Bracket Installation Procedure; Determine Location And Direction - Kannad 406 AF-COMPACT Installation Manual

B. Bracket installation procedure

(1)Determine location and direction

• Determine the location of the ELT onboard according to
and bracket installation recommendations page
CAUTION: Do not install the ELT in a location directly exposed to the
sun.
- The G-Switch axis shall be directed to sense the primary crash pulse
along the longitudinal axis of the aircraft. Reference to the G-Switch is
given by the arrow "Flight direction" on the label affixed to the top of the
ELT.
Figure 8: KANNAD 406 AF-COMPACT, axis of installation
(a) Fixed wing aircraft
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-COMPACT shall be mounted:
- with the arrow of the "Flight direction" label pointed towards the front of
INITIAL INSTALLATION MANUAL
KANNAD 406 AF-COMPACT / KANNAD 406 AF COMPACT ER
paragraph A. ELT
8.
MAY 05/2010
SEP 16/2009
PAGE: 9