|
|
|
|
|
II
|
FUEL(2)
|
|
RANGE IN AIR MILES
|
U.S.
|
|
STATUE
|
NAUTICAL
|
GALS
|
|
33 U.S. (27 IMP.) GALLONS NOT AVAILABLE IN FLIGHT
|
243
|
|
650
|
570
|
210
|
|
590
|
510
|
190
|
|
530
|
460
|
170
|
|
460
|
400
|
150
|
|
____400____
|
____350____
|
130
|
|
310
|
270
|
100
|
|
250
|
215
|
80
|
|
190
|
165
|
60
|
|
120
|
105
|
40
|
|
60
|
55
|
20
|
|
|
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.
|
|
15000
|
2450
|
211
|
274
|
F.T.
|
86
|
72
|
|
12000
|
2300
|
216
|
268
|
F.T.
|
83
|
69
|
|
9000
|
2150
|
220
|
260
|
33
|
81
|
67
|
|
6000
|
2150
|
223
|
250
|
34
|
78
|
65
|
|
3000
|
2150
|
225
|
240
|
34
|
75
|
62
|
|
S.L.
|
2150
|
224
|
230
|
34
|
72
|
60
|
|
|
NOTE:After belly tankis emptied use sheet 3. After Belly tank is dropped,
use sheet 1. When carrying 500lb. bomb, use data below this line. |
|
(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 ___5000___FEET ALTITUTUDE. RETURN FUEL FLOWS TO TANKK ___FUSELAGE__ USE FUEL FROM TANKS IN THE FOLLOWING ORDER: _FUS.__TO_35__GAL., __REAR_WING,_ _FRONT_WING, _BALANCE_FUSELAGE___ |