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c. Safety pin - Remove if Hook Is Securely
Latched Up.
5. Backup flight control module -No Leaks (feel
afl of inspection doors), Filter Pins Flush, Close
Both Access Doors.
I 1. Flight hydraulic reservoir - 1,800 Psi Minimum,
Filter Pins Flush. 6. Fuel dump - No Leakage From Mast, Free of
FOD.
12. Flight hydraulic system tape gauge -Minimum
of Seven on Tape. 7. Stations 3 through 6 stores
Note
Engine must be running for an accurate
reading.
13. Hook dashpot pressure gauge - 800 i10 Psi.
ORIGINAL 7-4
a. Stores-Aligned.
b. Access panels - Secure.
c. Stores safety pins - Installed.
NAVAIR Ol-Fl4AAD1
8. Fuel cavity drains -No Leakage.
9. [T] Pod - Check for Security
10. [T] Protective window covers -Removed.
Il. [T] Camera windows - Clean,
12. [T] Camera sensor control - As Briefed.
13. [T] Light meter - Facing Outboard.
14. [T] Lens filter -As Briefed.
7.2.8.6 @Left Glove and Wing
1. Slats, flaps, and cove doors - Surfaces and
Hinges Secure.
2. Wing cavity seal -Free of Cuts and Chafing.
3. Formation and position lights - Intact, Lenses
Clean.
7.2.8.7 @I Left Nacelle and Spot-son
1. Station 1 and 2 racks and stores
a. Racks and stores -Aligned.
b. Access panels-Secure.
c. Sidewinder missile launcher
(1) LAU-7 Sidewinder coolant doors -
Latched.
(2) LAU-138 chaff loading and gas bottle
safety handles - Stowed.
d. Stores safety pins - Installed.
If external tanks aboard:
e. Ground safety handle - Pulled.
f. Fuel quantity sight gauge-Ball Float Vertical.
g. Sway braces-Tightened Down.
h. Hook latch indicator - White Vertical Line
Visible.
i. Inboard and outboard fuel caps - Fastened
With Butterfly Latch Secured Facing Aft.
2. Main wheelwell
a. Doors and linkages - Secure.
b. Uplock microrollers -Free.
c. Uplock hooks-Secure.
d. Hydraulic lines-No Chafing.
3. Drag brace - Secure, Down Lock Safety Pin
Forward.
4. Side brace-Seated in Latch.
5. Main struts - Pistons Clean, Free of Cracks or
Scoring.
6. Brakes- Pucks Safety-Wired; Wear Indicators
Visible (pins at least flush). Lower Torque Arm
Swivel; Key and Key Retainer Properly Installed
and Safety-Wired.
7. Hubcap-Secure, Safety-Wired.
8. Main wheels and tires
a. Wheels and tires - Inflation, Cuts, Bulges,
Uneven Wear, Imbedded Objects (look behind
chocks).
b. Uplock hooks - Secure.
9. Gear-up microrollers - Contact Not Made.
10. Engine compartment (if applicable)
a. IDG - Fluid Visible (two) Pins Flush.
b. Engine oil servicing caps -Check.
c. Bilges -No FOD, Evidenceo f Overheatingo, r
Leakage.
d. Fuel, oil, and hydraulic lines - Free of Chafing
or Leaks.
e. Bleed air lines - No Heat Discoloration or
Damage.
f. Afterburner fuel filter - Pin Flush.
g. Lube and scavenge bypass filter - Pin Flush.
h. Oil nozzle filter - Pin Flush.
7-5 ORIGINAL
NAVAIR Ol-F14AAD-1
11, Combined hydraulic reservoir - 1,800 Psi Minimum,
Filter Pins Flush.
12. Combined hydraulic system tape gauge -Minimum
of Seven on Tape.
Note
Engine must be running for an accurate
reading.
13. Airstart door - Ground Hydraulic and Electric
Covers Tight.
14. Ventral - No Damage, IDG Oil Cooler Intake
Clear.
7.2.8.8 @I Left Inlet
Ramps, metal seals, and rubber seals - Intact,
Free of Dirt, Grit, and Cracks.
IGV - Blades and Stators IGV Free of Nicks and
Cracks.
Plane captain to verify that all visible damage has
been blended.
Ice detector(L) - Secure.
ECS heat exchanger inlet and fan
a. Fan-Free Rotation.
b. Overspeed pin -Recessed.
c. Inlet-Free ofFOD, Cables Connected (two).
5. Outboard spoiler module temperature indicator
and servicing - No Leaks, Fluid Indicator Rod
Protruding.
6. Inlet-Free of Standing Water, Drains Clear.
7.2.8.9 @ Fuselage Top Deck and Wings
1. Bleed exit doors - Free of FOD, Hardware
Intact.
2. ECS heat exchangere xhausts- Free of FOD and
Cracks.
3. Antennas-Check.
4. Overwing fakings -No Cracked or Bent Fingers
5. Eyebrow doors - Intact,
6. Speedbrake- No Distortion or Leaks.
7. Vertical tails and rudders-No Distortion, Lights
Intact.
7.2.8.10 @ Canopy
1. Canopy lanyard - Connected, Yellow Flag
Attached at Both Ends.
2. Auxiliary canopy bottle - Cable Taut.
3. Canopy hooks and seal - Secure, Seal Intact.
4. Ejection seat safe-and-arm device safety pins (see
Figure 7-2) -Pulled.
5. Auxiliary canopy bottle gauge - 800 psi Minimum.
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F-14D 飞行手册 Flight Manual 2(15)
