Kannad 406 AF, Installation Manual, Operation Manual, Inspection Log

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INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG
KANNAD 406 AF / AF-H / AF (6D)
PAGE: 204
JUN 23/2008
3. Installation
• Determine the location of the ELT on board according to FAR/RTCA
recommendations.
• Determine the axis of the ELT, according to the type of KANNAD 406:
- KANNAD 406 AF: Refer to A. KANNAD 406 AF installation, page 206 ;
- KANNAD 406 AF-H: Refer to B. KANNAD 406 AF-H installation, page
207 ;
- KANNAD 406 AF (6D): Refer to C. KANNAD 406 AF (6D) installation,
page 208 .
• Drill 4 holes Ø 6 mm in the aircraft structure according to "Drilling mask".
Holes 4,5,6,7 shall be preferred.
• If the aircraft structure is not solid enough to withstand a 500 kg traction on
the bracket, a reinforcement plate (not supplied) should be installed as
shown
Figure 202: Bracket installation .
• Fix the bracket with the 4 screws, 8 washers and 4 nylstop nuts supplied.
IMPORTANT: tighten to a torque between 4 and 5 Newton x meter.
Figure 202: Bracket installation
Screw
Mounting bracket
Ø 6 mm holes
Aircraft structure
Washer (large)
Nylstop nut
Reinforcement plate (not supplied)
1
3
4
5
6
7
8
9
10
Flight Direction Arrow
Washer (small)