PART 1II-HANDLING
HANDLING IN FLIGHT
57. Climbing
(a) Climb at full power within the j.p.t. limitations. The
following climbing speeds are recommended with or with-
out drop tanks fitted:-
300 knots until 0.63M is obtained, then 0.63M for the
remainder of the climb.
(b) If maximum rate of climb is not essential, the climb should
be made at 14,200 r.p.m., using the same airspeeds. Throttle
adjustment will be necessary to maintain this power setting.
(c) Particular care must be taken to maintain the correct
climbing speed at altitude, or a considerable increase in
time to height will result.
58. General flying
(a) Flying controls
(i) Ailerons. On aircraft fitted with geared tabs only, the
aileron feel becomes progressively heavier with in-
creasing airspeeds and mach numbers. When spring
tabs are fitted, the ailerons are light and pleasant but
become heavier with increase in mach numbers. Large
control column movements are required for effective
control at low I.A.S.
(ii) Elevator. The elevators are effective and sensitive
throughout the speed range. At low airspeeds they
become less sensitive but are effective down to the
stall.
(iii)Rudder. Control forces on the rudder become very
heavy at high speeds and with large deflections at low
speeds. Sustained asymmetric flight at low I.A.S. is
very tiring.
(b) Trimming controls
NOTE.- The elevator and rudder trimmers may ice up at
height. Exercising the trimmers at regular inter-
vals will help to prevent this happening. If neces-
sary, reduce height until they can be freed.
(i) Elevator trimmer. The elevator trimmer is spongy in
operation but very effective and the aircraft is easy to
trim under most conditions of flight. 44
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