TCDS 7E1

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 7E1 Revision 3 BMW GO-480-B1A6 March 28, 2007 TYPE CERTIFICATE DATA SHEET NO. 7E1 Engines of models described herein conforming with this data sheet (which is a part of type certificate No. 7E1) and other approved data on file with the Federal Aviation Agency meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portion of the Civil Air Regulations provided they are installed, operated and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder BMW Triebwerkbau G.m.b.H. Munich 68 Federal Republic of Germany Model BMW GO-480-B1A6 Type 6HOA, reduction gear ratio 77:120 Rating Max. continuous, hp., r.p.m., full throttle at: Sea level pressure altitude 260-3000 Takeoff (5 min.), hp., r.p.m. full throttle at: Sea level pressure altitude 270-3400 Fuel (Min. grade aviation gas.) 80/87 Lubricating oil MIL-L-6082 or Lycoming Spec. No. 301-D Bore and stroke, in. 5.125 X 3.875 Displacement, cu. in., 479.7 Compression ratio 7.3:1 Weight (dry) lb. 432 C.G. location (dry), in. (See Lycoming Dwg. No. 63050) From face of thrust bearing nut-surface "y" 19.37 From propeller shaft C.L. 0.27 below 0.36 right viewed from rear end of the engine Propeller shaft, SAE No. 20 spline Carburetor Bendix-Stromberg PS-58D carburetor Ignition, dual Scintilla S6-LN-20-21 magnetos Ignition, Timing, °BTC 25 Spark plugs Champion REM 39N or equivalent spark plugs according to Lycoming Service Bulletin No. 175H dtd 31 Dec 58 Oil sump capacity, qt. 12 Usable oil sump capacity, qt. 9.25 CERTIFICATION BASIS CAR 10. Type Certificate No. 7E1 issued October 18, 1960. Date of Application for Type Certificate March 14, 1960. The aviation authority for the Federal Republic of Germany Luftfahrt-Bundesamt (LBA), originally type certificated this engine. The FAA validated this product under U.S. Type Certificate Number 7E1. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of the Federal Republic of Germany. Page No. 1 2 Rev No. 3 3 Reformatted 12/93. 7E1, Rev 2 Page 2 IMPORT REQUIREMENTS To be considered eligible for installation on U.S. registered aircraft, each new engine to be exported to the United States with a Federal Republic of Germany LBA or EASA airworthiness approval shall have a Joint Aviation Authorities (JAA) or EASA Form 1, Authorized Release Certificate. The JAA or EASA Form 1 should state that the engine conforms to the type design approved under the U.S. Type Certificate 7E1, is in a condition for safe operation and has undergone a final operational check. NOTE 1. Maximum permissible temperatures: Cylinder head (well-type thermocouple) 475 °F Cylinder barrel 325° F Oil inlet 225 °F NOTE 2. Min. Max. Fuel pressure limits 11 p.s.i. 15 p.s.i. Oil pressure limits: (Normal operation) 65 p.s.i. 85 p.s.i. (Idling) 25 p.s.i. NOTE 3. The following accessory drive provisions are available: *Direction of Rotation **Speed Maximum Torque (in.-lb.) Max. Overhang Moment (in.-lb.) Continuous Static Starter C 1.000:1 ⎯ 3000 80 Generator C 2.577:1 90 250 200 Fuel pump C 1.000:1 50 450 10 Tachometer C .500:1 7 50 5 Vacuum pump C 1.333:1 100 800 25 (or Hydraulic pump) Prop. gov. C .801:1 125 825 ⎯ * "C" - clockwise, facing engine pad ** Speed - Times crankshaft r.p.m. NOTE 4. The GO-480-B1A6 series engine incorporates a crankshaft with five 3rd order and one 6th order torsional vibration dampers. NOTE 5. This engine incorporates provisions for abso rbing propeller thrust in both tractor and pusher type installations. NOTE 6. Each of the documents listed below must state that it is approved by the European Aviation Safety Agency (EASA) or, for approvals made before September 28, 2003 by the Federal Republic of Germany Luftfahrt- Bundesamt. Any such documents including those approved under a delegated authority, are accepted by the FAA and are considered FAA approved. • Service bulletins, • Structural repair manuals, • Vendor manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals. These approvals pertain to the type design only. ...END...