Navair F-14B, Emergency Procedure Tabs

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NAVAIR 01-F14AAP-1B
196
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210
GEAR UP
FLAPS DOWN
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
INBD
DIST
(nmi)
MACH
OR
KIAS
ALT
(feet)
MACH
OR
KIAS
DIST (nmi) KCAS
FUEL REQ
(lbs)
MACH
OR
KIAS
DIST (nmi)
INBD
DIST
(nmi)
MACH
OR
KIAS
ALT
(feet)
MACH
OR
KIAS
NO
WIND
50
Kn
HEAD
WIND
KCAS
NO
WIND
50
Kn
HEAD
WIND
MACH
OR
KIAS
NO
WIND
50
Kn
HEAD
WIND
0
200 180 8000 165 8 5 147 10,020 12,900 172 179 173
X
0
150 180 9000 165 9 6 147 7930 10,020 170 133 129
DE
X
100 180 10,000 165 10 7 147 5950 7300 170 89 86
G
IN
D
80 180 10,000 165 10 7 147 5190 6260 172 72 70
R
AG
I
60 180 9000 165 9 6 147 4430 5420 170 55 54
DR
A
40 180 6000 165 6 4 147 3650 4230 170 38 37
D
20 180 3000 165 3 2 147 2850 3160 170 20 20
200 180 8000 165 8 5 146 10,290 13,340 170 180 177
X
50
150 180 8000 165 8 5 146 8180 10,410 168 134 131
D
EX
5
100 180 9000 165 9 6 146 6100 7540 166 90 88
IND
E
80 180 9000 165 9 6 146 5310 6440 166 72 70
A
G I
N
60 180 8000 165 8 5 146 4510 5380 166 56 54
D
RA
G
40 180 6000 165 6 4 146 3700 4310 164 38 36
D
R
20 180 3000 165 3 2 146 2870 3200 164 20 19
00
200 175 7000 165 7 5 144 10,630 13,910 170 183 180
X
10
0
150 175 7000 165 7 5 144 8420 10,810 168 134 133
D
EX
1
100 175 8000 165 8 5 144 6240 7780 166 90 88
IND
E
80 175 8000 165 8 5 144 5410 6630 166 72 71
A
G I
N
60 175 8000 165 8 5 144 4580 5490 164 55 54
D
RA
G
40 175 6000 165 6 4 144 3750 4390 164 38 38
D
R
20 175 3000 165 3 2 144 2900 3240 164 20 20
0
200 170 6000 165 6 4 143 11,000 14,510 170 183 180
X
150
150 170 6000 165 6 4 143 8680 11,240 168 137 136
D
EX
1
100 170 7000 165 7 4 143 6390 8040 166 91 89
IND
E
80 170 8000 165 8 5 143 5510 6800 166 74 72
A
G I
N
60 170 8000 165 8 5 143 4650 5620 164 56 54
D
RA
G
40 170 6000 165 6 4 143 3800 4470 162 38 37
D
R
20 170 3000 165 3 2 143 2920 3280 162 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 40 COUNTS TO DRAG INDEX.
0–F52P–33–6
NOTES
NAVAIR 01–F14AAP–1B
196 Change 2