# STC SR00566DE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Air Methods Corporation, United States
- Description: Installation of an Emergency Medical System (EMS) interior
- Applied: August 6, 2004
- Status date: July 14, 2006
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H88EU](https://openairdocs.org/tcds/H88EU)
- Certificate PDF: https://openairdocs.org/files/sha256/95/22/952235a5fdc08eed138fe4d8229ebeb341398e75972acd7e672648d1e31cba96
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D225BD0DF6D74505862572660066B1C7.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00566DE-D

## ADs that name it (0)

None.

## Approved models (1)

- Eurocopter Deutschland GmbH EC135 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))

## 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 SR00566DE-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 H88EU Original Product⎯Type Certificate Number: H88EU Make: Eurocopter Deutschland GmbH (ECD) Model: EC 135P2 Description of the Type Design Change:

Installation of an Emergency Medical System (EMS) interior in accordance with Air Methods Corporation Master Drawing List MDL #: 731-9010, Revision A, dated November 6, 2004, FAA approved November 22, 2004, 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 FAA Approved Rotorc raft Flight Manual Supplement Number 080-0314, Rev. IR, dated October 19, 2004, FAA approved November 22, 2004 or later FAA approved revision must be maintained as a part of the permanent records for the modified rotorcraft.

3. Instructions for Continued Airworthiness, R eport AMMS 050-0368, Rev. IR, dated August 26, 2004, FAA accepted dated November 22, 2004, or later FAA accepted revision is required for this installation.

4. If the holder agrees to permit another per son to use this certificate 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: August 06, 2004 Date reissued: July 14, 2006 Date of issuance: November 24, 2004 Date amended:

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

## Every issue (1)

- July 14, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/95/22/952235a5fdc08eed138fe4d8229ebeb341398e75972acd7e672648d1e31cba96)

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