|
|
|
IV
|
FUEL(2)
|
|
RANGE IN AIR MILES
|
U.S.
|
IMP
|
|
STATUTE
|
NAUTICAL
|
GALS
|
|
AT S.L.
|
AT 1200
|
AT S.L.
|
AT 1200
|
170
|
142
|
|
690
|
|
600
|
140
|
117
|
|
640
|
|
555
|
130
|
108
|
|
590
|
|
515
|
120
|
100
|
|
540
|
|
470
|
110
|
92
|
|
495
|
|
430
|
100
|
83
|
|
445
|
|
385
|
90
|
75
|
|
395
|
|
340
|
80
|
67
|
|
345
|
|
300
|
70
|
58
|
|
295
|
|
255
|
60
|
50
|
|
245
|
|
215
|
50
|
42
|
|
195
|
|
170
|
40
|
33
|
|
150
|
|
130
|
30
|
25
|
|
100
|
|
85
|
20
|
17
|
|
50
|
|
45
|
10
|
8
|
|
|
DENSITY ALT.
|
R.P.M.
|
I.A.S
|
T.A.S
|
M.P.
|
U.S
|
IMP.
|
|
IN FEET (1)
|
MP.H.
|
MP.H.
|
IN. Hg
|
G.P.H.
|
G.P.H.
|
|
20000
|
2250
|
186
|
161
|
F.T.
|
55
|
46
|
|
15000
|
2000
|
194
|
168
|
F.T.
|
52
|
43
|
|
12000
|
1900
|
194
|
168
|
29
|
50
|
42
|
|
9000
|
1850
|
194
|
168
|
29
|
48
|
40
|
|
6000
|
1850
|
194
|
168
|
29
|
45
|
37
|
|
3000
|
1850
|
192
|
167
|
29
|
43
|
36
|
|
S.L.
|
1800
|
190
|
165
|
29
|
41
|
34
|
| (1) INDICATED ALTITUDE CORRECTED FOR FREE AIR TEMPERATURE |
| (2) ALLOW___30___U.S. GALS.,___25__IMP. GALS. FOR WARM UP, TAKE-OOF AND CLIMB TO ___9000___FEET ALTITUTUDE. RETURN FUEL FLOWS TO TANKK ___FUSELAGE__ USE FUEL FROM TANKS IN THE FOLLOWING ORDER: _FUS.__FOR 15 MIN., BELLY, FUS. TO 35 GAL., REAR WING, FRONT WING, 35
GAL. FUS RESERVE_ |
| *30 GAL. FOR WARM-UP, TAKE-OFF AND CLIMB, NOT AVAILABLE IN FLIGHT |
|