TCDS 1E14

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1E14 Revision 5 Lycoming Engines TVO-540-A1A TIVO-540-A2A December 17, 2003 TYPE CERTIFICATE DATA SHEET NO. 1E14 Engines of models described herein conforming with this data sheet (which is a part of type certificate No. 1E14) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Civil Air Regulations/Federal Aviation 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 William sport, Pennsylvania 17701 Type Certificate Holder Record Textron Lycoming, AVCO Corporation transferred TC E14EA to Lycoming Engines, An Operating Division of AVCO Corporation on December 17, 2003 Model Ly coming TVO-540-A1A TIVO-540-A2A Type 6HOA Vertical-Mounted Direct Drive Turbosupercharged Rating (See NOTE 5) Maximum continuous, hp., r.p.m. 305-3200 315 @ 3200 Takeoff, hp., r.p.m. 305-3200 315 @ 3200 . Fuel (Minimum grade aviation gasoline) 100/130 - - Lubricating oil (Lubricants should conform to the MIL-L-6082 or - - specifications as listed or to subsequent revisions Lycoming Spec. No.301-E thereto.) Bore and stroke, in. 5.125 x 4.375 - - Displacement, cu. in. 541.5 - - Compression ratio 7.3:1 - - Weight (dry), lb. 499 507 C.G. location (dry and in horizontal position) From front face of crankcase, in. 16.00 - - Off crankshaft C.L., in. 1.53 below - - & 0.60 left - - Propeller shaft Flangs type power takeoff - - Crankshaft dampers and balancers None - - Carburetion Marvel-Schebler MA-6AA - - Fuel injection - - Bendix RS-5BD2 Turbosupercharger AiResearch model T-1112 - - Ignition, dual Scintilla S6RN-200 - - & S6LN-204 - - Timing, °BTC 25 - - Spark plugs see NOTE 4 - - Oil sump capacity Dry sump - - NOTES 1, 2, 3, 4, 5, 6 1, 2, 3, 4, 5, 6 “- -” indicates “same as preceding model” “—” indicates “not applicable” Page No. 1 2 3 Rev. No. 5 4 4 1E14 Page 2 of 3 Certification basis Date Type Certificate Regulations & Amendments Model Date of Application No.1E14 Issued or Amended CAR 13 effective June 15, 1956 As amended by 13-1, 13-2, 13-3 TVO-540-A1A March 17, 1961 October 18, 1961 13-4 TIVO-540-A2A March 5, 1963 August 16, 1963 Production basis: Production Certificate No. 3 NOTE 1. Maximum permissible temperatures: TVO-540-A1A TIVO-540-A2A Cylinder head (well type thermocouple) 500°F 500°F Cylinder base 300°F 305°F Oil inlet 235°F 235°F Carburetor inlet air 345°F — Fuel injector inlet air — 320°F Exhaust gas 1650°F 1650°F (Turbo inlet shown on Lycoming Drawing No.___) (63156) (63203) Compressor temperature rise, maximum 340°F 240°F NOTE 2. Fuel, oil and air pressure limits: Max. Min. Idle Fuel pressure limits p.s.i. (Above car buretor or fuel injector inlet air pressure.) TIVO-540-A2A (at inlet to injector) 45 29 — TWO-540-A1A (at inlet to carburetor) 8 4 Oil pressure limits p.s.i. 70 50 25 Carburetor inlet air pressure in. Hg.(TWO-540-A1A) 39.5 — — Fuel injector inlet air pressure in. Hg. (TIVO-540-A2A) 40.0 Manifold pressure in. Hg. (TVO-540-A1A) 34.5 Manifold pressure in. Hg. (TIVO-540-A2A) 36.0 NOTE 3. The following accessory provisions are incorporated: Rotation Speed Ratio Max.Overhand Facing To Maximum Torque Moment Accessory Drive Pad Crankshaft (in. - lb.) (in. - lb.) Continuous Static Starter C 1.000:1 - 12,000 300 Starter (opt.) Generator* C 2.600:1 500 2,200 400 Generator (opt.) Fuel pump CC .803:1 25 450 25 Vacuum Pump C 1.219:1 200 800 25 Hydraulic Pump C 1.083:1 400 1,650 75 Tachometer CC .500:1 7 50 - “C” = Clockwise, “CC” = Counter-clockwise *Not available as generator drive when fitted with hand crank starter jaw. Page 3 of 3 1E14 NOTE 4. This engine is approved for helicopter appli cation and operation in a vertical mount installation. NOTE 5. This engine is equipped with an AiResearch Model T-1112 turbosupercharger and integral automatic power control which makes standard dry, sea level ra tings available at other than standard conditions up to critical altitudes. Performance data for this engine are presented on Lycoming Curve Nos. (12821 - TVO-540) & (12930-A - TIVO-540). The turbocharger control is servo-operated from eith er engine oil or an external supply of MIL-H-5606 hydraulic fluid at a pressure of 60-70 p.s.i. Th is control is not equipped to use “Skydrol” fluid. The turbocharger meets the containment require ments of CAR 13.116 and does not require external protection. NOTE 6. The following spark plugs are approved as shown: TVO-540 TIVO-540 AC SR83P, HSR83P, SR87, HSR87 HSR86L, HSR87LI, HSR87LP, 171, 181 271, 281, 281IR, 273, 283, 293 Auto Lite SH26, SH260, PH26, PH260 PL300, PL350 BC 485S, RB955S RB39R Champion REM-38E, RHM-38E REB36W, RHB36P, RHB36W, REB37N REM-38P, RHM-38P RHB37E, RHB37N, 32P, 32W, 32E Lodge - RS35-3R, RS35-4R ...END...