# STC SR01884AT

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Bell Helicopter Textron Inc., United States
- Description: Installation of Retractable Hardpoints System
- Applied: November 7, 1998
- Status date: May 19, 2016
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H1SW](https://openairdocs.org/tcds/H1SW), [TCDS H4SW](https://openairdocs.org/tcds/H4SW)
- Certificate PDF: https://openairdocs.org/files/sha256/8b/a2/8ba243ddfc66842e2cd111b78bd5a5ecf96b3db4e7015a82709355b641d5f547
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A0F627F5ECA9381386257FC70063B006.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR01884AT

## ADs that name it (0)

None.

## Approved models (6)

- Bell Helicopter Textron 205A ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))
- Bell Helicopter Textron 205A-1 ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))
- Bell Helicopter Textron 205B ([TCDS H1SW](https://openairdocs.org/tcds/H1SW))
- 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 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.

FAA Form 8110-2 (8/13) Page 1

Part of the Federal A viation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

Signature

Title

SR01884AT Bell Helicopter Textron, Inc.

441 Industrial Park Road Piney Flats, TN 37686 29 H1SW H4SW Bell Helicopter Textron, Inc.

205A, 205A-1, 205B 212, 412, 412EP Installation of Retractable Hardpoints System in accordance with Master Drawing List, Report No. AA-98166, Revision O, dated August 25, 2015, or later FAA approved revision. Aeronautical Accessories Instructions for Continued Airworthiness, Report No. AA-98169, Revision F, dated August 7, 2006, or later FAA accepted revision, is required. Aeronautical Accessories Rotorcraft Flight Manual Supplement, Report No. AA-15058, No Revision, dated May 16, 2016, or later FAA approved revision, is required.

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

11/7/1998 4/15/1999 6/6/2011 8/10/2001 5/19/2016 Thomas W. Brooks ODA Lead administrator BHTI ODA-710621-SW

FAA Form 8110-2 (8/13) Page 2

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

SR01884AT

FAA Form 8110-2 (8/13) Page 3

SR01884AT Continuation Sheet 1 of 1.

5/19/2016

Certification Basis:

Subpart C 29.301 [29-0], 29.303 [29-0], 29.305 [29-0], 29.307 [29-0];

Subpart D 29.601 [29-0], 29.603 [29-0], 29.605 [29-0], 29.607 [29-0], 29.609 [29-0], 29.613 [29-0], 29.625 [29-0],

29.865 [29-30];

Subpart G 29.1581 [29-15], 29.1583(c)(d)(e) [29-0], 29.1585(a) [29-2], 29.1589 [29-0].

- END -

## Every issue (2)

- May 19, 2016: Amended, Current. [certificate](https://openairdocs.org/files/sha256/8b/a2/8ba243ddfc66842e2cd111b78bd5a5ecf96b3db4e7015a82709355b641d5f547)
- June 6, 2011: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/3a/c7/3ac70d65cee84ad54fd3d3d0d7d7c70c4b555354d4651fab55b181164ea51ffe)

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