Optional Equipment
Air
−
Conditioning System
CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Original
10
−
5
PART II
LIMITATIONS
No change.
PART III
EMERGENCY AND MALFUNCTION PROCEDURES
NOTE
:
An automatic cutoff procedure similar to that for the heat/defog system shuts
down the air conditioner in flight if either engine becomes inoperative to maintain
the best power output from the running engine.
LOSS OF COOLING
Indications:
No cooling air with system ON
Conditions:
Automatic system safety shutdown, or internal failure
Procedures:
•
A/C control switch
OFF
•
Use fresh air vent system as required
Summary of Contents for MD900 Explorer
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