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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 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：F-14D 飞行手册 Flight Manual 2
