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
158*
132
______
755
______
655
130
108
695
605
120
100
640
555
110
92
580
505
100
83
520
455
90
75
465
405
80
67
405
350
70
58
350
300
60
50
290
250
50
42
230
200
40
33
175
150
30
25
115
100
20
17
60
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
2300
168
145
F.T.
46
38
20000
2050
180
156
F.T
45
37
15000
1800
183
159
26
42
35
12000
1800
181
157
25
40
33
9000
1800
178
154
25
37
31
6000
1800
172
149
25
34
28
3000
S.L.
(1) INDICATED ALTITUDE CORRECTED FOR FREE AIR TEMPERATURE
(2) ALLOW___28___U.S. GALS.,___23__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.__TO_35__GAL.,__REAR_WING, __FRONT_WING,_35 GAL_FUSELAGE_RESERVE__
* 28 GAL. FOR WARM-UP, TAKE-OFF AND CLIMB, NOT AVAILABLE IN FLIGHT