TCDS E10NE

* PAGE 1 2 3 4 5 REV. 4 4 4 4 4 LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" "---" NOT APPLICABLE NOTICE: ALL PAGES ARE REFORMATTED. SIGNIFICANT CHANGES, IF ANY ARE BLACK-LINED IN THE LEFT MARGIN. U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E1ONE TCDS NUMBER E10NE REVISION: 4* DATE: March 23, 2007 WYTWORNIA SPRZETU KOMUNIKACYJNEGO (WSK) "PZL-KALISZ" MODELS: ASz-62IR-16 ASz-62IR-M18/K9-BA ASz-62IR-M18 ASz- 62IR-M18/K9-BB Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E10NE) 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 Federal Aviation Regulations, provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. TYPE CERTIFICATE (TC) HOLDER Wytwornia Sp rzetu Komunikacyjnego "PZL-KALISZ" S.A. ul. Czestochowska 140 62-800 Kalisz P o l a n d I. MODELS ASz-62IR-16 ASz-62IR-M18 ASz-62IR-M18/K9-BA ASz-62IR-M18/K9-BB TYPE 9RA, .687:1 reduction gears / clockwise rotation of crankshaft and propeller shaft (viewed from rear), single-speed supercharger. RATINGS Maximum continuous hp, r.p.m., in. Hg., at: Critical pressure altitude (ft.) Sea level pressure altitude Takeoff (5 min.) hp, r.p.m., in. Hg., at: Sea level pressure altitude 812-2100-35.4-4920 793-2100-35.4-S.L 967-2200-41.3-S.L - - - - - - 954-2150-41.3-4920 917-2150-41.3-S.L. 1000-2200-45.2-S.L. FUEL Minimum grade aviation fuel Aviation gasoline 91 octane - - - - LUBRICATING OIL Mineral aircraft engine oils with a nominal viscosity of 20 cSt at 100ºC or 100 SUS at 210ºF and a minimum viscosity index of 80. Also refer to the Installation Manual. - - TCDS E10NE PAGE 2 I. MODELS (Continued) ASz-62IR- 16 ASz-62-IR-M18 ASz-62IR-M18/K9-BA /K9-BB COMPRESSION Bore and stroke, in. Displacement, cu. in. Compression ratio 6.10 X 6.87 1823 6.4:1 - - - - - - - - - - - - WEIGHT (Max.dry) (lb) 1302 1274 1280 CENTER OF GRAVITY (in) Aft of cylinder centerline Above crankshaft centerline 0.75 0.45 0.55 0.51 - - - - CRANKSHAFT DAMPERS Two mobile counterweights, 4.5 order, on rear arm of crankshaft. PROPELLER SHAFT Spline - - - - CARBURETION AKM-62IRA - - - - FUEL PUMP BNK-12BK - - - - IGNITION Two BSM-9 or BSM-9F Magnetos - - - - IGNITION TIMING, ºBTDC Right Left 20º ± 0.5º 15º ± 0.5º - - - - - - - - SPARK PLUGS Eighteen SD-48BSM or equivalent - - - - NOTES 1-3, 5-8 1-8 1-8 CERTIFICATION BASIS FAR 21.29 and FAR 33, including amendments 1 through 6. Type Certificate E10NE issued/revised: D a t e o f T C Model Date of Application issued/revised ASz-621R-16 02/02/79 12/16/80 ASz-621R-M18 02/02/79 12/16/80 ASz-62IR-M18/K9-BA 09/09/00 10/19/01 ASz-62IR-M18/K9-BB 09/09/00 10/19/01 The General Inspectorate of Civil Aviation of Poland originally type certificated this engine. The FAA validated this product under U.S. Type Certificate Number E10NE. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of Poland. PRODUCTION BASIS FAR 21.500 for production of engines or replacement parts under this type certificate by WSK "PZL-KALISZ" under control of the Republic of Poland General Inspectorate of Civil Aviation (GICA). TCDS E10NE PAGE 3 IMPORT REQUIREMENTS To be considered eligible for installation on U.S. registered aircraft, each new engine to be exported to the United States with the General Inspectorate of Civil Aviation of Poland 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 E10NE, is in a condition for safe operation and has undergone a final operational check. Additional guidance is contained in FAA Advisory Circular 21-23, Airworthiness Certification of Civil Aircraft, Engines, Propellers, and Related Products, imported into the United States. NOTES NOTE 1. Maximum permissible temperatures are as follows: Cylinder head Oil Inlet (gasket type thermocouple) 203ºF max. 3 minutes for oil viscosity 120 SUS at 210ºF 475ºF max. 15 minutes 185 o F max. 3 minutes for other oil types 410ºF no time limit 167 o F no time limit NOTE 2. Fuel and oil pressure limits M a x Min Fuel Pressure (psi) at rated power 4.97 3.55 at idle --- 2.13 Oil pressure at rated rpm 71.7 56.9 at idle --- 21.3 NOTE 3. The following accessory provisions are available: ACCESSORY ASz-62IR-16 ASz-62IR-M18 -M18/K9-BA and -M18/K9-BB Rotation Speed Ratio to Crankshaft Maximum Torque ft. lb. Maximum Overhang Moment ft. lb. Starter RIM-U-24IR Magneto BSM-9 or BSM-9F Carburetor AKM-62IRA Fuel Pump BNK-12BK Oil Pump MSz-8M Oil Pump MSz-8A+filter Centrifugal filter TCM-25 Propeller governor R-9SM2 Generator GSN-3000M Piston Air Compressor AK-50P-12 Hydraulic Pump PLT-2-3 or LUN6102.01-8 Hydraulic Pump PLTZ-15 Vacuum Pump 212CW X X X X --- X X X XX XX --- --- --- --- X X X X X --- --- X XX --- XX XX XX XX CC CC --- CC C C C CC C C C C CC CC 1:1 1.125:1 --- 1:1 1.125:1 1.125:1 3.345:1 1.114:1 2.52:1 0.825:1 2.17:1 2.17:1 1.78:1 1.78:1 795 2.21 --- 1.45 5.21 7.09 1.30 2.60 10.56 4.70 6.00 2.9 43.40 1.23 17.0 2.93 --- 0.44 1.45 9.40 1.81 --- 8.90 1.30 0.94 1.16 4.12 0.293 TCDS E10NE PAGE 4 NOTE 3.(continued) ACCESSORY ASz-62IR-16 ASz-62IR-M18 -M18/K9-BA and -M18/K9-BB Rotation Speed Ratio to Crankshaft Maximum Torque ft.lb. Maximum Overhang Moment ft.lb. Hydraulic Pump PZ-5TC Hydraulic Pump 1P-582 Vacuum Pump 3P-207 --- --- --- XX XX /K9-BA only XX /K9-BA only C C CC 0.825:1 1.6986:1 1.787:1 --- 9.4 --- 0.72 1.31 1.13 "X" Standard accessory "XX" Optional accessory "C" clockwise/facing drive pad "CC" counter-clockwise NOTE 4. The ASz-62IR-M18,-M18/K9-BA and -M18/K9-BB do not include provisions for an oil sump metal- chip detector. NOTE 5. Engine rating basis: Ratings are based on static sea level standard conditions of dry inlet air at 59ºF and 29.92 in. Hg., with no aircraft accessory drive loads. Production engines conforming with this type certificate must be capable of producting not less than 100 percent rated power at rated rpm and manifold pressure. NOTE 6. Starter, aircraft accessories, propeller, and engine oil not included in engine wieght. NOTE 7. Time Between Overhaul (TBO) is presente d in the GICA (CACA) - approved ASz-62IR engine manuals. NOTE 8. SERVICE INFORMATION: 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 General Inspectorate of Civil Aviation of Poland. 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. TCDS E10NE PAGE 5 NOTE 9. These models incorporat e the following characteristics: Model Characteristics ASz-62IR-16 Basic model which includes an electric metal chip detector in the oil s u m p . ASz-62IR-M18 Similar to basic model except for the absence of the chip detector and cylinder head and inter-cylinder air deflectors, and modified accessory gearbox drives. ASz-62IR-M18/K9-BB Similar to basic model except for a power increase resulting from an increase of the supercharger drive ratio from 7:1 to 8.325:1, absence of the chip detector and cylinder head and inter-cylinder air deflectors, and modified accessory gearbox drives. ASz-62IR-M18/K9-BA Similar to K9-BB except for inclusion of cylinder head and inter- cylinder air deflectors and modifi ed accessory gearbox that is adapted for hydraulic pump 1P-582 or vacuum pump 3P-207. ---THE END---