# STC SR00494DE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Air Methods Corporation, United States
- Description: Installation of an Auxiliary Seating/Litter System
- Applied: June 21, 2002
- Status date: November 17, 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/sha256/74/16/74161446dd9698c558ee3f48dea9cfb9eaa62324a47c8ce2c232abe70c6e5ca4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/312A358C41161A6886257266005FF21E.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00494DE-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 SR00494DE-D This certificate, issued to Air Methods Corporation 7301 South Peoria Englewood, Colorado 80112 Part 27 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: H9EU Make: Eurocopter France Model: EC 130 B4 Description of the Type Design Change:

Installation of an Auxiliary Seating/Litte r System in accordance with Air Met hods Corporation Master Drawing List (MDL) MDL-130003-1, Revision IR, dated April 9, 2003, FAA approved April 30, 2003, or later FAA approved revision.

1. This approval should not be extended to rotorcraft of th is model on which other prev iously approved modifications are incorporated unless it is determined that the inte rrelationship 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 Supplement Document No. FMS-130003-1, Revision IR, dated April 30, 2003 or later FAA approved re vision must be maintained as part of the permanent records for the modified aircraft.

3. Instructions for Continued Airworthiness, Docum ent No. ICA-130003-1, Revision IR, dated April 16, 2003, FAA accepted April 29, 2003 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 alte r 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 ot herwise established by the Administrator of the Federal Aviation Administration.

Date of application: June 21, 2002 Date reissued: November 17, 2006 Date of issuance: April 30, 2003 Date amended:

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

## Every issue (1)

- November 17, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/74/16/74161446dd9698c558ee3f48dea9cfb9eaa62324a47c8ce2c232abe70c6e5ca4)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.