CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Emergency and
Malfunction Procedures
FAA Approved
Reissue 2
Revision 1
3
−
18
ENGINE FIRE - DURING FLIGHT
Indications:
Engine FIRE warning annunciator ON and activation of the warning tone for
two cycles.
Procedures:
Airspeed
REDUCE TO O.E.I. V
NE
OR LESS
Attempt to confirm existence of fire
NOTE
:
If FIRE warning annunciator goes OUT, and no other indications of fire are
present, land as soon as practical.
If FIRE warning annunciator remains ON, proceed with next steps.
Engine control switch
OFF FOR AFFECTED ENGINE
Fuel boost pump
OFF FOR AFFECTED ENGINE
Fuel shutoff valve
OFF FOR AFFECTED ENGINE
Fire bottle discharge switch
PRI (ALT IF NECESSARY)
NOTE
:
The fire bottle will not discharge with the fuel valve ON.
If FIRE warning goes OFF
LAND AS SOON AS PRACTICAL
If FIRE warning remains ON
LAND IMMEDIATELY
After landing:
Engine control switch
OFF FOR OPERATING ENGINE
Rotor brake (if installed)
APPLY
Power switch
OFF
Passengers/crew
EVACUATE
TRANSMISSION AREA FIRE
Indications:
Transmission FIRE warning annunciator ON and activation of the warning
tone for two cycles.
Procedures:
Land immediately
After landing:
Engine control switches
OFF
Rotor brake (if installed)
APPLY
Power switch
OFF
Passengers/crew
EVACUATE
Fire extinguisher
USE AS APPROPRIATE
Summary of Contents for MD900 Explorer
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