# STC SR00015DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Air Methods Corporation, United States
- Description: Installation of emergency medical interior configuration using a Lifeport plus unit and ERDA swivelling seats.
- Applied: December 30, 1992
- Status date: February 4, 1993
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H9SW](https://openairdocs.org/tcds/H9SW)
- Certificate PDF: https://openairdocs.org/files/sha256/de/be/debeb88d754b83d51818e5b158874a8b4ebb3d1bcae89f9d55183c8bbdd0ffd8
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/740D76F7BA972CCB85256CC200622431.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00015DE

## ADs that name it (0)

None.

## Approved models (1)

- Bell Helicopter Textron (Canada) 222U ([TCDS H9SW](https://openairdocs.org/tcds/H9SW))

## 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 SRO0015DE 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 specified hereon meets the airworthiness reguirements of Part 29 of the rederal Aviation Regulations Original Product -Typebertificate Number: 1H9SW Make: Bell Helicopter Textron, Inc.

Model: 222U Description of Type Design Change:

Installation of emergency medical interior configuration using a Lifeport, Inc. Plus unit and ERDA swivelling seats in accordance with Air Methods Corporation Master Drawing List No. 121-9009, Rev. A, dated January 19, 1993, or later FAA approved revision.

1. FAA Approved Rotorcraft Flight Manual Supplement, dated February 4, 1993, is required with this installation.

2. Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change This contipede a cohe sinating assetech i Peles for a punal shall remain in effet until sum rendered, suspended, vevoked, or a termination date is otherwise established by the Adminis trate r of the Federal Aviation Administration .

Date of Application: December 30, 1992 Date Reissued:

Date of Issuance: February 4, 1993 Date Amended:

FEDERAL AVIATION By dirati on if the dininistratur au RICHARD E. JENNINGS Signalure) Manager TOMINISTRAI Northwest Mountain Region, Denver, Colorado Denver Aircraft Certification Field Office (Title)

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SROO015DE and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

A copy of this Certificate, Continuation Sheet, and FAA Rotorcraft Flight Manual Supplement, dated February 4, 1993, or later FAA approvec cevision, must be maintained as part of the permanent records for the modified aircraft.

**FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES**

## Every issue (1)

- February 4, 1993: Issued, Current. [certificate](https://openairdocs.org/files/sha256/de/be/debeb88d754b83d51818e5b158874a8b4ebb3d1bcae89f9d55183c8bbdd0ffd8)

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