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aircraft (conditions permitting) via the nose strut switch
will facilitate a safer exit for the aircrew. If sufficient Failure of the letI or right WOW switches to
time does not exist for ground personnel to deploy the the in-flight mode can cause loss of engine
boarding ladder, aircrew should egress to the rear of the ejecior air to the ID& and hydraulic heat
aircraft, over the horizontal stabilizers or wings, or di- exchangers causing thermal disconnect
rectly to the deck from the cockpit if the tail is over and/orh eat damaget o the generatorsa nd aircraft
hydraulic systems.
\
\
water. In the case of fne, the location and intensity of
the fne will dictate the safest escape mute. If electingto
egress directly t?om the cockpit, aircrew should grasp
the canopy rail with both hands, hang to full body extension,
a nd drop to the ground.A parachute-landingfa ll
maneuver may be required to minimize risk of injury.
Spacing of pitot static probes along both sides of the
fonvard fuselage will allow for an unobstructed egress.
Standing and jumping from the cockpit or
attempting to slide down the nose of the
aircraft during ground egress can result in
severe injury.
If the ENG/PROBE ANTI-ICE switch is
in the ORIDE position, touching the pitot
probes with bare skin will cause burns.
1. Kneel aircraft (if possible).
2. Canopy-OPEN or JETTISON
I
3. Parking bmke - Pull.
1. PUSHBUTTON TO OPEN DOOR.
2. SQUEEZE T-HANDLE AND
PULL TO JETTISON CANOPY.
NORMAL COCKPIT EN lRANCE
I
I
T
E
T
NAVAIR Ol-Fl4AAD-1
Figure 12-l. Emergency Entrance
NAVAIR Of-Fl4AAD-I
12.1.7.1 Failure Of Weight On-Off Wheels to
In-flight Mode
INDICATIONS:
1. WOW acronym displayed
2. Approach indexers illuminated.
3. Nozzles may be partially closed at idle rpm.
4. Nosewheel steering inoperative.
5. Launch bar light illtinatcd (if nosegear turned
>lOO).
6. Ground-roll braking inoperative.
7. Wing-sweep MASTER TEST disabled.
8. Oversweep disabled.
9. OutboardspoilermoduleonwithFLAPhandleUP
(wings less than 62’).
10. Aircraft will not kneel.
If two or more of the preceding anomalies are detected,
the following action should be taken:
1. Clear runway (if applicable).
2. Generators- OFF.
3. Throttles - OFF (after downlocks are in place).
Failure of the lefl or tight WOW switches to
the in-flight mode can cause loss of engine
ejector air to the IDGs and hydraulic heat
exchangers causing thermal disconnect
and/or heat damaget o the generatorsa nd aircratt
hydraulic systems.
1. RDR switch - OFF.
(,,,,,I
With faihne. of the WOW switch to the inflight
mode, the following l%nctions are enabled
a. Radarcanscanandradiate.
b. ALQ-165 can transmit.
c. Probe heaters will be on in AD-TO.
d. ALQ-167 can radiate (TARPS).’
e. BOL chatTcan dispense.
12.1.8 Binding/Jammed FllgM Controls On
Deck
1. Holdlightpmssumagaimtbindh@mshictiontothcilitate
maintenancetr oubleshootingp mce&ma.
m
Do not attempt to free controls by force, as
further damage to Sight control syatemmay
fMllt.
2. Abort mission.
12.1.9 Brake Failure at Taxl Speed
*l. ANTISKID SPOILER BK switch - SPOILER
BK or OFF.
2*. NWS - Verify Engaged
3.* Parking bmke - PULL (if requhed) (applying
parking brake will lock both main wheels.)
pi&-)
Complete loss of hydraulic fluid through the
wheelbrake hydraulic lines will render the
parking brake ineffective.
If brakes still inoperative:
4. Hook - DN.
NAVAIR Ol-Fl4AAD-l 7
\L
7. Both throttles-OFF (If required).
If collision imminent, DO NOT delay step 7.
After lowering the hook, NWS will automatically
center and will remain centered until
NWS is cycled.
p&G-)
5. Lights-ON. During shipboard operations, aircrew should
6. Notify ground and/or tower.
not delay ejection decision if aircraft departure
t?om flight deck is imminent.

NAVAIR 0%F14AAD-1
CHAPTER 13
Takeoff Emergencies
13.1 ABORTED TAKEOFF
Emergencies during takeoff are extremely critical
and require fast analysis and quick decision by the pilot.
The decision to abort should not be delayed just because
emergency arresting gear is available at the end of the
runway. Whether to abort or continue the takeoff deponds
on the length of runway remaining, refusal speed,
best single-engine climb speed, and the arresting gear
available. Failure of either engine, a fm warning light,
or a blown tire during takeoff dictates an immediate
　
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