# STC SH5236NM - Type: Supplemental type certificate - Status: Current, Issued - Holder: Air Methods Corporation, United States - Description: Installation of passenger grab bars - Applied: October 25, 1991 - Status date: January 30, 1992 - Product: Aircraft, Rotorcraft - Certification basis: Part 29 - Data sheets: [TCDS H4SW](https://openairdocs.org/tcds/H4SW), [TCDS H1SW](https://openairdocs.org/tcds/H1SW), [TCDS H6SW](https://openairdocs.org/tcds/H6SW) - Certificate PDF: https://openairdocs.org/files/sha256/29/7d/297d3710235882dc01b2b1a144e0519d43d53ea0f0410b5a4b820a60e81ed432 - Approved model list and other attachments: [SH5236NM_AML.pdf](https://openairdocs.org/files/sha256/34/03/3403ac1273a57b13043971e3da108e96a3dc110b17ae2799f9bf9a401a0ecee9) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101696205220260126214149.0001 - DRS record last changed: January 26, 2026 - Page: https://openairdocs.org/stc/SH5236NM ## ADs that name it (0) None. ## Approved models (4) - Bell Textron Inc. 205A ([TCDS H1SW](https://openairdocs.org/tcds/H1SW)) - Bell Textron Inc. 212 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) - Bell Textron Inc. 412 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) - McDermott 214 Holdings LLC 214B ([TCDS H6SW](https://openairdocs.org/tcds/H6SW)) ## 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 5452360M This certificate issued to: Air Methods corporation Part * of the Federal Aviation Regulations: Original Product -Typeberlificate Number: * see attached Approved Model List (AML.) Make: * Number SH5236NM for list of approved Model: * rotorcraft models and applicable airworthiness regulations. Installation of passenger grab bars in accordance with Air Methods Corp. Master Drawing List 141-9009, dated October 25, 1991 or later FAA approved revision. Approval Limitations and Conditions: 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 and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. Date of Application: October 25, 1991 Date Reissued: Date of Issuance: January 30, 1992 Date Amended: EDERAL ANTATION By Direction of the Administrator Richard E. Jennings Signature) Supervisor TOMINI STRAND Denver Aircraft Certification Field Office Northwest Mountain Region, Denver, Colorado (Titte) FAA FoRM 8110-2 (10-6B] ### SH5236NM_AML.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. AML AFM AMENDMENT SUPPLEMENT DATE NO. /DATE N/A N/A N/A Richard E. Jennings, Supervisor Denver Aircraft Certification FAA APPROVED MODEL LIST (AML) NO. SH5236NM FAA APPROVED DRAWING LIST REVISION NO. AND DATE NUMBER 10/25/91 141-9009 10/25/91 141-9009 10/25/91 141-9009 FAA Approved: Field Office Date: January 30, 1992 FOR CERTIFICATION ALTERATION FAR Part 29 FAR Part 29 Page 1 of 1 BASIS FOR CAR 7 ORIGINAL TYPE CERTIFICATE NUMBER HISW H4SW H6SW AIRCRAFT MODEL 205A 212, 412 214B AIRCRAFT MAKE ¡ Bell ¡ Bell | Bell ITEM 1 • 3. U.S. Department TRANSPORT AIRPLANE DIRECTORATE of Transportation Aircraft Certification Field Office Administration Federal Aviation 2390 Syracuse Street Denver, Colorado 80207 Telephone: (303) 398-0839 January 30, 1992 Air Methods Corporation 7301 S. Peoria Englewood, CO 80112 Project No. ANM-100D-0372 Gentlemen: We have completed our evaluation of your Supplemental Type Certificate (STC) project and find that you have satisfactorily demonstrated compliance with the applicable certification regulations. Accordingly, we have enclosed your STC No. SH5236NM dated January 30, 1992, which indicates our approval on the installation of Air Methods passenger grab bars on Bell Model 412, 212, 205A and 214B Rotorcraft. This STC is official Federal Aviation Administration (FAA) approval of your installation and may be used to authorize identical installations on other aircraft of the same model, subject to the limitations noted on the certificate. It may be transferred or otherwise made available to another party by means of a licensee arrangement in accordance with Federal Aviation Regulations (FAR) 21.47. You are requested to advise your local office within 30 days after the transfer when you transfer or grant licensee rights to the STC in order that we may take the necessary recording or reissuance action. As recipient of this approval, except as provided by FAR 21.3 (d), you are required to report any failure, malfunction, or defect in any product or part manufactured by you that you have determined has resulted or could result in any of the occurrences listed in FAR 21.3 (C) . The report should be communicated initially by telephone to the Supervisor, Denver Aircraft Certification Field office, telephone number (303) 398-0839, within 24 hours after it has been determined that the failure has occurred. In addition, written notification to the Supervisor at the above address is required. FAA Form 8010-4, Malfunction or Defect Report, or any other appropriate format is acceptable in transmitting the required details. 2 If you plan to manufacture replacement or modification parts for sale in conformance with approved data listed on the Certificate, you are required to comply with FAR Part 21.303. A Parts Manufacturer Approval (PMA) may be issued under the provisions of FAR 21.303 (d) when you submit a statement certifying that you have established a fabrication inspection system as required by FAR 21.303 (h). The identification requirements for parts produced under a PMA are in FAR 45.15. Your statement may be in letter form, with a reference to the STC number, and should be mailed to the address indicated below. Federal Aviation Administration Seattle Manufacturing District Office, ANM-108S 1601 Lind Ave., S.W. Renton, Washington 98055-4056 Sincerely, Richard E. Jennings Supervisor, Denver Aircraft Certification Field office Enclosure ## Every issue (1) - January 30, 1992: Issued, Current. [certificate](https://openairdocs.org/files/sha256/29/7d/297d3710235882dc01b2b1a144e0519d43d53ea0f0410b5a4b820a60e81ed432), [SH5236NM_AML.pdf](https://openairdocs.org/files/sha256/34/03/3403ac1273a57b13043971e3da108e96a3dc110b17ae2799f9bf9a401a0ecee9) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.