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PART III - HANDLING


            Although the minimum turning radius occurs at a rela-
            tively low mach number, it is better to not to allow the
            speed to drop below that for the maximum rate of climb
            for the particular altitude as, particularly at high altitude,
            height would have to be lost in order to accelerate quickly
            to the best climbing speed.  The table below sets out the
            approximate mach numbers above which a large increase
            in the turning radius occurs.
Altitude Speed for level turn Best climb speed
  Knots Mach No. Mach No.
40,000 230 .76 .80
35,000 275 .81 .79
30,000 315 .83 .76
25,000 360 .85 .73
20,000 400 .85 .71
15,000 435 .85 .68
10,000 475 .85 .66
5,000 520 .85 .64
S.L. 550 .83 .61

PART III - HANDLING


       65.  Spinning
       (i)  It is recommended that practice spins should be carried
            out on clean aircraft only and that a height of 20,000-
            25,000 feet be reached before commencing the spins.
       (ii) The spin is initiated in the normal manner and may vary
            between aircraft.  The behaviour may also vary between
            spins to the left and spins to the right.  In all cases the
            rate of rotation is slow, about four seconds per turn.  In
            some cases the spin may not develop fully, even with full
            pro-spin control.  In a fully developed spin the nose rises
            and falls slowly during each turn in which time about
            2,000 feet of height is lost.  Some buffeting may be
            experienced initially but this becomes less as the spin
            develops.
       (iii)Before recovery check that the air brakes are IN and that
            the engine is idling.  Recover by applying full opposite
            rudder and moving the control column forward until the
            spin stops.  Keep the ailerons central as the recovery may
            be seriously affected if aileron is used.  Centralise the
            controls as soon as the spin has stopped and, after gain-
            ing speed, ease the aircraft gently out of the dive.
       (iv) With a clean aircraft, recovery is effected within one
            turn, after taking the necessary corrective action.
       (v)  The aircraft will recover from spins when full, or partially

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