II
FUEL(2)
RANGE IN AIR MILES
U.S.
IMP
STATUTE
NAUTICAL
GALS
 AT S.L.
AT 1200
  AT S.L.
AT 1200
158*
132
______
485
______
420
130
108
445
390
120
100
410
355
110
92
370
325
100
83
335
290
90
75
300
260
80
67
260
225
70
58
225
195
60
50
185
160
50
42
150
130
40
33
110
95
30
25
75
65
20
17
35
30
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
2600
217
188
31
84
70
15000
2600
226
196
31
80
67
12000
2600
228
198
31
77
64
9000
2600
230
199
31
74
62
6000
2600
231
200
31
71
51
3000
2600
232
201
31
68
57
S.L.
2600
232
201
31
65
54
(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__
* 33 GAL. FOR WARM-UP, TAKE-OFF AND CLIMB, NOT AVAILABLE IN FLIGHT