TCDS E16EA

Page No. 1 2 3 Rev. No. 7 7 7 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E16EA Revision 7 Lycoming Engines TIO-360-A1A TIO-360-A1B TIO-360-A3B6 TIO-360-C1A6D January 31, 2020 TYPE CERTIFICATE DATA SHEET NO. E16EA Engines of models described herein conforming with this data sheet (which is a part of type certificate No. E16EA) and other approved data on file with the Federal Aviation Administration meet the minimum standards for use in certification aircraft i n 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 manual and other approved instructions. Type Certificate Holder Lycoming Engines An Operating Division of AVCO Corporation 652 Oliver Street Williamsport, Pennsylvania 17701 Type Certificate Holder Record AVCO Lycoming Williamsport Division, AVCO CORP. Williamsport PA transferred TC E16EA to Lycoming Engines, An Operating Division of AVCO Corporation on November 04, 2010 Model Lycoming TIO-360-A1A, -A1B TIO-360-A3B6 TIO-360-C1A6D Type 6H0A Direct Drive Turbocharged Rating (See NOTE 4) Maximum continuous hp., r.p.m., in Hg. at: Standard density critical alt. ft. 200-2575-37.5-15,000 200-2575-47.5-25,000 207-2575-44.0-10,000 Standard density sea level alt. ft. 200-2575-34.0-S.L. 200-2575-34.1-S.L. 210-2575-44.0-S.L. Takeoff (5 min.), hp. r.p.m., in. Hg. Standard density critical alt. ft. 200-2575-37.5-15,000 200-2575-47.5-25,000 207-2575-44.0-10,000 Standard density sea level alt. ft. 200-2575-34.0-S.L. 200-2575-34.1-S.L. 210-2575-44.0-S.L. Fuel (minimum grade aviation gasoline) Lycoming Service Instruction 1070 - - - - Lubricating oil Lycoming Service Instruction 1014 - - - - Bore and stroke, in. 5.125 x 4.375 - - - - Displacement, cu. in. 361.0 - - - - Compression Ratio 7.30:1 - - - - Weight (dry), lb. 355 364 348 C.G. Location (with starter and alternator installed) 18.51 18.01 15.27 From front face of prop mounting flange, in. 1.35 below 1.45 below 0.53 below Off crankshaft C.L., in. 0.15 left 0.01 left 0.88 right Propeller shaft flange, SAE No. type 2 modified (AS 127) - - - - Crankshaft dampers (torsional) See NOTE 9 - - - - Fuel injection + RSA-5AD1 - - LFR-NNSS5 "- -" Indicates "same as preceding model" "—" Indicates "does not apply" + For alternate fuel injectors see latest revision of Lycoming Service Instruction 1532 2 E16EA Model Lycoming TIO-360-A1A, -A1B TIO-360-A3B6 TIO-360-C1A6D Turbocharger HET+ T04 - - HET+ 3BT1EE10J2 Ignition, dual*# TCM S4LN-1208, S4LN-1209 - - D4LN-3000 Ignition timing °BTC 20 - - - - Spark plugs See NOTE 6 - - - - Oil Sump Capacity, qt. 8 - - - - Usuable oil, qt. 6 - - - - (30° nose up or down) NOTES 1,2,3,4,5,6,7,8,9 - - - - "- -" Indicates "same as preceding model." "—" Indicates "does not apply." +Hartzell Engine Technologies (HET) formerly Kelly Aerospace formerly AiResearch, formerly Roto-Master * For alternate ignition systems see latest revision of Lycoming Service Instruction 1443. # Teledyne (TCM) formally Bendix CERTIFICATION BASIS. Date Type Certificate Regulations & Amendments Model Date of Application E16EA Issued/Revised FAR 33, 33-1 effective TIO-360-A1A March 10, 1967 November 20, 1967 February 1, 1965, as amended TIO-360-A1B November 13, 1967 November 20, 1967 by 33-2 TIO-360-A3B6 January 18, 1972 February 16, 1972 33-3 TIO-360-C1A6D March 7, 1983 March 16, 1983 Production basis: Production Certificate No. 3 NOTE 1. Maximum permissible temperatures: Cylinder head (well type thermocouple) 500°F Cylinder base NOTE 5 Oil inlet 245°F Fuel injector inlet air 400°F Exhaust gas (turbo inlet at location shown on Lycoming installation Drawing) 1650°F NOTE 2. Fuel, Air, and Oil Pressure Limits: Min. Max. Idle (min) Idle Cutoff Fuel pressure limits (above fuel injector inlet air pressure) at inlet to engine fuel injector -A1A, -A1B, -A3B6 20 p.s.i. 45 p.s.i. 12 p.s.i. - -C1A6D 22 p.s.i. 65 p.s.i. 12 p.s.i. - at inlet to engine fuel pump -A1A, -A1B -2 p.s.i. 50 p.s.i. - Max. 55 p.s.i. -A3B6, -C1A6D -2 p.s.i. 65 p.s.i. - - Fuel injector inlet air pressure -A1A, -A1B - 40 in. Hg. - -A3B6 - 47.5 in. Hg. - Manifold pressure (cumulative total with altitude adjustment) -A1A, -A1B - 40 in. Hg. - -A3B6 - 47.5 in. Hg. -C1A6D - 44.0 in. Hg. - Oil pressure limits: Oil pressure may be measured at either the accessory housing or top of crankcase for TIO-360-A models. Accessory Housing OR Top of Crankcase Min. Max. Idle Min. Max. Idle Normal 55 p.s.i. 95 p.s.i. 25 p.s.i. 49 p.s.i. 89 p.s.i. 22 p.s.i. Start, warm-up, taxi & takeoff - 115 p.s.i. - - 109 p.s.i. - 3 E16EA NOTE 3. The following accessory provisions are available: Accessory TIO-360 -A1A, - A1B TIO- 360 -A3B6 TIO- 360 -C1A6D Rotation Facing Drive Pad Speed Ratio to Crankshaft Maximum Torque (in. -lb.) Maximum Overhang Moment (in. lb.) Continuous Static Starter■ * * ** CC 16.556:1 - 450 150 Generator■ * - - C 1.910:1 60 120 175 Generator■ ** - - C 2.500:1 60 120 175 Alternator■ ** * * C 3.250:1 60 120 175 Vacuum Pump● * * * CC 1.300:1 70 450 25 Tachometer● * * * C 0.500:1 7 50 5 Propeller * - ** C 1.182:1 125 1200 40 Governor (.895:1 for -C1A6D) Fuel pump * * * CC 1.000:1 25 450 25 Optional Dual Drive Mounting on Vacuum Pump Drive Pad: -A1A, -A1B Vacuum pump ** - ** CC 1.300:1 70 450 6 Hydraulic pump ** - ** CC 1.300:1 Total Total 10 (C for -C1A6D) * Standard "C" = Clockwise "CC" = Counter Clockwise **Optional ■ These accessories are optional, see latest revision of Lycoming Service Instruction 1154 for the approved alternates. ● These drives are optional and accessory pads may be cast over. NOTE 4. The TIO-360-A1A, -A1B and -A3B6 are equipped with a Hartzell Engine Technologies (HET) (formerly Kelly Aerospace) Model T04 and the -C1A6D is equipped with a HET(formerly Kelly Aerospace) 3BT1EE10J2 turbocharger mounted as an integral part of the engine. Performance data for these models are presented by Lycoming Curve Nos. 13079-A1A, A1B; 13224-A3B6; 13430-C1A6D. The turbocharger meets the containment requirements of 14 CFR 33.27 and does not require external protection. NOTE 5. Cylinder base temperature limits are not applicable to engine models which incorporate internal piston cooling oil jets. NOTE 6. Spark plugs approved for use on these engines are listed in the latest revision of Lycoming Service Instructions No. 1042. NOTE 7. These engines incorporate the following similarities or differences: TIO-360-A1A Basic model - four cylinder air cooled, horizontally - opposed direct drive, fuel injected, tuned induction turbocharged engine incorporating internal piston cooling oil jets. TIO-360-A1B Similar to -A1A except has straight tubular casting in induction system without pressure differential door on 14° down fuel injector adapter. TIO-360-A3B6 Similar to -A1B except equipped with one 6.3 order and one 8th order counterweights and has a pressurized ignition system for high altitude operation. TIO-360-C1A6D Similar to TO-360-C1A6D except for LFR-NNSS5 fuel injector instead of LHC-6-6BPA carburetor. NOTE 8. Starters, generators and alternators approved for use on these engines are listed in the latest revision of the Lycoming Service Instruction No. 1154. NOTE 9. Engines of this series incorporate no crankshaft dampers unless the third section of the model designation exhibits a numerical digit in its fourth position, i.e., TIO-360-A3B6. The digit "6" in the fourth position indicates the incorporation of one 6.3 order and one eight order counterweights. ... END ...