|
|
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
|
|
|
|
|
|
|
|
20000
|
2250
|
198
|
172
|
F.T
|
55
|
46
|
|
15000
|
2000
|
206
|
179
|
F.T
|
52
|
43
|
|
12000
|
1900
|
206
|
179
|
29
|
50
|
42
|
|
9000
|
1850
|
206
|
179
|
29
|
47
|
39
|
|
6000
|
1850
|
204
|
177
|
29
|
45
|
37
|
|
3000
|
1850
|
204
|
177
|
29
|
43
|
36
|
|
S.L.
|
1800
|
202
|
175
|
29
|
41
|
34
|
| (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__ |
| * 28 GAL. FOR WARM-UP, TAKE-OFF AND CLIMB, NOT AVAILABLE IN FLIGHT |
|