STC SA01678SE

Supplemental type certificate · Steve's Aircraft

Holder
Steve's Aircraft · United States
Status
Current · Issued
Status date
June 8, 2006
Applied
October 12, 2003
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDS1A6

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

What it approves

Installation of a Lycoming O-360-A1P engine with a Hartzell HC-C2YK-1BF/F7666A propeller.

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 SA01678SE

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

White City, OR 98503

Part 3 of the Civil Air Regulations.

Original Product⎯Type Certificate Number: 1A6 Make: Piper Model: PA-22, PA22-135, PA22-150, PA22-160 Description of the Type Design Change: Installation of a Lycoming O-360-A1P engine with a Hartzell HC- C2YK-1BF/F7666A propeller in accordance with Steve’s Aircraft Document 3200-5-2, Revision 2, Installation Instructions, dated April 19th, 2006 and Steve’s Aircraft Document SP-3200-5, Revision 2, Master Drawing List (MDL), dated April 19th, 2006 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. Aircraft modified in accordance with this STC must be operated with a copy of the FAA approved Aircraft Flight Manual Supplement (AFMS), Document 3200-5-8, Rev IR, dated June 8th, 2006 or later FAA approved revision. A copy of this STC, the Instructions for Continued Airworthiness (ICA), Document 3200-5-1, Initial Revision (IR), dated July 25, 2004 and the AFMS, Document 3200-5-8, Rev IR, dated June 8th, 2006 or later FAA approved revision shall 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: October 12, 2003 Date reissued:

Date of issuance: June 8, 2006 Date amended:

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

Any alteration of this certifica te is pun ishable by a fin e of not exce eding $1,000, or imprisonment not exceeding 3 y ears, or both.

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 · 4

MakeModelData sheet
The New Piper Aircraft Inc.PA-221A6
The New Piper Aircraft Inc.PA-22-1351A6
The New Piper Aircraft Inc.PA-22-1501A6
The New Piper Aircraft Inc.PA-22-1601A6