Navair F-14B, Emergency Procedure Tabs

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NAVAIR 01-F14AAP-1B
197
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211
GEAR DOWN
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 .40 19,000 .44 28 15 187 6230 8610 214 159 143
X
0
150 .40 19,000 .44 28 15 187 5240 7030 212 122 109
DE
X
100 .40 18,000 .43 26 14 187 4250 5510 210 85 76
G
IN
D
80 .40 16,000 .41 23 12 187 3850 4910 210 70 63
R
AG
I
60 .40 13,000 .40 18 9 187 3440 4310 210 55 50
DR
A
40 210 7000 210 10 5 187 3000 3680 210 38 36
D
20 210 1000 210 1 1 187 2520 2910 208 20 20
200 .40 18,000 .42 25 13 186 6520 9180 210 161 146
X
50
150 .40 18,000 .42 25 13 186 5450 7450 210 123 111
D
EX
5
100 .40 17,000 .41 23 12 186 4390 5780 208 85 77
IND
E
80 .40 16,000 .41 22 11 186 3960 5120 208 70 64
A
G I
N
60 200 12,000 200 16 8 186 3530 4490 208 54 52
D
RA
G
40 205 8000 205 11 5 186 3060 3780 206 37 37
D
R
20 205 2000 205 3 1 186 2550 2970 206 19 20
00
200 .40 17,000 .41 22 12 185 6820 9800 206 162 148
X
10
0
150 .40 17,000 .41 22 12 185 5670 7900 206 124 112
D
EX
1
100 .40 17,000 .41 22 12 185 4530 6050 204 86 77
IND
E
80 .40 15,000 .40 19 10 185 4080 5350 204 70 64
A
G I
N
60 200 12,000 200 15 8 185 3610 4650 202 54 51
D
RA
G
40 200 8000 200 10 5 185 3120 3890 202 37 36
D
R
20 200 1000 200 1 1 185 2580 3030 202 20 20
0
200 .40 15,000 .40 18 9 183 7160 10,500 204 165 152
X
150
150 .40 16,000 .40 20 10 183 5890 8380 204 125 114
D
EX
1
100 .40 16,000 .40 20 10 183 4680 6360 204 86 78
IND
E
80 .40 14,000 .39 17 9 183 4190 5590 202 71 64
A
G I
N
60 200 12,000 200 15 7 183 3700 4820 202 55 50
D
RA
G
40 200 8000 200 10 5 183 3170 4010 202 38 36
D
R
20 200 2000 200 2 1 183 2610 3090 202 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 70 COUNTS TO DRAG INDEX.
0–F52P–33–7
NOTES
NAVAIR 01–F14AAP–1B
Change 2 197