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position highor then actual spoiler position (that is, DN
vice drooped and extended vice DN), e spoiler zero-degree
switch has failed. Spoiler symmebyprotection circuitry
is inoperative and spoiler ground-roll braking in
flight is possible.
b. SPOILERBK - Select.
c. SPOILER FLR ORIDE operation.
(1) INBD end OUTBD SPOILER FLR ORIDE switches - ORIDE.
(2) MASTER TEST switch - STICK SW.
(3) Verify all spoilers remain extended (559.
(4) INBD end OUTBD SPOILER FLR ORIDE switches - NORM
Verify INBD and OUTBD spoilers fait down and SPOILER light illuminates.
m
With SPOILER FLR ORIDE switches in ORIDE,
spoiler symmetry protection circuitry is disabled. Ensure
that switches are in NORM.
(5) Verify spoilers down.
(6) MASTER TEST switch - OFF.
(7) MASTERRESET - Depress.
d. MASTER TEST switch - STICK SW.
(1) Verify GO light illumioates with l-inch lateral stick inputs left and right.
(2) MASTER TEST switch - OFF.
(3) MASTERRESET - Depress.
Verify SPOILER light goes out and all spoilers extend to 55’.
e. SPOILER BK/THROTTLE inte.rlocks - Check
44. Displays - CHECK.
45. Tacan - BIT.
46. ARA-63 - BIT.
Check HUD, VDI, and standby gyro needles.
NAVAIR Of-FMAAD-1
PROFILE
A
AB
A
ABC
AB
47. Gunsight - Verify (manual mode).
a. Select A/A.
b. Select GUN.
c. Select manual mode via CAGE/SEAM switch.
d. Dial in 34 mils. Verify the manual reticle is positioned over the HUD heading tick
48. Autopilot emergency disengage.
a. Paddle switch - Hold Depressed.
b. Verify throttles in manual mode.
49. OXYGEN Monitor - TEST.
The TEST button must be held for up to 1 minute to vent oxygen from the monitor oxygen
sensor.O ncet he monitor sensesin sufficient oxygen concentration,t he cockpit cautionl ights
will be illuminated and oxygen supply source shifted to BOS. Release the TEST button as
soon as the OBOGS light is illuminated. Verify OBOGS light is extinguished within 20
seconds.
The monitor will fail without any indication to the aircrew.
For this reason,i t is essentiatl hat the pilot testt he
monitor function prior to launch and prior to ascending
above 10,000 feet MSL. If the aircrew suspects the
onset of hypoxia at any time, immediately select
BACKUP. The monitor may be tested once the aircraft
has descendedt o a maximum cabin altitude of 10,000
feet by reselecting ON on the OBOGS master switch.
Note
The monitor can take up to 2 minutes to warm up, dcpending
on the ambientt emperature.T he OBOGS light
will not be illuminated during the warmup period.
10.3.4 Taxi
50. Turn needle/slip indicator - Check.
10.35 Engine Runup
51. Engine runup - Check.
10-11 ORIGINAL
ROFILE
Onb oards hip,u seo f MRT andM IN AB is restrictedto
s amimum of 30 secondsto preventd amageto the
holdbackb ar andt heJ BD.
NO2 position (%) AT MIL
OIL (PSI)
RPM (%)
EGT (‘C)
FF (PPH)
Lafl Right Llmlts
clod nominal 3 to 10
25to65
95 to 104 nominal (107.7 maximum)
935’
9,ooo to 12,000
s. Verify hooki s stoweda ndR ATSl ighti s out.
b. Righte nginem ode- SEC.
c. Rightthmttle - ME.
Notea cceleratiotnim e (lessth an 10s econds).
d. Righte nginem ode- PRI.
Recorde nginep arameters.
e. Hook - DOWN.
Verify RATSl igbta nd3 -to 6-percenrtp m decay.
f. Right throttle - MIN AB.
Verify rpm increase3s to 7 percent.
g. THROTTLEMODEswitch - MAN.
h. Rigbttluottle - IDLE.
i. THROTTLE MODE switch - BOOST.
j. Hook-UP.
Verify hook is stowed and, RATS light is out.
k. Repeast tepsb throughj with left engine.
ORIGINAL 1012
NAVAIR 0%FMAAD-I
PROFILE
10.3.6 Takeoff and Climb
A
A
AB
52. Landing gear - Retract (9 to 15 seconds nominal).
53. Barometer and radar altimeters - Check Below 5,000 Feet.
54. AFTC - Check.
l SEC mode transfer while in minimum AB may result
in pop stalls. Nonemergency manual selection of
SEC mode airborne should be performed in basic
engine with the power set above 85-percent RPM.
l If the fan speed limiter circuit has failed, engine rollback
may occur with the selection of SEC mode. In
the event of engine rollback, PRI mode most be rese=
lected above 59-percent rpm or flameout will occur
and an airstart will not be possible.
a. LENGmodeswitch - SEC.
b. Left throttle - Check Basic Engine Power Response.
c. L BNG mode switch - PRI.
d. R ENG mode switch - SEC.
e. Right thmttle - Check Basic Engine Power Response.
f. R ENG mode switch - PRI.
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F-14D 飞行手册 Flight Manual 2(51)
