PART II-LIMITATIONS

      For operation of flaps between:-

          0° and 30°	..	..	155 knots.
          30° and fully down	..	145 knots.

      The speed quoted for the operation of a service also
      applies for flight with the service in the extended position.

  (c) Maximum all-up weights:-

      Take-off and gentle manoeuvres
        only	..	..	..	13,380 lb.

       All other permitted forms of
         flying	..	..	..	11,610 lb.

   (d) G limitations

       The following accelerometer readings must not be
       exceeded:-

           Clean aircraft	..	..	+6G.
           With drop tanks (full or empty)..	+4G.

        The maximum permitted negative accelerometer reading
        is - 3½G. 
        
        NOTE.-Until Mod. 3500 or Mod. 3535 is embodied the
        application of negative G should be avoided;
        otherwise there is a risk of flash fire caused by
        penetration of fuel into the engine bay.

    (e) The aircraft must not be taxied with the canopy open.
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Page 31(f) Aircraft approach limitations
Para. 51
A.L.3            The A.A.L.'s are as follows:

            G.C.A., precision radar	..	.. 200ft 250 ft.
            G.C.A., search radar	..	.. 400 ft.
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