|
|
V (MAX. RANGE)
|
FUEL(2)
|
RANGE IN AIR MILES
|
U.S.
|
IMP
|
STATUTE
|
NAUTICAL
|
GALS
|
AT S.L.
|
AT 1200
|
AT S.L.
|
AT 1200
|
170
|
142
|
|
780
|
|
680
|
140
|
117
|
|
725
|
|
630
|
130
|
108
|
|
670
|
|
580
|
120
|
100
|
|
615
|
|
530
|
110
|
92
|
|
560
|
|
485
|
100
|
83
|
|
505
|
|
435
|
90
|
75
|
|
445
|
|
385
|
80
|
67
|
|
390
|
|
340
|
70
|
58
|
|
335
|
|
290
|
60
|
50
|
|
280
|
|
240
|
50
|
42
|
|
225
|
|
195
|
40
|
33
|
|
165
|
|
145
|
30
|
25
|
|
110
|
|
95
|
20
|
17
|
|
55
|
|
50
|
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.
|
25000
|
2250
|
159
|
138
|
F.T
|
45
|
38
|
20000
|
2000
|
168
|
146
|
25
|
44
|
37
|
15000
|
1800
|
171
|
148
|
25
|
41
|
34
|
12000
|
1800
|
168
|
146
|
25
|
38
|
32
|
9000
|
1800
|
163
|
141
|
24
|
36
|
30
|
6000
|
1800
|
155
|
135
|
24
|
33
|
28
|
3000
|
|
|
|
|
|
|
S.L.
|
|
|
|
|
|
|
(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 |
|