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KLM MD-11 - Engine out Operation; Unconfirmed EO PERF Page

KLM MD-11
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MD-11 Flight Crew Operations Manual
k
FMS -
Controls and Displays
FMS.30.118
Engine Out Operation
Unconfirmed EO PERF Page
The FMS ENGINE OUT mode predicts 1-Engine Out (EO) performance. If the
FCC detects an EO or the pilot pushes the ENG OUT key, a *CONFIRM ENG
OUT CLEAR* prompt appears for pilot selection. The actual EO or ENG OUT
key push is shown on the above modified PERF page. Pushing LSK 6R clears the
FMCFMC EO request. Confirming the EO request (LSK 6L) activates the
computations that provide EO maximum altitude and new MAX CLB, MAX
END and ECON speed targets. The climb/descent paths and fuel consumption
predictions are recomputed and displayed.
If an EO occurs during a standard instrument departure for which an EOSID is
provided in the database, the flight plan page will automatically appear with
*CONFIRM EOSID CLEAR*. Confirming the EOSID activates the EOSID flight
plan. If the database does not have an EOSID or the aircraft has flown past the
diversion point, the modified PERF page is displayed. The original SID and flight
plan will be flown as EO speeds/altitudes.
The T/O EO speed target is the speed obtained at the time of EO detection
(between V2 and V2 + 10) until the EO ACCEL altitude. At the EO ACCEL
altitude, the aircraft levels and accelerates to V3 and continues to climb at V3 until
reaching the all engine ACCEL altitude. The speed target will then become either
the next constraint speed or 250 KTS (whichever occurs first). T/O or G/A thrust
limit is maintained for EO operation until the following three conditions are met:
V3 or above is obtained, aircraft attains a clean configuration, altitude is above the
all engine ACCEL altitude.
After the conditions are met, thrust limit changes to MCT.
If the FCP altitude is set below the all engine ACCEL altitude, the ACCEL
altitude will be automatically edited when the FCC transitions to altitude capture.
Upon capture the FMS speed target will become VCL. Thrust cutback will not
occur until the FCC enters altitude hold and the configuration is clean.
LB1-3-0133
1L
2L
3L
4L
5L
6L
1R
2R
3R
4R
5R
6R
October 02, 2006

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