# STC SR00624DE-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Air Methods Corporation, United States
- Description: Installation of DeVore Tail Rotor and Clamshell Door Floodlights
- Applied: March 26, 2007
- Status date: May 21, 2007
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H13EU](https://openairdocs.org/tcds/H13EU)
- Certificate PDF: https://openairdocs.org/files/sha256/25/39/25392b67143bf89d2c46c62a8ccedf7255625af2fb9a147ee55775289a6574ce
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BAD7A97F97BB475A862573C900680BCF.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00624DE-D

## ADs that name it (0)

None.

## Approved models (1)

- Eurocopter Deutschland GmbH MBB-BK 117 C-2 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU))

## 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 SR00624DE-D This certificate, issued to Air Methods Corporation 7301 South Peoria Englewood, Colorado 80112 Part 29 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: H13EU Make: Eurocopter Deutschland GmbH (ECD) Model: MBB BK117 Model C-2 Description of the Type Design Change:

Installation of DeVore Tail Rotor and Clamshell Door Floodlights in accordance with Air Methods Corporation Master Data Index (MDI) No. 771-9033, Revision “-“, dated May 21, 2007, FAA approved May 21, 2007, 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 Rotorcraft Flight Manual Supplem ent Number 080-0376, Rev. IR, dated May 2, 2007, or later FAA approved revision must be maintained as part of the permanent records for the modified rotorcraft.

3. Instructions for Continued Airworthiness, Report AMMS 050-0425, Rev, A, dated April 17, 2007, FAA accepted April 19, 2007, 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.

Date of application: March 26, 2007 Date reissued:

Date of issuance: May 21, 2007 Date amended:

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

Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (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)

Signature of grantor (In ink):

## Every issue (1)

- May 21, 2007: Issued, Current. [certificate](https://openairdocs.org/files/sha256/25/39/25392b67143bf89d2c46c62a8ccedf7255625af2fb9a147ee55775289a6574ce)

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