# STC SA2438NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Heath Tecna Inc., United States
- Description: Installation of new cabin interior components consisting of overhead storage compartments, ceiling sidewall and lighting system.
- Applied: May 9, 1984
- Status date: February 17, 2005
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A5EU](https://openairdocs.org/tcds/A5EU)
- Certificate PDF: https://openairdocs.org/files/sha256/ac/1e/ac1ef890459e1335872facdb7b99fdf2d0b56b2dac9b61c7657cbeb2fb6a50c1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D79F51A575845A7F862579D600784591.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2438NM

## ADs that name it (0)

None.

## Approved models (2)

- British Aerospace Airbus Limited 1-11 200 Series ([TCDS A5EU](https://openairdocs.org/tcds/A5EU))
- British Aerospace Airbus Limited 1-11 400 Series ([TCDS A5EU](https://openairdocs.org/tcds/A5EU))

## 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 SA2438NM

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: A5EU Make: British Aerospace Model: BAC-1-11-400, BAC-1-11-200 series

Description of the Type Design Change: Installation of new cabin interior components, consisting of overhead storage compartments, ceiling sidewall and lighting system, in accordance with HITCO Drawing List 9100000DL, Revision U, dated September 24, 1984, 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 these models 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. 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: May 9, 1984 Date reissued: 9/28/90; 10/28/94; 6/1/96;

7/20/00; 2/17/05

Date of issuance: September 27, 1984 Date amended: 5/21/85

(Signature) Acting Manager, Seattle Aircraft C ertification Office (Title)

## Every issue (1)

- February 17, 2005: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ac/1e/ac1ef890459e1335872facdb7b99fdf2d0b56b2dac9b61c7657cbeb2fb6a50c1)

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