STC SA02867NY

This certificate issued to

Part 23 of the Federal Aviation Regulations.

Installation of the Lord Corporation Nose Wheel Shimmy Damper Part Number SE-1088-1 in accordance with Lord Corporation Installation Drawing List Document No. SE-1088-IDL, Revision IR, dated 4/22/2008 or later FAA approved revisions.

1. Maintenance must be in accordance with Instructions for Continued Airworthiness (ICA) for Lord Se-1088-1 Shimmy Damper installed on Cessna 177 Aircraft Models, Lord Bulletin No. SM-6526, Revision A, dated 2/19/2009 or later FAA accepted revisions.

2. The installer must determine whether this design change is compatible with previously approved modifications.

3. 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.

LORD Corporation 2000 West Grandview Blvd Errie, PA 16514-0039 A13CE Make: Cessna Aircraft Company Model: 177, 177A, and 177B Date of application: March 11, 2007

Date of issuance: December 21, 2010 Date reissued:

( Signature) Anthony Socias Manager New York Aircraft Certification Office

( Title)

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

Number SA02867NY

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, for non-significant changes to type design, the certification basis elected by the STC holder for the modification to the Cessna 177 series aircraft modified by this change is as follows:

a. The type certification basis for Cessna 177 series airplanes is shown on TCDS A13CE for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, March 11, 2007, is based upon part 23 as amended by Amendment 23-55. Based on 14 CFR §§ 21.115 and

21.101, and the FAA policy for non-significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be as shown in the TCDS A13CE except the regulations listed below:

Section Title Amendment §23.233 Directional Stab ility and Control 23-50 §23.301 Loads 23-48 §23.305 Strength and Deformation 23-45 §23.603 Materials and Workmanship 23-23 §23.605 Fabrication Methods 23-23 §23.607 Fasteners 23-48 §23.611 Accessibility [Provisions] 23-48 §23.613 Material Strength Properties and Material Design Values 23-45 §23.1301 Function and Installation 23-49 §23.1309 Equipment, Systems, and Installations 23-49 §25.1529 Instructions for Continued Airworthiness 23-26

---END---