ELT ELT406GPS, Инструкция по установке, эксплуатации и обслуживанию

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The GPS system is tested separately.
GPS Self Test
Color Flashes Disposition
Green 5 ELT Valid GPS Data Present
Yellow 5 ELT Test Good
No GPS Data
Red 4 Battery Odometer less than 36 hours
Red 3 Transmitter Chain Failure
Red 2 Antenna Fault
1. Apply External Power to ELT
2. Move the aircraft to a location that has clear access to the GPS signal
3. Allow 10 minutes to acquire a GPS signal.
4. Press the Test button (3) times for one second each and release
5. The switch will return to the ARM position.
6. A green light will illuminate for 10 seconds after the second activation.
7. Light will go out for three seconds.
8. Note the fault legend for systems status
9. Insure reported GPS signal is within 2 NM range ( Average is 100 meters)
(Fig 17)
6.2 Self-Test Failure Chart
See the Systems Self Test (fig 16) and GPS (fig 17) in sec 6.1 for fault test charts.
6.3 Transmitter Test
The 406.037 frequency is tested by using the self test feature on either the front switch or the
remote switch. Unit status can be measured by the indication of light flashes. See Sec 6.1For
details. A troubleshooting guide in App. D is available.
Only one self test can be accomplished at a time. The design of this unit prevents continuous
testing. See Sec. 2.3 for details. These precautions will reduce the likelihood of false alerts and
reduce the demand on the overburdened SAR system.
6.4 Record of inspections
A.C. 43.13-1B Para. 12-23 (f) suggests the following sign-off after inspection:
I inspected the 406ELT system in this aircraft according to applicable Aircraft and
Manufacturer’s instructions and applicable FAA guidance and found that it meets the
requirements of section 91.207(d)
Signed ________________ Certificate _______________ Date ___________