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.
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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)
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(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.
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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.
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(d) Flaps Up, indicated up.
Airbrakes Test.
Brake pressure Min. 200 lb./Max. 450 lb.
sq. in.
47
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