What it approves
Installation of steel nose landing gear link.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00410SE This certificate issued to: Paul M. Sterling 13113 S.E. 228th Place Kent, WA 98031 Part 23 of the Federal Aviation Regulations.
Original Product -Type Certificate Number A18SO Make: Piper Model: PA-38-112 Description of Type Design Change: Installation of steel nose landing gear link, manufactured in accordance with Paul Sterling Drawings SA10100, SA10101, SA10102, SA10103, and SA10104, original release, all dated January 13, 1997, or later FAA approved revisions.
Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.
This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.
Date of Application: August 21, 1995 Date Reissued:
Date of Issuance: February 7, 1997 Date Amended:
FEDERAL AVIATION By Direction of the Administrator drea но - (Signature) HOMINIST RATION Acting Manager, Seattle Aircraft Certification Office (Title)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| The New Piper Aircraft Inc. | PA-38-112 | A18SO |