Engine Failure During Flight (Speed Below Vmca ) - Piper SEMINOLE 2013 Pilot Operating Handbook

SECTION 3
EMERGENCY PROCEDURES
3.5a Engine Inoperative Procedures (continued)
After the faulty engine has been identified and power loss has been
verified, complete the Engine Securing Procedure. Continue a straight
ahead climb until sufficient altitude (minimum of 1000 feet above ground
elevation) is reached to execute the normal One Engine Inoperative
Landing procedure at the nearest suitable airport.
Engine failure During flight (Speed Below V
Rudder .............................................................. APPLY AGAINST YAW
THROTTLES (Both Engines) .......RETARD TO ARREST TURN/YAW
Pitch Attitude...................................LOWER NOSE TO ACCELERATE
Operating Engine...........................INCREASE POWER AS AIRSPEED
If altitude permits, a restart may be attempted.
If restart fails or if altitude does not permit restart:
Inoperative Engine............................................. IDENTIFY and VERIFY
PROPELLER (Inop. Engine) ...................................................FEATHER
MIXTURE (Inop. Engine)......................................................... CUT-OFF
Trim .............................................................ADJUST TO 2° to 3° BANK
COWL FLAP (Operating Engine) ...................................AS REQUIRED
COWL FLAP (Inop. Engine)......................................................... CLOSE
MAG LEFT/RIGHT Switches (Inop. Engine).....................................OFF
FUEL PUMP (Inop. Engine)...............................................................OFF
ALTR Switch (Inop. Engine)...............................................................OFF
FUEL Selector (Inop. Engine).............................................................OFF
An inoperative engine can be identified by various means, including
the fact that directional control is maintained by applying rudder pressure
toward the operative engine (DEAD FOOT INDICATES DEAD ENGINE).
Additionally, engine indications such as EGT and oil pressure may help in
identifying an inoperative engine. After identification, verify complete
power loss on that engine by retarding its throttle and noting the absence of
engine or aircraft response.
REPORT: VB-2307
3-12
PA-44-180, SEMINOLE
ABOVE V
INCREASES ABOVE V
TOWARD OPERATIVE ENGINE
WITH APPROXIMATELY 1/2
TRAPEZOID SLIP INDICATED ON
THE TURN AND BANK INDICATOR
mca
(56 KIAS)
mca
(56 KIAS)
mca
ISSUED: June 5, 2013
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