INSTALLATION MANUAL OPERATION MANUAL INSPECTION LOG
KANNAD 406 AF-COMPACT
PAGE: 206
FEB 01/2008
• Drill 4 holes Ø 6 mm in the aircraft structure according to "Drilling mask"
Refer to § 2. ELT Drilling Mask, page 502
). Inner holes (1, 2, 3, 4) 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 203: 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.
• Verify that the ELT identification label matches the aircraft tail number.
Figure 203: Bracket installation
