# STC SR00377LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Arrow Falcon by Edgefield Manufacturing, United States
- Description: Installation of Arrow OH-58A+ engine out warning system.
- Applied: January 9, 1997
- Status date: May 14, 2024
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H22NM](https://openairdocs.org/tcds/H22NM)
- Certificate PDF: https://openairdocs.org/files/sha256/37/a1/37a1df41e12c5c2b121d1835846b78124400a2238e5e9d68f8a784039e9bec79
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142364466320240516153949.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR00377LA

## ADs that name it (0)

None.

## Approved models (1)

- Arrow Falcon by Edgefield Manufacturing OH-58A+ ([TCDS H22NM](https://openairdocs.org/tcds/H22NM))

## 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 (03/21) FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 1 of 2

Number: SR00377LA Arrow Falcon by Edgefield Manufacturing 27400 Southeast Nelson Road PO Box 429 Sandy, Oregon 97055 Sandy Oregon 97055

Part *of the Federal Aviation Regulations.

* § 21.25, See TCDS H22NM for complete certification basis.

Original Product Type Certificate Number: H22NM Make: Arrow Falcon by Edgefield Manufacturing Model: OH-58A+

Description of Type Design Change: Installation of Arrow Falcon Exporters, Inc. OH-58A+ Engine Out Warning System, Part No. 83009, in accordance with FAA approved Master Drawing List No. 83009-1, Revision A, dated April 16, 1997, or later FAA approved revision, and Arrow Falcon Exporters, Inc. FAA Approved Rotorcraft Flight Manual Supplement Report No. AF5164, dated May 14, 1997, to Army TM 55 1520-228-10, and Arrow Falcon RFM Supplement AF5150.

Limitations and Conditions: Approval of this change in type design applies to the above noted models only.

This approval should not be extended to rotorcraft of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that Rotorcraft. A copy of this certificate must be maintained as part of the permanent records for the modified rotorcraft. The STC holder will provide a written permission statement to each person it authorizes to use this certificate to alter the product.

Date of Application: January 9, 1997 Date Reissued: April 11, 2024; May 14, 2024

Date of Issuance: May 15, 1997 Date Amended:

Title: For Gregory S. DiLibero Branch Manager, West Certification Branch Compliance and Airworthiness Division Aviation Safety

FAA Form 8110-2 (03/21) FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 2 of 2

Number: SR00377LA

## Every issue (2)

- May 14, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/37/a1/37a1df41e12c5c2b121d1835846b78124400a2238e5e9d68f8a784039e9bec79)
- May 15, 1997: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/de/a7/dea734cc495f5c7ec820cbbd52efd1742271720d2a3718d56893fadea1aa96d7)

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