# STC SA00426DE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Quality Aircraft Components LC, United States
- Description: Installation of Model FB-01 "Swing Arm" Pilot Arm Rest System on R/H side of pilot seat.
- Applied: February 9, 2000
- Status date: June 12, 2001
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS 3A21](https://openairdocs.org/tcds/3A21)
- Certificate PDF: https://openairdocs.org/files/sha256/85/d1/85d11bd4c6e9f6c95c4602983b6362ad9227405bcb6354d0abb5b8c2504f5314
- Approved model list and other attachments: [SA00426DE.pdf](https://openairdocs.org/files/sha256/3d/57/3d57c27ed097f888782946db9214a10678cea89d7f8af3da3cf9a0d6b8ba76ea)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/72AFB0A6144AA0A485256CC1007DC914.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00426DE

## ADs that name it (0)

None.

## Approved models (74, first 50)

- Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182R ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182S ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company 206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 210-5 (205) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210-5A (205A) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210C ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210D ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210E ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210G ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210H ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210J ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210K ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210L ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210M ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210R ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company P206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company P210R ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company R182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company T182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company T206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company T207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company T207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company T210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210G ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210H ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210J ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210K ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210L ([TCDS 3A21](https://openairdocs.org/tcds/3A21))

All 74: https://openairdocs.org/stc/SA00426DE/models.md

## 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 APPROVED MODEL LIST (AML) NO. SA00426DE FOR**

**INSTALLATION OF SWING ARM PILOT ARM REST SYSTEM**

**ITEM**

**AIRCRAFT MAKE**

**AIRCRAFT MODEL**

**ORIGINAL TYPE**

**CERTIFICATE NUMER**

**CERTIFICATION**

**BASIS FOR**

**ALTERATION**

**FAA APPROVED**

**MASTER DRAWING LIST REVISION NO.**

**NUMBER AND DATE AFM**

**SUPPLEMENT**

**APPROVAL**

**NUMBER/DATE**

AML

**AMENDMENT DATE**

Cessna

Cessna

Cessna

182E, F, G, H, J, K, L, M, N, P, Q, R, T182, R182, TR182, and 182S

206, P206, P206A, TP206A, P206B, TP206B, P206C, TP206C, P206D, TP206D, P206E, TP206E, U206, U206A, TU206A, U206B, TU206B, U206C, TU206C, U206D, TU206D, U206E, TU206E, U206F, TU206F, U206G, TU206G, 206H, and T206H

207, T207, 207A, and T207A

3A13

A4CE

A16CE

**FAR 23**

**FAR 23**

**FAR 23**

**MDL-01-1**

**MDL-01-1**

**MDL-01-1**

Rev. B – 11/01/00

Rev. B – 11/01/00

Rev. B – 11/01/00

**FMS-01 - 8/1/00**

**FMS-01 - 8/1/00**

**FMS-01 - 8/1/00**

June 12, 2001

June 12, 2001

June 12, 2001

Cessna

210C, -5, -5A, D, E, F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, T210N, 210R, T210R, P210N, and P210R

3A21

**FAR 23**

**MDL-01-1**

Rev. B – 11/01/00

**FMS-01 - 8/1/00**

June 12, 2001

FAA Approved:

David R. Showers, Small Airplane Program Manager Denver Aircraft Certification Office

Date: August 1, 2000 Revised: June 12, 2001

### SA00426DE.pdf

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

United States of America Repartment of Oransportatio-Federal Aviatim Administration Supplemental Ogne Certificate Number SA00426DE This certificate, issued to Quality Aircraft Components LC 2255 South 1800 West Woods Cross, Utah 84087 cortifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part * of the * Régulations.

Original Product-Type Certificate Number: * See attached FAA Approved Model List Make: * (AML) No. SA00426DE, dated June 12, 2001 or later FAA Model: * approved revision for list of approved aircraft models and applicable airworthiness regulations.

Description of the Type Design Change:

Installation of Model FB-01 "Swing Arm" Pilot Arm Rest System on R/H side of pilot seat in accordance with Quality Aircraft Components Master Drawing List Number as listed on FAA AML No. SA00426DE, dated August 1, 2000 or later FAA approved revision.

Limitations and Conditions:

1.) Compatibility of this design change with previously approved modifications must be determined by the installer.

2.) A copy of this certificate and FAA approved Airplane Flight Manual Supplement FMS-01, Revision IR, dated 01/01/00 or later FAA approved revision must be maintained as part of the permanent records of the modified aircraft.

3.) Instructions for Continued Airworthiness Document No. ICA-01-1, Revision IR, dated 01/01/00 or later FAA approved revision is a required part of the permanent records for the modified aircraft, and defines inspection and maintenance requirements.

4.) 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.

This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: February 9, 2000 Date reissued:

Date of issuance: July 31, 2000 Date amended June 12, 2001 FEDERAL AVIATION By direction of the Administrator Daings. Shoves David R. Showers Signature Small Airplane Program Manager ADMIST RATION Denver Aircraft Certification Office Northwest Mountain Region, Denver, Colorado (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

This certificate may be transferred in accordance with FAR 21.47.

**FAA FORM 8110-2(10-68)**

## Every issue (1)

- June 12, 2001: Amended, Current. [certificate](https://openairdocs.org/files/sha256/85/d1/85d11bd4c6e9f6c95c4602983b6362ad9227405bcb6354d0abb5b8c2504f5314), [SA00426DE.pdf](https://openairdocs.org/files/sha256/3d/57/3d57c27ed097f888782946db9214a10678cea89d7f8af3da3cf9a0d6b8ba76ea)

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