Eads eurocopter AS 365 N3 - Page 342

COMPLEMENTARY FLIGHT MANUAL
AS 365 N3
9.31
07-50 Page 2
1.3 BRIEF DESCRIPTION
The navigation and radio-navigation equipment, the autopilot and flight coupler,
interface with the MFD system via the switching unit.
The structure of the system compensates for the loss of essential information:
- Loss of an attitude or heading gyro or air data computer ( reconfiguration on the
second sensor),
- Loss of the upper PFD screen (display of PFD function on lower screen and
possibility of complementary display of main navigation information in
COMPOSITE mode),
- Loss of ND screen (possibility of complementary display of main navigation
information on PFD upper screen in COMPOSITE mode).
Figure 1 - Display System