Navair F-14B, Emergency Procedure Tabs

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NAVAIR 01-F14AAP-1B
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192
Note
Climb performance will improve by 20
feet in 30-second climb for every
1,000-pound gross weight reduction.
Minimum performance criteria is based
on optimum conditions (day, VMC,
steady deck, experienced aircrew, nor-
mal wind over deck, etc.) and should be
increased for degraded conditions
based on judgment.
5. If minimum performance criteria are not passed
and all options are exhausted (stores jettisoned,
minimum gross weight, and divert not possible),
eject under controlled conditions.
If configured for landing: 123
4. Throttle MIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5. Ensure a minimum of 500-fpm rate of climb at 14
units AOA available for CV approach.
When preparing for landing:
Shipboard recovery in single-engine
SEC mode is considered extremely
hazardous and should be conducted
only as a last resort and if the perfor-
mance check is successful.
6. RUDDER AUTH light Verify Out . . . . . . . . . . . . . .
7. Wing sweep Set at 20
°
. . . . . . . . . . . . . . . . . . . . . . .
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