Cirrus SR22 Pilot Operating Handbook page 456

Aircraft serials 22-3915 & subsequent 3600 pound takeoff weight
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Section 9
Supplements
even if the radiating ELT's antenna is disconnected.
Therefore, it does not check the integrity of the ELT system or
provide the same level of confidence as does an AM radio.
1. Tune aircraft receiver to 121.5 MHz.
2. Push switch lever to TEST position for approximately 1 second,
then release.
3. Results of the test are displayed by a series of indications (flash
codes), where the local LED, remote switch LED and buzzer(s)
activate for ½ second ON, followed by ½ second OFF. Error
codes, indicated by multiple flashes separated by 1-second
periods, will begin to display after approximately 1 second.
4. Flash Codes displayed with the associated conditions are as
follows:
a. 1-Flash: Indicates that the system is operational and that no
error conditions were found.
b. 2-Flashes: Not used. If displayed, correct condition before
further flight.
c. 3-Flashes: Not used. If displayed, correct condition before
further flight.
d. 4-Flashes: Indicates low output power. If displayed, correct
condition before further flight.
e. 5-Flashes: Indicates no position data present. If displayed,
correct condition before further flight.
f.
6-Flashes: Indicates G-switch loop is not present. If displayed,
correct condition before further flight.
g. 7-Flashes: Battery check. If displayed, correct condition
before further flight.
h. 8-Flashes: Indicates programming data missing. If displayed,
correct condition before further flight.
Section 10 - Safety Information
No Change.
6 of 6
Cirrus Design
SR22 / SR22T
P/N 13772-156
Original Issue: 11-20-14

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