Engine Start Abort
Engine start shall be aborted if:
Engine Start Abort Procedure:
Engine start shall be aborted if:
-Engine ITT approaches or exceeds 920°C,
Engine Start Abort Procedure:
Roll Control Jam
When can you suspect a roll control jam:
Roll Control Jam Procedure:
A roll control jam is to be expected whenever manual aileron control wheel movement is restricted.
Immediate response is important especially if aircraft is in a climb or descent.
If a roll control jam is suspected, the Pilot Flying shall immediately:
If control still jammed:
Call for Roll Control Jam Checklist.
Pitch Control Jam:
What is a pitch control jam:
Pitch Control Jam Procedure:
A pitch control jam is to be expected whenever manual elevator control wheel movement is restricted.
Immediate response is important especially if aircraft is in a climb or descent. If a pitch control jam is
suspected, the Pilot Flying shall immediately:
Pitch Control Jam Procedure:
If control still jammed:
3. Both pilots attempt to control by force against jam.
If unable to overcome jam:
Control Column Force - Relax
PITCH Disconnect handle - Pull and turn 90°
Control Column - Both pilots attempt pitch control
Aircraft control - Pilot with free control column
Call for Pitch Control Jam Checklist.
FO Originating Flow: (18))
FO Before Start Flow: (TO THE LINE)
21
FO Before Start Flow: (BELOW THE LINE)
22-31) (10 total
(After Weight & Balance data is received) 22. FMS Weight Data – ENTER 23. AeroData tFDP EFB Takeoff Performance – REVIEW 24. ELEC Sys. Page on #2 MFD – DISPLAY 25. V-Speed Indexes & Bugs – SET When CA Calls “Below the Line” 26. HYD #3 ISO VLV – PRESS IN 27. Hydraulic Pressure – CHECK 28. HYD #3 ISO VLV – PRESS OUT 29. Transponder – ON ALT 30. Annunciator Panel – CHECK 31. MAIN BUS TIE - TIE
FO Engine Start Flow:
10
FO After Start Flow:
17
1. START & SELECT lights – VERIFY EXTINGUISHED 2. BLEED Flow Control – AS REQ’D 3. RECIRC Fan – VERIFY RECIRC 4. #2 MFD - CHECK 5. HYD #3 ISO VLV – PRESS IN (ON) 6. Elevator travel - CHECK 7. Ailerons & Roll Spoilers - CHECK 8. HYD #3 ISO VLV – PRESS OUT (DARK) (When AC GEN Caution Lights extinguish) 9. Flaps – SET FOR TAKEOFF 10. STBY HYD PRESS – PRESS IN (ON) 11. PTU CONTROL – PRESS IN (ON) 12. Hydraulic Pressure - CHECK 13. TANK 1 & 2 AUX PUMP switches – PRESS IN (ON) 14. MTOP switch (if used) – PRESS IN (SELECT) 15. AUTOFEATHER switch – PRESS IN (SELECT) 16. ESID Control Panel – SELECT NAV 17. DEICE PRESS 1 & 2 indicator - CHECK
FO Before Takeoff Flow:
8
(If ATC clearance not received at gate, or if amended): 1. ATC Clearance / Amendment – RECORD 2. FMS Flight Plan – REVISE 3. Flight Attendant Announcement – ANNOUNCE 4. Yaw Damper (YD)- ON 5. F/D Command – VERIFY CORRECT / RE-SYNCH HDG (At least one minute prior to takeoff) 6. Bleed Flow Control- MIN
(When Captain calls “Below the Line”
FO After Takeoff Flow:
15
1. LANDING GEAR handle – SELECT UP (When “Flaps Zero – Climb Power” commanded by PF:) 2. FLAPS – SELECT UP ONE NOTCH AT A TIME TO 0° DETENT 3. MTOP switch (if used) – PRESS OUT 4. Condition Levers – SLIDE AFT ONE DETENT TO PROPS 900 5. BLEED 1 & 2 – CONFIRM ON 6. Bleed Flow Control - NORM (When FLAP indicates 0°) 7. “Flaps Zero” – ANNOUNCE (When PF calls “After Takeoff Checklist”) 8. AUTOFEATHER Switch – PRESS OUT (DARK) 9. TANK 1 & 2 AUX PUMP switches – PRESS OUT (DARK) 10. STBY HYD PRESS switch – PRESS OUT (DARK) 11. PTU CNTRL switch – PRESS OUT (DARK)
PM 10,000 Climbing Flow
11
PM Cruise Flow
What is PF Command?
(5)
(When PF commands “Set Cruise”: )
1. Condition Levers – SLIDE AFT ONE DETENT TO PROPS 850 2. MCR rating ED– VERIFY 3. Target cruise airspeed (if requested) - DETERMINE 4. Cabin Diff. Pressure – CHECK 5. Cabin Altitude – CHECK
PM Descent Flow (8)
PM Approach Flow (14)
(If SAT is 10° or greater)
1. Windshield HEAT – SELECT OFF
PM Landing Flow: (12)
FO After Landing Flow (4)
FO Parking Flow (15)