TCDS E-239

* PAGE 1 2 3 4 5 REV. 6 4 6 5 5 LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E-239 TCDS NUMBER E-239 REVISION: 6* DATE: April 30, 2013 Franklin Sp. z.o.o. MODELS FRANKLIN 4A4-75-A2, A3, B2, B3 4A4-85-A2, A3, B2, B3 4A4-95-A2, A3, B2, B3 4A4-100-B2, B3 Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number 239) 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 E-239 to Franklin Sp. z.o.o. on August 17, 2006 I. MODELS 4A4-75-A2, A3 4A4-75-B2, B3 4A4-85-A2, A3 TYPE 4HOA RATINGS Maximum Continuous hp, r.p.m., full throttle at: Sea level pressure altitude Takeoff hp, r.p.m., full throttle 75-2050-S.L. 75-2050 75-1950-S.L. 75-1950 85-2350-S.L. 85-2350 FUEL Minimum grade aviation gasoline 73 80 73 COMPRESSION Bore and stroke, in. Displacement, cu. in. Compression ratio 4.5 x 3.5 225 6.5:1 - - - - 7:1 - - - - 6.5:1 TCDS E-239 2 I. MODELS (Continued) 4A4-75-A2, A3 4A4-75-B2, B3 4A4-85-A2, A3 WEIGHT (DRY) (lb) 191, 198 - - - - CENTER OF GRAVITY (in) Forward of rear mounting lug C.L. Below prop. shaft 6.6 4.8 with starter and 15 amp generator 0.93 - - - - - - - - - - - - PROPELLER SHAFT SAE No. 2, flange - - - - CARBURETION Marvel-Schebler MA-5 - - IGNITION (dual) Eisemann LA-4 magnetos, impulse coupling - - - - TIMING, øBTC 28 34 28 SPARK PLUGS Champion 78S, J-10, C- 10, S, AC-SA-47, Auto- Lite A5-B, A4-S - - - - OIL SUMP CAPACITY, QT. 6.5 --- - - NOTES 1 - 4 - - - - II. MODELS 4A4-85-B2, B3 4A4-95-A2, A3 4A4-95-B2, B3 4A4-100-B2, B3 TYPE 4HOA RATINGS Maximum Continuous hp, r.p.m., full throttle at: Sea level pressure altitude Takeoff hp, r.p.m., full throttle 85-2200-S.L. 85-2200 95-2600-S.L. 95-2600 95-2450-S.L. 95-2450 100-2550-S.L. 100-2550 FUEL Minimum grade aviation gasoline 80 73 80 - - COMPRESSION Bore and stroke, in. Displacement, cu. in. Compression ratio 4.5 x 3.5 225 7:1 - - - - 6.5:1 - - - - 7:1 - - - - - - TCDS E-239 3 II. MODELS (Continued) 4A4-85-B2, B3 4A4-95-A2, A3 4A4-95-B2, B3 4A4-100-B2, B3 WEIGHT (DRY) (lb) 191, 198 - - - - - - CENTER OF GRAVITY (in) Forward of rear mounting lug C.L. Below prop. shaft 6.6 4.8 with starter and 15 amp generator 0.93 - - - - - - - - - - - - - - - - - - PROPELLER SHAFT SAE No. 2, flange - - - - - - CARBURETION Marvel-Schebler MA-5 carburetor - - - - - - IGNITION (dual) Eisemann LA-4 magnetos, impulse couplin - - - - - - TIMING, øBTC 34 - - - - - - SPARK PLUGS Champion 78S, J-10, C-10, S, AC-SA-47; Auto-Lite A5-B, A4-S - - - - - - OIL SUMP CAPACITY, QT. 6.5 - - - - - - NOTES 1 - 4 - - - - - - CERTIFICATION BASIS CAR 13 Type Certificate 239 issued/revised: Date of Date TC Model Application Issued/Revised 4A4-75-A2 06/04/45 09/27/45 4A4-75-A3 06/04/45 09/27/45 4A4-75-B2 06/04/45 09/27/45 4A4-75-B3 06/04/45 09/27/45 4A4-85-A2 06/04/45 09/27/45 4A4-85-A3 06/04/45 09/27/45 4A4-85-B2 06/04/45 09/27/45 4A4-85-B3 06/04/45 09/27/45 4A4-95-A2 06/04/45 09/27/45 4A4-95-A3 06/04/45 09/27/45 4A4-95-B2 06/04/45 09/27/45 4A4-95-B3 06/04/45 09/27/45 4A4-100-B2 06/04/45 09/27/45 4A4-100-B3 06/04/45 09/27/45 TC Inactivated 12/05/50 TC Re-activated 01/11/62 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 TCDS E-239 4 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. The General Inspectorate of Civil Aviation of Poland originally type certificated this engine. The FAA validated this product under U.S. Type Certificate Number E-239. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of Poland. 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 E-239, 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 cylinder head, barrel, and oil inlet temperatures, 500øF, 300øF and 230øF, respectively. NOTE 2. The following accessory provisions and typical engine accessories are eligible at the indicated weight increases: ACCESSORY WEIGHT - lbs. Starter: Models - 3 only Auto-Lite, Part No. 10118 Delco-Remy, Part No. 10750 Generator: Models - 3 only Auto-Lite, Part No. 10119 or 11497, 15 amp Delco-Remy, Part No. 17556, 25 amp Fuel Pump: AC Diaphragm type, Part No. 10551 Miscellaneous: Ratio Shielding Fram P 1/2 Filter 16 16 12 16 3 3 --- TCDS E-239 5 NOTE 2. (CONT.) 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 Moment (in. - lb.) Starter None CC 11.444:1 - - 240 30 Generator None CC 1.000:1 12 35 55 Tachometer AND 10005 CC 0.500:1 20 60 2 "C" - Clockwise facing engine drive pad, "CC" - Counterclockwise facing engine drive pad NOTE 3. Eligible with a temporary propeller shaft flange drilled for six 3/8- inch bolts on a 4-inch circle. NOTE 4. 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---