# STC SR00567DE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Air Methods Corporation, United States
- Description: Installation of Dual Searchlights
- Applied: August 6, 2004
- Status date: November 17, 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/sha256/36/7f/367fe8b00d6dd3a0decffc8c0d522957de6833fcc3f32870ab35f9002a7607d6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4D56726839CE2A91862572660066B220.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00567DE-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 SR00567DE-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 135 P1, P2, T1, T2 Description of the Type Design Change:

Installation of Dual Searchlights in accordance with Air Methods Corporation Master Data Index MDI #: 731-9021, Revision -, dated November 11, 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, incl uding changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft.

2. A copy of this Certificate and FAA Approved Rotorcraft Flight Manual Supplement Number 080-0313, Rev. -, dated November 26, 2004, or later FAA approved revisi on must be maintained as a part of the permanent records for the modified rotorcraft.

3. Instructions for Continued Airworthiness, Report AMMS 050-0367, Rev. IR, dated July 14, 2004, FAA accepted dated November 2, 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: November 17, 2006 Date of issuance: November 26, 2004 Date amended: November 17, 2006

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

## Every issue (1)

- November 17, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/36/7f/367fe8b00d6dd3a0decffc8c0d522957de6833fcc3f32870ab35f9002a7607d6)

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