A quick question here:
The question:
(Refer to Annex 033-033 or Flight planning Manual SEP 1 Figure 2.4)
Given:
Aeroplane mass at start-up 3663 lbs
Aviation gasoline (density 6 lbs/gal)-fuel load 74 gal
Take-off altitude sea level
Headwind 40 kt
Cruising altitude 8000 ft
Power setting full throttle 2300 RPM 20
The question:
(Refer to Annex 033-033 or Flight planning Manual SEP 1 Figure 2.4)
Given:
Aeroplane mass at start-up 3663 lbs
Aviation gasoline (density 6 lbs/gal)-fuel load 74 gal
Take-off altitude sea level
Headwind 40 kt
Cruising altitude 8000 ft
Power setting full throttle 2300 RPM 20
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