PART II-HANDLING
ing light should go out. If desired, the pressurising lever
can be turned on after take-off. If above 17,000 ft. the
cockpit pressurising system fails, indicated by the cock-
pit altimeter reading the same as the aircraft altimeter
and/or the warning light coming on, the climb should not
be continued above 30,000 ft. During the climb the pilot
should regulate the oxygen supply to correspond to the
cockpit altimeter reading.
32. General flying
(i) Stability
At all loads stability is satisfactory at all altitudes and in
all conditions of flight, except that when carrying drop
tanks, or flying without ammunition longitudinal stability
is slightly decreased and there is a tendency to tighten in
turns at high altitude.
(ii) Changes of trim
Flaps down ... Nose up
Flaps up ... Nose down
Dive brakes open Nose up accompanied by buffet-
ing (strong nose up at high
speed when carrying external
stores)
Dive brakes closed Nose down
Operation of the undercarriage in either direction pro-
motes little change of trim. Closing the throttle at high
speed promotes a slight nose down change of trim and
opening it at low speed causes a nose up change.
(iii) Controls
All controls are light, effective and well harmonised and
the aircraft is easy and pleasant to fly. The elevator is
powerful throughout the speed range and relatively small
stick forces may induce large accelerations. The eleva-
tor trimming tab is light and moderately effective but
becomes less effective at high altitudes.
(iv) Flying at reduced airspeed
Use the dive brakes to reduce speed to 145 knots, lower
30° of flap and close the dive brakes. Fly at about 140
knots.
(v) Throttle manipulation
Movements of the throttle should normally be made
slowly to avoid engine surging and high jet pipe tempera-
tures. In an emergency, such as the case of a baulked
landing the throttle may be opened rapidly.
A.L.3 |(vi) Flight in turbulent conditions
Para. 32 | Speed in conditions of severe turbulence is 220 knots.
(vi)
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