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STUDENT GUIDE
VISUAL NAVIGATION
T-1A FUEL FLOW
T-1A NORMAL THRUST CLIMB
TWO ENGINES
TWO ENGINES
ALT
ALT
TIME
FUEL
DIST
TAS
PPH
SL
300
1800
(1000's)
(mins)
(lbs.)
(NM)
10,000'
300
1200
10
3
150
12
15
5
230
22
360
1800
20
7
300
32
21
8
320
36
16,500'
330
1200
23
9
360
43
20,000'
360
1600
25
10
400
50
27
12
440
60
30
14
500
75
23,000'
420
1500
33
18
570
96
35
20
620
107
25000'
420
1400
37
23
670
124
39
28
760
154
27000'
420
1300
41
38
930
215
29000'
420
1250
31000'
420
1175
33000'
420
1150
35000'
420
1100
37000'
420
1075
39000'
420
1050
NOTE: Data in this figure to be used only to work the problems in this text. The In Flight
Guide is the only approved source for flight computations.)
1. FIGURES BASED ON 16,000# GW ON TAKEOFF (10,500# AIRCRAFT, 4500# FUEL, 3
CREWMEMBERS)
2. START/TAXI/TAKEOFF CONSUMES 200# (10 MIN) AND IS NOT INCLUDED IN ABOVE
FIGURES.
3. FUEL REQUIRED FOR APPROACH: 200#.
4. RESERVE FUEL PER USAF REGULATION 500#.
5. TOTAL FUEL: 4500# (4+00 FOR VNAV, 4+45 FOR ANAV)
6. DESCENT: ALLOW 10#, 1.5 MINUTES, AND 8 MILES PER 5000' OF ALTITUDE.
7. ENROUTE BETWEEN LOW-LEVELS:
10.5K---300 KTAS, 1300 PPH
16.5K---300 KTAS, 1200 PPH
Figure 6-14
6-19


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