NAVAIR 01-F14AAP-1B
198
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212
GEAR DOWN
FLAPS DOWN
BINGO
48,000 lb
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
INBD
MACH
MACH
DIST (nmi)
FUEL REQ
(lbs)
MACH
DIST (nmi)
INBD
DIST
(nmi)
MACH
OR
KIAS
ALT
(feet)
MACH
OR
KIAS
NO
WIND
50
Kn
HEAD
WIND
KCAS
NO
WIND
50
Kn
HEAD
WIND
MACH
OR
KIAS
NO
WIND
50
Kn
HEAD
WIND
0
200
160
6000
160
6
4
139 10,960 14,590
162
185
182
X
0
150
160
7000
160
7
4
139
8590 11,200
160
137
134
DE
X
100
160
8000
160
8
5
139
6340
8030
158
91
88
G
IN
D
80
160
9000
160
9
6
139
5470
6800
158
73
70
R
AG
I
60
160
9000
160
9
6
139
4640
5640
156
56
54
DR
A
40
160
7000
160
7
4
139
3800
4490
156
39
37
D
20
160
3000
160
3
2
139
2930
3310
156
20
20
200
160
6000
160
6
4
138 11,210 15,010
162
186
183
X
50
150
160
7000
160
7
4
138
8770 11,510
160
138
134
D
EX
5
100
160
7000
160
7
4
138
6490
8290
158
92
88
IND
E
80
160
8000
160
8
5
138
5580
6990
158
73
70
A
G I
N
60
160
8000
160
8
5
138
4710
5770
156
55
54
D
RA
G
40
160
7000
160
7
4
138
3850
4570
156
38
37
D
R
20
160
3000
160
3
2
138
2950
3340
156
19
19
00
200
155
5000
155
5
3
137 11,590 15,670
162
190
186
X
10
0
150
155
6000
155
6
4
137
9040 11,960
160
140
136
D
EX
1
100
155
6000
155
6
4
137
6660
8570
158
92
90
IND
E
80
155
7000
155
7
4
137
5700
7210
158
74
72
A
G I
N
60
155
7000
155
7
4
137
4800
5920
156
56
54
D
RA
G
40
155
7000
155
7
4
137
3900
4660
156
38
36
D
R
20
155
3000
155
3
2
137
2970
3390
156
20
19
0
200
155
4000
155
4
2
136 11,990 16,360
162
192
189
X
150
150
155
5000
155
5
3
136
9320 12,450
160
142
138
D
EX
1
100
155
6000
155
5
4
136
6790
8800
158
93
90
IND
E
80
155
6000
155
5
4
136
5830
7440
158
75
72
A
G I
N
60
155
6000
155
5
4
136
4890
6090
156
56
54
D
RA
G
40
155
6000
155
5
4
136
3950
4760
156
38
37
D
R
20
155
2000
155
2
1
136
3000
3440
154
20
20
•
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
•
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
NOTES
NAVAIR 01–F14AAP–1B
198
Change 2
Summary of Contents for F-14B
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Page 44: ...NAVAIR 01 F14AAP 1B 22 28 EJECT EGRESS...
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Page 52: ...NAVAIR 01 F14AAP 1B 30 36...
Page 66: ...NAVAIR 01 F14AAP 1B 44 50 ENG...
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Page 92: ...NAVAIR 01 F14AAP 1B 70 76...
Page 130: ...NAVAIR 01 F14AAP 1B 106b 114...
Page 144: ...NAVAIR 01 F14AAP 1B 120 128 FUEL...
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Page 176: ...NAVAIR 01 F14AAP 1B 146 158 LAND LAND GEAR...
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Page 194: ...NAVAIR 01 F14AAP 1B 162b 176...
Page 201: ...NAVAIR 01 F14AAP 1B 169 183 EMERGENCY FIELD ARRESTMENT GUIDE SHEET 2 169 SE...
Page 202: ...NAVAIR 01 F14AAP 1B 170 184 SE...
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Page 215: ...NAVAIR 01 F14AAP 1B 183 197 2 TO...
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Page 302: ...NAVAIR 01 F14AAP 1B 332...
Page 316: ...NAVAIR 01 F14AAP 1B 276 300 276 Change 3...
Page 319: ...NAVAIR 01 F14AAP 1B 279 295 AC RIGHT MAIN CIRCUIT BREAKER PANEL LEFT AFT PANEL NO 2...
Page 320: ...NAVAIR 01 F14AAP 1B 280 296 AC ESSENTIAL NO 2 PHASE A CIRCUIT BREAKER PANEL LEFT PANEL NO 3...
Page 323: ...NAVAIR 01 F14AAP 1B 283 299 DC ESSENTIAL NO 1 CIRCUIT BREAKER PANEL RIGHT SIDE PANEL NO 6...
Page 326: ...NAVAIR 01 F14AAP 1B 286 302 DC MAIN CIRCUIT BREAKER PANEL RIGHT AFT PANEL NO 8 UPPER SEGMENT...
Page 327: ...NAVAIR 01 F14AAP 1B 287 303 DC MAIN CIRCUIT BREAKER PANEL RIGHT AFT PANEL NO 8 LOWER SEGMENT...
Page 331: ...NAVAIR 01 F14AAP 1B 291 307 AIRCRAFT SERVICING LOCATIONS...
Page 334: ...NAVAIR 01 F14AAP 1B 294 310 AIRCRAFT SERVICING DATA SHEET 3...
Page 335: ...NAVAIR 01 F14AAP 1B 295 311 AIRCRAFT SERVICING DATA SHEET 4...
Page 336: ...NAVAIR 01 F14AAP 1B 296 312 AIRCRAFT SERVICING DATA SHEET 5 296 Change 2...
Page 337: ...NAVAIR 01 F14AAP 1B 297 313 AIRCRAFT SERVICING DATA SHEET 6...
Page 338: ...NAVAIR 01 F14AAP 1B 298 314 AIRCRAFT SERVICING DATA SHEET 7...
Page 339: ...NAVAIR 01 F14AAP 1B 299 315 AIRCRAFT SERVICING DATA SHEET 8 299 300 blank...
Page 340: ...NAVAIR 01 F14AAP 1B 300 316...