PART Vi-OPERATING DATA
below. For every 1,000 ft. the aerodrome altitude is
above sea level increase the above distances by:-
10 per cent. for ground run.
8 per cent. to clear 50 ft.
(a) Clean aircraft
Temperature °C. |
-15 |
0 |
+15 |
+30 |
+45 |
Zero Wind |
Ground Run .. |
560 |
630 |
720 |
820 |
940 |
To clear 50 ft. |
1,000 |
1,140 |
1,300 |
1,460 |
1.640 |
30 knot Wind |
Ground run .. |
290 |
330 |
380 |
430 |
490 |
To clear 50 ft. |
610 |
700 |
800 |
900 |
1,000 |
(b) With drop tanks
Temperature °C. |
-15 |
0 |
+15 |
+30 |
+45 |
Zero Wind |
Ground Run .. |
830 |
980 |
1,120 |
1,280 |
1,460 |
To clear 50 ft. |
1,480 |
1,680 |
1,920 |
2,200 |
2,520 |
30 knot Wind |
Ground run .. |
380 |
550 |
630 |
710 |
820 |
To clear 50 ft. |
950 |
1,100 |
1,250 |
1,410 |
1,600 |
94. Fuel consumptions
The following are the approximate fuel consumptions in
pounds per hour for various altitudes and power settings.
Altitude (feet) |
At 10,600 r.p.m. |
At 10,250 r.p.m. |
At best range speed |
Clean |
With tanks |
Sea level .. .. |
4,910 |
4,325 |
1,925 |
2,150 |
10,000 ft. .. .. |
3,850 |
3,310 |
1,425 |
1,690 |
20,000 ft. .. .. |
2,920 |
2,460 |
1,115 |
1,230 |
30,000 ft. .. .. |
2,230 |
2,000 |
962 |
1,078 |
40,000 ft. .. .. |
1,540 |
1,540 |
880 |
1,078 |
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