TCDS E18EA

* PAGE 1 2 3 4 REV. 5 5 4 4 LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" "---" INDICATES "DOES NOT APPLY" 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 E18EA TCDS NUMBER E18EA REVISION: 6* DATE: April 30, 2013 Franklin Sp. z.o.o. MODELS: FRANKLIN 6AS-350-A 6AS-350-A1 Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E18EA) 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 Franklin Sp. z.o.o. Ul. Chelmińska 208 86-300 Grudziądz Poland TYPE CERTIFICATE (TC) HOLDER RECORD WSK-PZL-RZESZOW transferred TC E18EA to Franklin Sp. z.o.o. on August 17, 2006 I. MODELS 6AS-350-A 6AS-350-A1 TYPE 6HOA Horizontally-Mounted Direct Drive Turbosupercharged 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: Critical pressure altitude, ft. Sea level pressure altitude 235-2800-38.0-15,000 235-2800-39.2-S.L. 250-2800-41.3-12,500 250-2800-42.0-S.L. - - - - - - - - FUEL Minimum grade aviation gasoline 100/130 - - LUBRICATING OIL (Engine and Turbo) MIL-L-6082 or MIL-L-22851 - - OIL GRADE above 40 o F ambient air temp. below 40 o F ambient air temp. SAE 50 SAE 30 - - - - TCDS E18EA PAGE 2 I. MODELS (Continued) 6AS-350-A 6AS-350-A1 COMPRESSION Bore and stroke, in. Displacement, cu. in. Compression ratio 4.625 x 3.5 350 7.4:1 - - - - - - WEIGHT (DRY) (lb) 376.85 - - CENTER OF GRAVITY (in) (with all accessories) Forward from rear face of crankcase Above C.L. of crankshaft 6.31 0.81 6.81 - - PROPELLER SHAFT SAE ARP 502, six 1/2 in. bolts on 4 in. circle - - CARBURETION Marvel-Schebler MA-5 - - TURBOSUPERCHARGER AiResearch TE 0657 - - IGNITION Bendix S6RN-1227 - - TIMING, o BTC 25 SPARK PLUGS AC 273 or Champion RHB32E - - OIL SUMP CAPACITY, QT. 8.8 - - USEABLE OIL, QT. (starting with full tank) 15 o nose down 20o nose up 6.8 5.8 - - - - NOTES 1-6, 8 1-8 CERTIFICATION BASIS FAR 33, effective February 1, 1965, as amended by 33-1. Type Certificate E18EA issued/revised: Date of Date TC Model Application Issued/Revised 6AS-350-A 06/27/66 07/19/68 6AS-350-A1 11/22/68 12/05/68 Reissued to PEZETEL 08/01/79 Reissued to WSK "PZL-RZESZOW" 11/05/81 Reissued to WSK "PZL-RZESZOW" SA 12/8/94 Reissued to Franklin Sp. z.o.o. 04/30/13 The General Inspectorate of Civil Aviation of Poland originally type certificated this engine. The FAA validated this product under U.S. Type Certificate Number E18EA. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of Poland. PRODUCTION BASIS 1. Production Certificate No. 9 for U.S. production. There will be no further production of engines or replacement parts under this production certificate. 2. FAR 21.500 for production of engines or replacement parts under this type certificate by WSK "PZL-RZESZOW" SA under control of the Republic of Poland General Inspectorate of Civil Aviation (GICA). Parts produced under either production basis are eligible to be used interchangeably. TCDS E18EA 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 E18EA, 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 (o F): Cylinder head 400 (bayonet thermocouple) Cylinder base 320 Oil inlet 250 Carburetor inlet air 225 NOTE 2. Fuel pressure limits: Max Min Inlet to fuel pump 14 p.s.i. 10 p.s.i. Oil pressure limits: Idle - - 25 p.s.i. Normal operation - - 55-80 p.s.i. NOTE 3. The following accessory drives are provided: ACCESSORY Type of Drive Pad Rotation Facing Drive Pad Speed Ratio to Crankshaft Max. Torque (in. lb.) Cont. Static Maximum Overhang in. lb. Starter Alternator Tachometer Fuel Pump Propeller Governor Vacuum Pump Special Belt AND 10005 AND 20000 AND 20010 AND 20000 CC CC CC CC CC C 11.44:1 1.6:1 0.5:1 1.65:1 0.847:1 0.847:1 140 100 7 100 125 125 450 800 50 800 825 825 90 --- 5 30 25 25 "C" - clockwise facing engine drive shaft, "CC" - counter clockwise facing engine drive pad Yes NOTE 4. This engine is equipped with an AiResearch model TE 0657 turbosupercharger, which meets the containment requirements of FAR 33.27 and does not require external protection. TCDS E18EA PAGE 4 NOTE 5. Performance data on this engine are presented in Franklin Curve Nos. PE4283 through PE4286 and PE4298. NOTE 6. Power tolerance for production engines is +4%, -3% of the nominal rating. NOTE 7. The 6AS-350-A1 incorporates a geared starter which is located over the crankcase. 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. ---THE END---