Side-Power SEP 100/185 T Servisní příručka stáhnout pdf (Strana 282)

Section 924

KANNAD AF 406 ELT

924 - 6 Page Date: 29. September 2014

Pilot´s Operating Handbook

EXTRA 330LX

924.7.1 SWITCH OPERATION

In a crash, an acceleration activated crash sensor (G-switch) turns the ELT ‘on’ automatically.

Activation is also accomplished by switching the cockpit mounted remote switch or the switch on

the ELT to the 'ON' position. To deactivate the ELT switch the switch on the ELT unit to the ‘OFF’

position.

N O T E

With remote switch disconnected or during transport the ELT can still be manually

activated using the local switch on the front of the ELT. Care should be taken when

transporting or shipping the ELT not to move the switch or allow packing material to

become lodged such as to toggle the switch.

It is possible to stop the ELT in case of unintentional activation:

• Switch to 'OFF'.

Regulations state that no transmission must be interrupted unless all means are used to contact

and inform the Air Traffic Controller of this action.

N O T E

As 406 MHz transmission is effective 50 seconds after the ELT activation, if it is switched

off within this delay, no further radio contact will be necessary.

924.8 HANDLING, SERVICING AND MAINTENANCE

Refer to the following applicable manufacturer instructions for further detailed information or when

working on the Kannad 406 AF ELT:

• Installation and Operation Manual 406 AF-COMPACT ELT (P/N: DOC08038E Rev. 04)

• Initial Installation Manual 406 AF-INTEGRA ELT (P/N: DOC09081C Rev. 02)

• Operation Manual 406 AF-INTEGRA ELT (P/N: DOC09078C Rev. 02)

Manufacturer:

Kannad Aviation (McMurdo Group)

Orolia SAS

Z.I. des 5 Chemins BP 23

56520 Guidel (F)

924.8.1 PERIODIC INSPECTION

Depending if the ELT is opened or not, PART 145 or FAR 145 (or equivalent) may be required. Refer

to local regulations.

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Side-Power SEP 100/185 T Servisní příručka Strana 282