STC SA01577SE

Supplemental type certificate · Adams Stephen

Holder
Adams Stephen · United States
Status
Current · Issued
Status date
July 14, 2005
Applied
February 15, 2005
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
Data sheet
TCDS1A6

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval for change in type design is limited to Piper Model PA-22-150, serial number 22-5243 only.

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.

United States of America Department of Transportation _ Federal Aviation Administration Supplemental Type Certificate Number SA01577SE

This certificate, issued to Stephen Adams 5608 Center Rd.

Lopez Island, WA 98261 Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: 1A6 Make: Piper Model: PA-22-150

Description of the Type Design Change : Replacement of the Piper PA-22 series aileron/elevator control yoke assembly with a Piper PA-16 series control stick assembly.

Limitations and Conditions: Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval for change in type design is limited to Piper Model PA-22-150, serial number 22- 5243 only. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

Date of application: February 15, 2005 Date reissued:

Date of issuance: July 14, 2005 Date amended:

(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.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
The New Piper Aircraft Inc.PA-22-1501A6