# STC SR02134LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Hawaii Helicopters, United States
- Description: Installation of Hawaii Helicopters' Air Conditioning System.
- Applied: November 14, 2003
- Status date: May 21, 2008
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU)
- Certificate PDF: https://openairdocs.org/files/sha256/77/e0/77e0c58293f4c638123c2d24622c512907706d9dfc690f6f3f01630cce0a8df4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/962BF473FACC9B2B8625751B00730417.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR02134LA

## ADs that name it (0)

None.

## Approved models (1)

- Eurocopter France EC 130 B4 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))

## What the certificate says

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SRO2134LA This certificate issued to: Hawaii Helicopters 1 Kahului Airport Road #106 Kahului, Hawaii 96732 Part 27 of the Federal. Avialion Pegulations. *Certification basis is set forth in Type Certificate Data Sheet.

Original Product Type Certificate Number: HOEU Make: Eurocopter France Model: EC130 B4 Description of Type Design Change: Installation of Hawaii Helicopters' Air Conditioning System in accordance with FAA approved Hawaii Helicopters Master Drawing List, HH-AC-010, Revision B, dated May 5, 2008, or later FAA approved revision. Hawaii Helicopters Rotorcraft Flight Manual Supplement, HH-AC-009, Revision N/C, FAA approved on May 9, 2008 or later FAA approved revision is required as part of this modification.

Limitations and Conditions: This approval requires the inspections and overhaul schedules to be performed as mandated by Hawaii Helicopters' Instructions for Continued Airworthiness, HH-AC-008, Revision IR, dated November 12, 2007, or later FAA accepted revision.

This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the 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 this permission.

Date of Application: November 14, 2003 Date Amended:

Date of Issuance: May 21, 2008 FEDERAL AVIATION By Direction of the Administrator Han Raft (Signature) Manager, Cabin Safety/Mechanical & TOMNISTRATO Los Angeles Aircraft Certification Office Environmental Systems Branch (Title)

TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street) (City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- May 21, 2008: Issued, Current. [certificate](https://openairdocs.org/files/sha256/77/e0/77e0c58293f4c638123c2d24622c512907706d9dfc690f6f3f01630cce0a8df4)

---
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.