F-14D. FLIGHT MANUAL (2004)

NAVAIR 01-F14AAP-1B

ABORTED TAKEOFF

TAKEOFF

*1. Throttles .

IDLE

*2. Speedbrakes .

EXT

*3. Stick .

Aft

Note

The stick should be positioned fully aft

at a rate that will not cause any more

rotation.

*4. Hook .

DN (1,000 feet before wire)

*5. Brakes .

As Required

*6. Right engine .

OFF (if required)

CAUTION

Aircrew should expect hot brakes

following heavy gross weight, high-

speed aborts. Application of the park-

ing brake could cause the brake

assembly to fail and result in a brake

failure.

Note

If performing no flap/maneuvering flap

takeoff, lowering the flap handle

slightly during an abort will deploy all

spoilers for ground roll braking if SPL

BK or BOTH is selected, assisting in

decelerating the aircraft.

Change 2

187

NAVAIR 01-F14AAP-1B

BLOWN TIRE DURING TAKEOFF

TAKEOFF ABORTED OR AFTER LANDING

TOUCHDOWN

*1. Nosewheel steering .

Engaged

*2. ANTI SKID SPOILER BK .

SPOILER BK

CAUTION

D Do not delay engaging nosewheel

steering in order to center rudder

pedals.

D Aircraft should have ground locks

installed and engine secured before

moving aircraft.

TAKEOFF CONTINUED OR AFTER LANDING

GO-AROUND

*1. Throttles .

As Required

*2. Landing gear and

flaps .

Leave as Set for Takeoff

3. HYD ISOL switch .

FLT

Note

This will require bending the cam on

the gear handle in order to move the

HYD ISOL isolate switch to FLT.

4. Refer to Blown Tire Landing procedures.

188

NAVAIR 01-F14AAP-1B

BINGO

Note

During descent with engines in PRI mode,

advancing throttle(s) slightly to partially

closed nozzle(s) will increase range.

Drag Table

190a

Weight Table

190c

Gear Up/Flaps Up (48,000) — Two Engines

191

Gear Up/Flaps Down (48,000) — Two Engines

192

Gear Down/Flaps Up (48,000) — Two Engines

193

Gear Down/Flaps Down (48,000) — Two Engines

194

Gear Up/Flaps Up (48,000) — Single Engine

195

Gear Up/Flaps Down (48,000) — Single Engine

196

Gear Down/Flaps Up (48,000) — Single Engine

197

Gear Down/Flaps Down (48,000) — Single Engine

198

Gear Up/Flaps Up — Wings 68_ (48,000) —

Two Engines

199

Gear Up/Flaps Up — Wings 68_ (48,000) —

Single Engine

200

Gear Up/Flaps Up (53,000) — Two Engines

201

Gear Up/Flaps Down (53,000) — Two Engines

202

Gear Down/Flaps Up (53,000) — Two Engines

203

Gear Down/Flaps Down (53,000) — Two Engines

204

Gear Up/Flaps Up — Wings 68_ (53,000) —

Two Engines

204a

Gear Up/Flaps Up (48,000) — Two Engines

Extended Range

204b

Gear Up/Flaps Up (53,000) — Two Engines

Extended Range

205

Change 3

189/(190 blank)

NAVAIR 01-F14AAP-1B

DRAG TABLE

DRAG INDEX

STORE

STATION(S)

(PER STATION)

OPEN AIM−7 CAVITIES (CLEAN)

3, 4, 5, 6

5 (TOTAL)

AIM−7

3, 6/5, 4

2, 2/2, 2

AIM−7

1B, 8B

6, 6

AIM−9

1, 8

8, 8

AIM−54

3, 4

12, 8

(See

AIM−54

6, 5

12, 8

NOTE

AIM−54

1B, 8B

12, 12

AIM−54 WPNS RAIL

3, 4, 5, 6

AIM−54 RAIL FAIRING

3, 6

—

TARPS POD

MULTIPURPOSE PYLON

1, 8

3, 3

AIM−54 ADAPTOR/LAUNCHER

1B, 8B

3, 3

AIM−7 ADAPTOR/LAUNCHER

1B, 8B

2, 2

AIM−9 ADAPTOR/LAUNCHER

1, 8

1, 1

AIM−9 LAUNCHER

1A, 8A

—

BRU−32/ADU−703A/A

3, 4, 5, 6

BRU−42 (ITER)

3, 4, 5, 6

MK 76 (3 BOMBS)

3, 4, 5, 6

MK 82/BSU−33 (NTP)

3, 4, 5, 6

(TP)

3, 4, 5, 6

MK 82/BSU−86 (NTP)

3, 4, 5, 6

(See

NOTE

(TP)

3, 4, 5, 6

3, 4)

MK 83 CONICAL (NTP)

3, 6

(NTP)

4, 5

(TP)

3, 6

(TP)

4, 5

MK 83/BSU−85 (NTP)

3, 6

(NTP)

4, 5

(TP)

3, 6

(TP)

4, 5

MK 84 CONICAL (NTP)

3, 6

(NTP)

4, 5

(TP)

3, 6

(TP)

4, 5

GBU−10

3, 4, 5, 6

GBU−16

3, 4, 5, 6

Change 3

190a

NAVAIR 01-F14AAP-1B

DRAG TABLE

DRAG INDEX

STORE

STATIONS

(PER STATION)

MK 20/ROCKEYE/

3, 6

OBU−99/100

4, 5

CBU−78 GATOR

3, 6

4, 5

CBU−59 APAM

3, 6

4, 5

TALD

3, 4, 5, 6

EXTERNAL FUEL TANK

2, 7

9, 9

EXTERNAL FUEL TANK RACK

2, 7

1, 1

ALQ−167 POD

NOTES

1. FOR AIRCRAFT BUNO 159025 AND EARLIER AIRCRAFT

WITH AFC 301 (MODIFIED BOATTAIL), ADD 10 COUNTS

TO DRAG INDEX. DRAG INDEX OF ZERO REFERS TO

FAIRED AIM−7 CAVITIES.

WEAPONS DRAG COUNT

____________

RAILS/LAUNCHERS DRAG COUNT

____________

EXTERNAL FUEL DRAG COUNT

____________

MISCELLANEOUS DRAG COUNT

____________

TOTAL DRAG COUNT

2. DRAG INDEX VALUES ARE 12, 12 WHEN (2) AIM−54 ARE

CARRIED ONLY ON STATIONS 4 AND 5

(NTP) NONTHERMALLY PROTECTED

(TP) THERMALL PROTECTED

4. DRAG INDEX IS FOR EACH STATION.

EX: FOR FOUR SMOOTH MK 84 CONICAL BOMBS, DRAG

INDEX IS 4 X 10 = 40; FOR BOMBS ONLY

190b Change 3

NAVAIR 01-F14AAP-1B

WEIGHT TABLE

POUNDS

STORE

PER STORE

20 MM AMMUNITION

0.6

LB/ROUND

AIM−9

200

AIM−7

500

AIM−54

1,000

TARPS POD

1,750

AIM−54 RAIL/LAUNCHER

500

AIM−54 RAIL FAIRINGS

100

(COMBINED)

MULTIPURPOSE PYLON

500

(PAIR)

AIM−54 ADAPTER/LAUNCHER

200

AIM−7 ADAPTER/LAUNCHER

100

AIM−9 ADAPTER/LAUNCHER

100

AIM−9 LAUNCHER (1a, 8a)

100

BRU−32/ADU−703A/A

186

BRU−42 (ITER)

MK 76 (3 BOMBS)

MK 82/BSU−33 (NTP)

527

(TP)

540

MK 82/BSU−86 (NTP)

566

(TP)

579

MK 83 CONICAL (NTP)

971

(TP)

987

MK 83/BSU−85 (NTP)

1,006

(TP)

1,022

MK 84 CONICAL (NTP)

1,970

(TP)

1,989

GBU−10

2,083

GBU−16

1,100

MK 20 ROCKEYE/CBU−99/100

490

CBU−78 GATOR

490

CBU−59 APAM

760

TALD

400

EXTERNAL FUEL TANK

200

EXTERNAL TANK RACK

100

NOTE

CERTAIN WEIGHTS ROUNDED TO NEAREST 100 POUNDS.

BASIC AIRCRAFT WEIGHT.

____________

FUEL WEIGHT (INC EXT)

____________

ARMAMENT WEIGHT

____________

TANKS, LAUNCHERS, RAILS

____________

TOTAL GROSS WEIGHT

____________

(NTP) NONTHERMALLY PROTECTED

(TP) THERMALLY PROTECTED

190c/(190d blank)

Change 3

NAVAIR 01-F14AAP-1B

GEAR UP

48,000 lb

BINGO

FLAPS UP

TWIN ENG

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED BASED

ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

100

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

.75

42,000

.72

149

101

210

4250

4950

278

114

101

150

.75

37,000

.71

120

210

3810

4390

278

100

.75

29,000

.60

210

3350

3830

276

.75

25,000

.60

210

3140

3580

276

.75

20,000

.56

210

2910

3300

276

.75

15,000

.52

210

2660

2960

276

.75

6000

.44

210

2360

2550

274

200

.73

43,000

.73

135

205

4420

5180

262

112

150

.73

38,000

.70

110

205

3950

4570

264

100

.73

30,000

.60

205

3450

3970

264

.73

26,000

.60

205

3230

3700

264

.73

21,000

.55

205

2990

3400

264

.73

15,000

.49

205

2710

3040

264

.73

8000

.44

205

2390

2600

264

200

.72

43,000

.73

120

201

4610

5420

256

112

150

.72

39,000

.71

102

201

4100

4750

256

100

.72

31,000

.62

201

3560

4120

256

.72

27,000

.60

201

3330

3830

254

.72

22,000

.56

201

3070

3510

254

.72

16,000

.49

201

2770

3130

254

.72

8000

.42

201

2420

2660

254

200

.70

42,000

.72

104

197

4810

5680

246

112

150

.70

40,000

.72

.96

197

4250

4950

246

100

.70

32,000

.63

197

3680

4270

244

.70

28,000

.58

197

3430

3960

244

.70

23,000

.52

197

3150

3620

242

.70

16,000

.47

197

2830

3220

242

.70

8000

.40

197

2460

2710

242

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0-F52P-33-1

191

NAVAIR 01-F14AAP-1B

GEAR UP

48,000 lb

BINGO

FLAPS DOWN

TWIN ENG

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED BASED

ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

100

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

.40

29,000

.46

149

7790

11,130

188

131

108

150

.40

29,000

.45

149

6480

9010

186

102

100

.40

28,000

.44

149

5180

6970

184

.40

27,000

.44

149

4660

6170

184

.40

23,000

.40

149

4120

5440

182

.40

17,000

175

149

3530

4590

182

195

6000

185

149

2830

3570

182

200

.40

28,000

.44

148

8010

11,581

188

133

110

150

.40

28,000

.43

148

6630

9330

186

102

100

.40

28,000

.43

148

5270

7150

184

.40

27,000

.43

148

4730

6310

184

.40

24,000

.41

148

4170

5490

182

.40

17,000

175

148

3570

4670

182

195

7000

185

148

2860

3610

180

200

.40

27,000

.43

147

8250

12,070

188

134

112

150

.40

28,000

.43

147

6770

9650

186

103

100

.40

28,000

.43

147

5370

7360

184

.40

27,000

.43

147

4810

6460

184

.40

23,000

.40

147

4230

5630

182

195

15,000

170

147

3610

4810

182

195

7000

180

147

2880

3660

180

200

.40

26,000

.42

145

8480

12,570

186

136

112

150

.40

27,000

.43

145

6940

10,000

184

104

100

.40

27,000

.43

145

5470

7580

182

.40

26,000

.41

145

4890

6640

180

.40

23,000

.39

145

4290

5750

180

165

15,000

170

145

3650

4900

180

195

7000

180

145

2900

3710

178

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0-F52P-33-2

192

NAVAIR 01-F14AAP-1B

GEAR DOWN

48,000 lb

BINGO

FLAPS UP

TWIN ENG

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED BASED

ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

100

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

.56

36,000

.65

194

5530

6760

.56

122

100

150

.56

35,000

.63

194

4820

5800

.56

100

.56

33,000

.60

194

4100

4840

.56

30,000

.58

194

3800

4460

.56

.49

20,000

.47

194

3460

4120

.49

.43

13,000

.41

194

3050

3600

.43

225

3000

220

194

2570

2930

.36

200

.56

35,000

.61

191

5720

7060

.33

123

100

150

.56

35,000

.61

191

4960

6010

.33

100

.56

33,000

.60

191

4200

4990

.33

.56

30,000

.56

191

3880

4580

.33

.50

21,000

.47

191

3520

4210

.33

.43

13,000

.40

191

3090

3680

.33

225

4000

210

191

2590

2980

.32

200

.56

35,000

.61

189

5910

7350

.33

123

100

150

.56

35,000

.61

189

5100

6230

.32

100

.56

33,000

.58

189

4290

5130

.32

.56

30,000

.54

189

3950

4710

.32

.51

22,000

.47

189

3580

4300

.32

.44

14,000

.40

189

3140

3750

.32

225

4000

210

189

2620

3030

.32

200

.56

35,000

.61

187

6110

7660

.33

124

100

150

.56

35,000

.61

187

5250

6450

.32

100

.56

33,000

.58

187

4390

5290

.32

.56

30,000

.54

187

4040

4830

.32

.51

22,000

.45

187

3640

4410

.32

.44

14,000

.40

187

3180

3840

.32

225

5000

205

187

2640

3070

.32

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0-F52P-33-3

193

NAVAIR 01-F14AAP-1B

GEAR DOWN

48,000 lb

BINGO

FLAPS DOWN

TWIN ENG

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED BASED

ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

100

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

.40

26,000

.40

142

8720

13,230

170

136

112

150

.40

27,000

.40

142

7120

10,480

168

104

100

.40

27,000

.41

142

5610

7900

166

.40

26,000

.40

142

5010

6910

166

.40

23,000

160

142

4390

5970

164

195

14,000

160

142

3720

5110

164

195

7000

160

142

2930

3820

164

200

.40

26,000

.40

140

8910

13,670

170

136

113

150

.40

27,000

.40

140

7270

10,810

168

104

100

.40

27,000

.40

140

5720

8120

166

.40

26,000

.40

140

5100

7090

166

.40

22,000

160

140

4460

6130

164

195

14,000

160

140

3760

5200

164

195

7000

160

140

2950

3880

162

200

.40

25,000

.40

138

9160

14,220

170

138

115

150

.40

26,000

.40

138

7450

11,200

168

106

100

.40

26,000

.40

138

5830

8370

166

.40

25,000

160

138

5190

7290

164

.40

22,000

160

138

4520

6260

164

195

14,000

160

138

3790

5300

164

195

6000

160

138

2970

3950

162

200

.40

25,000

136

9370

14,680

170

140

116

150

.40

25,000

136

7640

11,600

168

107

100

.40

26,000

136

5940

8600

166

.40

25,000

160

136

5280

7470

164

.40

21,000

160

136

4590

6440

164

195

13,000

160

136

3840

5440

162

195

7000

160

136

2990

3990

162

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0-F52P-33-4

194

NAVAIR 01-F14AAP-1B

GEAR UP

48,000 lb

BINGO

FLAPS UP

SINGLE ENG

DATE: SEPTEMBER 1987

N1 = WINDMILLING

DATA BASIS: ESTIMATED

N2 = 0 RPM

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

100

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

.44

24,000

.59

196

4650

5750

260

149

135

150

.44

23,000

.58

196

4060

4930

258

116

106

100

.44

18,000

.51

196

3460

4120

258

.44

16,000

.50

196

3200

3770

256

.44

13,000

.47

196

2930

3400

256

.44

9000

.43

196

2650

3000

256

.44

4000

.40

196

2340

2540

256

200

.43

23,000

.52

194

4940

6230

246

150

136

150

.43

22,000

.51

194

4280

5290

244

116

106

100

.43

19,000

.50

194

3600

4350

244

.43

16,000

.47

194

3320

3960

244

.43

14,000

.45

194

3020

3540

242

.43

9000

.41

194

2710

3110

242

.43

4000

.40

194

2370

2600

242

200

.42

21,000

.50

192

5240

6780

244

152

139

150

.42

21,000

.50

192

4500

5680

244

117

108

100

.42

18,000

.47

192

3740

4600

242

.42

16,000

.45

192

3430

4160

242

.42

13,000

.43

192

3110

3710

242

.42

9000

.40

192

2770

3220

240

.42

4000

230

192

2410

2660

240

200

.40

20,000

.49

189

5560

7360

228

152

142

150

.40

19,000

.48

189

4730

6100

230

117

109

100

.40

17,000

.46

189

3890

4870

230

.40

16,000

.45

189

3550

4370

230

.40

14,000

.43

189

3200

3860

230

.40

9000

220

189

2830

3340

230

.40

5000

220

189

2440

2720

228

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

NOTES

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

• IF BOTH ROTORS ZERO RPM ADD 80 COUNTS TO DRAG INDEX.

0-F52P-33-5

Change 2

195

NAVAIR 01-F14AAP-1B

GEAR UP

48,000 lb

BINGO

FLAPS DOWN

SINGLE ENG

DATE: SEPTEMBER 1987

N1 = WINDMILLING

DATA BASIS: ESTIMATED

N2 = 0 RPM

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

INBD

MACH

FUEL REQ

MACH

DIST

ALT

DIST (nmi)

KCAS

(lbs)

DIST (nmi)

(feet)

(nmi)

KIAS

INBD

MACH

ALT

DIST

KCAS

(feet)

WIND

HEAD

WIND

HEAD

WIND

HEAD

(nmi)

KIAS

WIND

200

180

8000

165

147

10,020

12,900

172

179

173

150

180

9000

165

147

7930

10,020

170

133

129

100

180

10,000

165

147

5950

7300

170

180

10,000

165

147

5190

6260

172

180

9000

165

147

4430

5420

170

180

6000

165

147

3650

4230

170

180

3000

165

147

2850

3160

170

200

180

8000

165

146

10,290

13,340

170

180

177

150

180

8000

165

146

8180

10,410

168

134

131

100

180

9000

165

146

6100

7540

166

180

9000

165

146

5310

6440

166

180

8000

165

146

4510

5380

166

180

6000

165

146

3700

4310

164

180

3000

165

146

2870

3200

164

200

175

7000

165

144

10,630

13,910

170

183

180

150

175

7000

165

144

8420

10,810

168

134

133

100

175

8000

165

144

6240

7780

166

175

8000

165

144

5410

6630

166

175

8000

165

144

4580

5490

164

175

6000

165

144

3750

4390

164

175

3000

165

144

2900

3240

164

200

170

6000

165

143

11,000

14,510

170

183

180

150

170

6000

165

143

8680

11,240

168

137

136

100

170

7000

165

143

6390

8040

166

170

8000

165

143

5510

6800

166

170

8000

165

143

4650

5620

164

170

6000

165

143

3800

4470

162

170

3000

165

143

2920

3280

162

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

NOTES

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

• IF BOTH ROTORS ZERO RPM ADD 40 COUNTS TO DRAG INDEX.

0-F52P-33-6

196

Change 2

NAVAIR 01-F14AAP-1B

GEAR DOWN

48,000 lb

BINGO

FLAPS UP

SINGLE ENG

DATE: SEPTEMBER 1987

N1 = WINDMILLING

DATA BASIS: ESTIMATED

N2 = 0 RPM

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

100

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

.40

19,000

.44

187

6230

8610

214

159

143

150

.40

19,000

.44

187

5240

7030

212

122

109

100

.40

18,000

.43

187

4250

5510

210

.40

16,000

.41

187

3850

4910

210

.40

13,000

.40

187

3440

4310

210

7000

210

187

3000

3680

210

1000

210

187

2520

2910

208

200

.40

18,000

.42

186

6520

9180

210

161

146

150

.40

18,000

.42

186

5450

7450

210

123

111

100

.40

17,000

.41

186

4390

5780

208

.40

16,000

.41

186

3960

5120

208

200

12,000

200

186

3530

4490

208

205

8000

205

186

3060

3780

206

205

2000

205

186

2550

2970

206

200

.40

17,000

.41

185

6820

9800

206

162

148

150

.40

17,000

.41

185

5670

7900

206

124

112

100

.40

17,000

.41

185

4530

6050

204

.40

15,000

.40

185

4080

5350

204

200

12,000

200

185

3610

4650

202

200

8000

200

185

3120

3890

202

200

1000

200

185

2580

3030

202

200

.40

15,000

.40

183

7160

10,500

204

165

152

150

.40

16,000

.40

183

5890

8380

204

125

114

100

.40

16,000

.40

183

4680

6360

204

.40

14,000

.39

183

4190

5590

202

200

12,000

200

183

3700

4820

202

200

8000

200

183

3170

4010

202

200

2000

200

183

2610

3090

202

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

NOTES

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

• IF BOTH ROTORS ZERO RPM ADD 70 COUNTS TO DRAG INDEX.

0-F52P-33-7

Change 2

197

NAVAIR 01-F14AAP-1B

GEAR DOWN

48,000 lb

BINGO

FLAPS DOWN

SINGLE ENG

DATE: SEPTEMBER 1987

N1 = WINDMILLING

DATA BASIS: ESTIMATED

N2 = 0 RPM

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

160

6000

160

139

10,960

14,590

162

185

182

150

160

7000

160

139

8590

11,200

160

137

134

100

160

8000

160

139

6340

8030

158

160

9000

160

139

5470

6800

158

160

9000

160

139

4640

5640

156

160

7000

160

139

3800

4490

156

160

3000

160

139

2930

3310

156

200

160

6000

160

138

11,210

15,010

162

186

183

150

160

7000

160

138

8770

11,510

160

138

134

100

160

7000

160

138

6490

8290

158

160

8000

160

138

5580

6990

158

160

8000

160

138

4710

5770

156

160

7000

160

138

3850

4570

156

160

3000

160

138

2950

3340

156

200

155

5000

155

137

11,590

15,670

162

190

186

150

155

6000

155

137

9040

11,960

160

140

136

100

155

6000

155

137

6660

8570

158

155

7000

155

137

5700

7210

158

155

7000

155

137

4800

5920

156

155

7000

155

137

3900

4660

156

155

3000

155

137

2970

3390

156

200

155

4000

155

136

11,990

16,360

162

192

189

150

155

5000

155

136

9320

12,450

160

142

138

100

155

6000

155

136

6790

8800

158

155

6000

155

136

5830

7440

158

155

6000

155

136

4890

6090

156

155

6000

155

136

3950

4760

156

155

2000

155

136

3000

3440

154

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

NOTES

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

• IF BOTH ROTORS ZERO RPM ADD 30 COUNTS TO DRAG INDEX.

0-F52P-33-8

198

Change 2

NAVAIR 01-F14AAP-1B

GEAR UP

48,000 lb

BINGO

FLAPS UP

TWIN ENG

WINGS

= 68_

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

SEA LEVEL

CLIMB

CRUISE

DESCEND

CRUISE

INBOUND

MACH

ALT

DIST

VELOCITY

FUEL

DIST

DISTANCE

(FEET)

(nmi)

(KCAS)

REQ (lb)

(nmi)

KIAS

200

.85

39,000

.89

274

4820

.54

122

150

.85

39,000

.88

274

4160

.54

100

.85

37,000

.85

274

3520

.54

.85

33,000

.81

274

3260

.54

.85

27,000

.77

274

3010

.54

.85

20,000

.66

274

2730

.54

.85

11,000

.60

274

2410

.54

200

.81

38,000

.86

263

5100

.47

122

150

.81

38,000

.86

263

4380

.47

100

.81

37,000

.84

263

3670

.47

.81

34,000

.81

263

3390

.47

.81

28,000

.78

263

3110

.47

.81

21,000

.61

263

2800

.47

.81

11,000

.55

263

2450

.47

200

.78

36,000

.82

255

5400

.46

123

150

.78

36,000

.82

255

4620

.46

100

.78

35,000

.81

255

3840

.45

.78

33,000

.80

255

3528

.45

.78

28,000

.78

255

3210

.45

.78

21,000

.67

255

2880

.45

.78

11,000

.55

255

2500

.45

200

.74

34,000

.80

247

5730

.46

126

150

.74

34,000

.80

247

4870

.46

100

.74

33,000

.80

247

4020

.45

.74

32,000

.80

247

3670

.45

.74

28,000

.78

247

3330

.45

.74

21,000

.67

247

2970

.45

.74

11,000

.55

247

2540

.45

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0-F52P-33-9

199

NAVAIR 01-F14AAP-1B

GEAR UP

48,000 lb

BINGO

FLAPS UP

SINGLE ENG

WINGS

= 68_

DATE: SEPTEMBER 1987

N1 = WINDMILLING

DATA BASIS: ESTIMATED

N2 = 0 RPM

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

SEA LEVEL

CLIMB

CRUISE

DESCEND

CRUISE

INBOUND

MACH

ALT

DIST

VELOCITY

FUEL

DIST

DISTANCE

(FEET)

(nmi)

(KCAS)

REQ (lb)

(nmi)

KIAS

200

.55

15,000

.60

240

5610

.46

123

150

.55

15,000

.60

240

4725

.45

100

.55

15,000

.60

240

3860

.45

.55

15,000

.60

240

3510

.45

.55

13,000

.57

240

3160

.45

.55

10,000

.54

240

2800

.45

.55

5000

.49

240

2420

.45

200

.51

15,000

.60

228

6090

.46

169

150

.51

15,000

.60

228

5090

.45

128

100

.51

15,000

.60

228

4110

.45

.51

13,000

.57

228

3710

.45

.51

12,000

.56

228

3310

.45

.51

9000

.53

228

2900

.45

.51

5000

.49

228

2470

.45

200

.48

14,000

.59

219

6630

.46

172

150

.48

14,000

.59

219

5490

.46

130

100

.48

13,000

.57

219

4370

.45

.48

12,000

.56

219

3920

.45

.48

10,000

.54

219

3460

.45

.48

8000

.52

219

3000

.45

.48

4000

.48

219

2520

.45

200

241

11,000

.56

213

7240

304

178

150

241

11,000

.55

213

5930

302

134

100

241

11,000

.55

213

4650

300

245

10,000

.54

213

4140

298

250

9000

.53

213

3630

298

264

6000

.50

213

3100

296

279

3000

.47

213

2570

296

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

NOTES

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

• IF BOTH ROTORS ZERO RPM ADD 90 COUNTS TO DRAG INDEX.

0-F52P-33-10

200

Change 2

NAVAIR 01-F14AAP-1B

GEAR UP

53,000 lb

BINGO

FLAPS UP

TWIN ENG

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

100

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

.75

41,000

.73

134

220

4350

5090

288

116

104

150

.75

37,000

.72

114

220

3880

4460

290

100

.75

29,000

.62

220

3380

3870

288

.75

25,000

.60

220

3170

3610

288

.75

20,000

.57

220

2940

3310

288

.75

14,000

.53

220

2670

2960

288

.75

7000

.46

220

2370

2550

286

200

.73

41,000

.73

118

215

4540

5340

272

115

100

150

.73

38,000

.72

105

215

4030

4660

272

100

.73

30,000

.64

215

3500

4020

270

.73

26,000

.60

215

3270

3740

270

.73

21,000

.58

215

3010

3420

268

.73

15,000

.51

215

2730

3050

268

.73

8000

.45

215

2400

2600

268

200

.72

40,000

.72

102

210

4750

5600

262

115

150

.72

39,000

.73

210

4190

4860

262

100

.72

31,000

.65

210

3620

4170

262

.72

27,000

.60

210

3370

3870

262

.72

22,000

.58

210

3100

3540

260

.72

16,000

.51

210

2790

3140

260

.72

8000

.44

210

2430

2660

260

200

.70

40,000

.72

207

4960

5880

258

115

150

.70

39,000

.73

207

4360

5080

256

100

.70

32,000

.66

207

3750

4330

256

.70

27,000

.60

207

3480

4020

254

.70

22,000

.54

207

3190

3660

254

.70

16,000

.49

207

2860

3240

254

.70

8000

.42

207

2470

2720

254

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0-F52P-33-11

201

NAVAIR 01-F14AAP-1B

GEAR UP

53,000 lb

BINGO

FLAPS DOWN

TWIN ENG

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

100

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

.40

27,000

.45

156

8250

11,820

196

137

115

150

.40

27,000

.45

156

6810

9510

194

106

100

.40

27,000

.45

156

5390

7270

192

.40

25,000

.44

156

4820

6418

192

.40

22,000

.41

156

4240

5560

192

.40

15,000

180

156

3610

4710

190

195

6000

180

156

2870

3590

190

200

.40

27,000

.44

155

8490

12,310

194

138

116

150

.40

27,000

.45

155

6970

9840

194

106

100

.40

26,000

.44

155

5490

7480

192

.40

25,000

.43

155

4900

6570

192

.40

22,000

.40

155

4300

5680

192

.40

15,000

180

155

3650

4790

190

195

6000

180

155

2890

3640

190

200

.40

25,000

154

8570

12,840

194

139

119

150

.40

26,000

154

7140

10,210

192

106

100

.40

26,000

154

5600

7710

192

.40

25,000

154

4990

6730

190

.40

22,000

154

4370

5810

190

195

15,000

180

154

3700

4890

190

195

6000

180

154

2920

3700

190

200

.40

24,000

.42

152

9000

13,370

192

141

120

150

.40

25,000

.43

152

7320

10,580

192

107

100

.40

25,000

.43

152

5710

7950

190

.40

25,000

.42

152

5080

6910

188

.40

22,000

.40

152

4430

5930

188

195

14,000

180

152

3740

5000

188

195

6000

180

152

2940

3760

186

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0-F52P-33-12

202

NAVAIR 01-F14AAP-1B

GEAR DOWN

53,000 lb

BINGO

FLAPS UP

TWIN ENG

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

100

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

.56

34,000

.66

203

5790

7100

.35

128

106

150

.56

33,000

.63

203

5010

6050

.35

101

100

.56

31,000

.60

203

4230

5010

.35

.55

25,000

.55

203

3910

4650

.35

.47

18,000

.47

203

3530

4220

.35

.42

11,000

.41

203

3100

3660

.35

225

3000

225

203

2590

2940

.35

200

.56

34,000

.63

201

5990

7410

.56

127

106

150

.56

33,000

.61

201

5160

6280

.56

100

.56

32,000

.60

201

4330

5150

.56

.55

25,000

.53

201

3990

4790

.55

.49

20,000

.48

201

3600

4300

.49

.42

11,000

.41

201

3140

3750

.42

225

4000

225

201

2610

2990

.37

200

.56

33,000

.61

199

6200

7750

.34

128

106

150

.56

33,000

.61

199

5320

6520

.34

101

100

.56

31,000

.58

199

4430

5320

.34

.56

29,000

.55

199

4070

4840

.34

.49

20,000

.46

199

3660

4420

.33

.43

13,000

.41

199

3190

3810

.33

225

4000

225

199

2640

3040

.33

200

.56

33,000

.61

197

6420

8080

.34

128

106

150

.56

33,000

.61

197

5480

6760

.34

102

100

.56

31,000

.58

197

4540

5490

.34

.56

28,000

.54

197

4155

5000

.33

.50

21,000

.46

197

3730

4510

.33

.43

13,000

.41

197

3240

3900

.33

225

4000

225

197

2670

3100

.33

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0-F52P-33-13

203

NAVAIR 01-F14AAP-1B

GEAR DOWN

53,000 lb

BINGO

FLAPS DOWN

TWIN ENG

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

CLIMB

CRUISE

DESCEND

SEA LEVEL CRUISE

FUEL REQ

DIST (nmi)

(lbs)

INBD

MACH

ALT

100

DIST

KCAS

(feet)

(nmi)

KIAS

WIND

HEAD

WIND

HEAD

WIND

HEAD

WIND

200

.40

24,000

.40

149

9240

14,060

178

140

119

150

.40

25,000

.41

149

7500

11,080

176

107

100

.40

25,000

.40

149

5850

8280

174

.40

25,000

.40

149

5190

7180

172

.40

21,000

165

149

4530

6180

172

200

13,000

165

149

3800

5210

172

200

6000

170

149

2970

3870

170

200

.40

24,000

.40

147

9450

14,530

178

141

120

150

.40

24,000

.40

147

7690

11,480

176

108

100

.40

25,000

.40

147

5960

8510

174

.40

24,000

.40

147

5290

7380

172

.40

21,000

165

147

4600

6310

172

200

13,000

165

147

3840

5310

172

200

6000

165

147

2990

3920

170

200

.40

23,000

.40

145

9720

15,120

178

144

122

150

.40

24,000

.40

145

7850

11,840

176

110

100

.40

24,000

.40

145

6080

8770

174

.40

24,000

.40

145

5380

7570

172

.40

20,000

160

145

4660

6490

172

200

13,000

160

145

3880

5410

170

200

6000

165

145

3010

3980

170

200

.40

23,000

.40

143

9940

15,610

176

144

123

150

.40

23,000

.40

143

8050

12,270

174

110

100

.40

24,000

.40

143

6200

9020

172

.40

24,000

.40

143

5480

7770

172

.40

20,000

160

143

4730

6630

172

200

13,000

160

143

3930

5510

170

200

6000

160

143

3030

4040

170

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0-F52P-33-14

204

NAVAIR 01-F14AAP-1B

GEAR UP

53,000 lb

BINGO

FLAPS UP

TWIN ENG

WINGS

= 68_

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

SEA LEVEL

CLIMB

CRUISE

DESCEND

CRUISE

INBOUND

MACH

ALT

DIST

VELOCITY

FUEL

DIST

DISTANCE

(FEET)

(nmi)

(KCAS)

REQ (lb)

(nmi)

KIAS

200

.85

37,000

.88

288

5040

.56

129

150

.85

37,000

.88

288

4330

.56

100

.85

36,000

.86

288

3620

.56

.85

32,000

.82

288

3340

.56

.85

27,000

.80

288

3060

.56

.85

19,000

.68

288

2760

.56

.85

10,000

.60

288

2430

.56

200

.81

36,000

.86

276

5340

.49

128

150

.81

36,000

.86

276

4560

.49

100

.81

35,000

.85

276

3780

.49

.81

32,000

.81

276

3480

.49

.81

27,000

.80

276

3170

.49

.81

20,000

.69

276

2840

.49

.81

10,000

.57

276

2470

.49

200

.78

34,000

.83

268

5680

.48

130

150

.78

34,000

.82

268

4820

.48

100

.78

34,000

.82

268

3970

.47

.78

32,000

.80

268

3630

.47

.78

27,000

.80

268

3280

.47

.78

20,000

.69

268

2930

.47

.78

11,000

.58

268

2520

.47

200

.74

32,000

.80

260

6040

318

131

150

.74

32,000

.80

260

5090

316

100

.74

32,000

.80

260

4160

314

.74

30,000

.80

260

3780

314

.74

27,000

.80

260

3400

312

.74

20,000

.69

260

3010

312

.74

11,000

.58

260

2570

310

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0−F52P−33−15

Change 3

204a

NAVAIR 01-F14AAP-1B

GEAR UP

EXTENDED

48,000 lb

FLAPS UP

RANGE BINGO TWIN ENG

DESCEND

FUEL REQ (lb)

DISTANCE (nmi)

INBD

100KT

DIST

CLIMB

HEAD

100KT

(nmi)

MACH

WIND

KCAS

WIND

HEAD

300

0.745

123

212

5330

6440

400

0.745

121

212

6310

7770

500

0.745

120

212

7310

9130

600

0.745

118

212

8330

10,510

700

0.745

116

212

9350

11,910

800

0.745

124

212

10,400

13,330

900

0.745

122

212

11,450

14,810

1000

0.745

121

212

12,510

16,330

300

0.732

111

206

5580

6790

400

0.732

110

206

6650

8240

500

0.732

108

206

7740

9740

600

0.732

106

206

8850

11,250

700

0.732

105

206

9980

12,790

800

0.732

112

206

11,120

14,370

900

0.732

110

206

12,280

15,970

1000

0.732

108

206

13,460

17,610

300

0.718

100

202

5840

7140

400

0.718

202

6990

8710

500

0.718

202

8160

10,340

600

0.718

202

9360

11,970

700

0.718

102

202

10,590

13,660

800

0.718

100

202

11,830

15,380

900

0.718

202

13,090

17,140

1000

0.718

202

14,380

18,920

300

0.705

198

6100

7500

400

0.705

198

7340

9200

500

0.705

198

8600

10,960

600

0.705

198

9910

12,730

700

0.705

198

11,220

14,560

800

0.705

198

12,560

16,450

900

0.705

198

13,930

18,320

1000

0.705

198

15,320

20,280

OPTIMUM ALTITUDE (FEET)

CRUISE MACH

GROSS

DRAG INDEX

WEIGHT

0.718

(1,000 lb)

100

150

32,300

33,400

33,900

34,200

33,900

35,000

35,500

35,700

35,500

36,600

37,100

37,300

38,300

38,800

39,100

39,300

40,200

40,600

40,900

• MILITARY POWER CLIMB FROM SEA LEVEL TO OPTIMUM

ALTITUDE FOR INITIAL CLIMB WEIGHT

• STEP UP ALTITUDE AS GROSS WEIGHT DECREASES

NOTES

• IDLE POWER MAXIMUM RANGE DESCENT SPEED BRAKES RETRACTED

• FUEL REQUIRED INCLUDES 2,000 POUNDS RESERVE

204b

Change 3

NAVAIR 01-F14AAP-1B

GEAR UP

53,000 lb

BINGO

FLAPS UP

TWIN ENG

WINGS

= 68_

DATE: SEPTEMBER 1987

DATA BASIS: ESTIMATED

BASED ON FLIGHT TEST

INITIAL ALTITUDE: SEA LEVEL

SEA LEVEL

CLIMB

CRUISE

DESCEND

CRUISE

INBOUND

MACH

ALT

DIST

VELOCITY

FUEL

DIST

DISTANCE

(FEET)

(nmi)

(KCAS)

REQ (lb)

(nmi)

KIAS

200

.85

37,000

.88

288

5040

.56

129

150

.85

37,000

.88

288

4330

.56

100

.85

36,000

.86

288

3620

.56

.85

32,000

.82

288

3340

.56

.85

27,000

.80

288

3060

.56

.85

19,000

.68

288

2760

.56

.85

10,000

.60

288

2430

.56

200

.81

36,000

.86

276

5340

.49

128

150

.81

36,000

.86

276

4560

.49

100

.81

35,000

.85

276

3780

.49

.81

32,000

.81

276

3480

.49

.81

27,000

.80

276

3170

.49

.81

20,000

.69

276

2840

.49

.81

10,000

.57

276

2470

.49

200

.78

34,000

.83

268

5680

.48

130

150

.78

34,000

.82

268

4820

.48

100

.78

34,000

.82

268

3970

.47

.78

32,000

.80

268

3630

.47

.78

27,000

.80

268

3280

.47

.78

20,000

.69

268

2930

.47

.78

11,000

.58

268

2520

.47

200

.74

32,000

.80

260

6040

318

131

150

.74

32,000

.80

260

5090

316

100

.74

32,000

.80

260

4160

314

.74

30,000

.80

260

3780

314

.74

27,000

.80

260

3400

312

.74

20,000

.69

260

3010

312

.74

11,000

.58

260

2570

310

• MILITARY POWER CLIMB TO INDICATED ALTITUDE FROM SEA LEVEL

• IDLE POWER MAXIMUM RANGE DESCENT TO SEA LEVEL

(SPEED BRAKES RETRACTED)

NOTES

• FUEL REQUIRED INCLUDES 2000 POUNDS RESERVE FUEL

• WT = ZERO FUEL WEIGHT

• FOR DISTANCES GREATER THAN 200 nmi, ADD FUEL REQUIRED FOR

SHORTER DISTANCES AND SUBTRACT EXCESS FUEL RESERVE (S).

0-F52P-33-15

205/(206 blank)

NAVAIR 01-F14AAP-1B

REFERENCE DATA

Administrative Brief

209

Airspeed Indicator Failure

252

Cockpit Procedures

213

Ascent Checklist

241

Engine Start — Pilot

221

Final Checker (Aboard CV)

237

Final Checker (Ashore)

236

Interior Inspection — Pilot

213

Interior Inspection — RIO

216

Landing Checklist

243

Postlanding — Pilot

244

Postlanding — RIO

245

Poststart — Pilot

225

Poststart — RIO

232

Preland and Descent

241

Prestart — Pilot

217

Prestart — RIO

221

Takeoff Checklist

239

Taxi — Pilot

238

Taxi — RIO

238

Ejection Seat Inspection

210

Hot Refueling Procedures

246

Hot Switch Procedures

247

In-Flight Refueling Checklist

248

Landing Approach Airspeed (15 Units AOA)

255

Landing Distance Ground Roll — Flaps Down

257

Landing Distance Ground Roll — Flaps Up

259

On-Deck, Maintenance Troubleshooting

247

Single-Engine Maximum Endurance on Station

254

Takeoff Speed and Ground Roll Distance, Flaps Down

250

Takeoff Speed and Ground Roll Distance, Flaps Up

249

Two-Engine Maximum Endurance on Station

253

207/(208 blank)

NAVAIR 01-F14AAP-1B

Note

A bracketed T [T] in a procedural step identi-

fies items pertaining only to TARPS aircraft.

ADMINISTRATIVE BRIEF

The following items should be covered for each flight regard-

less of the mission.

1. Event number

2. Launch/recovery times/recovery order

3. Lineup/call signs/avionics plan

4. Missions assigned/alternate missions

5. External assets/call signs

6. Weather

a. Base, en route, target, area, divert

b. Water/air temperature, sea state

7. Ordnance and stores carried/preflight/restrictions on use

8. Communications plan

9. Area/NOTAMs

10. Clearance/NAVAIDs

11. Ground/deck procedures

12. Takeoff/departure/rendezvous

13. En route/formation

14. Tanking plan

15. Combat checks/OBC

16. Recovery procedures (VFR/IFR)

17. Joker/bingo fuel

18. NORDO procedures

19. Emergencies/diverts/SAR/birdstrike

20. Training rules

21. Contingencies

209

NAVAIR 01-F14AAP-1B

EJECTION SEAT INSPECTION

1. Face curtain locking tab

Up (locked)

2. Lower ejection handle

Guard Up (locked)

3. Face curtain connecting link (R)

Safe Indication

4. Time release mechanism trip rod

Connected

If sear is not fully inserted into firing release

mechanism, inadvertent operation of the tim-

ing release mechanism will occur. This will

safe the lower firing handle and release the

occupant from the seat. The seat kit and para-

chute will remain attached to the aircrew via

lap belts and koch fittings.

5. Face curtain automatic release

linkage

Disconnected

6. System initiator

Connected and Pin Removed

7. Time release mechanism rod

Scissors Release

Pin Protruding

8. Drogue chute link lines

Clips Engaged

9. Scissors shackle

Stowed,

Drogue Lanyard, Connected

10. Ejection gun sear

Connected and Pin Removed

11. Ejection gun sear withdrawal links

Connected

12. Drogue chute housing flaps

Tacked Down

13. Face curtain

Secure

14. Face curtain connecting link (L)

Safe Indication

15. Drogue chute lines (L)

Clips Engaged

16. Drogue withdrawal line

Connected to Drogue Slug

210

NAVAIR 01-F14AAP-1B

17. Drogue slug shear pin

Head Impressed

18. Top latch mechanism

Flush

19. Parachute withdrawal line screw

connector

Fingertight

If the personnel parachute withdrawal line is

not securely connected, automatic deployment

of the parachute will not occur after ejection.

20. Guillotine cutter

Withdrawal Line

Routed Through Guillotine

21. Power inertial reel sear

Connected

22. Fork ends of harness sear rods

Connected

23. Rocket motor initiator sear

and Pin Removed

Connected

24. Drogue gun trip rod

Connected and Pin Removed

25. Rocket motor initiator sear extraction

lanyard

Attached

26. Parachute premature deployment lanyard

Secured

27. Shoulder harness

Secured

28. Canopy releases

Proper Installation

29. Ripcord

Routed Through Parachute Pack Ring

30. Manual ripcord eyelet

Connected to

Leap Ripcord Pin

31. Ripcord pins

Straight/No Corrosion

32. Ventilation hose

Connected to Seat or

Disconnected

33. Personnel services block

Verify Connection

to Seat Bucket Disconnect

Lanyard(s) (Two)

Secured to Deck

211

NAVAIR 01-F14AAP-1B

34. Raft release handles

Note Type

35. Lapbelt restraint

Secured

36. Emergency oxygen trip cable

Secured

37. Survival kit sticker clips and

lugs

Secured and Engaged

38. Survival kit front lock release lever

Full Forward

Failure of survival kit front lock release lever

to return to its full-forward position will pre-

vent ejection by means of the lower ejection

handle.

39. Emergency oxygen supply bottle

Full Indication,

1,800 Psi (in black)

40. Emergency oxygen actuator

Connected, Stowed

41. Leg restraint cords

Secured to Deck,

Routed Through Snubber,

Anchored to Seat Release Fitting

42. Survival kit forward restraint pin

Engaged

43. URT-33 lanyard

Connected

44. Emergency restraint release handle

Down

and Secured, Pin Removed

45. Guillotine initiator sear

Connected

46. Ejection and canopy pins

Stowed

212

NAVAIR 01-F14AAP-1B

COCKPIT PROCEDURES

INTERIOR INSPECTION — PILOT

NATOPS prohibits the attaching or storing of

unauthorized equipment on or above the can-

opy rails during CV launch or arrestment due

to potential for missile hazard.

1. Harnessing

Fasten

2. Oxygen

Check

3. VENT AIRFLOW thumbwheel

Set

4. Tone VOLUME CONTROLS

Set

5. TACAN function selector

OFF

6. ICS panel

Set

7. STAB AUG switches

OFF

8. UHF function selector

OFF

9. Wing-sweep mode switch

MANUAL

10. Emergency wing sweep handle

Corresponding

11. Left and right throttles

Off

12. Speedbrake switch

RET

13. Exterior lights master switch

Set

14. FLAP handle

Corresponding

15. Throttle friction lever

Off(aft)

16. ASYM LIMITER switch

ON (guard down)

17. L and R ENG MODE SELECT switches

PRI

18. BACKUP IGNITION switch

OFF

19. THROTTLE TEMP switch

NORM

213

NAVAIR 01-F14AAP-1B

20. THROTTLE MODE switch

BOOST

21. L and R INLET RAMPS switches

AUTO

22. ANTI SKID SPOILER BK switch

OFF

23. FUEL panel

Set

a. WING/EXT TRANS switch

AUTO

b. REFUEL PROBE switch

RET

c. DUMP switch

OFF

d. FEED switch

NORM (guard down)

24. LDG GEAR handle

Check HYD ISOL switch to TO/LDG.

25. NOSE STRUT switch

OFF

26. Parking brake

Pull

27. Radar altimeter

OFF

28. Altimeter

Set

29. Left and right FUEL SHUT OFF handles

30. ACM switch

OFF (guard down)

31. MASTER ARM switch

OFF (guard down)

32. Weapon select

OFF

33. VDIG and HSD retaining locks

Engaged

34. Standby attitude gyro

Caged

35. G-meter

Reset

36. Clock

Wind and Set

37. Fuel BINGO

Set

38. Circuit breakers

Checked

39. Brake accumulator pressure

Check in Green

40. HYD HAND PUMP

Check

41. HOOK handle

Corresponding

214

Change 2

NAVAIR 01-F14AAP-1B

42. DISPLAYS panel

Set

43. ELEV LEAD knob

Set

44. INBD and OUTBD spoiler switches

NORM

(guard down)

45. L and R generator switches

NORM

Ground engine operation without electrical

power supplied by either the generators or

external power may cause 20-mm ammunition

detonation because of excessive heat in the

gun ammunition drum.

46. EMERG generator switch

NORM

(guard down)

47. Air-condition controls

Set

a. TEMP mode selector switch

AUTO

b. TEMP thumbwheel control

As Desired

(5 to 7 midrange)

c. CABIN PRESS switch

NORM

d. AIR SOURCE pushbutton

OFF

48. WSHLD AIR switch

OFF

49. ANTI-ICE switch

AUTO/OFF

50. COMPASS panel

Set

51. ARA-63 panel

OFF

52. MASTER LIGHT panel controls

As Required

53. MASTER TEST switch

OFF

54. EMERG FLT HYD switch

AUTO

(guard down)

55. HYD TRANSFER PUMP switch

SHUTOFF

(guard up)

215

NAVAIR 01-F14AAP-1B

56. CANOPY AIR DIFFUSER lever

CABIN AIR

57. VIDEO CONTROL switch

OFF

58. Storage case

Inspect

INTERIOR INSPECTION — RIO

1. Left and right circuit breakers

Set

2. Left and right foot pedals

Adjust

3. Harnessing

Fasten

4. Oxygen

Check

5. VENT AIRFLOW thumbwheel

OFF

6. SYS TEST-SYS PWR ground

check panel

Closed

7. [T] CPS switches

OFF

8. KY-28 or KY-58

. . . . . . . . . . . . . . . . . . . . . . . . . P/OFF

9. ICS panel

Set

10. CDNU

OFF

11. VHF/UHF MODE selector

OFF

12. LIQ COOLING switch

OFF

13. EJECT CMD lever

Set

Determined by squadron policy

14. Data storage unit

Secure

15. ARMAMENT control panel

Set

16. Standby attitude gyro

Caged

17. NAV MODE knob

OFF

18. PTID PWR switch

OFF

19. Clock

Set and Wind

20. WCS switch

OFF

21. IR/TV power switch

OFF

22. RECORD switch

OFF

23. RADAR WARNING RCVR PWR switch

OFF

216

NAVAIR 01-F14AAP-1B

24. DECM selector knob

OFF

25. AN/ALE-47 DCDU, MODE/PWR switch

OFF

26. AN/ALE-47 GROUND TEST/

DIMMER PNL

GUARD DOWN

27. APX-76

OFF

28. INTERIOR LIGHTS panel

Check

29. IFF MASTER knob

OFF

30. MODE 4 switch

Out

31. IFF ANT and TEST panel

Set

32. RADAR BEACON switch

OFF

33. RADAR BEACON

MODE switch

Single or Double

34. POWER SYS TEST switch

OFF

35. DATA/ADF switch

OFF

PRESTART — PILOT

1. External electrical power

2. If wings are not in OV SWP:

a. WING SWEEP DRIVE NO. 1 and

WG SWP DR NO. 2/MANUV

FLAP cb’s (LE1, LE2)

Pull

b. Emergency WING SWEEP

handle

Extend and Match

Captain Bars With

Wing Position Tape

CAUTION

Wings will move to emergency handle

position regardless of wing-sweep cb position.

Change 2

217

NAVAIR 01-F14AAP-1B

Note

If wings are in OV SW, do not extend

handle.

3. ICS

Check

4. Landing gear indicator and transition light

Check

Check gear indication down and transition light off.

5. MASTER TEST switch

Check

Coordinate with RIO.

a. LTS

Initial failure with subsequent illumination

after slight adjustment of either fire warning

light during lights test is indicative of a weak-

ened fire light retaining clip and/or current

flow impediments at the bulb contact points.

Either condition seriously degrades fire warn-

ing indication reliability. The fire warning

lights must be seated securely with the oper-

able bulb contact points free of impediments to

current flow at all times to ensure proper

operation of the fire warning light.

218

NAVAIR 01-F14AAP-1B

Failure of the EMERG STORES JETT push-

button to illuminate during LTS check could

indicate that the pushbutton light is burned out

or that the test circuit is defective. If the switch

is actuated, stores will jettison when weight is

off wheels. If this occurs, status of the emer-

gency stores jettison circuit cannot be deter-

mined. Under some lighting conditions, it

may be difficult to determine when the light is

illuminated. Ensure that the light goes off

when LTS on MASTER TEST switch is dese-

lected. Failure of the light to go off indicates

emergency jettison is selected; stores will jetti-

son when weight is off wheels.

b. FIRE DET/EXT

c. INST

d. MASTER TEST switch

OFF

6. Ejection seats

Armed

Verify seat armed with RIO.

7. CANOPY handle

219

NAVAIR 01-F14AAP-1B

Flightcrews shall ensure that hands and for-

eign objects are clear of front cockpit hand-

holds and top of ejection seats and canopy sills

to prevent personal injury and/or structural

damage during canopy opening or closing

sequence. Only minimum clearance is

afforded when canopy is transitioning fore and

aft.

Note

If CLOSE does not close the canopy, depress

the grip latch, release and push handle out-

board and forward into BOOST. If it is neces-

sary to use BOOST, the handle shall be

returned to CLOSE to avoid bleed-off of pneu-

matic pressure.

8. ACM panel

Set

9. EMERG STORES JETT pushbutton light

Out

Note

The MASTER CAUTION light and the

EMERG JETT caution light illuminate when

the EMERG STORES JETT pushbutton is

activated.

10. LADDER light

OFF

11. Inform RIO

Ready To Start

12. Starter air

220

NAVAIR 01-F14AAP-1B

PRESTART — RIO

1. Seat, ICS, and U/VHF foot switches

Adjust

2. External power and air

3. ICS

Check

4. DL, tacan, and U/VHF

Set

5. Fuel quantity

Check

6. Lights

Check

7. LTS test

Check

8. Ejection seats

Armed

9. CANOPY handle

Alert pilot.

10. Acknowledge

Ready To Start

ENGINE START — PILOT

The RIO must monitor pilot procedures and plane captain sig-

nals to ensure maximum safety during the engine start

sequence.

Coordinate movement of any external surfaces

and equipment with the plane captain or

director.

221

NAVAIR 01-F14AAP-1B

CAUTION

D If engine chugs and/or rpm hangup is

encountered with one engine turning dur-

ing normal ground start, monitor EGT for

possible hot start. AIR SOURCE pushbut-

ton should be set for the operating engine

until rpm stabilizes at idle, then set to

BOTH ENG.

D To prevent possible engine overtempera-

ture during crossbleed start attempts, select

the operating engine for air source and

return to BOTH ENG after rpm stabilizes at

idle or above.

1. ENG CRANK switch

L (left engine)

2. ENG CRANK switch

OFF

3. ENG CRANK switch

R (right engine)

4. ENG CRANK switch

OFF

5. EMERG FLT HYD

switch

LOW-HIGH-AUTO (LOW)

CAUTION

Combined and brake accumulators should be

charged prior to backup module checks.

Checks should be made slowly enough to

ensure continuous ON indication in the

hydraulic pressure indicator to prevent dam-

age to the pump or motor.

222

Change 1

NAVAIR 01-F14AAP-1B

Note

Ensure combined and flight hydraulic pres-

sures are zero prior to testing emergency flight

hydraulic system to allow proper check of 300

psi priority valve.

6. ENG CRANK switch

R (right engine)

CAUTION

If no oil pressure or hydraulic pressure is in-

dicated, start shall be aborted by setting

ENG CRANK switch to OFF.

If the ENG CRANK does not automatically

return to the OFF position by 50-percent

rpm during start, ensure the ENG CRANK

switch is off prior to 60-percent rpm to

prevent starter overspeed.

If the START/VALVE caution light illumi-

nates after the ENG CRANK switch is off,

select AIR SOURCE to OFF to prevent

starter overspeed.

When attempting a crossbleed or normal

ground start, do not attempt to reengage the

ENG CRANK switch if the engine is

spooling down and rpm is greater than 46

percent. Between 30-and 46-percent rpm,

the ENG CRANK switch may not stay

engaged because of normal variations in

starter cutout speed.

Change 1

223

NAVAIR 01-F14AAP-1B

Note

During cold starts, oil pressure may exceed 65

psi. This pressure limit should not be exceeded

for more than 1 minute.

7. Right throttle

IDLE at 20-Percent Rpm

CAUTION

If an idle crossbleed start is attempted with

high-residual engine EGT and/or throttles are

advanced from OFF to IDLE prior to 20-per-

cent rpm, higher than normal EGT readings

may occur. If the EGT appears to be rising ab-

normally, increasing the supply engine to

80-precent rpm may yield a normal start tem-

perature.

Note

D Advancing the R throttle from OFF to

IDLE automatically actuates the ignition

system. An immediate indication of fuel

flow (300 to 350 pph) will be exhibited and

light-off

(EGT rise) should be achieved

within

5 to

15 seconds. Peak starting

temperatures will be achieved in the 40- to

50-percent rpm range. After a slight hesita-

tion, the EGT will return to normal. Ex-

ceeding

890°C constitutes a hot start.

During the initial starting phase, the nozzle

should expand to a full-open (100 percent)

position.

224

Change 1

NAVAIR 01-F14AAP-1B

Note

D Loss of electrical power may result in

smoke entering the cockpit via the ECS.

8. R GEN light

Out

9. R FUEL PRESS light

Out

10. Idle engine instrument readings

Check

a. Rpm

62 to 78 Percent

b. EGT

500° (nominal)

c. FF

950 to 1,400 Pph (nominal)

d. NOZ position

100 Percent

e. OIL

25 to 35 psi (nominal)

(15 psi minimum)

f. FLT HYD PRESS

3,000 Psi

11. External power

Disconnect

Ground engine operation without electrical

power supplied by either the generators or

external power may cause 20-mm ammunition

detonation because of excessive heat in the

gun ammunition drum.

12. ENG CRANK switch

L (left engine)

When combined hydraulic pressure reaches 3,000 psi,

return switch to neutral (center position).

13. HYD TRANSFER PUMP switch

NORMAL

Hydraulic transfer pump will operate from flight side to

maintain the combined side between 2,400 to 2,600 psi.

Change 1

224a

NAVAIR 01-F14AAP-1B

POSTSTART — PILOT

1. STAB AUG switches

All ON

2. MASTER TEST switch

EMERG GEN

3. MASTER RESET pushbutton

Depress

Verify DFCS caution lights extinguished.

Note

An FCS CAUTION at this point probably

indicates a PQVM fault due to a lack of pitch

and roll attitude inputs from the EGI (DCP

FAIL group will indicate IMU).

4. MASTER TEST switch

OFF

5. MASTER RESET pushbutton

Depress

Verify DFCS caution lights extinguished.

STAB AUG switches should not disengage.

6. Advise RIO that test and checks are completed.

7. Controls and displays

8. AFTC

Check

a. L ENG MODE SELECT switch

SEC

L ENG SEC light illuminates, RPM Drop, left NOZ

indicator pointer below zero.

b. Advance L throttle to ensure engine response.

c. L ENG MODE SELECT switch

PRI

L ENG SEC light goes out, left NOZ indicator to 100

percent.

Change 1

225

NAVAIR 01-F14AAP-1B

d. R ENG MODE SELECT switch

SEC

R ENG SEC light illuminates, RPM drop, right NOZ

indicator pointer below zero.

e. Advance R throttle to ensure engine response.

f. R ENG MODE SELECT switch

PRI

R ENG SEC light goes out, right NOZ indicator to 100

percent.

CAUTION

Selecting secondary

(SEC) mode closes

exhaust nozzles increasing exhaust nozzle jet

wake hazard.

Note

D Performing AFTC check during OBC

inhibits AICS ramps from programming.

Ramps must be reset before another OBC

can be performed.

D Operating engines in secondary mode

inhibits the engine monitoring system por-

tion of FEMS until primary mode is rese-

lected.

9. EMERGENCY WING SWEEP handle

OV SW

CAUTION

If the “OVER” flag is not displayed in the wing

sweep indicator with the wings in oversweep

the stick should remain centered.

226

NAVAIR 01-F14AAP-1B

CAUTION

If wings are not in oversweep, move the wings

to 68° using wing sweep emergency handle in

raised position. Then raise handle to full exten-

sion and hold until HZ TAIL AUTH caution

light goes out and OVER flag appears on wing

sweep indicator. Move handle to full aft OV

SW and stow.

10. WING SWEEP MODE switch

AUTO

11. WING SWEEP DRIVE NO. 1

and WG SW DR. NO. 2 /

MANUVFLAP cb

IN (LE1, LE2)

12. WING/EXT TRANS switch

OFF

13. COMM/NAV/GEAR/DISPLAYS

14. Trim

Set 000

15. Standby gyro

Erect

16. MASTER RESET pushbutton

Depress

17. DCP

Verify codes (FAIL, FLT, IBIT)

Change 3

227

NAVAIR 01-F14AAP-1B

Note

An FCS CAUTION at this point probably

indicates a PQVM fault due to a lack of pitch

and roll attitude inputs from the IMU (DCP

FAIL group will indicate IMU). This fault will

not affect DFCS IBIT results and can be extin-

guished with a MASTER RESET before or

after, but not during OBC.

18. MASTER TEST switch

OBC

19. AUTOPILOT switch

ENGAGE

CAUTION

OBC commencement with autopilot engaged

and nose down trim may result in a force link

disconnect when the stick hits forward stick

stop during the pitch parallel actuator checks.

20. OBC

Initiate

(coordinate with RIO and plane captain)

If CIA acronym is displayed in CM after

completion of OBC, aircrew must select main-

tenance display to determine type of failure in

the AWG-15. The possibility of inadvertent

stores release exists when this acronym is

present.

228

NAVAIR 01-F14AAP-1B

Increased suction around intakes during inlet

ramp programming and the automatic move-

ment of the horizontal stabilizers presents a

FOD hazard and a potential for injury to

ground personnel not clear of these areas.

21. Speedbrake switch

EXT, then RET

22. REFUEL PROBE switch

ALL EXT, then RET

23. WSHLD AIR switch

Cycle

24. MASTER TEST switch/OBC

OFF

25. WING/EXT TRANS switch

OFF

26. Trim

Checked and set 000

CAUTION

Ensure adequate clearance before moving

wings.

Note

For CV operations, omit steps 27 through 50.

27. EMERGENCY WING SWEEP handle

20_

28. MASTER RESET pushbutton

Depress

29. External lights

Check (prior to night/IMC flight)

229

NAVAIR 01-F14AAP-1B

During night operations, aircraft with inoper-

able tail and aft anticollision lights will not be

visible from the rear quadrant even under opti-

mum meteorological conditions, thus increas-

ing midair potential.

30. Flaps and slats

31. Flight controls

Cycle

Observe the following:

a. Pitch control

36_ TEU to 9_ TED

horizontal tail (33_ to 12_

without ITS)

b. Lateral control

24_ total differential tail

c. Directional control

±30_ rudder

d. Longitudinal/Lateral combined

35_ TEU

to 15_ TED horizontal tail

e. Spoilers

55_

32. DLC

Check

Verify horizontal tail shift with DLC input.

33. ANTI SKID SPOILER BK

SPOILER BK

34. Spoilers and throttles

Check

35. ANTI SKID SPOILER BK switch

OFF

36. DCP

Verify codes (FAIL, FLT, IBIT)

230

NAVAIR 01-F14AAP-1B

Aircraft shall be considered down with PFCC,

RFCC, or YFCC codes in the DCP FAIL group

or with an inoperative DCP display. Initiation

of OBC/IBIT with this condition will result in

invalid IBIT indications.

37. MASTER TEST switch

DFCS BIT (IBIT ARM)

38. AUTOPILOT switch

ENGAGE

39. MASTER TEST switch

DFCS BIT (IBIT RUN)

(coordinate with RIO and plane captain)

40. DCP

Verify & record codes (FAIL, FLT, IBIT)

41. DCP

Clear codes (FAIL & FLT)

42. Flaps and slats

43. Maneuver flaps

Down

44. WING SWEEP MODE switch

MAN 50_

CAUTION

If wing sweep commanded position indicator

(captain bars) does not stop at 50_, immedi-

ately select AUTO with WING SWEEP

switch.

45. Maneuver flaps

Crack up

46. WING SWEEP MODE switch

BOMB

47. EMERGENCY WING SWEEP handle

68_

48. EMERGENCY WING SWEEP handle

OV SW

49. WING SWEEP MODE switch

AUTO

231

NAVAIR 01-F14AAP-1B

50. MASTER RESET pushbutton

Depress

Note

CV checklist resumes.

51. ANTI SKID SPOILER BK switch

BOTH

52. ANTI SKID

BIT

53. ANTI SKID SPOILER BK switch

OFF

54. Radar altimeter

BIT

55. Displays

Check

56. Tacan

BIT

57. ARA-63

BIT

58. HUD-VIDEO

BIT

59. Altimeter

SET/RESET mode

60. Compass

Check

61. Flight instruments

Check

POSTSTART — RIO

Note

The RIO will ensure that the EMERG GEN

check is completed before commencing post-

start procedures.

1. CDNU

2. DATA LINK

3. DATA LINK Mode

CAINS/WAYPT (CV Ops)

TAC (Shore Based)

After CDNU SELF TEST complete:

4. NAV MODE switch

Align

5. WCS switch

STBY

Verify AWG-9 COND light illuminated.

232

NAVAIR 01-F14AAP-1B

6. PTID power switch

7. LIQ COOLING switch . . . AWG-9 or AWG-9/AIM-54

Verify that AWG-9 COND light goes off and that AUTO

BIT 2 is running

8. CDNU

Enter current POSITION/DATE/TIME

9. IR/TV power switch

STBY/IR/TV

10. Communications

On and Set

11. [T] CPS system switch

RDY

Observe DATA/MAN V/H light illuminated.

12. [T] IRLS switch

STBY

Observe IR NR light is illuminated for cooldown period

(maximum of 17 minutes).

13. TACAN/EGI select switch

EGI

14. RADAR WARNING RCVR panel

Set

15. DECM knob

STBY

a. When STBY light goes out, select HOLD 3 SEC, then

ACT for OBC.

16. IFF MASTER knob

STBY

17. AUTO BIT 2

Verify Completed

18. Verify pilot has OBC selected:

a. Observe SAT display on PTID.

b. Observe failed acronyms on PTID in CM.

If CIA acronym is displayed in CM after

completion of OBC, aircrew must select main-

tenance display to determine type of failure in

the AWG-15. The possibility of inadvertent

stores release exists when this acronym is

present.

233

NAVAIR 01-F14AAP-1B

c. Observe test completed on PTID.

d. Altimeter

Reset

19. CDNU

Enter desired data, WP, FP, etc.

20. [T] V/H check:

a. Manual V/H thumbwheel set . . 360 Knots/200 Feet

b. V/H switch

Test

Observe MAN V/H light is out.

c. V/H switch

MANUAL

21. [T] Vertical frame check

a. Manual V/H thumbwheel set

350 Knots/

1,800 Feet

b. FRAME switch

VERT

c. FILM switch

RUN

Observe exposure interval of 1.0 second and frame

camera green light illuminated; check camera frame

counter for proper operation.

d. FILM switch

OFF

e. FRAME switch

OFF

22. [T] PAN BIT check

a. PAN switch

BIT/RELEASE

Observe exposure interval of 1.0 second, green PAN

light illumination, and counter decrease as five frames

are exposed.

23. [T] PAN autocycle check

a. PAN switch

CTR

b. FILM switch

RUN

Observe exposure interval of 1.0 second, green PAN

light illumination, and check camera frame counter

for proper operation.

234

NAVAIR 01-F14AAP-1B

c. PAN switch

LEFT or RIGHT

Observe exposure interval of 2.0 seconds, PAN go

light illuminated, and frame counter for proper

operation.

d. FILM switch

OFF

24. [T] PAN pulse mode check

a. Manual V/H thumbwheel set 350 Knots/13,500 Feet

b. PAN switch

CTR

c. FILM switch

RUN

Observe exposure interval of 5.0 seconds, green PAN

light illumination, and check camera frame counter

for proper operation.

d. FILM switch

OFF

e. PAN switch

OFF

25. [T] IR sensor check

Note

Before IRLS system check, observe IR NR

light is out following cooldown and BIT.

Observe film counter movement by 1 foot.

a. IRLS switch

WFOV

b. Manual V/H thumbwheel set . . 350 Knots/600 Feet

c. FILM switch

RUN

Observe green IR LS light flashing at 5-second inter-

val and check proper film counter operation.

d. FILM switch

OFF

e. IRLS switch

STBY

26. Computer address panel

Set

27. DDD

Set

28. PTID controls

Set

29. Multiple display indicator

Set

30. DATA/ADF switch

BOTH

235

NAVAIR 01-F14AAP-1B

31. Hand control panel

Set

32. AN/ALE-47 DCDU, MODE/PWR SWITCH . . STBY

33. CANOPY DEFOG-CABIN AIR lever . . . CABIN AIR

34. D/L reply

As Required

35. AAI control panel

Set

36. Indicator lights

Test

37. DDI BIT

Test

38. After alignment is completed:

a. PTID NAV mode

INS

b. Program restart

Depress

c. STBY/READY lights

OFF

39. DEST data

Verify

40. BRG/DIST to destination

Check

41. OWN A/C groundspeed

Check

42. MAG VAR

Check

43. KY-28/58

As Required

44. Standby attitude gyro

Erect

45. Notify pilot

Ready To Taxi

FINAL CHECKER (ASHORE)

1. NOSE STRUT switch

Kneel, Check

Launch Bar Down

2. Hook

DN, Check RATS Advisory

Light On, Then UP

3. LAUNCH BAR switch

Cycle

4. NOSE STRUT switch

EXTD

236

Change 2

NAVAIR 01-F14AAP-1B

FINAL CHECKER (ABOARD CV)

1. Hook

DN on Director’s Signal

Check RATS Advisory

Light On, Then Up

CAUTION

Carrier operations with an inoperative RATS

will increase wind-over-deck requirements.

Failure to notify CV OPS may result in dam-

age to the ship’s arresting gear or aircraft tail-

hook assembly structure.

2. Nosewheel steering

Cycle Off, Then On

Failure to cycle nosewheel steering following

hook check will permit nosewheel steering

centering to remain engaged and may cause

mispositioning of the launch bar during cata-

pult hookup. This can result in launch bar dis-

engaging from shuttle during catapult stroke.

237

NAVAIR 01-F14AAP-1B

TAXI — PILOT

CAUTION

Taxiing with the left engine secured is not

authorized. Normal braking and nosewheel

steering control will be lost if the hydraulic

transfer pump (BIDI) fails while taxiing with

the left engine secured.

1. Parking brake

Release

2. Nosewheel steering

Check

3. Brakes

Check

4. Turn-and-slip indicator

Check

5. Ordnance

Safe

TAXI — RIO

1. Perform BIT confidence checks 2, 3, 4, 1 if not previously

checked and record results on BER form.

2. OWN A/C groundspeed

Check on ECMD

3. [T] Own A/C altitude

Check

238

NAVAIR 01-F14AAP-1B

TAKEOFF CHECKLIST

RIO CHALLENGE

PILOT REPLY

1. “BRAKES”

CHECK OK, ACCUMU-

LATOR PRESSURE UP”

2. “FUEL TOTAL

“NORMAL FEED, AUTO-

lb”

TRANSFER DUMP OFF,

TRANSFER CHECKED,

TOTAL

WINGS/EXT

AFT AND LEFT

FORWARD AND

RIGHT

FEED TANKS FULL

BINGO SET.

3. “CANOPY CLOSED,

“CLOSED, LOCKS

LOCKS ENGAGED,

ENGAGED, LIGHT OUT,

LIGHT OUT, STRIPES

SEAL INFLATED, HANDLE

ALIGNED, HANDLE IN

IN CLOSE POSITION”

CLOSE POSITION”

4. “SEAT — ARMED TOP

“ARMED TOP AND BOT-

AND BOTTOM

TOM, PILOT/MCO IN

COMMAND

WINDOW (as indicated),

EJECT

STRAPPED IN SIX WAYS”

(as briefed), STRAPPED

IN SIX WAYS”

5. “STAB AUG”

“ALL ON”

6. “ATLS”

“ON”

7. ALL CIRCUIT BREAK-

“ALL IN”

ERS SET”

8. “MASTER TEST

“OFF”

SWITCH”

9. “BIDIRECTIONAL”

“NORMAL”

Change 2

239

NAVAIR 01-F14AAP-1B

RIO CHALLENGE

PILOT REPLY

10. “COMPASS, STANDBY

“COMPASS SYNCHRO-

GYRO, TURN

NIZED, STANDBY GYRO

NEEDLE, AND

ERECT, GOOD TURN

NEEDLE, ALTIMETER SET

ALTIMETER”

(LOCAL SETTING) ”

CV — Approaching

CAT on Director’s Signal

11. “WINGS” (visually

“20°, AUTO, BOTH LIGHTS

checked)

OUT”

12. “FLAPS AND SLATS”

AS REQUIRED

(visually checked)

13. “SPOILERS AND

“SPOILER MODULE ON,

ANTISKID”

SPOILER BRAKES

SELECTED” (field)

“SPOILER MODULE ON,

SPOILER BRAKES OFF”

(CV)

14. “TRIM”

“0,0,0” (field) AS REQUIRED

(CV)

15. “HARNESS —

“LOCKED”

LOCKED”

16. “CONTROLS” (RIO

“FREE, 33_ AFT STICK,

visually check for full

FULL SPOILER DEFLEC-

spoiler deflection)

TION, LEFT AND RIGHT,

HYDRAULICS 3,000 PSI”

17. “ALL WARNING AND

“ALL WARNING AND CAU-

CAUTION LIGHTS

TION LIGHTS OUT”

OUT”

ASHORE — In Takeoff Position

18. “ANTISKID/SPOILER

“BOTH” (if operable)

BRAKES”

240 Change 3

NAVAIR 01-F14AAP-1B

ASCENT CHECKLIST

At level-off or 15,000 feet (whichever occurs first):

1. Cabin pressurization

Check

2. Fuel transfer

Check

3. In-flight OBC

Run

Failure of the CIA class I OBC to run could be

an indication of shorted master arm circuitry

and possible failure of the LAU-7 detent to

engage, resulting in inadvertent AIM-9 sepa-

ration from the aircraft during an arrested

landing.

PRELAND AND DESCENT

1. HOOK/HOOK BYPASS

As Desired

2. Exterior lights

As Desired

3. Compass/BDHI

Check With Mag Compass

4. Wing-sweep mode switch

As Desired

5. ANTI SKID SPOILER BK switch

BOTH

(if operable, CV-OFF)

6. Altimeter

Set

7. Radar altimeter

On/BIT Check

8. Fuel quantity and distribution

Check

9. Armament

Safe

10. CANOPY DEFOG/CABIN AIR lever

DEFOG

11. ANTI-ICE switch

AUTO/OFF

12. PDCP

Set

13. ARA-63/ACLS

ON/BIT Check

241

NAVAIR 01-F14AAP-1B

14. DECM switch

STBY

15. AN/ALE-47 DCDU, MODE/PWR SWITCH . . . OFF

If LAU-7 mounted stores are loaded, perform

steps 16 and 17 with the aircraft in a safe area

and headed in a direction where inadvertent

gun firing would not cause damage.

16. WEAPON SELECT

Cycle to GUN, Then OFF

If HOT TRIG light illuminates with MASTER

ARM switch OFF or CI/PSU acronym was

displayed during in-flight OBC, perform step

17.

17. STA 1/8 AIM-9 REL PWR cb (6D4, 6D3)

Pull

18. WCS switch

STBY or XMT (pulse)

The RIO should place WCS switch to STBY

or XMT (pulse) on final approach to prevent

unnecessary exposure of flight deck personnel

to RF radiation hazards.

19. [T] Resolution run

Completed

242

Change 2

NAVAIR 01-F14AAP-1B

Note

Before reconnaissance system shutdown, run

film leader to protect target imagery from

inadvertent exposure during film download.

20. [T] FRAME switch

OFF

21. [T] PAN switch

OFF

22. [T] IRLS switch

OFF

23. [T] FILM switch

OFF

CAUTION

Before selecting system switch to OFF, delay

15 seconds for sensor shutdown, IR door to

close, and mount to drive to vertical.

24. [T] CPS system switch

OFF

LANDING CHECKLIST

1. Wing-sweep mode switch

20° AUTO

2. Wheels

Three DN (check transition light out)

3. SAS

4. Flaps

Full DN

5. DLC

Checked

6. Hook

As Desired

7. Harness

Locked

8. Speedbrakes

EXT (out)

9. Brakes

Check

10. Fuel

Check

243

NAVAIR 01-F14AAP-1B

POSTLANDING — PILOT

1. Speedbrake switch

RET

2. ANTISKID SPOILER BK switch

OFF

3. Flaps and slats

4. WING SWEEP MODE switch

BOMB

CAUTION

Ensure that emergency WING SWEEP handle

and wings move to 55_.

5. EMERGENCY WING SWEEP handle

OV SW

6. Avionics

OFF

7. DCP

Verify & record codes (FAIL, FLT, IBIT)

8. Right throttle

OFF

9. HYD TRANSFER PUMP switch

SHUTOFF

(after BIDI check)

10. Ejection seats

SAFE (coordinate with RIO)

11. Ordnance

Dearm (field)

12. Wheels

Chocked

13. Parking brake

Pull

CAUTION

Do not pull parking brake subsequent to a field

landing if the brakes have been used exten-

sively.

14. UHF FUNCTION selector

OFF

15. OXYGEN switch

OFF

After removing mask, turn oxygen off.

244

NAVAIR 01-F14AAP-1B

16. EMERG generator switch

OFF

17. Standby attitude gyro

Cage

18. Left throttle

OFF (alert RIO)

19. Lights

OFF

20. EJECT CMD indicator

Verify PILOT

21. CANOPY handle

OPEN (alert RIO)

POSTLANDING — RIO

1. Ejection seat

Safe

2. EJECT CMD lever

PILOT

3. Radar beacon

OFF

4. IFF

Mode 4 Hold, Then OFF

5. Data link

OFF

6. DECM switch

OFF

7. CDNU

RECORD BLENDED/

GPS/FREE INERTIAL POS

Record RNAV page data after aircraft parked.

8. NAV MODE switch

OFF

Requires 10 seconds to restore history data prior to

removal of electrical power.

9. RECORD switch

OFF

Requires at least 20 seconds to allow tape to unthread

prior to removal of electrical power.

10. IR/TV power switch

OFF

11. WCS

OFF

12. PTID power switch

OFF

13. LIQ COOLING switch

OFF

14. Standby attitude gyro

Cage

15. OXYGEN switch

OFF

16. U/VHF MODE selector

OFF

17. [T] CPS switches

OFF

245

F-14D. FLIGHT MANUAL (2004) - page 19