Just Flight BAe 146 Professional Flows

Pre-Flight Checks & Power Up Packs One to ON

WX Check Off  PACK 1 on odd dates
 Tilt 15 degrees UP  PACK 2 on even dates
Transponder Verify STBY Engine Air Verify all OFF
Air brake Verify IN Overhead Panel Press and hold TEST
Flaps Verify UP Annunciators  Verify annunciators lit and
extinguish after releasing
Batt 1 & Batt 2 ON
 Check BATT ammeter shows a Cockpit Emergency ARM
discharge Lighting
 Check for minimum 24V on the Pre-flight Testing
VOLT/AMP selector
MWS Press in fully
Nav Lights HI INT  Verify all MWS annunciators illumi-
No Smoking AUTO nated and chime sounds
Cabin Emergency ARM Return to middle position (unlit)
Lighting Flight Deck Press and hold FLT ANNUN
Landing Gear Verify lever DOWN and 3 Greens Annunciators  Verify windshear and altitude
callouts
Parking Brake Verify YEL and set  Verify flight deck annunciations
GPU (Ext AC) ON (if available) light, and extinguish once released
APU Gen ON (if required or GPU not avail) Ground Tests Engine Fire 1-4
 Verify MWS annunciation and fire
L Inner Fuel Pump ON
bell warning
APU START Stall Warn 1 & 2
 Monitor RPM for increase  Verify stick-shaker and caution
 Monitor TGT for increase, peak, Speed Warn 1 & 2
decrease  Verify horn and caution
 Check APU PWR AVAIL annun- Optionally complete other ground tests.
ciation
DC Pump ON
APU Air ON
 Verify rise in YELLOW brake pres-
Master Switches Yaw Damp 1 & 2 sure (below v-speed)
 ON OFF
AP Master
 ON AC Pump ON
Avionics A & B  Verify rise in YELLOW system pres-
 ON sure (above switch)
Ground Ignition Check setting PTU ON
 A for odd dates, B for even  Verify rise in GREEN system pres-
dates sure
 BOTH for cold weather cond.  Verify all annunciators extinguished
Anti-Skid ON AC Pump & PTU OFF
Lift Spoilers YEL & GRN WX Set to STBY
 ON
Transponder Set XPDR
Hydraulic Pumps ENG Pump 2 & 3  1 on odd dates
 Verify OFF  2 on even dates
Bus-Ties AC & DC Set to AUTO Press TEST to run TCAS check
Stby Inv & Stby Gen ARM Brake Temp TEST
Galley/Shed ON Indicators  Verify displays 750°C & OVHT
 Set to ON
Generators GEN 1 & 4
Oxygen Flight crew oxygen test left and right
 Verify OFF/RESET
 Verify air flow
Engine Anti-Ice Verify all ON Passenger oxygen supply on FO side
Cabin Air Set to RECIRC  Turn valve to ON
 Before Start Pushback & Engine Start
EFB FWD PAX Stairs To retract airstairs
 Open  AC Pump ON
Airstairs  Retract Stairs via EFB
 Down  AC Pump OFF
Fuel, Passenger, Cargo boarding can Doors Verify closed and secured
begin Lock flight deck door
Parking Brake Verify set  Check MWS door cautions extin-
Brake PSI Verify YELLOW >2,500 PSI guished
 If lower, turn DC Pump ON until APU & APU Gen On, if not already (follow blue flows un-
pressure has risen der Pre-Flight & Power Up)
Thrust Levers Verify FUEL OFF position Chocks & GPU Remove via EFB
Hydraulics Verify all switches in OFF position Fasten Belts ON
Ctr Tank Trans- AUTO Beacon ON
fer APU Air OFF (if APU has been running)
Pressurisation Verify MODE set to AUTO Packs OFF
 BARO set to standard
Parking Brake ON Until Tug Requests Disconnect
 Use ALT SET to set flight altitude
Ice Detection ON, replace guard Pushback Commence
Flight Data Re- Set date and flight leg Fuel Pumps All to ON
corder Engine Anti-Ice All to ON for start
Transponder Set squawk code or 2000 without ATC
Press ATC/FID Start PWR Verify set NORM
 Set flight ID (i.e. EG2102) using key- Start Master ON
pad  Verify START PWR ON annunciation
 ENTER to confirm Engine 4 Start START SELECT knob to 4
 ATC/FID again to switch back to ATC  Press ENGINE START switch to
mode START for 2 seconds
TMS Press PWR to turn on  Verify ENG IGN ON and STARTER
 TEST OPERATING annunciations
 Verify annunciations on each key  Monitor N1, N2, TGT gauges
 Set TREF to outside air temp At 10% N2
 Select TO for Take-Off mode  Engine 4 Thrust lever to FUEL ON
 Set TGT to 840°C  Monitor increase in values
Gauge Bugs Set N1 and TGT bugs to TMS values  At 100+ N1 and TGT verify ENG IGN
Set airspeed indicator bugs to flipchart annunciators extinguished, move
values for takeoff flaps/weight onto Eng 3
(or click the flipchart to set the bugs Engines 1-3 Repeat above in order 3, 2, 1.
automatically)
Monitor all gauges to ensure stable at
TMS Press PWR to turn off idle once all engines live.
Flight Directors Both to ON
Return START SELECT to OFF.
Altimeters Set QNH
After Start
FMS/Navigation Program FMS for LNAV navigation, or
tune VORs/courses as required Start Master OFF
Engine Anti-Ice As required
Set HSI accordingly; Ice Protect Heat All to ON
 NAV = VOR navigation
 RNAV = LNAV & FMS navigation Generators GEN 1 & 4 to ON
 Verify OFF LINE annunciators extin-
Altitude Set and ARM
guished
Radios ON and tune as required Hydraulic Pumps ENG Pump 2 & 3 to ON
DME Turn to ON  Pump 3 must remain OFF until tow-
bar disconnect
 Check YEL and GRN gauges climb
and indicate +3000psi
 After Start (cont) Takeoff & Climb
AC Pump & PTU ON once pressure has reached +3000psi Thrust Levers Advance to 55% N1
 Must remain OFF until towbar dis-  Verify stable
connect  Once stable, advance to approxi-
Brake Fans AUTO mately the gauge bugs
APU Air ON  TMS will take over and fine tune

Packs Both to ON VR Speed Pitch to 10°

Flaps Set as required Positive Rate
Transponder Set to TA Gear UP
Taxi Pitch Adjust to maintain V2+10kt
Taxi Lights ON  No steeper than 20°
WX Set to WX or MAP 1,500ft AGL
Parking Brake Release Pitch Adjust to achieve 250kt climb
Brake Test Switch to GREEN VTFO Flaps UP
 Test and verify increase in pressure
Autopilot Engage
Return to YELLOW
 Arm LNAV for FMC navigation
 Test and verify increase in pressure
 Arm V/L for VOR navigation
Flight Controls Check free & clear  Arm IAS to hold speed
Trims Rudder TMS Select SYNC mode
 Verify centered  Reduce thrust levers to 88% N1
Aileron  Increase by 1% per 5,000ft
 Verify centered Alternatively select TGT mode
Elevator  Set TGT of 840°
 Within green band range (click CG% Gear Verify UP
box on EFB to set automatically) Flaps Verify UP
Config Check Verify no horn
Cabin Air Set to FRESH
Taxi Speeds Engine Air All to ON
Runway Max 50kts APU Air OFF
Taxiway Max 30kts  Verify APU VLV NOT SHUT annuncia-
Apron Max 15kts tor extinguishes
AC Pump & PTU OFF
Before Takeoff
APU STOP
CONT IGN A & B to ON if conditions are poor
APU Gen Set to OFF/RESET
Cabin Call Press (cabin secure and crew seated)
 Wait for verification that cabin is
Cabin Call Press once in steady and safe climb
secure (releases cabin crew)
 Check that Cabin Secured slider has 10,000ft
been moved to Take-Off
Landing Lights OFF
Landing Lights ON
Fasten Belts OFF
Strobe Lights ON
Pitch Adjust to achieve 280kt climb
Brake Temps Normal runway conditions  Optionally select MCT mode on TMS
 Verify below 300°C to maintain max safe thrust
Contaminated runway conditions At 0.66 Mach speed
 Ride brakes to achieve 50-100°C  Arm MACH to hold speed to cruise
TMS PWR on altitude
 TO to arm takeoff mode
MWS All annunciations extinguished except
Greens
 ICE PROT may display
Yaw Damper ON
 Verify YD1 and YD2 lit
Transponder Set to TA/RA
 Cruise Flaps & Gear Precision App Non-Precision App
Speeds Maintain 280kt/0.68M for normal cruise Flaps 18 Intercept altitude Intercept altitude
 Max cruise 290kt/0.72M
Fuel Monitor Gear Down 1 dot below GS 3nm from FAF

Pressurisation Monitor Flaps 24 0.5 dots below GS 2nm from FAF

CONT IGN A & B to ON if turbulence is encountered Flaps 33 After GS intercept 1nm from FAF
Top Of Descent Calculate via EFB or;
Gear Verify 3 Greens
 3x difference in altitude, ± 1nm per
10kt headwind/tailwind Anti-Ice Airframe Anti-Ice
Top of Descent  OFF by 500ft AGL
Engine Anti-Ice
Pressurisation Set to landing altitude & landing QNH  As required
 Monitor for drop in cabin pressure
Air Supply Normal Procedure
Altitude Set and ARM  Cabin Air to RECIRC
 Engine Air and Packs all stay ON
TMS Select DESC mode
If Engine Anti-Ice is on
 For expedited descent select SYNC
 Pack 1 & 2 to OFF
to force lower N1
 Engine Air 1, 2, 3 to OFF
Thrust Levers Idle If APU running
Speeds Maintain 250-280kt on descent  Pack 1 to OFF
 Use airbrake as necessary  Cabin Air to RECIRC
 IAS hold in smooth conditions  APU Air On
 V/S of 2000ft in turbulent conditions  Engine Air all to OFF
Landing
Descent
10,000ft Airbrake Extend when passing through 100ft AGL
 In case of engine failure/s do not
Lights Taxi Lights to ON when controlled deploy until passing threshold
 R LANDING on when approach given Thrust Levers Ground idle when passing threshold
 L LANDING on when clear to land
Landing Lights to ON when uncontrolled Lift Spoilers Deploy once nose gear on the ground
Speeds Maintain 250kt unless otherwise advised APU Usage and 2-3 Engine Taxi
Anti-Ice If OAT is 10°C or lower with visible mois- Normal operations do not start the APU for landing or taxi-
ture in to the gate. APU should only be used for landing;
 Engine & Airframe Anti-Ice to ON  When the runway surface is contaminated
Fasten Belts ON  When ground equipment isn’t available (i.e. GPU)
 When 2 engine taxi is expected to the gate
AC Pump & PTU ON Taxi-in can be accomplished with 3 engines without APU for
Navigation Tune ILS/NDB/VOR frequency and course extended taxi/delays. 2 engine taxi must have APU on.

Decision Height Set After Landing

Taxi Lights ON
APU & APU Gen If required for landing
 START at 5,000ft (follow blue flows Strobe Lights OFF
under Pre-Flight & Power Up)
TMS OFF
Approach & Landing
Gauge Bugs Check flipchart for VREF/VAPP speeds Transponder Set STBY
for intended landing flaps Flaps UP
(or click flipchart to set these automati-
cally) Airbrake & Lift IN
Spoilers
Cabin Call Press at final descent point altitude
(cabin secure and crew seated) CONT IGN Verify both set to OFF
Navigation Switch HSI source to NAV for ILS/LOC Packs One to OFF (if both are ON)
approach  Pack 2 on odd dates
 Arm V/L once on intercept course  Pack 1 on even dates
(45° or less) Flight Directors Both to OFF
 Arm GSL once on final course
Altitude Set to zero
 Taxi In & Stand EFB FWD PAX
Thrust Levers If required, Engines 1 and/or 4 can be  Open
shut down on taxi-in to gate Airstairs
 Down
If APU is not running Chocks
 Thrust Lever 1 to FUEL OFF  Set
 GEN 1 to OFF/RESET
If APU is running Deboarding can now begin. Plane is in
 Thrust Levers 1 & 4 to FUEL OFF turnaround state—repeat flows from
 GEN 1 & 4 to OFF/RESET BEFORE START to begin new flight
Taxi Lights OFF when turning onto stand Shutdown
Parking Brake Verify YEL and set Master Switches Avionics Master A & B
 OFF
GPU (Ext AC) Request via EFB and connect Autopilot Master
 Set to ON  OFF
Thrust Levers 1, 2 and 3 Yaw Damper Master 1 & 2
(cont.)  FUEL OFF  OFF
Brake Fans If brake temps are <300°C
4 (if APU isn’t running)  Set to OFF
 Remain on until GPU connected Anti-Skid OFF
 Once GPU connected, FUEL OFF and
GEN 4 to OFF/RESET Lift Spoilers OFF
GPU (Ext AC) Request via EFB and connect
 Set to ON Galley Power SHED
Pressurisation Verify depressurized completely Packs OFF
 Cabin pressure should match air-
port elevation APU Air OFF
 Verify APU VLV NOT SHUT annuncia-
MWS Pull out fully tor extinguishes
Hydraulics PTU APU STOP
 Set to OFF  Needs to be shutdown within 30s of
AC Pump APU Air being set to OFF
 Set to OFF  Can be shortcut by holding the APU
ENG Pump 2 & 3 OVSPD test button
 Set to OFF Fuel Pumps Verify all OFF
DC Pump
 Verify OFF Lights Turn off all remaining
 Cabin emergency lighting
Fuel Pumps All to OFF  Flight deck emergency lighting
 If on APU power leave L INNER  Nav lights
pump to ON  No Smoking
Air Supply Cabin Air
 Set to RECIRC Batteries BATT 1 & BATT 2
Engine Air  OFF
 All to OFF
APU Air
 On if APU running
Packs
 Verify one ON (1 on odd dates, 2 on
even dates)
Anti-Ice Engine Anti-Ice (if off)
 Set to ON
Airframe Anti-Ice
 Verify OFF
Ice Protect Heat All to OFF
Ice Detection OFF, replace guard
With many thanks to Liam (Books) for his help in putting
Beacon OFF these flows together.