P/N 13772-152 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
Original Issue: 02-01-13
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