|
|
|
|
|
|
V (MAX. RANGE)
|
FUEL(2)
|
|
RANGE IN AIR MILES
|
U.S.
|
|
STATUE
|
NAUTICAL
|
GALS
|
|
33 U.S. (27 IMP.) GALLONS NOT AVAILABLE IN FLIGHT
|
243
|
|
1025
|
890
|
210
|
|
920
|
800
|
190
|
|
825
|
715
|
170
|
|
730
|
640
|
150
|
|
____630____
|
____550____
|
130
|
|
490
|
425
|
100
|
|
390
|
340
|
80
|
|
290
|
250
|
60
|
|
190
|
165
|
40
|
|
100
|
90
|
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
|
1950
|
172
|
223
|
26
|
44
|
37
|
|
12000
|
1850
|
178
|
220
|
27
|
43
|
36
|
|
9000
|
1800
|
175
|
206
|
27
|
40
|
33
|
|
6000
|
1800
|
175
|
197
|
27
|
38
|
32
|
|
3000
|
1800
|
171
|
184
|
26
|
36
|
30
|
|
S.L.
|
1800
|
168
|
173
|
26
|
34
|
28
|
|
|
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___ |