INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG
KANNAD 406 AF / AF-H / AF (6D)
PAGE: 206
JUN 23/2008
A. KANNAD 406 AF installation
Figure 205: KANNAD 406 AF installation
(1) Fixed wings
The G-Switch sensor axis shall be pointed to sense the primary crash
pulse along the longitudinal axis of the aircraft (with maximum tolerance of
15°). Consequently, the KANNAD 406-AF shall be mounted with the arrow
of the "Direction of Flight" label pointed towards the front of the aircraft.
(2) Helicopters
The KANNAD 406 AF can be installed in its standard version on helicopter.
The ELT unit should be mounted:
• with the front face connectors pointing downwards at a 45° angle to
the yaw axis;
• and with "Direction of Flight" arrow towards the front of the helicopter.
NOTE: Should the KANNAD 406 AF be installed on board helicopter, it will
be necessary to make a special mounting base to install the ELT.
Summary of Contents for 406 AF
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