STC SA00283BO

Number SA00283BO

Part 3 of the Civil Air Regulations.

Installation of Lycoming O-320-A, -A1B, -A2A, -A2B, -A2C, -C1A, -C1B, -C2A or –C2B engine and Sensenich 74DM6 propeller in accordance with Cedric M. Abbott Report 08-20/1, Instructions for Continued Airworthiness, rev. A, dated August 28, 2008, or later FAA- approved revisions.

1. Cedric M. Abbott Flight Manual Supplement for Piper PA-16, dated February 23, 2009, or later FAA-approved revisions, is required and must be carried in the aircraft during all flights.

2. This installation is to be maintained in accordance with Cedric Abbott Report 08-20/1 Instructions for Continued Airworthiness, rev. A, dated August 28, 2008, or later FAA-approved revisions.

3. Compatibility of this design with previously approved modifications must be determined by the installer.

If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Cedric M. Abbott 66 Gesner Rd.

Buckfield, ME 04220 This certificate issued to Original Product - Type Certificate Number: 1A1 Piper Make:

Model: PA-16

( Signature) Robert G. Mann Manager Boston Aircraft Certification Office

( Title)

Date of application : December 23, 2007

Date of issuance : February 27, 2009

FAA Form 8110-2-1(10-69) Page 3 of 3

Number SA00283BO

This STC amends TCDS 1A1 as follows:

Engine: Lycoming O-320-A1A, -A1B, -A2A, -A2B, -A2C, -C1A, -C1B, -C2A or -C2B

Propeller and Propeller Accessories

Propeller – Sensenich 74DM6 Static r.p.m. at max. permissible throttle setting:

Not over 2450, not under 2250 No additional tolerance permitted Diameter: Not over 74 inches, not under 72 inches

End