# STC SR00534DE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Air Methods Corporation, United States
- Description: Installation of Aft Jump Seat
- Applied: June 13, 2003
- Status date: November 10, 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/sha256/6e/11/6e114e4da99612d0e1a588b3be91ba6c0c3862aa01e25253a3f69e9b50f02dc3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CBC166125DB5A785862572660066B198.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00534DE-D

## ADs that name it (0)

None.

## Approved models (8)

- Eurocopter France AS-350B ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350B1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350B2 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350B3 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350BA ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350C ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350D ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350D1 ([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 SR00534DE-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: AS350 Models C, D, D1, B, BA, B1, B2, B3 Description of the Type Design Change:

Installation of Aft Jump Seat in accordance with Ai r Methods Corporation Master Drawing List MDL 741-9011, Revision IR, dated November 20, 2003, FAA approved December 5, 2003, 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 dete rmined that the interrelationship between this c hange 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 Roto rcraft Flight Manual Supplement, Document No. RFMS 080- 0302, Revision IR, dated December 5, 2003, or later F AA approved revision must be maintained as part of the permanent records for the modified rotorcraft.

3. Instructions for Continued Airwor thiness, Document No. AMMS 050-0336, RevisionIR, dated September 15, 2003, FAA accepted December 3, 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 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 ot herwise established by the Administrator of the Federal Aviation Administration.

Date of application: June 13, 2003 Date reissued: November 10, 2006 Date of issuance: December 5, 2003 Date amended:

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

## Every issue (1)

- November 10, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/6e/11/6e114e4da99612d0e1a588b3be91ba6c0c3862aa01e25253a3f69e9b50f02dc3)

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