# STC SR09467RC

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aircraft Systems & Mfg, United States
- Description: Installation of ASM Swing Arm Assembly kit
- Applied: January 28, 2005
- Status date: July 27, 2006
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H4SW](https://openairdocs.org/tcds/H4SW)
- Certificate PDF: https://openairdocs.org/files/sha256/02/2b/022bbabf776b627b3d571b5a4bdcfd36f6736c4d02a27a55d9183ccdb78668cc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E6AC190BBB0AAA1C862571C50069DFDA.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR09467RC

## ADs that name it (0)

None.

## Approved models (4)

- Bell Helicopter Textron 212 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW))
- Bell Helicopter Textron 412 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW))
- Bell Helicopter Textron 412CF ([TCDS H4SW](https://openairdocs.org/tcds/H4SW))
- Bell Helicopter Textron 412EP ([TCDS H4SW](https://openairdocs.org/tcds/H4SW))

## 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.

Number SR09467RC This certificate issued to Aircraft Systems & Manufacturing, Inc.

302 Toledo Trail Georgetown, TX 78268

Part 29 of the Federal Aviation Regulations.

Original Product -- Type Certificate Number : H4SW Bell Helicopter Textron Make :

212 ; 412 ; 412CF ; 412EP

Description of Type Design Change: Installation of ASM Swing Arm Assembly kit in accordance with Aircraft Systems & Mfg., Inc. Drawing List 5664-0001-00, Revision B, Dated June 10, 2006 or later FAA approved revisions.

Limitations and Conditions: The Rotorcraft Flight Manual Supplement, Aircraft Systems & Mfg., Inc.

Drawing No. 5664-2160-00 Rev. IR, dated July 27, 2006 or later FAA approved revision is required.

Instruction for Continued Airworthiness, Aircraft Systems & Mfg., Inc., Report No. 5664-2170-00, Revision IR, dated April 27, 2006, or later revision required. Compatibility (See continuation sheet 3 of 3)

Date of application : January 28, 2005

Date of issuance : July 27, 2006 Date reissued :

( Signature) Carl F. Mittag, Manager Rotorcraft Certification Office Southwest Region

(Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

Number SR09467RC Date of Issuance: July 24, 2006

of this design change with previously approved modifications must be determined by the installer. 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 approval is only for the installation of the Swing Arm Assembly Kit.

Class A, B, C or D external load operations are not authorized for use with the Swing Arm Assembly Kit.

Removal of all aft side facing seats on the same side of the aircraft as the Swing Arm Assembly is required.

## Every issue (1)

- July 27, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/02/2b/022bbabf776b627b3d571b5a4bdcfd36f6736c4d02a27a55d9183ccdb78668cc)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.