TCDS E-244

* PAGE 1 2 3 4 5 6 7 8 REV. 22 21 21 22 21 21 21 21 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 E-244 TCDS NUMBER E-244 REVISION: 22* DATE: April 30, 2013 Franklin Sp. z.o.o. MODELS FRANKLIN 6V4-178-B32 (0-335-3) 6V4-178-B33 (0-335-4) 6V4-200-C32 (0-335-2)(0-335-5) 6V4-200-C33 (0-335-6) 6A-335-A, -B, -B1A, -D 6A-335-B1 6V-335-A, -B Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number 244) 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-244 to Franklin Sp. z.o.o. on August 17, 2006 I. MODELS 6V4-178-B31 6V4-178-B3,-B32,-B33 6V4-200-C32,-C33 TYPE 60A Vertically-Mounted Direct Drive RATINGS Maximum Continuous hp, r.p.m., at: Sea level pressure altitude Takeoff hp, r.p.m., full throttle 178-3000-S.L. 178-3000 - - - - 200-3100-S.L. 200-3100 FUEL Minimum grade aviation gasoline 80/87 - - 91/96 OIL GRADE above 40øF ambient air temp. below 40øF ambient air temp. SAE 50 SAE 40 - - - - - - - - TCDS E-244 2 I. MODELS (Continued) 6V4-178-B31 6V4-178-B3,-B32,-B33 6V4-200-C32,-C33 COMPRESSION Bore and stroke, in. Displacement, cu. in. Compression ratio 4.5 X 3.5 335 7:1 - - - - - - - - - - 8.5:1 WEIGHT (DRY) (lb) 274 293 298 CENTER OF GRAVITY (in) (with all accessories) Forward from rear face of crankcase Above rear face of crankcase Below top face of crankcase Above C.L. of crankshaft From crankshaft C.L. toward carb. side --- --- 15.0 --- 1.2 --- --- - - --- - - --- 4.6 --- --- 1.9 DRIVE SHAFT END Integral flange, with 8- 5/16 in. threaded holes on 3-5/16 in. circle - - - - PROPELLER SHAFT --- --- --- CARBURETION Marvel Schebler MA4-5 or Bendix Stromberg PS5 Marvel Schebler MA4-5 or MA4-5A Marvel Schebler MA4-5, MA4-5AA or Bendix Stromberg PS-5B IGNITION (dual) Eisemann LA-6 magneto Scintilla S6RN-21 Scintilla S6RN-21, -23 TIMING, øBTC 32 - - 36 SPARK PLUGS Champion AJ-66, REJ-38, J43; Auto-Lite A4, A4S - - Champion AJ-10 (See NOTE 6) REL37B; AC A47LY, LA47, SE47P; Jet Ignition 14-17-450S; Auto-Lite PE26-X3 OIL SUMP CAPACITY, QT. 8 9.6 10 USEABLE OIL, QT. (See NOTE 3) (starting with full tank) 15ø nose down 20ø nose up a.4 a.6 a.5.6 b.7.6 a.6 b.8 NOTES 1-6, 8, 12, 13 1-8, 12, 13 1-13 TCDS E-244 3 II. MODELS 6V-335-A, -B(1) 6V-335-A (2) 6A-335-D 6A-335-B,-B1,-B1A TYPE For models 6V-335-A, -B(1) : 60A Vertically-Mounted Direct Drive For models 6A-335-A(2), 6A-335-D, 6A-335-B, -B1, -B1A: 60A Horizontally- Mounted Direct Drive RATINGS Maximum Continuous hp, r.pm., at: Sea level pressure altitude Takeoff hp, r.p.m., full throttle 210-3100-S.L. 210-3100 200-3100-S.L. 200-3100 180-2800-S.L. 180-2800 FUEL Minimum grade aviation gasoline 91/96 100/130 80/87 OIL GRADE above 40øF ambient air temp. below 40øF ambient air temp. SAE 50 SAE 40 - - - - - - - - COMPRESSION Bore and stroke, in. Displacement, cu. in. Compression ratio 4.5 x 3.5 335 8.5:1 - - - - - - - - - - 7:1 WEIGHT (DRY) (lb) 303(1) 305(2) 292 328 (B, B1) 324 (B1A) CENTER OF GRAVITY (in) (with all accessories) Forward from rear face of crankcase Above rear face of crankcase Below top face of crankcase Above C.L. of crankshaft From crankshaft C.L. toward carb. side 8.1 (2) 4.6 (1) --- 0.7 (2) 1.9 (1) 9.1 --- --- - - --- 7.2 --- --- 0.3 --- DRIVE SHAFT END Integral flange, with 8- 5/16 in. threaded holes on 3-5/16 in. circle --- --- PROPELLER SHAFT --- Integral flange 6-1/2 in. holes on 4 in. circle - - CARBURETION Marvel Schebler MA4-5 or MA4-5A - - Marvel Schebler MA-5 IGNITION (dual) Scintilla S6RN-21, -23 - - - - TIMING, øBTC 36 (1) 32 (2) 32 28 SPARK PLUGS Champion REL37B; AC A47LY, LA47, SD47 Champion REG-32W, -36W, RHB-33E, -32N, -36W, -36P II. MODELS (Continued) 6V-335-A, -B(1) 6A-335-A (2) 6A-335-D 6A-335-B,-B1,-B1A TCDS E-244 4 OIL SUMP CAPACITY, QT. 10 (1) 8.8 (2) --- 8.8 USEABLE OIL, QT. (See NOTE 3) (starting with full tank) a.6 (1) b.8 (2) c.8 d.7 c.6.8 d.5.8 NOTES 1-13 1-5, 8, 13 1-5, 13 CERTIFICATION BASIS Type Certificate 244 issued/revised: Date of Date TC Model Application Issued/Revised CAR 13, effective August 1, 1941 6V4-178-B31 09/09/46 and 03/19/46* 6V4-178-B3 10/01/46 (letters) 10/14/46* 0-335-1 6V4-178-B32 03/12/46 04/29/47 0-335-3 6V4-165-B32F 10/10/47 12/22/47* 6V4-178-B33 09/13/48 11/05/48 0-335-4 6V4-200-C32 08/09/48 11/26/48 0-335-2 0-335-5 YO-335-5 CAR 13 effective August 1, 1949, as amended by 13-1 and 13-2 6V4-200-C33 10/04/51 11/02/51 0-335-6 YO-335-6 CAR 13 effective June 15, 1956 6V-335-A 11/15/56 11/27/56 6V-335-B 11/15/56 11/27/56 6A-335-A 11/28/56 12/11/56 CAR 13 effective June 15, 1956, as amended by 13-1 to 13-4, inclusive. 6A-335-B 05/31/62 03/28/63 6A-335-D 10/17/62 03/28/63 6A-335-B1 09/18/63 10/10/63 6A-335-B1A 04/07/70 04/20/70 Reissued to WSK "PZL-RZESZOW" 11/05/81 Reissued to WSK "PZL-RZESZOW" SA 120/8/94 Reissued to Franklin Sp. z.o.o. 04/30/13 *Engine models 6V4-178-B3, 6V4-178-B31, and 6V4-165-B32F were deleted from Type Certificate 244 on December 05, 1950. These models are no longer eligible for installation on certificated aircraft. This note reflects the issuance of two Type Certificates for administrative purposes; one under 21.21 for engines produced in the United States, and one under 21.29 for engines produced in Poland. Both type certificates have identical numbers. 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-244. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of Poland. TCDS E-244 5 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 E-244, 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): 6V4-178-B3 6V4-178-B31 -B32, -B33 6V4-200-C32, -C33 Cylinder head 520 530 530 (spark plug gasket) Cylinder head 435 445 435 (well type thermocouple) Cylinder base 310 310 310 Oil inlet 230 230 230 6V-335-A 6V-335-A, -B 6A-335-B, -B1, -B1A, -D Cylinder head --- --- (spark plug gasket) Cylinder head 435 390 (well type thermocouple) Cylinder base 315 315 Oil inlet 235 235 NOTE 2. Carburetor fuel pressure limits: Marvel Schebler MA4-5, MA4-5AA and MA-5 0.5 to 9 p.s.i. Bendix PS-5C and PS-5BD 9 to 14 p.s.i. Lubricating oil pressure limits: Normal operation 40 - 65 p.s.i. (55 - 80 p.s.i., 6A-335-B, -B1) Idle 25 p.s.i. TCDS E-244 6 NOTE 3. 6V Model Engines (Vertical) a. With crankshaft flange tilted 15ø from vertical, in the direction of the oil pan. b. With crankshaft flange tilted 15ø from vertical, in the direction of the crankcase cover. 6A-335-A, -B, -B1, -B1A, -D Engines (Horizontal) c. 15ø Nose down d. 20ø Nose up NOTE 4. 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 6V4-178-B3, B31 Except B3, B31 Generator 6V4-178-B31 Except B31, B, B1, A, D 6A-335-B, B1 B1A 6A-335-A, D Tachometer All Propeller Governor 6A-335-B, B1, B1A Fuel Pump** All except B31, A, D Fuel Pump 6A-335-A, D Vacuum Pump 6A-335-B, B1, B1A None None None None None None AND10005 Type 1 or AND 20005 Type XV-B AND 20010 AND 20000 AND 10000 AND 10000 AND 20000 CC CC CC CC CC CC CC CC CC CC CC C 11.444:1 11.444:1 1.500:1 1.500:1 1.500:1 1.500:1 0.500:1 0.847:1 0.847:1 1.500:1 1.500:1 0.847:1 70 140 8 12 18 25 2 125 125 5 5 100 240 300 15 35 50 70 6 825 825 600 600 825 30 90 45 55 75 75 3 25 25 7 7 25 * "C" - clockwise viewing drive pad, "CC" - counter clockwise ** (Optional on right or left magneto drive housing) TCDS E-244 7 NOTE 5. The above engines incorporate the following detailed differences: Model Characteristics 6V4-178-B3 Similar to -B32 except has direct drive starter. 6V4-178-B31 Similar to -B32 except has old type accessory section, small oil sump and direct drive starter. 6V4-178-B32 Basic engine, incorporates a geared starter. 6V4-178-B33 Similar to -B32 except for revised intake manifold to relocate carburetor. 6V4-200-C32 Similar to -B32 except for improved crankcase, modified cylinders and cylinder hold-down stud base circle, optional cylinder tie plate, increased cross-sectional area inlet manifold and zone pipe, 8.5:1 compression ratio pistons. 6V4-200-C33 Similar to -C32 except for revised intake manifold to relocate carburetor. The above engines incorporate the following detailed differences: Model Characteristics 6V-335-A Similar to -C32 except for revised cylinder, camshaft and magneto timing. 6V-335-B Similar to 6V-335-A except for relocated carburetor. 6A-335-A Similar to 6V-335-A except mounts in horizontal position. 6A-335-B Similar to 6A-335-A except intended for fixed wing installation and includes provision for propeller governor. 6A-335-B1 Similar to 6A-335-B except for carburetor zone, zone and equalizer pipes. 6A-335-B1A Similar to 6A-335-B except for intake system and accessory case. 6A-335-D Similar to 6A-335-A except carburetor located at front of engine instead of rear. NOTE 6. The Champion AJ-10 spark plug must be inspected at 50 hour interval. The AJ-10 spark plug was previously designated LA-10. The Champion C-10S spark plug has been obsoleted. NOTE 7. Military 0-335 engine models are identical to the corresponding 6V4 models as indicated. When installed in certificated aircraft the commercial equivalent designation and TC No. 244 should be added to the engine nameplate. YQ-335-5 engines are same as 6V4-200-C32 engines with serial numbers 26209 and under. 0-335-5 engines are same as 6V4-200-C33 engines with serial numbers 26210 and over. YO-335-6 and O-335-6 engines are military equivalents of 6V4-200-C33 engine model. YO-335-6 engines are serially numbered E- 600001 and E-600002, 0-335-6 engines are serially numbered E-60003 and over. 0-335-5D engines are military equivalents of the 6V-335-B engine model. NOTE 8. The following models have been approved specifically for helicopter installation: 6V4-200-C32 serially numbered 26210 and over 6V4-200-C33 0-335-5 0-335-6 6V-335-A, -B 6V-335-A, -D Engines not covered by this note that are currently installed in helicopters should not be operated at speeds in excess of the MC rating. A note to this effect should be incorporated in the pertinent helicopter flight manual. NOTE 9. Engine Serial Numbers 26677 and above incorporate revised intake manifold kit part number 19515 and 19516. When these parts are added to engines serially numbered 26676 and under, suffix letter "A" will be added to the pertinent engine serial number. TCDS E-244 8 NOTE 10. Engine Serial Numbers 26721 and above incorporate sodium cooled exhaust valve part number 19518 or 19631. Engine Serial Numbers 26001 to 26720, and 600001 to 600733 were not originally equipped with the sodium cooled exhaust valve. When this part is installed in these engines, suffix letter "B" will be added to the pertinent engine serial number. NOTE 11. Model 6V4-200-C33 and 6V-335-B engines equipped with Marvel Schebler MA4-5AA carburetor setting no. 10-3847 approved for following ratings: 6V4-200-C33 6V-335-B Maximum permissible carburetor air temperature 180øF 180øF Maximum continuous and takeoff, hp., r.p.m., in Hg, at: Critical altitude, ft. 200-3100-31.2 -7000 210-3000-30.4-7000 Sea level pressure altitude 200-3100-32.5-S.L. 210-3000-31.8-S.L. NOTE 12. External valve cover drain system optional on all 6V model (vertical) engines. NOTE 13. 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---