INITIAL INSTALLATION MANUAL
AF INTEGRA / AF-H INTEGRA
PAGE: 11
JUN 01/2011
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.
(a) Fixed wing aircraft with AF INTEGRA
Refer to Figure 10: KANNAD AF INTEGRA, axis of installation
.
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
± 2°). Consequently, the AF INTEGRA shall be mounted:
- with the arrow of the "Flight direction" label pointed towards the front of
the aircraft;
- in any position parallel to the roll axis.
(b) Helicopters with AF INTEGRA
Refer to Figure 10: KANNAD AF INTEGRA, axis of installation
.
AF INTEGRA may be installed on helicopter. The ELT unit should be
mounted (with maximum tolerance of ± 2°):
• with "Flight direction" arrow towards the front of the helicopter;
• with the front face connectors pointing downwards at a 45° angle to
the yaw axis;
• in any position parallel to the 45° axis.
(c) Helicopters with AF-H INTEGRA
Refer to Figure 11: KANNAD AF-H INTEGRA, axis of installation
.
IMPORTANT: AF-H INTEGRA is designed to be mounted on board
helicopters only.
Summary of Contents for AF INTEGRA
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