# STC SA1065NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Heath Tecna Inc., United States
- Description: Installation of new cabin interior components consisting of overhead enclosed storage compartments, flush passenger service units, ceilings, sidewalls, & fluorescent lighting system.
- Applied: February 10, 1979
- Status date: February 17, 2005
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/f0/09/f0093c38c4021bdbc1efcf71a0162084d7e9c9c78391b4c37d3b435a24b6f19d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B1E1DDB3F108851786257A1400660022.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1065NM

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 727-100 Series ([TCDS A3WE](https://openairdocs.org/tcds/A3WE))

## 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.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA1065NM

This certificate, issued to: Heath Tecna Inc.

3225 Woburn Street Bellingham, WA 98226

Part 4b of the Civil Air Regulations.

Original ProductType Certificate Number: A3WE Make: Boeing Model: 727-100 series

Description of the Type Design Change: Installation of new cabin interior components consisting of overhead enclosed storage compartments, flush passenger service units, ceilings, sidewalls, and fluorescent lighting system in accordance with HITCO Drawing List 9200004DL, Revision D, dated July 17, 1980, 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 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 previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. The resulting interior arrangement, along with the required placarding, has not been evaluated and is not part of this STC. A copy of this Certificate must 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: February 10, 1979 Date reissued: 11/16/91; 2/10/92; 10/28/94;

6/1/96; 7/20/00; 2/17/05 Date of issuance: January 26, 1981 Date amended:

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

## Every issue (1)

- February 17, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f0/09/f0093c38c4021bdbc1efcf71a0162084d7e9c9c78391b4c37d3b435a24b6f19d)

---
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.
