# TCDS 1H14: Omega Aircraft Corporation - Type: Type certificate data sheet - Status: Current - Holder: Omega Aircraft Corporation - Revision: 0 - Revised: May 8, 1961 - Product: Aircraft, Rotorcraft - Certification basis: CAR 6 - Data sheet PDF: https://openairdocs.org/files/sha256/da/d5/dad53f053f758c80a5abcf7073bd77fb24a5bf396b64e3934bbf63f469023062 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3FFE39795F4B609B85256715006F2974.0001 - Page: https://openairdocs.org/tcds/1H14 ## Models (1) As the data sheet lists them. - BS-12D1 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 Rev. No. - - FEDERAL AVIATION AGENCY 1H14 Page 1 OMEGA BS-12D1 May 8, 1961 TYPE CERTIFICATE DATA SHEET NO. 1H14 This data sheet which is a part of type certificate No. 1H14 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder Omega Aircraft Corporation Municipal Airport New Bedford, Mass. I - Model BS-12D1, 5 PLCH, Approved May 2, 1961 Engine 2 Lycoming 0-540-F1A5 or 0-540-F1B5 Fuel 91/96 minimum grade aviation gasoline Engine limits For twin engine operation: HP RPM MP In. Hg. ALT 235 2800 26.0 S.L. 235 2800 25.0 4000' For single engine operation only: 5 min. 260 2800 28.0 S.L. 5 min. 260 2800 27.5 800' (Straight line manifold pressure variation with altitude shown) Rotor limits Maximum 350 r.p.m. Minimum 280 r.p.m. Airspeed limits Vne 95 m.p.h. (82 knots) CAS C.G. range (118.0) to (126.0) Empty weight C.G. range None Datum 124 in. forward of centerline main rotor Leveling means Plumb bob at centerline of aircraft (179) Maximum weight 4750 lb. No. of seats 5. (2 at 39.5, 3 at 70.5) Maximum baggage None Fuel capacity 78 gal., 39 gal. at (133), 39 gal. at (161) Oil capacity 6 gal. (131) Rotor blade and control For rigging information refer to Maintenance Manual. movements 1H14 2 Serial Nos. eligible 1002 and up Certification basis CAR 6, December 20, 1956, and Amendment 6-1 through 6-4. Type Certificate No. 1H14 issued May 2, 1961. Date of Application for Type Certificate May 7, 1960. Production basis None. Prior to certification of each aircraft, a FAA representative must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data, and a check of flight characteristics. Equipment: The basic required equipment as prescribed in the applicable airworthiness regulations (see certificated basis) must be installed in the helicopter for certification. In addition, the following items of equipment are required: (a) FAA Approved Rotorcraft Flight Manual dated May 2, 1961. NOTE 1. Current weight and balance report including list of equipment in certificated empty weight, and loading instructions when necessary, must be in each helicopter at the time of original certification and at all times thereafter except in the case of operators having an approved weight control system. NOTE 2. The following placard must be displayed in front of and in clear view of the pilot: "THIS HELICOPTER MUST BE OPERATED IN COMPLIANCE WITH THE OPERATING LIMITATIONS SPECIFIED IN THE FAA APPROVED ROTORCRAFT FLIGHT MANUAL." NOTE 3. Information essential to the proper maintenance of the helicopter is contained in the manufacturer's Maintenance Manual provided with each helicopter. ...END... ``` ## ADs (1, in force first) - [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies ยท Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006 ## Registered aircraft by registry model (OpenAirDocs) - [Omega BS-12D1](https://openairdocs.org/model/omega-bs-12d1): 0 aircraft (registry code 6620104) ## STCs approved under this data sheet (9) - [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC - [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc - [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC - [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC - [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.. M-20 Oil Separators LLC - [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP.. M-20 Oil Separators LLC - [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International - [STC SA01435DE](https://openairdocs.org/stc/SA01435DE) (historical): Installation of engines, modified with a Firewall Forward Technologies.. Centri-Lube Technologies LLC --- 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.