|
|
|
|
|
|
V (MAX. RANGE)
|
FUEL(2)
|
|
RANGE IN AIR MILES
|
U.S.
|
IMP
|
|
STATUE
|
NAUTICAL
|
GALS
|
|
28 U.S. (23 IMP.) GALLONS NOT AVAILABLE IN FLIGHT
|
158
|
131
|
|
670
|
590
|
130
|
108
|
|
620
|
540
|
120
|
100
|
|
____520___
|
____450____
|
100
|
83
|
|
420
|
360
|
80
|
67
|
|
310
|
275
|
60
|
50
|
|
210
|
180
|
40
|
33
|
|
105
|
90
|
20
|
17
|
|
|
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.
|
|
15000
|
1900
|
172
|
223
|
25
|
41
|
34
|
|
12000
|
1800
|
172
|
212
|
25
|
39
|
32
|
|
9000
|
1800
|
172
|
203
|
25
|
37
|
31
|
|
6000
|
1800
|
168
|
190
|
25
|
35
|
29
|
|
3000
|
1800
|
161
|
161
|
25
|
32
|
27
|
|
S.L.
|
1800
|
158
|
163
|
24
|
30
|
25
|
|
|
(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 ___5000___FEET ALTITUTUDE. RETURN FUEL FLOWS TO TANKK ___FUSELAGE__ USE FUEL FROM TANKS IN THE FOLLOWING ORDER: _FUS.__TO_35__GAL., __REAR_WING,_ _FRONT_WING, _BALANCE_FUSELAGE___ |