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(5)
Climb at 107 KIAS (95 KIAS with obstacles directly
ahead).
(6)
Trim aircraft for single-engine climb.
SYSTEM EMERGENCY PROCEDURES
FUEL SYSTEM
ENGINE DRIVEN FUEL PUMP FAILURE
(1)
Fuel Selector - MAIN TANK (feel for detent).
(2)
Auxiliary Fuel Pump - ON.
(3)
Cowl Flap - OPEN.
(4)
Mixture - ADJUST for smooth engine operation.
(5)
As Soon as Practical - LAND.
(6)
Fuel in auxiliary and opposite main tank is unusablE
NOTE
If both an engine-driven fuel pump and an
auxiliary fuel pump fail on the same side of
the aircraft, the failing engine cannot be
supplied with fuel from the opposite MAIN
tank since that auxiliary fuel pump will
operate on the low pressure setting as long
as the corresponding engine fuel pump is
operative.
ELECTRICAL
SYSTEM
ALTERNATOR FAILURE (SINGLE)
(Indicated
by
illumination of failure light)
(1)
Electrical Load - REDUCE.
(2)
If Circuit Breaker is Tripped:
(a)
Shut off affected alternator.
(b)
Reset affected alternator circuit breaker.
3-15
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