CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Systems Description
Original
7
−
55
Reissue 2
ACQUISITION
COMPLETE
MAIN ROTOR TRACK
MAIN ROTOR
SOLUTION OPTIONS
RUN XX M/R
MEASUREMENTS
BALANCE MONITOR
COLLECT M/R DATA
MAIN ROTOR
BALANCE
f92
−
084
NOTE: TO RETURN TO PREVIOUS HIGHER LEVEL - PRESS
MENU
FLY 100% GROUND
PRESS REC
ACQUIRING
100% GND LAT
FLY HOVER IGE
PRESS REC
FLY 120 KIAS
PRESS REC
ACQUIRING
100% GND LAT
X.XX IPS AT YY.YY
NOTAR
BALANCE
SPECTRUM
BMS FAULT LOG
BMS VERSION LOG
MAIN ROTOR
CONFIGURATION
TOP LEVEL
SECOND LEVEL
THIRD LEVEL
FOURTH LEVEL
DISPLAY M/R
SOLUTION RUN XX
NOTE 2
NOTE 3
ACQUIRING
HOVER IGE LAT
HOVER IGE LAT
X.XX IPS AT YY.YY
NOTE 3
ACQUIRING
120 KIAS LAT
NOTE 2
120 KIAS LAT
X.XX IPS AT YY.YY
NOTE 3
NOTE 2
120 KIAS VERT
X.XX IPS AT YY.YY
NOTE 4
NOTE 2: AUTOMATICALLY STEPS THROUGH ACQUIRING
MEASUREMENTS SPECIFIED FOR THIS REGIME.
NOTE 3: WHEN COMPLETE, THE RESULT IS DISPLAYED
FOR 4 SECONDS AND THE DISPLAY GOES TO
NEXT REGIME.
NOTE 1: WHEN COMPLETED, MESSAGE IS DISPLAYED
FOR 1 SECOND
RUN XX RPM XXX
120 KIAS VERT
FLY 80 KIAS
PRESS REC
ACQUIRING
ACQUIRING
80 KIAS LAT
80 KIAS LAT
X.XX IPS AT YY.YY
80 KIAS VERT
X.XX IPS AT YY.YY
80 KIAS VERT
NOTE 1
NOTE 2
NOTE 3
NOTE 5: THE DISPLAY GOES BACK TO THE FIRST
REGIME WHEN THE ABOVE DATA HAS BEEN
COLLECTED
BMS ADVISORY LOG
BMS MAINTENANCE
NOTE 2
ACQUISITION
COMPLETE
NOTE 1
ACQUISITION
COMPLETE
NOTE 1
ACQUISITION
COMPLETE
NOTE 1
REDO 100% GND
PRESS REC
NOTE 5
NOTE 4: WHEN COMPLETE, THE RESULT IS DISPLAYED
FOR 4 SECONDS
NOTE 2
NOTE 3
Figure 7
−
29. Balance Monitor, Main Rotor Balance
Summary of Contents for MD900 Explorer
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