|
|
|
I (MAX. CONT. POWER)
|
FUEL(2)
|
|
RANGE IN AIR MILES
|
U.S.
|
IMP
|
|
STATUTE
|
NAUTICAL
|
GALS
|
|
AT S.L.
|
AT 1200
|
AT S.L.
|
AT 1200
|
158
|
132
|
| ______ |
350
|
______ |
305
|
130
|
108
|
|
325
|
|
280
|
120
|
100
|
|
295
|
|
260
|
110
|
92
|
|
270
|
|
235
|
100
|
83
|
|
245
|
|
210
|
90
|
75
|
|
215
|
|
185
|
80
|
67
|
|
190
|
|
165
|
70
|
58
|
|
160
|
|
140
|
60
|
50
|
|
135
|
|
115
|
50
|
42
|
|
110
|
|
95
|
40
|
33
|
|
80
|
|
70
|
30
|
25
|
|
55
|
|
45
|
20
|
17
|
|
25
|
|
25
|
10
|
8
|
|
|
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.
|
|
25000
|
2600
|
194
|
168
|
F.T.
|
69
|
57
|
|
20000
|
2600
|
224
|
194
|
F.T.
|
91
|
76
|
|
15000
|
2600
|
252
|
218
|
F.T.
|
115
|
96
|
|
12000
|
2600
|
259
|
224
|
38.3
|
119
|
99
|
|
9000
|
2600
|
262
|
227
|
38.3
|
116
|
97
|
|
6000
|
2600
|
264
|
229
|
38.3
|
113
|
94
|
|
3000
|
2600
|
267
|
232
|
38.3
|
109
|
91
|
|
S.L.
|
2600
|
269
|
234
|
38.3
|
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 ___9000___FEET ALTITUTUDE. RETURN FUEL FLOWS TO TANKK ___FUSELAGE__ USE FUEL FROM TANKS IN THE FOLLOWING ORDER: _FUS.__ TO_35__GAL., __REAR_WING, __FRONT_WING, _35 GAL_FUSELAGE_RESERVE__ |
|