Cirrus SR22T Maintenance Manual

Brand
Cirrus
Model
SR22T
Type
Maintenance Manual

This manual is also suitable for

CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
25-60
Page 1
All
EFFECTIVITY:
EMERGENCY
1. DESCRIPTION
A. Emergency Locator Transmitter (ELT)
This airplane is equipped with a self-contained ELT. The ELT transmitter is installed immediately
behind the aft cabin bulkhead. The ELT is mounted slightly to the right of the airplane centerline. The
transmitter and antenna are accessible through an access panel at the base of the baggage compart-
ment bulkhead. ELT models available on the airplane include the ACK E-01 ELT, the Artex ME406 ELT,
and the Artex ELT 1000.
Serials 22-0002 thru 22-3827, Serials 22T-0001 thru 22T-0267 w/ ACK E-01 ELT: The transmitter unit
is mounted longitudinally in the airplane. If rapid deceleration is detected, the transmitter will repeat-
edly transmit VHF band audio sweeps at 121.5 Mhz and 243.0 Mhz approximately 0.5 seconds apart.
The transmitter can be removed from the airplane and used as a personal locating device if it is neces-
sary to leave the airplane after an accident.
The main transmitter control switch is labeled ON-OFF-ARMED. The transmitter is in the armed posi-
tion for normal operations. Eight dated “D” cell alkaline batteries contained within the transmitter unit
provide power to the transmitter. Replace all ELT batteries at the same time and with the same expira-
tion date stamp. The expiration date of the batteries must be indicated on the outside of the ELT bat-
tery case and recorded in the aircraft logs.
The ELT Remote Switch and Control Panel Indicator (RCPI) is located below the circuit breakers on
the circuit breaker panel. The RCPI provides test and monitoring functions for the transmitter. The
panel contains a button labeled ON, a button labeled RESET, and a red LED indicator light. The ON
button is used to test the unit in accordance with the manufacturer’s approved Instructions For Contin-
ued Airworthiness. The RESET button can be used to cancel an inadvertent transmission. The red
light flashes when the ELT is transmitting. A Duracell PX28L or Kodak K28L 6-volt lithium battery
mounted in the panel powers the LED.
WARNING:
The ACK E-01 ELT is designed to use only Duracell MN1300 or PC 1300 alkaline
batteries which are dated by the manufacturer. This ELT does not meet the
requirements of TSO-91a or 14 CFR 91.207 if used with any other type of battery.
ELT and RCPI batteries must be inspected in accordance with the requirements of
the replacement schedule in Chapter 5. The ELT and RCPI batteries must be
replaced upon reaching the date stamped on the batteries or whenever the batter-
ies have been in use for one cumulative hour.
For additional information on the ACK ELT, refer to the Model E-01 ELT Installation and Operation Man-
ual. (Refer to 05-10)
Serials w/ Artex ME406 ELT: The transmitter unit is mounted longitudinally in the airplane in order to
detect deceleration greater than 2.3 g. If rapid deceleration is detected, the transmitter will repeatedly
transmit VHF band audio sweeps at 121.5 Mhz until battery power is gone. In addition, for the first 24
hours of operation, a 406 MHz signal is transmitted at 50-second intervals. This transmission lasts 440
ms and contains identification data programmed into the beacon and is received by Cospas-Sarsat
satellites. The transmitted data is referenced in a database (maintained by the national authority
responsible for ELT registration) and used to identify the beacon and owner. The transmitter can be
removed from the airplane and used as a personal locating device if it is necessary to leave the air-
plane after an accident.
15 Dec 2014
25-60
Page 2
All
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
15 Dec 2014
The main transmitter control switch is labeled ON-ARM. The transmitter is in the armed position for
normal operations. A red LED indicator light flashes when the ELT is transmitting. A battery pack con-
sisting of two “D” cell lithium batteries mounts to a cover assembly within the transmitter to provide
power to the transmitter. The expiration date of the batteries must be indicated on the outside of the
ELT battery case and recorded in the aircraft logs.
Serials w/o Perspective Avionics: The ELT Remote Switch and Control Panel Indicator (RCPI) are
located below the circuit breakers on the circuit breaker panel.
Serials w/ Perspective Avionics: The ELT Remote Switch and Control Panel Indicator (RCPI) are
located forward of the circuit breakers on the LH side of the center console.
The RCPI provides test and monitoring functions for the transmitter. The panel contains a switch
labeled ON-ARM and a red LED indicator light. The ON switch is used to test the unit in accordance
with the manufacturer's approved service instructions. The red LED indicator light flashes when the
ELT is transmitting. Power to the LED is supplied by either the clock bus on the MCU (Serials 22-1863
thru 22-2083) or by a 6V lithium battery in the RCPI (Serials 22-2084 thru 22-4163, 22T-0001 thru 22T-
0953, 22T-0955 thru 22T-0962).
A warning buzzer is mounted to the ELT shelf. When the ELT is activated, the buzzer “beeps” periodi-
cally. This buzzer operates in tandem with the ELT panel indicator and would serve as a redundant
indicator. Power to the buzzer is supplied by the ELT batteries.
After setting transmitter switch to ARM position, the ELT automatically enters a self-test mode. The
self-test transmits a 406 MHz test coded pulse that monitors certain system functions before shutting
off. The test pulse is ignored by any satellite that receives the signal, but the ELT uses this pulse to
check output power and frequency. Other parameters of the ELT are checked and a set of error codes
is generated if a problem is found. The error codes are indicated by a series of pulses on the transmit-
ter LED, remote control panel indicator LED, and alert buzzer. One pulse indicates that the system is
operational and no error conditions were found. For a list of error codes, refer to the Installation and
Maintenance Manual for the ME406 ELT. (Refer to 05-10)
WARNING:
ELT and RCPI batteries must be inspected in accordance with the requirements of
the replacement schedule in Chapter 5. The ELT and RCPI batteries must be
replaced upon reaching the date stamped on the batteries, after an inadvertent
activation of unknown duration, or whenever the batteries have been in use for
one cumulative hour.
For additional information on the Artex ME406 ELT, refer to the Installation and Maintenance Manual
for the ME406 ELT. (Refer to 05-10)
Serials 22-4164 & subs, 22T-0954, 22T-0963 & subs w/ Artex ELT 1000: The transmitter unit is
mounted longitudinally in the airplane in order to detect deceleration greater than 2.3 g. The transmit-
ter unit is automatically activated upon sensing a change of velocity along its longitudinal axis exceed-
ing 4 to 5 feet per second, or upon sensing deployment of the Cirrus Airframe Parachute System
(CAPS). Once activated, the ELT transmits VHF band audio sweeps at 121.5 MHz until battery power
is gone. In addition, for the first 24 hours of operation, a 406 MHz signal is transmitted at 50-second
intervals. This transmission lasts 440 milliseconds and contains aircraft-specific information and GPS
position data provided by the Garmin avionics. The transmitted data is referenced in a database main-
tained by the national authority responsible for ELT registration to identify the beacon and owner. The
transmitter can be removed from the airplane and used as a personal locating device if it is necessary
to leave the airplane after an accident.
The main transmitter control switch is labeled ON-ARM/OFF-TEST. The transmitter is in the ARM/OFF
position for normal operations. A red LED indicator light flashes when the ELT is transmitting. A battery
pack consisting of two "D" cell lithium batteries mounts to a cover assembly within the transmitter to
provide power to the transmitter. The expiration date of the batteries must be indicated on the outside
of the ELT battery case and recorded in the aircraft logs.
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
25-60
Page 3
All
EFFECTIVITY:
The ELT Remote Switch and Control Panel Indicator (RCPI) are located forward of the circuit breakers
on the LH side of the center console.
The RCPI provides test and monitoring functions for the transmitter. The panel contains a switch
labeled ON-ARM/OFF-TEST and a red LED indicator light. The TEST button is used to test the unit in
accordance with the manufacturer's approved service instructions. The red LED indicator light flashes
when the ELT is transmitting.
A warning buzzer is mounted to the ELT shelf. When the ELT is activated, the buzzer "beeps" periodi-
cally. This buzzer operates in tandem with the ELT panel indicator and would serve as a redundant
indicator. Power to the buzzer is supplied by the ELT batteries.
After pressing and releasing TEST on the RCPI switch, the ELT automatically enters a self-test mode.
The self-test transmits a 406 MHz test coded pulse that monitors certain system functions before shut-
ting off. The test pulse is ignored by any satellite that receives the signal, but the ELT uses this pulse to
check output power and frequency. Other parameters of the ELT are checked and a set of error codes
is generated if a problem is found. The error codes are indicated by a series of pulses on the transmit-
ter LED, remote control panel indicator LED, and alert buzzer. One pulse indicates that the system is
operational and no error conditions were found. For a list of error codes, refer to the Installation and
Maintenance Manual for the Artex ELT 1000. (Refer to 05-10)
WARNING:
ELT batteries must be inspected in accordance with the requirements of the
replacement schedule in Chapter 5. The ELT batteries must be replaced upon
reaching the date stamped on the batteries, after an inadvertent activation of
unknown duration, or whenever the batteries have been in use for one cumulative
hour.
For additional information on the Artex ELT 1000, refer to the Installation and Maintenance Manual for
the Artex ELT 1000. (Refer to 05-10)
15 Dec 2014
25-60
Page 4
Serials 22-0002 thru 22-3827, Serials 22T-0001 thru
22T-0267 w/ ACK E-01 ELT
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
01 May 2012
2. MAINTENANCE PRACTICES
A. Emergency Locator Transmitter - Serials 22-0002 thru 22-3827, Serials 22T-0001 thru 22T-0267
w/ ACK E-01 ELT (See Figure 25-601)
(1) Removal - ELT
(a) Remove access panel CB06. (Refer to 06-00)
(b) Set transmitter control switch to OFF position.
(c) Disconnect remote control panel indicator cable from transmitter.
(d) Disconnect antenna cable from transmitter.
(e) Remove portable antenna from transmitter.
(f) Open quick release straps securing transmitter to mounting tray. Remove transmitter from
airplane.
(2) Installation - ELT
CAUTION: ELT must be installed with printed arrow on battery case pointing in the direction
of flight.
(a) Position transmitter to mounting tray with printed arrow on battery case pointing in direc-
tion of flight.
Note: The quick release straps which secure the transmitter to the mounting tray
are slightly different sizes. The strap which fits around front of transmitter is
marked FRONT. The strap which fits around battery end of transmitter is
marked BATTERY.
(b) Close quick release straps securing transmitter to mounting tray.
(c) Position portable antenna to transmitter and secure.
(d) Connect antenna cable to transmitter.
(e) Connect remote control panel indicator cable to transmitter.
(f) Perform Operational Test - ELT. (Refer to 25-60)
(g) Install access panel CB06. (Refer to 06-00)
(3) Operational Test - ELT
Note: Regulations require that transmitter tests only be done during the first 5 minutes of
each hour and must not last for more than 3 audio sweeps (1.5 seconds). If you
are at a location where there is an FAA control tower or other monitoring facility,
notify the facility before beginning the tests. Never activate the ELT while airborne
for any reason.
A low quality AM broadcast receiver should be used to determine if energy is
being transmitted from the antenna. When the antenna of the radio (tuning dial on
any setting) is held about 6 inches from the activated ELT antenna, the ELT aural
tone will be heard on the AM broadcast receiver. This is not a measured check,
but it does provide confidence that the antenna is radiating sufficient power to aid
search and rescue. The aircraft’s VHF receiver, tuned to 121.5 MHz, may also be
used. This receiver, however, is more sensitive and could pick up a weak signal
even if the radiating ELT’s antenna is disconnected. Thus it does not check the
integrity of the ELT system or provide the same level of confidence as does an AM
radio.
(a) Remove access panel CB06. (Refer to 06-00)
(b) Monitor 121.5 Mhz using aircraft COM receiver or portable hand-held receiver.
(c) Turn receiver squelch control all the way down or to OFF position.
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
25-60
Page 5
Serials 22-0002 thru 22-3827, Serials 22T-0001 thru
22T-0267 w/ ACK E-01 ELT
EFFECTIVITY:
(d) Set transmitter control switch to ON position.
(e) Verify audio sweep tone can be heard on COM receiver.
(f) Set transmitter control switch to ARMED position.
(g) Press ON button on remote control panel indicator.
(h) Verify LED flashes and is readily visible from pilots operating position.
(i) Verify audio sweep tone can be heard on COM receiver.
(j) Push RESET button on remote control panel indicator.
(k) Verify LED stops flashing and audio sweep tone stops transmitting.
(l) Install access panel CB06. (Refer to 06-00)
(4) Inspection/Check - ELT
Note: Perform Inspection/Check in accordance with 14 CFR 91.207.
(a) Remove ELT. (Refer to 25-60)
(b) Visually inspect mounting tray, fasteners, and mechanical assemblies for security.
(c) Visually inspect antenna cable and RCPI cable for cuts, abrasions, or signs of wear.
(d) Visually inspect all cable connectors and mating plugs for signs of corrosion.
Note: Pay special attention to antenna cable center conductor pins which are
prone to retracting into connector housing.
(e) Visually inspect and confirm proper seating of all connector pins.
(f) Check transmitter batteries for expiration date and corrosion. Replace if necessary. (Refer
to 25-60)
(g) Check RCPI battery for expiration date and corrosion. Replace if necessary. (Refer to 25-
60)
(h) Verify operation of G-switch.
Note: Regulations require that transmitter tests only be done during the first 5
minutes of each hour and must not last for more than 3 audio sweeps (1.5
seconds). If you are at a location where there is an FAA control tower or
other monitoring facility, notify the facility before beginning the tests.
1
Set transmitter control switch to ARMED position.
2
Hold transmitter with printed arrow on battery case pointing forward.
3
Activate ELT with a rapid forward throwing motion coupled by a rapid reversing
motion.
4
Verify transmitter activation by monitoring 121.5 Mhz with aircraft COM receiver or
portable hand-held receiver.
5
Set transmitter control switch to OFF position.
(i) Install ELT. (Refer to 25-60)
01 May 2012
25-60
Page 6
Serials 22-0002 thru 22-0820
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
01 May 2012
Figure 25-601
ACK E-01 ELT - Serials 22-0002 thru 22-0820 (Sheet 1 of 3)
CIRCUIT BREAKER
PANEL
(REF)
8
11
12
9
LEGEND
1. ELT Portable Antenna
2. Antenna Cable
3. RJ-11 Coupler
4. RCPI Connecting Cable
5. ELT
6 ELT Antenna
7. Adel Clamp
8. Washer
9. Nut
10. Cable Tie
11. Remote Control
Panel Indicator (RCPI)
12. Screw
SR22_MM25_1419D
1
2
2
ELT MOUNTING
TRAY
(REF)
3
4
5
6
7
8
9
4
10
7
Serials 22-0002 thru 22-0820.
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
25-60
Page 7
Serials 22-0821 thru 22-3025 w/o Perspective Avionics
EFFECTIVITY:
Figure 25-601
ACK E-01 ELT - Serials 22-0821 thru 22-3025 w/o Perspective Avionics (Sheet 2 of 3)
Serials 22-0821 thru 22-3025 w/ ACK E-01 ELT w/o Perspective Avionics.
CIRCUIT BREAKER
PANEL
(REF)
8
11
12
9
LEGEND
1. ELT Portable Antenna
2. Antenna Cable
3. RJ-11 Coupler
4. RCPI Connecting Cable
5. ELT
6 ELT Antenna
7. Adel Clamp
8. Washer
9. Nut
10. Cable Tie
11. Remote Control
Panel Indicator (RCPI)
12. Screw
SR22_MM25_1920D
10
7
9
8
6
5
3
ELT MOUNTING
TRAY
(REF)
2
2
1
4
15 Dec 2014
25-60
Page 8
Serials 22-3026 thru 22-3827, Serials 22T-0001 thru
22T-0267 w/ Perspective
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
15 Dec 2014
Figure 25-601
ACK E-01 ELT - Serials 22-3026 thru 22-3827, Serials 22T-0001 thru 22T-0267 w/ Perspective (Sheet 3 of 3)
8
2
12
ELT MOUNTING
TRAY
(REF)
12
11
12
8
6
8
9
1
10
5
13
8
LEGEND
1. ELT Portable Antenna
2. Antenna Cable
3. RJ-11 Coupler
4. RCPI Connecting Cable
5. ELT
6 ELT Antenna
8. Washer
9. Nut
10. Cable Tie
11. Remote Control
Panel Indicator (RCPI)
12. Screw
13. ELT Shield
14. Clamp
15. Spacer
9
12
8
15
14
3
4
Serials 22-3026 thru 22-3827, Serials 22T-0001 thru 22T-0267
w/ ACK E-01 ELT & w/ Perspective Avionics.
CENTER
CONSOLE
(REF)
SR22_MM25_2883C
8
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
25-60
Page 9
Serials 22-1863 thru 22-4163, 22T-0001 thru 22T-0953,
22T-0955 thru 22T-0962 w/ Artex ME406 ELT, Serials
22-4164 & subs, 22T-0954, 22T-0963 & subs w/ Artex
EFFECTIVITY:
B. Emergency Locator Transmitter - Serials 22-1863 thru 22-4163, 22T-0001 thru 22T-0953, 22T-
0955 thru 22T-0962 w/ Artex ME406 ELT, Serials 22-4164 & subs, 22T-0954, 22T-0963 & subs w/
Artex ELT 1000 (See Figure 25-602)
(1) Removal - ELT
(a) Remove access panel CB06. (Refer to 06-00)
(b) Disconnect antenna cable from transmitter.
(c) Disconnect remote control panel indicator cable from transmitter.
(d) Loosen strap securing transmitter to mounting tray. Remove transmitter from airplane.
(2) Installation - ELT
(a) Position transmitter to mounting tray and secure with strap.
(b) Connect remote control panel indicator cable to transmitter.
(c) Connect antenna cable to transmitter.
(d) Serials w/ Artex ME406 ELT: Perform Operational Test - ELT. (Refer to 25-60)
(e) Serials w/ Artex ELT 1000: Perform Operational Test - ELT. (Refer to 25-60)
(f) Install access panel CB06. (Refer to 06-00)
(3) Operational Test - ELT - Serials 22-1863 thru 22-4163, 22T-0001 thru 22T-0953, 22T-0955 thru
22T-0962 w/ Artex ME406 ELT
Note: Regulations require that transmitter tests only be done during the first 5 minutes of
each hour and must not last for more than 5 seconds. If you are at a location
where there is an FAA control tower or other monitoring facility, notify the facility
before beginning the tests. Never activate the ELT while airborne for any reason.
(a) Remove access panel CB06. (Refer to 06-00)
(b) Monitor 121.5 Mhz using aircraft COM receiver or portable hand-held receiver.
(c) Turn receiver squelch control all the way down or to OFF position.
(d) Set remote control panel indicator switch to ON position.
(e) Verify three audio sweep tones can be heard on COM receiver or portable hand-held
receiver.
(f) Verify audio tone can be heard from buzzer.
(g) Verify LED flashes and is readily visible from pilot’s operating position.
(h) Set remote control panel indicator switch to ARM position.
(i) Verify LED stays on for approximately 1 second, then turns off.
(j) If LED displays an error code, refer to Installation and Maintenance Manual for the Artex
ELT 1000. (Refer to 05-10)
Note: A low quality AM broadcast receiver should be used to determine if energy
is being transmitted from the antenna.The aircraft transceiver is not recom-
mended for the following steps because it is too sensitive to verify the integ-
rity of the antenna system and it may pick up a weak signal even if the
antenna is disconnected from the ELT. Thus it does not check the integrity
of the ELT system or provide the same level of confidence as does an AM
radio.
This is not a measured check, but it does provide confidence that the
antenna is radiating sufficient power to aid search and rescue.
(k) Locate radio approximately six inches from antenna.
(l) Set remote control panel indicator switch to ON position.
(m) Verify three audio sweep tones can be heard on portable hand-held receiver.
(n) Set remote control panel indicator switch to ARM position.
15 Dec 2014
25-60
Page 10
Serials 22-1863 thru 22-4163, 22T-0001 thru 22T-0953,
22T-0955 thru 22T-0962 w/ Artex ME406 ELT, Serials
22-4164 & subs, 22T-0954, 22T-0963 & subs w/ Artex
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
15 Dec 2014
(o) Verify LED stays on for approximately 1 second, then turns off.
(p) If LED displays an error code, refer to Installation and Maintenance Manual for the Artex
ELT 1000. (Refer to 05-10)
(q) Install access panel CB06. (Refer to 06-00)
(4) Operational Test - ELT - Serials 22-4164 & subs, 22T-0954, 22T-0963 & subs w/ Artex ELT 1000
Note: Regulations require that transmitter tests only be done during the first 5 minutes of
each hour and must not last for more than 5 seconds. If you are at a location
where there is an FAA control tower or other monitoring facility, notify the facility
before beginning the tests. Never activate the ELT while airborne for any reason.
(a) Remove access panel CB06. (Refer to 06-00)
Note: If using portable AM receiver, locate radio approximately 20 to 30 feet from
antenna.
(b) Monitor 121.5 Mhz using aircraft COM receiver or portable hand-held receiver.
(c) Turn receiver squelch control all the way down or to OFF position.
(d) On remote control panel indicator switch, press TEST for 1 second, then release. LED will
begin flashing continuously.
(e) Verify three audio sweep tones can be heard on COM receiver or portable hand-held
receiver.
(f) Verify audio tone can be heard from buzzer.
(g) Verify LED stays on for approximately 1 second, then turns off, and is readily visible from
pilot's operating position.
(h) If LED displays an error code, refer to Installation and Maintenance Manual for the Artex
ELT 1000. (Refer to 05-10)
Note: A low quality AM broadcast receiver should be used to determine if energy
is being transmitted from the antenna.The aircraft transceiver is not recom-
mended for the following steps because it is too sensitive to verify the integ-
rity of the antenna system and it may pick up a weak signal even if the
antenna is disconnected from the ELT. Thus it does not check the integrity
of the ELT system or provide the same level of confidence as does an AM
radio.
This is not a measured check, but it does provide confidence that the
antenna is radiating sufficient power to aid search and rescue.
(i) Locate radio approximately 6 inches from antenna.
(j) Set remote control panel indicator switch to ON position.
(k) Verify three audio sweep tones can be heard on receiver.
(l) Set remote control panel indicator switch to ARM/OFF position.
(m) Install access panel CB06. (Refer to 06-00)
(5) Inspection/Check - ELT
Note: Perform Inspection/Check in accordance with 14 CFR 91.207.
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
25-60
Page 11
Serials 22-1863 thru 22-4163, 22T-0001 thru 22T-0953,
22T-0955 thru 22T-0962 w/ Artex ME406 ELT, Serials
22-4164 & subs, 22T-0954, 22T-0963 & subs w/ Artex
EFFECTIVITY:
(a) Acquire necessary tools, equipment, and supplies.
(b) Remove ELT. (Refer to 25-60)
(c) Visually inspect mounting tray, fasteners, and hardware for cracks and security.
(d) Visually inspect antenna cable and RCPI cable for cuts, abrasions, or signs of wear.
(e) Visually inspect all cable connectors and mating plugs for signs of corrosion.
Note: Pay special attention to antenna cable center conductor pins which are
prone to retracting into connector housing.
(f) Visually inspect and confirm proper seating of all connector pins.
(g) Check transmitter batteries for expiration date, corrosion and damage to wiring and hous-
ing. Replace if necessary. (Refer to 25-60)
(h) Verify operation of G-switch.
Note: Regulations require that transmitter tests only be done during the first 5
minutes of each hour and must not last for more than 5 seconds. If you are
at a location where there is an FAA control tower or other monitoring facility,
notify the facility before beginning the tests.
G-switch activation requires pins 5 and 12 of the D-sub connector to be con-
nected (shorted) together. A shorting plug connector must be used to verify
operation of G-switch.
1
Connect shorting plug connector to transmitter.
2
Set transmitter control switch to ARM position.
3
Hold transmitter with printed arrow on battery case pointing forward.
4
Activate ELT with a rapid forward throwing motion coupled by a rapid reversing
motion.
5
Verify ELT activation by observing transmitter LED and by monitoring 121.5 Mhz
with aircraft COM receiver or portable hand-held receiver.
6
Reset ELT by setting transmitter control switch to ON position, then to ARM position.
(i) Install ELT. (Refer to 25-60)
Note: Digital message verification is not mandatory per 14 CFR 91.207 but is
highly recommended.
(j) Verify 406 MHz digital message.
1
Disconnect antenna cable from transmitter.
2
Connect ELT test set to transmitter.
3
Power up test set per manufacturer’s operating instructions.
4
Set transmitter control switch to ON position, then to ARM position.
Description P/N or Spec. Supplier Purpose
Shorting Plug Connector 500-0079 Artex Aircraft Supplies
Canby, Oregon 97013
800-547-8901
Enables G-switch
activation.
ELT Test Set 453-1000 Artex Aircraft Supplies
Canby, Oregon 97013
800-547-8901
Test 406 MHz digi-
tal message.
15 Dec 2014
25-60
Page 12
All
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
15 Dec 2014
5
After test set receives digital message from transmitter, verify information is correct
for country code, aircraft Identification, etc.
6
Verify 15 digit transmitter identification number matches number shown on transmit-
ter product label.
7
Power down test set per manufacturer’s operating instructions.
8
Disconnect test set from transmitter.
9
Connect antenna cable to transmitter.
C. ELT Battery
For additional information on the ELT battery, refer to the Model E-01 ELT Installation and Operation
Manual, the Installation and Maintenance Manual for the ME406 ELT, or the Installation and Mainte-
nance Manual for the Artex ELT 1000. (Refer to 05-10)
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
25-60
Page 13
Serials 22-1863 thru 3025 w/o Perspective Avionics
EFFECTIVITY:
Figure 25-602
Artex ME406 ELT Installation - Serials 22-1863 thru 3025 w/o Perspective Avionics (Sheet 1 of 4)
Serials 22-1863 thru 3025 w/
Artex ME406 ELT & w/o Perspective Avionics.
8
W
A
R
N
I
N
G
F
O
R
W
A
R
D
G
H
F
E
12
1
2
CIRCUIT BREAKER
PANEL
(REF)
9
10
7
ELT MOUNTING
TRAY
(REF)
SR22_MM25_2347C
LEGEND
1. Antenna Cable
2. RCPI Connecting Cable
3. ELT
4 ELT Antenna
5. Adel Clamp
6. Washer
7. Nut
8. Cable Tie
9. Remote Control
Panel Indicator (RCPI)
10. Screw
11. Buzzer
12. Label
13. ELT Shelf
CIRCUIT BREAKER
PANEL
(REF)
10
9
6
7
10
6
7
11
4
6
7
5
2
13
10
3
Serials 22-1863 thru 22-2083.
Serials 22-2084 thru 22-3025
15 Dec 2014
25-60
Page 14
Serials w/ Perspective Avionics
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
15 Dec 2014
Figure 25-602
Artex ME406 ELT Installation - Serials w/ Perspective Avionics (Sheet 2 of 4)
Serials 22-3025 thru 22-4030, 22-4032, 22-4045,
22T-0001 thru 0689 w/ Artex ME406 ELT.
SR22_MM25_3669
C
DETAIL
CENTER CONSOLE
(REF)
12
10
9
6
7
D
DETAIL
2
2
LEGEND
1. Antenna Cable
2. RCPI Connecting Cable
3. ELT
4 ELT Antenna
6. Washer
7. Nut
8. Cable Tie
9. Remote Control
Panel Indicator (RCPI)
10. Screw
11. Buzzer
12. Label
13. Spacer
14. Cable Tie Mount
15. Clamp
16. Grommet
17. ELT Shelf
1
10
ELT MOUNTING
TRAY
(REF)
10
6
11
4
6
7
13
17
8
10
3
6
6
10
14
15
16
6
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
25-60
Page 15
Serials w/ Perspective Avionics
EFFECTIVITY:
Figure 25-602
Artex ME406 ELT Installation - Serials w/ Perspective Avionics (Sheet 3 of 4)
2
2
13
17
CENTER CONSOLE
(REF)
LEGEND
1. Antenna Cable
2. RCPI Connecting Cable
3. ELT
4 ELT Antenna
6. Washer
7. Nut
8. Cable Tie
9. Remote Control
Panel Indicator (RCPI)
10. Screw
11. Buzzer
12. Label
13. Spacer
14. Cable Tie Mount
15. Clamp
16. Grommet
17. ELT Shelf
12
1
10
ELT MOUNTING
TRAY
(REF)
10
9
6
7
10
6
11
4
6
7
8
10
3
6
6
10
14
15
16
SR22_MM25_2881D
Serials 22-4031, 22-4033 thru 22-4044, 22-4046 thru 22-4163,
22T-0690 thru 22T-0953, 22T-0955 thru 22T-0962 w/Artex ME406 ELT.
6
F
DETAIL
E
DETAIL
15 Dec 2014
25-60
Page 16
All
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
01 Jan 2016
Figure 25-602
Artex ELT 1000 Installation (Sheet 4 of 4)
2
12
10
9
6
7
CENTER CONSOLE
(REF)
LEGEND
1. Antenna Cable
2. RCPI Connecting Cable
3. ELT
4 ELT Antenna
6. Washer
7. Nut
8. Cable Tie
9. Remote Control
Panel Indicator (RCPI)
10. Screw
11. Buzzer
12. Label
13. Spacer
14. Cable Tie Mount
15. Clamp
16. Grommet
17. ELT Shelf
1
10
ELT MOUNTING
TRAY
(REF)
10
6
11
4
6
13
17
8
10
3
6
6
10
14
15
16
SR22_MM25_3670
Serials 22-4164 & subs, 22T-0954, 22T-0963 & subs
.
6
2
H
DETAIL
G
DETAIL
NOTE
Torque nut to 25 - 30 in-lb
(2.8 - 3.4 Nm).
1
1
7
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
25-60
Page 17
Serials 22-0002 thru 22-3827, Serials 22T-0001 thru
22T-0267 w/ ACK E-01 ELT
EFFECTIVITY:
D. Remote Control Panel Indicator (RCPI) - Serials 22-0002 thru 22-3827, Serials 22T-0001 thru 22T-
0267 w/ ACK E-01 ELT (See Figure 25-601)
(1) Removal - Remote Control Panel Indicator
(a) Remove aft screws securing circuit breaker panel to console. Open circuit breaker panel.
(b) Disconnect transmitter cable from RCPI.
(c) Remove screws, washers, and nuts securing RCPI to circuit breaker panel. Remove RCPI
from airplane.
(2) Installation - Remote Control Panel Indicator
(a) Position RCPI to circuit breaker panel and secure with screws, washers, and nuts.
(b) Connect transmitter cable to RCPI.
(c) Perform Operational Test - ELT. (Refer to 25-60)
(d) Position circuit breaker panel to console and secure with screws.
15 Dec 2014
25-60
Page 18
Serials 22-1863 thru 22-4163, 22T-0001 thru 22T-0953,
22T-0955 thru 22T-0962 w/ Artex ME406 ELT, 22-4164
& subs, 22T-0954, 22T-0963 & subs w/ Artex ELT 1000
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
15 Dec 2014
E. Remote Control Panel Indicator (RCPI) - Serials 22-1863 thru 22-4163, 22T-0001 thru 22T-0953,
22T-0955 thru 22T-0962 w/ Artex ME406 ELT, 22-4164 & subs, 22T-0954, 22T-0963 & subs w/
Artex ELT 1000 (See Figure 25-602)
(1) Removal - Remote Control Panel Indicator
(a) Serials w/o Perspective Avionics: Remove aft screws securing circuit breaker panel to
console. Open circuit breaker panel.
(b) Serials w/o Perspective Avionics: Remove cable tie securing RCPI ground wire to RCPI
connecting cable.
(c) Disconnect transmitter cable from RCPI.
(d) Serials w/o Perspective Avionics: Remove screws, washers, and nuts securing RCPI to
circuit breaker panel. Remove RCPI from airplane.
(e) Serials w/ Perspective Avionics: Remove screws, washers, and nuts securing RCPI to
center console. Remove RCPI from airplane.
(2) Installation - Remote Control Panel Indicator
(a) Serials w/o Perspective Avionics: Position RCPI to circuit breaker panel and secure with
screws, washers, and nuts.
(b) Serials w/ Perspective Avionics: Position RCPI to center console and secure with screws,
washers, and nuts.
(c) Connect transmitter cable to RCPI.
(d) Serials w/o Perspective Avionics: Install cable tie securing RCPI ground wire to RCPI con-
necting cable.
(e) Serials 22-1639 thru 22-4163, SR22T-0001 thru 22T-0953, 22T-0955 thru 22T-0962 w/
Artex ME406 ELT: Perform Operational Test - ELT. (Refer to 25-60)
(f) Serials 22-4164 & subs, 22T-0954, 22T-0963 & subs w/ Artex ELT 1000: Perform Opera-
tional Test - ELT. (Refer to 25-60)
(g) Serials w/o Perspective Avionics: Position circuit breaker panel to console and secure with
screws.
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
25-60
Page 19
Serials 22-0002 thru 22-3827, Serials 22T-0001 thru
22T-0267 w/ ACK E-01 ELT
EFFECTIVITY:
F. Remote Control Panel Indicator (RCPI) Battery - Serials 22-0002 thru 22-3827, Serials 22T-0001
thru 22T-0267 w/ ACK E-01 ELT
(1) Removal - Remote Control Panel Indicator Battery
(a) Remove RCPI. (Refer to 25-60)
(b) Remove screws securing upper and lower half of RCPI.
(c) Loosen nuts securing switches to RCPI.
(d) Remove top half of RCPI to access battery compartment.
(e) Remove battery from RCPI.
(2) Installation - Remote Control Panel Indicator Battery
(a) Acquire necessary tools, equipment, and supplies.
(b) Visually inspect battery contacts for dirt or corrosion. If necessary, clean contacts with
nonabrasive electrical contact cleaner and a stiff brush.
(c) Insert battery with polarity as shown on bottom of battery compartment.
(d) Position top half of RCPI to bottom half and secure with screws.
(e) Tighten nuts securing switches to RCPI.
(f) Record next battery replacement date on one of the adhesive labels supplied with the ELT.
Affix label to ELT in a readily visible location when installed. Record battery replacement
date in logbook.
(g) Install RCPI. (Refer to 25-60)
Description P/N or Spec. Supplier Purpose
6-Volt Battery Duracell PX28L
or
Kodak K28L
Any Source Provide power to
RCPI.
15 Dec 2014
25-60
Page 20
Serials 22-2084 thru 22-4163, 22T-0001 thru 22T-0953,
22T-0955 thru 22T-0962 w/ Artex ME406 ELT
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
15 Dec 2014
G. Remote Control Panel Indicator (RCPI) Battery - Serials 22-2084 thru 22-4163, 22T-0001 thru
22T-0953, 22T-0955 thru 22T-0962 w/ Artex ME406 ELT
(1) Removal - Remote Control Panel Indicator Battery
(a) Remove RCPI. (Refer to 25-60)
(b) Remove screws securing upper and lower half of RCPI.
(c) Loosen nuts securing switch to RCPI.
(d) Remove top half of RCPI to access battery compartment.
(e) Remove battery from RCPI.
(2) Installation - Remote Control Panel Indicator Battery
(a) Acquire necessary tools, equipment, and supplies.
(b) Visually inspect battery contacts for dirt or corrosion. If necessary, clean contacts with
nonabrasive electrical contact cleaner and a stiff brush.
(c) Insert battery with polarity as shown on bottom of battery compartment.
(d) Position top half of RCPI to bottom half and secure with screws.
(e) Tighten nuts securing switches to RCPI.
(f) Record next battery replacement date on one of the adhesive labels supplied with the ELT.
Affix label to ELT in a readily visible location when installed. Record battery replacement
date in logbook.
(g) Install RCPI. (Refer to 25-60)
Description P/N or Spec. Supplier Purpose
6-Volt Battery 131-0001 Artex Aircraft Supplies
Canby, Oregon 97013
800-547-8901
Provide power to
RCPI.
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Cirrus SR22T Maintenance Manual

Brand
Cirrus
Model
SR22T
Type
Maintenance Manual
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