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3. Gear UP when positive rate of climb is established.
4. Maintain V2 speed to 1500 ft. AGL.
NOTE: If engine failure should occur after passing V2 on takeoff, it is
recommended that the speed at the time of engine failure (up to V2+10
knots) be maintained. A speed of V2+10 knots in single-engine takeoff
configuration will produce the maximum climb gradient available.
5. Flaps ................................................ UP WHEN VFS IS ATTAINED
(MAINTAIN SPEED FOR ADEQUATE STALL MARGIN)
6. Power .....................................MAXIMUM CONTINUOUS POWER
7. Engine Failure / Shutdown In Flight Checklist (Page EC-6).............
.....................................................................................COMPLETE
END
Quick Reference Handbook
REVISION 8 ABNORMAL / EMERGENCY PROCEDURES
Oct 11/02 Page EC - 3
Dual Engine Flameout AFM 4-09-40
If flameout is the result of volcanic ash encounter, an immediate
relight is not recommended. Reverse course to clear ash cloud
and proceed to Step 3.
1. Power Levers ...........................................................................IDLE
2. Airstart Ignition ...........................................................................ON
3. Airspeed ................ DESCEND AT VMO/MMO TO 25,000 FT THEN
SLOW TO 210 KCAS (NOT TO EXCEED MACH LIMITATIONS)
If engines fail to relight:
4. Oxygen Masks / Regulators ..............DON / 100% (IF REQUIRED)
5. Passenger Oxygen Masks ..................... DEPLOY (IF REQUIRED)
6. Power Levers ...........................................................................IDLE
7. HP Fuel Cocks .......................................................................SHUT
If below 28,000 ft., proceed to Step 15, otherwise:
8. Airstart Ignition ......................................................................... OFF
9. Battery Switches 1 and 2............................................ON (VERIFY)
10. Essential AC / DC Buses........................... E INV / BATT (VERIFY)
11. Electric Master Power Switches ..............................OFF (L AND R)
12. Crossflow / Boost Pumps .........................OPEN / ONE MAIN - ON
13. Electrical Load....................... REDUCE AS SITUATION PERMITS
14. Bleed Air Switches.................................................................... OFF
15. Symbol Generators 2 and 3 ....................................... ALTERNATE
16. EICAS Display ............................... TOP COMPACT (IF DESIRED)
When within airstart envelope (Below 25,000 ft., 200-324 KCAS):
17. Fire Handles .................................................................................IN
18. Crossflow / Boost Pumps .........................OPEN / ONE MAIN - ON
19. Airstart Ignition ..........................................................................ON
20. Engine RPM (HP and LP)............................................INDICATING
Continued on next page →
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 8
Page EC - 4 Oct 11/02
Dual Engine Flameout, ctd… AFM 4-09-40
21. HP Fuel Cocks (One At A Time) ......................................................
................................................OPEN (CHECK FOR FUEL FLOW)
NOTE: Use clock to time measurements of thirty (30) second airstart
attempts and engine drain time cycles.
22. Engine Parameters .........................................................MONITOR
CAUTION: ENGINE DAMAGE MAY RESULT IF RPM IS NOT
ALLOWED TO STABILIZE AT IDLE BEFORE ADVANCING POWER
LEVERS.
If engine does not relight within thirty (30) seconds or if engine
does not reach idle:
23. HP Fuel Cocks .......................................................................SHUT
24. Airstart Ignition .........................................................................OFF
Allow engines to drain for thirty (30) seconds.
25. Begin airstart procedure with Step 17.
After relight of one or both engines occurs:
26. Electrical Power.......................................................AS REQUIRED
27. Bleed Air Switches / Isolation Valve ........................AS REQUIRED
NOTE: With both engines running the configuration is BOTH BLEEDS - ON, BOTH
ECS PACKS - ON, and ISOLATION VALVE - CLOSED.
NOTE: With one engine running the configuration is OPERATING ENGINE BLEED -
ON, BOTH ECS PACKS - ON, and ISOLATION VALVE - OPEN.
28. Pressurization ............................................RESET AS REQUIRED
29. “E” Batts ...................................................................................ARM
30. Airstart Ignition ..........................................................................OFF
　
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