# STC SH4036NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Dart Aerospace USA Inc., United States
- Description: Installation of door actuators.
- Applied: September 21, 1988
- Status date: August 22, 2023
- Product: Aircraft, Rotorcraft
- Data sheets: [TCDS 4H12](https://openairdocs.org/tcds/4H12)
- Certificate PDF: https://openairdocs.org/files/sha256/d5/71/d571aa951bceb2f456ff7426ca182f337fff0e0c53a0276e7f47ddd5c908236d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113076433120231006154954.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SH4036NM

## ADs that name it (0)

None.

## Approved models (5)

- Schweizer Aircraft Corporation 269A ([TCDS 4H12](https://openairdocs.org/tcds/4H12))
- Schweizer Aircraft Corporation 269A-1 ([TCDS 4H12](https://openairdocs.org/tcds/4H12))
- Schweizer Aircraft Corporation 269B ([TCDS 4H12](https://openairdocs.org/tcds/4H12))
- Schweizer Aircraft Corporation 269C ([TCDS 4H12](https://openairdocs.org/tcds/4H12))
- Schweizer Aircraft Corporation 269C-1 ([TCDS 4H12](https://openairdocs.org/tcds/4H12))

## 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 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 1 of 2 SH4036NM Dart Aerospace USA, Inc 3845 NE 30th Avenue Hillsboro, OR 97124 Part 6 the Civil Air Regulations 4H12 Schweizer Aircraft Corporation 269A, 269A-1, 269B, 269C, 269C-1 Installation of door actuators in accordance with FAA approved drawing list 269DA-100DL, dated October 6, 1988, FAA approved October 25, 1988, or subsequent FAA approved revision.

September 21, 1988 August 22, 2023 November 4, 1988 October 6, 1995 for Manager, West Certification Branch

1. The following placard must be displayed on each actuator:

"REMOVE WHEN DOOR IS REMOVED."

2. This approval should not be extended to aircraft of this model on which other previously approved modifications as incorporated unless, it is determined that the interrelationship between this change and any those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

3. 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.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 2 of 2 SH4036NM

## Every issue (2)

- August 22, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d5/71/d571aa951bceb2f456ff7426ca182f337fff0e0c53a0276e7f47ddd5c908236d)
- October 6, 1995: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/01/dc/01dc670186227d5b69604a995ade7d15f4e4ecf21e6be8b89378542732146220)

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