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Q400 FLIGHT CERT
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0% found this document useful (0 votes)
221 views22 pagesFlight Cert
Q400 FLIGHT CERT
Uploaded by
Rudro KumarCopyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF or read online on Scribd
/ 22
BOMBARDIER
AEROSPACE BOMBARDIER Colgan Air [ere
400 Acceptance Flight Guidelines Revs Paget
4 PRE-FLIGHT
14.3 System Tests
‘Cockpit Preparation, — Confirm the following system tests are functional.
External Cheek 20°C or electrical load
increases are not detected, windshield
heat can only be tested during fight.
on
of
‘Complete or Unable due to Warm OAT a
[ad Engine Intake Bypass Door
Engine intake Bypass Doors. Open
Close lights out and Open gts dkuminate
within 10 seconds.
ISAT is s +10°C Hr segment must
iluminate and AC Load Left and Right 8
Phase will show an increase
Engine intake Bypass Doors.
Note: OATis > 10°C, heater can only be
tested during fight
Close
of
\Cothplate- br UhabTe au to Warm OAT = Colgan
BOMBARDIER
0400 Acceptance Flight Guidelines
- T
ir 20 May 2010.
Revs | Page 6
5 FLIGHT CONTROLS
1 Elevator Control
HYD #3 ISOL VLV Sw. «Press
= Gonfim ISOL VLV SW Advisory ight Open
Confirm #3 HYD system pressure cycles
between 2300 and 3500 PSI.
Elevator Controls.
= Full nose up then full nose down,
= Confirm full deflection on PFCS indicator and
normal response to contro! input.
Pitch Disconnect Handle Pull and Tum 90°
Pilot's Control Whee! sae Operate
— Full nose up then full nose down.
= Confirm movement of the left elevator only.
= Elevator Asymmetry Caution light illuminates,
in response to elevator movements.
Corpilot’s Control Wheel,
~ Full nose up then full nose down.
~ Confirm movement of the right elevator only.
= Elevator Asymmetry Caution light illuminates
in response to elevator movements.
Pitch Disconnect Handle Reset
HYD #3 ISOL VLV SW. Press y
— Confirm ISOL VLV SW Advisory light out
Confirm #3 HYD system pressure decays to”
1000 PSI or less.
‘Complete,
. Check
Operate /
52 Alleron Control and Trim
Flight/Taxi Switch Taxi ¥
COMO! LOCK .seeeresee of 4
Contro! Lock Spring Tension. Check #
= Freedom of movement
— Trigger release.
Aileron Trim: Neutral v
Flight Taxi soon Taxi ¥
Roll Disconnect Handle. oe Pall and Turn 90° 7
Pilot's Control Whee! Operate
— Free and independent.
= Allerons do not operate.
Co-pilot's Control Wheel... Operate ~
Full left wing down.
Left spoilers do not extend.
Splr 1 and Spir 2 Push Off Switchiights. /
ituminate.
= Full ight wing down, |
— Right spoilers do not extend.
— Spir 4 and Spir 2 Push Off Switchlights
iluminate.
Roll Disconnect Handle... Reset
Confirm both control wheels operate together
normally
FlightTaxi Switch Flight
~ Spoilers deploy in ground mode.
— Roll INBD and OUTBD Advisory ight
iluminate.
SPLR 1 PressiOft
Roll Spr Hyg and Roll Spr Inod Gna
auton lights iltuminates.
— Inboard spoiers retract,
SPLR1 Press/On
Rll Spr nod Hyd an Rol Spr Inbd Gnd
caution lights go out.
Inboard spoilers extend.
SPLR2
Press/Ott
Roll Spr Outbd Hy, Splr Out, anc Roll
Splr Outbd Gnd caution lights illuminate.
‘Outboard spoilers retract.
SPLR2 Press/On
= Roll Spr Oubd Hye, Spr Outs, and Rall
Spir Outbd Gnd caution lights go out
= Outboard spoilers extend,
Flight/Taxi Switch, 7
= Allspollers retract,
~ Rall Inbd and Outbd advisory lights go out.
Control Lock.
‘Coinplate®
Taxi
On
@
v
y
J
J
/ 20 May 2010
BOMBARDIER , eee
L
Q400 Acceptance Flight Guidelines
Rev §
Page 7
[53 Rudder Controt
Flap. 0
Steering switch ony
Rudder Operate ~
= Confit rudder travel is restricted to the first
division of travel on the PFCS indicator.
Flap. 25
Rudder Operate
— Confirm full deflection on PFCS indicator.”
RUD A ea Pross/Ott
— #1 Rud Hyd caution light illuminates,
— Confirm full rudder deflection is available
RUDE eee ProssiOn
— #1 Rud Hyd caution light goes out
RUD2.... Press/Oft
#2 Rud Hyd caution light illuminates:
~ Confirm full rudder deflection is available.
RUD ai reeeetie Pression
— #2 Rud Hyd caution light goes out os
Steering switch. ‘on
‘Complete aw | BOMBARDIER Colgan Air
0400 Acceptance Fligh
20 May 2010__|
it Guidelines Rev5 Page 8
6 DEPARTURE
— Complete QRH Taxi and Line Up Checks.
6.1. Flight instriments
6.1.1 Standby Instruments
— Compare operation of the ISI to PFD indications
during the course of the flight
— [Sl within 1 degree of elther PFD pitch and
roll, within 1/4 needle width slip/skid.
~ [Sl airspeed (within chart values).
= [Slaltimeter (within chart values).
ISI Airspeed Indication Tolerance
__ Flap 0.@ any Alt
KIAS SI
ISI Altitude Indication Tolerance
Flap 0 @ 200 KT
= Compare Standby Compass within + 10° of
either AHRS 1 and 2 headings in level, un-
accelerated fight.
Complete a
6.2. Communications i
621 VHF Comm
VHF 4 Check
= Check transmit and receive functions with a
Suitable ground station
Repeat for VHF Comm 2 &
‘Complete oe
63 Navigation a
631 VOR
VOR 4 and 2 snuw(Ghek Indications
— Select Pilot and Co-pilot NAV sources to VOR 1
and 2 respectively.
— Tune and identify nearby VOR station.
= Confirm course deviation bar, To/From and
bearing pointer indications on PFD 1 and 2
and MFD 1 and 2 NAV pages are not flagged
and provide steady indications.
= Confirm VOR 4 and VOR 2 bearing
indications to the station are within 4° of each
other.
HSI Sel... Left
Pilot's Course Selector. Rotate
= Set the selected course to obtain at least one dot
course bar deviation indication,
Hg Bug a Rotate
~ Set the selected heading so that the aircraft track.
will intercept the selected radial at approximately
48°
Nav Button snes POSS
= White VOR mode arm indication
= Aircraft smoothly captures selected radial
with proper mode sequence to VOR tracking
indication.
Repeat for VOR 2 ahd Hst/Sel right wy
Complete. 2 or | BOMBARDIER
Colgan Air
Q400 Acceptance Flight Guidelines
20 May 2010.
Rev 5
Page 9
63.2 DME
DME 1 and 2 Check Indications
— Tune and identify a nearby DME station.
~ Confirm distance indications on PED 1 and 2
and MFD 4 and 2 NAV pages are not flagged
and provide steady indications.
— Confirm DME 1 and 2 distances indications
are within 0.5 NM of each other.
DME 1 Hold... oe Check
Select DME 1 Hold then tune DME 1 to a different
station.
Confirm appropriate hold indications are
displayed and aistance indications do not
change on PFD 1 and 2 and MFD 1 and 2
NAV pages.
De-select DME Hold
Repeat for DME 2 of
Complete ©
633 ADF
ADF 1 Check Indications
— Tune and identify a suitable NDB station.
— Confirm bearing pointer indications on PFD 1
and 2. and MFO 1 and 2 NAV pages are
reasonable
Repeat for ADF 2) w
Complete nes wy
‘Area Navigation
UNS-1E
FMS 1 and 2...
= Select Pilot and Co-pilot NAV Sources to FMS 1
and 2 respectively.
= Execute a flight pian segment to a suitable nearby
waypoint,
= Confirm FMS 1 and 2 course deviation bar,
‘TolFrom and bearing pointer indications on
PFD 1 and 2 are reasonable.
~ Confirm map displays on MFD 1 and 2 NAV
pages are reasonable.
HSI Sel Left
Aireraf Maneuver
~ Position the aircraft to obtain at least one dot
course bar deviaiion indication and fly parallel to
the original course.
FMS 1 Heading Mode
Press the MNVR line select key NAV Page 1
followed by the HDG selection.
= Confim the CMD HDG field appears on the
right side of the NAV 1 page, pre-filled with
the current aircraft heading and flashing,
Press the ENTER button to confirm the heading
Press the NAV button on the FCP.
Green LNAV HDGSEL tateral mode
Indication illuminates.
~ Aircraft tes commanded heading,
FMs 1 IntercopyTrack
— Select a new heading so that the aircraft track wil
intercept the original course at approximately 45°.
= Confirm the aircraft heading changes to the
new value of the commanded heading,
— Insert an intercept of the original course and
confirm:
= AFCS lateral mode indication changes to
LNAV HDGINT.
Aircraft maintains selected heading then
‘smoothly captures selected track.
= Lateral mode indication changes to LNAV.
‘Repeat for FMS 2
(Check Indications Colgan Air
BOMBARDIER
400 Acceptance Flight Guidelines
20 May 2010
Rev §
| Page 10
UNS-1E VNAV
HSI Sel Lett
Aircraft Maneuver
Execute a fight plen segment to a suitable nearby
waypoint and track towards that waypoint using
LINAV mode,
FMs 1 \VNAV Mode
Press the VNAV button on the FMS CDU,
Confirm the VNAV PATH page appears pre-
filed with the active “To" and "Next"
waypoints,
Press the line select key adjacent to the “To”
‘waypoint allitude field and enter an altitude at
least 2000’ below current height,
Enter in the TGT VIS field a vertical speed which
rasults in a top of descent point at least 2 minutes
away.
Continue to fly current track and altitude,
MSG light flashes and 2 MIN TO TOP OF
DESCENT message is posted.
Vertical deviation scale is displayed on PFD.
Select Altitude Pre-selector to programmed
altitude.
Press VNAV and Alt Sel buttons on the FGCP.
‘White VNAV and ALT SEL vertical mode
armed indications illuminate
Aircraft continues to maintain current altitude.
Magenta VERT ALRT annunciation appears
‘on PFD 15 seconds prior to descent
Vertical rode indication changes to VNAV.
Aireraft smoothly pitches over then smoothly
captures selected path.
As aircraft approaches programmed altitude:
Vertical mode indication sequences to ALT
hold,
Aircraft smoothly captures selected altitude.
Repeat for FMS 2
‘Complete .
¥
y
ATC and TCAS.
65.4
ATC 1
Check Mode C function of ALT 1 and ALT 2
sources with air traffic control
ATC Transponder
Check
Ropeat for atc 2 lng
(Comtete:* w
652 TCAS
TCAS.. — ciceras Check
— Check TCAS mode operation
~ Cycle TCAS to STBY then TA ONLY then
TARA modes,
Confirm corresponding TCAS STBY, TA
ONLY and TARA mode indications are
displayed both PFD's and MFD Nav pages.
Check TCAS target displays.
Solect range on MFD 1 and 2 to 10 nm, 20
fam or 40 nm,
Ensure “full ime” TCAS traffic mode is
selected as incicated by display of the 2 NM
range ring,
Confirm targets of opportunity are displayed
as traffic at the appropriate position and
altitude on MFD 1 and 2 Nav pages.
‘Complete: wy Colgan Air
7 12,000 MSL
7a tim E
‘Aircraft ‘Straight and Level
= Fuel balanced within 50kg/1001b
Airspeed 200KTS:
PVD. of
Splr 1 and Spl 2 i Pushiowt
= Roll Splr Inbd Hyd, Spir Outbd Hyd and Splr
Outbd caution fights itluminate. ¢
= Confirm inboard and outboard spoilers
Indicate fuly-retracted on PFCS display.
Rudder Tim
— Trim ball centered with feet off the rudders.
Aileron Tim
~ Trim wings level with hands off the control wheel.
Table 7: Record Aileron and Rudder Trim
tem__[ 200KiaS [Lins
Merentim |g | 204d0
Ruddertim| gC | 210aW
pir and Spr Pushion
APD... 2s aid
coinileta x
72 Pitot-Static Check
Aircraft Svight and Level %
Airspeed 180 KTS
Table 8: Record Pilot's, Co-Pilot's and Standby
Airspeeds.
Tem IAS. Limits
Pilot TB. ‘within 4 KIAS of
Corpilol Teo each other
ist iT 172-164
Table 9: Record Pilot's, Co-Pilot's and Standby
Altitudes,
iter Altude Limits
Pilot i140. within 40° of
Co-pilot [weso each other _
Ist (peo | t1860-12100"
x
‘Completa 2 t
Q400 Acceptance Flight Guidelines
{ Page 11 |
20 May 2010.
Revs
73. Altemate Landing Gear Extension
734
Airspeed
UG Inhibit Switch.
— Landing Gear INOP caution light illuminates.
Landing Gear Selector Down
— Selector Handle amber and red Unsafe lights .7
illuminate.
Landing Gear Alternate Release Door. Open
Main Gear Release Handle Pull Fully Down
= Maximum pull force < 90 pounds
— L Door and R Door amber lights iluminate.
= Left Gear and Right Gear Down Green Lights
fluminated,
Landing Gear Alternate Extension Door Open ©
Nose Gear Release Handle Pull Fully Up.
= Nose Door amber light illuminates,
Nose Gear Down green light iluminated.
Alternate Gear-Locked-Down Indicators, Check
~ Hold switch and check for 3 green lights.
Alternate Gear Extension System... Check ©
Insert pump handle in socket and operate pump
Unt fully pressurised,
Alternate Landing Gear Extension
185 Kis (Max) ©
Inhibit
AntiSkid Test
~ Confirm Inba and Out Antiskid caution
lights illuminate for 3 seconds and go out
‘Complete or
20.1.1 Gear Retraction
Landing Gear Alt Releaso/Extension Doors... lose =
UG IMD rrr Norm
— Landing Gear INOP Caution light
extinguishes and gear doors close.
Landing Gear Selector... an Up ~
Normal retraction sequence.
‘Complete: ue a BOMBARDIER ceenare
400 Acceptance Flight Guidelines
20 May 2010,
Rev
Page 12
7.4 Radar
MFD 1 and 2 Rotary Selectors. Nav
WX Rotary Selector. 7 WX
WX ON message on MFD 1 and 2 NAV
displays and radar map outline appear.
Caer Up/Down
— Correct direction of response and limits of +/-
18
‘Adjust tit to obtain ground returns over a band of
‘approximately 20 to 80 NM from the aircratt.
Tit
Range 10/20/40/80/160/240...... Select
Select range on pilots and copilots EFCP
simultaneously y
Confirm position of retums on MFD 1 and 2
Change appropriately as range is changed
AMTCRt oc nnrnsninnnnenan PRE Up OF down 10°
Confirm positon of ground returns stays
constant
Airerat - Left and Right Bank Turns 25°
— Confirm are of ground returns stays constant
~ Cycle switches and confirm general corect ¥
operation of functions.
WX Rotary Selector nannies Sy
Complete BOMBARDIER Colgan Air 20 May 2010
{2400 Acceptance Flight Guidelines Rev Page 13,
8 FL250 Table 13: Record Pilot's, Co-Pilot's and Standby
aA Cab TTT] Altus.
Cabin Altitude Rate of Cimb Zer0 i oe shins
— Allow cabin altude to stabilize. o SE SiOL Ot] in iat
~ Differential pressure is 5.46 psi nominal eee 2 §cesu
Table 10: Record Cabin Altitude. a saTeeaenee
item Aittude Limits
Table 14: Record Engine Parameters
Cabin Altitude: Rad 8000" # 450) eae oe
Cabin ~ ~ os vs Check oe
~ Proceed to the cabin and check the following: Eng 1 tem
= Forward Baggage door does not leak, Gs Torque ik
Airstair Door and Emergency Exits do not = ni |
leak. Sen eeeene so
— Interior doors and bins open, close and latch We ae we
correctly nh wz
Fumishing panels do not rate. oF (Re
Operation of ANVS.
Nr |
— Landing Gear doors close tightly. 22 S| 84. -
On Pree 2 pst
‘Complete x ® GB
Ol Temp FT
82 MCR | _ MFD Elec Sys Page. Select —
BP a {OnF/ DG and AC Volts and Loads Check «
‘onditon Levers onan B50" e
eee ier eee MFO Fuel Sys Page... Select
Fuel Transfer seoneTO Tank 1 ~
‘Acoelerate to stable flight for 2 to 3 min
Table 11: Record Aircraft Weight
‘Aircra ZFW | 7 09
Fost ten Tak | Gee
Foal RghiTank | 477 BO
AlUpWeigt | YR Yay
Table 12: Record Pilot’s, Co-Pilot’s and Standby
Airspeeds. i
start: 212 stop: LDF
a Se
Pit 13 Ye Within 5 KAS
[Pe Teo] wate as
copie Peas bee
st BORAT
244 Plots AS
Tank Aux Pump 2 light iluminates.
— Confirm fuat is transferring by use of ED and
MFD Fuel page and check for correct pump
and value indications.
Fuel Telos ees on
Repeat to Tank’2 we
Complete wy Colgan Air
BOMBARDIER
2400 Acceptance Flight Guidelines
20 May 2010.
Rev 5
8.3. Ice Protection ‘]
8.3.1. Airframe Deice
Airframe Mode Selector. Fasvort *
Airframe Deicing Check
= Visually confirm boot inflation where able.
Advisory lights iluminate in proper sequence.
Deice pressure 18 +3.
ICE PROTECTION
AIRFRAME
OFF MANUAL,
AIRFRAME MODE SELECT
OFF
‘Select
van ( 08
}
Fast
boc
rors
e [
‘Complete: ma
(a7 Propeller Deice
MFO Electical Page. i Select
Prop Selector. enon
Confirm Oil Temperature low mit (bottom of
‘green band) changes from 0°C to +65°C.
Confirm Left Prop advisory light iluminates
and cycles,
Loft AC Generator oads increases on A.B
and C Phases by 0.16 + 0.02
Confirm Right Prop advisory ight illuminates
and cycles
Right AC Generator loads increases on A.B
and C Phases by 0.16 + 0.02.
of
Prop Selector.
‘Soinplete:
85 Engine Intake
MFD Elec Sys Page Select
Engine Intake Bypass Doors PressiOpen
Closed light segment goes out and Open
light segment dluminates,
Htr light segment iluminates when SAT <
++6°C in fight and Left AC Phase ‘B’ and
Right AC Phase ‘8! show an increase.
comprete
6 ECS
Blood Air 1 and 2 ‘OnyNorm
Cabin Pack... Auto
Fit Compt Pack of
‘Temp Gauge Rotary Selector Cab and FC duct
‘Temperature readings ate reasonable for the
prevailing operating condition.
Repioat with Cabin Pack Switch Of and Fit
‘Compartment Pack Switch in Auto
Auto
as req
Pack Switches.
Pack Temp Controls
‘Complete:
9 DESCENT
ee)
~ Confirm VMO indications through selected
altitudes.
Gomptete:
a BOMBARDIER [ Colgan A ne
2400 Acceptance Flight Guidelines RevS | Page 18
@ 10 Arproacues Left GA Button Press
aes ey Wings Level and GA message
Autopilot disengages.
‘Conduct missed approach.
— Complete QRH Descent and Approach checks.
eck indica /
tus t and2 som Check indications Gomptete 7
= Plot and Co-plot NAV Soureas to ILS 1 and 2
respectively 1012 Ws2
— Tune ana identity a sutabe ILS station Commence localize caplure 2s required at east 2
= Confirm course deviation bor. expanded NM outs of FAF
[oclzer poner and aidesiope porter HSI Se... ' ight
incieations are reasonable on PFD 1 and 2 faeepn Sannin eaae yey
4044 1S Corilot’s DH. Set
te commence localize capture asrequired atleast 2 Pos and Copilots Course Selectors Set
NM outside the FAF Set the course selectors to the published inbound
HSI Sel ease Left localizer course.
Pilot's DH... Set 0 Hg BUG -.eeseseeesserst Set
Complete OH Set500° — Set he intercept heading as roa,
PiiosCo-pat's MDA SetILSiminmums APPR Buon Press
Pilots and Corp's Course Selectors Set White LOC and GS arm indications.
Set the couse selectors othe published inboune Aircraft smoothly captures localizor with
localize couse proper mode sequence to LOC tacking
Hag Bu one Set Aircraft smoothly captures gideslopo wth
e — Set the intercept heading as. required proper mode sequence to GS tracking,
APPR Button ........ Press Sees
\White LOG and GS arm indications. ADE beeing pons cveree andor OM
Ara smoothiy captures lcalizr wih
Nea ie dojucnee to LOC tacking, Pitot en corpo baro-litude ndcations
Pee etn canises oceieat broas check wit pubished essing ate
proper mode sequence to GS tracking. within 40.
= AFAR 11200" AGL
‘ADF boating pointers reverse andar OM "Dual FO’ message and HSI SEL darnonds
isu an aural nications left and right bot laminated
= Pilot and co piot baro-alitides cross-cneck
with published crossing altitude within 40". Ld
= 81200" AGL = A500" AGL
“Dua in FD message and HSI SEL DH indcation appears on PED 1
diamonds left and night both illuminated, GPWS Mode 6 aural advisory “Minimums,
EGPWS Minin
ee Rare on ton 7 Press
DH indication appears on PFO 2, ae
GPWS Mode 6 aural advisory “Minimums, — Conduct missed approach. ee
Minimums" ‘Complete ae la
= Atminimums
MDA indication appears on PFD 1 and 2.
MM visual and aural indications if available
Continue approach to 100" AGL. Colgan Air
400 Acceptance Flight Guidelines
20 May 2010
Rev5
Page 16
= Complete Descent, Approach and Landing
Checks.
10.2 Landing
Aircraft
Confirm the following at touch down.
~ No asymmetric thrust as power levers are
moved to discing,
= Spoilers deploy normally.
‘Complete’
‘SOP Approach and Landing
ra
40.3 Shutdown’
= Complete Shutdown checks.
(On external inspection check for leaks, loose
panels, and tire condition.
Complete:
oe BOMBARDIER
AEROSPACE
Flight Test Worksheet
quo | smi 4345
Page Complete:
BAOM 212
RevR_ | 20May 10 | Grvrit#
Page 68
FLIGHT TEST RESULT SHEETS.
Table 6, Record Outboard Spoiler Extension and
Retraction Airspoeds. (Pg.44)
Table 1. Record Alttude(P9.18) ier mS iia
Altimeter [Limits Extension 165 # SKIAS
1 2 Speed _ 766 é
Retraction 1702 5KIAS
6/0 | 6/0 ach other seat” | 174
Within 60 fof
G10 |artana?
Table 7. Record Aileron and Rudder Trim (P9.45)
Table 3. Record Take-off Power (P9.29)
; tem [200.18 | 260KiqS | Limits
Table 2, Record Engine Start Parameters (P9.25) Fiat NO Far] ear | dar er
Eng t_[ tiem [Eng Tis 1 ria
‘Siar Oat wee “Aeron vt 7 roa
# TTT Peak te Tim [0 law © Nawal av
[320 we wos BIG Teele 1]
Cis eran | e449 [mea wer isd leh &
Hea Rudder B “3/2 £10
Tim z ele oe
Aifitudes. (Pg.44)
Table 5. Record Pilot's, Co-Pilot’s and Standby
Tem Auitode Cinils
Pilot L350 | within 40° of
Co-pilat [L208 | each other
1S
1-9 yO] 11860-12100
PAT 620 ice Table 8. Record Start Parameters (P¢.47)
ET Tem Ey Tas mat
ng Eng?
Torave Bmax
deat ef 7eae Peatlictamaistls ss
n mm | Ga _|