Navair F-14B, Emergency Procedure Tabs

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NAVAIR 01-F14AAP-1B
201
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215
GEAR UP
FLAPS UP
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 .75 41,000 .73 134 91 220 4350 5090 288 116 104
X
0
150 .75 37,000 .72 114 76 220 3880 4460 290 93 82
DE
X
100 .75 29,000 .62 79 51 220 3380 3870 288 69 62
G
IN
D
80 .75 25,000 .60 64 40 220 3170 3610 288 58 54
R
AG
I
60 .75 20,000 .57 47 29 220 2940 3310 288 47 44
DR
A
40 .75 14,000 .53 31 18 220 2670 2960 288 34 32
D
20 .75 7000 .46 15 8 220 2370 2550 286 19 18
200 .73 41,000 .73 118 80 215 4540 5340 272 115 100
X
50
150 .73 38,000 .72 105 70 215 4030 4660 272 92 80
D
EX
5
100 .73 30,000 .64 74 47 215 3500 4020 270 68 60
IND
E
80 .73 26,000 .60 60 38 215 3270 3740 270 58 52
A
G I
N
60 .73 21,000 .58 45 28 215 3010 3420 268 46 42
D
RA
G
40 .73 15,000 .51 30 18 215 2730 3050 268 34 31
D
R
20 .73 8000 .45 15 9 215 2400 2600 268 19 18
00
200 .72 40,000 .72 102 68 210 4750 5600 262 115 99
X
10
0
150 .72 39,000 .73 98 65 210 4190 4860 262 92 79
D
EX
1
100 .72 31,000 .65 70 44 210 3620 4170 262 68 60
IND
E
80 .72 27,000 .60 58 36 210 3370 3870 262 57 52
A
G I
N
60 .72 22,000 .58 44 26 210 3100 3540 260 46 43
D
RA
G
40 .72 16,000 .51 30 17 210 2790 3140 260 34 32
D
R
20 .72 8000 .44 14 8 210 2430 2660 260 18 18
0
200 .70 40,000 .72 93 61 207 4960 5880 258 115 98
X
150
150 .70 39,000 .73 89 58 207 4360 5080 256 92 78
D
EX
1
100 .70 32,000 .66 67 42 207 3750 4330 256 68 58
IND
E
80 .70 27,000 .60 53 32 207 3480 4020 254 58 50
A
G I
N
60 .70 22,000 .54 41 24 207 3190 3660 254 47 42
D
RA
G
40 .70 16,000 .49 28 16 207 2860 3240 254 34 31
D
R
20 .70 8000 .42 13 7 207 2470 2720 254 19 18
•
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–33–11
NOTES