# STC SR00689DE-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Air Methods Corporation, United States
- Holder's repair stations: [2A6D933B](https://openairdocs.org/faa-repair-station/2A6D933B/air-methods-llc.md) Mesa, AZ; [2A6R933B](https://openairdocs.org/faa-repair-station/2A6R933B/air-methods-llc.md) West Mifflin, PA; [QMLR253U](https://openairdocs.org/faa-repair-station/QMLR253U/air-methods-llc.md) Englewood, CO (OpenAirDocs)
- Description: Installation of Reduced Instrument Panel and Enhanced Avionics.
- Applied: May 12, 2010
- Status date: May 12, 2010
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU)
- Certificate PDF: https://openairdocs.org/files/sha256/e4/78/e478e80464c048e3ed1553d1081c87dfacb197193c17d373e8f3be2ab5756c43
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/673F105882DA66BE862577C700735D03.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00689DE-D

## ADs that name it (0)

None.

## Approved models (1)

- Eurocopter France EC 130 B4 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))

## PMA parts approved under this STC (OpenAirDocs) (2)

Parts manufacturer approvals whose approval basis names this STC, from the PMA records in DRS. In force first, newest first.

- [MDL 721-9030](https://drs.faa.gov/browse/excelExternalWindow/B90823D4E6CB894A862578260067FA4E.0001): Reduced Instrument Panel and Enhanced Avionics. Air Methods Corp International · PMA PQ1816NM · Jan 20, 2011
- [MDL 721-9026](https://drs.faa.gov/browse/excelExternalWindow/4874B15578C07C11862578260067FA1C.0001): Reduced Instrument Panel and Enhanced Avionics. Air Methods Corp International · PMA PQ1816NM · Jan 20, 2011

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR00689DE-D This certificate issued to: Air Methods Corporation 7301 South Peoria Englewood, Colorado 80112 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirement's of Part 27* of the Federal Aviation Regulations. *See Continuation Page 3 Original Product Type Certificate Number: H9EV Make: Eurocopter France Model: EC130 B4 Description of Type Design Change:

Installation of Reduced Instrument Panel and Enhanced Avionics in accordance with Master Drawing Lists, Air Methods Corporation Document Number 721-9026, revision IR dated 3/12/2010, and Air Methods Corporation Document Number 721-9030, revision IR dated 4/22/2010, or later FAA approved revisions.

1. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.

2. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

3. A copy of this certificate and FAA Approved Rotorcraft Flight Manual Supplement, Air Methods Corporation Document Number 080-0473, revision IR dated 5/7/2010, or later FAA approved revision must be maintained as part of the permanent records for the modified rotorcraft.

Limitations and Conditions: continued on page 3 of 3)

Date of Application: December 4, 2009 Date Reissued:

Date of Issuance: May 12, 2010 Date Amended:

FEDERAL AVIATION By Direction of the Administrator → A hour Kreg R. Voorhies, ODA administrator (Signature) ADMINISTRATION ODA-635841-NM Air Methods Corporation (Title)

Anita States of Amaica Pepentent uf Craneutation - Federal Avertim Administratio Supplemental Type Certificate (Continuation Sheet) Number: SR00689DE-D Limitations and Conditions: (Continued):

4. The following Instructions for Continued Airworthiness (ICA) must be made available to the operator at the time of installation:

a. Air Methods Corporation Document Number 050-0542, Revision B dated 3/29/2010, or later FAA accepted revision must be made available to the operator at the time of installation.

b. Air Methods Corporation Document Number 050-0543, Revision B dated 4/15/2010, or later FAA accepted revision must be made available to the operator at the time of installation.

Certification Basis:

The certification basis for this modification is as follows:

In accordance with Type Certificate Data Sheet, H9EU, revision 17 dated February 15, 2007, EC 130B4 Certification Basis;

FAR Part 21.29 and FAR Part 27 Amendment 27-1 through Amendment 27-32 except FAR 27.952 is not adopted.

FAR 36 Appendix H through Amendment 20 Special Condition 27-009-SC for HIRF Equivalent Level of Safety Findings

- FAR 27.1549(b) Powerplant Instrument Markings

- FAR 27.1027(b)(2) Main Gearbox Oil Filter Bypass -END--------

## Every issue (1)

- May 12, 2010: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e4/78/e478e80464c048e3ed1553d1081c87dfacb197193c17d373e8f3be2ab5756c43)

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