TYPE CERTIFICATE DATA SHEET Nº EM-9105 Type Certificate Holder: TELEDYNE CONTINENTAL MOTORS 2039 Broad Street Mobile, Alabama, 36601 U.S.A EM-9105-01 Sheet 01 TELEDYNE CONTINENTAL O-200-A, O-200-D 23 September 2011 Engines of models described herein conforming with this data sheet, which is part of Type Certificate No. 9105, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Brazilian Aeronautical Regulations provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other instructions. MODEL TYPE O-200-A, O-200-D 4HOA RATINGS O-200-A O-200-D Max. continuous, hp. - rpm. full throttle at: Sea level pressure altitude: 100-2750 --- Takeoff, hp. - rpm full throttle at: Sea level pressure altitude: 100-2750 ---
TELEDYNE CONTINENTAL 23 September EM-9105-01 Sheet 2/5 MODEL O-200-A O-200-D FUEL TYPE (mínimum grade aviation gasoline) 80/87 100/100LL, RH100/130 CARBURETION / INJECTION (See Note 4 for injectors) Marvel-Schebler MA-3SPA (TCM P/N 627143, 633028 or 640416) --- OIL, LUBRICATION (lubrication oil, ambient air temperature) Oil Grade Oil Grade Below 4.4 C (40 F) SAE 20 SAE 30 Above 4.4 C (40 F) SAE 40 SAE 50 BORE AND STROKE mm (in) 103.2 x 98.4 (4.062 x 3.875) --- DISPLACEMENT L (cu.in) 3.3 (201) --- COMPRESSION RATIO 7:1 8.5:1 IGNITION 2 Bendix-Scintilla S4LN-21 or -1227 or 1 ea. S4LN-200 and -204; Slick-Electro 447, 4001 or 4201 magnetos Slick electro 4301 ( both sides) or 1ea. TCM S4LSC- 200 and S4LSC204 or 1 ea. TCM S4LSC-200 and S4LSC204T or TCM S4LSC- 21 (both sides) C.G. LOCATION (with accessories) Fwd. of rear face of mounting lugs, mm (in) 116.8 (4.6) 157.5 (6.2) Below crankshaft center line, mm (in) 30.5 (1.2) 24.4 (.96) Beside crankshaft centerline, toward 1-2 cylinder side (model O-200-A), and toward 1-3 side (model O-200-D), mm (in) 6.1 (.24) 1.5 (0.06) TIMING, BTC 24 Top, 24 Bottom 24 ± 1 SPARK PLUGS See NOTE 6 ---
TELEDYNE CONTINENTAL 23 September EM-9105-01 Sheet 3/5 MODEL O-200-A O-200-D OIL SUMP CAPACITY L (qts) 5.7 (6) 4.7 (5) WEIGHT (DRY) kg (lb) 86.2 (190) 80.1 (176.5) PROPELLER SHAFT SAE Nº. 1 Flange TCM/Cessna APPLICABLE NOTES 1,2,3,4,6,7 --- IMPORT REQUIREMENTS Each engine imported separately and/or spare parts must be accompanied by an Airworthiness Certificate for Export and/or an Airworthiness Approval Tag, respectively, issued by FAA, attesting that the particular engine and/or parts were submitted to the governmental quality control before delivery and are in conformity with the ANAC approved type design. CERTIFICATION BASIS Model Application Issued TC Part 13 of the Civil Air Regulations O-200-A 12 Nov. 1990 02 September 1991 RBAC 33, which endorses 14 CFR Part 33, effective February 1, 1965 O-200-D 22 Mar. 2011 23 September 2011 - Amendments 1 through 24, effective 05 November 2007. PRODUCTION BASIS FAA Production Certificate No. 7 and No. 508 NOTES: NOTE 1 Maximum permissible temperatures: O-200-A O-200-D Cylinder head, C (F ) 273.9 (525) 248.9 (480) Cylinder barrel, C (F ) 143.3 (290) N/A Oil inlet, C (F ) 107.2 (225) - Straight mineral 115.6 (240) 115.6 (240) - Detergent meeting MHS -24, see NOTE 6
TELEDYNE CONTINENTAL 23 September EM-9105-01 Sheet 4/5 NOTE 2 Pressure limits: Carburetor fuel inlet pressure limits Minimum Maximum MA-3SPA, TCM P/N 627143, 633028, 640416 5 In Fuel Head 6 PSIG Carburetor Air Intake Assembly, TCM A40793, used with MA-3SPA, Marvel-Schebler Carburetor. Oil pressure limits for O-200 Series: 276 to 414 (30 to 60) Minimum idling with hot oil: 69 (10) NOTE 3 The following accessory drive or mounting provisions are available: Rotation facing Speed Ratio to Max. Torque N.m (in.-lb.) Accessory Drive Pad Crankshaft Cont Static Max. Overhang Moment N.m (in.-lb.) Tachometer (***) C 0.500:1 0.8 (7) 50 2.8 (25) Generator/ Alternator CC 2.035:1 6.8 (60) 600 11.3 (100) Starter C 35.7:1 # # # Vacuum Pump (*) CC 1.0:1 11.3 (100) 90.4 (800) 2.8 (25) Fuel Pump (diaphragm) (**) 0.500:1 # # # "C" Clockwise "CC" Counter Clockwise (*) Only engine model O-200-A (**) TCM Eq. 5809 incorporating TCM P/N 40585 pump approved as part of type design of the engine O-200-A. (***)Does not apply to engine model O-200-D. NOTE 4 NOTE 5 NOTE 6 The model O-200-D is similar to the O-200-A except for special crankshaft flange, overall engine weight reduction, oil sump assembly, and higher compression pistons. The O-200-D does not have provisions for a vacuum pump or the diaphragm fuel pump. Reserved Detergent oil meeting Continental Specification MHS-24 required when using 115.6 C (240 F) oil inlet limitis except during break-in period. Follow manufacturer s instructions for break-in or when changing oil types. Marking or placards prescribing use of Continental
TELEDYNE CONTINENTAL 23 September EM-9105-01 Sheet 5/5 NOTE 7 Specification MHS-24 oil only shall be installed on or near the oil filter on installations using 115.6 C(240 F) oil inlet temperatures. The following spark plugs are approved for use on engine models as indicated: O-200-A, -D AC Auto Lite BG Champion Red Seal HSR83IR, SR83IR, HSR83P, SR83P, A88, HS88, HSR88, S88, S88D, SR88, SR88D, HSR93, SR93 18A1, SH15, H15, SH15R,SH20A, SH150, SH200A, PH26 RB485S, 706, 706S,919SR5, RB955S C27, C27S, RC27S, REM37BY,REM38P, REM38W, RHM38P, RHM38W, REM40E, RHM40E, ED41N, D41N, EM41E, EM41N, HM41E, M41E, M41N, EM42E, M42E SA190, SE190, SJ190, SE230, SJ230 (General Manager, Aeronautical Product Certification)