MD Helicopters 369E, Руководство по летной эксплуатации вертолетов

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Normal Procedures
CSP − E − 1 ROTORCRAFT FLIGHT MANUAL
MD 500E
(Model 369E)
Revision 13
4 − 21
FAA Approved
Engine ANTI−ICE:
AS REQUIRED
Use engine ANTI−ICE when OAT is below 5
°
C (41
°
F) and visible moisture is
present.
Check for TOT increase when turning anti−ice ON
NOTE
: Hover performance is reduced with ANTI − ICE ON (Ref. Sections V and VIII).
Optional inflight test of the auto−reignition/engine out warning
system: (Early Generic Configuration Only):
NOTE
: See Section I and Figure 4 − 2 to determine which version (‘‘early generic” / ‘‘late
generic”) of the generic wire harness is installed in the aircraft.
This check may be performed at the pilot’s discretion.
Prior to takeoff:
While on the ground at 102−103% N
2,
place RE−IGN test switch in the FLT
(middle) position. RE−IGN and ENGINE OUT lights should illuminate.
Bring the aircraft to a hover and observe actuation of the engine out audible
warnings.
NOTE
: If audible warnings are not heard, this indicates a possible rigging problem with
the air/ground switch. Refer to applicable maintenance instructions for
adjustment.
Land helicopter and return RE−IGN test switch to OFF and press RE−IGN
light to reset system.