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AGUSTA A109E - Page 244

AGUSTA A109E
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WARNING
In the event of 1 a.c. bus system failure the following
instruments and equipment will continue to operate:
- VOR/ILS N°2
- ADF
-VG2
- SAS 2
WARNING
In the event of N°2 a.c. bus system failure the following
instruments and equipment will continue to operate:
- VOR/ILS N°1
-VG1
- SAS 1
- GYRO COMPASS
- HSI
RAD-MSTR (RADIO MASTER) SWITCH FAILURE
In case of RAD-MSTR (Radio Master) switch failure disengage the 1 and 2
RADIO MASTER OVRD circuit breakers then use the radio equipment as
desired by means of their control panels.
HELIPILOT MALFUNCTION
During operation of the Helipilot System, malfunctions may occur which
require pilot intervention.
These malfunctions are discussed in detail in the following paragraphs.
CAUTION
Following a single SAS failure, the AUTOTRIM function is
inoperative. In this condition the pilot is recommended to fly
continuously checking and re-centering the API position or to fly
decoupled (in ATTD mode), due to the reduced system authority.
RFM A109E
3-48V E.A.S.A. Approved
Rev. 35
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