TCDS 1E1

Page No. 1 2 3 Rev No. 5 5 5 Reformatted 8/94 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1E1 Revision 5 Lycoming Engines VO-360-A1A -A1B, -B1A IVO-360-A1A June 23, 2010 TYPE CERTIFICATE DATA SHEET NO. 1E1 Engines of models described herein conforming with this data sheet (which is a part of type certificate No. 1E1) 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 portions 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 Lycoming Engines An Operating Division of AVCO Corporation Williamsport, Pennsylvania 17701 Type Certificate Holder Record Lycoming Division, AVCO CORP., Williamsport, PA. transferred TC 1E1 to Lycoming Engines, An Operating Division of AVCO Corporation on June 23, 2010 Model Lycoming VO-360-A1A VO-360-A1B, -B1A IVO-360-A1A Type 4H0A Vertical Mounted Direct Drive Rating Max. continuous, hp., r.p.m., full throttle at: Sea level pressure altitude 180-2900-S.L. - - - - Takeoff (5 min.) hp., r.p.m., full throttle at: Sea level pressure altitude 180-2900-S.L. - - - - Fuel (minimum grade aviation gasoline) 91/96 - - - - Lubricating oil Lycoming Spec. No. 301-G** - - - - Bore and stroke, in. 5.125 x 4.375 - - - - Displacement, cu. in. 361 - - - - Compression ratio 8.5:1 - - - - Weight (dry), lb. 270 269 272 C.G. location (dry with starter and generator installed) From front fact of power takeoff flange, in. 14.24 - - - - Off crankshaft centerline, in. 1.62 below & .05 right - - - - Propeller shaft Flange type power takeoff - - - - Crankshaft dampers and balancers None - - - - Carburetion or Fuel Injection MA-4-5+ MA-4 5AA+ Fuel Injector, RSA-5AD1# Ignition, Dual * Two S4LN-21* S4LN-200*, S4LN-204* - - ** See latest edition of Lycoming Service Instruction 1014 + Volare formerly PAC, formerly Marvel-Schebler # PAC formerly Bendix *TCM formerly Bendix "- -" indicates "same as preceding model" "—" indicates "does not apply" 1E1 2 Model Lycoming VO-360-A1A VO-360-A1B, -B1A IVO-360-A1A Timing, °BTC 25 - - - - Spark plugs See NOTE 6 - - - - Oil sump capacity, qt. 6.0 - - - - Minimum usable oil, qt. Engine position Vertical 1.5 - - - - 10° from vertical 1.5 - - - - 20° from vertical 1.5 - - - - 30° from vertical 2.0 - - - - NOTES 1,2,3,4,5,6,7 - - - - CERTIFICATION BASIS Date Type Certificate Regulations & Amendments Model Date of Application No. 1E1 Issued/Revised CAR 13 effective June 15, 1956 VO-360-A1 A November 30, 1956 January 29, 1959 As amended by 13-1, 13-2, and 13-3 VO-360-A1B August 17, 1960 August 23, 1960 VO-360-B1A March 26, 1962 May 18, 1962 IVO-360-A1A April 16, 1963 May 17, 1963 Production basis Production Certificate No. 3 NOTE 1. Maximum permi ssible temperature: Cylinder head Cylinder Oil (well type thermocouple) base inlet 500° 325°F 245°F NOTE 2. Min. Max. Fuel Pressure Limits For VO-360 series at carb. inlet 0.5 p.s.i. 8.0 p.s.i. For IVO-360-A1A at injector inlet 14.0 p.s.i. 45.0 p.s.i. Oil Pressure Limits (normal operation) 60 p.s.i. 90 p.s.i. (idling) 15 p.s.i. — Starting and warm-up — 100 p.s.i. NOTE 3. The following accessory provisions are available: Accessory VO-360- A1A -A1B -B1A IVO- 360-A1A *Direction of Rotation **Speed Maximum Torque (in. -lb) Cont. Static Maximum Overhang Moment (in. -lb.) Starter X X X — CC 13.556:1 — 450 150 Starter — # # X CC 16.556:1 — 450 150 Generator X X X X C 1.910:1 60 120 175 Generator — # # # C 2.500:1 60 120 175 Alternator # # # # C 3.20:1 60 120 175 Vac. Pump X X # # CC 1.300:1 70 450 25 Tachometer X X X X C 0.500:1 7 50 5 Fuel Pump X X X X CC 1.300:1 70 450 25 X - Standard # - Optional *"C" - Clockwise, "CC" - Counter Clockwise facing engine pad. ** Speed - Times crankshaft RPM. "- -" indicates "same as preceding model" "—" indicates "does not apply" 3 1E1 NOTE 4. This engine is approved for helicopter app lication and operation in a vertical installation. NOTE 5. The above engine models incorpor ate additional characteristics as follows: VO-360 Models Characteristics VO-360-A1A Basic model. TCM S4LN magnetos. VO-360-A1B Same as -A1A except has altitude compensated carburetor and retard breaker magnetos. VO-360-B1A Same as -A1B except has piston cooling oil jets. IVO-360-A1A Similar to VO-360-B1A except has fuel injector. NOTE 6. Spark plugs: See latest revision of Lycomi ng Service Instruction No. 1042 for approved equipment. NOTE 7. Starters, generators, and alternat ors approved for use on these engines are listed in the latest revision of Lycoming Service Instruction No. 1154. ...END...