PART III-OPERATING DATA

  (iii)   The aircraft is designed for general training duties.   Spin-
          ning and aerobatics are permitted, except when the rear
          seat is occupied and at weights above 4,000 lb.

   (iv)   Power is liable to fail immediately in inverted flight.
          Pending modification and the issue of further instructions
          all manoeuvres involving sustained negative "g" must be
          avoided and inversions should be restricted to the brief
          period essential to the peerformance of normal aerobatics.

    49.   Position error corrections

          The position error, flaps up or down, is less than 1½ knots
          throughout the speed range.

    50.   Fuel capacities and approximate consumptions

    (i)   Capacity of each tank	...	...	...	20 galls.
                 Total capacity	...	...	...	40 galls.

   (ii)   Approximate fuel consumption:-
          At maximum climbing power	...	  20 galls./hour.
          At maximum continuous (rich) power	  16 galls./hour.
          At maximum continuous (weak) power	  12 galls./hour.

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