Navair F-14B, Emergency Procedure Tabs

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NAVAIR 01-F14AAP-1B
192
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206
GEAR UP
FLAPS DOWN
BINGO 48,000 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 29,000 .46 35 17 149 7790 11,130 188 131 108
X
0
150 .40 29,000 .45 35 17 149 6480 9010 186 102 84
DE
X
100 .40 28,000 .44 34 16 149 5180 6970 184 72 60
G
IN
D
80 .40 27,000 .44 32 15 149 4660 6170 184 60 50
R
AG
I
60 .40 23,000 .40 27 12 149 4120 5440 182 48 40
DR
A
40 .40 17,000 175 19 8 149 3530 4590 182 35 30
D
20 195 6000 185 6 2 149 2830 3570 182 19 19
200 .40 28,000 .44 33 15 148 8010 11,581 188 133 110
X
50
150 .40 28,000 .43 33 15 148 6630 9330 186 102 84
D
EX
5
100 .40 28,000 .43 33 15 148 5270 7150 184 72 60
IND
E
80 .40 27,000 .43 31 14 148 4730 6310 184 60 50
A
G I
N
60 .40 24,000 .41 27 12 148 4170 5490 182 48 40
D
RA
G
40 .40 17,000 175 18 7 148 3570 4670 182 35 31
D
R
20 195 7000 185 7 3 148 2860 3610 180 19 18
00
200 .40 27,000 .43 31 14 147 8250 12,070 188 134 112
X
10
0
150 .40 28,000 .43 32 15 147 6770 9650 186 103 85
D
EX
1
100 .40 28,000 .43 32 15 147 5370 7360 184 72 60
IND
E
80 .40 27,000 .43 31 14 147 4810 6460 184 60 50
A
G I
N
60 .40 23,000 .40 25 11 147 4230 5630 182 48 40
D
RA
G
40 195 15,000 170 16 6 147 3610 4810 182 35 31
D
R
20 195 7000 180 7 3 147 2880 3660 180 20 18
0
200 .40 26,000 .42 29 13 145 8480 12,570 186 136 112
X
150
150 .40 27,000 .43 30 13 145 6940 10,000 184 104 86
D
EX
1
100 .40 27,000 .43 30 13 145 5470 7580 182 73 60
IND
E
80 .40 26,000 .41 29 13 145 4890 6640 180 61 50
A
G I
N
60 .40 23,000 .39 25 10 145 4290 5750 180 48 40
D
RA
G
40 165 15,000 170 15 6 145 3650 4900 180 35 32
D
R
20 195 7000 180 7 2 145 2900 3710 178 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–33–2
NOTES