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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