INSTALLATION MANUAL OPERATION MANUAL
KANNAD 406 SURVIVAL
PAGE: 205
JUL 08/2013
(2) Bracket installation
• Determine the location of the ELT on board according to FAR/RTCA
recommendations.
CAUTION: Do not install the ELT in a location directly exposed to the
sun.
• Drill 3 holes Ø 5,5 mm in the aircraft structure according to "Drilling mask"
page 503 of this document.
• Fix the bracket with the 3 screws and nylstop nuts or 3 rivets.
(3) ELT installation
• Check that the ELT identification label matches the aircraft tail number.
• If the mounting bracket is fitted with a Programming Dongle (P/N
S1820514-01), remove the Water Switch Sensor connector and connect
the programming dongle to the ELT.
• Perform a Self-test (see paragraph "SELF-TEST").
• If test result is OK, switch back to "OFF".
• Disconnect the Programming
Dongle (if applicable) and stow
it in the compartment designed
to this effect inside the bracket
(for Mounting bracket
S1820511-03 only)
• Reconnect the Water Switch Sensor (if applicable).
SW
ITC
H
TO
"A
R
M
"
T
OE
N
AB
L
E
AU
TO
M
AT
IC
W
A
T
ER
A
C
T
IV
A
T
IO
N
SW
IT
C
H
TO
"A
R
M"
T
O
E
N
AB
LE
AU
T
O
M
A
TI
C
W
AT
ER
A
C
T
IVA
TI
O
N
An
t
Ar
m
Of
f
O
n
R
C
An
t
Ar
mO
ff
O
n
RC
