# STC SR00182DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Air Methods Corporation International, United States
- Description: Installation of an emergency medical interior system.
- Applied: July 24, 1995
- Status date: September 20, 1995
- Product: Aircraft, Rotorcraft
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/ee/a4/eea41431b6d465876179bdf0c32746f19682374f64f216267638ff1f3360be42
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119797144320260107174210.0001
- DRS record last changed: January 7, 2026
- Page: https://openairdocs.org/stc/SR00182DE

## ADs that name it (0)

None.

## Approved models (1)

- Bell Helicopter Textron (Canada) 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))

## What the certificate says

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

Matt Bake at Anta Department of Transportation - Moderal Authen Adaistcation Supplemental Type Certificate Number SRO0182DE This certificate issued to: Air Methods Corporation International Certifies that the change in the type design for the following product with the limitations and conditions therefor as sreaified herean meeis the airoorthiress requirments of Part 5 of the Civil Air Regulations.

Original Product - Type Genificate Number: H2SW Make: Bell Helicopter Textron, Inc.

Model 206L-3 Description of Type Design Change:

Installation of an Emergency Medical Interior system in accordance with Air Methods Corporation Configuration Control Drawing No. 119-9003, Rev. A, dated 9/19/95, or later FAA approved revision.

1. FAA approved Rotorcraft Flight Manual Supplement RFMS 080-0170, Rev. N/C, dated September 20, 1995.

or later FAA approved revision is required and must be maintained as part of the permanent records for the modified rotorcraft.

2. 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. A copy of this Certificate must be maintained as part of the permanent records for the modified rotorcraft.

3. This modification must use Air Methods Litter P/N: 018-1055-80, or an FAA Approved Litter only with the installed litter platform.

4. This modification requires co-pilot seat, cyclic, and collective controls to be disabled and removed.

Date of Application: July 24, 1995 Dats misund Dais of istancs: September 20, 1995 Date Amended: .

FEDERAL y divotion of the Administrist RONALD F. MAY pageaure Manager O * EMPAST PASION Denver Aircraft Certification Office Northwest Mountain Region, Denver, Colorado (Title)

**FAA FORM B1 10-2(10-68)**

## Every issue (2)

- September 20, 1995: Issued, Current. [certificate](https://openairdocs.org/files/sha256/ee/a4/eea41431b6d465876179bdf0c32746f19682374f64f216267638ff1f3360be42)
- September 20, 1995: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/1d/42/1d42f5cc8842ef40ca09d4f94fd4d6c48b2e81a891dd2ab2fabafa7b752c770c)

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