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Turns into the wingman will not be made at altitudes less
than 500 feet above ground level.
7.4.9.2 Wingman. The wingman should strive to
matcht he leader’sa ttitudea sw ell asm aintainp aradeb earing
with wingtip separationW. hen both aircratla res afely
airborne,t he geari s retractedo n signal tiom the leader
In the event of an aborted takeoff, the aborting
aircraft must immediately notify the
other aircraft and the tower. The aircraft not
aborting should ensure positive wingtip
separation is maintained and select till militarypower
to acceleratea heado fthe aborting
aimaft. This will allow the aborting aimrat?
to move to the center of the runway and engage
the available arresting gear, if required.
7-21 ORIGINAL
It is imperative that the wingman be alert for
the ove.mmning situation and take timely action
to preclude this occurrence. Should an
overrunning situation develop after becoming
airborne, the wingman should immediately
increase. lateral separation l?om the
leader to maintain wing position. Safe flight
ofbothaircmftmuatnotbejeopardizedinan
attempt to maintain position.
7A.10 TakeoffAborted. See Chapter 13, paragraph
13.1.
7.4.11 Takeoff Checklist. Prior to takeoff, the
checklist will be completed by the challenge (RIO) and
reply (pilot) method via the ICS on HOT MIC as a
double-check of the aircrafi configuration status.
For CV operations, steps 1 through 9 may be completed
while tied down. For field operations, stops 1
through 15 should he completed in the warmup area.
RIO CHALLENGE
1. ‘BRAKES”
2. ‘FUEL TOTAL
lb.’
3. ‘CANOPY CLOSED,
LOCKS ENGAGED,
LIGHT OUT, STRIPES
ALIGNED. HANDLE
IN CLOSE POSITION’
I 4. ‘SEAT. ARMED,
STRAPPED IN EIGHT
WAYS COMMAND
EJECl- (as b&fed)
5. “STAB AUG
6. -ATLS’
7. ‘ALL CIRCUIT
BREAKERS SET”
PILOT REPLAY
‘CHECK OK,
ACCUMULATOR -
PRESSURE Up”
‘NORMAL FEED,
AUTO TRANSFER,
DUMP OFF.
TRANSFEd
CHECKED (if AUX
tanks cmied). TOTAL,
~~;D~E~PP.)
FORWARD AND
RIGHT FEED TANKS
FULL BINGO SET-’
‘CLOSED, LOCKS
ENGAGED, LIGHT
OUT, SEAL
INFLATED. HANDLE
IN CLOSE POSITION
‘ARMED, STRAPPED
IN EIGHT WAYS,
PILOT/MC0 IN
WINDOW (as
indicated)
%LL ON
“ALL IN’
RIO CHALLENGE PILOT RESPONSE
0. ‘MASTER TEST ‘OFF”
SWITCH
9. ‘BI-DIRECTIONAL’ ‘NORMAL’
10. ‘INBD AND OUTBD ‘ORIDE”
SPOILER FLR ORIDE
SWITCHES
11. ‘COMPASS AND ‘ALL HEADINGS
STANDBY GYRO MATCH, STANDBY
GYRO ERECT’
12. ‘OXYGEN
CV - APPROACHING
CAT ON DIRECTOR’S SIGNAL
13. WINGS (visually 20’, AUTO, NO
checked) WING-SWEEP CAWs.
14. ‘FiAPS AND SLATS
(visually checked)
As REQUIRED
15. ‘SPOILERS AND
ANTISKID’
‘SPOILER MODULE
ON, SPOILER BRAKES
SELECTED” (field)
‘SPOILER MODULE
ON. SPOILER
BRAKES OFF (CV):
16. 7RIM
17. ‘SAHRS ATTITUDE
REFERENCE
10. ‘DISPLAYS
19. ‘HARNESS LOCKED’
20. ‘CONTROLS” (RIO
visually check for full
spoiler deflection)
21. ‘ALL WARNING AND
CAUTIONS OUT
‘0.0.0: @Id) AS
REQUIRED (Cv)
‘GOOD SAHRS
ATTITUDE’
SET FOR TAKEOFF.
HUD CAGED’
‘LOCKED’
‘FREE, STICK FULL
FORWARD AND AFT.
FULL SPOILER
DEFLECTION, LEFT
AND RIGHT,
HYDRAULICS 3,000
PSI
ILL WARNING AND
CAUTIONS OUT
ASHORE - IN TAKEOFF POSlllON
22. ‘ANTISKID/ ‘BOTH” (if operable)
SPOILER BRAKES
ORIGINAL 7.22
NAVAIR 01.F14AAD.1
7.4.12 Ascent Checklist. At level-off or 15,000
feet (whichever occurs fmt):
1. Cabin pressurization - Check.
2. Fuel transfer-Check.
3. In-flight OBC - Run.
4. Oxygen monitoring system-Test.
1 WARNING 1
Subsequenfta ilure of the oxygenm onitor system
will not be evident to the aircrew resulting
in OBOGS output of unknown quality.
Note
Pilot should ensure oxygen monitor test button
is released as soon as possible after illumination
of the OBOGS caution light to
preclude unnecessary depletion of the
backup oxygen system.
7.4.13 In-Flight OBC. If desired or required OBC
check should be run.
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F-14D 飞行手册 Flight Manual 2(25)
