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6. Affected Engine FUEL CONTROL ..............................................................SHUT
7. Affected Engine FIRE Handle (Do Not Rotate)..........................................PULL
8. Engine Failure / Shutdown In Flight Checklist (Steps 5 and Subsequent).....
COMPLETE
See Section 05-10-10, Engine Failure / Shutdown In Flight.
WARNING
DO NOT RESTART FAILED ENGINE AS A HIGH
PROBABILITY OF ENGINE FIRE EXISTS.
9. Failed Side MAIN and ALT Boost Pumps .............................RECONFIRM OFF
10. Fuel Crossflow Valve.......................................................RECONFIRM CLOSED
11. Fuel Intertank Valve......................................................................AS REQUIRED
Balance fuel by using the intertank valve and establishing a small sideslip
(approximately ½ trapezoid or ball width). Move the rudder trim arrow in the
direction of the tank from which you desire to transfer fuel. This will create a slight
wing down condition toward the tank to which you desire to transfer fuel.
12. Nearest Suitable Airport..............................................................................LAND
See Section 05-10-40, One (1) Engine Inoperative Landing Procedure if required.
FUEL TANK LEAK:
13. Affected Side MAIN and ALT Boost Pumps ..................................................ON
The ßight crew must now evaluate the fuel loss rate and distance to nearest
suitable landing airÞeld. Consideration should be given but is not limited to the
following: two engine vs. single engine climb to altitude in order to achieve greater
range, maximum transfer of fuel to good tank vs. lateral controllability, and
affected side engine failure due to fuel starvation.
NOTE:
Up to 4000 lb. of fuel imbalance between tanks in ßight
has been safely demonstrated while under abnormal
conditions. For approach and landing with abnormal
fuel imbalance and an engine shut down, be prepared
to use full rudder and aileron as necessary.
14. Fuel Crossflow and Intertank Valve ...........................................AS REQUIRED
WARNING
IF INTERTANK VALVE IS USED FOR MAXIMUM
FUEL TRANSFER RATES, ENSURE PROPER
SIDESLIP IS MAINTAINED TO PREVENT FUEL
FROM FLOWING BACK INTO LEAKING TANK.
15. Fuel Transfer To Good Side.........................................INITIATE AS REQUIRED
16. Autopilot .........................................................................................DISCONNECT
OPERATING MANUAL
05-16-00 EXPANDED ABNORMAL / EMERGENCY PROCEDURES
Page 2
October 11/02
Revision 8
17. Airspeed ...........................AS REQUIRED TO MAINTAIN LATERAL CONTROL
CAUTION
IF IT BECOMES APPARENT THAT PRIOR TO LANDING
ENGINE ON LEAKING SIDE WILL FAIL DUE TO
FUEL STARVATION, SHUT DOWN ENGINE. (SEE
SECTION 05-10-10, ENGINE FAILURE / SHUTDOWN
IN FLIGHT.) OBSERVE MAXIMUM FUELIMBALANCE
LIMITS (SEE THE CHART BELOW OR SECTION
01-28-10, USABLE FUEL CAPACITIES) PRIOR TO
LANDING.
18. Nearest Suitable Airport..............................................................................LAND
See Section 05-10-40, One (1) Engine Inoperative Landing Procedure if required.
WARNING
DO NOT USE THRUST REVERSERS ON LANDING.
OPERATING MANUAL
EXPANDED ABNORMAL / EMERGENCY PROCEDURES 05-16-00
Page 3
October 11/02
Revision 8
Permissible Fuel Inbalance For All Flight Operations
Figure 1
OPERATING MANUAL
05-16-00 EXPANDED ABNORMAL / EMERGENCY PROCEDURES
Page 4
October 11/02
Revision 8
05-16-20: Fuel Boost Pump Failure
L-R MAIN FUEL FAIL (AMBER)
L-R ALT FUEL FAIL (AMBER)
1. Same Side Operative Fuel Boost Pump ........................................................ON
2. Fuel Boost Pump Switch.................................CHECK FOR “CB” INDICATION
3. If “CB” Indication Is Not Illuminated.CONFIGURE FUEL BOOST PUMPS AS
FOLLOWS
A. Fuel Boost Pump Switch ....................................................................OFF
B. Fuel Boost Pump Circuit Breaker (PDB) ........................................PULL
4. If “CB” Indication Is Illuminated ........CONFIGURE FUEL BOOST PUMPS AS
FOLLOWS
A. Fuel Boost Pump Switch ....................................................................OFF
B. Fuel Boost Pump Circuit Breaker (PDB)......................................RESET
CAUTION
RESET CIRCUIT BREAKER ONLY IF USE OF PUMP
IN QUESTION IS REQUIRED FOR CONTINUED
SAFE FLIGHT AND LANDING.
C. Fuel Boost Pump Switch ......................................................................ON
5. Indications .............................................................................................MONITOR
　
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