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4. Nose wheelwell:
a. Electrical leads -Connected, No Evidence of
Overheating.
b. Hydraulic lines -No Chafing or Leaks,
c. Doors and linkages -Cotter Pins Installed, No
Distortion.
d. Brake accumulators - 1,900 Psi Minimum.
Figure 7- 1. Exterior Inspection
ORIGINAL 7-2
NAVAIR QMIUAD-1
e. Canopy air bottle gauge - 1,200 Psi Minimum.
f. Emergency landing gear nitrogen bottle gauge
- 3,000 Psi Minimum.
g. Emergency landing gear air release valve -
Ensure That Valve Is in Closed Position.
h. Retract actuator- Piston Clean, No Leaks.
i. Flight maintenance indicator- Secure.
j. Antiskid control box BIT flags-Not Tripped.
k. Cabin pressurep ort screens- Clean.
1. Master arm override - Cover Closed.
5. Nose strut - Piston Clean, Free of Cracks and
Scoring, and Uplock Roller Free.
6. Steering actuator - Secure, No Leaks.
7. Launch bar and holdback fitting
a. Abort - Full Up.
b. Roller - Free Rotation.
c. Uplatch and holdback - Free Movement.
8. Nosewheels and tires - Inflation, No Cuts,
Bulges, Uneven Wear, or Imbedded Objects.
9. Drag brace -No Leaks, Door Secure.
10. Approach lights - Lenses Clean, No Cracks,
Secure.
11. TV camera - Check, Blue Desiccant.
12. Dual chin pod - IRST, TV Cameras (or simulators),
and Anticollision Light Secure.
13. Radome - Lock Handle Fastened, Rosemont
Probe Straight.
14. OBOGS concentrator vent outlet - No
Obstructions.
7.2.8.2 @Right Inlet
1. Ramps, metal seals, and rubber seals - Intact,
Free of Dirt, Grit, and Cracks.
2. IGV-BladesandStatorsFreeofNicksandCmcks.
Plane captain to verify that all visible damage has
been blended.
3. ECS heat exchanger inlet and fan
a. Fan-Free Rotation.
b. Overspeed pin - Recessed.
c. ECS inlet - Free of FOD, Cables Connected
@JN.
4. Inlet-Free of Standing Water, Drains Clear. I
7.2.8.3 @ Right Nacelle and Sponson
1. Station 7 and 8 stores
a. Stores -Aligned.
b. Access panels-Secure.
c. Sidewinder missile launcher
I
(1) LAU-7 Sidewinder coolant doors
Latched.
I
(2) LAU-138 chaff loading and gas bottle
safety handle - Stowed. I
d. Stores safety pins - Installed.
If external t ankMXUdl1 aboard:
e. Ground safety handle-Pulled.
f. Fuel quantity sight gauge -Ball Float Vertical.
g. Sway braces - Tightened Down.
h. Hook latched indicator- White Vertical Line
Visible.
i. Inboard and outboard fuel caps - Fastened
With Butterfly Latch Secured Facing AA.
2. Main wheelwell
a. Doors and linkages - Secure.
b. Uplock microrollers -Free.
c. Uplock hooks - Secure,
d. Hydraulic lines-No Chafing or Leaks.
7-3 ORIGINAL
NAVAIR Ol-Fl4AAD-1
3. Drag brace - Secure, Downlock Safety Pin
Forward.
4. Side brace - Seated in Latch.
5. Main struts - Pistons Clean, Free of Cracks or
scoring.
6. Brakes - Pucks Safety-Wined; 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)
14. Ventral - No Damage, IDG Oil Cooler Intake
Clear.
7.2.8.4 @I Right Glove and Wirig
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.
7.2.8.5 @Aft and Under Fuselage
1. Horizontal tails - Leading Edges Free of Damage.
2. Exhaust nozzles and fakings:
a. Nozzles and fairings - No Cracked or Missing
Flaps or Seals.
9. Gear down microrollers -Contact Made.
10. Engine compartment (ii applicable)
a. Integrated drive generator-transmission fluid
-Fluid Visible, Filter (two) Pins Flush.
b. Engine oil servicing caps-Check.
b. Fairing cable - Properly Tensioned (pull on
cable, fairing flaps should not move).
c. Bottom surface - No Scrapes or Cracks,
d. Spray bars and flameholder - Intact.
c. Bilges-No FOD, Evidence ofOverheating, or
Leakage.
d. Fuel, oil, and hydraulic lines -Free ofchaflng
or Leaks.
e. Turbine blades -No Evidence of Overheating.
3. Fuel vent -No Leakage or FOD.
4. Tailhook
a. Hook point - Smooth.
e. Bleed air lines - No Heat Discoloration or
Damage.
f. Al3 fuel pump filter - Pin Flush.
g. Lube and scavenge bypass filter -Pin Flush.
h. Oil nozzle filter -Pin Flush.
b. Nut and cotter pin - Installed.
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F-14D 飞行手册 Flight Manual 2(14)
