|
|
|
|
|
|
II
|
FUEL(2)
|
|
RANGE IN AIR MILES
|
U.S.
|
IMP. |
|
STATUE
|
NAUTICAL
|
GALS
|
|
28 U.S. (23 IMP.) GALLONS NOT AVAILABLE IN FLIGHT
|
158
|
131
|
|
400
|
350
|
130
|
108
|
|
370
|
320
|
120
|
100
|
|
____310____
|
____270____
|
100
|
83
|
|
240
|
210
|
80
|
67
|
|
180
|
160
|
60
|
50
|
|
120
|
105
|
40
|
33
|
|
60
|
55
|
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
|
2500
|
216
|
280
|
F.T.
|
88
|
73
|
|
12000
|
2300
|
220
|
273
|
F.T.
|
84
|
70
|
|
9000
|
2150
|
225
|
265
|
34
|
82
|
68
|
|
6000
|
2150
|
223
|
253
|
34
|
79
|
66
|
|
3000
|
2150
|
227
|
244
|
34
|
76
|
63
|
|
S.L.
|
2150
|
227
|
233
|
34
|
73
|
61
|
|
|
|
(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___ |
|