STC SA1437NM

Supplemental type certificate · Plane Plastic, Ltd

Holder
Plane Plastic, Ltd · United States
Status
Current · Reissued
Status date
December 3, 1996
Applied
July 14, 1981
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDS2A13

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

What it approves

Installation of a rear cabin shelf and closeout panel.

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 NumberSA1437NM This certificate issued to:

Plane Plastic, Ltd.

612 Murray Drive Alva, OK 73717 Purt 3 of the Civil Ait Foegulations Original Product Type Certificate Number: 2A13 Abako : Piper Model: PA-28 -140 Description of Type Design Change: Installation of a rear cabin shelf and closeout panel in accordance with Pegasus Northwest, Inc. Installation Instructions No. PNW 140-001-5 and Drawing No. PNW 140-001 (Sheet 1), 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 aircraft of this model 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. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.

Date of Application: July 14, 1981 Date Reissued: February 07, 1989 December 03, 1996 Date of Issuance: . December 10, 1981 Date Amended:

FEDERAL AVIATION By dived fion oAthe Administrator Paul C. Sconyers TOMINISTRATOR Associate Manager, ACE-117A Atlanta Aircraft Certification Office (Title) 000, or imprisonment not exceeding 3 years, or both.

FAR FORM 8110-2110-681 PAGE 1 of 2 PAGES

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1437NMs This certificate issued to: Oxford Design Group Purt 3 othe Civil Air Regulalions.s Amendments 3-1, 3-2 and 3-4.

Original Product -Type bentificate Number: 2A13 Make: Piper Model: PA-28-140 Description of Type Design Change: Installation of a rear cabin shelf and closeout pane n accordance with Pegasus Northwest, Inc. Installation Instructions No. PNW 140-001- and Drawing No. PNW 140-001 (sheet 1), or later FAA approved revision.

By HCE-II1A Deto 2-22-91 Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft of this model 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. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

Date of Application: July 14, 1981 Jule missued: February 7, 1989 Date of Issuance: December 10, 1981 Date Amended:

FEDERAL AVIATION By Direction of the Administrator

7.7 Reappr PMINISTRAIO Acting Manager, Seattle Aircraft Certification Office (Title) 47 FAA FoRM 8110-2 (10-68)

Department Cransportation -federal Abiation Ad stration Supplemental Type Certificate Number: SA1437NM This certificate issued to: Pegasus Northwest, Inc.

Part 3 efthe CIVi| Air Regulations, Amendments 3-1, 3-2, and 3-4.

Original Product -Type bentificate Numben: 2A13 Make: Piper Model: PA-28-140 Desoritions Jype Design bhange: Installation of a rear cabin shelf and closeout panel in accordance with Pegasus Northwest, Inc. Installation Instructions No. PNW 140-001-5 and Drawing No. PNW 140-001 (Sheet 1).

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft of this model 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. A copy of this Certificate shall be maintained as part of the permanent records for the modified aircraft.

Date of Application: JUly 14, 1981 Date Reissued:

Date of Issuance: December 10, 1981 Date Amended:

FEDERAL AVIATION By Direction of the Administrator ( Signature ) HOMINISTE Chief, Seattle Area Aircraft Certification Office (Title)

Memorandum U.S. Department of Transportation Federal Aviation Administration Subject: Supplemental Type Certificate (STC) SA1437NM INFORMATION: Transfer and Reissue of Make: FEB 2 7 1997 Reply to From: Associate Manager, Atlanta Aircraft Certification Attn of Office, ACE-117A To: Manager, Special Certification Office ASW-190 The subject STC has been transferred to a holder in your geographical area:

Rotorcraft Directorate Special Certification Office ASW-190 2601 Meacham Blvd.

Fort Worth, TX 76137-4298 Attached is the STC data package including the correspondence, drawings, reports, and other data pertaining to this STC.

austenger Attachment

Small Airplane Directorate U.S. Department of Transportation Atlanta Aircraft Certification Office Federal Aviation Campus Building Administration 1701 Columbia Avenue, Suite 2-160 College Park, Georgia 30349 FEB 2 7 1997 Mr. Paul Kinzie P.O. Box 847 Alva, OK 73717 Dear Mr. Kinzie:

Please find enclosed Supplemental Type Certificate (STC) SA1437NM which is transferred to Plane Plastics, LTD., from Oxford Design Group, Inc. Our Special Certification Office (ASW-

190) is in possession of the FAA files associated with your STC. Any questions, design changes, or requests for information on this STC should be directed to the Special Certification Office at:

Federal Aviation Administration Rotorcraft Directorate Special Certification Office (ASW-190) 2601 Meacham Blvd.

Fort Worth, TX 76137-4298 Phone (817) 222-5190 Your responsibilities as an STC holder are defined in Federal Aviation Regulations 14 CFR part 21, Certification Procedures for Products and Parts. These responsibilities include the requirement that you maintain, in your possession, the technical data which substantiated the approval.

Sincerely, можа Roger D. Anderson Manager, Atlanta Aircraft Certification Office Enclosure

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
Piper Aircraft Inc.PA-28-1402A13