Navair F-14B, Emergency Procedure Tabs, Page: 231 / 355

NAVAIR 01-F14AAP-1B
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209
GEAR UP
FLAPS UP
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
100
Kn
HEAD
WIND
KCAS
NO
WIND
100
Kn
HEAD
WIND
MACH
OR
KIAS
NO
WIND
100
Kn
HEAD
WIND
0
200 .44 24,000 .59 52 30 196 4650 5750 260 149 135
X
0
150 .44 23,000 .58 49 28 196 4060 4930 258 116 106
DE
X
100 .44 18,000 .51 37 21 196 3460 4120 258 81 77
G
IN
D
80 .44 16,000 .50 33 18 196 3200 3770 256 66 64
R
AG
I
60 .44 13,000 .47 26 14 196 2930 3400 256 51 50
DR
A
40 .44 9000 .43 18 9 196 2650 3000 256 35 36
D
20 .44 4000 .40 8 4 196 2340 2540 256 18 20
200 .43 23,000 .52 45 26 194 4940 6230 246 150 136
X
50
150 .43 22,000 .51 43 24 194 4280 5290 244 116 106
D
EX
5
100 .43 19,000 .50 36 20 194 3600 4350 244 82 74
IND
E
80 .43 16,000 .47 30 16 194 3320 3960 244 67 63
A
G I
N
60 .43 14,000 .45 26 14 194 3020 3540 242 52 50
D
RA
G
40 .43 9000 .41 16 8 194 2710 3110 242 36 36
D
R
20 .43 4000 .40 7 4 194 2370 2600 242 19 19
00
200 .42 21,000 .50 38 21 192 5240 6780 244 152 139
X
10
0
150 .42 21,000 .50 38 21 192 4500 5680 244 117 108
D
EX
1
100 .42 18,000 .47 32 17 192 3740 4600 242 82 76
IND
E
80 .42 16,000 .45 28 15 192 3430 4160 242 68 63
A
G I
N
60 .42 13,000 .43 22 12 192 3110 3710 242 52 50
D
RA
G
40 .42 9000 .40 15 8 192 2770 3220 240 37 37
D
R
20 .42 4000 230 7 3 192 2410 2660 240 19 20
0
200 .40 20,000 .49 33 18 189 5560 7360 228 152 142
X
150
150 .40 19,000 .48 31 17 189 4730 6100 230 117 109
D
EX
1
100 .40 17,000 .46 28 15 189 3890 4870 230 82 76
IND
E
80 .40 16,000 .45 26 14 189 3550 4370 230 68 63
A
G I
N
60 .40 14,000 .43 22 12 189 3200 3860 230 52 49
D
RA
G
40 .40 9000 220 14 7 189 2830 3340 230 37 36
D
R
20 .40 5000 220 8 4 189 2440 2720 228 19 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 80 COUNTS TO DRAG INDEX.
0–F52P–33–5
NOTES
NAVAIR 01–F14AAP–1B
Change 2 195