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Revision 02: 08-26-09
P/N 13772-129 7 of 8
Cirrus Design Section 9
SR22 Supplements
Section 6 - Weight & Balance
Installation of the subject propeller adds the following optional (Sym =
O) equipment at the weight and arm shown in the following table.
Section 7 - Systems Description
The airplane employs a 3 blade, constant speed, non-feathering
propeller. The composite blades are mounted in an aluminum hub
which contains the pitch changing mechanism consisting of a piston/
cylinder, piston rod, and blade actuating components. Refer to the
basic POH for additional information on the propeller system.
ATA /
Item Description Sym Part Number Unit
Wt Arm
61-01 Propeller Installation without Ice
Protection
O 13599-007 67.2 48.0
61-02 Propeller Installation with
Ice Protection
O 15319-00x 68.0 48.0
61-03 Lightweight Hub Propeller
Installation without Ice Protection
O 13599-010 62.4 48.0
61-04 Lightweight Hub Propeller
Installation with Ice Protection
O 15319-013 63.2 48.0
Revision 02: 08-26-09
8 of 8 P/N 13772-129
Section 9 Cirrus Design
Supplements SR22
Section 8 - Handling, Servicing & Maintenance
Propeller Servicing
The spinner and backing plate should be cleaned and inspected for
cracks frequently. Before each flight the propeller should be inspected
for nicks, scratches, and gouges. If found, they should be repaired as
soon as possible by a rated mechanic, since a nick or scratch causes
an area of increased stress which can lead to serious cracks or the
loss of a propeller tip.
Propeller blades are painted with a durable specialized coating that is
resistant to abrasion. If this coating becomes eroded, it is necessary to
repaint the blades to provide proper erosion protection. Painting
should be performed by an authorized propeller repair station.
It is permissible to perform a blade touch-up with aerosol paint in
accordance with Hartzell Propeller Owner’s Manual, p/n 145, revision
1 or later.
Section 10 - Safety Information
No Change.
Revision 02: 08-26-09
13772-131 1 of 8
Cirrus Design Section 9
SR22 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Artex ME406 406 MHz ELT System
When Artex ME406 406 MHz ELT System is installed in the Cirrus
Design SR22, this POH Supplement is applicable and must be
inserted in the Supplements Section (Section 9) of the Cirrus Design
SR22 Pilot’s Operating Handbook. This document must be carried in
the airplane at all times. Information in this supplement adds to,
supersedes, or deletes information in the basic SR22 Pilot’s Operating
Handbook.
This POH Supplement Change, dated Revision 01: 05-13-08,
supersedes and replaces the Original release of this POH
Supplement dated 08-15-07.
Revision 01: 05-13-08
2 of 8 13772-131
Section 9 Cirrus Design
Supplements SR22
Section 1 - General
The 406 MHz emergency locator transmitter (ELT) is a radio-frequency
transmitter that generates a signal to assist in search and rescue for
missing aircraft. The ELT automatically transmits the standard sweep
tone on 121.5 MHz if rapid deceleration is detected. In addition, for the
first 24 hours of operation, a 406 MHz signal containing aircraft
specific information is transmitted at 50 seconds for 440 milliseconds.
8
CIRCUIT
BREAKER
PANEL
OR
ALT AIR
BRACKET
(REF)
4
MOUNTING
TRAY (REF)
SR22_FM09_2677A
LEGEND
1. LED Annunciator
2. Remote Switch
3. Antenna
4 Remote Cable
5. Main Control Switch
6. Antenna Jack
7. Attach Straps
8. Artex ME406 ELT
1
2
3
7
6
1
5
WARNING FORWARD
Artex ME406 ELT System
Revision 01: 05-13-08
Figure - 1
13772-131 3 of 8
Cirrus Design Section 9
SR22 Supplements
Section 2 - Limitations
No Change.
Section 3 - Emergency Procedures
Forced Landing
Before performing a forced landing activate the ELT transmitter
manually by turning the ELT remote switch to the 'ON'-position.
Immediately after a forced landing, perform the following procedure:
• Note •
The ELT Remote Switch and Control Panel Indicator could be
inoperative in the event of a forced landing. If inoperative, the
inertia “G” switch will activate automatically. However, to turn
the ELT OFF and ON will require manual switching of the main
control switch located on the ELT unit.
　
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