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