Eurocopter AS 350 83 Flight Manual page 267

COMPLEMENTARY FLIGHT MANUAL
.SECTION 7.9
2 -AC POWER SYSTEM
1~
The AC power generation system is an optional installation required when
the aircraft is equipped with an automatic pilot or with certain
gyroscopic instruments.
Two different types of installation are available, depending on the power
capacity required.
AC power is supplied by a static inverter from the DC power system. The
.
inverter is located beneath the cabin floor. Performance characteristics
are as follows:
250-VA A.C Dower svstem
--Input voltage 28 VDC
-Output voltages 115 and 26 VAC
-Frequency 400 Hz
-Power output: 115 VAC 150 VA ) limited to 2S0 VA
26 VAC 150 VA)
10-VA A.C. Dower svstem
-Input voltage 28 VDC
-Output voltage 26 VAC
-Frequency 400 Hz
-Power output 10 VA
2 DESCRIPTION OPERATION
The static inverter is supplied from bus bar PP9, through a fuse located on
the RH side fuse panel (16-amp. fuse for the 250-VA power system, 2.5-amp.
fuse for the 10-VA power system).
The system is switched on by means of the "INVERT" push-button located on
the control panel.
.
AC power distribution circuits are protected by fuses located on the LH
side fuse panel.
An amber caution light on the instrument panel indicates a failure of the
A.C. power generation system.
.
350 83 7.9
97-40 Page 5