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|  APPENDIX H
FLIGHT PLANNING DATA
T-39 NORMAL THRUST CLIMB
TWO ENGINES
T-39 FUEL FLOW
TWO ENGINES
TAS
PPH
ALT
SL
300
3000
10,000'
300
2400
ALT
TIME
FUEL DIST
15,000'
300
2200
(mins)
(lbs.)
(nm)
(1000's)
360
2300
10
3
200
12
20,000'
360
2000
15
5
350
22
23,000'
360
1900
20
7
430
32
390
2100
21
8
480
38
420
2200
23
9
500
40
25
10
600
48
25,000'
360
1800
27
12
650
57
390
1950
30
13
780
72
420
2100
33
16
800
80
35
18
920
102
27,000'
360
1750
37
20
1000
118
390
1850
39
26
1150
147
420
2000
41
31
1500
233
29,000'
360
1650
43
37
1680
265
420
1900
45
44
1800
305
31,000'
360
1500
1. START/TAXI/TAKEOFF CONSUMES 400# (JP-5) AND IS NOT
390
1650
INCLUDED IN ABOVE FIGURES.
420
1800
33,000
420
1750
2. FUEL REQUIRED FOR APPROACH: 400#.
35,000'
390
1550
420
1650
3. RESERVE FUEL COMPUTED AT 175 KIAS, 10K MSL, 1800 PPH
FOR A 14,000# AIRCRAFT IS 600#.
37,000'
390
1500
420
1600
4. TOTAL FUEL: 7200# (JP-5), 6900# (JP-4)
3+10 FOR VNAV AND 4+00 FOR INAV.
39,000'
390
1450
420
1550
5. DESCENT: ALLOW 30#, 2 MINUTES, AND 10 NM PER 5000 FEET
OF ALTITUDE.
41,000'
390
1350
420
1450
6.
ENROUTE BETWEEN LOW-LEVELS:
43,000'
420
1300
10.5K, 300 KTAS, 2400 PPH
16.5K, 300 KTAS, 2000 PPH
45,000'
420
1200
H-1
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