# STC SA280SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Tulsa Airmotive, Inc, United States
- Description: Installation of Piper forward fuselage section and long nose 30542-02.
- Applied: August 5, 1963
- Status date: September 21, 1963
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 1A10](https://openairdocs.org/tcds/1A10)
- Certificate PDF: https://openairdocs.org/files/sha256/c9/9b/c99bd6a5466ec53ab644888d3d07920bf5c2a904bb0f44b6078a3ccb28cf8759
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F052476CC61BCECA86257D9A00778907.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA280SW

## ADs that name it (0)

None.

## Approved models (1)

- Piper Aircraft Inc. PA-23-250 ([TCDS 1A10](https://openairdocs.org/tcds/1A10))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

**FEDERAL AVIATION AGENCY**

**SUPPLEMENTAL TYPE CERTIFICATE FORM APPROVED, BUDGET BUREAU NO. M-R01S**

**INSTRUCTIONS - SUBMIT IN TRI PLICATE TO LOCAL FAA FLIGHT STANDARDS INSPECTOR.**

COPY WILL BE flETURNED TO APPLICANT UPON

**ISSUANCE**

1. NAME AND ADDRESS OF APPLICANT Xulaa Ainootlve, Inc.

P. 0. Bo* i7t> Brcten Arrow, Oklahoma

2. SUPPLEMENTAL TYPE CERTIFICATE APPLIED FOR:

AlRCRAFT ENGINE PROPELLER

ORIGINAL MODEL DESIGNATION Piper PA*23-250 NEW MODEL DESIGNATION (If dmmlrid) DESCRIPTION OF CHANGE Installation of Piper forward fuselage section and Piper long OOU p/N 30542-02 in accordance ultb drawings 1700 (2 sheets) dated 7/23/63, 1701 dated 9/19/63 (five plice) or 1704 uateti S/W/W (flvt place), Tula* Alriaotive fioglneering Report ST-filOl, end Piper Report 1036, revieed by Tulaa Mraotivc tor weigbe and bai«oc«.

1. FAA Approve Airplane Flight Mrtttial Supplcucnt dated 3/l9A'3 required.

2. Tld.8 MDOificatloa is eligible on tiper PA-23-2SO, PA-2>250 (6 place) and PA-23-25O aircraft Mdifted per STC'a SA2-1172 and 3A162SW.

3. The weight and balance end loading ocnedule per Tulaa Almotive Kapert Vo.

1006 la to be added to each airplane modified by thia SIC and a 1702 plotter

•fright and Balance ia to be furnished with the airplane for the 6 place configuration ami a 1701 plotter weight & balance ia to be furnished with the 2 place configuration.

»*. WILL DATA 6E AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS? C2 YES

b. WILL PARTS BE MANUFACTURED FOR SALE (Saf. CAS l.S5)1 t— ] YES NO NO

**5. SIGNATURE AND TITLE OF APPLICANT**

**SIGNATURE**

5. 1963

**DATE OF APPLICATION TITLE**

6. To fee Completed by FAA

NATURE AND LOCATION OF DATA Data lleted in item three above, Piper Reports 1036 and 1204, and DUL tf. Fred Stewart'a fAA-1600 feted 8/15/63 ou file at SU-210.

Reference £ reject A377SW-4.1.

Applicable xegulaciona MM «• original certilication.

**ORIGINAL TYPC CERTIFICATE NO.**

1A10 -•••"PLEMENTAL TYPE CERTIFICATE NO.

SA2808W

**DATE OF APPROVAL 9/21/63**

**FAA APPROVAL H.**

SI MATURE Slaughter Bnginearlng and Manufact'oring Branch Tl TLE AC eZ-4Z07 FORM FAA-Z417 (5-59)

## Every issue (1)

- September 21, 1963: Issued, Current. [certificate](https://openairdocs.org/files/sha256/c9/9b/c99bd6a5466ec53ab644888d3d07920bf5c2a904bb0f44b6078a3ccb28cf8759)

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