CSP–900RFM206E–1
Emergency and
Malfunction Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
FAA Approved
Original
3–7
WATER LANDING − OEI/AEO
Conditions:
Available power allows hovering.
NOTE
:
The gross weight of the aircraft will determine whether sufficient power is
available to terminate the approach at a hover or whether a run–on landing must
be performed if landing OEI.
Procedures:
F
Establish normal approach to intended landing point.
F
Cabin doors may be opened when airspeed is 60 KIAS or less.
F
Plan to arrive at 100 FT above touchdown at approximately 40 KIAS.
F
At approximately 50 FT, enter a decelerating attitude and increase power to
reduce rate of closure.
F
Descend to hovering altitude over water.
F
Passengers and copilot exit aircraft.
F
Fly a safe distance away from all personnel in the water to avoid injury.
F
Place ENGINE CONTROL switch(s) in OFF and perform a hovering autorota
tion.
F
Allow aircraft to settle in a level attitude while applying full collective pitch.
F
When aircraft begins to roll, reduce collective to full down to minimize blades
skipping off the water.
F
Release safety harness and exit the aircraft as soon as the blades have stopped
turning.
Do not inflate personal flotation gear until clear of the aircraft –
safe exit will be restricted.
WARNING
Содержание MD900 with PW206E
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