|
|
|
|
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
|
2600
|
241
|
312
|
F.T.
|
98
|
82
|
|
12000
|
2600
|
258
|
318
|
F.T.
|
112
|
93
|
|
9000
|
2600
|
264
|
310
|
38.5
|
116
|
97
|
|
6000
|
2600
|
266
|
299
|
38.5
|
112
|
93
|
|
3000
|
2600
|
270
|
289
|
38.5
|
109
|
91
|
|
S.L.
|
2600
|
270
|
277
|
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 ___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__ |
|