What it approves
Installation of cabin door loop manufactured
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Number SA00793SE
This certificate, issued to: Paul M. Sterling 13113 SE 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 the Type Design Change: Installation of cabin door loop manufactured in accordance with Paul Sterling Drawing SA10400, Revision B, dated March 9, 2000, and installed in accordance with Paul Sterling Drawing SA11400, Revision N/C, dated January 3, 2000, or later FAA-approved revision.
Limitations and Conditions: Approval of this change in type design applies to to the above model aircraft only.
This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those 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.
If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
Date of application: July 12, 1999 Date reissued: Xxxxxxx ##, #### Date of issuance: April 18, 2000 Date amended: March 17, 2010
(Signature) 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 |
|---|---|---|
| Piper Aircraft Inc. | PA-38-112 | A18SO |