# STC SR00806SE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Simplex Manufacturing Company, United States - Description: Fabrication of Simplex Model 914 adjustable cargo mirror system - Applied: November 30, 1999 - Status date: June 1, 2000 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS H1SW](https://openairdocs.org/tcds/H1SW), [TCDS H4SW](https://openairdocs.org/tcds/H4SW) - Certificate PDF: https://openairdocs.org/files/sha256/15/c1/15c1ecdb63393cdf8a68e430c5e4b112b28b2130faed7428615819cf8ae5074b - Approved model list and other attachments: [AML SR00806SE.pdf](https://openairdocs.org/files/sha256/75/6f/756fc2ff2ce96643992a38cd4475e2a41495f08831fe791d8cc2b40c69a2fee8) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C3671858E996FF9785256CC200622620.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SR00806SE ## ADs that name it (0) None. ## Approved models (4) - Bell Helicopter Textron Inc. 205A-1 ([TCDS H1SW](https://openairdocs.org/tcds/H1SW)) - Bell Helicopter Textron Inc. 212 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) - Bell Helicopter Textron Inc. 412 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) - Bell Helicopter Textron Inc. 412EP ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) ## 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. United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SR00806SE This certificate, issued to Simplex Manufacturing Company 13340 NE. Whitaker Way Portland, OR 97230 Part * of the * Regulations. Original ProductType Certificate Number: *See attached Approved Model List (AML) Make: No. SR00806SE for list of approved rotorcraft Model: models and applicable airworthiness regulations Description of the Type Design Change: Fabrication of Simplex Model 914 adjustable cargo mirror system in accordance with Simplex Master Drawing List No. MDL 914, dated April 3, 2000, or later Federal Aviation Administration (FAA) approved revision; and installation of this system in accordance with Installation Document No. 914-102 002-001, dated March 30, 2000, or later FAA approved revision. This modification must be maintained in accordance with Simplex Maintenance Manual Supplement, Document No. 914-102 005-001, dated April 6, 2000, or later FAA approved revision. Limitations and Conditions: Approval of this change in type design applies to the Bell model rotorcraft listed above. This approval should not be extended to other rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that helicopter. Rotorcraft modified in accordance with this STC must be operated in accordance with an FAA approved copy of the Rotorcraft Flight Manual Supplement (RFMS), Simplex Document No. 914-102 003-002, dated June 1, 2000, or later FAA approved revision. A copy of this Certificate, AML, Maintenance Manual Supplement and FAA approved RFMS must be maintained as part of the permanent records of the modified helicopter. 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 ba sis 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: November 30, 1999 Date reissued: Date of issuance: June 1, 2000 Date amended: (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ### AML SR00806SE.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. ISSUE DATE: JUNE 1, 2000 AML AMENDMENT DATE Original Original Acting Manager, Seattle Aircraft Certification Office Page 1 of 1 RFM SUPPLEMENT NO. AND DATE 914-102 003-002 6/1/00 914-102 003-002 6/1/00 AML) NUMBER SR00806SE FAA APPROVED MASTER DRAWING REV Original, 4/3/00 Original, 4/3/00 SIMPLEX MANUFACTURING COMPANY NUMBER MDL-914 MDL-914 FAA Approved: FAA APPROVED MODEL LL FOR CERTIFICATION BASIS FOR ALTERATION CAR 7, dated 8/1/58 and Amendments 7-1 through 7-4, Category B FAR Part 29, dated 2/1/65 and Amendments 29-1 and 29-2. See TCDS H4SW for additional information TYPE CERTIFICATE NUMBER H1SW H4S W AIRCRAFT MODEL 205A-1 212, 412, 412EP **AIRCRAFT MAKE BELL BELL ITEM** ## Every issue (1) - June 1, 2000: Issued, Current. [certificate](https://openairdocs.org/files/sha256/15/c1/15c1ecdb63393cdf8a68e430c5e4b112b28b2130faed7428615819cf8ae5074b), [AML SR00806SE.pdf](https://openairdocs.org/files/sha256/75/6f/756fc2ff2ce96643992a38cd4475e2a41495f08831fe791d8cc2b40c69a2fee8) --- 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.