Navair F-14B, Процедуры для чрезвычайных ситуаций

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NAVAIR 01-F14AAP-1B
198
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212
GEAR DOWN
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
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
50
Kn
HEAD
WIND
KCAS
NO
WIND
50
Kn
HEAD
WIND
MACH
OR
KIAS
NO
WIND
50
Kn
HEAD
WIND
0
200 160 6000 160 6 4 139 10,960 14,590 162 185 182
X
0
150 160 7000 160 7 4 139 8590 11,200 160 137 134
DE
X
100 160 8000 160 8 5 139 6340 8030 158 91 88
G
IN
D
80 160 9000 160 9 6 139 5470 6800 158 73 70
R
AG
I
60 160 9000 160 9 6 139 4640 5640 156 56 54
DR
A
40 160 7000 160 7 4 139 3800 4490 156 39 37
D
20 160 3000 160 3 2 139 2930 3310 156 20 20
200 160 6000 160 6 4 138 11,210 15,010 162 186 183
X
50
150 160 7000 160 7 4 138 8770 11,510 160 138 134
D
EX
5
100 160 7000 160 7 4 138 6490 8290 158 92 88
IND
E
80 160 8000 160 8 5 138 5580 6990 158 73 70
A
G I
N
60 160 8000 160 8 5 138 4710 5770 156 55 54
D
RA
G
40 160 7000 160 7 4 138 3850 4570 156 38 37
D
R
20 160 3000 160 3 2 138 2950 3340 156 19 19
00
200 155 5000 155 5 3 137 11,590 15,670 162 190 186
X
10
0
150 155 6000 155 6 4 137 9040 11,960 160 140 136
D
EX
1
100 155 6000 155 6 4 137 6660 8570 158 92 90
IND
E
80 155 7000 155 7 4 137 5700 7210 158 74 72
A
G I
N
60 155 7000 155 7 4 137 4800 5920 156 56 54
D
RA
G
40 155 7000 155 7 4 137 3900 4660 156 38 36
D
R
20 155 3000 155 3 2 137 2970 3390 156 20 19
0
200 155 4000 155 4 2 136 11,990 16,360 162 192 189
X
150
150 155 5000 155 5 3 136 9320 12,450 160 142 138
D
EX
1
100 155 6000 155 5 4 136 6790 8800 158 93 90
IND
E
80 155 6000 155 5 4 136 5830 7440 158 75 72
A
G I
N
60 155 6000 155 5 4 136 4890 6090 156 56 54
D
RA
G
40 155 6000 155 5 4 136 3950 4760 156 38 37
D
R
20 155 2000 155 2 1 136 3000 3440 154 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 30 COUNTS TO DRAG INDEX.
0–F52P–33–8
NOTES
NAVAIR 01–F14AAP–1B
198 Change 2