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AGUSTA A109E - Page 242

AGUSTA A109E
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- SAS 1 system
- ADI pilot (EHSI-74 version)
- HSI standby (EHSI-74 version)
- Landing gear position indicator
- Landing light(s)
- Emergency floats
- Inverter #1
EMERGENCY BUS 2
- Fuel quantity 2
- Fuel pump 2
- Fuel shut-off valve 2
- Engine 2 fire detector system
- 2 engine compartment fire extinguisher system
- Hydraulic system
- Eng. Gov. CTL
- EDU N°2
- DAU ch B
- ADI standby
- Cockpit wander light (pilot)
- Searchlight (if installed)
- EADI pilot (EFIS version)
- Emergency floats
- VHF 2
- VOR 2
NOTE
The pilot is allowed to operate the VHF 2 system for a period
of 15 minutes reception and 3 minutes transmission during the
next 25 minutes, commencing from the expiration of the first 5
minutes.
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
3-48T E.A.S.A. Approved
Rev. 35
UNMAINTAINED COPY