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EXPANDED ABNORMAL / EMERGENCY PROCEDURES 05-09-00
Page 3
October 11/02
Revision 8
B. Both ECS PACK Switches ....................................................................ON
C. ISOLATION Valve .........................................................................CLOSED
WITH ONE ENGINE RUNNING:
D. Operating Engine BLEED AIR Switch .................................................ON
E. Both ECS PACK Switches ....................................................................ON
F. ISOLATION Valve ..............................................................................OPEN
28. Pressurization ..................................................................RESET AS REQUIRED
29. Emergency Batteries (E-BATTS)..................................................................ARM
30. AIR START Ignition ........................................................................................OFF
31. COWL ANTI ICE / WING ANTI ICE ..............................................AS REQUIRED
32. Windshield Heat .......................................................................CYCLE OFF / ON
33. Fuel Balance..........................................................................................MONITOR
34. APU...................................................................................START (IF REQUIRED)
05-09-50: Dual Engine Out Approach And Landing
1. APU (If Available) ...............................................START (ONE ATTEMPT ONLY)
2. Starting Point.....................ESTABLISH 5,000 FT AGL OVER LANDING AREA
3. Flaps .................................................................10° (EXTEND WITH AUX PUMP)
4. Airspeed ...........................................................VREF FOR 10° FLAPS +20 KCAS
5. 180° Position ....................................................................BANK TO ESTABLISH
A 25° bank will bring the airplane to a 180° position at approximately 2,500 ft AGL.
6. Flaps .................................................................20° (EXTEND WITH AUX PUMP)
7. Bank Angle................................................................MAINTAIN TO HIGH FINAL
The bank angle should be held at 25° or as necessary for turning to high final,
depending on winds.
8. Landing Gear.....................................BLOW DOWN BEFORE TURNING FINAL
9. AUX PUMP..............................................................................ON FOR LANDING
10. Flaps ..................................................................................................................20°
NOTE:
As airspeed is reduced on final for landing, hydraulic
fluid flow will decrease and flight controls may become
less responsive. Do not use Speed Brakes if possible,
as this could hasten loss of hydraulic pressure.
11. Brakes........................................................................AS NECESSARY TO STOP
12. Emergency Brakes ........................................PREPARE TO USE IF REQUIRED
OPERATING MANUAL
05-09-00 EXPANDED ABNORMAL / EMERGENCY PROCEDURES
Page 4
October 11/02
Revision 8
ENGINE SHUTDOWN / AIRSTART / SINGLE ENGINE PROCEDURES
05-10-10: Engine Failure / Shutdown In Flight
1. Power / Configuration ................ADJUST / CLEAN UP FOR STEADY FLIGHT
NOTE:
Autothrottle will disengage.
2. Engine Synchronizer......................................................................................OFF
3. Power Lever (Failed Engine) ........................................................................IDLE
WARNING
VERIFY PROPER ENGINE (LEFT OR RIGHT).
4. HP Fuel Cock (Failed Engine).....................................................................SHUT
5. Tone Warning..........................................................................................SILENCE
6. Fuel Boost Pumps (Failed Engine)...............................................................OFF
7. AIR START Ignition (Failed Engine) .............................................................OFF
8. ELECTRIC MASTER Power (Failed Engine) ................................................OFF
9. Electrical Load ......................................................................CHECK / MONITOR
NOTE:
The APU may be used as an alternate source of
electrical power if desired. See Section 05-04-20, APU
Inflight Operation: Alternate Electrical Source or
Section 05-04-30, APU Inflight Operation: Alternate
Electrical Source - ELWS (Loadmeter) / ASC 420
Procedures.
NOTE:
If an engine is shut down due to extreme vibration,
consideration should be given to pulling the FIRE
handle to shut off fluids.
10. BLEED AIR Switch (Failed Engine) ..............................................................OFF
　
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