PART I-DESCRIPTIVE

     CABIN EQUIPMENT AND OTHER CONTROLS

     22.  Access

     (i)  The sliding hood over the cockpit is divided into two
          halves, each half being operated by its own handle (34)
          at the forward lower end.   The handles can lock the
          hood in either the open or closed positions and may be
          operated from either inside or outside the aircraft.

    (ii)  If required, both halves of the hood can be jettisoned (see
          para. 51).

   (iii)  The rear hatch is released from inside or outside by lift-
          ing and rotating the catch at the bottom of the panel on
          the port side.

     23.  Seats

          Both pilots' seats are adjustable for height by a lever (1)
          on the right-hand side of each seat but the rear seat has
          no such adjustment.

     24.  Cockpit heating

          The control (41) is mounted below the instrument panel
          to the right of the air-intake heat control, and is marked
          PUSH ON, PULL OFF.   A trigger catch must be de-
          pressed before operating the lever.
    
     25.  Cockpit ventilation

          Cold air enters the cockpit ventilating louvres (25)
          mounted to the right and left of the front panel.   To re-
          duce the supply rotate the inlet socket towards the
          SHUT position.
    
     26.  Direct vision panels

          Both sides of the windscreen can be opened by un-
          screwing the knurled nut at the top and then the whole
          side panel may be let down inboard to rest on the coam-
          ing.   It should be pushed well forward and secured with
          the spring catch on the upper side of the coaming.

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