TCDS E6EA

* PAGE 1 2 3 4 5 6 REV. 9 7 9 8 7 8 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 E6EA TCDS NUMBER E6EA REVISION: 9* DATE: April 30, 2013 Franklin Sp. z.o.o. MODELS: FRANKLIN 4A-235-B 4A-235-B31 4A-235-B2 4A-235-B4 4A-235-B3 4A-235-B6 Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E6EA) 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 E6EA to Franklin Sp. z.o.o. on August 17, 2006 I. MODELS 4A-235-B 4A-235-B2 4A-235-B3 4A-235-B31 TYPE 4HOA horizontally-mounted direct drive RATINGS Maximum Continuous hp, r.p.m., at: Sea level pressure altitude Takeoff hp, r.p.m., full throttle at: Sea level pressure altitude 130-2800 130-2800 125-2800 125-2800 123-2800 123-2800 116-2800 116-2800 FUEL (See Note 7) Minimum grade aviation gasoline 100/130 - - - - - - OIL GRADE (See Note 7) above 40øF ambient air temp. below 40øF ambient air temp. all ambient air temp. SAE 50 SAE 30 SAE 15W50 SAE 20W50 - - - - - - - - - - - - - - - - - - - - - - - - TCDS E6EA PAGE 2 I. MODELS (Continued) 4A-235-B 4A-235-B2 4A-235-B3 4A-235-B31 COMPRESSION Bore and stroke, in. Displacement, cu. in. Compression ratio 4.625 x 3.5 235 8.5:1 - - - - - - - - - - - - - - - - - - WEIGHT (DRY) (lb) 225 223 230 226 CENTER OF GRAVITY (in) (with all accessories) Forward from rear face of crankcase Below C.L. of crankshaft 4.75 .94 5.18 .87 5.0 .94 4.33 1.42 DRIVE SHAFT END SAE ARP502 six 1/2 in. bolts on 4 in. circle - - - - - - CARBURETION Marvel-Schebler MA- 3SPA - - - - - - IGNITION (dual) Scintilla S4RN-20, 21 Slick 4074, 4075 Scintilla S4RN-20, 21 - - Slick 4392 TIMING, øBTC 32 26 32 - - SPARK PLUGS AC 271, 281, Champion RHB-32E, -32N, -33E, -36P, -36W - - - - - - (SD-48BSM) OIL SUMP CAPACITY, QT. 5.5 - - - - 6.5 USABLE OIL, QT. (starting with full tank) 15ø nose down 20ø nose up 4.5 3.5 - - - - 4.8 4.7 5.8 5.7 NOTES 1-8 - - - - - - II. MODELS 4A-235-B4 4A-235-B6 TYPE 4HOA horizontally-mounted direct drive RATINGS Maximum Continuous hp, r.p.m., at: Sea level pressure altitude Takeoff hp, r.p.m., full throttle at: Sea level pressure altitude 125-2800 125-2800 - - - - FUEL (See Note 7) Minimum grade aviation gasoline 100/130 - - OIL GRADE (See Note 7) above 40øF ambient air temp. below 40øF ambient air temp. all ambient air temp. SAE50 SAE30 SAE 15W50 SAE 20W50 - - - - - - - - TCDS E6EA PAGE 3 II. MODELS (Continued) 4A-235-B4 4A-235-B6 COMPRESSION Bore and stroke, in. Displacement, cu. in. Compression ratio WEIGHT (DRY) (lb) CENTER OF GRAVITY (in) (with all accessories) Forward from rear face of crankcase Below C.L. of crankshaft DRIVE SHAFT END CARBURETION IGNITION (dual) TIMING, øBTC SPARK PLUGS OIL SUMP CAPACITY, QT. USEABLE OIL, QT. (starting with full tank) 15ø nose down 20ø nose up NOTES 1-8 - - CERTIFICATION BASIS CAR 13, effective June 15, 1956, as amended by 13-1 to 13-5, inclusive. The 4A-235-B31 engine model complies with Federal Aviation Regulation Part 33, effective February 1, 1965, including amendments 33-1 to 33-14, inclusive, for sections 33.17, 33.19, 33.23, 33.25, 33.27, 33.35, 33.43, and 33.49. Type Certificate E6EA issued/revised: Date of Date TC Model Application Issued/Revised 4A-235-B 01/17/64 07/22/64 4A-235-B3 10/10/68 12/27/68 4A-235-B2 07/20/70 10/08/70 4A-235-B4 10/29/70 02/16/71 4A-235-B6 07/12/71 05/02/72 4A-235-B31 09/30/92 12/8/94 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 E6EA. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of Poland. TCDS E6EA PAGE 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. 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 E6EA, 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 (øF): 4A-235-B, B3, B31 4A-235-B2, B4, B6 Cylinder head 390 (bayonet thermocouple) 400 (bayonet thermocouple) Cylinder base 315 320 Oil inlet 230 285 NOTE 2. Fuel pressure limits (p.s.i.): Min Max All models except 4A-235-B31 Inlet to carburetor 0.5 6.0 4A-235-B31 Inlet to fuel pump 1.4 8.5 Oil pressure limits (p.s.i.): Idle Normal Operation Inlet to engine All models except 4A-235-B31 25 55-80 4A-235-B31 25 55-81.2 TCDS E6EA PAGE 5 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 Moment (in. lb.) Starter Tachometer Special AND 10005 CC CC 11.44:1 0.5:1 --- 7 450 50 90 5 Dual Drives Mounting on Alternator Drive Pad Alternator Vacuum Pump Belt Drive AND 20000 CC CC 1.08:1 1.08:1 100 Total 800 Total --- 25 Optional Dual Mounting on Alternator Drive Pad Fuel Pump Prop. Governor or Fuel Pump Hydraulic Pump or Fuel Pump Diaphragm AND 20010 Diaphragm AND 20000 Special Plunger CC Plunger CC CC 1.08:1 1.08:1 1.08:1 1.08:1 1.08:1 100 Total 100 Total 100 800 Total 800 Total 800 5 25 5 25 51.6 "C" - clockwise facing engine drive pad, "CC" - counter clockwise facing engine drive pad NOTE 4. Power tolerance for production engines is +4%, -3% of the nominal rating. NOTE 5. The 4A-235-B and -B2 models have the mounts in a horizontal plane below the cylinders and carburetor located behind the oil pan. The 4A-235-B3 model has the mounts in a vertical plane at the crankcase rear face and the carburetor located under the oil pan. The 4A-235-B4 model has the mounts in a vertical plane at the crankcase rear face and the carburetor located behind the oil pan. The 4A-235-B6 model is similar to the 4A-235-B2 model except for improved engine parts. The 4A-235-B31 model is the same as the -B3 except for modified oil pan, relocated carburetor, and modified alternator mount. TCDS E6EA PAGE 6 NOTE 6. NOTE 7. 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. Fuels and oils that meet the following specifications and the specified grades are acceptable for all engine models. Fuel: ASTM-D-910, M1L-G-5572, DERD 2485, AIR3401, GOST 1012-72. Oil: SAE-J-1966 (M1L-L-6082), DERD 2472 or SAE-J-22851 (M1L-L-22851), DERD 2450. Engine Serial Numbers xxxxx130 and above incorporate slide vane fuel pump drive instead of diaphragm pump drive. The serial number of these engines incorporates letter “S”. When slide vane fuel pump drive is installed in service, the suffix “/S” is affixed to the serial number. Fuel pump PLL-7-4 (WSK Part No 26.11.8320) is approved for these engines. This pump complies with Federal Aviation Regulation Part 33, effective February 1, 1965, including amendments 33-1 to 33-5. ---THE END---