|
|
V(MAX. RANGE)
|
FUEL(2)
|
|
RANGE IN AIR MILES
|
U.S.
|
IMP
|
|
STATUTE
|
NAUTICAL
|
GALS
|
|
(3)
|
158
|
131
|
|
720
|
620
|
130
|
108
|
|
670
|
580
|
120
|
100
|
|
550
|
480
|
100
|
83
|
|
440
|
390
|
80
|
67
|
|
330
|
290
|
60
|
50
|
|
220
|
190
|
40
|
33
|
|
110
|
100
|
20
|
17
|
|
|
DENSITY
|
R.P.M.
|
I.A.S
|
T.A.S
|
M.P.
|
U.S
|
IMP.
|
|
ALT. IN FEET
|
MP.H.
|
MP.H.
|
IN. Hg
|
G.P.H.
|
G.P.H.
|
|
15000
|
1900
|
185
|
240
|
26
|
42
|
35
|
|
12000
|
1800
|
188
|
267
|
26
|
41
|
34
|
|
9000
|
1800
|
183
|
255
|
26
|
38
|
32
|
|
6000
|
1800
|
181
|
244
|
26
|
36
|
30
|
|
3000
|
1800
|
177
|
233
|
26
|
33
|
27
|
|
S.L.
|
1800
|
173
|
223
|
26
|
31
|
26
|
| (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__ |
| (3) 28 U.S. (23 IMP.) GALLONS NOT AVAILABE DURING FLIGHT |
|