MD Helicopters MD900 with PW206E, Flight Manual

Page: 283 / 450

CSP–900RFM206E–1
ROTORCRAFT FLIGHT MANUAL
MD900 With PW 206E
Systems Description
Original
7–45
Table 7–1. Automatic Alphanumeric Display Warning/Caution/Advisory Messages
SAMPLE MESSAGE
(Fault)
CORRECTIVE ACTION CLR W/C/A
CAUSE FOR
DISPLAY
CHK BMS SENSOR
BMS sensor(s) fail
ure
2
C YES Advise maintenance
TORQ LFT 2:30
TORQ RT 2:30
EGT LFT 2:30
EGT RT 2:30
NG LFT 2 :30
NG RT 2:30
TOP or OEI count
down
A NO N/A
CARGO HOOK OPEN Cargo hook open A YES N/A
BATT DISCHARGE Battery Discharging A YES N/A
EXTGSHR PRESS LO
Optional fire extin
guishing system
bottle pressure low
A YES Advise Maintenance
RECORDING DATA
Crew commanded
data record
A NO N/A
DATA XFER CMPL
Download of data logs
to ground based com
puters
A YES N/A
CHECK FAULT LOG
Fault Log during
flight
2,3
A YES Advise Maintenance
CHK EXCEED LOG
Exceedance Log dur
ing flight
3
A YES Advise Maintenance
CHECK ROTOR BAL
Main rotor out of bal
ance
A YES Advise Maintenance
CHECK NOTAR BAL
NOTAR fan out of
balance
A YES Advise Maintenance
PRATT & WHITNEY
Engine Configura
tion
4
A YES N/A
NOTE
: 1.With a single system failure, this message is displayed when the failed system
pressure decreases to 250 PSI. This message will reappear when remaining
operating system pressure decreases to 500 PSI.
2.This caution does not affect dispatchability.
3.These messages are generated for conditions that create a fault log or an
exceedance log and are displayed only when the aircraft is on–ground as
determined by the AOG logic.
4.This message displayed for 5 seconds following the power–up ‘‘Lamp Test’’.