# STC SR00038BO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Simplex Manufacturing Company, United States
- Description: Installation of Helipod cargo containers.
- Applied: January 4, 1994
- Status date: July 7, 2009
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H10WE](https://openairdocs.org/tcds/H10WE)
- Certificate PDF: https://openairdocs.org/files/sha256/93/38/93388ea0afab1f9ea8b80bebbfca9c3cbf88134da5c4930e439ab9bc7a4e62b7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4BA99C68464ACB88862575FC00627E76.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00038BO

## ADs that name it (0)

None.

## Approved models (3)

- Robinson Helicopter Company R22 ([TCDS H10WE](https://openairdocs.org/tcds/H10WE))
- Robinson Helicopter Company R22 ALPHA ([TCDS H10WE](https://openairdocs.org/tcds/H10WE))
- Robinson Helicopter Company R22 BETA ([TCDS H10WE](https://openairdocs.org/tcds/H10WE))

## 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 SR00038BO

This certificate, issued to Simplex Manufacturing 13340 NE Whitaker Way Portland, OR 97230

Part 27 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: H10WE Make: Robinson Model: R22, R22 Alpha, R22 Beta

Description of the Type Design Change: Installation of Helipod Cargo Containers in accordance with Helipod USA Master Drawing List HSL-A-027-MDL, revision 1, dated March 31, 2005, or later FAA-approved revision. Weight and balance for the installation is 18 pounds per Helipod at a longitudinal arm of 99.0 inches and a lateral arm of +/-26.6 inches.

1. Helipod USA Pilot’s Operating Handbook Supplement No. 1, revision A, dated March 23, 2005, or later FAA- approved revision for Robinson R22 helicopters is required and must be carried during all flights.

2. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of those 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: January 4, 1994 Date reissued: January 28, 2004; July 7, 2009 Date of issuance: January 21, 1995 Date amended: May 25, 2006

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (2)

- July 7, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/93/38/93388ea0afab1f9ea8b80bebbfca9c3cbf88134da5c4930e439ab9bc7a4e62b7)
- May 25, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/2a/94/2a94cae0a4a9915ebfafc9791848e3316df73ed97194f2e04968da60337a840f)

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