|
|
|
|
|
|
|
III
|
FUEL(2)
|
|
RANGE IN AIR MILES
|
U.S.
|
|
STATUE
|
NAUTICAL
|
GALS
|
|
33 U.S. (27 IMP.) GALLONS NOT AVAILABLE IN FLIGHT
|
243
|
|
880
|
570
|
210
|
|
800
|
690
|
190
|
|
715
|
620
|
170
|
|
630
|
545
|
150
|
|
____545____
|
____470____
|
130
|
|
420
|
360
|
100
|
|
340
|
290
|
80
|
|
250
|
220
|
60
|
|
165
|
145
|
40
|
|
80
|
70
|
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
|
2300
|
198
|
257
|
28
|
59
|
49
|
|
12000
|
2300
|
200
|
247
|
28
|
57
|
47
|
|
9000
|
2200
|
197
|
233
|
28
|
53
|
44
|
|
6000
|
2200
|
198
|
223
|
28
|
51
|
42
|
|
3000
|
2200
|
199
|
214
|
28
|
49
|
41
|
|
S.L.
|
2200
|
197
|
202
|
28
|
47
|
39
|
|
|
|
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___ |
|