PROCEDURE
GEN 1 : Reset, then ON.
GEN BUS 2 : ON, check.
If failure is confirmed, proceed as follows:
Pilot ICS panel switch : Select FAIL position
BATTery switch : OFF. All loads of Generator
Bus #1 and Emergency Bus #1
are lost. All loads of Essential
Bus #1 are retained.
NOTE
In this event all loads on #2 Bus are maintained by Generator 2.
After switching off the BATTery
the following message will be
indicated: INV 1, SAS 1 OFF,
BATT OFF cautions, ELECTRI-
CAL warning as well as DAU ch
A and EDU Primary will be lost.
Failure of generator 2 and generator bus #1
(Helicopter equipped with emergency bus)
This failure is indicated by #2 DC GEN, BUS TIE caution messages and, if the
helicopter is equipped with battery discharge control box, by BATT DISCH
warning message on EDU 1.
PROCEDURE
GEN 2 : Reset, then ON.
RFM A109E
R.A.I. Approved 3-48L
Rev. 16
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