STC SA00851SE

Supplemental type certificate · Steve's Aircraft

Holder
Steve's Aircraft · United States
Status
Current · Issued
Status date
November 10, 2000
Applied
September 12, 2000
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
Data sheets
TCDS1A4TCDS1A6

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of Rudder Trim System.

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 SA00851SE This certificate, issued to Steve's Aircraft 15373 Jones Rd.

White City, OR 97503 Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: 1A4 and 1A6 Make: Piper Model: PA-20, PA-20S, PA-20 "115", PA-20S "115", PA-20 "135", PA-20S "135", PA-22, PA-22-108, PA-22-135, PA-22S-135, PA-22-150, PA-22S-150, PA-22-160, and PA-22S-160

Description of the Type Design Change: Installation of Rudder Trim System in accordance with Steve's Aircraft Installation and Drawing Number SP-3200~2, Initial Release, dated October 12, 2000, or later FAA approved revision.

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 on which other previously approved modifications are incorporated unless it is determined 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. This modification has been found compatible with tail wheel conversions to PA-22 series aircraft. A copy of this Certificate, along with a copy of the Instructions for Continued Airworthiness, dated October 12, 2000, and Steve's Aircraft Flight Manual Supplement, dated November 10, 2000, or later FAA approved revisions, 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.

This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: September 12, 2000 Date reissued:

Date of issuance: November 10, 2000 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 · 11

MakeModelData sheet
The New Piper Aircraft Inc.PA-201A4
The New Piper Aircraft Inc.PA-20-\"115\"1A4
The New Piper Aircraft Inc.PA-20S1A4
The New Piper Aircraft Inc.PA-221A6
The New Piper Aircraft Inc.PA-22 Series1A6
The New Piper Aircraft Inc.PA-22-1081A6
The New Piper Aircraft Inc.PA-22-1351A6
The New Piper Aircraft Inc.PA-22-1501A6
The New Piper Aircraft Inc.PA-22-1601A6
The New Piper Aircraft Inc.PA-22S-1501A6
The New Piper Aircraft Inc.PA-22S-1601A6