PART V-OPERATING DATA
CLIMB DATA -VENTRAL AND WING DROP TANKS
Climb at full throttle throughout, at speeds quoted in para.57
From |
To |
Time Mins. |
Fuel Galls. (AVTAG) |
Distance N.M. |
Sea Level |
10,000 ft. 20,000 ft. 30,000 ft. 35,000 ft. |
2 4½ 8½ 11 |
29 60 95 115 |
12 30 52 68 |
10,000 ft. |
20,000 ft. 30,000 ft. 35,000 ft. |
2½ 6½ 9 |
31 66 86 |
18 40 56 |
20,000 ft. |
30,000 ft. 35,000 ft. |
4 6½ |
35 55 |
22 38 |
30,000 ft. |
35,000 ft. |
2½ |
20 |
16 |
Temperature correction. For each 10°C. rise in ambient temperature, add
the following:-
From |
To |
Time |
Fuel |
Distance |
Sea Level 10,000 ft. 20,000 ft. 30,000 ft. |
10,000 ft. 20,000 ft. 30,000 ft. 35,000 ft. |
0.1 0.4 1.1 1.8 |
1.8 5.0 9.4 13.0 |
1.2 3.3 8.0 12.0 |
FUEL CONTENTS .. .. .. .. 700 gallons
TAXY AND TAKE-OFF ALLOWANCE .. .. 40 gallons
LANDING ALLOWANCE (excluding descent fuel).. 60 gallons
DESCENT DATA
As for clean aircraft
76
|