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 − 22
FAA Approved
While in cruise:
Place RE−IGN test switch in FLT position.
RE−IGN and ENGINE OUT lights should illuminate along with the
ENGINE OUT audible warning.
Return RE−IGN test switch to OFF.
Press RE−IGN light to reset system.
4 − 6. TAKEOFF
NOTE
: For takeoff in noise − sensitive areas, refer to paragraph 4 − 17 for noise impact
reduction procedures.
Determine that hover area and takeoff path are clear.
Follow normal helicopter takeoff procedure with N
2
set at 103 percent.
NOTE
: Governed N
2
rpm should increase 1/2 to 1 percent on takeoff − adjust as
necessary to maintain N
2
at 103 percent.
Follow recommended takeoff profile shown in Height Velocity Diagram (Ref.
Section V).
If sudden unusual or excessive vibrations should occur during
flight, a precautionary landing should be made. No further flights
shall be attempted until the cause of the vibration has been
identified and corrected.
NOTE
: Momentary fluctuation in indicated airspeed may occur during acceleration and
climbout. This fluctuation is characterized by a rapid rise in indicated air speed
to approximately 40 knots, followed by a drop back to 30 knots and then normal
increase as determined by the rate of acceleration. Maintain recommended
takeoff profile to minimize fluctuation. Indicated airspeed is unreliable when
climbing at less than 40 knots IAS.
Use Cyclic trim as desired to minimize stick forces.
NOTE
: Proper longitudinal trim is established when small fore and aft cyclic movements
require the same force.
WARNING