# STC SR01452SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Acrohelipro Global Services USA Inc, United States
- Description: Installation of structural provisions for four antenna pods, two on the underside of the fuselage and one each on the tips of the rotorcraft wings.
- Applied: April 19, 2004
- Status date: April 16, 2007
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H9SW](https://openairdocs.org/tcds/H9SW)
- Certificate PDF: https://openairdocs.org/files/sha256/71/c9/71c96ae57fbcd4d4e56a316093bea139c9396a63a1e3dc15d6e12b0ee236bcc1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F645C5DE0E5A21B9862572C100563CB1.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR01452SE

## ADs that name it (0)

None.

## Approved models (1)

- Bell Helicopter Textron (Canada) 430 ([TCDS H9SW](https://openairdocs.org/tcds/H9SW))

## What the certificate says

Some pages are OCR from the scanned FAA certificate. OCR can misread letters and numbers.

Number: SR01452SE This certificate issued to: ACROHELIPRO Global Services USA, Inc.

c/o Aero Services, 1890 Renshaw Way Juneau, AK 99801 Part 29 of the Federal Aviation Regulations.

Original Product ⎯Type Certificate Number: H9SW Make: Bell Helicopter Textron (Canada) Model: 430

Description of Type Design Change: Installation of structural provisions for four antenna pods, two on the underside of the fuselage and one each on the tips of the rotorcraft wings, per ACROHELIPRO Global Services Master Drawing List (MDL) HP 430-23-00-101, Revision “A”, dated March 12, 2007, or later FAA approved revision. This modification must be maintained in accordance with the ACROHELIPRO Global Services Instructions for Continued Airworthiness HP 430-05-00-252 revision N/C, dated March 15, 2004 or later FAA accepted revision.

Limitations and Conditions: Approval to this change in type design applies to the above model rotorcraft only, and is limited to rotorcraft equipped with high skid gear. This provisions-only approval does not authorize any active antenna or cable installation. This approval should not be extended to rotorcraft of these models 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 rotorcraft. Rotorcraft modified in accordance with this STC must be operated with an FAA approved copy of the Rotorcraft Flight Manual Supplement (RFMS), ACROHELIPRO Global Services Document No. FMS HP 430-23-00-301, Revision N/C, dated October 19, 2004, or later FAA approved revision. A copy of this certificate, the maintenance manual supplement and the RFMS shall 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: April 19, 2004 Date reissued: April 16, 2007 Date of Issuance: September 13, 2004 Date amended: August 5, 2005; April 16, 2007

___Original signed by Angelos Xidias (Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

30S-GA-05-84 2

## Every issue (1)

- April 16, 2007: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/71/c9/71c96ae57fbcd4d4e56a316093bea139c9396a63a1e3dc15d6e12b0ee236bcc1)

---
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.
