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applicable, is installed in the handbook and the supplement is properly
recorded on the Log of Supplements page.
FAA Approved POH Supplements must be in the airplane for flight
operations when the subject optional equipment is installed or the
special operations are to be performed.
• Note •
This Log of Supplements shows all Cirrus Design
Supplements available for the aircraft at the corresponding
date of the revision level shown in the lower left corner. A mark
(x) in the Part Number column indicates that the supplement is
installed in the POH.
March 2010
9-2 Information Manual
Section 9 Cirrus Design
Supplements SR22
March 2010
Intentionally Left Blank
Information Manual 9-3
Cirrus Design Section 9
SR22 Log of Supplements
Section 9
Log of Supplements
Part Number Title Date
___ 13772-114 SR22 Airplanes Registered in Canada 06-05-02
___ 13772-115 R7 Basic Ice Protection System 05-13-08
___ 13772-119 SR22 Airplanes Registered in Israel 12-03-03
___ 13772-122 SR22 Airplanes Registered in the European Union 04-12-06
___ 13772-129 R2 Hartzell Compact Series Propeller w/ Composite Blades 08-26-09
___ 13772-131 R1 Artex ME406 406 MHz ELT System 05-13-08
___ 13772-134 R2 TKS Anti-Ice System 11-17-09
___ 13772-135 R1 GFC 700 Automatic Flight Control System 08-26-09
___ 13772-136 Garmin Terrain Awareness/Warning System 05-13-08
___ 13772-138 Enhanced Vision System 07-29-08
___ 13772-140 S-Tec Fifty Five X Autopilot w/ Optional Flight Director 12-18-08
___ 13772-141 S-Tec Fifty Five SR Autopilot 12-18-08
___ 13772-143 R1 Part 135 Operation - Electrical Loading Shedding 03-26-09
___ 13772-145 SR22 Airplanes Registered in Argentina 09-30-09
March 2010
9-4 Information Manual
Section 9 Cirrus Design
Log of Supplements SR22
March 2010
FAA Approved POH Supplements must be in the airplane for flight operations when the
subject optional equipment is installed or the special operations are to be performed.
This Log of Supplements shows all Cirrus Design Supplements available for the aircraft
at the corresponding date of the revision level shown in the lower left corner. A mark (x)
in the Part Number column indicates that the supplement is installed in the POH.
P/N 13772-129 1 of 8
Cirrus Design Section 9
SR22 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Hartzell Compact Series Propeller
w/ Composite Blades
When Hartzell Propeller Model Number PHC-J3YF-1N/N7605(B) or
PHC-J3Y1F-1N/N7605(B) 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.
• Note •
This POH Supplement Change, dated Revision 02: 08-26-09,
supersedes and replaces the Revision 01 release of this POH
Supplement dated Oct 23, 2008.
Revision 02: 08-26-09
2 of 8 P/N 13772-129
Section 9 Cirrus Design
Supplements SR22
Section 1 - General
For additional information on Hartzell Compact Series Propeller with
Composite Blades refer to Hartzell Propeller Owner’s Manual, p/n 145,
revision 1 or later.
Section 2 - Limitations
Power Plant Limitations
Hartzell Compact Series Propeller with Composite Blades
Propeller Type........................................ Constant Speed, Three Blade
Model Number ................................................PHC-J3YF-1N/N7605(B)
Diameter ........................................................................................78.0"
Hartzell Compact Series Lightweight Hub Propeller with
Composite Blades
Propeller Type........................................ Constant Speed, Three Blade
Model Number ..............................................PHC-J3Y1F-1N/N7605(B)
Diameter ........................................................................................78.0"
Section 3 - Emergency Procedures
Glide performance on aircraft with the subject propeller installed is
slightly reduced. Refer to the following table.
Revision 02: 08-26-09
P/N 13772-129 3 of 8
Cirrus Design Section 9
SR22 Supplements
Maximum Glide
Best Glide Speed
3400 lb 88 KIAS
Maximum Glide Ratio ~ 8.5 : 1
Conditions Example:
Power OFF Altitude 10,000 ft. AGL
Propeller Windmilling Airspeed Best Glide
　
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