Optional Equipment
Controllable Landing/Search Light
CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Original
10
−
11
PART V
PERFORMANCE DATA
No change.
PART VI
WEIGHT AND BALANCE DATA
No change.
PART VII
SYSTEM DESCRIPTION
The search light is controlled by the three position SRCH
toggle switch. This switch
connects battery bus power to the search light. Later configurations are powered
through the left generator bus.
Movement of the search light is accomplished by actuating the search light control
switch located on the collective stick switch panel.
Maximum light extension is 120
°
from stowed.
If the search light is rotated 90
°
either side of center and with an extended segment
of 0
°
to 60
°
, an interlock switch automatically deenergizes the lamp while positioning
the light is still possible.
PART VIII
HANDLING SERVICING AND MAINTENANCE
No change.
PART IX
ADDITIONAL OPERATIONS AND PERFORMANCE DATA
No change.
Summary of Contents for MD900 Explorer
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