Navair F-14B, Emergency Procedure Tabs

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NAVAIR 01-F14AAP-1B
202
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216
GEAR UP
FLAPS DOWN
BINGO 53,000 lb
TWIN ENG
DATE: SEPTEMBER 1987
DATA BASIS: ESTIMATED
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
100
Kn
HEAD
WIND
KCAS
NO
WIND
100
Kn
HEAD
WIND
MACH
OR
KIAS
NO
WIND
100
Kn
HEAD
WIND
0
200 .40 27,000 .45 32 15 156 8250 11,820 196 137 115
X
0
150 .40 27,000 .45 32 15 156 6810 9510 194 106 88
DE
X
100 .40 27,000 .45 32 15 156 5390 7270 192 75 62
G
IN
D
80 .40 25,000 .44 29 14 156 4820 6418 192 62 52
R
AG
I
60 .40 22,000 .41 25 12 156 4240 5560 192 50 42
DR
A
40 .40 15,000 180 16 7 156 3610 4710 190 36 32
D
20 195 6000 180 6 3 156 2870 3590 190 19 19
200 .40 27,000 .44 30 14 155 8490 12,310 194 138 116
X
50
150 .40 27,000 .45 31 15 155 6970 9840 194 106 89
D
EX
5
100 .40 26,000 .44 30 14 155 5490 7480 192 74 62
IND
E
80 .40 25,000 .43 28 13 155 4900 6570 192 62 52
A
G I
N
60 .40 22,000 .40 25 11 155 4300 5680 192 49 42
D
RA
G
40 .40 15,000 180 16 7 155 3650 4790 190 36 32
D
R
20 195 6000 180 6 2 155 2890 3640 190 19 19
00
200 .40 25,000 43 28 13 154 8570 12,840 194 139 119
X
10
0
150 .40 26,000 44 29 14 154 7140 10,210 192 106 90
D
EX
1
100 .40 26,000 44 29 14 154 5600 7710 192 75 63
IND
E
80 .40 25,000 43 28 13 154 4990 6730 190 62 52
A
G I
N
60 .40 22,000 40 24 11 154 4370 5810 190 50 42
D
RA
G
40 195 15,000 180 16 7 154 3700 4890 190 36 32
D
R
20 195 6000 180 6 2 154 2920 3700 190 19 19
0
200 .40 24,000 .42 26 12 152 9000 13,370 192 141 120
X
150
150 .40 25,000 .43 27 12 152 7320 10,580 192 107 92
D
EX
1
100 .40 25,000 .43 27 12 152 5710 7950 190 76 64
IND
E
80 .40 25,000 .42 27 12 152 5080 6910 188 62 52
A
G I
N
60 .40 22,000 .40 23 10 152 4430 5930 188 49 42
D
RA
G
40 195 14,000 180 14 6 152 3740 5000 188 36 32
D
R
20 195 6000 180 6 2 152 2940 3760 186 19 19
•
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).
0–F52P–33–12
NOTES