CSP
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902RFM207E
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1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Optional Equipment
Annunciator Panel
Original
10
−
75
FAA Approved
Reissue 2
10
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16. OPERATING INSTRUCTIONS: ANNUNCIATOR PANEL
PART I
GENERAL
This panel advises the pilot of the operating mode and status of auxiliary fuel trans
fer, pitot heat, ground power unit door (aft mounted battery only), and airframe
fuel filter. These annunciator lights may be installed individually or in part as deter
mined by the optional equipment installed and are only available with the Honeywell
IFR Avionics STC.
PART III
EMERGENCY AND MALFUNCTION PROCEDURES
For actions following illumination of any of the caution/advisory annunciators, refer
to Section X for Supplemental Fuel System and Airframe Fuel Filter; for the remain
ing caution/advisories, refer to Section III.
PART IV
NORMAL PROCEDURES
To check the operation of the annunciators, press the ANNUN test button on the
Avionics switch panel.
f927
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11
0
AHRS1
AHRS2
TEST
DG
CCW
CW
MRKR
AP/SAS
ANNUN
SLVD
DG
SLVD
CCW
CW
DME
HOLD
ANNUN
DIM
BRIGHT
RELEASE
Figure 10
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27. Caution and Advisory Test Button
Summary of Contents for MD900 Explorer
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