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Airplane Flight Manual XA42
AFM-XA42-0040-002-A.01
Page 1.1
Page date:
Chapter 09
24.01.2011
9.1
EMERGENCY LOCATION TRANSMITTER
9.1.1
GENERAL
Emergency Location Transmitter (ELT) intalled is the Kannad 406 AF-COMPACT.
This supplement is a permanent part of the handbook and must be used as long as ELT is installed.
ELT is self powered by the ELT battery (replacement every 6 years).
ELT powered remote switch eliminated the need for aircraft power.
ELT qualifications: ETSO-2C91a & ETSO-2C126, (EUROCAE ED62), FAA TSO-C126 (RTCA-DO-204)
9.1.2 Limitations
In europe an ELT is mandatory for bordercrossing flights.
9.1.3 Emergency Procedures
To send an emergency signal, switch the ELT to “ON”
9.1.4 Normal Procedures
There are no changes to POH chapter 4.
9.1.5 Performance
There are no changes to POH chapter 5.
9.1.5 Weight and balance
Changes of CG and changes in empty weight are to be considered
if the ELT is removed according to chapter 6 of this POH.
9.1.7 Description of aircraft and systems
Controls:
1.
3-position switch ARM/OFF/ON;
2.
Visual indicator (red);
3.
DIN 12 socket for connection to an
optional Remote Control Panel, a
programming dongle or a programming equipment;
4.
BNC connector for the antenna.
Features:
• COSPAS-SARSAT Class II -20 °C to +55 °C
• 406 MHz transmission
• 121.5 MHz transmission
• G-Switch sensor (compliant with EUROCAE ED62 specifications)
• Battery (KIT BAT200 P/N: S1840510-01)
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