MD Helicopters MD900 with PW206E, Flight Manual

Page: 304 / 450

CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
Systems Description
Original
7–66
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 7–42. Aircraft Monitor, Fault Log Menu