TCDS 1H14

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...