|
|
|
|
|
|
|
I (MAX. CONT. POWER)
|
FUEL(2)
|
|
RANGE IN AIR MILES
|
U.S.
|
IMP
|
|
STATUTE
|
NAUTICAL
|
GALS
|
|
|
|
158
|
131
|
|
320
|
275
|
130
|
108
|
|
____300____
|
____260____
|
120
|
100
|
|
250
|
215
|
100
|
83
|
|
200
|
165
|
80
|
67
|
|
150
|
130
|
60
|
50
|
|
100
|
90
|
40
|
33
|
|
50
|
45
|
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
|
2600
|
225
|
293
|
F.T.
|
98
|
82
|
|
12000
|
2600
|
240
|
296
|
F.T.
|
112
|
93
|
|
9000
|
2600
|
245
|
290
|
38.5
|
116
|
97
|
|
6000
|
2600
|
250
|
280
|
38.5
|
112
|
93
|
|
3000
|
2600
|
251
|
269
|
38.5
|
109
|
91
|
|
S.L.
|
2600
|
253
|
259
|
38.5
|
106
|
88
|
|
|
(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___ |
|