PART IV-HANDLING

       Should excessive fuel have drained onto the ground, have
       the aircraft moved. Wait until the impeller has stopped
       rotating before attempting a restart.

   (e) If after a second attempt the engine fails to start, the
       cause should be investigated before any further attempts
       are made.
-----------------------------------------------------------------
Page 4760. Checks after starting 
Para
60 (a)   (a) Fire warning light		out.  
A.L.1         Idling r.p.m.		3,000 ± 200.
               J.p.t.			600° C. Max.
       Inverter indicator		Black (post-mod.F.T.C.
				   101)
-----------------------------------------------------------------
    (b) R.p.m.			Increase to 4,000.
        F.P.I. switch		ON.
        R.p.m. increase		1,000 r.p.m. pre-mod. 1130.
				  800-900 r.p.m. post-mod.
				  1130.
    If the desired increase is not achieved the system is
    unserviceable and the aircraft must not be flown.
-----------------------------------------------------------------
Page 47(c) Inverter magnetic indicator	Black. 
Para
60            Generator failure warning	Out.
(c)               light 
A.L.3    Pitot head heater		ON.
       F.P.I. switch		Off and check r.p.m. drop
				  to original figure. 
       V.H.F.			Select Set/Frequency as
				  required.
       Throttle			Close. Check idling
				  R.P.M.
       Artificial Horizon	Erect if necessary.
       Mk. 4F compass		Synchronise and compare
				  with E.2.
       D.M.E.			STANDBY.
-----------------------------------------------------------------
   (d) Flaps			Up, indicated up.
       Airbrakes		Test.
       Brake pressure		Min. 200 lb./Max. 450 lb.
				  sq. in.

47