STC SA1182NW

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA1182NW This certificate issued to: Full hart Insurance Agency, InC.

Part 3 of the CIVil Air Regulations, November 1, 1949 and amendments 3-1 through 3-12.

Original Product - Type Certificate Number: 1A15 Make: Piper Model: PA-24 Agency, Inc. photographs 1 through 2. Propeller on a Lycoming 0-360-A1D engine in accordance with Fullhart Insurance Description of Type Design Change: Installation of a Hartzell HC-C2YK- 1BF/F7666A-2 inadequate for duplication in other aircraft. Limitations and Conditions: Data pertaining to this modification are considered installation in Piper PA-24, Serial Number 24-39 only. A copy of this Certi- This approval is limited to the ficate, Addendum No. SA1182NW, and FAA Approved Airplane Flight Manual Supplement shall be maintained as part of the permanent records for the modified aircraft.

rendered, suspended, revked, or a termination date is therevise established by the Oldministrator of the Date of Application: November 21, 1980 Date Reissued:

Date of Issuance: February 18, 1981 Date Amended:

FEDERAI AVIATION Chance Chroeder TOMINISTRANIOT ( Signature ) Acting Chief, Seattle Area Aircraft Certification Office (Title) FAA FORM 8110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) February 18, 1981 Number SA1182NW Supplemental Type Certificate ADDENDUM NO, SA1182NW The conditions and limitations of Type Certificate Data Sheet Number 1A15 apply except where superseded by the following:

Supplemental Type Certificate Data Sheet, which is part of STC SA1182NW, prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Civil Air Regulations.

Supplemental Type Certificate HOLDER: Fullhart Insurance Agency, Inc.

PIPER PA-24 (LANDPLANE-NORMAL CATEGORY) AS MODIFIED BY STC SA1182NW Engine: Lycoming 0-360-A1D Engine Limits: 180 Нр @ 2700 грт Fuel: 91/96 or 100/130 minimum grade aviation gasoline Propeller and Propeller Limits: Hartzell HC-C2YK-1BF/F7666A-2 Diameter: Maximum 76"; Minimum 72" 180 Hp @ 2900 rpm Placards: AVOID CONTINUOUS OPERATION BETWEEN 2000 and 2250 RPM Serial Number Eligible: 24-39 only.

- END -

FAA FORM B110-2-1 (10-69) PAGE 3 OF 3 PAGES FAA AC 73-2651