MD Helicopters 369E, Руководство по летной эксплуатации вертолетов

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CSP − E − 1
ROTORCRAFT FLIGHT MANUAL
Optional Equipment
Utiltiy Floats
MD 500E
(Model 369E)
Revision 14 9 − 44
FAA Approved
PART III
EMERGENCY AND
MALFUNCTION PROCEDURES
AUTOROTATIONAL LANDING
Procedures:
Make a normal autorotational approach. Minimize forward speed prior to
water contact.
Recommended water contact speed 10 knots or less. Do not lower collec-
tive until forward speed is 5 knots or less.
Landings have been demonstrated at gross weights up to 3000 pounds and
touchdown speeds up to approximately 15 knots.
NOTE
: Landings should be made with the helicopter as level as possible laterally and
the nose of the helicopter slightly high. One − float − first landings may produce
undesirable but controllable yaw.
If emergency occurs at night over water, the dual landing lights should not be
illuminated above 1000 feet altitude in order to preserve battery power.
PART IV
NORMAL PROCEDURES
Rotor engagement on water:
Determine that sufficient clearance exists between the helicopter and any
obstacle during engine start. Tail swing, before directional control is ob-
tained, will be approximately 200 degrees.
Landing:
Make a normal landing approach. Minimize forward speed prior to water
contact. Recommended water contact speed 10 knots or less. Do not lower
collective until forward speed is 5 knots or less. Landings have been demon-
strated at gross weights up to 3000 pounds and touchdown speeds up to
approximately 15 knots.
NOTE
: Landings should be made with the helicopter as level as possible laterally and
the nose of the helicopter slightly high. One − float − first landings may produce
undesirable but controllable yaw.