMER AUDIO CANCEL................ GUARDED
ADC switch (if installed). RADAR............................................. STBY
ECP............................................ TEST/SET
GPS.....................................................ON
MCDU (If installed with the MPC)..........SET
CDLS....................................... Daily check
42 not PEC

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.01
Page 4 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

1.1. Start up without GPU during long transit (4/4)

Flight events CM1 CM2

AFTER CENTRAL
PANEL SCAN DO
SCAN ON CENTRAL PANEL
FUEL QTY............................. TEST / CHECK
TAT/SAT.......................................... CHECK
CAP................................................... CLR
STBY INSTRUMENTS...................... .CHECK
PWR MGT............................................T/O
SYNCHROPHASER................................ON
FUEL USED.....................................RESET
ENGINE INDICATORS............. TEST / CHECK
ENG PANEL.................................... CHECK
CAB PRESS PANEL......................... CHECK
AUTO PRESS..................... TEST / LANDING
ELEVATION
TRIM INDICATOR............................. CHECK
FLAPS INDICATOR........................... CHECK
STICK PUSHER....................... DEPRESSED
HYDRAULIC.................................... CHECK

SCAN ON GLARE SHIELD

fD BARS.............................................ON
NAV 1 AND 2............................. ON / TEST
ADU...................................................BRT

SCAN ON LEFT LATERAL PANEL

nW STEERING...................... ON/GUARDED
OXYGEN MASK.................................. TEST
MARKERS.................................. TEST / LO
AHRS............................................ CHECK
AUDIO1 SEL................................... Check
CAPT SWITCHING PANEL................. CHECK
(E)GPWS....................................GUARDED

SCAN ON LEFT INSTRUMENT PANEL

CLOCK................................................SET
AIR SPEED INDICATOR.................... CHECK
RMI/EHSI....................................... CHECK
EADI.............................................. CHECK
(E)GPWS........................................... TEST
ALTIMETER..........................................SET
VERTICAL AIR SPEED...................... CHECK

SCAN ON RIGHT LATERAL PANEL

EXTRACT AIR FLOW.......................... OPEN
OXYGEN MASK.................................. TEST
AHRS............................................ CHECK
F/O SWITCHING PANEL.................... CHECK
AUDIO 2 SEL.................................. CHECK

SCAN ON RIGHT INSTRUMENT PANEL

(E)GPWS........................................... TEST
VERTICAL AIR SPEED...................... CHECK
ALTIMETER..........................................SET
EADI.............................................. CHECK
RMI/EHSI....................................... CHECK
42 not PEC

AIR SPEED INDICATOR.................... CHECK

CLOCK................................................SET

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.01
Page 1 02
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

1. Hotel mode use

1.1. Start up without GPU during long transit (1/4)

72 PEC
CM2 alone may start eng 2 if necessary.

Refuel must be complete

CM1 CM2

DO
CARGO DOOR CONTROL
PANEL COVER.............................. CLOSED
FUEL X-FEED TEST:
EMERGENCY EQUIPMENT ...............CHECK
GEARS PINS.............................ON BOARD
ENG 1 PUMP ON: FEED LO PR 1 DOCUMENTATION..................... ON BOARD
Extinguished ; FEED LO PR 2 Illuminated C/B................................................ CHECK

42 PEC
STBY HORIZON ERECTION
FUEL X-FEED in line: FEED LO PR 1 and 2 KNOB.................... PULL AND MAINTAINED
Extinguished BATTERY.............................................. ON
STBY HORIZON ERECTION
KNOB.......................................RELEASED
FUEL X-FEED closed: FEED LO PR 1 MFC...............................................CHECK
Extinguished ; FEED LO PR 2 Illuminated VHF 1.................................................. ON
ATPCS...............................................TEST
ENG 2 PUMP ON: FEED LO PR 1 and 2 COCKPIT COM HATCH........................OPEN
Extinguished BRAKE HANDLE........................... PARKING
PL 1 AND 2........................................... GI
GUST LOCK.......................................... ON
CL 1 AND 2................................ FUEL S/O
DO FLAPS LEVER..................................CHECK
EXTERNAL INSPECTION EEC 1 AND 2..................................CHECK
LANDING GEAR LEVER..................... DOWN
WIPERS.............................................. OFF
PROP BRK........................................... ON

72 not PEC
FUEL PUMP 2...................................... ON
ENG 2 FIRE TEST.................... PERFORMED

READ AND CHECK

Refer TO QRH 3.01
(DOWN TO ENG 2 START IN HOTEL MODE)

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.01
Page 2 02
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

1.1. Start up without GPU during long transit (2/4)

72 PEC

Flight events CM1 CM2

READY TO START ANNOUNCE

ENGINE 2 IN HOTEL GROUND FROM COCKPIT
MODE READY TO START ENG 2 IN HOTEL MODE, DO
CONFIRM SERVICE DOOR CLOSED SERVICE DOOR............................ CLOSED
AND AREA CLEAR WING LIGHTS...................................... ON
PROP BRAKE......... ON/PROP BRK blue light
ENGINE START SELECT.... A+B (or A or B)*
*A+B for the first start of the day, then for the
next start, A for odd days and B for even
days, to detect ignition system hidden failure
ANNOUNCE
RIGHT SIDE CLEAR,
READY TO START ENG 2?
ANNOUNCE
I AM READY

After OUTSIDE
42 PEC

VISUAL CHECK DO
START 2 PB........................... DEPRESSED
DO ANNOUNCE
TIMING*............................................START STARTER ON
START 2..................................... CHECK ON
* For starter limitation time,
30 s maxi when starter off (45%NH)
NH=10% DO AND ANNOUNCE
(UNTIL NH=19% if CL 2.......................................... FEATHER
ITT>200C) TIMING*..........................................START
FUEL OPEN
*For ignition time, it should rise within 10 seconds
DO
ENGINE PARAMETERS.....................CHECK

ITT increasING DO ANNOUNCE

72 not PEC

ENGINE PARAMETERS.......................CHECK IGNITION

TIMING............................................. STOP

NH=45% ANNOUNCE
ANNOUNCE 45%
STARTER OFF
*If not, select rotary selector OFF/START ABORT DO
DO ITT MAX..........................................CHECK
TIMING............................................... STOP
ANNOUNCE
ITT XXX C

NH=61.5% ANNOUNCE
PARAMETERS STABILIZED

CM1 orders GPU disconnection to ground staff

PARAMETERS
STABILIZED
DO
ENGINE START........ OFF & START ABORT
DC GEN 2 FAULT.............EXTINGUISHED
DC BTC......................... CHECK CLOSED
BLEED / PACKS / X VALVE..............OPEN

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.01
Page 3 02
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

1.1. Start up without GPU during long transit (3/4)

72 PEC
Flight events CM1 CM2
AFTER ENG 2 DO
STARTED IN HOTEL EXTERNAL INSPECTION DO
MODE SCAN ON OVERHEAD PANEL
ANNUNCIATOR LIGHT......................... TEST
DOME LIGHT.........................AS REQUIRED
STANDBY COMPASS............................OFF
STORM LIGHT......................................OFF
FUEL X-FEED.................................. CHECK
ENG 1 PUMP........................................ON
DOORS.............................................. TEST
SPOILER LIGHTS..................................OFF
LDG GEAR INDICATOR..................... CHECK
TLU.................................................. AUTO
ENG 1 FIRE...................................3 TESTS
EXTERNAL LIGHTS...............AS REQUIRED
DC/AC PANEL................................. CHECK
CVR................................................... TEST
SIGN PANEL................................... CHECK

42 PEC
DE-ICING/ANTI-ICING................LIGHTS OFF
PROBES HEATING.................................ON
WINDSHIELD HEATING..........................ON
ACW PANEL................................... CHECK
HYD PANEL.................................... CHECK
EMER LOC XTMR.............................. AUTO
AIR COND PANEL............................ CHECK
AVIONICS VENT................................. AUTO
OXYGEN......................................... CHECK
COMPT SMK...................................... TEST
EXHAUST MODE..............................RESET

SCAN ON PEDESTRAL
LIGHTS.................................AS REQUIRED
FDEP (If installed)...FLIGHT NUMBER+DATE
ATC recommendation: TRIMS....................TEST AND SET NEUTRAL
In case of dual installation check TCAS........................................ TEST/STBY
both system using: VHF............................................. ON/ TEST
System 1 / A for odd days. ADF............................................. ON/ TEST

72 not PEC
System 2 / B for even days. TRANSPONDER........................ STBY/ TEST
IDLE GATE.................................... PULLED
Example: Transponder, Ignition, EMER AUDIO CANCEL................ GUARDED
ADC switch (if installed). RADAR............................................. STBY
ECP............................................ TEST/SET
GPS.....................................................ON
MCDU (If installed with the MPC)..........SET
CDLS....................................... Daily check

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.01
Page 4 02
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

1.1. Start up without GPU during long transit (4/4)

72 PEC

Flight events CM1 CM2

AFTER CENTRAL
PANEL SCAN DO
SCAN ON CENTRAL PANEL
FUEL QTY............................. TEST / CHECK
TAT/SAT.......................................... CHECK
CAP................................................... CLR
STBY INSTRUMENTS...................... .CHECK
PWR MGT............................................T/O
42 PEC PEC 1 & 2............................................ON
72 PEC FUEL USED.....................................RESET
ENGINE INDICATORS............. TEST / CHECK
ENG PANEL.................................... CHECK
CAB PRESS PANEL......................... CHECK
AUTO PRESS..................... TEST / LANDING
ELEVATION
TRIM INDICATOR............................. CHECK
FLAPS INDICATOR........................... CHECK
42 PEC

STICK PUSHER....................... DEPRESSED

HYDRAULIC.................................... CHECK

SCAN ON GLARE SHIELD

fD BARS.............................................ON
NAV 1 AND 2............................. ON / TEST
ADU...................................................BRT

SCAN ON LEFT LATERAL PANEL

nW STEERING...................... ON/GUARDED
OXYGEN MASK.................................. TEST
MARKERS.................................. TEST / LO
AHRS............................................ CHECK
AUDIO1 SEL................................... Check
CAPT SWITCHING PANEL................. CHECK
(E)GPWS....................................GUARDED

SCAN ON LEFT INSTRUMENT PANEL

72 not PEC

CLOCK................................................SET
AIR SPEED INDICATOR.................... CHECK
RMI/EHSI....................................... CHECK
EADI.............................................. CHECK
(E)GPWS........................................... TEST
ALTIMETER..........................................SET
VERTICAL AIR SPEED...................... CHECK
ADC SWITCH.................................1 OR 2

SCAN ON RIGHT LATERAL PANEL

EXTRACT AIR FLOW.......................... OPEN
OXYGEN MASK.................................. TEST
AHRS............................................ CHECK
F/O SWITCHING PANEL.................... CHECK
AUDIO 2 SEL.................................. CHECK

SCAN ON RIGHT INSTRUMENT PANEL

APM (IF INSTALLED)................. DAILY TEST
(E)GPWS........................................... TEST
VERTICAL AIR SPEED...................... CHECK
ALTIMETER..........................................SET
EADI.............................................. CHECK
RMI/EHSI....................................... CHECK
AIR SPEED INDICATOR.................... CHECK
CLOCK................................................SET

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.01
Page 5 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

ENGINE START WITHOUT GPU FLOW

CM1 CM2
1 MECHANICAL CALL: PERFORMED 1 U CHECK: PERFORMED
Start timing when CM2 announces Starter ON. DOORS : CLOSED
Check the UNLK amber light is extinguished.
2 TIMING: START WING LIGHTS : ON, to visually inform that start is in Hotel
1 Start timing when CM2 announces Starter ON. Mode.
1 3 Fuel Pump N2: RUN
2
5 8 3 STARTER 2: CHECK ON PROPELLER BRAKE : ON
9 If no AC GPU, press HYD AUX PUMP, in order to get the
4 ENGINE PARAMETERS: MONITOR READY green light, then propeller brake switch to ON.
According to the CM2 callouts. ENGINE START ROTARY SELECTOR (or A or B)

5 START OFF: CHECK 2 START PB: DEPRESSED

At 45% NH, check Start ON light is extinguished and START 2 PB : ON
announce STARTER OFF and stop timing. Depress START 2 PB after a visual check on right side.
Announce: STARTER ON.

3 CL2: FEATHER
Advance CL 2 to feather when NH reaches 10% and
announce: FUEL OPEN.
6
4 TIMING: START

4 5 ENGINE PARAMETERS: MONITOR

2 When the ITT needle increases, announce: IGNITION.
ITT must increase within 10 sec on CM2 Timing.

ALL ATR
Otherwise CL2 shut off.
5
7 6 ECU FAULT LIGHT: EXTINGUISH
4 At 25% NH, check ECU fault light exinguishes, announce
ECU ON.

7 ENGINE PARAMETERS: MONITOR

At 45% NH, announce 45%.

8 ENGINE START ROTARY SELECTOR: OFF

When engine parameters are stabilised, announce
PARAMETERS STABLISED, then turn the rotary
selector to OFF/START ABORT.

9 BLEED 2 / PACKS 1+2 / X VALVE: OPEN

When only one BLEED is OPEN on ground, the X VALVE
is opened to supply both packs.

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.01
Page 6 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

PERSONAL NOTES
1.2. Start up without GPU during short transit
ENG 2 FIRE tests are performed before starting engine 2 in Hotel mode.

Flight events CM1 CM2

DO DO

EXTERNAL INSPECTION ENG 1 FIRE.................................... 3 TESTS

FDEP (If installed)..... FLIGHT NUMBER+DATE
MCDU (If installed).................................SET
FUEL QTY................................. TEST/CHECK
FUEL USED....................................... RESET
AUTOPRESS......... TEST/LANDING ELEVATION
COCKPIT COM HATCH......................... OPEN

1.3. Ramp arrival without GPU

ENG 2 runs until Leaving the Aircraft Procedure.

Flight events CM1 CM2

ALL DOCUMENTATION ORDER

FILLED LEAVING THE AIRCRAFT PROCEDURE
DO
OXYGEN MAIN SUPPLY........................... OFF
ICE AND RAIN PROTECTION OFF

ALL ATR
EXT LTs................................................. OFF
EFIS..................................................... OFF
RADAR................................................. OFF
COMs................................................... OFF
CL2............................................. SHUT-OFF
FUEL PUMPS........................................ OFF
EMER EXIT LT..................................DISARM
CDLS (if installed).................................. OFF
CDLS CTL Panel FAULT LIGHT............. CHECK
BAT...................................................... OFF

ANNOUNCE
LEAVING THE AIRCRAFT
PROCEDURE COMPLETE

PROCEDURE READ FOR HIMSELF

COMPLETE LEAVING THE AIRCRAFT CHECKLIST

Refer to QRH 6.01

ANNOUNCE
CHECKLIST COMPLETE

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.01
Page 7 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

ARRIVAL WITHOUT GPU FLOW

CM2
1 OXYGEN MAIN SUPPLY: OFF

11 2 ICE AND RAIN PROTECTION: OFF

1
3 EXTERNAL LIGHTS OFF
2
9 4 CM1 EFIS: OFF

5 CM2 EFIS: OFF

3
10 6 RADAR: OFF

7 COMs: OFF

8 CL 2: FUEL S/O

9 BOTH FUEL PUMPS: OFF

10 EMER EXIT LIGHT: DISARM

11 BATTERY: OFF

ALL ATR
4 6 5

8
7

FOR TRAINING ONLY

PERSONAL NOTES PERSONAL NOTES

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.02
Page 1 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

2. Noise abatement procedures

The noise abatements procedures contained in PANS-OPS (Vol 1 Part I section 7) have been
designed for application to turbojet aeroplanes only.

Even if not required for turbopropeller aeroplanes, ATR recommends the following procedures for
noise reduction on the ground.

Do not use reverse while taxiing

Minimize the use of reverse at landing

No particular noise abatement procedures are recommended in flight.

Note:

1. Nothing in these procedures shall prevent the pilot-in-command from exercising authority
for the safe operation of the aeroplane [PANS-OPS Vol 1 Part I section 7 chap 1]

2. These procedures should not be required in adverse operating conditions such as:

a) if the runway is not clear and dry, i.e. if it is adversely affected by snow, slush, ice or water,
or by mud, rubber, oil or other substances.

b) In conditions when the ceiling is lower that 150 m (500ft) above aerodrome elevation, or

ALL ATR
when the horizontal visibility is less than 1.9 km

3. These procedures should not be required in case of any technical problem affecting the
safe operation of the aeroplane

Local aerodrome procedures: Refer to published airport manuals (In Jeppesen charts, the
Noise Abatement page is usually in chapter 10-4).

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.03
Page 1 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

3. Icing conditions
Please refer to Cold Weather Operations book.
ALL ATR

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.04
Page 1 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

4. Operations on wet and contaminated runways

Please refer to the Performance book.

ALL ATR

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.05
Page 1 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

5. Push-back operations
5.1. Power back
72 PEC

Power back is done after ATC clearance.

Ground staff area checked cleared before and during power back, by using conventional signs
and / or headphones with several people, as per prevailing airline policy.
To avoid moving forward, apply slight power back just before releasing brake.
Each crew member keeps his feet on the floor. NEVER USE BRAKES during power back
(to avoid tail strike).
Nose wheel steering remains ON.
Use Ground Idle or positive power to decrease speed or stop.
Power back is performed at low speed.
No specific ground staff phraseology.

5.2. Push-back with Tug

CAUTION: To avoid NAC OVHT triggering, the wind direction has to be taken into account for the
push back in hotel mode.
Push back is done after ATC clearance.
Ground staff remains connected with the aircraft by using conventional signs and / or headphones
with several persons according to airline policy. Parking brake released and steering OFF.
Each crew member keeps his feet on the floor. NEVER USE BRAKES during push back (to avoid
ALL ATR

tail strike and / or constraint on towing system). Wait for disconnection of the tow bar by the ground
staff before switching ON the steering
Set nose wheel steering to ON. Caution: never set the hydraulic of the steering before the
deconnection of the tow bar.
Specific phraseology is used:
72 not PEC

Flight events CM1 GROUND STAFF

CLEARED TO DO
PUSH BACK NOSE WHEEL STEERING SWITCH.........OFF
PARKING BRAKE..................................OFF

ANNOUNCE
GROUND FROM COCKPIT, I CONFIRM CLEAR
TO PUSH, NOSE NORTH (SOUTH, EAST, ANNOUNCE
WEST), PARKING BRAKE IS OFF, NOSE WHEEL STARTING PUSH
STEERING IS OFF

WHEN PUSH BACK

ANNOUNCE
COMPLETE
DO COCKPIT FROM GROUND, PUSH BACK
PARKING BRAKE...................................ON COMPLETE, PARKING BRAKE ON

TOW BAR ANNOUNCE

DISCONNECTED DO TOW BAR IS DISCONNECTED, YOU MAY
AND VISUALLY NOSE WHEEL STEERING SWITCH..........ON CONNECT NOSE WHEEL STEERING
CONFIRMED BY CREW
ANNOUNCE
NOSE WHEEL STEERING IS ON, YOU CAN
DISCONNECT YOURSELF, GOOD BYE

CM 2 REQUEST TAXI CLEARANCE

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.06
Page 1 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

6. Start up engine n1 during taxiing

The ATR Training Center uses "start of both engines on stand". Nevertheless, ATRs planes are technically
able to start ENG 1 during taxiing. This procedure is an operators choice and under its responsiblity. For
safety reasons, engine 1 start must be performed on a clear taxiway, and in low workload environment.
Flight events CM1 CM2
On captain ORDER
decision START ENGINE 1, RADIO MY SIDE

After OUTSIDE ANNOUNCE

VISUAL CHECK STARTING ENG 1

DO
START 1 PB........................... DEPRESSED
TIMING.......................................... START

NH = 10% DO AND ANNOUNCE

(UNTILL NH=19% if CL 1...................................... FEATHERED
ITT>200C FUEL OPEN

DO
ENGINE PARAMETERS................... CHECK

ITT increasING ANNOUNCE

IGNITION
DO
ENGINE PARAMETERS................... CHECK

NH = 25% ANNOUNCE
ECU

NH NCREASING DO AND ANNOUNCE

ENGINE PARAMETERS................... CHECK
OIL PRESS

NH = 45% ANNOUNCE
45%, STARTER OFF

DO
STARTER OFF................................ CHECK
TIMING............................................STOP
ITT MAX........................................ CHECK

ANNOUNCE
ITT XXX C

NH = 61.5% ANNOUNCE
PARAMETERS STABILIZED

PARAMETERS DO
STABILIZED ENGINE START........... OFF & START ABORT
DC GEN 1 FAULT............... EXTINGUISHED
DC BTC................................ CHECK OPEN
BLEED / PACKS...... LIGHTS EXTINGUISHED
OVERHEAD PANEL DARK (EXCEPTED THE
FAULT LIGHT ILLUMINATED ON EXHAUST
MODE PB FOR 2 MINUTES AND ALSO ACW
GEN 1 FAULT LIGHT)
ORDER
42 not PEC

CL1 MAX RPM DO AND ANNOUNCE

CL 1......................................... MAX RPM
CL1 MAX RPM

WHEN NP STABILISED ANNOUNCE

AROUND 71% LOW PITCH
CHECK
ACW GEN 1................................ ON LINE

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.06
Page 1 02
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

6. Start up engine n1 during taxiing

The ATR Training Center uses "start of both engines on stand". Nevertheless, ATRs planes are technically
72 PEC

able to start ENG 1 during taxiing. This procedure is an operators choice and under its responsiblity. For
safety reasons, engine 1 start must be performed on a clear taxiway, and in low workload environment.
Flight events CM1 CM2
On captain ORDER
decision START ENGINE 1, RADIO MY SIDE

After OUTSIDE ANNOUNCE

VISUAL CHECK STARTING ENG 1
DO
START 1 PB........................... DEPRESSED
TIMING.......................................... START

NH = 10% DO AND ANNOUNCE

(UNTILL NH=19% if CL 1...................................... FEATHERED
ITT>200C FUEL OPEN
DO
42 PEC

ENGINE PARAMETERS................... CHECK

ITT increasING ANNOUNCE
IGNITION
DO
ENGINE PARAMETERS................... CHECK
NH NCREASING DO AND ANNOUNCE
ENGINE PARAMETERS................... CHECK
OIL PRESS

NH = 45% ANNOUNCE
45%, STARTER OFF
DO
STARTER OFF................................ CHECK
TIMING............................................STOP
ITT MAX........................................ CHECK

ANNOUNCE
72 not PEC

NH = 61.5%
ITT XXX C

PARAMETERS ANNOUNCE
STABILIZED PARAMETERS STABILIZED
DO
ENGINE START........... OFF & START ABORT
DC GEN 1 FAULT............... EXTINGUISHED
DC BTC................................ CHECK OPEN
BLEED / PACKS...... LIGHTS EXTINGUISHED
OVERHEAD PANEL DARK (EXCEPTED THE
FAULT LIGHT ILLUMINATED ON EXHAUST
MODE PB FOR 2 MINUTES AND ALSO ACW
42 PEC ORDER GEN 1 FAULT LIGHT)
72 PEC CL1 AUTO DO AND ANNOUNCE
CL 1............................................... AUTO
CL1 AUTO
72 not PEC ORDER
CL1 MAX RPM DO AND ANNOUNCE
CL 1......................................... MAX RPM
CL1 MAX RPM

WHEN LOW PITCH 42 PEC ANNOUNCE

AND SGL CH LIGHTS
ILLUMINATED
72 PEC SINGLE CHANNEL LOW PITCH

72 not PEC ANNOUNCE

LOW PITCH

WHEN NP STABILISED CHECK

AROUND 71% ACW GEN 1................................ ON LINE

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.06
Page 2 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

ENGINE 1 START DURING TAXI FLOW

CM2
1 ENGINE START ROTARY SELECTOR: A+B
START 1 PB: ON
Depress the START 1 PB after a visual check on left side.
10
2 TIMING: START

3 CONDITION LEVER 1: FEATHER

7
1 Advance condition lever 1 to feather when NH reaches
10% and announce: FUEL OPEN.

4 ENGINE PARAMETERS: MONITOR

When the ITT needle increases, annouce: IGNITION.

5 ECU FAULT LIGHT: EXTINGUISH

At 25% NH, check that the ECU fault light extinguishes,
announce ECU ON.

6 ENGINE PARAMETERS: MONITOR

OIL PRESS needle increase, announce OIL PRESS
At 45% NH, announce 45%
42 not PEC
Stop timing, announce STARTER OFF if ON, white light
9 5 extinguished on START 1 PB.
2 7 ENGINE START ROTARY SELECTOR: OFF

ALL ATR
When engine parameters are stabilised, announce
8 6 PARAMETERS STABLISED, then turn the rotary
selector to OFF/START ABORT.
72 PEC 4
8 CONDITION LEVER 1: MAX RPM/AUTO
42 PEC
8 PEC SINGLE CHANNEL TEST: CHECK
Check SGL CH is illuminated, then extinguished.

9 LO PITCH LIGHT: ILLUMINATED

10 ACW GEN 1: ON LINE

8 Check ACW BTCs OPEN.

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.07
Page 1 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

PERSONAL NOTES
7. Operating minima
7.1. Definitions

MEA (Minimum En-route IFR Altitude)

The lowest published altitude (or Flight Level) between radio fixes that meets obstacle clearance
requirements between those fixes and in many countries assures acceptable navigational and
radio signal coverage.

MORA (Minimum Off-Route Altitude)

A MORA route provides reference point clearance within 10 NM (18.5 km) of the route centerline
(regardless of the route width) and end fixes.

A MORA grid altitude provides a reference point clearance within the section outlined by latitude
and longitude lines.

MORA values clear all reference points by 1000-ft (300 m) in areas where the highest reference
points are 5000-ft (1500 m) MSL, or lower.

MORA values clear all reference points by 2000-ft (600 m) in areas where the reference points are
above 5000-ft (1500 m) MSL.

ALL ATR
When a MORA is shown along a route as unknown or within a grid as unsurveyed a MORA is
not shown due to incomplete or insufficient information.

MOCA (Minimum Obstruction Clearance altitude)

The lowest published altitude in effect between radio fixes on VOR airways, off-airways routes, or
route segments, which meets obstacle clearance requirements for the entire route segment.

MSA (Minimum Sector Altitude)

Altitude depicted on instrument approach, SID or STAR charts and identified as the minimum safe
altitude which provides a 1000 ft (300 m) obstacle clearance within a 25 NM (46 km) (or other value
as stated) radius from the navigational facility upon which the MSA is predicated.

Terminal area

Except during IFR approach or departure, when on track with a published minimum altitude on
airport charts, the minimum altitude must not be lower than the Minimum Sector Altitude (MSA).

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.07
Page 2 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

7.2 Approach minima

7.2.1. Classification of airplanes

For approach, aircraft are classified in categories: A, B, C, D, and E.

The criteria taken into account for the classification of airplanes is the indicated airspeed at threshold
(VAT ) in landing configuration at the maximum certified landing weight.

VAT = 1.3 VS for ATR 42 300 or VAT = 1.23 VS1G for the other ATR models. ATR aircraft are
classified class B.

The airplane categories corresponding to VAT values are in the table 2 below:

Aircraft category (multi-engine) - Extracted from Appendix 2 to OPS 1.430 c

Aeroplane
VAT
Category
A VAT < 91 kt
RVR = Reported Meteorological
B 91visibility
kt  VATmultiplied
<121 kt by
Lighting element in operation
Day Night
C 121 kt  VAT <141 kt

ALL ATR
HI approach and runway lighting 1.5 2.0
D
Any type of lighting installation other 141 kt  VAT <166 kt
1.0 1.5
than above
No lighting E 1.0kt  VAT < 211
166 Notktapplicable

* This table can be used only for flight management, never for flight preparation.

7.2.2 Procedure protections

Indicated speed in Kt
ATR is integrated in category B

Vat 91/120 Kt
* Speed use in parallel
entry
Initial Approach 120/180/(170) Kt*

Final Approach 85/130 Kt

Circle to land 135 Kt

Missed approach 130/150 Kt

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.07
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ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

7.2.3. Obstacle clearance

The arrow represents the radius for the circle to land protection zone.

ATR is integrated in category B

Speed 135 Kt

Radius 2.8 Nm

Obstacle clearance 295 Ft

OCH 492 Ft

Minimum visibility 2.8 Km

7.2.4. Entry in the standard Patterns:

(1) parallel entry

ALL ATR

Parallel holding course, turn left and return to holding fix or intercept holding course

(2) teardrop entry

Proceed on outbound track of 30 to holding course, turn right to intercept holding course.

(3) direct entry

Turn right and fly the pattern.

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.07
Page 4 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

7.3. RVR / visibility

All tables are extracted from the OPS 1.430 appendix 1.

7.3.1. Take-off
Facilities RVR / Visibility (3)
Facilities RVR / Visibility (3)
Nil (day only) 500 m
Nil (day only) 500 m
Runway edge lighting and/or centreline marking 250/300 m (1) (2)
Runway edge lighting and/or centreline marking 250/300 m (1) (2)
Runway edge and centreline lighting 200/250 m (1)
Runway edge and centreline lighting 200/250 m (1)
Runway edge, centreline lighting and multiple
Runway edge, centreline lighting and multiple 150/200 m (1) (4)
RVR information 150/200 m (1) (4)
RVR information
(1) Higher values apply to Category D aircraft.
(1)
(2) Higher
For values
night apply to
operations, atCategory
least the D aircraft.
runway edge and runway end lights are required.
(2)
(3) For night
The operations,
Reported VisibilityatRepresentative
least the runway edgefor
/ RVR andtherunway end of
initial part lights are required.
the take-off
(3) Themay
run Reported Visibility
be replaced byRepresentative
a pilot assessment./ RVR for the initial part of the take-off
(4) run may
The be replaced
required RVR value by amust
pilotbe
assessment.
achieved for all of the relevant RVR
(4) The required
reporting RVR
points valueasmust
except be in
stated achieved for all of the relevant RVR
(3), above.
reporting points except as stated in (3), above.

System minima for non precision approach aids

System minima for non precision approach aids
7.3.2. Non-precision approach
Facility (approach aid) lowest MDH (ft)
Facility (approach aid) lowest MDH (ft)
ILS with no glide path (LLZ) 250
ILS with no glide path (LLZ) 250
SRA (terminating at 1/2 NM.) 250

ALL ATR
SRA (terminating at 1/2 NM.) 250
SRA (terminating at 1 NM.) 300
SRA (terminating at 1 NM.) 300
SRA (terminating at 2 NM.) 350
SRA (terminating at 2 NM.) 350
VOR 300
VOR 300
VOR/DME 250
VOR/DME 250
NDB 300
NDB 300
VDF (QDM and QGH) 300
VDF (QDM and QGH) 300

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.07
Page 5 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

7.3.3. Cat I approach

Facilities/RVR (5)
Decision
Height Full Basic Nil
(7) Intermediat
(1)(6) (3)(6) (4)(6)
e (2)(6)
200 ft 550 m 700 m 800 m 1000 m

201-250 ft 600 m 700 m 800 m 1000 m

251-300 ft 650 m 800 m 900 m 1200 m

301 ft and
800 m 900 m 1000 m 1200 m
above
(1) Full facilities comprise runway markings, 720 metres of HI/MI approach lights, runway
edge lights, threshold and end lights. Lights must be on.
(2) Intermediate facilities comprise runway markings. 420-719 metres of HI/MI approach
lights, runway edge, threshold and end lights. Lights must be on.
(3) Basic facilities comprise runway markings, less than 420 metres of HI/MI approach
lights, runway edge, threshold and end lights. Lights must be on.
(4) Nil approach light facilities comprise runway markings, runway edge, threshold and
end lights or no lights at all.
(5) The RVR values are either as reported, or met visibility converted as in the previous
table.
(6) The above figures are only applicable to conventional approaches with a slope not
exceeding 4.
(7) The DH mentioned in the table refers to the initial calculation of DH; when selecting the
associated RVR it is not necessary to take account of rounding up to the nearest ten feet which
may be done for operational purposes.
ALL ATR

7.3.4. RVR / visibility conversion

RVR = Reported Meteorological

visibility multiplied by
Lighting element in operation
Day Night

HI approach and runway lighting 1.5 2.0

Any type of lighting installation other
1.0 1.5
than above
No lighting 1.0 Not applicable

* This table can be used only for flight management, never for flight preparation.

Indicated speed in Kt
ATR is integrated in category B

Vat 91/120 Kt
* Speed use in parallel
entry
Initial Approach 120/180/(170) Kt*

Final Approach 85/130 Kt

Circle to land 135 Kt

Missed approach 130/150 Kt

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.07
Page 6 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

7.4. Flight preparation

ALL ATR

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.07
Page 7 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

7.5. Airport approach facilities

7.5.1. Runway approach line

ALL ATR

Full facilities comprise runway markings, 720 meters of HI/MI approach lights, runway edge lights,
threshold and end lights. Lights must be on.

Intermediate facilities comprise runway markings. 420-719 meters of HI/MI approach lights runway
edge, threshold and end lights. Lights must be on.

Basic facilities comprise runway markings, less than 420 meters of HI/MI approach lights, runway
edge, threshold and end lights. Lights must be on.

Nil approach light facilities comprise runway markings, runway edge, threshold and end lights or
no lights at all.

FOR TRAINING ONLY

 NORMAL PROCEDURES 04.07
Page 8 01
ADDITIONAL STANDARD
OPERATING PROCEDURES JUN 09

7.5.2. Visual aids

VASI STANDARD VASI 2 BARS

(Used for ATR cockpit)

HIGH

HIGH

HIGH
ON
SLOPE

ON
SLOPE
LOW

LOW

ALL ATR
PAPI

HIGH

SLIGHTLY HIGH

ON SLOPE

SLIGHTLY LOW

LOW

FOR TRAINING ONLY

PERSONAL NOTES

FOR TRAINING ONLY

 05.01
NORMAL PROCEDURES Page 1 01
SCHEMATICS JUN 09

1. Take-off
Normal or icing conditions

ALL ATR
FOR TRAINING ONLY
 05.02
NORMAL PROCEDURES Page 1 01
SCHEMATICS JUN 09

2. ILS 2 Engines
Normal or icing conditions

RESPECT STABILIZATION SCREEN HEIGHT: 1000 FT IMC / 500 FT VMC. IF NOT:

ALL ATR
GO-AROUND

flaps

FOR TRAINING ONLY

 05.03
NORMAL PROCEDURES Page 1 01
SCHEMATICS JUN 09

3. Non precision approach

Normal or icing conditions

RESPECT STABILIZATION SCREEN HEIGHT: 1000 FT IMC / 500 FT VMC. IF NOT:

GO-AROUND

ALL ATR
FOR TRAINING ONLY
 05.04
NORMAL PROCEDURES Page 1 01
SCHEMATICS JUN 09

4. Circling approach
Normal or icing conditions

ALL ATR
FOR TRAINING ONLY
 05.05
NORMAL PROCEDURES Page 1 01
SCHEMATICS JUN 09

5. Go-around 2 engines
Normal or icing conditions

ALL ATR
FOR TRAINING ONLY
 05.06
NORMAL PROCEDURES Page 1 01
SCHEMATICS JUN 09

6. Standard visual pattern 1500 ft AAL

Normal or icing conditions

ALL ATR
RESPECT STABILIZATION SCREEN HEIGHT: 1000 FT IMC / 500 FT VMC. IF NOT:
GO-AROUND

White Bug White Bug +10

or Red Bug or Red Bug +10

FOR TRAINING ONLY

 Dear Readers,
Every effort has been made to ensure document quality.

However please do not hesitate to share your comments and information with us by using
the following address: flight-ops-support@atr.fr

Yours faithfully

Your ATR Training and Flight Operations support team.

ATC June 2009

All reasonable care has been taken by ATC to ensure the accuracy of the present document.
However this document does not constitute any contractual commitment from the part of ATC which will offer,
on request, any further information on the content of this brochure. Information in this brochure
is the property of ATC and will be treated as confidential. No use or reproduction or release to a third part
may be made there of other than as expressely authorized by ATC.