# STC SA3813NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: BAS Inc, United States
- Description: Installation of a BAS tail pull handle in the aft fuselage.
- Applied: August 13, 1986
- Status date: December 2, 2010
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A24](https://openairdocs.org/tcds/3A24)
- Certificate PDF: https://openairdocs.org/files/sha256/fd/04/fd04a08b2a3794cff969a78a29a953cf9d77bf56316b763470c46a0771bcc4dd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/70EE4EB18B80A83B862577FB00645EBC.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3813NM

## ADs that name it (0)

None.

## Approved models (8)

- Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185B ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185D ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company A185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company A185F ([TCDS 3A24](https://openairdocs.org/tcds/3A24))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Ope Certificate Number: SA3813NM This certificate issued to: BAS, Inc.

411 Super Cub Drive North PO Box 190 Eatonville, WA 98328 Part 3 of the Civil Air Regulations.

Original Product - Type Certificate Number: 3A24 Make: Cessna Model: 185, 185A, 185B, 185C, 185D, 185E, A185E, and A185F Description of Type Design Change: Installation of a BAS, Inc. tail pull handle in the aft fuselage in accordance with BAS, Inc. Installation Instructions No. TPH-1, Sheets 1, 2, and 3, dated March 20, 1987, or later FAA-approved revision and Drawing No. TPH-1, Sheets 1 through 5, dated March 20, 1987, 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 other 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: August 13, 1986 Date Reissued:

Date of Issuance: March 27, 1987 Date Amended: December 02, 2010 FEDERAL AVIATION By Direction of the Administrator ADMINIST RATION (Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- December 2, 2010: Amended, Current. [certificate](https://openairdocs.org/files/sha256/fd/04/fd04a08b2a3794cff969a78a29a953cf9d77bf56316b763470c46a0771bcc4dd)

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