# STC SA1288NW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: James D Woodward, United States
- Description: Increase in gross weight to 3890 pounds
- Applied: July 7, 1981
- Status date: August 7, 1981
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS ATC 444](https://openairdocs.org/tcds/ATC%20444)
- Certificate PDF: https://openairdocs.org/files/sha256/fc/b4/fcb48b5280befc507c314c6ca5360ad0bc0ff6a2027e855433d82196d44eaaed
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/33364AD451BDB59B86257A3A006467C7.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1288NW

## ADs that name it (0)

None.

## Approved models (1)

- Curtiss-Wright Corporation Sedan 15-D ([TCDS ATC 444](https://openairdocs.org/tcds/ATC%20444))

## What the certificate says

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 Sunder SA1288NK This certificute, cued le James D. WOOdwara Purt * ef the * Kuyululu. *Aeronautical Bulletin 7A.

Priginal Paul- Type furifink. lunder: ATC-444 (Converted From ATC-425) Make: Curtiss-Wright Model: 15D (Converted from 15C) Lescriplion fLype Design thunge: Increase in gross weight to 3890 pounds in accordance with Issaquah Parachute Center Report IPC-100, dated June 5, 1981, relocation of the battery to fuselage station 115 inches, installation of 50 pounds of permanent ballast at fuselage station 233 inches, and removal of cabin doors for the purpose of sport parachuting in accordance with Operating Limitations dated August 7, 1981.

Limilulunandfunditin: Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Curtiss-Wright 15D (converted), Serial Number 15C-2001 only. A copy of this Certificate and Operating Limitations dated August 7, 1981, shall be maintained as part of the permanent records for the modified aircraft. NOTE: When the aircraft is operating at weights above 3360 pounds, the VNE is restricted to 115 mph IAS.

I ate of repeplication. July 7, 1981 Jute missued:

Date of Issuance: . August 7, 1981 I ate unended FEDERAL EVIATION By dinstion of thy thinistrater (Dignature TOHINISTELIO Chiet, Seattle Area Aircraft Certification Office « Title i

47.

**FAA FORM 8110-2 110-68)**

## Every issue (1)

- August 7, 1981: Issued, Current. [certificate](https://openairdocs.org/files/sha256/fc/b4/fcb48b5280befc507c314c6ca5360ad0bc0ff6a2027e855433d82196d44eaaed)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.