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A.L.1.                      PART II - LIMITATIONS
Para.
56 (d) (e)
Page 49   (d)  Maximum all-up weights
                         With RP's and inboard tanks        21,735 lb.
                         With four drop tanks                    21, 735 lbs.
                         With two drop tanks                    19,750 lb.
                         Clean                                           17,500 lbs.
                         Landing                                       15,600 lbs.

              (e)  Gun firing
                     (i)   The guns may be fired on the ground.

                     (ii)   In the air, gun firing is permitted at any height and
                            irrespective of the length of the burst subject to the
                            following limitations:-

     
No. of
guns
Type of
ammo.
Maximum speed
(knots)
Remarks
2 LV or HV 550 Without Mod. 646
2 LV or HV 620 With Mod. 646
       
4 LV 400 Without Mods. 592 & 598
4 HV 250 below 25,000 ft.                    "
4 HV 350 above 25,000 ft.                    "
4 LV or HV 550 With Mods. 592 & 598
4 LV or HV 650 With Mods. 592, 598 and
      646
                 NOTE.-1. If the guns are fired, with airbrake OUT at
                          speeds above 550 knots a limited number of
                          ejected case strikes on the airbrake will be
                          experienced; such firing should therefore be
                          confined to cases of operational necessity.
                         
                       2. When carrying external stores the minimum
                          firing speed is:-
                               350 knots without Mod. 645 embodied.
                               150 knots with Mod. 645 embodied.
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A.L.2    (f)  Bomb release and jettison
Para. 56
(f)
2X1,000 lb. bombs may be carried, on inboard pylons Page 49 only, released or jettisoned at all speeds and dive angles up to 590 knots and 60° respectively. There is no mach number limitation, but pilots are warned against commit- ting their aircraft to dives which will result in exceeding 0.9M without sufficient height for pullout, in view of the deterioration in longitudinal control above this speed

49

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