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PART I-DESCRIPTIVE

   (iii)  An AIR EXTRACT magnetic indicator (49) which
          shows white if a breakdown occurs in the air
          extraction system for the space between the jet
          pipe outer casing and the fuselage skin in zone 4
          (see para. 13). It also shows white momentarily
          when selecting undercarriage up or down.

     12.  Operation of the reheat system. (See para. 54.)

     (a)  Reheat is selected by moving the throttle into the reheat
          gate with the shut-off switch at NORMAL, and the
          reheat L.P. cock open. Light up should occur within 2-5
          seconds of selection, depending on altitude. During this
          period and for 2-3 seconds after light-up the jet-pipe
          "eyelids" position indicator will show white.

     (b)  The throttle position at which the throttle-operated
          reheat switch is closed is always the same. but minimum
          r.p.m. obtainable, once reheat has been engaged, vary
          from about 7,300 at sea level to 7,800 at 45,000 ft.
          R.p.m. with reheat in use may be varied by throttle
          movement but r.p.m. should not be allowed to fall below
          7,600.

     (c)  Reheat is cancelled by pulling the throttle out of the
          reheat gate and throttling back. At the lower altitudes
          to avoid falling below 7,600 r.p.m. it will be necessary
          to cancel reheat by pulling the throttle out of the gate
          and then operating the shut-off switch.
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A.L.2     (d)  Reheat can be cancelled by operating the shutoff switch with-
12 (c).13       out pulling the throttle out of the gate. but should the switch be
Page 17        set back to NORMAL with throttle still in the gate. the reheat
                  will relight.

            (e)  A reheat top-temperature limiter automatically cancels reheat
                  and closes the eyelids if the J.P.T. exceeds 700°C. In this event
                  the nozzle position indictor shows white until the throttle is
                  pulled out of the gate. When mod. 739 is embodied a NORMAL/
                  OVERRIDE switch (36) is fitted to the port side of the instrument
                  panel. When the switch is set to NORMAL the limiter is in
                  operation; when set to OVERRIDE the limiter is inoperative.
                  This position should be selected at take-off.
  
           13.  Fire-extinguishers and fuselage ventilation

           (a)  Two independent fire-extinguisher systems are fitted and
                  may be operated by combined warning light/press

17

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