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8.(F-14B/D ONLY) ASYM THRUST LIMITER SW -- OFF (IF REQUIRED)
WARNING
ASYMMETRIC THRUST LIMITER SHOULD ONLY BE DISABLED IF REQUIRED
TO ASSIST/MAINTAIN CONTROL. (F-14B/D ONLY)
9./8. PERFORM ARRESTED LANDING.
WARNING
USE ONLY OPPOSING THROTTLE FOR WAVEOFF/BOLTER.
CAUTION
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CNO 051758Z APR01 Page 6 of 9 NA 01-F14AAA-1 IC 147
NA 01-F14AAA-1B IC 103
NA 01-F14AAP-1 IC 45
NA 01-F14AAP-1B IC 29
NA 01-F14AAD-1 IC 25
NA 01-F14AAD-1B IC 14
IF RUDDER PEDAL AUTHORITY IS RESTRICTED, NOSEWHEEL STEERING
SHOULD NOT BE ENGAGED UPON LANDING ROLLOUT.
(3) RENUMBER RUNAWAY STABILIZER TRIM PROCEDURE, PARA 14.12.7.2
IN F-14B NFM AS NEW PARA 14.12.7B, AND PARA 14.12.5.2 IN
F-14D NFM AS NEW PARA 14.12.5B. (NO RENUMBERING OF RUNAWAY
STABILIZER TRIM PROCEDURE IN F-14A NFM IS NECESSARY).
(4) NOTE THAT PARAGRAPHS NUMBERED AS, FOR EXAMPLE, 14.12.7A AND
14.12.7B ARE NOT SUBORDINATE TO 14.12.7, BUT FALL BETWEEN
14.12.7 AND 14.12.8 AT THE SAME LEVEL. THIS IS DONE TO AVOID
RENUMBERING PARAGRAPHS 14.12.8 AND SUBSEQUENT AT THIS TIME.
RENUMBERING OF THE SUBSEQUENT PARAGRAPHS WILL OCCUR DURING
PRODUCTION OF THE NEXT REVISION OR CHANGE TO EACH
PUBLICATION.
4. CHANGE REFS D (F-14A PCL), REF E (F-14B PCL), AND REF F (F-14D
PCL) AS FOLLOWS:
A. F-14A PAGE 46 / F-14B PAGE-56 / F-14D PAGE 70, CONTROLLABILITY
CHECK PROCEDURE:
(1) DELETE EXISTING PROCEDURE.
(2) ADD (INSERT) REPLACEMENT PROCEDURE:
CONTROLLABILITY CHECK.
IT IS ABSOLUTELY IMPERATIVE THAT THE AIRCREW THOROUGHLY AND SAFELY
EVALUATE THE DEGRADED HANDLING CHARACTERISTICS OF DAMAGED OR
MALFUNCTIONING AIRCRAFT PRIOR TO CONTINUED FLIGHT AND LANDING. THIS
CHECK DOES NOT TAKE PRIORITY OVER EXISTING EMERGENCY PROCEDURES.
WARNING
IF AIRCRAFT STALLS OR DEPARTS IN DIRTY CONFIGURATION,
IMMEDIATELY UNLOAD AND PLACE THROTTLES AT MILITARY. DO NOT
RAISE FLAPS UNTIL RECOVERED. (IF DURING FLAP/SLAT TRANSITION,
FOLLOW UNCOMMANDED ROLL/YAW PROCEDURES.)
WARNING
A CONTROLLABILITY CHECK REQUIRES THE TOTAL ATTENTION AND
AWARENESS OF THE AIRCREW. THE AIRCREW MUST BE PREPARED TO
ENCOUNTER UNUSUAL HANDLING CHARACTERISTICS SINCE THE
AERODYNAMIC PROPERTIES OF THE AIRCRAFT MAY BE SIGNIFICANTLY
CHANGED. STALL SPEED AS WELL AS FLIGHT AND GROUND HANDLING
CHARACTERISTICS MAY BE DRASTICALLY DIFFERENT FROM NORMAL.
NOTE
IF FLIGHT CONTROL MALFUNCTION IS DUE TO UNCOMMANDED STAB AUG
TRANSIENTS, SPOILER MALFUNCTION, FLAP/SLAT ASYMMETRY, RUDDER
MALFUNCTION (HARDOVER), AND/OR WINGSWEEP MALFUNCTIONS; PERFORM
APPLICABLE EMERGENCY PROCEDURE(S) AS NECESSARY BEFORE BEGINNING
A CONTROLLABILITY CHECK.
1. CLIMB TO 10,000 FEET AGL MINIMUM.
2. OBTAIN VISUAL CHECK IF POSSIBLE.
3. DECELERATE GRADUALLY TO 200 KNOTS IF FEASIBLE.
4. DIRTY AIRCRAFT, ONE CONFIGURATION CHANGE AT A TIME, WHILE FLYING
STRAIGHT AND LEVEL.
NOTE
LANDING GEAR SHOULD BE LOWERED BEFORE FLAPS. DO NOT LOWER
ARRESTING HOOK UNTIL LANDING GEAR IS CONFIRMED DOWN AND LOCKED.
5. IF FLAPS ARE LOWERED, DO SO INCREMENTALLY AND BE ALERT FOR A
FLAP/SLAP ASYMMETRY.
6. IF MANEUVER FLAPS ARE USED FOR LANDING APPROACH: WING SWEEP
_______________________________________________________________________
CNO 051758Z APR01 Page 7 of 9 NA 01-F14AAA-1 IC 147
NA 01-F14AAA-1B IC 103
NA 01-F14AAP-1 IC 45
NA 01-F14AAP-1B IC 29
NA 01-F14AAD-1 IC 25
NA 01-F14AAD-1B IC 14
DRIVE NO. 1 AND WG SWP DR NO. 2 / MANUV FLAP CB'S -- PULL (LE1
AND LE2 FOR F-14A/B; LD1 AND LE1 FOR F-14D).
NOTE
FAILURE TO PULL WING SWEEP DRIVE CIRCUIT BREAKERS (LE1 AND LE2
FOR F-14A/B; LD1 AND LE1 FOR F-14D) COULD RESULT IN INADVERTENT
MANEUVER DEVICE RETRACTION OR WING SWEEP DURING APPROACH.
NOTE
WINGSWEEP WARNING, WINGSWEEP ADVISORY, AND FLAP CAUTION LIGHTS
WILL ILLUMINATE WITH BOTH WING SWEEP DRIVE CIRCUIT BREAKERS
PULLED (LE1 AND LE2 FOR F-14A/B; LD1 AND LE1 FOR F-14D).
7. USE DIFFERENTIAL THRUST, IF REQUIRED, TO ACHIEVE ACCEPTABLE
FLIGHT CHARACTERISTICS.
8. SLOW-FLY AIRCRAFT TO DETERMINE APPROACH HANDLING CHARACTERISTICS,
INCLUDING TURNS.
9. FLY SIMULATED APPROACH TO EVALUATE LINEUP CORRECTIONS, POWER
CHANGES, AND WAVEOFF/BOLTER PERFORMANCE, AND FLIGHT
CHARACTERISTICS.
10. FOR LANDING, USE MINIMUM SAFE CONTROL SPEED, BUT NO SLOWER THAN
OPTIMUM AOA.
11. IF PERFORMANCE AND FLIGHT CHARACTERISTICS DICTATE THAT A CV
LANDING IS NOT POSSIBLE -- DIVERT.
12. IF DIVERTING WITH A FLIGHT CONTROL MALFUNCTION -- MAKE ARRESTED
LANDING, IF POSSIBLE.
NOTE
IF NORMAL LANDING ROLLOUT IS ATTEMPTED, FLAP HANDLE SHOULD BE
　
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