TCDS E-274

Page No. 01 02 03 04 05 06 07 Rev. No. 22 22 16 16 20 14 17 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E-274 Revision 22 Lycoming Engines O-320-A1A, -A1B, -A2A, -A2B, -A2C, -A2D, -A3A, -A3B, -A3C, -B1A, -B1B, -B2A, -B2B, -B2C, -B3A, -B3B, B3C, -B2D, -B2E -C1A, -C1B, -C2A, -C2B, -C2C, -C3A, -C3B, -C3C, -D1A, -D1B, -D1C, -D1D, -D1F, -D2A, -D2B, -D2C, -D2F, -D2G, -D2H, -D2J, -D3G, -E1A, -E1B, -E1C, -E1F, -E1J, -E2A, -E2B, -E2C, -E2D, -E2F, -E2G, -E2H, -E3D, -E3H, -H1AD, -H1BD, -H2AD, -H2BD, -H3AD, -H3BD April 30, 2013 TYPE CERTIFICATE DATA SHEET NO. E-274 Engines of models described herein conforming with this data sheet, (which is part of type certificate No. 274) 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 Williamsport, Pennsylvania 17701 Type Certificate Holder Record Textron Lycoming/Subsid iary of Textron, Inc. transferred TC E-274 to Lycoming Engines, An Operating Division of AVCO Corporation on December 17, 2003 E-274 Page 2 of 7 Model O-320-A1A, -A1B, -A2A, -A2B, -A2C, -A2D, -A3A, -A3B, -A3C, -C1A, -C1B, -C2A, -C2B, -C2C, -C3A, -C3B, -C3C, -E1A, -E1B, -E1C, -E1F -E1J, -E2A, -E2B, -E2C, -E2D, -E2F, -E2G, -E2H, -E3D, -E3H O-320-H1AD, -H1BD, -H2AD, -H2BD, -H3AD, -H3BD O-320-B1A, -B1B, -B2A, -B2B, -B2C, -B2D, -B3A, -B3B, -B3C, -B2E -D1A, -D1B, -D1C, -D1D, -D1F, -D2A, -D2B, -D2C, -D2F, -D2G, -D2H, -D2J, -D3G Type 4H0A - - - - Rating Max. continuous, h.p. r.p.m. full throttle at: Sea level pressure altitude 150-2700 160-2700 160-2700 Takeoff, h.p. r.p.m. full throttle at: Sea level pressure altitude 150-2700 (See NOTE 8) 160-2700 See NOTE 8 160-2700 (See NOTE 8) Fuel (Minimum grade aviation gasoline) 80/87* 100 or 100LL* 91/96* Carburetion** LVC-5-4PA - - - - (-B2D,-D1D- LHC-6-6BPA) Pressure limits See NOTE 2 - - - - Pump Drive See NOTE 3 - - - - Oil, Lubrication (Lubricants should conform to the Lycoming Specification specifications as listed or to No. 301-F - - - - subsequent revisions thereto) Oil sump capacity, Qt. 8 6 8 Usable oil sump capacity, Qt. 6 4 6 Temperature Limits See NOTE 1 - - - - Pressure Limits See NOTE 2 - - - - Ignition Dual magnetos See NOTE 9 - - - - Timing BTC 25 25 25 Spark plugs See NOTE 4 - - - - Compression Bore and stroke, in. 5.125 x 3.875 - - - - Displacement, cu. in. 319.8 - - - - Compression ratio 7.00:1 9.00:1 8.50:1 Weight (dry) Lb. See NOTE 9 - - - - C.G. location (dry) From face of propeller mounting flange, in. 14.25 14.57 14.25 14.25 14.70 Off propeller shaft C.L., in. .97 Below .71 Below .97 Below .97 Below .79 Below .03 Right .12 Left (-E2D, -E3D, -E2H, -E3H) .00 (on C.L.) .03 Right .11 Left (-B2D, -D1D) Propeller shaft-specification A.S. 127 Integral flanged hub SAE 2 modified - - - - Crankshaft dampers (torsional) ⎯ ⎯ ⎯ * See latest revision of Lycoming Service Instruction 1070 for alternate fuel grades ** See latest revision of Lycoming Service Instruction 1523 for alternate carburetors. NOTES: "- -" indicates "same as preceding model." "—" indicates "does not apply." Page 3 of 7 E-274 Regulations & Amendments Models Date of Application Date T.C. No. 274 Issued/Revised CAR 13 effective March 5, 1952 O- 320, October 13, 1952 July 28, 1953 O-320-A1A As amended by 13- & 13-2 O-320-A2 A October 21, 1954 October 28, 1954 CAR 13 effective June 15, 1956 O-320-B1A, -B2A May 24, 1957 July 25, 1957 As amended by 13-1 & 13-2 O-320-A1B, -A2B, -A3A, -A3B, -B1B, -B2B, -B3A, -B3B February 1959 March 23, 1959 13-3 O-320-C2A, -C2B, -C3A, -C3B January 18, 1960 February 11, 1960 O-320-A2C, -A3C, -B2C, -B3C March 29, 1960 April 27, 1960 13-3 O-320-D1A, -D2A O-320-D1B, -D2B O-320-E1A, -E2A, -E1B, -E2B November 1, 1961 December 8, 1961 January 26, 1962 November 30, 1961 December 20, 1961 February 15, 1962 13-4 O-320-C1A, -C1B, -C2C, -C3C O-320-E2C O-320-D2C O-320-E2D O-320-E1C O-320-E1F, -E2F O-320-E2G O-320-E3D O-320-D1F, -D2F O-320-E2H, -E3H O-320-D1C O-320-A2D O-320-D2G O-320-D1D O-320-E1J O-320-H1AD, -H1BD, -H2AD, -H2BD O-320-H3AD, -H3BD O-320-D3G O-320-D2H O-320-D2J January 22, 1963 November 11, 1965 April 14, 1966 December 19, 1966 May 27, 1969 July 24, 1970 December 11, 1970 January 26, 1971 February 26, 1971 July 15, 1971 September 14, 1971 March 2, 1972 March 14, 1974 March 27, 1974 January 21, 1975 September 10, 1975 June 1, 1976 August 11, 1976 May 17, 1977 December 28, 1978 March 3, 1964 November 24, 1965 May 2, 1966 January 27, 1967 June 4, 1969 August 3, 1970 December 23, 1970 February 3, 1971 March 3, 1971 July 27, 1971 September 30, 1971 March 14, 1972 March 21, 1974 May 1, 1974 January 29, 1975 January 26, 1976 June 4, 1976 August 23, 1976 May 20, 1977 January 4, 1979 O-320-B2D June 11, 1992 June 25, 1992 O-320-B2E January 30, 2003 July 8, 2003 Production basis Production Certificate No. 3 NOTE 1. Maximum permissible temperatures are as follows: Cylinder head 500°F (well-type thermocouple) Cylinder barrel 325°F Oil inlet 245°F NOTE 2. Fuel pressure limits: Minimum 0.5 p.s.i. - Maximum 8 p.s.i. For gravity feed systems, minimum fuel pressure is 15.0 inches of gasoline differential pressure across the fuel inlet fitting on 0-320-D2J. Oil pressure limits: (Normal operation) Minimum 55 p.s.i. - Maximum 95 p.s.i. (Idling) 25 p.s.i. (Starting and warm- up) Maximum 115 p.s.i. E-274 Page 4 of 7 NOTE 3. The following accessory drive provisions are available: O-320 Models Accessory All Models not otherwise Shown -H1AD, -H1BD, -H3AD, -H3BD -A2D, -E2D, -E2G, -E2H, -E3D, -E3H -H2AD, -H2BD Rotation facing Drive Pad Speed Ratio to Crankshaft Max. Torque (in.-lb.) Cont. Static Max. Overhang Moment (in.-lb.) Starter * * * * CC 13.556:1 — 450 150 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 1.910:1 60 120 175 Alternator ** * * * C 3.250:1 60 120 175 Vacuum Pump * — * — CC 1.300:1 70 450 25 Vacuum Pump — * — ** CC 1.313:1 70 450 25 Hydraulic Pump — — — — C 1.300:1 100 800 40 Tachometer * * * * C .500:1 7 50 5 Prop. governor — — — — C .895:1 125 1200 40 Prop. governor * — — — C .866:1 125 1200 40 Fuel Pump (Plunger) ** ** * ** — .500:1 — — 10 Fuel Pump ** ** — ** CC 1.000:1 25 450 25 Optional Dual Drive Mounting on Vacuum Pump Drive Pad Vacuum Pump ** — — — CC 1.300:1 70 450 6 Hydraulic Pump ** — — — CC 1.300:1 Total Total 10 or Vacuum Pump ** — — — CC 1.300:1 70 450 6 Vacuum Pump — ** — ** CC 1.313:1 70 450 6 Prop. Governor ** — — — CC 1.300:1 Total Total 10 Prop. Governor — ** — ** C 1.000:1 125 1200 40 "—" Does not apply *Standard **Optional "C" Clockwise "CC" Counter Clockwise Accessory -D1C -D1D -D1F -E1E -E1J -B2E -D2F -E2F -B2D -D2G -D2H -D3G -D2J Rotation facing Drive Pad Speed Ratio to Crank shaft Max. Torque (in.-lb.) Cont. Static Max. Overhang Moment (in.-lb.) Starter * * * * * CC 13.556:1 — 450 150 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 1.910:1 60 120 175 Alternator * * * * * C 3.250:1 60 120 175 Vacuum Pump ** ** ** * * CC 1.300:1 70 450 25 Vacuum Pump — — — — — C 1.910:1 60 120 175 Hydraulic Pump — * ** — — C 1.300:1 100 800 40 Tachometer * * * * * C .500:1 7 50 5 Prop. governor — * — — — C .895:1 125 200 40 Prop. governor * — — — — C .866:1 125 1200 40 Fuel Pump (Plunger) * ** * * — — .500:1 — — 10 Fuel Pump — — — — — CC 1.000:1 25 450 25 Optional Dual Drive Mounting on Vacuum Pump Drive Pad Vacuum Pump ** — — ** ** CC 1.300:1 70 450 6 Hydraulic Pump ** — — ** ** CC 1.300:1 Total Total 10 or Vacuum Pump ** — — ** ** CC 1.300:1 70 450 6 Vacuum Pump — — — — — CC 1.313:1 70 450 6 Prop. Governor ** — — — ** CC 1.300:1 Total Total 10 Prop. Governor — — — — — C 1.000:1 125 1200 40 "—" Does not apply *Standard **Optional "C" Clockwise "CC" Counter clockwise Page 5 of 7 E-274 NOTE 4. Spark plugs approved for use on these engines are listed in the latest revision of Lycoming Service Instruction No. 1042. NOTE 5. The above models incorporate additional characteristics as follows: O-320 Models Characteristics O-320 Basic model - four cylinder, horizonta lly opposed air cooled, direct drive with automotive type generator and starter, provides for single acting controllable pitch propeller. O-320-A1A Same as O-320, mode l designation change only. O-320-B1A Same as O-320-A1A except for co mpression ratio, fuel grade and rating. O-320-A1B, -B1B Same as O-320-A1A and -B1A respec tively except have straight bore carburetor riser. O-320-A2A, -A2B, and -B2A, -B2B Same as O-320-A1A, -A1B, -B1A and B1B respectively except have no provisions for controllable pitch propellers. O-320-A2D Same as O-320-E3D except crankcase m achined for conical instead of Dynafocal mounts. O-320-A3A, -A3B, -B3A, and -B3B Same as O-320-A1A, -A1B, -B1A, and -B1B respectively except have provisions for 7/16" propeller attaching bolts. O-320-A2C, -A3C Same as O-320-A2B and -A 3B respectively, except for magnetos. O-320-B2C, -B3C Same as O-320-B2B and -B 3B respectively, except for magnetos. O-320-B2D Same as O-320-D1D except coni cal engine mounts and no prop governor O-320-B2E Similar to –B2B except carburet or located same as O-320-D models O-320-C2A, -C2B, -C3A, -C3B Same as O-320-B2A, -B2B, -B3A and B3B respectively, except have O-320-A series, low compression pistons, reduced ratings and lower grade fuel requirements. O-320-C1A, -C1B, -C2C, -C3C Same as O-320-B1A, -B1B, -B2C, -B3C respectively, except have been converted to low compression pistons. O-320-D1A Same as O-320-B3B except ha s provisions for dynafocal mounts. O-320-D1B, -D2B Same as O-320-D1A and -D2A receptively, except for magnetos. O-320-D1C Identical to O-320-D2C except has provision for controllable pitch propellers. O-320-D1D Similar to O-320-D1A except incorporates Slick instead of Bendix magnetos and has a horizontal carburetor and induction housing O-320-D1F Identical to O-320-E1F except is equippe d with high compression pistons and has higher H.P. rating. O-320-D2A Same as O-320-D1A except has no pr ovisions for controllable pitch propellers O-320-D2C Similar to model O-320-D2A except for magnetos. O-320-D2F Similar to O-320-D1F but does not have provisions for controllable pitch propeller. O-320-D2G Identical to O-320-D2A except incorporat es Slick instead of Bendix magnetos and 7/16 instead of 3/8 prop. flange bolts. E-274 Page 6 of 7 O-320 Models Characteristics O-320-D2H Same as D2G except has O-320-B sump and intake pipes and provision for AC type fuel pump. O-320-D2J Similar to O-320-D2G except is equipped with two Slick impulse coupling magnetos and the prop. governor pad, fuel pump and governor pads on accessory housing are not machined. O-320-D3G Same as D2G except has 3/8 in prop. attaching bolts. O-320-E1A, -E2A Same as O-320-D1A and -D2A resp ectively, except have lower compression ratio and performance. O-320-E1B, -E2B Same as O-320-E1A and -E2A respectively except for magnetos. O-320-E1C, -E2C Same as O-320-E1A and -E2A respectively except have 1200 series magnetos. O-320-E1F Similar to O-320-E1C except has propeller governor drive located on left front of crankcase instead of on the accessory housing. O-320-E1J Same as O-320-E1F except is equipped with Slick magnetos. O-320-E2D Similar to O-320-E2A except has no pr ovisions for controllable pitch propeller. O-320-E2F Identical to O-320-E1F including provisi ons for propeller governing but does not contain propeller governor drive gears. O-320-E2G Similar to O-320-E2D except is equipped with O-320-A series sump and intake pipes. O-320-E2H Identical to O-320-E2D except incorporates Bendix instead of Slick magnetos. O-320-E3D Identical to O-320-E2D except has provisi ons for .375 in. propeller flange bolts instead of .4375 in. flange bolts. O-320-E3H Identical to O-320-E2H except has .375 in . propeller flange bushings instead of .4375 in. flange bushings. O-320-H1AD Integral accessory section crankcase, front mounted fuel pump external mounted oil pump and D4RN-2O21 impulse coupling dual magneto. O-320-H2AD Same as -H1AD but with fixed pitch propeller. O-320-H3AD Same as -H2AD but with 3/8 in. instead of 7/16 in. propeller flange bolts. O-320-H1BD Same as -H1AD but with D4RN-2200 retard breaker dual magneto. O-320-H2BD Same as -H2AD but with D4RN-2200 retard breaker dual magneto. O-320-H3BD Same as -H3AD but with D4RN-2200 retard breaker magneto. NOTE 6. These engines incorporate provisions for absorbing pr opeller thrust in both tractor and pusher type installations. NOTE 7. These engines are approved for horiz ontal helicopter application and operation. NOTE 8. The O-320-E2A and -E2C have alternate rating of 140 hp. @ 2450 r.p.m., the O-320-D series have alternate ratings of 150 hp at 2500 r.p.m. and 155 hp. at 2600 r.p.m.; the O-320-H series have an alternate rating of 150 h.p. at 2600 r.p.m. Page 7 of 7 E-274 NOTE 9. O-320- Weight (dry) and ignition, dual. Models Weight Lb. Magnetos * -A1A, -A1B, -A2A-A2B, -A3A, -A3B 244 S4LN21, S4LN20 ( TCM)+ -A2D 249 4251, 4250 (Slick) -A2C, -A3C 243 S4LN-200, S4LN-204 ( TCM) -B1A, -B1B, -B2A 250 S4LN-21, S4LN-20 ( TCM) -B2B, -B3A, -B3B 250 S4LN-21, S4LN-20 ( TCM) -B2C, -B3C 249 S4LN-200, S4LN-204 ( TCM) -B2D 283 4373, 4370 (Slick) -B2E 250 4373, 4370 (Slick) -C1A, -C1B, -C2A 250 S4LN-21, S4LN-20 ( TCM) -C2B, -C3A, -C3B 250 S4LN-21, S4LN-20 ( TCM) -C2C, -C3C 249 S4LN-200, S4LN-204 ( TCM) -D1A, -D2A 255 S4LN-21, S4LN-20 ( TCM) -D1B, -D2B 254 S4LN-200, S4LN-204 ( TCM) -D1C, -D2C 256 24LN-1227, SRLN-1209 ( TCM) -D1D 253 4251, 4250 (Slick) -D1F, -D2F 255 S4LN-1227, S4LN-1209 ( TCM) -D2G 251 4251, 4250 (Slick) -E1A, -E2A 244 S4LN-21, S4LN-20, S4LN-204 ( TCM) -E1B, -E2B 243 S4LN-200, S4LN-204 ( TCM) -E1C, -E2C 245 S4LN-1227, S4LN-1209 ( TCM) -E1F, -E2F 248 S4LN-1227, S4LN-1209 ( TCM) -E2D 249 4251, 4250 (Slick) -E2G 249 4251, 4250 (Slick) -E2H 252 S4LN-21, SRLN-20 ( TCM) -E3D 249 4250, 4251 (Slick) -E3H 252 S4LN-21, S4LN-20 ( TCM) -E1J 245 4251, 4250 (Slick) -D2H 251 4251, 4250 (Slick) -D2J 255 (2) 4251 (Slick) -D3G 251 4251, 4250 (Slick) -H1AD 253 D4RN-2021 ( TCM) -H2AD 253 D4RN-2021( TCM) -H3AD 253 D4RN-2021 ( TCM) -H1BD 253 D4RN-2200 ( TCM) -H2BD 253 D4RN-2200 ( TCM) -H3BD 253 D4RN-2200 ( TCM) * For alternate magnetos see latest revision of Lycoming Service Instruction 1443 + TCM formally Bendix NOTE 10. All models equipped with one impulse coupling magneto may use two impulse coupling magnetos as optional equipment. Starters, generators and alternators approved for use on the engines are listed in the latest revision of Lycoming Service Instruction No. 1154. ----END----