|
|
|
|
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
|
2450
|
229
|
297
|
F.T.
|
85
|
71
|
|
12000
|
2300
|
234
|
290
|
F.T.
|
83
|
69
|
|
9000
|
2150
|
238
|
280
|
34
|
80
|
67
|
|
6000
|
2150
|
241
|
270
|
34
|
78
|
65
|
|
3000
|
2150
|
243
|
260
|
34
|
75
|
62
|
|
S.L.
|
2150
|
244
|
250
|
34
|
72
|
60
|
| (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 |
|