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10.6
NAVAIR Ol-F’l4AAD.1
PROFILE
ABC 34. AFTC - Check.
a. L ENG select switch - SEC.
L ENG SEC light illuminates; left NOZ position indicator pointer below xero.
b. L J3NG select switch - PRI.
L ENG SEC light goes out, NOZ position indicator to 100 percent.
c. R ENG select switch - SEC.
R ENG SEC light illuminates; right NOZ position indicator pointer below zero.
d. R ENG select switch - PRI.
R ENG SEC light goes out; NOZ position indicator pointer to lOOpercent.
m
Selecting secondary (SEC) mode closes exhaust noxzles,
increasing exhaust nozzle jet wake hazard.
Note
l Performing AFTC check during OBC inhibits AICS
ramps from programming. Ramps must be reset before
another OBC can be performed.
l NOZ position indication is lost in SEC mode.
35. MASTER TEST switch - WG SWP.
Wing-sweep mode switch must be in AUTO.
Wing-sweep program index moves f?om 20’ to 44’ and back to 20’. The following lights
illuminate at start of test and are out at test completion (approximately 25 seconds): WING
SWEEP, FLAP, and REDUCE SPEED.
Note
l During the wing-sweep preflight test, both altimeters
may fluctuate momentarily.
l The WING SWEEP advisoty light illuminates 3 seconds
atIer the test starts, then goes out and illuminates
again 8 seconds into the test.
l The WING SWEEP advisoty light goes out at the end
of the test. The RUDDER AUTH, HZ TAIL AUTH,
and MACH TRIM lights illuminate for the entire test
and remain ilhnninated at the end of the test.
10-7 ORIGINAL
NAVAIR Ql-Fl4AAD-1
PROFILE
A
AB
ABC
ABC
ABC
ABC
ORIGINAL
36. UHF/VHFOTIDS/KS.
Check complete operation of pilot COMM switch - UHF 1, UHF 2, JTIDS, ICS.
37. OBC (autopilot ENGAGE).
fior to running OBC, clear FHF.
a. After ramps are extended - Select Ramps to STOW.
b. Verify RAMP lights go off and INLET lights illuminate.
c. When OBC is complete:
(1) Reset both AICS and check that INLET RAMPS are in AUTO.
(2) Reinitiate complete normal OBC.
(3) Upon completion, record OBC, MCF and FHF.
38. Speedbrake switch.
a. EXT-RET.
b. Verify stabilizers shift 2’ TED (clean) or 3’ TED (AIM-54 rails) on extension and
opposite on retraction (ITS).
39. ECS.
a. AIRSOURCEpushbuttonsshouldbepressed: LENG,RENG,OFF,thenbacktoBOTH
ENG. There will be slight reductioni n flow with single-enginea ir sources elected.T here
should be no excessive interruptions in airflow when source changes are made.
b. Cockpit temperature conhol (TEMP mode selector switch) should be checked in both
MAN and AUTO modes to eosure proper temperature control.
40. Flaps down.
a. Verify stabilizer shifts 3’ TEU (ITS).
41. Flight controls - TRIM.
a. Trim - Full Nose Down (9’ TED).
b. Stick full aft - Check for Free Movement.
c. Trim - FullNose Up (grater than 18’ TEU) (17 to 19 seconds).
d. Stick full forward - Check for Free Movement.
e. Yaw trim - 7O Left to 7O Right (12 to 14 seconds).
f. Trim - Full Left (check 6O differential tail split).
IO-8
NAVAIR 9%FldAAD-1
PROFILE
ABC
ABC
g. Stick full left - Check Power Approach Spoiler Gearing and Uniform Spoiler
Extension.
h. Trim - Full Right (16 to 18 seconds); Check 6O Differential Tail Split.
i. Stick - Full Right; Check Power Approach Spoiler Gearing and Uniform Spoiler
Extension.
42. Flight controls - Cycle.
Observe following:
a. Longitudinal - 33O TEU to 7O TED Horizontal Tail (33” to 10” without ITS).
b. Lateral - 24” Total Differential Tail.
c. Depressa utopilot emergencyd isengagep addle - 14” Total Differential Tail.
d. Directional - 30°Rudder.
e. Longitudinal - Lateral Combined, 35’ TEU to 15” TED.
f. Spoilers - 55’.
43. Spoiler checks.
a. DLC - Check.
(1) Engage DLC. Verify stabilizer shifts 2-3/4” TED. Inboard spoilers extend to
17-l/2”.
(2) Full up DLC. Verify stabilizer returns to trim. Inboard spoilers go to -4-112”.
(3) Full down DLC. Verify stabilizer remains 2-3/4O below trimmed position and
inboard spoilers extend to 55”.
(4) Stick 2 inches left (check spoiler gearing).
(a) Left wing outboard +30”.
(b) Left wing inboard +55O.
(c) Right wing both -4-l/20.
(5) Stick right 2 inches (check spoiler gearing),
(a) Right wing outboard +30°.
@) Right wing inboard +55O.
(c) Left wing both -4-l/2”.
IO-9 ORIGINAL
NAVAIR 0%FI4AAD-1
,ROFlLE
ORIGINAL 10-10
Note
If either right SPOILER position indicator shows one
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F-14D 飞行手册 Flight Manual 2(50)
