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III-7-5 ORIGINAL
e. Light/antenna radomes - CHECK CONDITION
(1) Tail light (top)
(2) ALQ-165 low/high band receiver (middle)
(3) ALR-67 receiver (bottom)
f. Dump outlet - CLEAR
g. Stabilator - CHECK CONDITION
h. Exhaust nozzle and afterburner section - CHECK CONDITION
13. Arresting hook area
a. Arresting hook - CHECK CONDITION (make sure cotter key installed in hook point attach
bolt).
b. Arresting hook pin - REMOVED
c. Towed decoy stand-off bar (when installed) - CHECK CONDITION
14. Aft fuselage (left side)
a. Exhaust nozzle and afterburner section - CHECK CONDITION
b. Stabilator - CHECK CONDITION
c. Vertical tail and rudder - CHECK CONDITION
d. Antenna radomes - CHECK CONDITION
(1) ALQ-165 high band transmitter (top)
(2) ALQ-165 low band transmitter (middle)
(3) ALR-67 receiver (bottom)
e. Dump outlet - CLEAR
f. Strobe light - CHECK CONDITION
g. Fuel vent outlet - CLEAR
h. Hydraulic reservoir gauge - CHECK IN THE GREEN OR ABOVE
15. Aft fuselage (underside)
a. APU intake (screened) and exhaust ducts - CLEAR
b. ATS exhaust ducts (screened) - CLEAR
A1-F18EA-NFM-000
III-7-6 ORIGINAL
c. ALE-50 dispenser - CHECK CONDITION (make sure live or protected magazine installed)
16. Left main wheelwell
a. Hydraulic filter indicators (delta-Ps) - NOT POPPED
b. Doors and linkages - CHECK CONDITION
c. Landing gear downlock and retract actuators - CHECK CONDITION
d. Landing gear pin - REMOVED
17. Left wing
a. TEF - CHECK CONDITION
b. Aileron - CHECK CONDITION, FAIRED WITH WINGS FOLDED
If the wings are folded, note the position of the ailerons. If the aileron
locking pins do not restrain the ailerons in the faired position, ensure the
ailerons are moved to a faired or outboard position prior to engine start
to preclude damage to the ailerons and TEFs.
c. Wingtip AIM-9 (if installed) - PREFLIGHT
d. Position lights - CHECK CONDITION
e. Wingfold area - CHECK CONDITION AND VERIFY WINGFOLD PIN REMOVED
f. Pylons and external stores - PREFLIGHT
g. LEF - CHECK CONDITION
h. Flush LEF antenna (ALR-67/ALQ-165 receivers) - CHECK CONDITION
18. Left main landing gear
a. Tire and wheel - CHECK CONDITION
b. Brake wear indicator - EXTENDED (not flush or below flush)
c. Planing link - CHECK CONDITION
d. Strut - CHECK CONDITION
e. Tiedown rings (2) - CHECK SPRING CONDITION
19. Station 5 missile or TFLR (if installed) - PREFLIGHT
A1-F18EA-NFM-000
III-7-7 ORIGINAL
20. Forward fuselage (left side)
a. Chaff/flare dispensers (2) - PREFLIGHT (ensure chaff/flare buckets or access covers
installed).
b. Left engine intake - CLEAR
c. Heat exchanger ram air inlet (top, inside intake) - CLEAR
d. Fuel cavity drains (underside) - VERIFY NO LEAKS
e. Loose fasteners - CHECK
f. Flush LEX antenna (ALQ-165 low/high band transmitter) - CHECK CONDITION
7.1.4 Before Entering Cockpit.
1. Boarding ladder - SECURE (2 points)
2. Fuselage (upper surface)
a. Spoilers - CHECK CONDITION
b. Upper blade antenna (Comm 1, DL, TCN) - CHECK CONDITION
c. ECS auxiliary duct doors - CHECK DOWN/CONDITION
3. Over-the-shoulder cameras (2) - CHECK SECURE
4. CVRS tapes - INSTALL IN RECORDERS (if desired)
5. EMI shields (covers over bay behind ejection seat) - CLOSED/SECURED
Ensure the EMI shields are properly closed and secured prior to closing
the canopy to prevent damage to the shields and the canopy actuation
link.
6. Ejection seat SAFE/ARMED handle - SAFE
7. Ejection seat(s) - PREFLIGHT
a. Manual override handle - FULL DOWN and LOCKED
b. Right pitot - STOWED
c. Ballistic gas quick-disconnect - CONNECTED (indicator dowel flush or slightly protruding)
A1-F18EA-NFM-000
III-7-8 ORIGINAL
d. Top latch plunger locking indicator - FLUSH WITH THE END OF THE PLUNGER
If the top latch plunger locking indicator is not flush, the seat could come
loose on the mounting rails.
e. Catapult manifold valve - CHECK (hoses and manifold connected; retaining pin installed)
f. Parachute withdrawal line - CONNECTED/SECURED
g. Parachute container lid - SECURE
h. Left pitot - STOWED
i. Electronic sequencer - NOT ACTIVATED
(1) Indicator should be BLACK (not activated).
(2) White is UNSAT (activated).
j. Thermal batteries - NOT ACTIVATED
(1) Indicator should be WHITE or PINK (not activated).
(2) Black or purple is UNSAT (activated).
k. Console oxygen/comm lines - CONNECTED/SECURED
l. Survival kit - CHECK
(1) Oxygen/comm lines - CONNECTED/SECURED
(2) Emergency oxygen gauge - IN THE BLACK
(3) Seat pan - CHECK SECURED TO SEAT (pull up on front end to test security).
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本文链接地址：
NATOPS Flight Manual 飞行手册 1(130)
