CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Systems Description
Original
7
−
69
Reissue 2
AIRCRAFT MONITOR
ENT
ENT
FAULT LOG
L ENG S/N
R ENG S/N
DATE
TIME
IIDS FALT1=X XX
XX, XX
IIDS FALT XX
ACFT FALT=X
SENS FALT=X
BMS FALT=X
LEFT EEC
DSCWD1 =X XX XX
NCFUR1=X XX
NCFUR2=X XX XX
NCFUR3=X XX
CFUR=0
RIGHT EEC
DSCWD1=
RIGHT EEC MENU SAME AS
LEFT EEC MENU.
NOTE: PRESSING THE
BUTTON WILL TAKE YOU
TO THE PREVIOUS HIGHEST MENU LEVEL.
MENU
TOP LEVEL
SECOND LEVEL
THIRD LEVEL
F92
−
098
EXCEEDANCE LOG
TREND LOG
FAULT LOG
IIDS SETUP
THE FAULT LOG
CONTAINS DATA ASSOCIATED WITH EEC
FAULTS AND FAILURES DETECTED IN THE IIDS, BMS, OR
AIRCRAFT TRANSDUCERS/SENSORS. THIS LOG IS RE
CORDED WHENEVER AN IIDS OR EEC FAULT IS DE
TECTED. STORAGE IS AVAILABLE FOR 100 FAULT LOGS.
Figure 7
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43. Aircraft Monitor, Fault Log Menu
Summary of Contents for MD900 Explorer
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