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Continental Motors O-200-D Скачать руководство пользователя страница 39

O-200-D & X Series Engine Installation and Operation Manual

2-17

3 January 2017

Engine Description

2-3.5. Lubrication System

The engine lubrication system delivers lubricating oil throughout the engine to various
bearings, bushings, and engine components. The wet sump lubrication system consists of
an internal engine-driven oil pump, a fixed, non-adjustable pressure relief valve, an oil
sump and oil sensing ports. An optional oil cooler adapter is available to connect a remote
mounted oil cooler.

Figure 2-12. Lubrication Schematic

2-3.5.1. Oil Pump

The engine-driven, positive displacement, gear type oil pump (Figure 2-13) consists of
two meshed steel gears that revolve inside the oil pump cavity machined in the accessory
case. The camshaft drives the oil pump drive gear, which drives the oil pump driven gear.
The oil pump driven gear is supported by a shaft pressed into the accessory case and the
oil pump cover plate. The oil pump drive gear shaft is supported by bushings pressed into
the accessory case.

OIL
SUCTION
TUBE

OIL PRESSURE
RELIEF VALVE

CRANKSHAFT
BEARINGS

CAMSHAFT
BOSS

INTAKE

EXHAUST

PUSHROD
HOUSING

PUSHROD

HYDRAULIC
LIFTERS

OIL SUMP

OIL PUMP GEARS

OIL FILTER AND
BYPASS
ASSEMBLY

OIL COOLER
ADAPTER

OIL
SUCTION
TUBE

OIL PRESSURE
RELIEF VALVE

CRANKSHAFT
BEARINGS

CAMSHAFT
BOSS

INTAKE

EXHAUST

PUSHROD
HOUSING

PUSHROD

HYDRAULIC
LIFTERS

OIL SUMP

OIL PUMP GEARS

OIL FILTER AND
BYPASS
ASSEMBLY

OIL COOLER
ADAPTER

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Содержание O-200-D

Страница 1: ...Publication OI 2 2017 CONTINENTAL MOTORS INC JAN 2017 O 200 D X CONTINENTAL AIRCRAFT ENGINE INSTALLATION AND OPERATION MANUAL FAA APPROVED...

Страница 2: ...3 January 2017 Page Change Page Change Page Change Page Change Cover 0 A 0 i viii 0 1 1 thru 1 12 0 2 1 thru 2 32 0 3 1 thru 3 28 0 4 1 thru 4 22 0 A 1 thru A 2 0 B 1 thru B 2 0 C 1 thru C 2 0 Publish...

Страница 3: ...rements It is not intended and should not be used by a pilot owner or maintenance personnel Installation and Operation instructions in this manual may be modified or used intact to create the aircraft...

Страница 4: ...ii O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Intentionally Left Blank...

Страница 5: ...er 2 Engine Description 2 1 General Engine Description 2 1 2 1 1 Engine Model Number Definition 2 2 2 1 2 Cylinder Number Designations 2 2 2 2 Aircraft Interface Requirements 2 3 2 2 1 Crankcase Breat...

Страница 6: ...System 2 17 2 3 5 1 Oil Pump 2 17 2 3 5 2 Oil Sump 2 18 2 3 5 3 Oil Pressure Relief Valve 2 18 2 3 5 4 Oil Cooler Adapter 2 19 2 3 6 Ignition System 2 19 2 3 7 Starter Assembly 2 21 2 3 8 Alternator 2...

Страница 7: ...In 4 3 4 2 3 1 Engine Break In 4 3 4 2 3 2 Flight Check 4 4 4 3 Normal Operation 4 5 4 3 1 Pre operational Requirements 4 5 4 3 2 Engine Start 4 6 4 3 2 1 Cold Start 4 7 4 3 2 2 Flooded Engine 4 7 4...

Страница 8: ...ix A Glossary Appendix B Torque Specifications Appendix C Standard Practices C 1 Handling Parts C 1 C 2 Replacement Parts C 1 C 2 1 Background C 1 C 2 2 Acceptable Replacement Parts C 1 C 2 2 1 Know Y...

Страница 9: ...elated Publications 1 11 Table 2 1 Recommended Instrument Range Markings 2 5 Table 2 2 Oil Gauge Rod Error 2 7 Table 2 3 O 200 D Specifications 2 23 Table 2 4 O 200 X Specifications 2 25 Table 2 5 Acc...

Страница 10: ...Harness Routing typical 2 20 Figure 2 17 Engine Cooling 2 21 Figure 2 18 Fuel Flow vs Brake Horsepower 2 29 Figure 2 19 Full Throttle and Prop Load Curves 2 30 Figure 2 20 Sea Level Performance 2 31...

Страница 11: ...ries including the O 200 A B C model engines engine accessories or the airplane refer to the appropriate manual This document is intended for use only by an OEM or STC customer for assistance in defin...

Страница 12: ...ormation in this manual must be incorporated into the applicable aircraft design data and the Airplane Flight Manual Pilot s Operating Handbook AFM POH by the aircraft manufacturer Refer to the AFM PO...

Страница 13: ...O 200 D X Series Engine Installation and Operation Manual 1 3 3 January 2017 Introduction Figure 1 1 Figure and Index Reference...

Страница 14: ...releases publication changes in the form of either change pages or complete publication revisions depending upon the extent of change Continental Motors issues service documents in the form of Servic...

Страница 15: ...riginal publication date and an itemized list of changes issued for the technical manual Figure 1 3 If change pages are issued for the manual the change will be identified with an effective date under...

Страница 16: ...1 6 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Introduction Figure 1 3 List of Effective Pages...

Страница 17: ...eration of an aircraft persons or property on the ground unless some specific action inspection repair replacement etc is taken by the owner or operator Documents in this category are candidates for i...

Страница 18: ...Inspection M 0 SB96 12 Continued Airworthiness for TCM Cylinders Scheduled Inspection M 0 SB97 6B Mandatory Replacement Parts Engine Inspection Assembly M 0 SIL98 9E Time Between Overhaul Periods Eng...

Страница 19: ...rt a copy of the service document behind the last page of this section Make pen ink corrections where appropriate to the original text in the manual with a citation to the service document i e see SB9...

Страница 20: ...letin Number Release Date Affected Sections Title Bulletin Number Release Date Affected Sections Title Bulletin Number Release Date Affected Sections Title Bulletin Number Release Date Affected Sectio...

Страница 21: ...ccess our web site to confirm and review the latest revision of this manual If you have not subscribed to Internet service and are using printed manuals contact using the Contact Information in Sectio...

Страница 22: ...service If customers have an inquiry or require technical assistance they should contact their local Continental Motors distributor or field representative To contact a factory representative refer t...

Страница 23: ...ped with carburetors and an updraft induction system The engines are designed with a wet sump positive displacement oil pump installed in the accessory case When properly maintained under normal opera...

Страница 24: ...he rear of the engine is the accessory end Viewed from the rear of the engine the left side cylinders are designated by even num bers 2 4 with Cylinder 2 being closest to the rear The right side cylin...

Страница 25: ...on Audit The purpose of the audit is to review compliance with the minimum requirements set forth within this document Satisfactory completion of the audit is required before Continental Motors will d...

Страница 26: ...embly and the aircraft air filter and the alternate air system in compliance with the applicable regulations The engine induction air system consists of individual tubes connected between the cylinder...

Страница 27: ...fuel flow values Minimize fuel line lengths to decrease residence time of the fuel Minimize elevation changes Minimize the number of bends and fittings Route fuel lines away from heat generating comp...

Страница 28: ...Fuel Boost Pump An aircraft boost pump can aid starting and vapor suppression on a carburetor equipped engine The airframe manufacturer must ensure the minimum and maximum fuel pressure at the carbur...

Страница 29: ...ground attitude oil levels in the POH should be increased by 0 5 quarts 2 2 6 4 Oil Filter The O 200 D X series engines are fitted with a spin on full flow oil filter with integral bypass as standard...

Страница 30: ...al connector for grounding the magneto through a switch In cases where only the left magneto is equipped with an impulse coupling the right magneto must be grounded when the starter is energized Groun...

Страница 31: ...opeller and spinner exhaust system and all accessories required for operation 2 2 11 Propeller System O 200 D X series do not provide hydraulic control for propeller pitch control A fixed pitch propel...

Страница 32: ...acked crankshaft main bearing inserts are line bored through web bosses Camshaft bearings are bored directly in the case metal Bearings are divided equally by the parting surface camshaft bearings bei...

Страница 33: ...r of each case casting affords an engine mounting point The arm bosses of the crankcases are bored through and counterbored for mount bushing assemblies The flange surrounding the rear end of the cran...

Страница 34: ...s a propeller mount flange forged on the front end with six tapped holes in the flange Six bolts screwed into the propeller flange clamp the propeller between a loose front flange and the propeller fl...

Страница 35: ...amshaft main journals are supported in the crankcase by machined bearing saddles Hydraulic tappets move inward and outward in their bores following the eccentric shape of the cam lobes Four unequally...

Страница 36: ...t side of the accessory case for installation of a non adjustable oil pressure relief valve Oil pump gear chambers are machined in the interior of the accessory case The oil pump drive gear shaft hole...

Страница 37: ...ber for an optional primer jet which may be installed by the owner The port is sealed by a pipe plug from the factory An external base flange below the cylinder barrel fins is mounted flat and drilled...

Страница 38: ...he hydraulic valve tappet lifter provides an interface between the camshaft lobe and the remaining valve train Hydraulic valve tappets ride on the eccentric cam lobes opening and closing the intake an...

Страница 39: ...2 13 consists of two meshed steel gears that revolve inside the oil pump cavity machined in the accessory case The camshaft drives the oil pump drive gear which drives the oil pump driven gear The oi...

Страница 40: ...on The upper section features a rib reinforced crankcase mounting flange and a boss for the pressed oil gauge rod and extension tube assembly The lower oil sump body is fitted with a threaded drain pl...

Страница 41: ...inental Motors magneto model number identifies the key features of each magneto model as shown in Figure 2 15 The magnetos generate and distribute high voltage ignition pulses through high tension lea...

Страница 42: ...Magneto one drive two output distributors Cylinders Fired 4 Four Cylinders 6 Six Cylinders 8 Eight Cylinders Rotatlon Viewed Looking in to Drive End L Left counterclockwise R Right clockwise Designato...

Страница 43: ...ailed description of Continental Motors alternators refer to Continental Motors Alternator Service Instructions 2 3 9 Engine Cooling The engine cylinders are cooled by transferring heat from the cylin...

Страница 44: ...he intake manifold is attached to two studs on the lower crankcase flange The carburetor is attached to the bottom of the intake manifold with a gasket and four fasteners Air passage through the manif...

Страница 45: ...Power WOT 1 88 bhp 2450 rpm Fuel System Specifications Fuel Minimum Grade3 100 100LL conforming to ASTM D910 Fuel Grade People s Republic of China4 RH 95 130 conforming to GB 1787 Minimum fuel pressu...

Страница 46: ...of rear accessory case Below crankshaft centerline Beside crankshaft centerline toward 1 3 side 14 55 0 96 0 06 369 60 24 40 1 50 1 Performance is based on sea level standard day zero water vapor pre...

Страница 47: ...2450 rpm Fuel System Specifications Fuel Minimum Grade3 100 100LL conforming to ASTM D910 Fuel Grade People s Republic of China4 RH 195 130 conforming to GB 1787 Minimum fuel pressure at the carburet...

Страница 48: ...d of rear accessory case Below crankshaft centerline Beside crankshaft centerline toward 1 3 side 14 55 0 96 0 06 369 60 24 40 1 50 1 Performance is based on sea level standard day zero water vapor pr...

Страница 49: ...ximum Torque in lbs Maximum Overhang Moment in lbs Cont Static Magneto CW 1 1 Starter Motor CW 35 7 1 Alternator gear driven CCW 2 035 1 60 600 100 Mass Flow Sea level standard day conditions 100 bhp...

Страница 50: ...X configuration as cafeteria type selections Performance specifications for both engine models are identical WARNING The performance charts included in this manual indicate uninstalled engine perform...

Страница 51: ...iption 2 4 5 1 O 200 D X Performance Charts Figure 2 18 Fuel Flow vs Brake Horsepower 20 25 30 35 40 45 50 55 60 50 55 60 65 70 75 80 85 90 95 100 Fuel Flow lbs hr Corrected Brake Horse Power Data Mea...

Страница 52: ...Rich Fuel Mixture Minimum Engine 0 45 0 50 0 55 0 60 0 65 1900 2000 2100 2200 2300 2400 2500 2600 2700 2800 Brake Specific Fuel Consumption lb hphr Engine Speed rpm Prop Load Full Throttle Data Measu...

Страница 53: ...ermine actual HP 1 Locate RPM Pm on Alt Perf Chart Pt A 2 Locate RPM Pm on Sea Level Perf Chart Pt B 3 Transfer CBHP equal to Pt B on Sea Level Chart to Alt Perf Chart Pt C 4 Draw line from Pt C to Pt...

Страница 54: ...mponents provided by the aircraft manufacturer Table 2 6 O 200 D X Accessory Weights Accessory Weight lbs Model Specification D1B D2B D3B D4B X2B Basic Engine Weight 158 2 Starter Skytec 12V 9 2 X X X...

Страница 55: ...3 Engine Transport Stand 4 Oil conforming to SAE J1966 break in oil non dispersant mineral oil or MIL C 6529 Type II Fly away oil or 5 MIL P 46002 Grade 1 oil 6 100 100LL aviation fuel conforming to A...

Страница 56: ...and inspect the desiccant bag through the plastic shipping bag Desiccant bag is attached to the engine mount at the rear of the engine 5 Inspect the engine according to the Acceptance Inspection crite...

Страница 57: ...on 3 2 2 Prepare the Engine for Installation b If damage or corrosion is discovered contact the supplier of the engine for disposition Do not install a damaged or corroded engine or place it in storag...

Страница 58: ...recommends hose replacement coincident with engine overhaul to avoid immediate contamination or failure at a later date 2 Replace all aircraft flexible oil and fuel hoses according to the aircraft ma...

Страница 59: ...nstructions in Section C 3 of M 0 Standard Practice Maintenance Manual 9 Install all aircraft manufacturer required components according to the aircraft manufacturer s instructions including the follo...

Страница 60: ...aft manufacturer s instructions 8 Install the propeller according to the aircraft and propeller manufacturer s instructions 9 Perform the Engine Pre oiling procedure according to the instructions in S...

Страница 61: ...or valve to the ON position 3 Allow a minimum of one quart 0 94 liter of fuel to flow through a paper filter until the fuel is free of contaminants 4 Position the fuel selector valve to the OFF positi...

Страница 62: ...ct the oil cooler and oil filter for signs of leaks or physical discrepancies 5 Check the following on the engine for physical damage a External cylinder barrels b Cylinder barrel fins c Areas between...

Страница 63: ...g Handbook POH Perform a flight check before releasing the engine for normal service to ensure the installed engine meets the aircraft manufacturer s performance and operational specifications WARNING...

Страница 64: ...p gaskets for oil leaks c Inspect oil sump for cracks d Inspect cylinder head exhaust gaskets for evidence of exhaust leaks e Inspect oil return hoses and air inlet for evidence of chafing from oil co...

Страница 65: ...d to assist the aircraft manufacturer determine appropriate fittings and fasteners for aircraft interconnect requirements Pay particular attention to the engine models depicted when referencing drawin...

Страница 66: ...3 12 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Engine Installation Figure 3 3 60 Amp Alternator Detail Figure 3 4 50 Amp Alternator Detail...

Страница 67: ...O 200 D X Series Engine Installation and Operation Manual 3 13 3 January 2017 Engine Installation Figure 3 5 Engine Mounts...

Страница 68: ...3 14 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Engine Installation Figure 3 6 Starter Connection Details...

Страница 69: ...0 D X Series Engine Installation and Operation Manual 3 15 3 January 2017 Engine Installation Figure 3 7 Ignition Distribution Champion Slick Magnetos Figure 3 8 Ignition Distribution Continental Magn...

Страница 70: ...3 16 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Engine Installation Figure 3 9 Ignition Switch Connections to Magneto...

Страница 71: ...O 200 D X Series Engine Installation and Operation Manual 3 17 Reverse Blank 3 January 2017 3 3 2 O 200 D Installation Drawings Figure 3 9 O 200 D Engine Installation Drawing Left Side and Rear Views...

Страница 72: ...3 18 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Intentionally Left Blank...

Страница 73: ...O 200 D X Series Engine Installation and Operation Manual 3 19 Reverse Blank 3 January 2017 Figure 3 10 O 200 D Engine Installation Drawing Front and Top View...

Страница 74: ...3 20 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Intentionally Left Blank...

Страница 75: ...O 200 D X Series Engine Installation and Operation Manual 3 21 Reverse Blank 3 January 2017 Figure 3 11 O 200 D Engine Installation Drawing Detail Views...

Страница 76: ...3 22 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Intentionally Left Blank...

Страница 77: ...O 200 D X Series Engine Installation and Operation Manual 3 23 Reverse Blank 3 January 2017 3 3 3 O 200 X Installation Drawings Figure 3 12 O 200 X Engine Installation Drawing Left Side and Rear Views...

Страница 78: ...3 24 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Intentionally Left Blank...

Страница 79: ...O 200 D X Series Engine Installation and Operation Manual 3 25 Reverse Blank 3 January 2017 Figure 3 13 O 200 X Engine Installation Drawing Top and Front Views...

Страница 80: ...3 26 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Intentionally Left Blank...

Страница 81: ...O 200 D X Series Engine Installation and Operation Manual 3 27 Reverse Blank 3 January 2017 Figure 3 14 O 200 X Engine Installation Drawing Detail Views...

Страница 82: ...3 28 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Intentionally Left Blank...

Страница 83: ...r aircraft operating procedures 4 2 Flight Prerequisites Perform the sequential tasks listed in the Engine Operational Check instructions in Section 6 3 6 of the Maintenance and Overhaul Manual M 2 on...

Страница 84: ...of an engine the first time high power is applied If the aircraft is inadvertently serviced with the incorrect grade of aviation fuel or jet fuel the fuel system must be completely drained and the fu...

Страница 85: ...to prevent undesirable engine cooling If power must be reduced for long periods adjust the propeller to minimum governing RPM if equipped to obtain desired performance levels If outside air temperatur...

Страница 86: ...ure to drop below 300 F 149 C 5 Descend at low power cruise settings Avoid long descents with engine speed below 1500 RPM Carefully monitor engine instrumentation to maintain levels above the minimum...

Страница 87: ...een completed in addition to the aircraft manufacturer s instructions found in the AFM POH Operation of a malfunctioning engine can result in additional damage to the engine bodily injury or death Sup...

Страница 88: ...r Verify the tasks listed in Table 4 2 Flight Prerequisites have been completed in addition to those required by the aircraft POH aircraft manufacturer or Supplemental Type Certificate STC holder Note...

Страница 89: ...arts and runs smoothly at idle indicated oil pressure is greater than 10 psi If the engine fails to start refer to the troubleshooting instructions in Chapter 8 of the Maintenance and Overhaul Manual...

Страница 90: ...rtently start and cause personal injury or death This condition must be corrected prior to continued aircraft operation CAUTION Do not underestimate the importance of the magneto check When operating...

Страница 91: ...ight Magneto channel drop results Maximum allowable RPM drop spread between magneto channels is 75 RPM CAUTION Do not operate the engine at speeds in excess of 2000 RPM longer than necessary to comple...

Страница 92: ...t take off Determine cause and take corrective action necessary to maintain airworthiness Supplement the AFM POH take off procedures with these engine settings 1 Mixture FULL RICH 2 Cowl Flaps per AFM...

Страница 93: ...esired altitude has been reached supplement the AFM POH instructions with these steps 1 Adjust the throttle for the desired cruise power settings 2 Monitor Engine Instruments Allow engine temperatures...

Страница 94: ...in Section 6 5 3 of M 0 Standard Practice Maintenance Manual Supplement the AFM POH with the following 1 Descend at cruise power settings with mixture control positioned for smooth engine performance...

Страница 95: ...NOTE The difference between magnetos individual operation should not exceed 75 RPM Maximum RPM drop for either magneto is 150 RPM Observe engine smoothness during magneto switching If the engine runs...

Страница 96: ...specific steps in addition to the AFM POH requirements when responding to emergency conditions If a malfunction should occur in flight certain remedial actions may eliminate or reduce the severity of...

Страница 97: ...4 4 2 Engine Roughness WARNING If roughness is severe or the cause cannot be determined engine failure may be imminent Follow the AFM POH emergency procedures and LAND AS SOON AS POSSIBLE 5 Upon land...

Страница 98: ...speed If the overspeed event duration is less than ten seconds perform a Category I Overspeed Inspection according to instructions in Section 6 5 3 of M 0 Standard Practice Maintenance Manual If the o...

Страница 99: ...e indication may be caused by a faulty gauge or thermocouple If oil temperature drops as temperature increases 1 Cowl Flaps OPEN if equipped 2 Airspeed Increase 3 Reduce Power if steps 1 and 2 do not...

Страница 100: ...1 4 OPEN 3 Ignition Switch START hold until engine starts 4 Mixture Control Advance slowly until proper proper fuel air mixture is reached 5 Throttle Adjust for desired RPM 4 4 8 Engine Fire In Flight...

Страница 101: ...to the Engine Preheating instructions in Section 7 4 1 1 of M 0 Standard Practice Maintenance Manual 4 5 1 1 1 Engine Preheat with a Combustion Heater Refer to the Engine Preheat with a Combustion He...

Страница 102: ...and fuel vapor Until the entire fuel system becomes filled with liquid fuel difficult starting and unstable engine operation can be expected Hot weather operation situations requiring special instruc...

Страница 103: ...following engine run up face the aircraft into the wind with the engine idling at 900 1000 RPM 4 5 2 3 Take off and Initial Climb Out in Hot Weather 1 Mixture control FULL RICH NOTE Under extreme cond...

Страница 104: ...equired during takeoff If higher than desired temperatures are experienced during the climb phase establish a lower angle of attack or higher climb speed consistent with safe operating practices to pr...

Страница 105: ...O 200 D X Series Engine Installation and Operation Manual A 1 3 January 2017 Glossary Appendix A Glossary Refer to Appendix A in M 0 Standard Practice Maintenance Manual...

Страница 106: ...A 2 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Glossary Intentionally Left Blank...

Страница 107: ...O 200 D X Series Engine Installation and Operation Manual B 1 3 January 2017 Torque Specifications Appendix B Torque Specifications Refer to Appendix B in M 0 Standard Practice Maintenance Manual...

Страница 108: ...B 2 O 200 D X Series Engine Installation and Operation Manual 3 January 2017 Torque Specifications Intentionally Left Blank...

Страница 109: ...e Manual C 2 4 Mandatory Overhaul Replacement Parts Refer to Appendix C 2 4 in M 0 Standard Practice Maintenance Manual C 2 5 Authorized Oversize Undersize Parts Refer to Appendix C 2 5 in M 0 Standar...

Страница 110: ...pendix C 9 in M 0 Standard Practice Maintenance Manual C 10 Gasket Installation Refer to Appendix C 10 in M 0 Standard Practice Maintenance Manual C 11 Hose and Tubing Installation Refer to Appendix C...

Страница 111: ......

Страница 112: ...www continentalmotors aero...

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