# STC SA2786CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation of fuselage shell upholstery panels, window shade assemblies, cabinets, table, and seat upholstery
- Applied: September 17, 1991
- Status date: January 23, 2017
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A60EU](https://openairdocs.org/tcds/A60EU)
- Certificate PDF: https://openairdocs.org/files/sha256/de/08/de08bcd9785212601dba7bd6f3886144109ae59d5617ed85294d93d749ae6573
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/ECA4ED02A3A10E32862580B40069BB83.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2786CE

## ADs that name it (1)

- [AD 98-08-27](https://openairdocs.org/ad/98-08-27): Left-Hand Wheel Assembly · SOCATA TBM 700 with STC SA2786CE. Effective May 31, 1998. Named in the applicability

## Approved models (1)

- SOCATA TBM 700 ([TCDS A60EU](https://openairdocs.org/tcds/A60EU))

## 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.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title 1987, plus amendments listed in the Type Certificate Data Sheet.

SA2786CE Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 23 Federal Aviation Regulations effective January 15, A60EU Socata, Groupe Aerospatiale TBM700 (S/N 1 and after) 2 Installation of Fuselage Shell Upholstery Panels, Window Shade Assemblies, Cabinets, Table, and Seat Upholstery per Precision Pattern Drawing List Number 12220, stamped FAA Approved and dated January 10, 1992, or later FAA approved revision.

This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of those airplanes.

January 31, 2015, January 23, 2017 November 10, 1993 September 17, 1991 January 10, 1992 Grant E. Youngdahl Program Manager Wichita Aircraft Certification Office

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

2 SA2786CE

## Every issue (2)

- January 23, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/de/08/de08bcd9785212601dba7bd6f3886144109ae59d5617ed85294d93d749ae6573)
- January 31, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/32/86/32864227a218efc9a52524affbc963477aae194ea2387dc0ca8454b8ae777ab9)

---
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.