|
|
|
|
|
|
|
III
|
FUEL(2)
|
|
RANGE IN AIR MILES
|
U.S.
|
IMP
|
|
STATUE
|
NAUTICAL
|
GALS
|
|
28 U.S. (23 IMP.) GALLONS NOT AVAILABLE IN FLIGHT
|
158
|
131
|
|
540
|
470
|
130
|
108
|
|
500
|
430
|
120
|
100
|
|
____420____
|
____360____
|
100
|
83
|
|
330
|
290
|
80
|
67
|
|
250
|
210
|
60
|
50
|
|
165
|
145
|
40
|
33
|
|
85
|
70
|
20
|
17
|
|
|
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
|
203
|
263
|
28
|
60
|
50
|
|
12000
|
2300
|
204
|
252
|
28
|
58
|
48
|
|
9000
|
2200
|
202
|
238
|
28
|
55
|
46
|
|
6000
|
2200
|
203
|
228
|
28
|
53
|
44
|
|
3000
|
2200
|
203
|
218
|
28
|
50
|
42
|
|
S.L.
|
2200
|
203
|
209
|
28
|
48
|
40
|
|
|
|
|
(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___ |
|