# STC SA1810WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aztec Nomad Inc., Canada
- Description: Installation of left-hand passenger entry door.
- Applied: November 21, 1967
- Status date: August 16, 2021
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 1A10](https://openairdocs.org/tcds/1A10)
- Certificate PDF: https://openairdocs.org/files/sha256/d0/46/d04693df878dd8c10844137a25a3f51ab2bb31206aea692a6e32c5fcc47429be
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A7D7C2124AE35C5F8625873B0054704C.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1810WE

## ADs that name it (0)

None.

## Approved models (1)

- The New Piper Aircraft Inc. PA-23-250 ([TCDS 1A10](https://openairdocs.org/tcds/1A10))

## 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 This certificate issued to:

IMPORT SA1810WE Aztec Nomad Inc.

1201 Gravenhurst Parkway Gravenhurst, Ontario Canada P1P 1R1 .

the Civil Air Regulations Original Product 1A10 Make:

Piper Aircraft, Inc.

PA-23-250

1. Installation of left-hand passenger entry door must be done in accordance with Jobmaster Company Sealed Drawing List No. JA-730 dated November 11, 1967.

1. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

(Limitations and Conditions Continued on Page 3 of 3)

November 21, 1967 Date Reissued:

October 17, 1968 December 26, 1968; May 20, 1982; August 16, 2021 February 2, 1982 By Direction of the Administrator Signature:

Timothy J. Hadsall Acting Manager, New York ACO Branch Compliance & Airworthiness Division Aircraft Certification Service

**IMPORT SA1810WE**

SA1810WE To (Name and address of transferee):

IMPORT SA1810WE Date Reissued: August 16, 2021

2. The installer must determine whether this design change is compatible with previously approved modifications.

3. 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 that airplane.

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## Every issue (1)

- August 16, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d0/46/d04693df878dd8c10844137a25a3f51ab2bb31206aea692a6e32c5fcc47429be)

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