# STC SR00595DE-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Air Methods Corporation, United States
- Description: Installation of a Supplemental Lighting System
- Applied: December 14, 2005
- Status date: November 28, 2006
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU)
- Certificate PDF: https://openairdocs.org/files/sha256/b3/76/b3765fbc950e5b2c594d72eb6c2e5222f461b879d83b6e0d646e85ba94a62482
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EBB55FE99B0ED9C2862572660066B2CB.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00595DE-D

## 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

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 SR00595DE-D This certificate, issued to Air Methods Corporation 7301 South Peoria Englewood, Colorado 80112 Part 27* of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet H9EU Original Product⎯Type Certificate Number: H9EU Make: Eurocopter France Model: EC 130 B4 Description of the Type Design Change:

Installation of a Supplemental Lighting System in accordance with Air Methods Corporation Master Data Index (MDI) No. 721-9021, Revision A, dated October 27, 2006, FAA approved November 28, 2006, or later FAA approved revision.

1. 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, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft.

2. A copy of this Certificate and F AA Approved Rotorcraft Flight Manual Supplement Number 080-0337, Rev. A, dated November 22, 2006, or later FAA approved revision must be maintained as a part of the permanent records for the modified rotorcraft.

3. Instructions for Continued Airworthiness, Report A MMS 050-0398, Rev. B, dated November 21, 2006, FAA accepted November 22, 2006, or later FAA accepted revision is required for this installation.

4. If the holder agrees to permit another person to use this cert ificate to alter the product, the holder shall give the other person written evidence of that permission.

This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: December 14, 2005 Date reissued:

Date of issuance: November 28, 2006 Date amended:

Robert C. Lazaroff (Signature), DAS administrator DAS-635841-NM Air Methods Corporation (Title)

## Every issue (1)

- November 28, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/b3/76/b3765fbc950e5b2c594d72eb6c2e5222f461b879d83b6e0d646e85ba94a62482)

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