Supplemental type certificate · Air Methods LLC

Holder
Air Methods LLC · United States
Status
Current · Reissued
Status date
December 4, 2024
Applied
September 1, 1994
Product
Aircraft · Rotorcraft
Certification basis
Part 29
Data sheet
TCDSH13EU

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of enlarged aft cargo door windows.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number This certificate issued to:

SR00126DE-D Air Methods, LLC 5500 South Quebec Street Suite 300 Greenwood Village, CO 80111 Part 29 Title 14 of the Code of Federal Regulations H13EU Airbus Helicopters Deutschland GMBH MBB-BK 117A-1,A-3,A-4,B-1,B-2,C-1

1. This approval is for the -91 configuration only.

(Limitations and Conditions continued on Page 3) 09/01/1994 12/04/2024 09/23/1994 ODA administrator, ODA-635841-NM Air Methods, LLC 3 Installation of Enlarged Aft Cargo Door. Windows in accordance with Air Methods Configuration Control Drawing 179-9000, Rev. C, dated September 1, 1994, or later FAA-approved revision.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number

Date o transfer:

SR00126DE-D 12/04/2024 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SR00126DE-D 12/04/2024 Limitations and Conditions (Continued):

2. A copy of this certificate and Rotorcraft Flight Manual Supplement, dated September 23, 1994, or later FAA-approved revision, must be maintained as part of the permanent records for the modified rotorcraft.

3. Approval of this change in type design applies to the above model rotorcraft only. This approval should not be extended to rotorcraft of the above models on which other previously approved modifications are incorporated unless it is determined that the relationship 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.

4. 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.

-------------------------------END---------------------------- 3 3

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 6

MakeModelData sheet
Airbus Helicopters Deutschland GmbH (AHD)MBB-BK 117 A-1H13EU
Airbus Helicopters Deutschland GmbH (AHD)MBB-BK 117 A-3H13EU
Airbus Helicopters Deutschland GmbH (AHD)MBB-BK 117 A-4H13EU
Airbus Helicopters Deutschland GmbH (AHD)MBB-BK 117 B-1H13EU
Airbus Helicopters Deutschland GmbH (AHD)MBB-BK 117 B-2H13EU
Airbus Helicopters Deutschland GmbH (AHD)MBB-BK 117 C-1H13EU