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and carrier-based procedures are maintained the
same,e xceptf or the responsere lative to the checks.T he
expanded procedures presented in this flight manual
describe in detail those items that should be checked on
each flight. Adherence to these procedures will provide
the flightcrew with a detailed status of weapons system
performance incident to flight. However, it is incumbent
on the flightcrew to expand the checks as necessaryt o
verify the corrective status of previously reported discrepanciesR.
eferences hould be madet o the functional
checktlightprocedures( Chapter lO,paragraph1 0.2)f or
more detailed tests that can be performed on the aircraft
and weapons systems if deemed necessary. The flightcrew
should be thoroughly familiar with the details of
the procedures outlined herein so that the abbreviated
checklist forms of the procedures may be safely employed.
As the fmt level of simplification, NAVAIR
Ol-F14AAD-1B contains a reprint of the normal procedures,
with less amplifying information.
7.1.1 Tactical Air Reconnaissance Pod System.
A [T] preceding the text of a procedural step
identities items pertaining only to TARPS aircraft.
7.2 EXTERIOR INSPECTION
A proper preflight inspection begins with a thorough
review of aircraft status and past maintenance history.
An understandingo f previous discrepancies,c orrective
action and their impact on the flight can best be gained
at this time. The flightcrew should ensure that any and
all discrepancies have been properly corrected or de- I
ferred prior to accepting the aircraft as ready for flight.
7.2.1 Area Around Aircraft. En route to the aircraft,
attention should be directed to the maintenance
effort going on in the line area. The flightcrew should
ensuret hatn o hazardouss ituationse xist. The entirea rea
should also be generally examined for FOD hazards.
The area around the aircraft that may not be visible
from the cockpit should be examined. Particular attention
should be paid to support equipment adjacent to the
aircraft. It shouldbe determined that the wings and flight
controls can be safely moved and that the effect of jet
blast during start and taxi will not create a dangerous
situation.
7.2.2 Foreign Object Damage and Leak Inspection.
Engine intakes and adjacent deck area are of
prime concern since the Fl lo-GE-400 is highly susceptible
to FOD damage and the engines are capable of
picking up objects from the deck. AICS ramps, bleed
doors, ECS cooling intakes, exhausts, and afterburner
ducts are catchalls for loose objects. They should be
closely inspected for security and foreign objects, Inspect
all panels for security and loose fasteners. While
inspecting the aircraft for FOD, the flightcrew should
also be alert for any evidence of oil, hydraulic fluid, or
fuel leaks.
7.2.3 Ground Safety Devices and Covers. The
following items should be installed:
1. MLG ground safety locks (two)
2. Nose landing gear ground safety pin
3. Tailhook safety pin (ashore)
4. Wheel chocks
5. LAU-7/LAU-138/LAU-92 ground safety pins
6. Sidewinder seeker-headc overs (if applicable).
7-l ORIGINAL
NAVAIR Ol-F14AAD-1
The following items should be removed:
1. Intake, probe, bleed door, and ECS duct covers
2. Water-intrusion tape
3. Launch abort mechanism lock (if the aircraft is to
be towed)
4. Tailhook safety pin (shipboard).
7.2.4 Surface Condition. All surfaces should be
checked for cracks, distortion, or loose or missing fasteners.
All lights and lenses shouldbe checked for cracks
and cleanliness.
7.2.5 Security of Panels. All fasteners should be
flush and secure on all panels.
7.2.6 Leaks. All surfaces,l ines, and actuatorss hould
be checked for oil, fuel, and hydraulic leaks. Particular
attention should be paid to the underside of the fuselage,
engine nacelles, and outer wing panels.
7.2.7 Movable Surfaces. All movable surfaces
(flight controls and high-lift devices) should be inspected
for position, clearance, and obvious damage,
7.2.6 Inspection Areas. The following exterior inspection
is divided into 10 areas. (See Figure 7-l.)
Checks peculiar to only one side are designated (L) or
(R) for the lefl or right side. Both the pilot and RIO
should preflight the entire aircraft individually.
7.2.6.1 @ Forward Fuselage
1. Access panel fasteners forward of engine inlets -
No Loose or Missing Fasteners.
2. Gun (L) - Safety Pin Installed in Clearing Sector
Holdback Assembly, Louvers Clear.
3. Probes - Secure, Openings Clear, AOA Probe
Free For Rotation.
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F-14D 飞行手册 Flight Manual 2(13)
