GEN BUS 1 : ON, check.
If failure is confirmed, proceed as follows:
Pilot ICS panel switch : Select FAIL position
BATTery switch : OFF. All loads of Generator
Bus #2 and Emergency Bus #2
are lost. All loads of Essential
Bus #2 are retained.
NOTE
In this event all loads on #1 Bus are maintained by Generator 1.
After switching off the BATTery
the following message will be
indicated: INV 2, SAS 2 OFF,
BATT OFF cautions, ELECTRI-
CAL warning as well as DAU ch
A and EDU Primary will be lost.
Failure of generator 1 or 2 and generator bus #1 or #2
(Helicopter equipped with emergency bus)
The failure of Generator 1 and#1DCBUSisindicated by #1 DC GEN, BUS
TIE, caution messages on EDU 1.
All loads of Generator Bus #1 and both copilot EFIS (if installed) are lost. All
loads of Essential Bus #1 and Emergency Bus #1 are retained.
NOTE
In this event all loads on #2 Bus are maintained by Generator 2.
NOTE
The landing light(s) or the searchlight (if installed) can be turned
ON for only one minute before landing.
Simultaneous operation of the landing light(s) and the searchlight
is prohibited.
RFM A109E
3-48M E.A.S.A. Approved
Rev. 35
To Next Page
Loading...