# STC SA208WE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Glacier View Skyways Inc, United States - Description: Remove right hand cabin door and control column for parachute jumping aerial photography etc - Applied: August 31, 1962 - Status date: September 30, 1962 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheets: [TCDS A-696](https://openairdocs.org/tcds/A-696) - Certificate PDF: https://openairdocs.org/files/sha256/0d/35/0d35cd27bd55d1a24b56a4c4646bc6f66c8fddefb6fe84cbfd033ac4a5803e7a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8E7F4507A556B2BE86257A4B00684D82.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA208WE ## ADs that name it (0) None. ## Approved models (2) - Taylorcraft 2000 LLC BC12-D ([TCDS A-696](https://openairdocs.org/tcds/A-696)) - Taylorcraft 2000 LLC BC12-D1 ([TCDS A-696](https://openairdocs.org/tcds/A-696)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. CORAL AVIATION AGENCY FEDERAL AVIATION AGENCY In reply please WESTERN REGION refer to WE-210.2 P.O. BOX 90007, AIRPORT STATION Los Angeles 9, California NOV 14 Glacier View Skyways, Inc. Box 252 Kalispelı, Montana Issuance of Supplemental Type Certificate(g) Relative to Removal of Right-Hand Cabin Door and Control Column for Purposes of Parachute Jumping, Aerial Photography, etc. - Universal (Taylorcraft) BC12-D and BC12-D1 Aircraft. Gentlemen: The necessary investigations associated with the subject design modification(s) have been completed, and we are transmitting herewith your Supplemental Type Certificate (8) No. SA208WE. The Certificate(g) reflect(s) the approval of your type design modification (s) and may be used to authorize identical modification (s) of other airplanes of the sane model. The Certificate (s) may be transferred or otherwise made available to another party, such as by means F232S of a licensee arrangement. when you transfer or grant licensee rights to the Certificate(s), in order that we may take the necessary recording or reissuance action. If you plan to manufacture for sale, articles in conformance with the subject Supplemental Type Certificate(s), you will be required to comply with Part 1.55 of the Civil Air Pegulations. Parts shipped without identification and evidence of FAA inspection at source will not be eligible for installation in certificated aircraft. Application for Parts Manufacturing Approval should be made in letter form giving the part name and number, Supplements' Type Certificate Number (8), and model of type certificated product for which the part has been approved for installation. The application should be addressed to: Federal Aviation Agency. P. O. Box 90007, Airport Station, Los Angeles 9, California. Attn: Chief, Manufacturing and Inspection Section. Please do not hesitate to request any additional information we may be able to provide with respect to the Supplemental Type Certificate(s) or Parts Manufacturing Approval procedures. Sincerely, Charles R. Hawks, Chiet, Engineering & Manufacturing Branch Flight, Standards Division Enclosure (a) LA-421(11/61) FEDERAL AVIATION AGENCY Supplemental Type Certificate **1. NAME AND ADDRESS OF APPLICANT FORM APPROVED, BUDGET BUREAU NO. 04-R015** **INSTRUCTIONS - SUBMIT IN TRI FLICATE TO LOCAL FAA FLIGHT STANDARDS INSPECTOR.** **COPY WILL BE RETURNED TO APPLICANT UPON** ISSUANCE Supplemental Type Certificate APPLIED FOR: Glacier View Skyways, Inc. | AIRCRAFT ENGINE PROPELLER Box 252 ORIGINAL MODEL DESIGNATION Kalispell, Montana Universal (Taylorcraft) BC12-D, BC12-D1 NEW MODEL DESIGNATION (If desired) None 3. DESCRIPTION OF CHANGE Remove right-hand cabin door and control column for purposes of parachute jumping aerial photography, etc. LIMITATION OF APPLICABILITY. This approval should not be extended to other specific airplanes of these models 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 will introduce no adverse effect upon the airworthiness of that airplane. See Reverse Side for Operations Limitations. See Reverse Side for Instructions for Removal of Right-Hand Control Column. No further data required. Certification Basis: CAR-4a. 4a. WILL DATA BE AVAILABLE FOR SAKEXOX RELEASE TO OTHER PERSONS? YES NO b. WILL PARTS BE MANUFACTURED FOR SALE (Ref. CAR 1.55)? YES X NO **5. SIGNATURE AND TITLE OF APPLICANT** SIGNATURE August 31, 1962 President Date of Application: TITLE 6. To be Completed by FAA NATURE AND LOCATION OF DATA No further data required. ORIGINAL TYPE CERTIFICATE NO. FAA APPROVAL Pree Lins A-696 Supplemental Type Certificate NO. Charles R. Hawks SA208WE DATE OF APPROVAL September 30, 1962 Chief, Engineering and Manufacturing Branch Flight Standards Div. TITLE * U.S. GOVERNMENT PRINTING OFFICE: 1959 0-509657 FORM FAA- 2417(5-59) OPERATIONS LIMITATIONS A COPY OF THESE LIMITATIONS SHALL BE CARRIED IN THE AIRCRAFT AT ALL TIMES. The following placards are required in full view of the pilot and passenger: "AIRPLANE'S MANEUVERS ARE LIMITED TO NORMAL TAKE-OFFS, CLIMBS, BANK ANGLES NOT TO EXCEED 30°, YAW ANGLES NOT TO EXCEED 15°, GLIDES, LANDINGS AND SPEEDS NOT IN EXCESS OF 90 MPH TIAS. 2. "NO SMOKING PERMITTED. 3. "FAA APPROVED SEATING PROVISIONS WITH SAFETY BELTS MUST BE PROVIDED FOR PILOT AND PASSENGER. 4. "ALL LOOSE OBJECTS IN THE CABIN MUST BE PROPERLY SECURED." NOTE: In addition 'to placards i through 4, inciusive, placards 5-and 6 are required when aircraft used for Parachute Jumping Operations. 5. "JUMPER'S STATIC LINE MUST BE INSTALLED IN A MANNER TO PREVENT INTERFERENCE WITH PILOT'S CONTROLS AND CONTROL SURFACES. 6. "PILOT SHALL WEAR A PARACHUTE." **INSTRUCTIONS FOR REMOVAL OF RIGHT-HAND CONTROL COLUMN** 1. Remove the 3/16-inch bolt on the wheel side of the control tube universal joint. 2. Remove the control column from the instrument panel by pulling the column aft. 3. Check to determine that controls operate freely. Reverse the above procedure when activating the Right-hand Control. Maintain all original safetying provisions. ## Every issue (1) - September 30, 1962: Issued, Current. [certificate](https://openairdocs.org/files/sha256/0d/35/0d35cd27bd55d1a24b56a4c4646bc6f66c8fddefb6fe84cbfd033ac4a5803e7a) --- 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.