|
|
|
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
|
170
|
142
|
|
345
|
|
300
|
140
|
117
|
|
320
|
|
275
|
130
|
108
|
|
295
|
|
255
|
120
|
100
|
|
270
|
|
235
|
110
|
92
|
|
245
|
|
210
|
100
|
83
|
|
220
|
|
190
|
90
|
75
|
|
195
|
|
170
|
80
|
67
|
|
170
|
|
150
|
70
|
58
|
|
145
|
|
130
|
60
|
50
|
|
125
|
|
105
|
50
|
42
|
|
100
|
|
85
|
40
|
33
|
|
75
|
|
65
|
30
|
25
|
|
50
|
|
45
|
20
|
17
|
|
25
|
|
20
|
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
|
181
|
157
|
F.T.
|
69
|
57
|
|
20000
|
2600
|
208
|
180
|
F.T.
|
91
|
76
|
|
15000
|
2600
|
232
|
201
|
F.T.
|
115
|
96
|
|
12000
|
2600
|
238
|
206
|
38.3
|
119
|
99
|
|
9000
|
2600
|
241
|
209
|
38.3
|
116
|
97
|
|
6000
|
2600
|
244
|
212
|
38.3
|
113
|
94
|
|
3000
|
2600
|
246
|
214
|
38.3
|
109
|
91
|
|
S.L.
|
2600
|
248
|
215
|
38.3
|
106
|
88
|
| (1) INDICATED ALTITUDE CORRECTED FOR FREE AIR TEMPERATURE |
| (2) ALLOW___30___U.S. GALS.,___25__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.__FOR 15 MIN., BELLY, FUS. TO 35 GAL., REAR WING, FRONT WING, 35
GAL. FUS RESERVE_ |
|