# STC SR01822SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Fliegen Works Inc., United States - Description: Installation of Immersive Camera Mount - Applied: March 5, 2008 - Status date: March 21, 2011 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW), [TCDS H11NM](https://openairdocs.org/tcds/H11NM) - Certificate PDF: https://openairdocs.org/files/sha256/75/43/754348c54dcb6cf5bfae97afacde32a1d63b352a36c0a30e4b1a087f70214e1b - Approved model list and other attachments: [SR01822SE.pdf](https://openairdocs.org/files/sha256/41/8d/418d7ba50c216c9d1562fbe1dd164510cc5e02a6e59b60836dbf48f32eb2489b) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D66E6C8AED233676862579BB007794FC.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SR01822SE ## ADs that name it (0) None. ## Approved models (10) - Bell Helicopter Textron Canada Limited 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206A-1 (OH-58A) ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-1 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-3 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 206L-4 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Bell Helicopter Textron Canada Limited 407 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW)) - Robinson Helicopter Company R44 ([TCDS H11NM](https://openairdocs.org/tcds/H11NM)) - Robinson Helicopter Company R44 II ([TCDS H11NM](https://openairdocs.org/tcds/H11NM)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. FAA APPROVED MODEL LIST (AML) SR01822SE FOR Fliegen Works Inc., Immersive Camera Mount ISSUE DATE: March 5, 2008 FAA APPROVED SEALED DRAWING LIST1 ROTORCRAFT FLIGHT MANUAL SUPPLEMENT1 ITEM AIRCRAFT MAKE AIRCRAFT MODEL ORIGINAL TC NUMBER **CERTIFICATION** BASIS FOR ALTERATION Number Revision Drawing Revision AML REV DATE **1. BELL 206A, 206A-1, 206B, 206L, 206L-1, 206L-3, 206L-4, 407 H2SW** FAR 27, dated February 1, 1965, including amendments 27-1 through 27-30 FW-IMC407-90 L 2/21/11 FW-IMC407-11- BHT206 A 3/18/11 3/21/2011 2. Robinson R44, R44II H11NM FAR 27, dated February 1, 1965, including amendments 27-1 through 27-24 FW-IMC407-90 L 2/21/11 FW-IMC521-11- R44 A 3/18/11 3/21/2011 Notes: 1. Or later FAA Approved Revision FAA Approved: Acting Manager, Seattle Aircraft Certification Office AMENDED: April 02, 2010; March 21, 2011 Reissued: ### SR01822SE.pdf United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SR01822SE This certificate, issued to Fliegen Works, Inc. 921 SE 47th Avenue Portland, OR 97215 certifies that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirements of Part 27 of the Federal Aviation Regulations. Original Product⎯Type Certificate Number: * See attached Approved Model List Make: * (AML) SR01822SE Model: * Description of the Type Design Change: Immersive Camera Mount, manufactured in accordance with Fliegen Works Master Drawing List, as listed on the attached AML, or later FAA-approved revision; and installed in accordance with Fliegen Works Instructions for Continued Airworthiness and Component Maintenance Manual, document number FW-IMC407-13, Revision B, dated March 18, 2010, or later FAA-accepted revision. Limitations and Conditions: This STC does not provide approval for electrical installation/connection to the helicopter. Approval of this change in type design applies to the aircraft listed in AML SR01822SE only. The modified aircraft must be maintained in accordance with Fliegen Works Instructions for Continued Airworthiness and Component Maintenance Manual (ICA), document number FW-IMC407-13, Revision B, dated March 18, 2010, or later FAA-accepted revision, and operated in accordance with the FAA-approved Rotorcraft Flight Manual Supplement (RFMS) as listed on AML SR01822SE, or later FAA-approved revision. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of the 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, the AML, the FAA-approved RFMS, and the ICA must be maintained as part of the permanent records for the modified aircraft. 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. This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: May 18, 2007 Date reissued: Date of issuance: March 05, 2008 Date amended: April 02, 2010 Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. This certificate may be transferred in accordance with FAR 21.47. **FAA FORM 8110-2 (10-68)** By direction of the Administrator __________________________________________ (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) Original Signed by Scott A. Fung ## Every issue (3) - March 21, 2011: Amended, Current. [certificate](https://openairdocs.org/files/sha256/75/43/754348c54dcb6cf5bfae97afacde32a1d63b352a36c0a30e4b1a087f70214e1b), [SR01822SE.pdf](https://openairdocs.org/files/sha256/41/8d/418d7ba50c216c9d1562fbe1dd164510cc5e02a6e59b60836dbf48f32eb2489b) - April 2, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/41/8d/418d7ba50c216c9d1562fbe1dd164510cc5e02a6e59b60836dbf48f32eb2489b), [AML SR01822SE.pdf](https://openairdocs.org/files/sha256/00/5a/005af0276c7ebcdc63a1ec578c414d53988d8559d8012914610ab967379bbbe7) - May 18, 2007: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/e1/f1/e1f13cdf22a06707bec35e04fb716c27591200a3bdaaf86869976b060bcd831d), [AML SR01822SE.pdf](https://openairdocs.org/files/sha256/8b/da/8bda6051f89ad0f4409b2fe5eb335111ea2b4ee3bea774b4e23f54f4aa61e7e1) --- 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.