B1900D

STANDARD
OPERATING
PROCEDURES
(SOP)
Issue Date 31 Aug 2015
Revision date 17 Jul 2017

WARNING
The Raytheon Beech B1900D must be operated in accordance
with the FAA approved Aeroplane Flight Manual.

This document is to assist crews undergoing conversion

training to integrate the aircraft manufacturers procedures into a
practical flow. This document therefore must be consulted in
conjunction with the B1900D AFM and should a discrepancy
exist the aircraft AFM shall take precedence.

Controlled Document – Do not copy/reproduce without prior permission of

Director Operations
 TABLE OF CONTENTS

Serial Items Pages

1 INTRODUCTION 5
1.1 INTRODUCTION 6
1.2 DISTRIBUTION LIST 6
1.3 HOW TO FILE REVISION 6
1.4 REVISION SUMMARY 7
1.5 REVISION RECORD 8
1.6 LIST OF EFFECTIVE PAGES 9
2 GENERAL 10
2.1 GENERAL OPERATION 11
2.2 STERILE COCKPIT 11
2.3 TRANSPONDER USAGE 11
2.3.1 VHF RADIO USAGE 11
2.4 ILLUMINATION OF MASTER 11
WARNING/CAUTION
2.4.1 OPERATION OF ENGINE ANTI-ICE 11
2.5 REJECTED TAKE OFF PROCEDURE 16
2.6 AUTOPILOT AND FLIGHT CONTROL PANEL 16
PROCEDURES
2.7 ATC CLEARANCES 16
2.8 CHECKLIST USAGE 16
2.9 NORMAL CHECKLIST 18-19
3 PREFLIGHT DUTIES / COCKPIT 20
PREPARATION
3.1 BRIEFINGS
3.2 CREW DUTIES
3.3 DOCUMENTATION
3.4 COCKPIT SAFETY CHECKS 21-22
3.5 COCKPIT SYSTEM CHECKS 23-24
3.6 COCKPIT PRE FLIGHT 25-29
3.6.1 REVIEW OF SPEEDS AND TAKE OFF DATA 26
3.6.2 THREATS, HAZARDS AND BRIEFINGS 27
4 ENGINE START 30
4.1 BEFORE START 31
4.2 ENGINE START (BATTERY) 32-36
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Serial Items Pages

5 TAXI 38
5.1 TAXI 39
5.2 POWER BACK 39
5.3 EXTERIOR LIGHTS 39
5.4 BRAKES CHECKS 39
5.5 TAXI SPEED 39
5.6 WEATHER RADAR 39
5.7 INSTRUMENT AND REVERSE THRUST 39
CHECK
5.8 ATC CLEARANCE 39
5.9 TAXI PROCEDURE 40
5.9.1 SYSTEM CHECKS 40
6 BEFORE TAKE OFF 41
6.1 PRIOR TO RUNWAY ENTRY 42-44
6.2 CLEARED TO ENTER THE RUNWAY 45
6.3 TAKE OFF CLEARANCE OBTAINED 45
7 TAKE OFF & DEPARTURE 46
7.1 TAKE OFF 47-49
7.2 AT TRANSITION ALTITUDE 50
7.3 AT FL 100 50
7.4 CLIMB 50
7.5 AT TOP OF CLIMB 50
8 CRUISE 51
8.1 TOP OF CLIMB 52
8.2 CRUISE 52
8.3 TURBULENCE 52
8.4 NAV AID / FLIGHT PLAN 52
8.5 WEATHER RADAR 52
8.6 ENROUTE WEATHER 52
9 DESCENT AND LANDING 53
9.1 BEFORE TOP OF DESCENT 54
9.2 DESCENT 55
9.3 APPROACHING FL 100 55
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9.4 AT TRANSITION LEVEL 55
9.5 BEFORE LANDING 56
9.6 AFTER LANDING 57
9.7 ONCE CLEAR OF THE ACTIVE RUNWAY 57-59
9.8 STATIONARY AT PARKING BAY 60
9.9 SHUTDOWN 60-61
10 APPROACHES 62
10.1 500 FT APPROACH STABLE 63-65
10.2 MONITORED APPROACH 66-68
10.3 PRECISION APPROACH CALL OUTS
10.4 NON-PRECISION APPROACH CALL OUTS
11 NON-NORMAL PROCEDURES 69
11.1 INTRODUCTION 70
11.2 DODAR PROCESS 71
11.3 RMM PROCESS 72
11.4 ABORTED TAKE OFF AND EVACUTION 73
11.5 ENGINE FAILURE 73
11.6 ENGINE FAILURE AT OR AFTER V1 75
11.7 ENGINE FIRE OR FAILURE IN FLIGHT 76
11.8 GO AROUND 77
11.8.1 SINGLE ENGINE GO AROUND 78
11.9 STALL RECOVERY (CLEAN) 79-80
11.9.1 STALL RECOVERY (CONFIGURED) 81
11.10 STEEP TURNS PROFILE 84
11.11 EMERGENCY DESCENT PROFILE 85
12 ADVERSE WEATHER OPERATIONS 86
12.1 TAKE OFF 87
12.2 LANDING 87
12.3 WINDSHEAR 87
12.3.1 WINDSHEAR AVIODANCE 87
12.3.2 WINDSHEAR RECOVERY MANOEUVRE 87-88
12.3.3 WINDSHEAR RECOVERY MANOEUVRE 88
CALL OUTS
13 SYSTEM CHECKS 89
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Serial Items Pages

13.1 AUTO FEATHER CHECK 90
13.2 OVERSPEED GOVERNOR & RUDDER 90
BOOST CHECK
13.3 GROUND IDLE LOW PITCH STOP CHECK 91
13.4 PRIMARY GOVERNOR CHECK 91
13.5 MANUAL FEATHER CHECK 91
14 CIRCUIT AND LANDING 92
14.1 CIRCUIT AND LANDING / TOUCH AND GO 93-97
PROCEDURE
GLOSSARY 98
 1900D Chapter 1 Page 5
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017

CHAPTER - 1

INTRODUCTION

Serial Items Pages

1.1 INTRODUCTION 6
1.2 CALL OUTS 6
1.3 REVISION SUMMARY 6
1.4 HOW TO FILE REVISION 7
1.5 REVISION RECORD 8
1.6 LIST OF EFFECTIVE PAGES 9
 1900D Chapter 1 Page 6
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
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1.1 INTRODUCTION
The operational policies, recommended procedures for crew coordination and CRM are
covered in this document to provide a basis for standardization. It should however be
noted that good judgment and logic cannot be replaced when conditions fall beyond the
scope of the procedures. Each crew member is assigned an area of responsibility.

1.2 DISTRIBUTION LIST

Master Copy of B-1900D Standards Operating Procedures is retained and controlled by
the office of Chief Pilot Training. Distribution list of B-1900D SOP is as under:

1. Head of Flight Operations.

2. All Flight Operations Chief Pilots.
3. All flight crew (B-1900D)

The distribution list will be maintained and updated by Chief Pilot Training according to
operational needs and requirements.

1.3 HOW TO FILE REVISIONS

This manual is controlled document and is audited to ensure that it is properly
maintained. When a revision is issued for this manual, following instructions shall be
followed as a guide line for the manual update process:-

STEP 1
Upon receipt of a revision packet, ensure that the revision received is in continuation to
the last revision record.

STEP 2
Before updating this manual with the new revision, make sure the manual has previous
revisions inserted.
1. Revision records for this manual are shown on page 8.
2. Compare the last revision signed off in the manual to the new revision.
3. The new revision will be the next number in sequence.
4. Insert the new revision and remove the old pages.

STEP 3
When new revision is inserted, turn to the REVISION RECORD page, insert date and sign
on the appropriate revision line.

NOTE: As revisions are received and entered in to this manual, complete the revision
record boxes. To maintain an accurate history of revisions, keep revision records sheet in
this manual. If a new revision record page is received, place the new page on top of the
previous page.

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STANDAR OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017

1.4 REVISION SUMMARY

This revision represents a major design change in the original Multi Crew Standard
Procedures, which has been an adaptation from the B190 SARPs. This revision
incorporates industry best practice and safety recommendations. The following list is a
summary of design and philosophy changes.
1. Standard Procedures and briefings simplified. Simpler procedures allows for
easier compliance and situational awareness in demanding situations.
2. Areas of responsibility. Major emphasis of crew operating areas of
responsibility. The same applies to the normal and non-normal operations.
3. PM responsibilities. The role and responsibility of the Pilot Monitoring
emphasized.
4. Checklist simplified. Only critical items and aircraft performance related items
are retained in the checklist. Other items are still done by flow but not
required in the checklist.
5. All briefings, aircraft setup and non taxi critical items are completed while the
aircraft is stationary allowing the crew to focus, not combining two things
together and avoid distractions during taxi.
6. Runway occupancy. Checklist and on runway actions reduced to minimize
runway occupancy time.
7. Emphasis on threat and error management.
8. Procedures re-aligned to conform to AFM requirements.
9. Non-precision call outs for CANPA (Constant Angle Non Precision
Approach)/Constant Descent Final Approach (CDFA) as recommended by
ICAO.
 1900D Chapter 1 Page 8
STANDARD OPERATING Issue Date 31 Aug 2015
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1.5 REVISION RECORD

Revision Issue Date Chapter Number Pages Date Entered Entered By Sig
Number
1 AUG 15 Title page
1 AUG 15 Table of contents 3,4
1 AUG 15 0 10 31 AUG 15
1 AUG 15 1 11,12,14,15,18,20 31 AUG 15
1 AUG 15 2 22,25,28 31 AUG 15
1 AUG 15 3 34 31 AUG 15
1 AUG 15 5 44,46 31 AUG 15
1 AUG 15 6 47,48,50 31 AUG 15
1 AUG 15 7 54 31 AUG 15
1 AUG 15 8 56,57 31 AUG 15
1 AUG 15 9 62,65,69 31 AUG 15
1 AUG 15 10 70,74,78,81-84 31 AUG 15
1 AUG 15 11 85,88 31 AUG 15
1 AUG 15 12 89-92 31 AUG 15
1 AUG 15 13 93-98 31 AUG 15

2 2 MAY 17 1.2 6 2 MAY 17

2 2 MAY 17 2.12, 2.13 7,18 2 MAY 17
2 2 MAY 17 3.3.2 27 2 MAY 17
2 2 MAY 17 5.9.1 40 2 MAY 17
2 2 MAY 17 11.2 71 2 MAY 17
2 2 MAY 17 11.10 84 2 MAY 17
2 2 MAY 17 11.11 85 2 MAY 17
2 2 MAY 17 12.3.3 88 2 MAY 17
2 2 MAY 17 14.1 93-97 2 MAY 17
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1.6 LIST OF EFFECTIVE PAGES

Chapter Item Effective Pages Revision Revision Date

2 AREA OF ACTION & RESPONSIBILITY 14,15 2 2 MAY 17
2.12 DOCUMENTATION 17 2 2 MAY 17
2.13 NORMAL CHECKLIST 18 2 2 MAY 17
3 SAFETY INSPECTION, SYSTEM CHECKS, 22,24,29 2 2 MAY 17
COCKPIT PREFLIGHT CHECKS
3.3.2 THREATS, HAZARDS AND BRIEFINGS 27,28 2 2 MAY 17
4 BEFORE TAXI FLOWS 37 2 2 MAY 17
5.9 TAXI PROCEDURE 40 2 2 MAY 17
6 PRIOR TO RUNWAY ENTRY FLOWS 43,44 2 2 MAY 17
9 AFTER LANDING, SHUTDOWN FLOWS 58-59, 61 2 2 MAY 17
11.2 DODAR PROCESS 71 2 2 MAY 17
11 CLEAN STALL RECOVERY PROFILE, TAKEOFF 80,82,83, 2 2 MAY 17
CONFIGURED STALL RECOVERY PROFILE,
LANDING CONFIGURED STALL RECOVERY
PROFILE
11.10 STEEP TURNS PROFILE 84 2 2 MAY 17
11.11 EMERGENCY DESCENT PROFILES 85 2 2 MAY 17
12.3.3 WINDSHEAR RECOVERY MANOEUVRE CALL 88 2 2 MAY 17
OUTS
14.1 CIRCUIT AND LANDING / TOUCH AND GO 93-97 2 2 MAY 17
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CHAPTER-2

GENERAL

Serial Item Page

2.1 GENERAL OPERATION 10
2.2 STERILE COCKPIT 11
2.3 TRANSPONDER USAGE 11
2.3.1 VHF RADIO USAGE 11
2.4 ILLUMINATION OF MASTER WARNING/ 11
CAUTION
2.4.1 OPERATION OF ENGINE ANTI-ICE 11
2.5 500 FT APPROACH STABLE 12
2.5.1 MONITORED APPROACH 12
2.6 BRIEFINGS 12
2.7 CREW DUTIES 12-13
2.8 REJECTED TAKE OFF PROCEDURES 16
2.9 AUTOPILOT AND FLIGHT CONTROL PANEL 16
PROCEDURES
2.10 ATC CLEARANCES 16
2.11 CHECKLIST USAGE 16
2.12 DOCUMENTATION 17
2.13 NORMAL CHECKLIST 18-19
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PROCEDURES
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2.1 General Operation

With regard to flight safety and general cockpit management, it is imperative that all
crewmembers adhere strictly to all governing documents (SARPS, Operations Manuals,
etc.). Standard call-outs are compulsory and unscheduled call-outs are only to be made
when deviations from standard flight paths are observed.

2.2 Sterile Cockpit

During ground maneuvering, operating in terminal areas while airborne, flight crew must
devote their full attention to operating the aircraft and must not allow secondary activities
such as paper work, unnecessary radio transmissions, unnecessary cockpit set-up, casual
conversation or interference from cabin crew or passengers to distract them from their
primary task. The Crew shall ensure a sterile cockpit when below 10000 ft AMSL and/or
clear of the terminal area and conversation shall be limited to only that pertinent to flight.

2.3 Transponder Usage

Transponders are to be used in flight at all times. If no transponder code has been
allocated, then 2000 on mode C is to be set.

2.3.1 VHF Radio Usage

VHF 1 should be used to communicate with ATC. VHF 2 should be used for all other
operational radio communication. Crew are to adhere to the requirements of position
reports as applicable. All radio procedures are to be made in accordance with ICAO Doc
4444 and to comply with ICAO ANNEXTURE 2 policies regarding use of head phones and
flight deck speaker use.

2.4 illumination of master warning/caution

If any caution/warning lights illuminate, either of the pilots will inform the other of the
reason for the illumination of the light before extinguishing the master caution light.

2.4.1 Operation of ENGINE ANTI-ICE

Ground: Engine Anti-Ice should remain ON for all ground operations. Engine Anti-Ice
should be set prior to take-off.
In-flight: Engine Anti-ice should be on whenever OAT is +5°C or below in visible moisture.

Take-off: Engine anti-ice must be OFF for all take-offs on paved runways above 10°C OAT.
For unpaved runways the take-off must be done with regards to the applicable
performance criteria as laid out in the AFM Supplementary section.

Landing: When landing on gravel/grass strips, Engine Anti-Ice should be opened prior to
landing. This shall be briefed during the normal Approach briefing.

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 STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES Revision 2 May 2017

2.5 500 FT APPROACH STABLE

The call “500 ft Approach Stable” is made by PM at 500 ft above DA/MDA referenced to
the pressure altimeter. This call is to ensure a last chance check that the aircraft is on a
stable flight path and will remain so until touchdown. Should the following parameters
not be satisfied, a Go-around must be executed for that approach. The aircraft should be
fully configured for landing by 1000 ft AGL in IMC OR in VMC by 500 ft AGL, with landing
checklist completed.

INSTRUMENT APPROACH VISUAL APPROACH

. Within ½ scale fly left / right . Within a 10 degree cone of runway centerline
. Within ½ scale glide slope . Within 20 degrees of runway heading
. Speed Vref to Vref +20kt . On visual glide path (VASI / PAPI)
. Engine above flight idle . Speed Vref to Vref +20kt
. Landing configuration . Engine above flight idle
. Stable rate of descent . Landing configuration
. Stable rate of descent

2.5.1 MONITORED APPROACH

All non-precision approaches should be flown as a monitored approach as well as all ILS
approaches where the weather is below: Cloud Base is less than 500ft and or if the
reported visibility is less than 2000m.

2.6 BRIEFINGS
Briefing between the two pilots is essential to achieve a safe multi-crew operation. It is
essential that each pilot is aware of what to expect in both normal and abnormal
situations. Briefings should be specific to the requirements of operation. Emphasis of the
briefings shall be on threat and error management and practical conduct of flight.

2.7 CREW DUTIES

Captain shall not designate if:
 Cloud base below 500ft or visibility less than 2000M (see monitored
approach).
 Cross wind component exceeds 15 Kts.
 Runway is slippery/contaminated or braking action reported as less than
good.
Pre-flight and post flight crew duties are divided between the Captain and First Officer.
Phase of flight duties are divided between the Pilot Flying (PF) and the Pilot Monitoring
(PM).

Each crewmember is responsible for moving the controls and switches in their area of
responsibility:

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 STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES Revision 2 May 2017

 The phase of flight areas of responsibility for both normal and non-normal
procedures are shown in the Area of Responsibility illustrations in this section.
Typical panel locations are shown.
 The Captain shall be designated '' Pilot Flying (PF)'' while the aero plane is on
the ground. He will taxi the aero plane and call for the required checklist. The
Captain shall handover the controls to the First Officer after the aero plane is
lined up and the Take off power is set (if the First Officer is designated to fly
the sector). Captain shall take over the controls prior to vacating the runway
after landing.

Captain may direct actions outside of the crewmember’s area of responsibility.

General PF phase of flight responsibilities are:

 Taxiing.
 Flight path and airspeed control.
 Airplane configuration.
 Navigation.

General PM phase of flight responsibilities are:

 Monitoring taxiing, flight path, airspeed, airplane configuration and
navigation.
 Checklist reading.
 Communications.
 Tasks asked for by the PF.

Any time that control of the aircraft is transferred from one pilot to the other, the
following phraseology shall be used:-
 Pilot taking control: “I HAVE CONTROL”.
 Pilot handing over control: “YOU HAVE CONTROL”.

When control is transferred, the pilot handing over control must make the other pilot
aware of the intentions and flight conditions e.g. track, altitude, autopilot selection
(on/off), flight director selection, etc.

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2.8 REJECTED TAKE OFF PROCEDURE

Procedure for RTO as given in chapter 11 is supplemented by the following:-

Decision to Reject Take Off. Whenever the either pilots decide to reject Take off, he/she
shall call ''STOP'' and promptly executes rejected Take off actions as stipulated in Chapter
11, sub Para 11.4. PF will keep his hand on the power levers until V1. PM shall precisely
call any malfunction or threat affecting the safety of the aircraft.

2.9 AUTOPILOT (AP) AND FLIGHT CONTROL PANEL (FCP) PROCEDURES

Crew must always monitor:-
 Airplane course.
 Vertical path.
 Speed.
When selecting a value on the FCP (Flight Control Panel), verify that the respective value
changes on the FMA (Flight Mode Annunciator), as applicable.
The Flight Control Panel (FCP) is the PF’s responsibility. On the B1900D both FCP’s operate
independently. For this reasoned due to the position of the FCP panels the PF must make
his own FCP selections and direct the PM to also make changes on their panel. The Auto
Pilot (AP) is the PF’s responsibility. When flying manually, the PF directs the PM to make
the changes on the (FCP) Flight Control Panel.
Announcing changes on the FMA (Flight Mode Annunciator) display when they occur is
good CRM practice.

2.10 ATC CLEARANCES

When a clearance are received and copied but not understood by both pilots as the same,
clarification from ATC should be sought immediately to resolve the conflict. Never resolve
a clearance issue by cockpit consensus alone. Acknowledge all clearances with a
COMPLETE read back including your FULL CALL SIGN.

At 1000 ft. before pre-selected altitude the PM will call, “1000 to level off”. The PF will
respond with the call, “Check”.

The following must be confirmed and acknowledged between pilots:-

 ATC clearance and altimeter settings and amendments thereto.
 Runway clearance before proceeding on to the active runway.
 Take-off clearance before power application.
 Landing clearance before landing.

If any doubt exists as to the clearance, a clarification will be requested from ATC
immediately.
 1900D Chapter 2 Page 17
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017

2.11 CHECKLIST USAGE

The normal checklist is challenge and response type checklist. The PF will call for the
checklist by name, where upon the PM will first read the checklist heading then the
checklist items. Upon a challenge from the PM the PF will respond with the appropriate
response.
In situations where the checklist states “As required” the correct response is that
corresponding to switch position. In situations where both pilots must respond the PF
shall respond first, followed by the PM.
The exceptions are the “After Take-off Checklist” which is done as a read and respond
checklist by the PM and the “Secure Checklist” which is completed as a read and do
checklist.
Abnormal checklists are completed as a “read and do” by the PM. Actions are based on
area of responsibility. Memory items in a checklist should be verified by both crew
members.

2.12 DOCUMENTATION
The following documents to be carried on board an aircraft:-
1. Certificate of Registration.
2. Certificate of Airworthiness.
3. Certificate of Radio Installation.
4. Noise Certificate.
5. PTA License.
6. Insurance Certificate.
7. Weight and Balance.
8. Operations Specification.
9. Charter and Arial Work License.
10. Aircraft Deferred Defect Discrepancy Record.
11. Journey Log Book.
12. Aircraft Technical Log Record.
13. Aircraft Repeated Defect Monitoring.
14. Passenger Manifest.
15. CMR (Cert of Maintenance Review).
16. MR (Maintenance Release).
17. Aircraft Flight Manual.
18. POH.
19. MEL.
20. Operations Manual.
21. Pilot Checklist.
22. KHF 950/990.
23. Normal Checklist.
24. Jeppesen Plates.
 25. SOP B1900D.

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STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017
2.13 BEECHCRAFT 1900D NORMAL CHECKLIST

PREFLIGHT (Read by FO) Response

Cockpit preparation............................ COMPLETED Both
Oxygen (First Flight of the Day)…. ON & CHECKED Both
Park Brake…………………………….…..……...…...... SET Capt
Nose Wheel Chocks…………………………………..... ON Both
BEFORE START (Read by FO) (start clearance)
Control Locks, Pogo stick……..…………… REMOVED Both
Beacon………………………..…………….….…....... GND Capt
Fasten Seatbelts Light …………………………….... ON Capt
Battery ................................…….….……_____VOLTS Capt
Doors……………………………………………...... CLOSED Capt
Fuel……..………….…….………….............. LBS Capt
Engine Anti-Ice ……………………………………….... ON Capt
Prop Levers …………………………………………...... TAXI Capt
Circuit Breakers….……….…….…….…….... CHECKED Both
BEFORE TAXI (Read by FO)
Nose Wheel Chocks Signal ………………. REMOVED Capt
Electrical.............….....…..…………….….. CHECKED Capt
T/O Data.................................. REVIEWED & SET PF
Flight Instruments..….....…….... SET & X-CHECKED PF
Standby Horizon...................... ON & UNCAGED FO
Flight Controls.........……....…….……....... CHECKED PF
Trims.......................................................... SET PF
Suction / Pneumatics………..….….….…... CHECKED FO
Pressurisation………………...…….….……....……. SET Capt
Rudder Boost.............................................. ON Capt
Electric Trim ………………………………………….... ON Capt
Manual Feather ………………………………. CHECKED Capt
T/O Briefing ………………………………..... COMPLETED PF
Cabin Briefing............................. TRANSMITTED Capt
BEFORE TAKE-OFF (Read by PM)
(Prior to entering runway)
Prop Levers…………..……..……….... FULL FORWARD PF
Fuel Condition Levers …………………….. HIGH IDLE PF
Flaps..........................….......……..…. 17, CHECKED PF
Trims….................................………..…....…... SET Capt
Bleeds / Environmental..........………………….. OFF PF
TCAS/Transponder................……..……......…. SET PF
WX Radar …………………………………………........ ON Capt
Engine Anti Ice….……….…………….... AS REQUIRED Capt
Auto-feather..…….…….…..…………..…...…. ARMED Capt
Ice Protection...................….…..….…..………. ON Capt
Annunciators………….………….....…... CONSIDERED PF
- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - --- (Cleared for Takeoff)
Auto Ignition…………………………………… ARMED Capt
Landing Lights………………………..….……......... ON PF

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STANDARD OPERATING Issue Date 31 Aug 2015
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Revision 2 May 2017
AFTER TAKE-OFF (Read by PM)
Landing Gear………..…..…..…….…........ UP, NO LIGHTS PM
Flaps...................………….………...……………....... UP PM
Yaw Damper…............…….…….…..……………….. ON PM
Bleeds / Environmental….…...….……... OPEN / AUTO PM
Engine Instruments……….…..….…..…… CHECKED PM
- - - - - - - - - - - - ---- TRANSITION ALT- - - - - - - - - - - ----
Altimeters.......….…….…………...... SET & X – CHECKED PM
Air-conditioning & Pressurization…..….... CHECKED PM
DESCENT AND APPROACH (Read by PM)
Landing Data…………………...……...……………..... SET PF
Approach Briefing ……………………… ... COMPLETED PF
Pressurization……….…...……………..…....... CHECKED PF
Auto-Feather....……...…………………….……. ARMED Capt
- - - - - - - - -------- AT TRANSITION LEVEL - - - - - - - - - --
Altimeters..….………………..…...... SET & X-CHECKED PF
Flight and Nav Instruments…….. SET & X-CHECKED PF
BEFORE LANDING (Read by PM)
Prop Levers …………………………...... FULL FORWARD PF
Landing Gear……….……………...... DOWN, 3 GREENS PF
Flaps…………………...…….……...……….................. 35 PF
Yaw Damper…………………………..……….……....... OFF PF
AFTER LANDING (Read by PM)
Strobes…………………………………....…………........ OFF PM
Lights……………………….……………...... AS REQUIRED PM
Engine Anti Ice……….…….……….….……...……..... ON PM
Auto-feather & Ignition…….…………….………….. OFF PM
Transponder ……………………………………............ STBY PM
Ice Protection…………………….………....………...... OFF PM
Prop Levers................................................... . TAXI PM
Fuel Condition Levers ……………………........ LOW IDLE PM
Flaps……………………….………………….….…….. UP PM
Trimmers…………………………….………........... NEUTRAL PM
Wx Radar.…………………………………….......... STBY/OFF PM
SHUTDOWN (Read by FO)
Park Brake…………………….……………………... SET Capt
Standby Horizon ………………………….... CAGED/OFF FO
EFIS switches........................................... OFF FO
Blowers/ Environmental …….……….…...... AUTO/OFF FO
EFIS Aux Power ……………………………………. OFF Capt
Avionics Switch………………….……………….… OFF Capt
AC Busses……………………………..….………..... OFF Capt
Prop Levers……………………….………...........FEATHERED Capt
Gang Bar…………….…………….……………..…... OFF Capt
Oxygen (Last Flight of the Day)……….…….. OFF Capt
- - - - - - - - - - - - - - - - - - - - - - - - - - (night operations)
Emergency Lights…...……..……………………… OFF Capt
Lights……………………….……………….………..... OFF Capt
 1900D Chapter 3 Page 20
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017

CHAPTER - 3

PRE FLIGHT DUTIES/COCKPIT PREPARATION

Serial Items Pages

3.1 COCKPIT SAFETY CHECKS 21-22
3.2 COCKPIT SYSTEM CHECKS 23-24
3.3 COCKPIT PRE FLIGHT 25-27
3.3.1 REVIEW OF SPEEDS AND TAKE OFF DATA 26
3.3.2 THREATS, HAZARDS AND BRIEFINGS 27
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STANDARD OPERATING Issue Date 31 Aug 2015
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3.1 COCKPIT SAFETY CHECKS
3.2

CAPT FO
THE CAPTAIN IS RESPONSIBLE FOR CHECKING THE THE FIRST OFFICER IS RESPONSIBLE FOR DOING THE
SERVICABILITY/ AVAILABILITY OF THE FOLLOWING LOADSHEET AND PAPER WORK FOR EACH SECTOR.
EQUIPMENT:
ELEVATOR TRIM………………………. 1.5 UNITS NOSE UP
CRASH AXE
GOGGLES FO AND CAPT COMPLETE THE WALK AROUND AS PER THE BEECH
HALON EXTINGUISHER (BELOW CO-PILOTS SEAT) 1900 D AFM
SAFETY EQUIPMENT
FIRST AID KIT --------------------------------------------------------------------
SIGNAL STRIPS
SURVIVAL KIT (IF CARRIED) HALON EXTINGUISHERS…………..…......SERVICABLE
DOCUMENTATION
FLIGHT FOLIO (VALID CERT. OF SAFETY) 1. AT FWD DOOR
MEL 2. CARGO COMPARTMENT (IF INSTALLED)
AFM ₀ CHARGE IN GREEN ARC
POH ₀ EXPIRY DATE
EMERGENCY CHECKLIST ₒ CONTENT
NORMAL CHECKLIST ₒ SECURED IN CLIPS
TOLD CARDS
JEPPS EMERGENCY EXITS………………....……...UNLOCKED
LOADSHEET
GENERAL DECLARATION (if required) GROUND LOCK PINS REMOVED

PASSENGER BRIEFING CARDS……….....EACH SEAT

SAFETY INSPECTION CHECKS CABIN DOOR PRESSURE GAUGE.......1350 – 1450 PSI

CONTROL LOCKS………………..……................REMOVED (WITH OPEN DOOR)
MIC SELECT (Pilot & Co Pilot)....................NORMAL
WINDSHIELD WIPERS………...……………….....OFF
MASTER PANEL LIGHT SWITCH…………......AS REQ.
LIGHT RHEOSTATS ……………………..............AS REQ.
EXTERIOR LIGHTS......................................OFF

BATT VOLTAGE…..……………....….…........…...CHECK
MINIMUM OF 23 VOLTS FOR BATTERY START

CABIN OXYGEN………………………………..........CLOSED
PILOT’S SUBPANEL SWITCHES………….....…..ALL OFF
ENGINE ANTI-ICE……………………………………..ON
LANDING GEAR………………………...………........DOWN
LG GEAR RELAY CB IN
LDG GEAR DOWN LOCK REL LATCH IN PLACE

FLAP LEVER.........................MATCHES FLAP POSITION

L/G ALTERNATE EXTENSION HANDLE...…......STOWED

1900D Chapter 3 Page 22

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 1900D Chapter 3 Page 23
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3.2 COCKPIT SYSTEM CHECKS (FIRST FLIGHT OF THE DAY)
CAPT FO
FUEL FIREWALL VALVES……..……...PULL CLOSED ENSURE LOAD AND BAGGAGE IS SECURE
BATT…………………………….…………...…...……ON
BATTERY…………………………………………………MIN 23V
ANNUNCIATOR LIGHTS……….……….…..…..TEST
WARNING AND CAUTION / ADVISORY PANELS
MASTER WARNING / CAUTION
AFX REPEATER, GND COMM PWR, VG FAST ERRECT
ALT ALERT, YD ENGAGE,
STANDBY HORIZON POWER/ EFIS AUX POWER
FIRE EXT L/R ………………..…………………….TEST
TEST A…………....…YELLOW D & GREEN OK ILLUMINATED
TEST B……………….GREEN OK ILLUMINATED
FIREDET L/R..….…..……………………………….TEST
LOOP…………….....…FIRE LOOP & MASTER CAUTION
ANNUNCIATORS ILLUMINATED
AMP…………………….....…..........T-HANDLES ILLUMINATED
..RED L + R ENG FIRE PUSH TO EXT ILLUMINATED
.....….MASTER WARNING FLASHERS ILLUMINATED

STALL/OVERSPEED WARNING…………...….TEST
COCKPIT VOICE RECORDER.......................TEST
LANDING GEAR HANDLE LIGHTS…..….………TEST
CHECK SERVICABILITY OF BOTH GLOBES

STBY BOOST PUMPS…..……………………….…....ON

FUEL FIREWALL VALVES………...…….....PUSH OPEN
RIGHT……….R FUEL PRESS ANNUNCIATORS EXTINGUISHED
LEFT………….L FUEL PRESS ANNUNCIATORS EXTINGUISHED

L/R STANDBY PUMPS INDIVIDUALLY……………OFF

LEFT…………….L FUEL PRESS ANNUNCIATORS ILLUMINATED
……………....MASTER WARNING FLASHER ILLUMINATED
RIGHT………….R FUEL PRESS ANNUNCIATORS ILLUMINATED
…………....MASTER WARNING FLASHER ILLUMINATED
TRANSFER FLOW………………………........LEFT/RIGHT
LEFT……………….....TRANSFER ANNUNCIATOR ILLUMINATED
……..RIGHT FUEL PRESS ANNUNCIATOR EXTINGUISHED
RIGHT……………......TRANSFER ANNUNCIATOR ILLUMINATED
………..LEFT FUEL PRESS ANNUNCIATOR EXTINGUISHED
AUX PUMP SWITCHES...............................AS REQ.
FUEL QUANTITY……………………………….....…CHECK
MAIN AND AUX QUANTITIES
BATT VOLTAGE.................……….…………..CHECK
BATTERY………………………………………………........MIN 23V
TRIPLE BUS………………………………………………….MIN.22V
CENTRE BUS…………………………………………………MIN23V
BATTERY……….…………………………….………...OFF
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3.3 COCKPIT PRE-FLIGHT
CAPT FO
OAT GAUGE...………………………..………..........CHECK GOGGLES……………………..………….…...STOWED
FUEL PANEL...…….......................................CHECKED/ SET OXYGEN MASK……….…..…SELECT 100%, PUSH TO TEST
 CIRCUIT BREAKERS…………………………………...CHECK AUDIO PANEL………………….SET AS REQUIRED
 AUX PUMP (IF FUEL IN AUX TANKS)…………..AUTO  L & R ROTARY TRANSMIT SELECTOR…….COMM 1
PILOT’S STATIC AIR SOURCE..…..…….........NORMAL  L & R AUDIO SELECTORS……………COMM 1 & ON
OXYGEN...............................……….…….......PULL ON  OTHER AUDIO SELECTORS…………………OFF
EFIS AUX POWER.......................................TEST  SPEAKERS …………………………………………OFF
 TEST.....................Green Test Annunciator Illuminated  HOT MIC……………………………………………ON
 ON..................Amber Aux ON Annunciator Illuminated  TRANSPONDER……………………………......SELECT #1
 .................................Aux Battery Warning Horn Sounds STANDBY HORIZON PWR.......................ON
 Aux Batt. Warning Horn..........................Push to Cancel  TEST.....................Green Test Annunciator
COMPASS MODE……...........….…....…........SLAVED Illuminated
CLOCK…….……………...................WIND, SET UTC, X CHECK  ON..................Amber Aux ON Annunciator
ASI…………………………..….………………...........CHECK Illuminated
 Pointer Zero  .................................Aux Battery Warning Horn
 Barbers Pole indicating 247 KIAS Sounds
RMI……………………......................CHECK SERVICABLE/FLAG  Aux Batt. Warning Horn..........................Push to
Cancel
EADI/EHASI DIMMERS.............................. OFF MAX
 Standby Horizon Aux
BALANCE BALL ON EADI………………………....CHECK
power.....................................OFF
ENCODING ALTIMETER…..............……........SET/FLAG STANDBY HORIZON............................CAGED
 FIELD ELEVATION
AVIONICS PANEL……………………………….SET
VSI..............................................................ZERO
 COMM CONTROLLERS………ON
PROP SYNC…………………………….…….…........ON
 NAV CONTROLLERS……………ON
ENGINE INSTRUMENTS…………….……….......CHECK
 ALT SEL……………INITIAL ALT SET
 ITT’S……........................................................COOL DOWN
TEMP
 GPS…………………………………ON
 TORQUE’S ……..…………………………………………..RESIDUAL  ADF…………………………………ADF
 PROP PRM’S ……………………………………………...ZERO  TRANSPONDER ……………….STBY
 N1……………………………………………………………...ZERO ASI….…………………………...……………….....CHECK
 FUEL FLOW………………………………………………….ZERO RMI……..………....…….............CHECK SERVICEABLE/FLAG
 OIL PRESSURES …………………………………………...ZERO EADI/EHSI DIMMERS.........................OFF MAX
 OIL TEMP’S ………………………………………………...ZERO EADI BALANCE BALL………………………...CHECK
ALTIMETER………….……………….............A/F ELEVATION
PILOT AIR AND DEFROST…................…......SET VSI………………………..….……………………....ZERO
OXYGEN MASK………………………………...........CHECK OXYGEN GUAGE……………………............SERVICEABLE
 SELECT 100% COMPASS MODE…...……...………………..SLAVED
 PUSH TO TEST VENT AIR…………………..…….……............PUSH CLOSE
MASTER PANEL LIGHT SWITCH…………........SET BLEED AIR VALVES………..…..……….......ENVIR OFF
LIGHT RHEOSTATS ……………………......….......SET BLOWERS..…….……..………..……………..…AUTO
CABIN LIGHTS……………………...……..….….......AS REQUIRED AUTO TEMP………………..……….…..........AS REQUIRED
LOAD/VOLT/ BATT AMMETER GUAGES…...CHECK ENVIR MODE CONTROL…..…..……..…..OFF
FREQ/AC VOLTMETER GAUGE……………......CHECK CABIN AIR AND CO-PILOT AIR…..…......AS DESIRED
EMERGENCY LIGHTS…………….........…..........AS REQ SUCT/PNEUMATICS GAUGES..………...CHECK
STBY COMPASS………………….….………...........CHECK OXYGEN CONTENTS……..................SUFFICIENT FOR FLT
FUEL FIREWALL VALVES…….………..……........PUSH OPEN CO-PILOTS STATIC AIR SOURCE….....….NORMAL
FLAP GAUGE……..…………….……….….…..........CHECK CO-PILOTS CIRCUIT BREAKER PANEL..…CHECK
CABIN VSI…………………..………...………….........ZERO
CABIN ALT……...…………………….....................PRESS ALT
 1900D Chapter 3 Page 26
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CABIN DIFF…………………….…….…………..........ZERO
POWER LEVERS…………..........................MOVEMENT/IDLE/
SET FRICTION KNOBS
CAUTION: DO NOT LIFT AND MOVE INTO GROUND FINE RANGE
PROP LEVERS……............................MOVEMENT/FORWARD/
SET FRICTION KNOB
COND. LEVERS.……....................MOVEMENT/FUEL CUTOFF/
SET FRICTION KNOB
ELEVATOR TRIM ..……..........................CHECK/SET FOR T/O
AILERON TRIM………….……….…………..…0 (NEUTRAL)
RUDDER TRIM………….……….…………..….0 (NEUTRAL)
EFIS POWER SWITCHES.………..……….................……OFF
EFIS REVERSIONARY PANEL SWITCHES..................SET
 AP/YD TO SIDE OF PF
 ALL OTHER SELECTIONS OFF OR NORMAL
EFIS DSP PANEL......................................................SET
 NAV DATA........................GSP
 HSI MODE.........................HSI
 COURSE SELECT................ACT
RADAR.…………………………………………...................…..SET
 STBY
 MAX GAIN
 TILT 5° UP
 STAB ON
 25nm RANGE
RUDDER BOOST......................................................ON
ELEVATOR TRIM….…………………...................……..….ON
PARK BRAKE..………….…………………...…..............…....SET
PRESS SWITCH……………...........….…”PRESS” POSITION
CABIN RATE CONTROLLER .…...........12 O'CLOCK POS
CABIN CONTROLLER..….….…….............….….………..SET
 ACFT 1000 FEET ABOVE CRUISE FLIGHT LEVEL
 MAX 25000 FEET

COMPLETE TOLD CARD

ARRANGE JEPP PLATES FOR BRIEFING

ONCE FO HAS COMPLETED HIS/HER BEFORE START

PROCEDURES
3.3.1 REVIEW SPEEDS AND T/O DATA WITH FO & SET UP
SPEEDS BUGS CHECK SPEEDS
SET UP SPEED BUGS
ST
 1 BUG SET AT V1/VR
 2ND BUG SET AT V2  1ST BUG SET AT V1/VR
 3RD BUG SET AT Vyse (128KTS)  2ND BUG SET AT V2
 400 FT ABOVE A/F ELEV BUGGED ON ALTIMETER  3RD BUG SET AT 128KTS (Vyse)
 400 FT ABOVE A/F ELEV BUGGED ON ALTIMETER
 1900D Chapter 3 Page 27
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 1900D Chapter 3 Page 28
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3.3.2 THREATS, HAZARDS AND BRIEFINGS REVIEW PROCEDURES WITH THE CAPTAIN
a. TOLD CARD
b. START, TAXI & NORMAL DEPARTURE
 No-1/ 2 start first.
 Battery or GPU start.
 Captain to review Start limitations.
 Expected Taxi route INCLUDING HAZARDS/ HOT SPOT
 PF to brief normal departure/ SID.
c. EMERGENCY BRIEFINGS
 PRIOR TO FIRST FLIGHT OF THE DAY OR AFTER A CREW
PARTNER CHANGE, AN EMERGENCY BRIEFING MUST BE
COMPLETED.
 CAPTAIN SHALL IMMIDIATELY TAKE OVER CONTROLS AND
BECOME PF IN CASE OF ANY MALFUNCTION DURING TAKE
OFF.
d. REJECTED T/O (RTO) AND EVACUATION BRIEFING
 IN EVENT OF A DECISION TO STOP BEFORE V1 EITHER ONE
Engine Failure At or Below V1:
OF US WILL CALL STOP.
 I WILL SIMULTANEOUSLY CLOSE BOTH POWER LEVERS TO  Power Levers………..Ground Fine
IDLE, APPLY GROUND FINE/ BRAKING AS REQUIRED AND  Brakes…………….Maximum
BRING THE AIRCRAFT TO A STOP FACING INTO WIND AND (Or as required to achieve stopping distance
SET PARKING BRAKE.
 YOU WILL MONITOR DECELARATION AND ADVISE ATC.
 WE WILL ASSESS THE SITUATION AND IF AN EVACUATION
IS NECCESSARY, I WILL COMPLETE THE SHUT DOWN
MEMORY ITEMS.
 AS THE PROPELLARS STOP I WILL ANNOUNCE EVACUTION
ON PA INDICATING THE SIDE FROM WHERE TO EVACUATE.
ON MY COMMAND YOU WILL GO BACK AND HANDLE THE
PASSENGERS. I WILL NOTIFY ATC, SECURE THE COCKPIT
AND ASSIST YOU WITH EVACUATION.
e. TAKE OFF CONTINUED AFTER V-1
 ABOVE V1, TAKE OFF SHALL BE CONTINUED.ON POSITIVE
CLIMB RATE LANDING GEARS WILL BE RAISED AND V-2
WILL BE MAINTAINED TILL 400 FEET AGL.
 PM WILL ENSURE AFFECTED PROPELLER HAS FEATHERED
UNTIL ACCELERATION ALTITUDE OF 400 FT AGL.
 AT ACCELERATION ALTITUDE SELECT ALT AND HDG.
 AT FLAP RETRACTION SPEED (123 KTS), RETRACT FLAPS
AND SELECT IAS ON MY COMMAND AND CLIMB TO 1500
FT AGL FOR SECURING OF ENGINE.
 GIVE MAYDAY CALL WHEN APPROPRIATE.
f. PILOT FLYING TO BRIEF ONE ENGINE INOPERATIVE
FLIGHT PATH AS APPROPRIATE
g. THREATS (CREW TO REVIEW ALL THE THREATS
INCLUDING):-
 WEATHER
 SNAGS/ MEL
 TERRAIN
 ATC/ AIRSPACE CONGESTION
 NOTAMS
 BIRDS ACTIVITY/ RUNWAY INCURSIONS
 1900D Chapter 3 Page 29
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SEAT AND HARNESS…...SET AND SECURE SEAT AND HARNESS…...SET AND SECURE

REQUEST

COMPLETE CHECKLIST
“PREFLIGHT CHECKLIST”
“PREFLIGHT CHECKLIST COMPLETED”

ENSURE POGO, CHOCKS REMOVED AND DOORS CLOSED

WHILE CAPTAIN PREPARES FLIGHT DECK, THE FIRST OFFICER

WILL GREET PAX AS THEY BOARD THE AIRCRAFT. ONCE
EVERYONE IS ON BOARD, FIRST OFFICER WILL ENSURE THAT
MAIN CABIN DOOR IS CLOSED AND SECURE AND ALL CARRY ON
BAGGAGE IS SAFELY STOWED. FO WILL THEN BRIEF THE
OCCUPANTS IN THE EMERGENCY EXIT ROWS ON THE USE OF
EXITS. CARE SHOUDL BE TAKEN TO ENSURE THAT THESE
PERSONS ARE PHYSICALLY ABLE TO OPERATE THE EXIT (i.e. NO
CHILDREN OR ELDERLY)

WHEN FIRST OFFICER HAS RETURNED TO THE COCKPIT COMPLETE PAX BRIEF

REQUEST FIRST OFFICER TO OBTAIN START CLEARANCE

GND COMM PWR……………………………..….ON

SET FREQUENCY AND REQUEST START CLEARANCE
 1900D Chapter 4 Page 30
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CHAPTER - 4

ENGINE START

Serial Items Pages

4.1 BEFORE START 31
4.2 ENGINE START (BATTERY) 32-36
 1900D Chapter 4 Page 31
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4.1 BEFORE START
CAPT FO
BATTERY……………………………..……..............ON
BEACON ……………...…………….……...............GND
BATTERY VOLTAGE………………...................CHECK
 MINIMUM 23 VOLTS
DOORS .......................................................CLOSED
 DOOR ANNUNCIATORS EXTINGUISHED
FUEL PANEL .…………………..………….CHECK
 QUANTITY ……………CONFIRM
 STBY PUMPS…………OFF
 TXFR FLOW…………..OFF
 AUX PUMPS………….AUTO OR OFF - AS REQUIRED
CIRCUIT BREAKERS ......................CHECKED

REQUEST : CIRCUIT BREAKERS................CHECKED

“BEFORE START CHECKLIST” COMPLETE CHECKLIST AND CALL

“BEFORE START CHECKLIST COMPLETED”

4.2 ENGINE START (BATTERY)

CAPT FO
“ CLEAR RIGHT?”  LOOKOUT AND CHECK RIGHT PROP CLEAR
“CLEAR RIGHT”
“ STARTING RIGHT”
RIGHT IGNITION AND ENGINE START SWITCH……….....ON
 AT FIRST INDICATION OF N1

“N1”
 WITH ROTATION OF RIGHT PROPELLER
 AT FIRST INDICATION OF OIL PRESS ON RIGHT OIL “ROTATION”
PRESSURE GAUGE
“OIL PRESSURE RISING”
 AS RIGHT FUEL PRESS LO ANNUNCIATOR
 AFTER N1 STABLE OR MAX MOTORING. (MIN EXTINGUISHES
12% N1) “FUEL LOW PRESSURE LIGHT OUT”

RIGHT CONDITION LEVER………………….LOW IDLE  AS RIGHT OIL PRESS LO – ANNUNCIATOR

EXTINGUISHES
“FUEL FLOW” “ OIL LOW PRESSURE LIGHT OUT”
 AT FIRST SIGN OF FUEL FLOW  CONFIRM MIN OF 60 PSI ON OIL PRESSURE
 BOTH CREW MEMBERS START MENTAL CLOCK GUAGE
(FOR 10 SEC START LIMIT FOR LIGHT-UP
 BOTH CREW MEMBERS START MENTAL CLOCK
(FOR 10 SEC START LIMIT FOR LIGHT-UP)
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“LIGHT UP” (ITT RISE WITHIN 10 SECONDS)

“ ….. DEGREES”
ITT AND N1…………………….…….......…....MONITOR
 ITT 1000º C MAXIMUM (5 SECONDS)
RIGHT IGNITION AND ENGINE START SWITCH AT 50%
N1……………….…….………………...……....….OFF

ONCE ENGINE IS STABLE

 ITT LESS THAN 750° C
 TQ NOT POWERED (UE92 AND PRIOR)
 PROPS STABLE (LOW PITCH STOP NOT POWERED – RPM
+/- 750)
 CONFIRM LOW IDLE (65% N1)
 FUEL FLOW NORMAL
 OIL PRESS, TEMP IN THE GREEN
RIGHT CONDITION LEVER……………….....HIGH IDLE
 CONFIRM HIGH IDLE (72% N1)
RIGHT GENERATOR……….................GEN RESET THEN ON
 R DC GEN ANNUNCIATOR EXTINGUISHED
 L AND R GEN TIE OPEN ANNUNCIATORS EXTINGUISHED
 CHECK POS LOAD ON R GEN LOADMETER
L & R AC BUS..........................................CHECK
 ANNUNCIATORS................................ILLUMINATED
 L + R AC BUS.......................................ON
 L + R AC BUS ANNUNCIATORS...........EXTINGUISHED
 L INVERTER FREQUENCY...................CHECK (380 – 420
Hz)
 L INVERTER VOLTAGE.......................CHECK (110 – 120
volts)
 SELECT RIGHT HAND INVERTER AND REPEAT ABOVE
STEPS
R AC BUS.................................................OFF, THEN XFR
 ANNUCIATOR ILLUMINATED THEN EXTINGUISHED
 MASTER WARNING ON..............................CANCEL
 FREQ INDICATION RESTORED
R AC BUS.................................................ON
INVERTER INDICATION............................SELECT LEFT
L AC BUS..................................................OFF, THEN XFR
 ANNUCIATOR ILLUMINATED THEN EXTINGUISHED
 MASTER WARNING ON..............................CANCEL
 FREQ INDICATION RESTORED

L AC BUS.....................................................ON
CHARGE BATTERY UNTIL GEN LOAD IS BELOW 50% AND
AMMETER SHOWS A DROP IN CHARGE FROM MAXIMUM
(BATTERY)

 LOOKOUT LEFT AND CHECK LEFT PROP CLEAR

“ CLEAR LEFT”
“ STARTING LEFT”
 1900D Chapter 4 Page 33
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LEFT IGNITION AND ENGINE START SWITCH...........ON

 AT FIRST INDICATION OF N1

“N1”
 WITH ROTATION OF LEFT PROPELLOR
“ ROTATION”  AS LEFT FUEL PRESS LO ANNUNCIATOR
 AT FIRST INDICATION OF OIL PRESS ON RIGHT OIL EXTINGISHES
PRESSURE GAUGE “FUEL LOW PRESSURE LIGHT OUT”
“OIL PRESSURE RISING”  AS LEFT OIL PRESS LO – ANNUNCIATOR
 AFTER N1 STABLE OR MAX MOTORING. (MIN 12% EXTINGUISHES
N1) “ OIL LOW PRESSURE LIGHT OUT”
LEFT CONDITION LEVER……………...…LOW IDLE  CONFIRM MIN OF 60 PSI ON OIL PRESSURE
 AT FIRST INDICATION OF FUEL FLOW GUAGE
“FUEL FLOW”  BOTH CREW MEMBERS START MENTAL CLOCK
 BOTH CREW MEMBERS START MENTAL CLOCK (FOR 10 SEC START LIMIT FOR LIGHT-UP)
(FOR 10 SEC START LIMIT FOR LIGHT-UP)  AT PEAK/MAX ITT DURING START – AND NOTE
“LIGHT UP” (ITT RISE WITHIN 10 SECONDS) FOR TECH LOG
ITT AND N1 ……………….…………….…..MONITOR
 ITT 1000º C MAXIMUM (5 SECONDS)
LEFT IGNITION AND START SWITCH AT 50% N1.....OFF “ ….. DEGREES”

ONCE ENGINE IS STABLE

 ITT LESS THAN 750° C
 TQ NOT POWERED
 PROPS STABLE (LOW PITCH STOP NOT POWERED
– RPM +/- 750)
 N1 LOW IDLE (65%)
 FUEL FLOW NORMAL
 OIL PRESS, TEMP IN THE GREEN
LEFT & RIGHT CONDITION LEVER………...…LOW IDLE/ 65%

LEFT GENERATOR….…….......GEN RESET THEN ON

 L DC GEN ANNUNCIATOR EXTINGUISHED
 LOAD INDICATED ON L DC GEN LOAD METER
 L & R GEN TIE ANNUNCAITORS EXTINGUISHED

RIGHT GENERATOR..…………………………….OFF
 R DC GEN ANNUNCIATOR ILLUMINATED
 MASTER CAUTION ILLUMINATED
VOLTAGES CHECK
 BATT,L+R GEN,CTR BUS….......................27.5-29V
 TPL BUS……………………….......................…26.5-28V
 EXT PWR…….........................………………..0 VOLTS
 1900D Chapter 4 Page 34
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RIGHT GENERATOR............................GEN RESET THEN ON

 R DC GEN ANNUNCIATOR EXTINGUISHED
 CHECK POS LOAD ON R GEN LOADMETER
GEN TIES SWITCH……..……….……………OPEN
 L AND R GEN TIE OPEN ANNUNCIATORS
ILLUMINATED
 MASTER CAUTION ILLUMINATED
 LOAD METERS POSITIVE LOAD INDICATION
 L & R GEN VOLTAGES ........................27.5-29 V
 TPL BUS VOLTAGE..…………….……….…..26.5-28V
GEN TIES SWITCH……….……….……………NORMAL
 L & R GEN TIE OPEN ANNUNCIATORS
EXTINGUISHED
CENTRE BUS...…..………………....…….…...SELECT
BUS SENSE SWITCH...……..………………...TEST
 L AND R GEN TIE OPEN AND BATT TIE OPEN
ANNUNCIATORS ILLUMINATED
 MASTER CAUTION ILLUMINATED
 CTR BUS VOLTAGE..……….…………………ZERO V
BUS SENSE RESET SWITCH………..….…..RESET
 L AND R GEN TIE OPEN AND BATT TIE OPEN
ANNUNCIATORS EXTINGUISHED
 CTR BUS VOLTAGE………..…………….RESTORED
LOADMETERS…….…...PARALLELED WITHIN 10%

THESE ACTIONS COMPLETE THE ENGINE START

PROCEDURE – THE CAPT INDICATES THAT THE FO MAY
COMMENCE HIS/HER AFTER START FLOWS BY SELECTING
THE AVIONICS MASTER “ON”

AVIONICS MASTER………………………….....……ON 4 EFIS POWER SWITCHES....................ON

FUEL PANEL CBS…………....………………..........CHECK
AUTOFEATHER…………..……….……………........ARM ENVIRONMENTAL “T”...……FIRST FLT OF THE DAY
EFIS AUX PWR............................................ON  SELECT THE BOTH BLEED AIR SWITCH TO ENVIR
GPWS.........................................................TEST ON
 GPWS LIGHT ILLUMINATED  ROTATE MODE CONTROL to “T” POSITION
 AUDION WARNINGS CHECK  L&R ENVIR FAIL ANNUNCIATOR ILLUMINATE
FDR.................................................WARNING LIGHT EXT  ROTATE MODE CONTRL TO “AUTO”
ICE PROTECTION……..……...…................AS REQUIRED  SELECT THE BOTH BLEED AIR SWITCH TO ENVIR
 CONSIDER SYSTEM PROTECTION REQUIREMENTS OFF
WITH RESPECT TO AMBIENT CONDITIONS  L&R ENVIR FAIL ANNUNCIATOR EXTINGUISHED
ELEVATOR TRIM ..................................SET FOR TAKE OFF
 SET IN FWD RANGE FOR C.G’s IN FORWARD HALF
OF ENVELOPE AND IN AFT RANGE FOR C.G’s IN
AFT HALF OF ENVELOPE. (TAKE-OFF CONDITIONS)
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STANDARD OPERATING Issue Date 31 Aug 2015
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PROPELLERS.....................................CONFIRM TAXI PNEUMATICS AND SUCTION…............TEST/CHECK

FLAPS……………………..……..................SET AS REQUIRED  SELECT THE LEFT BLEED AIR SWITCH TO ENVIR OFF
BOTH EFIS DSP’s...............................SET FOR DEPARTURE  CHECK LEFT “ENVIR OFF” ANNUNCIATOR
 ACTIVE AND PRESELECT COURSES..................SET ILLUMINATED
 ONSIDE DATA (i.e. LEFT feeds LEFT)...............SET  SELECT LEFT BLEED AIR SWITCH TO “INST + ENVIR
 HDG BUGS..............................................RWY HDG OFF”
 CHECK SUCTION IN WIDE GREEN ARC AND PNEU.
 HSI POINTERS......................................SET AS REQ.
PRESS 17.5-19.0 PSI
 RADIO ALTIMETERS.....................................ZERO  SELECT THE RIGHT BLEED AIR SWITCH TO ENVIR OFF
RADAR....................................................TEST/STANDBY  CHECK RIGHT “ENVIR OFF” ANNUNCIATOR
PASSENGER BRIEFING………………...……...SEND ILLUMINATED
 CHECH NEEDLE IN GREEN BAND  SELECT RIGHT BLEED AIR SWITCH TO “INST + ENVIR
PASSENGER BRIEFING……............…………SEND OFF”
WAIT FOR CO-PILOT TO SELECT THE FLIGHT DIRECTOR  SUCT + PNEU WILL INDICATE ZERO
TO G/A AND THEN:  L + R “BL AIR FAIL” ANNUNCIATORS ILLUMINATED
REQUEST FLIGHT CONTROL CHECK  MASTER WARNING ANNUNCIATORS ILLUMINATED
AP CHECKS IF INSTALLED  SELECT THE LEFT BLEED AIR SWITCH TO “OPEN”
ELECTRIC TRIMS…..………............….CHECK AND SET  CHECK SUCTION IN WIDE GREEN ARC AND PNEU
 ELEV TRIM SWITCH……………..……………............ON PRESS 17.5-19.0 PSI
 PILOT’S AND COPILOT’S TRIM SWITCHES...CHECK  SELECT THE RIGHT BLEED AIR SWITCH TO “OPEN”
 PILOT’S TRIM WILL OVERRIDE COPILOT’S TRIM BLEED AIR VALVES……..…………..............AS REQUIRED
 MOVEMENT OF ONLY HALF OF SWITCH WILL NOT BLOWERS………….……………………...……...AUTO
ACTIVATE TRIM ENVIR MODE CONTROL…….………….…..AUTO
 TRIM DISCONNECT SWITCH ……PRESS TO 2ND CBs...………………………………………..….......CHECK
LEVEL AND RELEASE STANDBY HORIZON POWER.................ON/UNCAGE
 PITCH TRIM OFFANNUNCIATOR…....ILLUMINATED AVIONICS PANEL.…………………...............SET
 ELECTRIC PITCH TRIM ………............DEACTIVATED  COMM FREQ. AS BRIEFED...........SET
 ELEV TRIM SWITCH ……….…….........OFF, THEN ON  NAV FREQ AS BRIEFED................SET
 PITCH TRIM OFF ANNUNCIATOR ………...........OFF  STANDBY HORIZON.....................UNCAGED
 ALTITUDE PRESELECT...................SET
ELEVATOR TRIM…….….......….…......SET FOR TAKE-OFF  ADF..............................................SET
YAW DAMPER……………….….…………CHECK  TRANSPONDER............................SET
 YAW DAMPER SWITCH…………………………..ON  TCAS.............................................SET
 YD ANNUNCIATOR……………….…….ILLUMINATED  GPS...............................................SET
 RUDDER PEDALS…CHECK FOR ADDED FD MODE…………………….......SELECT GO AROUND
RESISTANCE WAIT FOR CAPTAIN AND THEN:
 CONTROL WHEEL DISCONNECT FLIGHT CONTROLS..........................CHECK
SWITCH……………………………..............…PRESS TO  CHECK FOR FREEDOM OF MOVEMENT AND
FIRST LEVEL (YAW DAMPER WILL DISENGAGE) CORRECT DIRECTION OF TRAVEL
 YAW DAMP …………………………..……………….ON ELECTRIC TRIMS ……………………………CHECK
 RUDDER BOOST/YAW CONTROL TEST  MOVE TRIM SWITCH AS DIRECTED
SWITCH……………………………...YAW CONTROL TEST ELEVATOR TRIM….….......….…......SET FOR TAKE-OFF
(YAW DAMP WILL DISENGAGE, RUD BOOST OFF YAW DAMPER…...………………………….…CHECK
ANNUNCIATOR – ILLUMINATED)
 RUDDER BOOST/YAW CONTROL TEST
SWITCH……………………………….......RUDDER BOOST
(RUD BOOST OFF ANNUNCIATOR –EXTINGUISHED
 1900D Chapter 4 Page 36
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EFIS COMPARATOR.................................CHECK EFIS COMPARATOR.................................CHECK

 CAPT MOMENTARILY DEPRESSES PLT TEST
 10* PITCH UP AND 10* RIGHT ROLL ON CAPT
EADI
 20* HDG INCREASE ON CAPT EADI
 RED TEST FLAG IN UPPER CORNER OF EADI
 CAPT PRESS “COMPARATOR PUSH TO RESET”
 CAPT MOMENTTARILY DEPRESS CO-PILOT TEST
 10* PITCH DOWN AND 10* LEFT ROLL ON CO-PLT
EADI
 20* HDG DECREASE ON CO-PLT EHSI
 RED TEST FLAG IN UPPER CORNER OF EADI
 CO-PLT PRESS “COMPARATOR PUSH TO RESET”

PERFORM PANEL SCAN

“ CLOCK INDICATES …, ASI ZERO, BARBERS POLE INDICATING THE FIRST OFFICER FOLLOWS THE CAPTAIN
…, EADI NO FLAGS WINGS LEVEL NOSE ON THE HORIZON, THROUGH ON HIS/HER INSTRUMENTS DURING
BALL IN THE CENTRE, ALTIMETER (10..) INDICATING … FT, THE PANEL SCAN AND CALLS OUT ANY
COMPASS MODE SLAVED, COMPASS HEADINGS … RMI, … DEVIATIONS.
EHSI NO FLAGS, HEADING BUG …, CRS …, VSI …, ENGINE
INSTRUMENTS NORMAL, COM 1 …, COM 2 …, NAV 1 …, NAV 2
…, ALT SEL SET TO …, ADF …, TRANSPONDER … SET STANDBY,
GPS SET.”

PERFORM MANUAL FEATHERING (EVERY FLIGHT) MANUAL FEATHER CHECK

 MOVE THE PROPELLER LEVERS TO FEATHER  NOTE TORQUE
POSITION  MOVE PROP LEVERS TO FEATHER
 NOTE TORQUE INCREASE AND PROP RPM
DECREASE TO APPROX 400 RPM
 CHECK RETURN TO ORIGINAL VALUES WHEN
UNFEATHERING

REQUEST:
“BEFORE TAXI CHECKLIST”
COMPLETE THE AFTER START CHECKLIST AND CALL
“BEFORE TAXI CHECKLIST COMPLETED”
 1900D Chapter 4 Page 37
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 1900D Chapter 5 Page 38
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CHAPTER - 5

TAXI

Serial Items Pages

5.1 TAXI 39
5.2 POWER BACK 39
5.3 EXTERIOR LIGHTS 39
5.4 BRAKES CHECK 39
5.5 TAXI SPEED 39
5.6 WEATHER RADAR 39
5.7 INSTRUMENT AND REVERSE THRUST 39
CHECK
5.8 ATC CLEARANCE 39
5.9 TAXI PROCEDURE 40
5.9.1 SYSTEM CHECKS 40
 1900D Chapter 5 Page 39
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5.1 TAXI
On completion of start up, Capt shall ensure removal of all ground connections and request
hand signal on appropriate side. First officer shall request taxi clearance from ATC. After
receiving signal from ground crew and taxi clearance from ATC, both pilots shall check respective
sides and announced “LEFT/RIGHT CLEAR”.

5.2 POWER BACK

Power back using reverse power should be avoided. If required it shall be carried out at slow
speed using the following precautionary measures:-
 ATC clearance obtained, specifically requesting power back.
 Ground staff briefed to check area clear before and during power back,
communication with cockpit through use of thumbs up to signal area clear and
thumbs down to signal an obstruction or any reason to stop the aircraft.
 Slight reverse power application, just before releasing the park brake to avoid
forward movement.
 Capt & First officer to keep their feet off the brake pedals and on the floor.
 Never use the brakes during power back to avoid possible tail strike.
 Use ground idle or positive power to decrease speed or stop.

5.3 EXTERIOR LIGHTS

Capt shall select TAXI light ON before taxi and announce “OFF BLOCK TIME ____”. First officer
shall record the time.

5.4 BRAKES CHECK

As soon as aircraft rolls check brakes as per procedure given in FCOM.

5.5 TAXI SPEED

 Straight taxi way 25Kts.
 Turn at or below 15 Kts.
 Sharp turn at or below 10Kts.

5.6 WEATHER RADAR

During taxi when clear of congested area, weather radar shall be selected to “WX” from “STBY”
to scan for weather.

5.7 INSTRUMENT AND REVERSE THRUST CHECK

Capt and First officer shall scan their instrument to check for any failure or flags.
PF will check the reverse thrust.

5.8 ATC CLEARANCE

First officer shall receive the ATC clearance, record it on the flight plan. Capt shall also cross
check the ATC clearance for conformity with the filed flight plan, ensuring that GPS (RWY/SID),
Altitude/FL and transponder are set accordingly.
 1900D Chapter 5 Page 40
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5.9 TAXI PROCEDURE
PF PM

REQUEST PILOT MONITORING TO OBTAIN TAXI OBTAIN TAXI CLEARANCE

CLEARANCE ONCE OBTAINED…………………...TAXI LIGHT ON

CLEAR AREA, TAXI OUT AND CHECK BRAKES

INSTRUMENT CHECKS INSTRUMENT CHECKS

 PERFORM A NORMAL INSTRUMENT TEST  FOLLOW PF THROUGH DURING TEST
DURING TAXI TURNS

PF TO CHECK REVERSE THRUST DURING TAXI WHEN CLEAR CHECK THAT SQUAWK AND NEXT REQUIRED
OF CONGESTED AREA ATC FREQUENCY IS ON STANDBY.

5.9.1 SYSTEM CHECKS

System checks are performed at the Holding point before line up as under:-

CAPT FO
AUTO FEATHER.……..............…..EVERY FLIGHT ENVIRONMENTAL “T”...……FIRST FLT OF THE DAY
RUDDER BOOST…….……………….FIRST FLIGHT OF DAY
OVERSPEED GOV….……….……….FIRST FLIGHT OF DAY
PRIMARY GOV………………………..FIRST FLIGHT OF DAY
LOW PITCH STOP………………...…FIRST FLIGHT OF DAY
 1900D Chapter 6 Page 41
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CHAPTER-6

BEFORE TAKE OFF

Serial Item Pages

6.1 PRIOR TO RUNWAY ENTRY 42-44
6.2 CLEARED TO ENTER THE RUNWAY 45
6.3 TAKE OFF CLEARANCE OBTAINED 45
 1900D Chapter 6 Page 42
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6.1 PRIOR TO RUNWAY ENTRY

After the system checks the crew should anticipate the timing of expected runway entry
clearance so as to have the following items completed prior to being cleared to enter the
runway without having the strobes and Ice Protection ON for an extended period of time.

CAPT FO
DUE TO THE POSITION OF FOLLOWING DUE TO THE POSITION OF THE FOLLOWING
SWITCHES ON PILOTS SUB PANEL, CAPT SWITCHES ON THE CO-PILOTS SUB PANEL, THE
WILL MAKE THE FOLLOWING SELECTIONS. F/O WILL MAKE THE FOLLOWING SELECTIONS.

ENGINE ANTI ICE …….…………..AS REQUIRED BLEEDS…………………………………........AS REQUIRED

WINDSHIELD HEATS….….………………………ON ENVIR MODE CONTROL………………. AS REQUIRED
 NORMAL  BLEEDS SET “ENVIRO OFF” AND ENVIRO MODE
CONTROL MUST BE “OFF”FOR MAX POWER TAKE
ICE PROTECTION…………….……………………ON OFF
 L FUEL VENT
 R FUEL VENT
 STALL WARNING
 L PITOT
 R PITOT
 ALT STATIC

ANNUNCIATORS……EXTINGUISHED/CONSIDERED
TAKE OFF WITH THE BATTERY CHARGE ANNUNCIATOR
ILLUMINATED IS PERMITTED IF A DECREASING BATTERY
CHARGE IS CONFIRMED

PROPS….........……………CONFIRM FULL FORWARD RADAR…...……………………………….…....WX

FLAPS...........................CONFIRM SET TRANSPONDER…..….…………………..…ALT
TRIMMERS..................CONFIRM SET
REQUEST:

“BEFORE TAKE OFF CHECKLIST TO THE LINE”

COMPLETE CHECKLIST TO THE LINE AND CALL

“BEFORE TAKE-OFF CHECKLIST COMPLETED TO THE

LINE”

OBTAIN TAKE OFF/ LINE UP CLEARANCE

 1900D Chapter 6 Page 43
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PRIOR TO RUNWAY ENTRY FLOWS

1900D Chapter 6 Page 44

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 1900D Chapter 6 Page 45
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6.2 CLEARED TO ENTER THE RUNWAY

PF PM
APPROACH.................................CONFIRM CLEAR APPROACH.................................CONFIRM CLEAR

STROBES.....................................ON

BEACON......................................FLT

6.3 TAKE-OFF CLEARANCE OBTAINED

CAPT PM
AUTO IGNITION.................................ARMED LANDING LIGHTS………………..……………….…ON

REQUEST :
COMPLETE CHECKLIST BELOW THE LINE AND CALL
“ BEFORE TAKE OFF CHECKLIST BELOW THE LINE”
“BEFORE TAKE-OFF CHECKLIST COMPLETED"

CONFIRM TAKE OFF CLEARANCE CONFIRM TAKE OFF CLEARANCE

ANNOUNCE WIND
 1900D Chapter 7 Page 46
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CHAPTER - 7

TAKE OFF AND DEPARTURE

Serial Items Pages

7.1 TAKE OFF 47-49
7.2 AT TRANSITION ALTITUDE 50
7.3 AT FL 100 50
7.4 CLIMB 50
7.5 AT TOP OF CLIMB 50
 1900D Chapter 7 Page 47
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7.1 TAKE OFF

PF PM
POWER LEVERS…………………………..ADVANCE  WHEN “AFX” ANNUNCIATORS ILLUMINATE
 RELEASE BRAKES ONCE PROPS ARE GOVERNING AT A “AUTO-FEATHER ARMED”
MIN OF 2000LBS TORQUE AND PM HAS CALLED
"AUTO FEATHER ARMED"
“SET MAX POWER” or “SET REDUCED POWER” POWER LEVERS………………….SET
 WHEN POWER IS SET
“MAX POWER SET” or “REDUCED POWER SET"
 MONITOR ASI, ON ACCLERATING THROUGH 80 KTS
“80 KNOTS ENGINE INSTUMENTS OK”
“CHECK”
 AT V1/V ROTATE
“V1/ROTATE”

 REMOVE HAND FROM POWER LEVERS  WITH POSITIVE CLIMB INDICATED ON THE PRESSURE
 ROTATE AT 3° / SEC INTO FLIGHT DIRECTOR BARS ALTIMETER AND VSI OR VISUAL CONFIRMATION
THAT THE AIRCRAFT HAS LEFT THE GROUND.
“POSITIVE CLIMB”
“GEAR UP”
 GEAR SELECTOR UP
 WHEN GEAR LIGHTS ARE OUT

“GEAR UP, NO LIGHTS”

 SWITCH TAXI LIGHT OFF
 PASSING 400 AGL AND 123KTS

“FLAPS UP” “FLAPS UP?”

(CONFIRMING UNDERSTANDING OF INSTRUCTION)

FLAP SELECTOR…………………………SELECT UP

 WHEN FLAPS INDICATING UP ON GAUGE

”
FLAPS UP INDICATED”

 ONCE FLAPS CONFIRMED UP

“ENGAGE YAW DAMPER ” YAW DAMPER………………………………...ENGAGE

 ONCE YAW DAMPER IS ENGAGED

“ YAW DAMPER ENGAGED”
BLEEDS……………………………………………..ON

ENVIR MODE CONTROL………………………AUTO

“HEADING MODE”
SELECT HEADING ON FCP
 1900D Chapter 7 Page 48
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“CHECKS” ONCE SELECTED AND HDG DISPLAYED IN GREEN ON EFIS

“HEADING GREEN”
“INDICATED AIR SPEED MODE”

SELECT IAS ON FCP

 ONCE SELECTED AND IAS DISPLAYED IN GREEN
ON EFIS
“INDICATED AIR SPEED GREEN”
“CHECKS”

 PASSING 1500’ AGL

“ SET CLIMB POWER”

POWER/ PROP LEVERS……….SET CLIMB POWER

REQUEST  DECREASE TORQUE TO 3300FT/LBS, SET PROPS
TO 1550 RPM, RESET MAXIMUM 3500FT/LBS (ITT
LIMIT 760 DEG)

“AFTER TAKE-OFF CHECKLIST TO THE LINE” “ CLIMB POWER SET”

COMPLETE CHECKLIST TO THE LINE AND CALL

“AFTER TAKE-OFF CHECKLIST COMPLETED TO THE LINE”

 1900D Chapter 7 Page 49
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TAKE OFF PROFILE

 1900D Chapter 7 Page 50
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7.2 AT TRANSITION ALTITUDE

PF PM
“ TRANSITION ALTITUDE”
ALTIMETER…………………..…….....SET STANDARD
ALTIMETER………………….………SET STANDARD
“ 1013, INDICATING …. FT … NOW”
“ CHECK” PRESSURISATION…………..…………….……CHECK
 CONFIRM DIFF INCREASING
 CABIN ROC +/- 500FT/MIN

REQUEST
COMPLETE CHECKLIST AND CALL
"AFTER TAKE OFF CHECKLIST BELOW THE LINE “AFTER TAKE-OFF CHECKLIST COMPLETED

7.3 AT FL100
PF PM
“ FLIGHT LEVEL 100” “CHECK”
LANDING LIGHTS………...…….………...…….OFF
PRESSURIZATION...................................CHECK

7.4 CLIMB
PF PM
“1000 TO LEVEL OFF” “CHECK”

7.5 AT TOP OF CLIMB

PF PM
 WHEN A/C HAS ACCELERATED TO CRUISE SPEED
“ SET CRUISE POWER”  CHECK CRUISE POWER SETTING IN QRH

POWER/ PROP LEVERS………SET CRUISE POWER

 ONCE CRUISE POWER IS SET

“ CRUISE POWER SET”

TCAS...................................................NORMAL
AUTOFEATHER…………………………………......OFF
FUEL…………………………………………….........…CHECK

 QUANTITY
 BALANCE
 1900D Chapter 8 Page 51
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CHAPTER - 8

CRUISE

Serial Items Pages

8.1 TOP OF CLIMB 52
8.2 CRUISE 52
8.3 TURBULANCE 52
8.4 NAV AIDS / FLIGHT PLAN 52
8.5 WEATHER RADAR 52
8.6 ENROUTE WEATHER 52
 1900D Chapter 8 Page 52
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8.1 TOP OF CLIMB

Level off shall be verified by FMA annunciators and PF shall announce ''ALT'' and then
''ALT GREEN''.At cruise flight level the PF shall announce '' Compute Cruise Parameters''.
The PM shall check OAT and compute cruise parameters from the performance graph.
Reaching cruise speed the PF shall select Power to calculated cruise Torque. After three
minutes with cruise torque set PM to note down the engine parameters in tech log on
first flight of the day.

8.2 CRUISE
Once stabilized in cruise, the PM will maintain the flight plan and fuel score on the flight
plan as per OM Chapter A8 Page 84.

8.3 TURBULENCE
In turbulent condition, speed shall be progressively reduced till a comfortable cruise
speed is attained. In moderate to severe turbulence, maximum 170 Kts shall be
maintained with seat belts sign switched ‘‘ON’’ and both PF and PM wearing shoulder
harnesses.

8.4 NAV AID/ FLIGHT PLAN

Nav aids such as VOR and NDB shall be tuned and identified by PM. PM shall also monitor
the flight on Jeppesen map and update the flight plan.

8.5 WEATHER RADAR

Weather radar tilt shall be adjusted as per weather radar manual for accurate weather
depiction on its display.

8.6 ENROUTE WEATHER

PM shall continue updating enroute airfields weather for in flight contingencies/
emergencies.
 1900D Chapter 9 Page 53
STANDARD OPERATING Issue Date 31 Aug 2015
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CHAPTER - 9

DESCENT & LANDING

Serial Items Pages

9.1 BEFORE TOP OF DESCENT 54
9.2 DESCENT 55
9.3 APPROACHING FL 100 55
9.4 AT TRANSITION LEVEL 55
9.5 BEFORE LANDING 56
9.6 AFTER LANDING 57-59
9.7 CLEAR OF THE ACTIVE RUNWAY 57
9.8 STATIONARY AT PARKING BAY 60
9.9 SHUTDOWN 60-61
 1900D Chapter 9 Page 54
STANDARD OPERATING Issue Date 31 Aug 2015
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9.1 BEFORE TOP OF DESCENT

CAPT FO
AUTOFEATHER…………………………………….ON
FUEL……………………………………………..CHECK
 QUANTITY
 BALANCE

PF PM
BRIEF ON THE DESCENT, APPROACH AND LANDING GET ATIS
COMPLETE LANDING CARD
SET UP COCKPIT FOR THE APPROACH (SPEED BUGS, ALTIMETER BUG………….……..SET DA/MDA/CIRCUIT ALT
MINIMUMS, NAV AIDS/ FREQS, COURSES)

REVIEW ANY THREATS (HIGH FEATURES, COMPANY

MINIMUMS VS VIS AND WX CONDITIONS, ALTERNATE TCAS.............................................SET “BELOW”
AIRFIELD)
PRESSURISATION ……....……….......SET AND CHECK

COMPLETE CHECKLIST TO THE LINE AND CALL

REQUEST :
“DESCENT AND APPROACH CHECKLIST COMPLETED
“DESCENT AND APPROACH CHECKLIST TO THE LINE” TO THE LINE”

TAKE DESCENT CLEARANCE

9.2 DESCENT

PF PM
 ONCE DESCENT IS COMMENCED AND IT IS
NOTED THAT CABIN IS DESCENDING OR
ALTERNATELY ON THE ‘GROUND’

“ CABIN IS DESCENDING”

OR

“ CABIN IS ON THE GROUND”

PASSENGER BRIEFING…...……......SEND/COMPLETE
BELOW 5000 FEET
 1900D Chapter 9 Page 55
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9.3 APPROACHING FL100

PF PM
“ FL 100” “CHECKS”
LANDING LIGHTS……………………..………… ON

CABIN PRESSURE …….……………….……CHECK

 COMPARE CABIN ALTITUDE TO A/C AND ENSURE
THAT A/C DOES NOT REACH CABIN ALTITUDE BY
ADJUSTING RATE CONTROLLER APPROPRIATELY

9.4 AT TRANSITION LEVEL

PF PM
“ TRANSITION LEVEL”

ALTIMETER …………………...........................SET QNH ALTIMETER ……………………..………...SET QNH

“ 10.., INDICATING ….FT … NOW”
“ CHECKS” OR “… FT HIGH/LOW"

REQUEST

“DESCENT AND APPROACH CHECKLIST BELOW THE

LINE”
COMPLETE CHECKLIST BELOW THE LINE AND CALL

“DESCENT AND APPROACH CHECKLIST COMPLETED”

 1900D Chapter 9 Page 56
STANDARD OPERATING Issue Date 31 Aug 2015
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9.5 BEFORE LANDING

PF PM
WHEN APPROPRIATE
 IAS BELOW 188 KTS
“FLAP 17” “FLAP 17?”
FLAP SELECTOR…………………SET TAKE OFF FLAP

 ONCE TAKE OFF FLAP INDICATED

 IAS BELOW 180 KTS “FLAP 17 INDICATED”
“GEAR DOWN”
“GEAR DOWN?”
GEAR SELECTOR………………………SELECT DOWN
GEAR SELECTED DOWN WITH 3 GREENS INDICATED
 ONCE GEAR CONFIRMED DOWN “GEAR DOWN, 3 GREENS”

“PROPS FULL FORWARD” “PROPS FULL FORWARD?”

PROPELLOR LEVERS………………FULL FORWARD

“PROPS SET FULL FORWARD”

"FLAPS 35” “FLAPS 35?”

 ONCE FLAP LANDING INDICATED

 BEFORE 1000’ ABOVE AIRFIELD ELEVATION, “FLAPS 35 INDICATED”

ENSURE FULLY CONFIGURED IN IMC

YAW DAMPER……………………………DISCONNECT
 DURING AUTO PILOT COUPLED APPROACH, YAW
DAMPER SHOULD NOT BE DICONNECTED UNTIL COMPLETE CHECKLIST AND CALL
THE AUTO PILOT IS DISENGAGED

REQUEST
“LANDING CHECKLIST” “ LANDING CHECKLIST COMPLETED”

 CONFIRM LANDING CLEARANCE

 TAXI LIGHT ………………….ON
 ANNOUNCE WIND
 CONFIRM LANDING CLEARANCE  IN VMC 500FT ABOVE AIRFIELD ELEVATION AND
AIRCRAFT IS ‘STABILISED’ ON FINAL APPROACH.
IN IMC REFER TO MONITORED APPROACH
“ 500 FEET STABLE ”
“ CHECK CONTINUEING”
 1900D Chapter 9 Page 57
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9.6 AFTER LANDING

PF PM
 AT 40KTS DURING THE LANDING ROLL
“CHECK”
 ENSURE POWER LEVERS OUT OF REVERSE “40 KNOTS”

9.7 ONCE CLEAR OF THE ACTIVE RUNWAY

CAPT PM
AUTO IGNITION…......…………………..…………..OFF
ENGINE ANTI ICE…....……………………………....ON STROBES, BEACON AND RECOG LIGHTS………AS REQ
AUTOFEATHER……....…………….………………...OFF TRANSPONDER……….…….….…….........STANDBY/2000
ICE PROTECTION…......................................AS REQ RADAR……………………………...…………...STBY/OFF
PROPELLER LEVERS.....................................TAXI TRIMS……………………………….……….…...SET

 ELEVATOR 1½ UNITS NOSE UP

RUDDER AND AILERON TRIM NEUTRAL

REQUEST FLAPS ………..……………………………………..….UP

“AFTER LANDING CHECKLIST”

COMPLETE CHECKLIST HALF-VOICE AND CALL

“AFTER LANDING CHECKLIST COMPLETED
 1900D Chapter 9 Page 58
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AFTER LANDING FLOWS

 1900D Chapter 9 Page 59
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 1900D Chapter 9 Page 60
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9.8 STATIONARY AT PARKING BAY

PF PM
PARK BRAKE ……..…………………………………. SET
TAXI LIGHT …………………………………………..OFF
 ONCE SET THE CAPT AND FO COMMENCE THEIR
RESPECTIVE SHUTDOWN FLOWS
 ON ENTRY TO PARKING BAY

9.9 SHUT DOWN

CAPT FO
EFIS AUX POWER……………...…….…….....OFF STANDBY HORIZON....................... CAGED & PWR OFF
AC BUSSES………………………………………...OFF BLOWERS……………………............….……………....AUTO
AVIONICS MASTER……………...…….……..OFF ENVIRONMENTAL MODE CONTROL …..………OFF

OXYGEN…………………………………………….OFF EFIS POWER SWITCHES..................................OFF

EMERGENCY LIGHTS…….......………………AS REQ
BATTERY CONDITION……..…............…..CHECK (23V MIN)

WAIT FOR THE FIRST OFFICER TO CALL

“CLEAR TO CUT” ONCE COMPLETED CALL
“CLEAR TO CUT”
ITT……………………………………………...........STABILISED
CONDITION LEVERS…...………….……...…..CUT-OFF
PROP LEVERS (BELOW 500 RPM)…............…FEATHER
WAIT FOR PROPELLERS TO STOP TURNING
GANG BAR .....................…….…..………….OFF
BEACON LIGHT……………………………….…..OFF
REQUEST

“SHUTDOWN CHECKLIST” ( AT NIGHT TO THE LINE)

COMPLETE THE SHUTDOWN CHECKLIST (TO THE
LINE AT NIGHT)

IT IS THE CAPTAINS’ DUTY TO ENSURE THAT ALL LIGHTS ARE “SHUTDOWN CHECKLIST TO THE LINE COMPLETE”
SWITCHED OFF INCLUDING THOSE LIGHTS ON THE HOT OR
BATTERY BUS ONCE NO LONGER REQUIRED (CABIN – “SHUTDOWN CHECKLIST COMPLETE”
PARTIAL, EMERGENCY INSTR. LIGHTS, CABIN DOOR AND
CARGO BAY LIGHTS). DURING NIGHT OPERATIONS THE SHUT THE FIRST OFFICER IS TO SECURE THE AIRCRAFT BY
DOWN CHECKLIST WILL BE DONE TO THE LINE. IT IS THE INSTALLING POGO STICK, COVERS, CLOSING THE DOORS
CAPTAINS RESPONSIBILITY TO COMPLETE THE CHECKLIST AND SECURING THE EMERGENCY EXITS.
BELOW THE LINE ONCE SECURING THE COCKPIT AND
INSTALLING CONTROL LOCKS.
 1900D Chapter 9 Page 61
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 1900D Chapter 10 Page 62
STANDARD OPERATING Issue Date 31 Aug 2015
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CHAPTER - 10

APPROACHES

Serial Items Pages

10.1 PRECISION APPROACH CALL OUTS 63-65
10.2 NON-PRECISION APPROACH CALL OUTS 66-68
 1900D Chapter 10 Page 63
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10.1 PRECISION APPROACH CALL OUTS
NOTE 1: The following procedure assumes:-
 The aircraft is hand flown by the PF(if the autopilot is used, the PF may make
the runway heading and missed approach altitude selections).
 The crews have been cleared for the approach.
 ILS has been selected and identified on NAV1 and NAV2.
 The aircraft heading is within 90 degrees of the inbound course.
NOTE 2: All precision approaches with cloud base below 500ft and less than 2000m
visibility should be flown monitored. For monitored approach Captain should be PM and
First Officer PF
PF(FO) PM(CAPT) Remarks
“ARM APPR MODE”  SELECT APPR ON FCP
SELECT APPR ON FCP  VERIFY (LOC) ARMED
VERIFY (LOC) ARMED “APPR MODE ARMED”
 WITH LOCALISER MOVEMENT
“LOCALISER ALIVE”

“CHECKS”  AT LOCALISER INTERCEPT

 VERFIFY (LOC) GREEN AND (GS)
ARMED
 CHECK (LOC) GREEN AND (GS) “LOCALISER GREEN, G/S ARMED” 1.5 DOT ABOVE GS SET
ARMED FLAPS 17⁰
“SET RUNWAY HEADING “  SET BOTH HDG BUGS TO RUNWAY
HEADING
“RUNWAY HEADING SET”
 WITH GLIDESLOPE MOVEMENT
“G/S ALIVE”

“CHECKS”

 AT HALF DOT FLY UP “GEAR DOWN?”

“GEAR DOWN AND PROP MAX” GEAR SELECTOR…………SELECT DOWN
 GEAR SELECTED DOWN WITH 3
GREENS INDICATED
 PROP MAX
“GEAR DOWN, 3 GREEN AND PROP MAX”

 AT G/S INTERCEPT, VERIFY (GS)

GREEN
 VERIFY (GS) GREEN “G/S GREEN”
“SET MISSED APPROACH ALTITUDE”  SET MISSED APPROACH ALTITUDE
ON ALLTITUDE SELECTOR.
“MISSED APPROACH ALTITUDE SET”

“FLAPS 35”
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YAD DAMPER…………………………DISCONNECT FLAPS 35 INDICATED”

 IF USING AUTOPILOT FOR
APPROACH, THEN YD TO BE
DISENGAGED WITH A/P BY 200
FT AGL
 AP DISCONNECT
SWITCH……..PUSH TO 1ST LEVEL
REQUEST “COMPLETE CHECKLIST AND CALL
”BEFORE LANDING CHCKILIST” “LANDING CHECKLIST COMPLETE”

 AT OUTER MARKER OR DME

CHECK HEIGHT
“OM______FT/______DME,________FT,
INSTRUMENTS AND ALTIMETERS SET
AND CROSS-CHECKED”
“CHECKS”
 AT 1000FT ABOVE MINIMUMS
AND AIRCRAFT IS STABILISED ON
FINAL APPROACH
“CHECKS” “1000 FEET, STABLE”
 AT 500FT ABOVE MINIMUMS AND
AIRCRAFT IS STABILISED’ ON FINAL
APPROACH
“MY CALLS” “500 FEET, STABLE”

IF MONITORED APPROACH, CAPTAIN PLACES

HANDS AND FEET LIGHTLY ON THE CONTROLS
 AT 100’ ABOVE MINIMUMS AND FOLLOWS PF INPUTS
“100’ TO MINIMUMS”

 AT MINIMUMS “CHECKS''
“MINIMUMS, DECIDE”

 WITH ADEQUATE VISUAL

REFERENCES
“LANDING”
OR
 WITHOUT ADEQUATE VISUAL
REFERENCE
“GO AROUND”
FOLLOW GO AROUND ACTIONS
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PRECISION APPROACH PROFILE

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10.2 NON PRECISION APPROACH CALL OUTS

NOTE 1: Non precision approaches should be flown as CDFA (Constant descent final
approach). Reference ICAO8168. (Jeppesen ATC P- 216).
NOTE 2: Use MDA +50’ for minimums to avoid descending below MDA during the Go-
Around.
NOTE 3: The follow procedure assumes:
 The aircraft is hand flown by the PF (if the autopilot is used, the PF may set
runway heading and missed approach altitude).
 Crew has been cleared for approach.
 VOR/ ADF has been selected and identified on NAV1 and NAV 2/ADF1 and
ADF2.
 The aircraft heading is within 90 degrees of the inbound course.
 The aircraft will be fully configured and the landing checklist completed prior
to reaching final approach fix (FAF).
 Vertical speed on final approach should be adjusted as applicable. Maximum
vertical speed on the inbound track is 655’/min (CAT B), 1000’/min (CAT C).
NOTE 4: Approach mode may be used within 10 DME for more accurate FD guidance.
NOTE 5: All non-precision approaches should be flown monitored. For monitored
approach Captain should be PM and First Officer PF.

PF (F/O) PM (CAPT) Remarks

“ARM APPR/NAV MODE” (VOR APPROACH  SELECT APPR AND CHECK
ONLY) ANNUCIATION ON BOTH EFIS
 SELECT APPR SCREENS
“APPR/NAV MODE ARMED”
 WITH VOR RADIAL ALIVE
''RADIAL ALIVE''
 AT RADIAL INTERCEPT, WITH VOR
 VERIFIY VOR RADIAL ALIVE ILLUMINATED
“CHECKS” “NAV GREEN”

 VERIFY NAV GREEN  SET BOTH HEADING BUGS TO

“SET RUNWAY HEADING” RUNWAY HEADING
“RUNWAY HEADING SET”
 PRIOR TO RECHING DESCENT
POINT ENSURE CONFIGURATION
AND LANDING CHECK LIST
COMPLETE
REQUEST COMPLETE CHECKLIST AND CALL
“BEFORE LANDING CHECKLIST” “LANDING CHECKLIST COMPLETE”
 SET MISSED APPROACH ALTITUDE
“SET MISSED APPROACH ALTITUDE” ON ALTITUDE SELECTOR
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“ALT OFF” “MISSED APPROACH ALTITUDE SET”

 DESELECT ALT HOLD  APPROACHING DESCENT POINT
“CHECKS”
 TRANSITION AIRCRAFT INTO “COMMENCE DESCENT AT …….MILES.”
DESCENT WITH APPROPRIATE
PITCH SETTING  DESELECT ALT HOLD
 IF USING VS SELECT VS WITH “ALT OFF”
CORRECT VS STABLE
''VS'' “COMMENCE DESCENT NOW”
BEFORE FINAL DESCENT/
 VS IF REQUIRED FAF AIRCRAFT TO BE
“V/S GREEN” FULLY CONFIGURED,
 AT FAF, CHECK ALTITUDE, CROSS LANDING CHECK LIST
CHECK ALTIMETERS AND COMPLETE AND
INSTRUMENTS ESTABLISHED INBOUND
”____NDB, ______FT/_______DME,
______FT
INSTRUMENT AND ALTIMETERS SET AND CROSS
“CHECKS” CHECKED”
 AT ANY ALTITUDE CROSSCHECKS IF
APPLICABLE
“AT ….DME ALTITUDE SHOULD BE ……FEET”
“CHECKS” “CHECK ……DME NOW “
 AT 1000FT ABOVE MINIMUMS WITH
AIRCRAFT IS STABILISED’ ON FINAL
APPROACH
“1000 FEET, STABLE”
“CHECKS”  AT 500FT TO MINIMUMS WITH
AIRCRAFT STABILISED ON
APPROACH
 CHECK MISSED APPROACH
ALTITUDE SET
“500 FT TO, MINIMUMS”
“MY CALLS”
IF MONITORED APPROACH, CAPTAIN PLACES
 AT 100’ ABOVE MINIMUMS HANDS AND FEET AT THE CONTROLS
“100’ TO MINIMUMS”
“CHECKS”

 AT MINIMUMS  WITH ADEQUATE VISUAL

“MINIMUMS, DECIDE” REFERENCES
“LANDING”
OR
 WITHOUT ADEQUATE VISUAL
FOLLOW GO AROUND ACTIONS REFERENCES
“GO AROUND”
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NON PRECISION APPROACH PROFILE

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CHAPTER - 11

NON-NORMAL PROCEDURES

Serial Items Pages

11.1 INTRODUCTION 70
11.2 DODAR PROCESS 71
11.3 RMM PROCESS 72
11.4 ABORTED TAKE OFF AND EVACUTION 73
11.5 ENGINE FAILURE 73
11.6 ENGINE FAILURE AT OR AFTER V1 75
11.7 ENGINE FIRE OR FAILURE IN FLIGHT 76
11.8 GO AROUND 77
11.8.1 SINGLE ENGINE GO AROUND 78
11.9 STALL RECOVERY (CLEAN) 79-80
11.9.1 STALL RECOVERY (CONFIGURED) 81
11.10 STEEP TURNS PROFILE 84
11.11 EMERGENCY DESCENT PROFILE 85
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11.1 Introduction
The following material is guidance for abnormal and emergency multi-crew operation of
the aircraft.

Latest CRM training and Simulator experience has proven that a systematic approach to
dealing with non-normal situations leads to the best possible outcome. It is recommended
the crew utilise a decision and risk management model (RMM). This model allows for
flexibility in the cockpit while still dealing with non-normal situations systematically.

The most important tasks are AVIATE, NAVIGATE and COMMUNICATE, in order of
priority. Only once the aircraft has reached a ‘Safety Window’ should one start the
Management process and non-normal Checklists. Abnormal and Emergency checklists
form part of the Management Model process.

A “Safety window” is a concept and cannot be defined by a fixed set of parameters. It will
vary according to the situation. For example:
1) In a busy circuit pattern: once clear of all the traffic (2000’ AGL and more than 5nm
from the field).
2) On an IFR departure: safely on track or en-route to a holding that has been requested
from ATC or even only once in the holding pattern.
3) In mountainous terrain…safely clear of terrain or MSA.

During all non-normal situations, pilot monitoring duties are essential. Where possible the
Captain should be the pilot monitoring.

All actions taken during the emergency are done in a positive and deliberate manner and
not done in haste.

In all abnormal and emergency procedures the following practice should be adopted:

AVIATE Control the Aircraft (Autopilot if available)

Contain (Memory items if required)

NAVIGATE To safety window

Lateral - stay on track or engine inoperative routing
Vertical - to terrain clearance/altitude limitations

COMMUNICATE Mayday or Pan call

(Be careful of further ATC distractions until situation is under
control)

Once SAFETY WINDOW is reached: Management Process (RMM)

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11.2 DODAR PROCESS

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11.3 RMM PROCESS

AIRBORNE RISK MANAGEMENT MODEL

AVIATE, NAVIGATE, COMMUNICATE
CONSIDER TIME MANAGEMENT
ASSESSMENT
(Seek information - Test understanding - Propose - Summarise)

1. ANALYSE: CIRCUIT BREAKERS & SWITCHES

CONFIRM ANNUNCIATOR SERVIVEABLE
2. DIAGNOSE: WHAT WENT WRONG?
IDENTIFY & VERIFY PROBLEM
3. IDENTIFY PROCEDURE TO RECTIFY/CONTAIN THE PROBLEM

ACTION
(Monitor - Test understanding)

COMPLETE PROCEDURE TO RECTIFY/CONTAIN THE PROBLEM

MANAGEMENT
(Summarise - Prioritise - Seek Information - Test Understanding)

WHAT IS THE STATUS OF THE EVENT/PROBLEM?

MAKING THE DECISION

CONSIDER:

OPERATIONAL NEEDS TASK NEEDS INDIVIDUAL NEEDS

Fuel/Endurance Company (CONTROL STRESS)
AWOPS/Weather Passengers Individual crew
A/C Performance Individual passengers
MEL
Maintenance
ATC/SAR Facilities

1. LIST BEST OPTIONS

2. BRAINSTORM OPTIONS
3. CHECK FOR POOR JUDGEMENT CHAIN
4. SUMMARISE

IMPLEMENT DECISION MONITOR PROGRESS - CHECK FOR POOR JUDGEMENT CHAINS

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11.4 ABORTED TAKE-OFF AND EVACUATION

PF PM
Power levers...................................GROUND FINE
Brakes.............................................AS REQUIRED
Power levers...................................FLIGHT IDLE ATC...............................ADVISE STOPPING
Park brake.......................................SET PAX...............................ADVISE TO REMAIN SEATED

CREW TO ASSESS. CAPTAIN TO ATTEND TO ANY MEMORY ITEMS

IF THE CAPTAIN DECIDES TO EVACUATE

CAPT FO
Condition levers (BOTH)....................CUT-OFF
Propeller levers (BOTH).....................FEATHER
Firewall valves (BOTH).......................CLOSE
PAX announcement............................ORDER EVACUATION Remove fire extinguisher from under seat
ATC.....................................................NOTIFY
Gang Bar............................................OFF Assist and direct passengers

Assist and direct remaining passengers

11.5 ENGINE FAILURES

In the event of an engine failure, the tasks of Aviate and Navigate become challenging and
are yet crucial to ensure a safe outcome. The PF must focus as much attention as possible
on controlling the aircraft. Using Flight Director and, where appropriate, the autopilot, will
reduce the PF’s workload considerably.

It is crucial that the PM monitors flight path and assists the PF with FDP selections.

The PM shall also action the memory items, however the PF must verify the correct switch
or lever selection before the PM may action it.

The principles of dealing with an engine failure in flight do not change (Identify, Verify,
and Memory Items). The SARPS (standard and recommended procedures) divide these
duties between the PF and PM. Additional items have been added to the Beech craft
procedures to include the use of the Flight Director, and to ensure that both crew
identifies the failed engine correctly.
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11.6 ENGINE FAILURE AT OR AFTER V1 (TAKE-OFF CONTINUED)

ANY PILOT TO CALL “ENGINE FAILURE!”

PF PM
 AT VR
 ROTATE AT 3°/SEC TO 8° NOSE UP, THEN “ROTATE”
MAINTAIN V2  WITH POSITIVE RATE OF CLIMB INDICATED ON
THE PRESSURE ALTIMETER AND VSI AND OR
VISUAL CONFIRMATION OF THE AIRCRAFT
HAVING LEFT THE GROUND
“POSITIVE CLIMB”

“GEAR UP” “GEAR UP?”

GEAR HANDLE…..………………………..SELECT UP
 SWITCH TAXI & LANDING LIGHT OFF
 VERIFY GEAR DOWN INDICATOR LIGHTS AND
THE LANDING GEAR HANDLE LIGHTS HAVE
EXTIGUISHED
“GEAR UP, NO LIGHTS”

 ENSURE FAILED ENGINE’S PROPELLER GAUGE

“CONFIRM AUTOFEATHER” INDICATES A RAPID DECREASE IN RPM
“PROPELLER HAS FEATHERED”

AT ACCELERATION ALTITUDE SELECT HEADING AND ALT ON FDP

"HEADING AND ALT" “HEADING AND ALT GREEN"

ACCELERATE TO FLAP RETRACTION SPEED – VENR 123 KTS SELECT IAS ON FDP
"IAS" "IAS GREEN"

“FLAPS UP?”
(CONFIRMING UNDERSTANDING OF INSTRUCTION)
“FLAPS UP” FLAP SELECTOR…………………………SELECT UP
 VERFIY FLAPS INDICATE UP ON GAUGE
“FLAPS UP INDICATED”

 ADVISE ATC WHEN PRACTICAL (MAYDAY call)

 CONTINUE WITH THE ENGINE INOPERATIVE

FLIGHT PATH  VERIFY WHICH ENGINE HAS FAILED BY
 AT OR ABOVE 1500’ AGL CONFIRMING AT THE TORQUE GAUGES
 IDENTIFY THE FAILED ENGINE BY USING THE “AFFIRM, LEFT/RIGHT ENGINE FAILURE”
DEAD LEG, DEAD ENGINE PRINCIPLE
“LEFT/RIGHT ENGINE HAS FAILED, CONFIRM?”

“ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1)

TAKEOFF CONTINUED” EMERGENCY CHECKLIST.
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TAKE OFF-POWER FAILURE AT OR ABOVE V1

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11.7 ENGINE FIRE OR FAILURE IN FLIGHT

EITHER PILOT TO CALL “ENGINE FAILURE/FIRE!”

PF PM
“SET MAX POWER”  SET MAXIMUM POWER (OBSERVE ITT LIMITS)
 BEGIN DRIFT DOWN GUIDANCE “MAX POWER SET”
 CALL FOR LOWER ALTITUDE IF IN CRUISE PHASE
 SELECT ALTITUDE ON ALT SELECTOR
“ALTITUDE .....” (IF APPLICABLE) “.........FEET” OR “FL...........”
“IAS ”  SELECT IAS ON FDP
“IAS GREEN”
IDENTIFY THE FAILED ENGINE BY USING THE DEAD LEG DEAD
ENGINE PRINCIPLE  VERIFY WHICH ENGINE HAS FAILED BY
CONFIRMING AT THE TORQUE GAUGES
“LEFT/RIGHT ENGINE HAS FAILED, CONFIRM?” “AFFIRM, LEFT/RIGHT ENGINE FAILURE”

PILOT MONITORING CALLS OUT THE MEMORY ITEMS

“ENGINE FIRE/FAILURE IN FLIGHT MEMORY ITEMS”
“CONDITION LEVER, FUEL CUT OFF”
 PLACE FINGER IN FAILED ENGINE’S CONDITION
LEVER
“LEFT/RIGHT CONDITION LEVER, CONFIRM?”
 VERIFY PM’S HAND IS ON THE CORRECT
CONDITION LEVER  CUT THE FAILED ENGINE’S CONDITION LEVER
“AFFIRM” “PROP LEVER, FEATHER”
 PLACE FINGER IN FAILED ENGINE’S PROPELLER
LEVER
“LEFT/RIGHT PROPELLER LEVER, CONFIRM?”

 VERIFY PM’S HAND IS ON THE CORRECT  FEATHER THE FAILED ENGINE’S PROPELLER
PROPELLER LEVER LEVER
“AFFIRM” “FIREWALL FUEL VALVE, CLOSE”
 PLACE FINGER IN FAILED ENGINE’S FIREWALL
FUEL VALVE SWITCH
“LEFT/RIGHT FIREWALL FUEL VALVE, CONFIRM?”

 VERIFY PM’S HAND IS ON THE CORRECT  CLOSE THE FAILED ENGINE’S FIREWALL FUEL
FIREWALL FUEL VALVE VALVE
“AFFIRM”

“FIRE EXTINGUISHER, ACTUATE”

 PLACE FINGER IN FAILED ENGINE’S FIRE
 VERIFY PM’S HAND IS ON THE CORRECT FIRE EXTINGUISHER
EXTINGUISHER “LEFT/RIGHT FIRE EXTINGUISHER, CONFIRM?”
“AFFIRM”  ACTUATE FAILED ENGINE’S FIRE EXTINGUISHER
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WHEN APPROPRIATE, ASK FOR THE “ENGINE FIRE IN FLIGHT COMPLETE ENGINE FIRE OR FAILURE IN FLIGHT CHECKLIST
OR ENGINE FAILURE IN FLIGHT” EMERGENCY CHECKLIST

11.8 GO-AROUND CALL OUTS (ON THE CALL OF GO-AROUND BY EITHER PILOT)
PF PM
“GO AROUND” (ANY PILOT) “GO AROUND” (ANY PILOT)
“SET MAX POWER”
SIMULTANEOUSLY
GO-AROUND BUTTON…………….PRESS
POWER LEVERS LEVERS………..ADVANCE PROP LEVERS………..FULL FORWARD
 ADVANCE POWER LEVERS SMOOTHLUY  ENSURE MAX POWER WAS SET BY PF
 SET MAX ALLOWABLE POWER  MONITOR TQ AND ITT LIMITS

“MAX POWER SET”

 ONCE CLEAR OF OBSTACLES AND ABOVE
VREF +5
“FLAP 17”
“FLAPS 17?”
 CONFIRMING UNDERSTANDING OF
INSTRUCTIONS
FLAP SELECTOR ………SELECT 17
 VERFIY FLAPS INDICATE 17 ON GAUGE

“FLAPS 17 INDICATED”
“GEAR UP”  WITH POSITIVE CLIMB INDICATED ON VSI
“POSITIVE CLIMB”

“GEAR UP?”
GEAR HANDLE ………….SELECT UP
TAXI LIGHT………………OFF
 PASSING 1000 AGL AND ABOVE 128KTS  VERIFY GEAR DOWN INDICATOR LIGHTS AND
THE LANDING GEAR HANDLE LIGHTS HAVE
EXTIGUISHED
“FLAPS UP” “GEAR UP, NO LIGHTS”

“FLAPS UP?”
 CONFIRMING UNDERSTANDING OF
INSTRUCTIONS
FLAP SELECTOR ……….....SELECT UP
 VERFIY FLAPS INDICATE UP ON GAUGE
''ENGAGE YAW DAMPER'' “FLAPS UP INDICATED”

''CHECK'' YAW DAMPER ENGAGED

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AT 160 KTS APPROX SELECT HDG AND IAS ON FLIGHT DIRECTOR

''FLIGHT DIRECTOR HDG, IAS''

''CHECK'' SET CLIMB POWER

''CLIMB POWER SET'' ''CLIMB POWER SET''

''CHECK'' ADVISE ATC

REQUEST
COMPLETE AFTER TAKE OFF CHECK LIST
''AFTER TAKE OFF CHECKLIST'' ''AFTER TAKE OFF CHECKLIST COMPLETED''

11.8.1 SINGLE ENGINE GO AROUND CALL OUTS

PF PM
“GO AROUND” (Any Pilot) “GO AROUND” (Any Pilot)
“SET MAX POWER”
SIMULTANEOUSLY POWER LEVERS…………………MAX POWRER
 DEPRESS GA ON POWER LEVERS “MAX POWER SET”
 ADVANCE POWER LEVERS
 ROTATE TO GA ATTITUDE ON FD TO MAINTAIN
VREF FLAP SELECTOR…………………………..17
“FLAPS 17” “POSITIVE CLIMB”
“GEAR UP” LANDING GEAR…………………………UP
TAXI LIGHT………………………………..OFF

“FLIGHT DIRECTOR……….................HDG, ALT'' ACCELERATION ALTITUDE

“ACCELERATION ALTITUDE”

FLIGHT DIRECTOR……………….. HDG, ALT

AT VYSE
“FLAPS UP” “VYSE”

''FLIGHT DIRECTOR……………………..IAS'' FLAP SELECTOR…………………………….UP

“ENGAGE YAW DAMPER”

FLIGHT DIRECTOR ………………………..IAS

“SET MAX CONTINUOUS POWER”

YAW DAMPER…………………ENGAGED

SET POWER
“MAX CONTINUOUS POWER SET”

“AFTER TAKEOFF CHECKLIST” ADVISE ATC

COMPLETE AFTER TAKE OFF CHECKLIST TO THE LINE

''AFTER TAKEOFF CHECKLIST COMPLETED''
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11.9 STALL RECOVERY (CLEAN)

PF PM

STALL WARNING, BUFFET OR SIGNS OF APPROACHING STALL

“STALL, SET MAX POWER”

SIMULTANEOUSLY

ATTITUDE ……… LOWER NOSE TO HORIZON

POWER LEVERS …………………ADVANCE PROPELLER LEVERS……FULL FORWARD

POWER LEVERS……………MAX POWER
“MAX POWER SET”

“CHECK”

AS SPEED INCREASES, RAISE NOSE TO ESTABLISH CLIMB WHEN VSI AND ALTIMETER SHOW POSITIVE RATE OF CLIMB
“POSITIVE CLIMB”

“CHECK”
FLIGHT DIRECTOR ……………...HDG, ALT
ABOVE 128 KNOTS AND CLEAR OF TERRAIN YAW DAMPER……………….ENGAGED
“FLIGHT DIRECTOR………………HDG, ALT

“ENGAGE YAW DAMPER”

SET CLIMB POWER
“CLIMB POWER SET”
“CHECK”

“CLIMB POWER SET”

CONTINUE AS PER NORMAL TAKE OFF PROCEDURE

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CLEAN STALL RECOVERY PROFILE

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11.9.1 STALL RECOVERY (CONFIGURED)

PF PM

STALL WARNING, BUFFET OR SIGNS OF APPROACHING STALL

“STALL SET MAX POWER”

SIMULTANEOUSLY

ATTITUDE……RELAX BACK PRESUURE, NOSE TO 5˚

POWER LEVERS………………..ADVANCE PROPELLER LEVERS ……FULL FORWARD

POWER LEVERS…………..MAX POWER
“MAX POWER SET”

“CHECK”
CROSSING MIN 100 KNOTS
“FLAPS 17”
“FLAPS 17”
SELECT GO AROUND, RAISE NOSE TO 8˚ ATTITUDE

WHEN VSI AND ALTIMETER SHOW POSITIVE RATE OF CLIMB

“GEAR UP” “POSITIVE CLIMB”

“GEAR UP, NO LIGHTS”

ABOVE 128 KNOTS AND CLEAR OF TERRAIN
“FLAPS UP” “FLAPS UP”

“FLIGHT DIRECTOR ………………...’’HDG'' FLIGHT DIRECTOR………… ‘’HDG’’

“ENGAGE YAW DAMPER” YAW DAMPER………......ENGAGED
“IAS” (TO CLIMB TO MSA)
SELECT “IAS”
“CLIMB POWER SET” SET CLIMB POWER
“CLIMB POWER SET”
REQUEST
“AFTER TAKE OFF CHECKLIST COMPLETE THE AFTER TAKE OFF CHECKLIST
''AFTER TAKE OFF CHECKLIST COMPLETED”
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TAKEOFF CONFIGURED STALL RECOVERY PROFILE

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LANDING CONFIGURED STALL RECOVERY PROFILE

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11.10 STEEP TURNS PROFILE

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11.11 EMERGENCY DESCENT PROFILE

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CHAPTER-12

ADVERSE WEATHER OPERATION

Serial Items Pages

12.1 TAKE OFF 87
12.2 LANDING 87
12.3 WINDSHEAR 87
12.3.1 WINDSHEAR AVIODANCE 87
12.3.2 WINDSHEAR RECOVERY MANOEUVER 87
12.3.3 WINDSHEAR RECOVERY MANOEUVER 88
CALL OUTS
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12.1 TAKEOFF
Slippery or contaminated runways significantly decrease the takeoff performance of the aircraft.
Tailwind takeoffs are not permitted on slippery runways.
Comply with the performance as applicable in the Supplementary section of the AFM. Takeoff is
not recommended if the braking action is reported to be less than medium.

12.2 LANDING
Braking will be significantly less effective on wet or icy runways. Do not land where deep
standing water, deep slush or deep snow is present unless diversion is not practical.

12.3 WIND SHEAR

Low altitude wind shear encounters are especially significant because wind shear can place the
crew in a situation which will test the maximum performance capabilities of the aircraft and the
crew. Wind shear encounters below 500’ AGL are the most threatening because there is little
time or altitude to respond to and recover from an inadvertent encounter.

12.3.1 WIND SHEAR AVOIDANCE

Carefully assess all available information such as pilot reports of wind shear or turbulence, low
level wind shear alerts and weather reports, including thunderstorm and virga activity. Avoid
areas of known severe wind shear. If severe wind shear is anticipated, delay takeoff or do not
continue an approach until conditions improve. If wind shear is suspected, be especially alert to
any of the danger signals and be prepared for the possibility of an inadvertent encounter.
Crew co-ordination and awareness is very important, particularly at night or in marginal weather
conditions, to ensure immediate recognition of a deteriorating flight path. Closely monitor the
vertical flight path instruments, such as VSI, altimeters and G/S indicators. The PM should
immediately call out any deviations from normal.

Wind shear may be recognised as a change in more than:

+ 15 knots IAS
+ 500 ft/min vertical speed
+ 5 pitch attitude
+ 1 dot displacement from the G/S

12.3.2 WINDS HEAR RECOVERY MANOEUVRE

The following action should be taken when preventative action is not successful, or whenever
flight path control becomes marginal below 500’ AGL on takeoff or landing. The flight crew must
determine the possibility of marginal flight path control using all the information available in the
cockpit.
Power - Set max power
Pitch - Maintain 12 to 15 Nose Up (Do not follow flight director)
Do not reconfigure or attempt to regain airspeed until ground contact no longer a factor.
PM to call any trends towards the ground.
If ground contact imminent, transient power may be required.
 1900D Chapter 12 Page 88
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PROCEDURES
Revision 2 May 2017

12.3.3 WINDSHEAR RECOVERY MANOEUVRE CALL OUTS

PF PM
AT FIRST INDICATION OF POSSIBLE WINDSHEAR

“WINDSHEAR, SET MAX POWER”

SIMULTANEOUSLY:
POWER LEVERS………………..ADVANCE
ROTATE TO 8-10 DEG PITCH ATTITUDE (DO NOT FOLLOW PROPELLER LEVERS ……FULL FORWARD
FLIGHT DIRECTOR - REFER TO BASIC ATTITUDE POWER LEVERS…………..MAX POWER
“MAX POWER SET”

MONITOR PITCH ATTITUDE AND CALL

INITIALLY, DO NOT ATTEMPT ANY CONFIGURATION CHANGE ''CHECK PITCH IF ATTITUDE IS BELOW 8-10DEG''

IF THE AIRCRAFT IS NOT CLIMBING, SMOOTHLY INCREASE

PITCH UNTIL A CLIMB IS ESTABLISHED OR THE STALL MONITOR ROC/ROD CAREFULLY, CALL OUT RADIO ALTIMETER
WARNING IS ENCOUNTERED. IF STALL WARNING IS HEIGHT AND AIRSPEED TREND
ENCOUNTERED, DECREASE PITCH TO DEPART THE STALL
WARNING REGIME

WHEN POSITIVELY CLIMBING AND PASSING 400FT AGL

“PASSING 400 FT, POSITIVE CLIMB”

CONTINUE WITH NORMAL GO AROUND

CONTINUE WITH NORMAL GO AROUND

 1900D Chapter 13 Page 89
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017

CHAPTER – 13

SYSTEM CHECKS

Serial Items Pages

13.1 AUTO FEATHER CHECK 90
13.2 OVERSPEED GOVERNOR & RUDDER 90
BOOST CHECK
13.3 GROUND IDLE LOW PITCH STOP CHECK 91
13.4 PRIMARY GOVERNOR CHECK 91
13.5 MANUAL FEATHER CHECK 91
 1900D Chapter 13 Page 90
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017

13.1 AUTO FEATHER CHECK

Auto feather System ..............................................................................................CHECK AND ARM

a. Auto feather Switch ..............................................................................................................OFF
• AUTO FETHER OFF Annunciator ...........................................................................ILLUMINATED
b. Auto feather Switch ............................................................................................................TEST
• AFX DISABLE Annunciator.....................................................................................ILLUMINATED
c. Power Levers .............................................................................ADVANCE ABOVE 1000 FT-LBS
• Approx 1000 Ft-Lbs - L & R AUTO FEATHER and L and R AFX Annunciators….ILLUMINATED
• AFX DISABLE Annunciator..............................................................................EXTINGUISHED
d. Power Levers ..........................................................................................RETARD INDIVIDUALLY
1) Approx 750 Ft-Lbs:
• Opposite AUTOFEATHER and AFX Annunciators.......................................EXTINGUISHED
• AFX DISABLE Annunciator............................................................................ILLUMINATED
2) Below 500 Ft-Lbs - On-side AUTOFEATHER and AFX Annunciators ..............EXTINGUISHED
(propeller starts to feather)
NOTE
AUTO FEATHER and AFX annunciators will cycle on and off with each fluctuation of torque as
the propeller starts feathering
3) Advance power lever above 1000 Ft-Lbs and repeat 1) and 2) by retarding opposite power
lever.
e. Power Levers .......................................................................................................................IDLE
• L and R AUTOFEATHER and left and right AFX Annunciators ...................EXTINGUISHED
• AFX DISABLE Annunciator............................................................................ILLUMINATED
f. Auto feather Switch ...............................................................................................OFF, then AR
• AFX DISABLE Annunciator..........................................................................EXTINGUISHED
(with switch in OFF or ARM position)
• AUTO FEATHER OFF Annunciator .............................................................EXTINGUISHED
(with switch in ARM position)
13.2 OVERSPEED GOVERNOR AND RUDDER BOOST CHECK :( With Propeller levers
full forward)
a. Prop Test Switch ......................................................................................HOLD TO OVERSPEED
b. Power Levers (individually...............................................Increase until prop is stabilized at
1535 to 1595 RPM. Continue to increase until
rudder pedal resistance is felt on side of
advancing power (approximately 1200 Ft-Lbs
differential torque). Observe ITT & torque
limits.
c. Control Wheel Disconnect Switch ..............................................................................1ST LEVEL
d. Rudder Boost .......................................................................................................INTERRUPTED
e. Power Levers .......................................................................................................................IDLE
f. Repeat Steps b, c, d, e on the opposite engine.
g. Prop Test Switch ...........................................................................................................RELEASE
 1900D Chapter 13 Page 91
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017

13.3 GROUND IDLE LOW PITCH STOP CHECK

a. Power Levers .......................................................................................................................IDLE

b. Condition Levers............................................................................HIGH IDLE, NOTE PROP RPM
c. Prop Test Switch .......................................................................................HOLD TO LOW PITCH
1) L & R RPM....................................STABILIZED APPROX 200 RPM BELOW VALUE IN STEP b.
2) PROP GND SOL Annunciator (if installed) ................ILLUMINATED IN APPROX 8 SECONDS
3) Each Power Lever ................................................................INDIVIDUALLY LIFT & RELEASE
a) L & R RPM ...............................................NOTE BOTH INCREASE TO ORIGINAL VALUE
IN STEP b. AS EACH POWER LEVER IS LIFTED
b) PROP GND SOL Annunciator (if installed) ............................................EXTINGUISHED

d. Prop Test Switch ..........................................................................................................RELEASE

1) L & R RPM................................................................VERIFY RETURNS TO VALUE IN STEP b.
2) PROP GND ...................................................................................REMAINS EXTINGUISHED
e. Condition Levers.........................................................................................LOW IDLE

13.4 PRIMARY GOVERNOR CHECK

a. Both Propeller Levers …………………………………………………………………………….FULL FWD POSITION

b. Both Power Levers ……………………………………………..ADVANCE, MONITOR Np UPTO 1500 PRPM
c. Both Propeller Levers …………………………………RETARD TO TAXI POSITION, THEN FULLY
FORWARD TO CHECK Np STABILIZES AT 1500
PRPM
d. Both Power Levers ………………………………………………………………………………………………………….IDLE

13.5 MANUAL FEATHER CHECK (TO BE CARRIED OUT PRIOR TAXI)

a. Note Torque
b. Propeller Levers ………………………………………………………………………MOVE TO FEATHER POSITION
c. Note Torque Increase & Prop RPM Decrease to APPROX 400 RPM
d. Propeller Levers ………………………………………………………………………………MOVE TO TAXI POSITION
e. Torque ………………………………………………RETURNS TO ORIGINAL VALUE WHEN UNFEATHERING
 1900D Chapter 14 Page 92
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017

CHAPTER - 14

CIRCUIT AND LANDING / TOUCH AND GO

Serial Items Pages

14.1 CIRCUIT AND LANDING / TOUCH AND GO 93-97
PROCEDURE
 1900D Chapter 14 Page 93
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017
14.1 CIRCUIT AND LANDING / TOUCH AND GO

PF PM
POWER LEVERS………………….ADVANCE  WHEN “AFX” ANNUNCIATORS ILLUMUNATE
 RELEASE BRAKES ONCE PROPS AND GOVERNING
AT A MIN OF 2000LBSTORQUE AND PM HAS
CALLED “AUTO-FEATHER ARMED” “AUTO-FEATHER ARMED”

 WHEN POWER IS SET

“SET MAX POWER” or “SET REDUCED POWER”
“MAX POWER SET” or “REDUCED POWER SET”

 MONITOR ASI, ON ACCLERATING THROUGH 80

KTS
“80 KNOTS”
 AT V1/V ROTATE
''V1 / ROTATE''
“CHECK”  WITH POSITIVE CLIMB INDICATED ON PRESSURE
ALTIMETER AND
 BOTH HANDS ON CONTROL COLUMN VSI OR VISUAL CONFIRMATION THAT THE
 ROTATE AT 3° / SEC INTO FLIGHT DIRECTOR BARS AIRCRAFT HAS LEFT THE GROUND

“POSITIVE CLIMB”

“GEAR UP”  GEAR SELECTOR UP WHEN GEAR LIGHTS ARE

OUT

“GEAR UP, NO LIGHTS”

 SWITCH TAXI LIGHT OFF
“FLAPS UP?”
 PASSING 400 AGL AND 123KTS (CONFIRMING UNDERSTANDING OF INSTRUCTION)
“FLAPS UP”
 FLAP SELECTOR………………SELECT UP
 WHEN FLAPS INDICATING UP ON GAUGE

” FLAPS UP INDICATED”
 YAW DAMPER…………...ENGAGE
 ONCE YAW DAMPER IS ENGAGED
 ONCE FLAPS CONFIRMED UP “ YAW DAMPER ENGAGED”
“ENGAGE YAW DAMPER ” BLEEDS……………………………….ON ENVIR MODE CONTROL………
AUTO
 AT APPROXIMATELY 150 KTS SELECT HEADING AND IAS ON FCP
“HEADING AND IAS MODE” ONCE SELECTED, HDG AND IAS DISPLAYED IN GREEN ON EFIS

“HEADING AND IAS GREEN”

“CHECK”
 1900D Chapter 14 Page 94
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017

500-1000 AGL…….. TURN DOWNWIND

(CLIMBING TURN - 25 DEGREE BANK)

 APPROACHING 1500 AGL  DECREASE TORQUE TO 1500FT/LBS, SET PROPS

''SET POWER 1500 FT LBS'' TO 1550 RPM
“ POWER SET”
REQUEST  LOOK FOR CONFLICTING TRAFFIC
“AFTER TAKE-OFF CHECKLIST”
(FIRST TAKE OFF ONLY) COMPLETE CHECKLIST TO THE LINE AND CALL
''AFTER TAKE-OFF CHECKLIST COMPLETED”
AT CIRCUIT ALTITUDE
''FLIGHT DIRECTOR ………. “ALTITUDE”
POWER ……………APPROX 1500 FT-LBS ''FLIGHT DIRECTOR ………. “ALTITUDE”
PROPS------------- 1550 RPM
SPEED …………………………160 KNOTS

ON DOWNWIND
“FLAPS 17”
“GEAR DOWN” “FLAPS 17”
“GEAR DOWN”
TOUCH AND GO BRIEFING
AFTER TOUCH DOWN, RESET MY FLAPS AND TRIM,
GO WHEN READY, SET TORQUE 3000 FT-IBS

ABEAM THRESHOLD PUNCH CLOCK FOR 30 SEC, INNITIATE

TURN AND SET RUNWAY HEADING.

ON BASE POSITION OR EQUIVALENT TO INITIATE DESCENT

TURN
“PROPS FULL FORWARD”
“PROPS FULL FORWARD” ''YAW DAMPER ………. DISCONNECT''
''YAW DAMPER ………. DISCONNECT''

TORQUE………………1000FT-LBS
REDUCED SPEED TO VREF + 10 KTS
ROD…………………500 FT/MIN APPROX

AT 1000 FT AGL
“FLAPS………………..35° ''FLAPS………………..35°
REQUEST
“LANDING CHECKLIST” COMPLETE THE LANDING CHECKLIST AND CALL
''LANDING CHECK LIST COMPLETED''

ONCE LANDING CLEARANCE RECEIVED

'' WE ARE CLEARED TO LAND''
''CHECK'' ''500 FEET STABLE'
 1900D Chapter 14 Page 95
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017

AFTER THE WHEELS ARE ON THE GROUND

FLAP SELECTOR………SET FOR TAKE OFF
TRIM………………..SET TO 2 DEG UP
CALL…………………”GO”
''ADVANCE POWER LEVERS''
WHEN AUTO FEATHER ANNUNCITOR ILLUMINATES
''AUTO FEATHER ARMED''

''SET POWER 3000 FT LBS'' WHEN POWER IS SET

“POWER SET”
AT V1/V ROTATE
''V1 / ROTATE''
BOTH HANDS ON CONTROL COLUMN
ROTATE AT 3° / SEC INTO FLIGHT DIRECTOR BARS

CONTINUE FROM “POSITIVE CLIMB” TO THE

NORMAL TAKE OFF PROCEDURE
 1900D Chapter 14 Page 96
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
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CIRCUIT & LANDING / TOUCH AND GO

 1900D Chapter 14 Page 97
STANDARD OPERATING Issue Date 31 Aug 2015
PROCEDURES
Revision 2 May 2017
 1900D Chapter 14 Page 98
STANDARD OPERATING Issue Date 31 Aug 2015
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Revision 2 May 2017

GLOSSARY

ABBREVIATION AND ACRONYMS

AFM Aircraft Flight Manual

AGL Above Ground Level
AMSL Above Mean Sea Level
ATC Air Traffic Control
CANPA Constant Angel Non Precision Approach
CAPT Captain
CDFA Constant Descent Final Approach
CRM Crew Resource Management
DA Decision Altitude
FCP Flight Control Panel
FDP Flight Director Panel
FMA Flight Management Annunciator
FO First Officer
GPS Global Positioning System
ICAO International Civil Aviation Organization
PAPI Precision Approach Path Indicator
IMC Instrument Meteorological Conditions
MDA Minimum Descend Altitude
OAT Outside Air Temperature
OM Operations Manual
PAPI Precision Approach Path Indicator
PF Pilot Flying
PM Pilot Monitoring
RMM Risk management Model
RWY Runway
SID Standard Instrument Departure
STBY Stand By
TA/RA Traffic Advisory / Resolution Advisory
VMC Visual Meteorological Conditions
VOR Visual Omni directional Range
WX Weather