NAVAIR 0%Fl4AAD-1
. WINO AND TNL WALKERS. AND MAIN LANOINO GEAR CHOCK
DO NOT EXCEED 90D MAXlM”M A”AILABLE NOSE- MEN SHALL BE AYAILABLE AT ALL TIMES DURING TOWING.
WHEEL SW,“EL ANGLE DURING PARKING OR SPOTTING
IN TGHT SPACES: STEERING DAMPER “NIT WILL BE . IN NOSEWHEEL WELL, BRAKE ACCUMULATORS PRESSURE
DAMAGED. GAGE SHALL INDICATE 3,999 psi. ON PILOT CENTER CON.
SOLE. BRAKE PRESSURE INDICATOR NEEDLE SHALL BE
AT RIGHT END OF NX GREEN BAND.
WINGS SHOWN IN 69’
SWEPT POSITION
CENTER PO,
BAR (TILLER BAR, IS REQUIRE
AT NOSEWHEEL FOR
DlRECTlONAL CONTROL
MAlN LANOlNG GEAR TIE DOWN RlNG fZl.
,2O’MAXlM”M AVAILABLE TOW BAR (TILLER BAR) IS REWIRED AT
NOSEWHEEL SWIVEL .4NGLE NOSEWHEEL FOR DlRECTlONAL CONTROL
LEFT OR RIGHT FROM CENTER
3TE
_ _. _ _ . - - TH WNGS IN ANY SWEEP ANGLE
FROM 2o” (UNSWEPT) TO 75” lOVERSWEPT)
TOW TRACTOR
/
MD-SA TOW TRACTOR.
AT-75 TOW TRACTOR, OR
ANYTRACTORUNDER
3 FEET 9 INCHES
,
AIRCRAFT TOW FITTINGS \
INCORPORATED IN LOWER STRUCTURE NT-4 NRCRAFT
OF EACHNACELLE “NIVERSAL TOW BAR
Figure 3-8. Towing
3-17 ORIGINAL
NAVAIR Ol-FWAAD-1
Figure 3-9. Tiedawn Arrangement (Sheet 1 of 2)
ORlblNikL 3-18
NAVAIR 01.Fl4AAD-1
AIRCRAFT TIEDOWN FITTINGS
Figure 3-9. Tiedown Arrangement (Sheet 2 of 2)
3-19 (Reverse Blank) ORIGINAL

NAVAIR 01.FI4AAD-I
CHAPTER 4
Operating Limitations
4.1 LIMITATIONS
This section includes the aircraft and engine limitations
that muat be observed during normal operations.
The aerodynamic and structural limitations in this section
apply only to F-14D aircraft for the store station
configurations shown in Figure 4-l. Engine limitations
apply to all aircraft with the Fl IO-GE-400 engine.
4.1.1 Engine Limits. Engine instrument markings
for various operation limitations are shown in Figure
4-2. Engine operating limitations are shown in Figure
4-3.
The engine secondary (SEC) mode may be intentionally
selected in flight only under the following
conditions:
1. Engine operating between 85-percent ‘pm and
military power
2. Airspeed less than 1 .O TMN.
4.1.2 Starter Limits. The starter cranking limits are
as follows:
1. Cross bleed - 2 minutes.
2. Start cart - 5 minutes.
When the time limit is reached, 10 minutes cooling
is required between cranking.
4.1.3 Airstart Envelope. The engine spooldown
andw indmill airstarte nvelopesa re showni n Chapter1 4,
Figure 14-3.
4.1.4 Crosswind Limits. Crosswind takeoffs and
landings are permitted with a crosswind component not
to exceed 20 knots at 90”.
4.1.5 Ground Operations Limits
1. Maximum tire speed - 190 knots.
2. Maximum canopy open speed - 60 knots
pi-z-1
Use of antiskid must be in accordancew ith
the following procedures:
a. Select antiskid while stopped on the runway in
the takeoff position; after landing, mm antiskid
off once slowed below 15 knots prior to clearing
the runway.
b. Use only during landing or aborted takeoff.
c. Do not use antiskid while taxiing.
4.1.6 Ejection Seat Operation Limits. See ejection
envelope curves, Chapter 16, Figure 16-l.
1. Maximum speed (seat) - 600 knots.
[WPIRNING)
Ejection above 350 knots is hazardous, the
decision to exceed 350 knots rests with the
aircrew.
4.1.7 Autopilot Limits. Autopilot should not be
used under the following conditions:
1. Airspeeds greater than 400 KCAV0.9 TMN
2. Altitude above 42,500 feet.
4.2 AIRSPEED LIMITATIONS
The limits and restrictions in this part represent the
maximum capability of the aircratl commensuratew ith
safeo perationsA. erodynamic and structurale xcesseso f
4-I ORIGINAL
NAVAIR Ol-Fl4AAD-1
I
STORE l-
CONFIGURATION 1A 16 l- 345&6 88 BA
lN*)
1Bl AIM-9 AIM-9 AIM-9 AIM-9
182 AIM-9 AIM-9
1c TANK TANK -
W”) 4 AIM-7
281 AIM-9 AIM-9 4 AIM-7 AIM-9 AIM-9
282 AIM-9 4 AIM-7 AIM-9
2B3 AIM-9 AIM-7 4 AIM-7 AIM-7 AIM-9
284 AIM-7 4 AIM-7 AIM-7
.w*j TANK 4 AIM-7 TANK
2Cl AIM-9 AIM-9 TANK 4 AIM-7 TANK AIM-9 AIM-9
2c2 AIM-9 TANK 4 AIM-7 TANK AIM-9
2C3 AIM-9 AIM-7 TANK 4 AIM-7 TANK AIM-7 AIM-9
2C4 AIM-7 TANK 4 AIM-7 TANK AIM-7
3A(*) 4 AIM-54
3Bi AIM-9 AIM-9 4 AIM-54 AIM-9 AIM-9
3B2 AIM-9 4AIM-54 AIM-9
383 AIM-9 AIM-7 4 AIM-54 AIM-7 AIM-9
384 AIM-7 4 AIM-64 AIM-7
385 AIM-9 AIM-64 4 AIM-64 AIM-54 AIM-9
386 AIM-54 4 AIM-54 AIM-54
3C(‘) TANK 4 AIM-54 TANK
3Cl AIM-9 AIM-9 TANK 4 AIM-64 TANK AIM-9 AIM-9
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：F-14D 飛行手冊 Flight Manual 2