PART II-HANDLING
37. Climbing
(i) For maximum rate of climb, use full throttle, 2,400 r.p.m.
and climb at 70 knots.
(ii) Unless operating in sandy or dust-laden conditions set
the air-intake filter control in at 1,000 ft.
38. General flying
(i) Stability
At all loadings, and under all conditions of flight, longi-
tudinal and directional stability are satisfactory. Lateral-
ly, however, the aircraft is neutrally stable.
(ii) Changes of trim
Flaps down ... ... ... ... Nose up
Flaps up ... ... ... ... Nose down
An appreciable nose-down change of trim occurs when
the throttle is closed amd vice-versa when it is opened.
There is no change of trim on opening or closing the
hood.
(iii) Controls
All controls are effective throughout the speed range.
The rudder and elevators are light, nut the ailerons are
heavy and lack harmony with the other controls.
(iv) Propeller
The propeller tends to overspeed when power is increased,
therefore, the r.p.m. control lever must be moved slowly
and carefully and rapid movement should be
avoided.
(v) Flying at reduced airspeed
Reduce speed to 85 knots and lower the flaps to the
TAKE OFF (maximum lift) position. Select 2,200 r.p.m.
and fly at 70 knots.
39. Stalling
(i) The stalling speeds, engine off are :-
Flaps up ... ... ... ... 52 knots
Flaps fully down ... ... ... 48 knots
(ii) Warning of the approach of the stall is given by elevator
buffeting and slight longitudinal pitching which occurs
about 5 knots above the stall. This may be mistaken for
the stall itself, but as the control column is eased fully
back the buffeting increases and the nose and either wing
(usually the left) drop. Recovery is normal and easy.
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