NOTE
It is possible to listen to only one of the ENG FIRE messages due
to the short length of the EDU TEST.
The ENG FIRE message of the second engine can be heard, even
during the test sequence, by pushing the MASTER WARNING
RESET pushbutton.
NOTE
If the helicopter is configured with the engine control panel
P/N 109-0900-55-101 on the central console, the test of the EDU
will also activate the FIRE warning lights adjacent to the engine
mode switches.
EDU 2 : The test sequence shall display
the MAIN format with the fol-
lowing data:
ENG OIL pressure 50 PSI
ENG OIL temperature 100°C
XMSN OIL pressure 40 PSI
XMSN OIL temperature 100°C
FUEL pressure 20 PSI
Hydraulic oil pressure1500 PSI
Fuel quantity, decreasing.
In the advisory area (lower part
of the screen) the test sequence
shall display:
EDU 1 and EDU 2 software
identification number.
DAU-A and -B software iden-
tification number.
EDU 1 BIT PASS.
EDU 2 BIT PASS.
DAU-A BIT PASS.
DAU-B BIT PASS.
RFM A109E
2-18 R.A.I. Approved
Rev. 11
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