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the MASTER RESET pushbutton) and the PITCH
and ROLL STAB AUG switches will be OFF.
4. Advise RIO that test and check is completed.
5. STAB AUG switches-All On.
6. AFTC -CHECK.
a. L ENG mode switch - SEC.
L ENG SEC light illuminates; left NOZ indicator
pointer below zero.
b. L ENG mode switch - PRI.
L ENG SEC light goes out; NOZ indicator to
100 percent.
c. R ENG mode switch - SEC.
R ENG SEC light illuminates; right NOZ indicator
pointer below zero.
d. R ENG mode switch - PRI.
R ENG SEC light goes out; NOZ indicator
pointer to 100 percent.
Selecting secondary (SEC) mode closes exhaust
nozzles increasing exhaust nozzle jetwake
hazard.
Note
Performing AFTC check during OBC inhibits
AICS ramps from programming.
Ramps must be reset before another OBC
can be performed.
Operating engines in secondary mode inhibits
the engine monitoring system portion
of FEMS until primary mode is
reselected.
7. Emergency WING SWEEP handle - OV SW.
If wings are not in oversweep, move the wings to
68’ using WING SWEEP emergency handle in
raised position. Then raise handle to full extension
and hold until HZ TAIL AUTH caution light goes
out and OVER flag appears on wing-sweep indicator.
Move handle to full aft OV SW and stow.
8. Wing-sweep switch - AUTO.
9. WING SWEEP DRIVE NO. 1 and WG SW DR
NO. 2/MANUV FLAP cb’s -IN (LDl, LET)
10. WING/EXT TRANS switch - OFF.
11. MASTER RESET pushbutton - Depress.
12. OXYGEN SUPPLY valve-ON.
Turn OXYGEN SUPPLY valve ON, place mask
to face and check for normal breathing and regulator
and mask operation. Turn OXYGEN SUPPLY
valve OFF, check no breathing.
13. COMM/NAV/GEAR/DISPLAYS - ON.
a. UHF MODE switch - T/R or T/R & G.
b. Tacan function selector - T/R.
c. MFDs -ON.
d. ARA-63 POWER switch -ON.
e. HUD PWR switch-ON.
f. Radar altimeter - ON.
g. VIDEO control switch - ON.
14. Trim -Set 000.
15. Standby gyro-Erect.
16. MASTER RESET pushbutton - Depress.
17. MASTER TEST switch - OBC.
Coordinate with RIO and plane captain.
Increaseds uction aroundi ntakesd uring inlet
ramp programming and the automatic movement
of the horizontal stabs presents a FOD
hazard and the potential for injury to ground
personnel not clear of these areas.
ORIGINAL 7-14
NAVAIR 01.F14AAD-1
18. Autopilot-Engage.
19. Failure history tile - Clear.
20. MFD OBC TEST -Select.
The following systems are automatically exercised
during the l-1/2 minutes required to complete
the OBC tests.
a. The AICS self-test turns on hydraulic power
and exercises the ramps through full cycle:
STOW-EXTND-STOW. During the test, the
respective RAMP light illuminates until the
ramps return to the fully stowed position and
the hydraulics are shut off. A failure is indicated
by an INLET light and/or OBC readout.
b. Pitch, roll, yaw stab aug; authority stops;
AFCS computers; Mach trim compensator;
autopilot, spoiler.
During the course of the test, the STAB AUG
lights remain illuminated until the test is satisfactorily
completed. All lights should be off at
termination of test.
OBC commencement with nose-down trim
may result in a force-link disconnect when
the stick hits the forward stick stop during the
pitch parallel actuator checks.
a. Autothrottle - This test is a computer self-test
with output commands inhibited to prevent
throttle movement.
21. Speedbrake switch - EXT, then RET. Cycle
speedbrakes witch to EXT, releasea nd check for
partial extension. Select EXT again, checking indicatorfortransition
for full extension. Select RET
and check indicator for an indication of full retraction.
Check for stabilizer position fluctuation during
speedbrakee xtension and retraction to verify
integrated trim operation.
22. REFUEL PROBE switch - All EXT, Then RET.
Cycle the probe to the extend position, noting illumination
ofthe probe transition light with switchprobe
position disparity. Check probe nozzle head
for condition, Retract probe and again check that
transition light goes out when fully retracted and
doors closed.
23. WSHLD AIR switch - Cycle.
24. MASTER TEST switch -OFF.
If engaged, verify that autopilot disengages
automatically.
25. WING/EXT TRANS switch-OFF.
26. Trim - Checked and Set 000.
Ensure adequate clearance before moving
wings.
Note
For CV operations,o mit steps2 7 through4 7.
27. Emergency WING SWEEP handle - 20”.
Move the emergency WING SWEEP handle to
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F-14D 飞行手册 Flight Manual 2(20)
