MD Helicopters MD900 Explorer, Руководство по эксплуатации самолета

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CSP − 902RFM207E − 1
Emergency and
Malfunction Procedures
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Original
3 − 23
Conditions:
Left pedal applied: This condition results in a thruster opening on the left
and may be understood either as a “stuck left pedal” or a break in the rotating
cone controls with the left pedal applied. In either failure mode, the thruster
would be opened on the left producing a thrust vector that causes the aircraft
to yaw to the left. The degree of yaw will be determined by the position of
the rotating cone at the time of failure.
Procedures:
Adjust airspeed and power for level flight at an airspeed between 80 and
100 KIAS.
Do not attempt an autorotation from forward flight unless an actual
dual engine failure occurs.
If able, place pedals in “neutral” position (approximately one inch, [25mm]
of right pedal).
NOTE
:
With pedals in neutral, the NOTAR fan will be at minimum pitch.
Select collective friction to 5 pounds.
VSCS OFF.
Use a shallow to normal approach into wind or left quartering headwind.
Maintain directional control with small adjustments in collective.
Plan to touchdown with little or no forward speed.
CAUTION