Engine Failure In Flight (Above 85 Knots); Single Engine Landing - Piper PA34-220T Handbuch

3.1.4

Engine failure in flight (above 85 knots)

Mixtures both
Propellers both
Throttles both
Rudder
Inoperative engine
Operative engine
Before securing inop. engine:
Fuel flow
Fuel quantity
Fuel selector (inop. eng.)
Alternate air
Mixture
Oil pressure and temp
Magneto switches
If engine does not start, complete Engine Securing Procedure
Power (operative engine)
Mixture (operative engine)
Fuel quantity (oper. eng. tank)
Auxiliary fuel pump (oper. engine)
Cowl flap (operative engine)
Trim
Electrical load
Land as soon as practical at nearest suitable airport
3.1.5

Single Engine Landing

Inop. engine propeller
When certain of making field:
Landing gear
Wing flaps
Maintain additional altitude and speed during approach
Final approach speed
Wing flaps
Breu Gerhard
FULL FORWARD
FORWARD/MAX. 40 in. Hg.
Apply towards operative
Adjust as required
Check (if deficient-
Auxiliary fuel pump HI BOOST,
if power is not restored, OFF)
Adjust for power
Adjust 5° bank
Toward operative eng.
Decrease to min. required
FULL RICH
engine
Identify
Check
Cross feed
ON
Check
Check
Check
As required
sufficient
As required
As required
FEATHER
DOWN
LOWER
92 KIAS
25°
3-53