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g. Cycle AICS cb’s at a constant subsonic Mach.
10.3.7 10,000.Foot Check
AB 55. OXYGENmonitor - TEST.
Note
The TEST button must be held for up to 1 minute to vent oxygen tirn the monitor oxygen
sensor,O ncet he monitor sense3in suflicient oxygen concentmtio~ the cockpit caution lights
will be illminated and oxygens upplys ouxe shiftedt o BOS. Releaseth e TEST buttona s soon
as the OBGGS light is -ted. Verify OBGGS light extinguishedw ithia 20 seconds.
I,,,,,,,(
The monitor will fail without any indication to the aircrew.
For this reason, it is essential that the pilot test the
monitor function prior to launch and prior to ascending
above 10,000f eetM SL. Ifthe aircrew suspectst he onset
of hypoxia at any time, immediately select BACKUP.
Themonitormaybetestedoncetheaircrafthasdescended
to a maximum cabin altiti of 10,000 feet by reselecting
ON on the OBGGS master switch.
IO-13 ORIGINAL
NAVAIR 0%F14AAD-I
‘ROFILE
LBC
LB
ORIGINAL
56. Fuel transfer - Check
57. ECS check (250 knots).
In CV environment, eusure external tanks are empty
prior to ECS checks.
ECS check should be performeda t altitudea bove 8,000 feet so cabin pressurizationc an be
checked,b ut low enought o preventl arge cockpit pressmec hangesw hen cockpit air is secured.
a. Cabin altitude approximately 8,000 feet.
b. Air distribution - CANOPY DEFOG-CABIN AIR.
c. Radar power switch - STBY (coordinate with RIO).
d. AIR SOURCE pushbutton - OFF.
Cockpit pressurization will quickly bleed off with cabin pressure altimeter moving
upward toward aircratl altitude.
m
Oxygen breathing time on BACKUP is limited.
Note
l When ECS service air to the OBOGS concentrator
is shut off, the aircrew has approximately 30 seconds
before depleting residual OBOGS pressure
and mask collapse.
l Restoration of service air (selecting RAM) will return
OBOGS to operation.
e. CABIN PRESS switch - DUMP.
Cockpit will completely depressurixe.
f. RAM AIR switch - INCR (35 to 50 seconds).
As ram air door opens( up to 50 secondst o openf ully), therew ill bean increasei n cockpit
airflow.
g. AIR SOURCE pushbutton - RAM.
With RAM selected, 400° manifold is repressurized, which maintains canopy seal,
airbags, and antenna waveguides pressurization. As canopy seal reinflates, cockpit pressurization
available from ram air will be much more apparent.
IO-14
h. CABINPRESS switch - NORM.
i. AIR SOURCEp ushbutton- BOTH BNG.
j. Radarp owers witch - XMIT (Coordinatwe ith RIO).
58. MFD OBC TEST - Select.
103.8 lS,OOO-Foot Checks
59. stab&e at 300 knots.
a Full stick roll - SAS OFF-ON.
Note Cdl extensiono f down-wings poilersS. ASon roll acc&mtion will be slightly
higherb ecausoef increasehdo rizontatla il authority.
b. Pit&pulse - SAS OFF-ON.
At slows peedsp,i tch SASO FFi s hardlyn oticeableL.a cko f pitch SASb ecomems ore
apparenat ss peedin creases.
c. Rudderp ulsele ft aadr ight - SASO FF-ON.
Yaw excursionssh ouldc easeim mediateluyp one ngagemeonft YAW STAB.
60. wii-aweq andmaneuvedre vices(c hecka t 0.5M ach).
a Maneuverdevi~s - EXTD.
b. Wiigaveep switch - AFT (check that wings stop at 500).
c. Maoeuvefrl apsp artialu p with thumbwheeEl. nsureth at devicesre tract.
d. Wing-sweepsw itch - BOMB.
(1) Verify maneuvedr evicesa utomaticallrye tracta ndt henw ingss weepto 55’.
c. Wmgaweep switch - MAN FULL AFT.
f. Wing-sweespw itch - AUTO.
g. EmergencWy ING SWEEPh aodle- Cycle 22’, -68’. -22”.
(1) Verify spiderd etente ngage emergencWy ING SWJIEPc autiono ff..
(2) MASTERR ESETp ushbutton- Depress.
CheckW ING SWEEPa dvisoryli ghto ff.
h. Maneuvedr evices- EXTD.
i. Accelerateto greatert han 0.79 Macha ndc heckm aneuvedr evicesa utomaticallrye -
tmeted( maneuvedre vicess tarta utomatirce tractiona t 0.68a .02 Mach).
10-15 OUIGINAL
NAVAlR 0%F14AAO-1
PROFILE
ABC
ABC
ABC
ORIGINAL
j. Deceleratteo lesst han0 .68M acha ndc heckm aneuvedr evicesre mainr etracted.
k. Wing-sweespw itch - AUTO.
61. ASYM LIMITER switch - Check( airspee3d 00k nots).
a. Throttles - MlLorLess.
b. ASYM LIMITER switch - OFF.
c. L&throttle - MAX AS.
Observe1 11A R available.
d. ASYM LJMITER switch - ON.
Observere ductionto min AR (12p ercent).
e. Repeast tepsa throughd for right engine.
62. High AOA AUTO MAN devices.
a. Roll SAS - OFF and ALPHA COMP cb (RBl) In.
b. Throttles - IDLE.
c. Slowlyi ncreasaei rcragA OA anda llowa ircraftt o stabilizem; aneuvedre vicese xtenda t
10.5 units AOA.
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F-14D 飞行手册 Flight Manual 2(52)
