# STC SR00599DE-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: Air Methods Corporation, United States - Description: Installation of a Supplemental Lighting and Filtration System. - Applied: May 3, 2005 - Status date: July 9, 2018 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW) - Certificate PDF: https://openairdocs.org/files/sha256/e9/87/e9873ac4fc2c66b8a23f0bed788eba10f901c7275fbeb9c23472e77a43dc9b7c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4B0990CB0A240267862582CC0050A7F4.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR00599DE-D ## ADs that name it (0) None. ## Approved models (1) - Bell Helicopter Textron (Canada) 407 ([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. AVIATION United States of America Department of Transportation SANESTEA Supplemental Type Certificate Federal Aviation Administration Number: SR00599DE This certificate issued to: Air Methods Corporation 5500 South Quebec Street Suite 300 Greenwood Village, Colorado 80111 Part _27*_ of the Federal Aviation Regulations. *See Page 3 Original Product - Type Certificate Number: Make: Bell Helicopter Textron Canada Limited H2SW Model: 407 Description of Type Design Change: Installation of a Supplemental Lighting and Filtration System in accordance with Air Methods Corporation Master Data Index (MDI) 181-9075, Revision *-", dated June 16, 2006, FAA approved June 26, 2006, or later FAA approved revision, including the latest FAA approved/accepted revision of the following documents: Master Drawing List (MDL) 181-9074 (ICDS Instrument Panel), Revision "", FAA approved June 26, 2006 Master Drawing List (MDL) 181-9088 (Analog Instrument Panel), Revision "", FAA approved June 27, 2008 Limitations and Conditions: 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. A copy of this certificate must be maintained as part of the permanent records for the modified rotorcraft. 3. FAA approved Rotorcraft Flight Manual Supplement (RFMS) 080-0354, Rev "-", dated June 23, 2006, or later FAA approved revision, is required for this installation. 4. FAA accepted Instructions for Continued Airworthiness (ICA) 050-0383, Rev B, dated June 16, 2006, FAA accepted June 22, 2006, or later FAA accepted revision, is required for this installation. Limitations and Conditions: continued on page 3 of 3) Date of Application: May 3, 2005 Date Reissued: Date of Issuance: June 26, 2006 Date Amended: June 27, 2008; July 9, 2018 By Direction of the Administrator Signature Karlt Title Michael R. Giambrocco, ODA administrator Air Methods Corporation, ODA-635841-NM The FAA will reissue the certificate in the name of the transferee and forward it to him. Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number. SRO0599DE To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): Date of transfer. FAA Form 8110-2 (5/14) Page 2 of 3 AVIATIO United States of America Department of Transportation Federal Aviation Administration BINISTRATO Supplemental Type Certificate (Continuation Sheet) Number: SR00599DE Limitations and Conditions: Continued: 5. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Bell Helicopter Textron Canada Limited Model 407 installation of Supplemental Lighting and Filtration System is as follows: a. The type certification basis for Bell Helicopter Textron Canada Limited 407 is shown on TCDS H2SW for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of application, May 3, 2005, is based upon part 27 as amended by Amendment 27-40. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant/not significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be: Regulations at the latest amendment level -NONE Regulations at an intermediate amendment level -NONE Regulations at the amendment level in TCDS H2SW -ALL • - END- FAA For B110-2 (5/14) Page 3 of 3 ## Every issue (2) - July 9, 2018: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e9/87/e9873ac4fc2c66b8a23f0bed788eba10f901c7275fbeb9c23472e77a43dc9b7c) - June 26, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/a8/1c/a81c427fbe47046b7a9e9bd3722a3c63810b49916a32386b00df81a7fb35f16d) --- 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.