Mooring Checklist; V Sse Intentional One Engine Inoperative Speed - Piper SEMINOLE 2013 Pilot Operating Handbook

With garmin g1000 system
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SEcTION 4
NORMAL PROcEDURES
4.5p Mooring checklist
MOORING
PARK BRAKE ................................................................. AS REQUIRED
Control Wheel ................................................... SECURED with seat belts
FLAPS ..........................................................................................FULL UP
Wheel Chocks ............................................................................IN PLACE
Tiedowns ...................................................................................... SECURE
If necessary, the airplane should be moved on the ground with the aid
of the optional nose wheel tow bar.
The ailerons and stabilator should be secured by looping the seat belt
through the control wheel and pulling it snug. The rudder need not be
secured under normal conditions, as its connection to the nose wheel holds
it in position. The flaps are locked when in the fully retracted position.
Wheel chocks should be positioned in place, or the parking brake set. Tie-
down ropes may be attached to mooring rings under each wing and to the
tail skid
4.5q V
- INTENTIONAL ONE ENGINE INOPERATIVE SPEED
sse
V
is not a limitation. However, it is recommended that, except for
sse
training, demonstrations, takeoffs, and landings, the airplane should not be
flown at a speed slower than V
The intentional one engine inoperative speed, V
is 82 KIAS.
REPORT: VB-2307
4-26
.
sse
REVISED: October 27, 2014
PA-44-180, SEMINOLE
, for the PA-44-180
sse
ISSUED: June 5, 2013

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Seminole 2014Pa-44-180

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