PART V-OPERATING DATA
Select the height at which maximum range is available
at that fuel state. The distance available includes
distance covered on the climb but not on the descent.
(Absolute maximum range is obtained by adding on
the descent distance, provided that the let-down starts
at that distance from the destination.) For short-
range flights, inspect the sea level block and select the
height at which the distance to be covered requires the
least amount of fuel. This is the best altitude for the
flight.
(ii) In-flight planning
At any stage of the flight, the available range may be
ascertained by applying the fuel state to the level
flight range in the particular block. If an increase in
range is required, or if a climb has to be made, the
new available range may be obtained by entering the
existing altitude block at the appropriate fuel state
and moving verticaslly downwards within the block
until the new altitude is reached. Figures in heavy
type indicate the best altitude for the maximum
increase in range. Above these heights, no further
increase in range is possible. If a descent is necessi-
tated, the new range is shown by moving direct from
the existing altitude level flight range for the appro-
priate fuel state to the new altitude level flight range.
(c) Cruise data charts
The cruise data charts show aircraft performance and fuel
consumption in level flight at various heights and r.p.m.
99. Endurance
At any altitude, maximum endurance will be obtained by
flying at the I.A.S. which requires the lowest r.p.m. to
maintain height. Increase in altitude gives increase in
endurance; however, the overall endurance may not be
improved by climbing above 20,000 ft., except when maxi-
mum fuel is available, owing to the proportion of fuel used
on the climb and the descent. All climbs should be made
at full power (within jet pipe limitations) and the
descent made as quickly as practicable. 70
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