F16C/D. FLIGHT MANUAL (2002) - page 39
T.O. GR1F16CJ1CL2
P29/PW/CFT
Diversion Decision Divert
DATA BASIS ESTIMATED
ENGINE F100PW229
CONDITIONS:
D
MIL CLIMB AT 433 KIAS OR
OPTIMUM ALTITUDE MACH
NO., WHICHEVER IS LESS
D
DESCEND AT IDLE,
221 KIAS
D
STANDARD DAY
D
NO FUEL RESERVE
D
ZERO WIND
D
ALL DESCENTS ARE
TO SEA LEVEL
D
DRAG INDEX = 55
NOTES:
D
4.0% RANGE GAIN FOR 10 KTS TAILWIND.
D
2.5% RANGE LOSS FOR 10 KTS HEADWIND.
D
SUBTRACT 2.5 NM FROM DESCENT DISTANCE FOR EACH
1000 FT OF DESTINATION ELEVATION.
D
TOTAL DIVERT RANGE AT CURRENT ALTITUDE INCLUDES
CRUISE AND DESCENT, AND TOTAL DIVERT RANGE AT OPTI
MUM ALTITUDE INCLUDES CLIMB, CRUISE, AND DESCENT.
IF YOU ARE AT SEA LEVEL
FUEL
ON
REMAIN
AT SEA LEVEL
CLIMB TO OPT ALTITUDE
DESCEND
ON
BOARD
AT SEA LEVEL
TOTAL
FROM
FUEL USED
BOARD
-LB
TOTAL DIVERT
RANGE-NM
ALT/MACH
TOTAL
DIVERT
RANGE-NM
FROM
OPT ALT
-NM
FUEL USED
IN DESCENT
-LB
200
19
5.0K/0.46
20
16
102
400
37
15.0K/0.55
45
38
200
600
55
25.0K/0.68
77
60
267
800
72 0.43M
30.0K/0.73
110
71
298
1000
90
35.0K/0.78
146
83
330
1500
134
40.0K/0.84
241
97
367
2000
178
40.0K/0.84
337
97
367
IF YOU ARE AT 5000 FEET
FUEL
ON
REMAIN
AT 5000 FT
CLIMB TO OPT ALTITUDE
DESCEND
ON
BOARD
AT 5000 FT
TOTAL
FROM
FUEL USED
BOARD
-LB
TOTAL DIVERT
RANGE-NM*
ALT/MACH
TOTAL
DIVERT
RANGE-NM
FROM
OPT ALT
-NM
FUEL USED
IN DESCENT
-LB
200
26
5.0K/0.46
26
16
102
400
46
15.0K/0.55
51
38
200
600
66
30.0K/0.72
86
71
298
800
85 0.47M
35.0K/0.78
121
83
330
1000
105
35.0K/0.78
158
83
330
1500
155
40.0K/0.84
254
97
367
2000
204
40.0K/0.84
350
97
367
*START DESCENT AT 16 NM. 102 LB FUEL USED IN DESCENT.
Figure P11.(Sheet 1)