Continental Motors TSIO-520-BE, Maintenance And Operator'S Manual

Page 1: ...Publication X30570 CHANGE 2 2011 2013 CONTINENTAL MOTORS INC OCT 2013 TSIO 520 BE CONTINENTAL AIRCRAFT ENGINE PERMOLD SERIES MAINTENANCE AND OPERATOR S MANUAL TECHNICAL CONTENT ACCEPTED BY THE FAA ...

Page 2: ...hru 2 42 0 3 1 thru 3 8 0 4 1 thru 4 4 0 5 1 thru 5 8 0 6 1 thru 6 8 0 7 1 thru 7 6 0 8 1 thru 8 6 0 9 1 thru 9 12 0 10 1 thru 10 12 0 11 1 thru 11 4 0 12 1 thru 12 2 0 13 1 thru 13 15 0 Published and printed in the U S A by Continental Motors Inc Available exclusively from the publisher P O Box 90 Mobile AL 36601 Copyright 2011 2013 Continental Motors Inc All rights reserved This material may not...

Page 3: ...der to assure safe and reliable engine performance Failure to comply will be deemed misuse thereby relieving the engine manufacturer of responsibility under its warranty This manual contains no warranties either expressed or implied The information and procedures contained herein provide the operator with technical information and instructions applicable to safe operation ...

Page 4: ...ts 4 1 5 Unpacking Installation Testing Removal 5 1 6 Normal Operating Procedures 6 1 7 Emergency Operating Procedures 7 1 8 Abnormal Environmental Conditions 8 1 9 Service and Maintenance 9 1 1O Trouble Shooting 10 1 11 Engine Preservation and Storage 11 1 12 Airworthiness Limitations 12 1 13 Engine Performance and Cruise Control 13 1 ii ...

Page 5: ...ance Full Rich Mixture 13 5 13 3 Constant Speed Sea Level Performance Best Power Mixture 13 6 13 4 Altitude Performance 13 7 13 5 Mixture Ratio Curve 80 2500 RPM and 32 8 Hg ADMP 13 8 13 6 Mixture Ratio Curve 75 2400 RPM and 32 5 Hg ADMP 13 9 13 7 Mixture Ratio Curve 65 2300 RPM and 30 0 Hg ADMP 13 10 13 8 Mixture Ratio Curve 50 2200 RPM and 25 8 Hg ADMP 13 11 13 9 Fuel Flow Vs Brake Horsepower 13...

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Page 7: ...Section 1 1 1 2 1 3 1 4 CHAPTER 1 INTRODUCTION Section Index Page Scope 1 2 Related Publications 1 3 Abbreviations and Glossary of Terms 1 4 Manual Revisions 1 6 1 1 ...

Page 8: ...s Failure to obseive the instructions contained in this manual constitutes unauthorized operation in areas unexplored during development of the engine or in areas which experience has proved to be undesirable or detrimental Notes Cautions and Warnings are included throughout this manual Application is as follows NOTE Special interest information which may facilitate the operation of equipment CAUT...

Page 9: ... prepaid from Teledyne Continental Motors Aircraft Products P 0 Box 90 Mobile AL 36601 Attn Accounts Receivable For price information see TCM Optional and Current Publications Service Bulletins II Accessory Manuals A Magnetos B Starter Motor C Alternator Service Manual Teledyne Continental Motors Aircraft Products P 0 Box 90 Mobile AL 36601 Attn Accounts Receivable Teledyne Continental Motors Airc...

Page 10: ... Cubic Feet Per Minute Center of Gravity Cylinder Head Temperature Counterclockwise Rotation Clockwise Rotation Degrees of Angle Degrees Fahrenheit Exhaust Gas Temperature Figure Illustration Propeller End Foot or Feet Full Throttle Foot Pounds Torque Gallons Per Minute Grams Water Mercury Inside Diameter Inches Hexagon Hour Inch Pounds Torque Side on which Nos 2 4 and 6 cylinders are located Rear...

Page 11: ...cause it was formerly measured by applying a brake to the power shaft of an engine The required effort to brake the engine could be converted to horsepower hence brake horsepower Brake Specific Fuel Consumption Fuel Consumption stated in pounds per hour per brake horsepower For example an engine developing 300 horsepower while burning 150 pounds of fuel per hour has a BSFC of 5 Fuel Consumption in...

Page 12: ... AC43 11 consists of the complete disassembly of an engine inspected repaired as necessary reassembled tested and approved for return to service within the fits and limits specified by the manufacturer s overhaul data This should be to new fits or limits The determination as to what fits and limits are used during an engine overhaul should be clearly understood by the engine owner at the time the ...

Page 13: ...uare inch RAM Increased air pressure due to forward speed Rated Power The maximum horsepower at which an engine is approved for operation Retard Breaker A device used in magnetos to delay ignition during cranking It is used to facilitate starting Rich Limit The richest fuel air ratio permitted for a given power condition It is not necessarily the richest condition at which the engine will run Rock...

Page 14: ...exerted on the liquid A device used to control the speed and thus the output of the turbocharger It does so by operating the wastegate which diverts more or less exhaust gas over the turbine A thermostatic valve used to divert oil through or around the oil cooler as necessary to maintain oil temperature within desired limits The characteristic of a liquid to resist flowing Regarding oil high visco...

Page 15: ...e of publication Any errors recommended changes or questions should be submitted in writing to Department Manager Technical Publications Department Teledyne Continental Motors P 0 Box 90 Mobile Alabama 36601 Manuals will be revised and updated as necessary Consult Teledyne Continental Motors Service Bulletin publications for latest technical information available 1 9 ...

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Page 17: ...CHAPTER 2 TOOLS AND EQUIPMENT Section Index Section Page 2 1 General Information 2 2 2 2 Special Tools 2 2 2 1 ...

Page 18: ...pecific tools illustrated or similar tools marketing by other manufacturers will be necessary for service and maintenance of the TSI0 520 BE aircraft engine The tool illustrations shown on the following pages are used with the permission of the respective manufacturers Most special tools illustrated in this section are marketed by Burroughs Tool and Equipment Corporation 2429 North Burdick Street ...

Page 19: ...mpany Owatonna Minnesota 55060 507 451 5310 McMASTER CARR SUPPLY CO P O Box 4355 Chicago Illinois 60680 312 833 0300 SNAP ON TOOLS 2611 Commerce Blvd Birmingham Alabama 35210 205 956 1722 Kell Strom Tool Company Inc 214 Church St Wethersfield CT 06109 2 3 GENERAL PRODUCT SUMMARY Instruments for Aircraft Special Tools Precision Instruments Measuring Instruments Precision Tools Spark Plugs lgnitors ...

Page 20: ...N CODE FOR TOOLS ALCOA INC BORROUGHS TOOL AND EQUIPMENT CORP CHAMPION SPARK PLUG CO EASTERN ELECTRONICS INC FEDERAL TOOL SUPPLY CO INC OTC TOOLS EQUIPMENT CO McMASTER CARR SUPPLY CO SNAP ON TOOLS KELL STROM TOOL COMPANY INC 44 Numbers referenced in the left hand bottom comer of each picture correspond to the numbers located in the Special Tool Index WARNING Whenever using test equipment keep equip...

Page 21: ...olding Fixture Cylinder Hold Down BTC 11 122 Valve Guide Cleaner Cylinder Reconditioning BTC 12 8066 Seal Seat Cutter Cylinder Reconditioning BTC 13 7521A Spring Checker Spring Inspection BTC 14 3611 Valve Guide Remover Cylinder Reconditioning BTC 2874 Valve Guide Remover Cylinder Reconditioning BTC 15 4912 Valve Guide Replacer Cylinder Reconditioning BTC 3619 Valve Guide Replacer Cylinder Recondi...

Page 22: ...4 8111A Connecting Rod Fixture Connecting Rod Inspection BTC 35 8042C Adapter Kit Connecting Rod Inspection BTC 36 874 40 41 Reamers Conrod Bushing Connecting Rod Reconditioning BTC 5008 8071 Reamers Conrod Bushing Connecting Rod Reconditioning BTC 37 8098 Remover Installer Set Connecting Rod Reconditioning BTC Connecting Rod Bushing 38 8122A Common Drive Handle Cylinder Reconditioning BTC 8139 40...

Page 23: ...423 Crankcase Splitter Crankcase Separation BTC 71 5209 Propeller Shaft Oil Seal Installation of seal over Propflange BTC Installer 72 8048 Oil Pressure Relief Spot Removal of surface Material around BTC Facer holes 8155 Oil Pressure Relief Spot Removal of surface Material around BTC Facer holes 73 8117A Runout Block Set Crankshaft Inspection BTC 74 8087A B Polishing Tools for Crank Crankshaft Rec...

Page 24: ...4 Reamer Square Shank Cylinder Reconditioning BTC 2686 Reamer Square Shank Cylinder Reconditioning BTC 2689 Reamer Square Shank Cylinder Reconditioning BTC 2693 Reamer Square Shank Cylinder Reconditioning BTC 4104 Reamer Square Shank Cylinder Reconditioning BTC 92 2848 1 Plug Gage Valve Guide Inspection BTC 2848 2 Plug Gage Valve Guide Inspection BTC 3615 Plug Gage Valve Guide Inspection BTC 93 73...

Page 25: ...emove filter from the engine and place on a drain tray Allow oil to drain through a clean cloth to determine if foreign material drains from the filter 2 Using the Champion CT 470 Can Cutter open the filter as follows See photos Oil Filter Can Cutter CT 470 0 a Insert threaded adapter in female threads of filter or screw rotating bushing on male threads of filter b Slightly tighten cutter blade ag...

Page 26: ... 3A 5 8 hex 3882 3 5 8 hex 3882 4 3 4 hex Cylinder Base Nut Wrench Special modified 3882 type wrench this special wrench is perfect for those occasional situations when the 3882 wrench won t fit It s a slightly different configuration as shown 8079 9 16 hex Cylinder Base Nut Wrench For 470 and 520 Series The special configuration of these wrenches permits access to the cylinder base nut areas as s...

Page 27: ...der size with universal joint action Optional set for use on TCM cylinders CFL1o Standard 3 to 4 1 4 CFL10 7 Optional 4 to 6 1 2 Crankshaft Blade and Dampener Bushing Removers Replacers Back up plates and forcing screws are rugged heat treated alloy steel Be sure to keep forcing screws greased 4965A 3604 3607 3607 1 8068 for 5 8 1 0 Bushing for 3 4 LO Bushing for 15 32 LO Bushing for GTSI0 520 for...

Page 28: ...with adapters Universal Cylinder Holding Fixture 5221 B This is a heavy duty precision fixture manu factured to extremely close tolerances Suitable for use on vertical mills or drill presses It allows quick indexing of required angles for valve work FEATURES For all Continental Engines Fixture indexes in all present positions required to machine valve guides Locks in at these angles 11 45 12 12 40...

Page 29: ...r wear Spring Checker 7521 A Per Continental Bulletin M74 16 Check valve spring quickly and easily Hy draulically actuated extremely accurate readout 0 160 pounds Includes step gauges for all required dimensions 7521 Checker Is less step gauges Max spring dimensions Ht 2 1 2 O D 2 Heat Shrink Type Valve Guide Removers Cold Force Removal Type Tough heat treated steel 3611 375 l D Gulde 2874 436 438...

Page 30: ...Driver and Adapter Assemblies also avaHable Individually The 8098 10 Base must be used with 8118G 811H 8118 J and 8118K Driver and Adapter Assemblies Makes rocker arm bushing removaljinstallation fast and easy All components of 8118 set are also available Individually Piston Ring Compressors Flexible Band Type 4901 for 3 7 8 and 4 1 6 bore engines 2839 for 5 and 5 1 4 bore engines 3818 for 4 7 16 ...

Page 31: ... with spring loaded tubes The 68 3 compresses the spring which can then be removed with furnished clips Eliminates wiring springs together to install slmply Insert spring then pull off clip Includes Instructions Flaring Tool for Push Rod Housing 4951 A For A C Serles expanding ball type tool Balls rotate inside housing expanding it into 122 aluminum boss J Valve Guide Remover 4981 Removes guides b...

Page 32: ...ncludes 1 Handle kwer assembly 12 Puller heads size to fit all Continental engines 1 O Installer pilots 1 Remover plug 6 feet of super flexible hose to attach to water supply Instructions Storage case Tool is rigged for removaL Center is plugged to route water Ovt thru small holes in rim oi removing head Fig 1 Installer Valve Seat Inserts 4910 For 1 45 64 0 0 Exhaust and 1 53 64 0 0 Intake Inserts...

Page 33: ...VALVE SEATS AND GUIDES CAN BE RE ALIGNED QUICKLY Here s how It s done Step 1 Removed old guides and seats Step 2 Install Expanding Gulde Body Into valve seat boss Step 3 Place Boring Bar Into Guide Bore valve guide boss concentric and perpendicular to valve seat Follow up with Reamer Step 4 Use your drill press for bore or ream operations as shown In this picture The same guide set up works for bo...

Page 34: ...Hole Dia 8116 16 525 8116 28 530 8116 38 535 8116 48 54 0 8116 58 545 8115 68 555 8116 108 620 8116 118 625 8116 128 630 8116 138 635 8116 148 640 8116 158 650 Example Use 8116 68 Boring Bar to bore hole to 555 then finish with 811 6R Reamer to 561 dia Expanding Minimum Maximum Body No Retracted Dia Expanded Dia 8116 1 1 656 1 681 Expanding 8116 2 1 685 1 710 Guide 8116 3 1 748 1 773 Bodies 8116 4...

Page 35: ...s for use in extracting studs from cylinder assemblies using Rosan type Studs Using the hammer drive the stud driver 1 over stud 2 as far as possible without making contact with the cylinder head 3 Using the ratchet or pull handle apply a firm constant pressure In the clockwise tightening direction the serration 4 on the stud will strip When the stud gives reverse the ratchet and back the stud out...

Page 36: ...hich as a dial indicator reading in ten thou sandths of an inch 0001 The gauge body is lapped into the mating bushing for accurate readings Instructions are included Adapter Kits 8042C for 520 470 E Series 8072C for 0 200 0 300 360 1 125 1 00 922 Reamers Connecting Rod Bushing High speed steel reamers with 3 4 diameter pllot Use with 8111A Base Retainer Kit and proper Adapter Kit as shown above 87...

Page 37: ... cutter By using the 8122A with the proper pilot from below you may choose to pHot into valve stem hole or valve guide boss Pilots All pilots are hardened and precision ground for accuracy Two choices pilot into valve stem hole or valve guide boss Piiot Choice No 1 Pilot Into Valve Stem Hole On new lnatallatlona only Part No Piiot Dia _ 8098 10 Base Included 8122A Common Drive Handle This handle f...

Page 38: ...haft Once the bushing Is removed or Installed a turn of the valve returns actuator for another cycle 8077A Includes 10 000 p s I pump and cylinder 5 ton output cylinder 3 ft long flex hydraulic hose all adapters to fit 0 300 and 360 470 and 520 Serles 80778 Oess hydraulics includes Items shown above in 8077A except no hydraulics are furnished The actuator head has 1 4 NPT female port for connectin...

Page 39: ...ate also rotates aso0 and locks In place with heat treated lock pin Flange holder Is pre drRled to accept all Con tinental engines Threaded adapters Included to mount non flanged crankshafts Shipping weight 400 lbs Tork Band Tension Adjuster 7726 Adjust belt tension without damage to compo nents Use on alternators compressors etc Allows grabbing difficult round components Generator Drive Holder Ho...

Page 40: ...ses w fittings 1 Propane Regulator 2 Controls 1 Y Connector 1 Stand 2 Cylinder Risers All screws nuts and washers needed and instructions Blind Needle Bearing 8093C Puller Use to remove 5 8 l D needle bearings in 470 and 520 Series engines Use with 8054 Slide 46 Hammer Starter Clutch Shaft Bearing Pullers 80930 for removing 3 4 l D bearings Controls Y Connector Regulator Standaro 20 lb Propane Tan...

Page 41: ...e maximum belt and bearing life The proper belt tension eliminates slippage and increases efficiency of belt driven opponents Compact only 3 1 4 wide to fit in crowded areas Easy to use just apply gauge to belt release ball handle and read tension on rotating diaf Calibrated for A section V belts 3 8 to 1 2 top width and K section 4 5 and 6 rib poly V belts Range 30 to 180 lbs and 130 to 800 newto...

Page 42: ...rotected Two point hook up field term and cigarette lighter Engine Timing Disc 3608A For all engines universal application from J3 to OC3 Fastens to prop tip and accurate to 1 4 degree Includes piston stop 3608A 15 PuUeyHolder 4974 For holding 2 1 2 to 3 1 2 dia pulleys grip in pulley groove Pulley Alignment Gage Bar 8082 The 8082 gage bar allows a quick and easy alignment check between driver she...

Page 43: ...ration Heavy steel wall 0 30 in Hg nozzle fits several sizes of tubing Generator Pulley Puller 61 5 Quick removes pulleys from 2 1 2 to 5 diameter Applies even pressure on outside of pulley in pulley groove All components are tough heat treated alloy steel Bearing and Bushing 8094B Drill Fixture Per Continental Bulletin 79 1 0 Use to rework your present stock of main journal bearings and starter s...

Page 44: ...u bolt dowel boss prior to inserting improved thru bolt with 0 ring seal Spark Plug Insert Tap 504 1 Use on all engines Spark Plug Insert Remover 4919 Use on all engines Slide Hammer 8054 Heavy duty slide hammer features 2 1 2 lb slide and 5 8 18 thread 24 long overall Use with 8114 Series removers Spark Plug Tap 445 18 millimeter threads High speed steel e 2 28 ...

Page 45: ...rills with pre set stops To modify 470 Scavenge Pump per Continental Bulletin M72 8 Drill Fixture 8025 For drllllng and Installing piston oft squirt nozzles In 0 470V engines converting to 0 470VO per Continental Bulletin M75 13 10 470 to 10 47008 Includes all drllls drill bushings and stops required to a fast and efficient job Crankcase Splitter Set L423 Makes splitting Continental crankcases eas...

Page 46: ...aterial removal Cutter blades are heat treated highspeed steel 8048 Spot Facer for 470 and 520 Runout Block Set 8177A Use this set to check runout on crankshafts etc up to 4 diameter Blocks are aluminum alloy with Teflon bearing surfaces Approx size 4 w x s 1 x5 h each Polishing Tools for Crankshafts Bearings Special aluminum frame and felt polishing surfaces 8087A 1 7 8 to 2 1 4 dia 80878 2 1 4 t...

Page 47: ...eel for durabllity Torque input and output Is marked on extension installer Is special thin walled 6 pt 1 2 hex socket Crankcase Thru Bolt Removers Use with 8054 Slide Hammer to remove stubborn bolts 8114 8 8114 7 8114 6 Remover 1 2 20threads Remover 7 16 20 threads Remover 3 8 24 threads Hex Drive for Hex Tube Nut 7912A Tubing nut wrench set for fuel systems hydraulic systems and brakes Rotabroac...

Page 48: ...1153 Pullers These pullers provide a more controlled method to remove press fit parts 679 1035 1079 2 32 927 1063 ...

Page 49: ... inside of holes to outside edges Dial Bore Gages Dial Bore Gages used for large volume go no go Inspections or for determination of actual dimensions Three point contact two guide pins and one interchangeable rod assure alignment within bore Zero point may be set with ring gage micrometer height master or gage blocks NOTE Ali prec1s1on measuring devices must have a current calibration that is tra...

Page 50: ...ble V Anvil Type 60 degree V Anvil and Conical Spindle are made of high grade special steel hardened and precision ground Depth Micrometers The Depth Micrometer is one of the basic measuring tools selected by machinists Rachet stop for consistent and repetitive measurements NOTE All precision measuring devices must have a current calibration that is traceable to the National Bureau of Standards 2 ...

Page 51: ...5129 1 5129 2 786 Pilot 5129 4 818 Finishing Use with 5129 1 5129 3 815 Pilot 5129 5 833 Finishing Use with 5129 1 5129 2 5129 3 5129 4 815 Pilot Reamer Rocker Shaft Bushing 5130 751 Std 707 Pilot Reamer Rocker Arm Bushing 7232 751 Std 732 Pilot Reamers Valve Guide Boss Use at 275 RPM maximum USE MORSE ADAPTER 4914 1HS 537 005 O S 531 Pilot 2689 4914 2HS 542 010 O S 534 Pilot 2689 4914 3HS 552 020...

Page 52: ...Gauges are used to check for new limits and service limits where applicable Gauges are heat treated alloy steel precision ground 2848 1 2848 2 3615 436 l D Guide 438 l D Guide 375 l D Guide USE MORSE CUTTING PILOT ADAPTER DIA 438 344 344 375 438 436 DIA NO 422 2686 331 2684 331 2684 363 2684 422 2686 422 2686 Suggestions For Reaming Valve Guide Stem Holes 1 Use high quality cutting oil 2 Reamers a...

Page 53: ...e English and Metric Measure Inside Measuring Instruments Three measuring surfaces are lapped parallel to the longitudinal axis of the Micrometer and stay aligned with the bore while measurements are taken Large ratchet stop provides constant measuring pressure to the wall surface and insures repet itive reading to 0002 or 0001 smaller ranges NOTE All precision measuring devices must have a curren...

Page 54: ... test alternators regulators batteries on 12 and 24 volt systems with currents up to 32 volts DC Has a pointer zero adjustment screw on the face of the instrument Circuitry is entirely solid state and no battery or power source is required Power for the unit is derived from the systems under test Multiple Voltage Circuit Tester For 12 24 Volts Model29 Designed to test continuity of circuits shorts...

Page 55: ...tor Model E25 Improves the accuracy and speeds up the process of timing an aircraft magneto to the engine Easily attached to the propeller spinner with mounting bands Has top dead center locator Cold Cylinder Test Model E10 Attach one wire with an alligator clamp and use another cable with a hand held probe to test comparative temperatures from cylinder to cylinder in a matter of seconds Spot sour...

Page 56: ... voltage pulses test insulation for leak Built in continuity lamp provides handy test of electrical connections Uses two c cell flashlight batteries Includes top grain cowhide carrying case Master Orifice Tool P N 646953 Attach to differential cylinder pressure tester to check calibration and determine the low leakage limit Ref TCM Service bulletin M84 15 ...

Page 57: ... volt LCD unit with a disposable battery Temperature Range 10000 1soooF Part Numbe 85328 Alcor Portable Digital CHT Unit This device is used with Type J Thermocouple It is a lightweight 9 volt LCD unit with disposable battery Temperature Range 200 6oooF Indication from 32 0000F WARNING Keep equipment and personnel clear of prop area 2 41 Part Number 85329 ...

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Page 59: ...ge 3 1 Description of Engine Model Code 3 2 3 2 Basic Design Features 3 2 3 3 Lubrication System 3 2 3 4 Induction System 3 3 3 5 Exhaust System 3 3 3 6 Turbocharger System 3 4 3 7 Ignition System 3 4 3 8 Fuel System 3 4 3 9 Cylinders 3 5 3 10 Valve Train 3 5 3 1 ...

Page 60: ...ve located in the oil cooler Engine cranking is accomplished by a geared right angle drive starter adapter and a direct current starter motor A gear driven alternator is installed on the right front side of the crankcase forward of the number 5 cylinder The engine is equipped with two gear driven magnetos The exhaust system is supplied by Teledyne Continental Motors 3 3 LUBRICATION SYSTEM Oil is d...

Page 61: ... f5 0 z m t m f5 TO GOVERNOR PAO OIL TRANSFER COLL AA TURBOCHARGER I t r v WASTI GATE CONTROLLER OIL SUCTION OIL THRU RELIEF VALVE OILTHAU TEMPERATURE CONTl IOL VALVE OIL UNDER PRESSURE OIL FROM GOVERNOR TURBOCHARGER RETURN ...

Page 62: ...ore efficient engine and turbocharger operation The induction air passes through the core of the after cooler and transfers some of its heat to the cooling fins which are exposed to the relatively cooler ram air The manifold is an air distribution system mounted on top of the engine It serves to carry induction air to the individual cylinder intake ports The cylinder intake ports are cast into the...

Page 63: ...BIENT AIR INLET EXHAUST GAS DISCHARGED EXHAUST WASTEGATE J EXHAUST GAS _ _ DISCHARGED TURBINE FIGURE 3 2 INDUCTION AND EXHAUST SYSTEM SCHEMATIC COMPRESSOR HOUSING AIR INLET COMPRESSED AIR DISCHARGE MAIN DRIVE HOUSING EXHAUST INLET TURBINE WHEEL FIGURE 3 3 TURBOCHARGER SECTIONAL 3 5 ...

Page 64: ...tch plate until it is forced inward by the coupling cover When the latch plate is released the coupling spring spins the magneto shaft through its neutral position and the breaker opens to produce a high voltage surge in the secondary coil The spring action permits the latch plate magneto and breaker to be delayed through a lag angle of 30 degrees to drive gear rotation during the engine cranking ...

Page 65: ... fNG1NE ftAING ORDER I 6 J 2 5 4 MAGN TO FIRING ORDER 1 2 3 4 5 6 FIGIJRE 3 4 IGNITION WIRING DIAGRAM DECK PRESSURE ABSOLUTE PRESSURE REGULATOR IDLE CUTOFF MIXTURE CONTROL FULL RICH l TURBINE WHEEL FOR ELECTRICAL FUEL FLOW I I SENSING ENGINE SET UP t ONLY NOT PART OF ENGINE FIGURE 3 5 FUEL INJECTION SYSTEM SCHEMATIC 3 7 ...

Page 66: ...re applied For this reason fuel flow may be accurately determined by measuring the pressure at the manifold valve Refer to Chapter 13 Performance Charts All of the items described above are interdependent on each other to meter the correct amount of fuel according to the power being developed by the engine 3 9 CYLINDERS The externally finned aluminum cylinder heads are heated and threaded on to th...

Page 67: ...CHAPTER 4 ENGINE SPECIFICATIONS AND OPERATING LIMITS Section Index Section Page 4 1 General 4 2 4 2 Engine Specifications 4 2 4 3 Operating Limitations 4 3 4 4 Accessories 4 4 4 1 ...

Page 68: ...n Width 42 50 In Height 33 50 In Engine Weight Dry No oil in sump Complete Engine Includes Crankcase assembly crankshaft assembly camshaft assembly valve drive train cylinder assemblies pistons 6 connecting rod assemblies oil sump assembly inter cylinder baffling alternator starter starter adapter assembly lubrication system includes oil filter accessory drives ignition system includes spark plugs...

Page 69: ...ification Refer to Chapter 9 for Spec MHS 24 or MHS 25 All Temperatures 15W 50 20W 50 Below 50 F Ambient Air Sea Level SAE 30 or 1OW 30 Above 30 F Ambient Air Sea Level SAE 50 Oil Pressure Idle Minimum psi 10 Normal Operation psi 30 to 60 Oil Sump Capacity U S Quarts 8 Usable Oil Quarts 16 Nose Up 5 Usable Oil Quarts 10 Nose Down 4 5 Oil Consumption Lb BHP Hr Max at rated power and RPM Oil Tempera...

Page 70: ...93 PL350 SL350 RHB32E RHB32N RHB32P RHB32W RHB33E RHB36P RHB36W LJ360 ACCESSORIES DRIVE RATIOS TO CRANKSHAFT Viewing Drive Direction of Accessory Rotation Tachometer CCW Magneto ccw Starter ccw Alternator Gear Dr CW Propeller Gov CW Fuel Pump Injection cw Accessory Drives 2 CW Acey Drive Optional ccw CW Clockwise and CCW Counterclockwise Drive Ratio to Crankshaft 5 1 1 5 1 48 1 3 1 1 1 1 1 1 5 1 3...

Page 71: ...VAL Section Index Page 5 1 Unpacking 5 2 5 2 Preparation for Service 5 2 5 3 Engine Installation Instructions 5 3 5 4 Pre Flight and Run Up 5 4 5 5 Flight Testing 5 4 5 6 Engine Removal Instructions 5 5 5 7 Ground Handling 5 6 5 8 Crating and Shipping 5 6 5 1 ...

Page 72: ...e engine is to be installed within five 5 days after unpacking remove the shipping plugs installed in the lower spark plug holes and tum the crankshaft through at least two complete revolutions in order to remove the cylinder preservation oil from the cylinders Remove the shipping plugs installed in the upper spark plug holes and inspect the cylinder bores with a flashlight or borescope for rust o...

Page 73: ...pass as one assembly Remove 2 nuts 2 bolts from turbomounting bracket remove 4 nuts 4 bolts from turbomounting flange remove 2 turbochargers engine is now ready for installation on airframe NOTE Install according to airframe manufacturer s instructions NOTE Remove all protective covers plugs caps and identification tags as each item is connected or installed 1 After engine is installed reinstall t...

Page 74: ...10 40 22 30 I I 7 32 12 88 FIGURE 5 1 INSTALLATION DRAWING TSI0 520 BE 5 4 ...

Page 75: ...I 42 20 14 62 ___ ____8 25 1 FIGURE 5 2 INSTALLATION DRAWING TSI0 520 BE 5 5 ...

Page 76: ...sure that the piston rings have seated and that no induction system exhaust system oil or fuel system leaks exist prior to releasing the aircraft for normal service Ambient air and engine operating temperatures are of major concern during this test flight Accomplish a normal pre flight run up in accordance with the aircraft flight manual Conduct a normal take off with full power and monitor the fu...

Page 77: ...tructions 3 Remove engine to airframe connections in accordance with airframe manufacturer s instructions 4 Disconnect and plug hoses from wastegate actuator and turbochargers Install caps on wastegate and turbocharger fittings to prevent entrance of foreign matter Remove clamp from left hand turbocharger tail pipe remove tie rod from right hand side of turbo bypass assembly remove left hand tailp...

Page 78: ...the engine or components If contact has occurred inspect for obvious or consequential damage 5 8 CRATING AND SHIPPING Category A cardboard container Lower engine onto container base and attach with metal banding straps Install and attach container cover Category B wooden container Lower engine onto container base Attach engine using shock mounts and bolts Cover engine with plastic bag Install and ...

Page 79: ...6 2 Prestarting 6 2 6 3 Starting 6 2 6 4 Cold Starts 6 3 6 5 Flooded Engine 6 3 6 6 Hot Starts 6 3 6 7 Ground Warm Up 6 3 6 8 Pre Takeoff Check 6 4 6 9 Power Control 6 5 6 1 o Take Off 6 6 6 11 Climb 6 6 6 12 Cruise 6 7 6 13 Descent 6 7 6 14 Landing 6 8 6 15 Engine Shutdown 6 8 6 1 ...

Page 80: ...LL Blue or 100 Green If the minimum grade required is not available use a higher rating Never use a lower rated fuel WARNING The use of a lower octane rated fuel can cause pre ignition and or detonation which can damage an engine the first time high power is applied possibly causing engine failure This could most likely occur on takeoff If the aircraft is inadvertently serviced with the wrong grad...

Page 81: ... to operate the primer intermittently for a few seconds in order to prevent the engine from stopping 6 5 FLOODED ENGINE 1 Mixture Control IDLE CUT OFF 2 Throttle 1 2 OPEN 3 Master Switch On 6 6 HOT STARTS 4 Both Magnetos On 5 Start Switch Start 6 When engine starts retard the throttle and slowly advance the mixture control to FULL RICH position Use the same procedure as for normal start except hav...

Page 82: ...ssary for warm up and testing 5 Increase engine speed to 1700 RPM only long enough to perform the following checks a Check Magnetos The difference between the two magnetos operated individually should not differ more than 50 RPM with a maximum drop for either magneto of 150 RPM Observe engine for excessive roughness during this check WARNING Absence of RPM drop when checking magnetos may indicate ...

Page 83: ...he cooler oil passages or air channels are obstructed Oil temperature above the prescribed limit may cause a drop in oil pressure leading to rapid wear of moving parts in the engine c Cylinder Head Temperature Any temperature in excess of the specified limit may cause cylinder or piston damage Proper cooling of cylinders depends on cylinder baffles being properly positioned on the cylinder heads a...

Page 84: ...igh power settings low airspeed extreme ambient temperature etc If excessive temperatures are noted and cannot reasonably be explained or if abnormal cowl flap and or mixture settings are required to maintain temperatures then an inspection should be performed to determine the cause Possible causes of high temperatures may include broken or missing baffles inoperative cowl flaps sticking oil tempe...

Page 85: ...ustment will prevent sudden spikes in cabin altitude At high altitude large reductions in manifold pressure may cause some reduction of cabin pressure 6 13 DESCENT Descent from high altitude is to be accomplished at cruise power settings and mixture control positioned accordingly CAUTION Rapid descents at high RPM and idle manifold pressure setting are to be avoided During Descent monitor cylinder...

Page 86: ...icated on fuel boost pump capability of providing 16 to 19 gallons per hour through the engine fuel system at wide open throttle full rich mixture engine stopped Priming to be done with wide open throtUe fu l rich mixture At temperatures above 20 F discontinue priming before cranking At temperatures of 20 F and betow continue priming while cranking 20 0 20 40 60 80 TEMPERATURE F AMBIENT FIGURE 6 1...

Page 87: ... Fire During Start 7 2 7 2 General In Flight Information 7 2 7 3 Engine Roughness 7 2 7 4 Turbocharger Failure 7 3 7 5 High Cylinder Head Temperature 7 4 7 6 High Oil Temperature 7 4 7 7 Low Oil Pressure 7 4 7 8 In Flight Restarting 7 4 7 9 Engine Fire In Flight 7 5 7 1 ...

Page 88: ...being used Do not arbitrarily go to Full Rich as the roughness may be caused by an overrich mixture 2 Magnetos Check On If engine roughness does not disappear after the above the following steps should be taken to evaluate the ignition system 1 Throttle Reduce power until roughness becomes minimal 2 Magnetos Turn Off then On one at a time If engine smooths out while running on single ignition adju...

Page 89: ...y When the proper mixture ratio is reached the engine will start Continue to adjust the mixture control unit until the correct fuel flow for the manifold pressure and RPM is obtained NOTE An interruption in fuel flow to the engine can cause engine power loss due to turbocharger run down At high altitude merely restoring fuel flow may not cause the engine to restart because the mixture will be exce...

Page 90: ...es proceed as follows 1 Cowl Flaps Open 2 Airspeed Increase 3 Power Reduce if steps 1 and 2 do not lower oil temperature CAUTION If these steps do not restore oil temperature to normal an engine failure or severe damage can result In this case it is recommended that the aircraft manufacturer s emergency instructions be followed 7 7 LOW OIL PRESSURE If the oil pressure drops without apparent reason...

Page 91: ...s manifold pressure until engine tempe ature reaches operating range Adjust mixture as required With Unfeathering Accumulator a Propeller Control FORWARD OF FEATHERING DETENT UNTIL ENGINE ATTAINS 600 RPM THEN BACK TO DETENT b Oil Pressure STABILIZED NOTE If propeller does not unfeather or the engine does not turn return the propeller control to the feather position and secure the engine c Mixture ...

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Page 93: ...ABNORMAL ENVIRONMENTAL CONDITIONS Section Index Section Page 8 1 General 8 2 8 2 Cold Weather Operation 8 2 8 3 Preheating 8 2 8 4 Hot Weather Operation 8 4 8 5 Ground Operations At High Altitude Airports 8 5 8 1 ...

Page 94: ...expected at temperatures below normal provided the engine is in good condition and the ignition and fuel systems are properly maintained The following procedures are recommended for preheating starting warm up run up and takeoff 1 Select a high volume hot air heater Small electric heaters which are inserted into the cowling opening do not appreciably warm the oil and may result in superficial preh...

Page 95: ...suddenly to less than 30 psi shut down the engine and inspect the lubrication system If no damage or leaks are noted preheat the engine for an additional 10 to 15 minutes before restarting 6 Before takeoff run up the engine to 1700 RPM If necessary approach this RPM in increments to prevent oil pressure from exceeding 100 psi At 1700 RPM adjust the propeller control to Full Decrease RPM until mini...

Page 96: ... will afford additional protection for a parked aircraft Flight operation during hot weather usually presents no problem since ambient temperatures at flight altitudes are seldom high enough to overcome the cooling system used in modern aircraft design There are however three areas of hot weather operation which will require special attention on the part of the operator These are 1 Starting a hot ...

Page 97: ...fficult from 30 minutes to one hour after shutdown Following that interval the fuel vapor will be less pronounced and normally will present less of a restart problem 2 Ground Operation in High Ambient Temperature Conditions Oil and cylinder temperatures should be monitored closely during taxiing and engine run up Operate with cowl flaps full open Do not operate the engine at high RPM except for ne...

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Page 99: ...G AND UNSCHEDULED MAINTENANCE Section Index Section Page 9 1 Servicing 9 2 9 2 Approved Products 9 3 9 3 Preflight Inspection 9 4 9 4 50 Hour Inspection 9 4 9 5 100 Hour Inspection 9 5 9 6 Unscheduled Maintenance 9 6 9 1 ...

Page 100: ...y responsible for the airworthiness of the airplane the owner or operator should select only qualified personnel to maintain the airplane Fuel Min Grade Aviation Grade 100 or 100LL WARNING The use of lower octane rated fuel can result in destruction of an engine the first time high power is applied This would most likely occur on takeoff If the aircraft is inadvertently serviced with the wrong gra...

Page 101: ... Company Quaker State Oil Refining Co Red Ram Limited Canada Mobil AV 1 BP Aero Oil Castrolaero AD Oil Chevron Aero Oil Conco Aero S Delta Avoil Oil Exxon Aviation Oil EE Gulfpride Aviation AD Mobil Aero Oil Pennzoil Aircraft Engine Oil Phillips 66 Aviation Oil Type A X C Aviation Multiviscosity Oil SAE 20W 50 SAE 20W flJ Quaker State AD Aviation Engine Oil Red Ram X C Aviation Oil 20W 050 Shell C...

Page 102: ...ecifications so that necessary repair or adjustment can be accomplished 2 Oil Filter 3 Oil 4 Air Filter 5 High Tension Leads 6 Magnetos 7 Magneto Filter 8 Visual 9 Exhaust System 10 Adjustments Repairs 11 Engine Condition Replace filter inspect cartridge Change oil if integral screen or small filter is used Inspect and clean or replace as necessary Inspect for chafing and deterioration Check and a...

Page 103: ...ration Check Adjust points and timing if necessary NOTE Minor changes in magneto timing can be expected during normal engine service The time and effort required to check and adjust the magnetos to specifications is slight and the operator will be rewarded with longer contact point and spark plug life smoother engine operation and less corrective maintenance between routine inspections NOTE At eac...

Page 104: ...outlined in TCM TBO Service Bulletin 86 6R1 or current revisions as applicable 9 7 CYLINDER COMPRESSION Leakage CHECK The differential pressure test is an accepted method of determining cylinder condition by measuring air pressure loss past the pistons rings and valves The operation of the equipment is based on the principle that for any given airflow through a fixed orifice a constant pressure dr...

Page 105: ...TO SPARK PLUG ADAPTER FIGURE 9 1 f l ASTER ORIFICE ASSEMBlY TOOL BORROUGHS P N 646953 STATIC SEAL Borroughs Tool Equipment Corp 2429 N Burdick St Kalamazoo Ml 49007 Tel 616 345 2700 CYLINDER HEAD BARREL SEAL CYLINDER WALL DIMENSION ANO CHOKE FIGURE 9 2 9 7 DYNAMIC SEAL ...

Page 106: ... reading After the master orifice calibrated pressure reading has been recorded close regulator pressure valve and remove Master orifice Tool from the cylinder adapter A schematic diagram of a typical differential pressure tester is shown in Figure 9 3 Performing The Check The following procedures are listed to outline the principles involved and are intended to supplement the manufacturer s instr...

Page 107: ... The source of air leakage should first be checked for the static seal Positive identification of static seal leakage is possible by listening for air flow sound at the exhaust or induction system cylinder port When checking the cylinder head to barrel leakage use a soapy solution between the fins and watch for bubbles use a soapy solution also around both spark plugs seals for leakage NO LEAKAGE ...

Page 108: ...tatic leakage replacement or repair inspect piston ring gap and cylinder wall for tolerance Ref Dynamic Seal Figure 9 2 Once the piston and the cylinder have been cleaned inspected and ring gap tolerance have been met reassemble to the engine Dynamic Seal Check 11 To check the dynamic seal of a cylinder proceed with the leakage test and observe the pressure and indication of the cylinder pressure ...

Page 109: ...ing removed and repaired Rework of cylinder should be accomplished as outlined in the engine overhaul manual and service bulletins FIRST CHECK I CHECK FOR METHOD 1 DISCREPANCY 2 CORRECTIVE 2 CORRECTIVE ACTION ACTION Carbon Stake Valve Intake Valve to Seat Listen for air Flow in Cracked Cylinder Replace Cylinder Seal Intake Port Seat Worn or Burned Grind or Replace Reinspect Valve Worn or Burned Gr...

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Page 111: ...1 General Information 10 2 10 2 Engine Troubleshooting Chart 10 2 10 3 Ignition Troubleshooting Chart 10 9 10 4 Oil System Troubleshooting Chart 10 1 o 10 5 Fuel Injection System Troubleshooting Chart 10 11 10 6 Exhaust System Troubleshooting Chart 10 13 1 1 ...

Page 112: ...leshooting chart is provided as a guide Review all probable causes given check other listings of troubles with similar symptoms items are presented in sequence of the approximate ease of checking not necessarily in order of probability TROUBLE Engine Will Not Start PROBABLE CAUSE Fuel tank empty Improper starting procedure Cylinder overprimed Engine flooded Induction system leak Excessive Starter ...

Page 113: ...ion malfunction Restrictions in air intake passages Fuel injection malfunction Piston rings excessively worn or broken Piston rings are not seated 10 3 CORRECTION Use low pitch INCREASE RPM position for all ground operations See Troubleshooting the Fuel Injection System Tighten loose connection or replace damaged part See Troubleshooting the Fuel Injection System Use FULL RICH position for all gro...

Page 114: ...te gate valve Malfunctioning turbocharger Exhaust system gas leakage Low Octane fuel Lean fuel air mixture due to improper manual leaning pro cedure Cylinder baffles loose or bent 10 4 CORRECTION Tighten mounting bolts Replace mount pads Clean Remove and repair See Troubleshooting the Ignition System Replace Clean Repair cylinder Remove and clean or replace Check and adjust linkage See Rigging of ...

Page 115: ...haft oil seal Around propeller mounting flange damaged hub o ring seal Around plugs fittings and gaskets due to looseness or damage Piston rings excessively worn Valve faces and seats worn Excessively worn cylinder walls Mixture too rich Mixture too rich Mixture too rich Fuel manifold valve not seating tightly Fuel manifold valve sticking closed 10 5 CORRECTION Clean thoroughly Check ignition and ...

Page 116: ...l system excessive fuel temperature Fuel gage line leak or air in gage line 10 6 CORRECTION Repair or replace manifold valve Repair or replace manifold valve Operatefuel boost pump accord to aircraft manufacturer s instruc tions See fuel flow per Chapter 13 Check mixture control for full travel Check for restrictions in fuel filters and lines adjust control and dean filter Replace damaged parts Ch...

Page 117: ...iscosity Malfunctioning oil temperature control valve in oil cooler oil cooler restriction Replace valve or clean oil cooler Check for restricted lines and loose connections and for partially plugged oil filter or screens Clean parts tighten connections and replace mal functioning parts Check manifold connections for leaks Tighten loose connections Check fuel control and linkage for setting and ad...

Page 118: ...e service air cleaner Check accessible cables and connections Replace malfunctioning spark plugs This troubleshooting chart is provided as a guide Review all probable causes given check other listings of troubles with similar symptoms Items are presented in sequence of the approximate ease of checking not necessarily in order of probability TROUBLE Engine Fails To Start Due to Ignition Trouble PRO...

Page 119: ...ondenser Tighten to specified torque Adjust to proper gap Check for faulty inspection Replace points and condenser Oean spark plugs Replace dead spark plugs Adjust to proper gap Referto Installation of Magnetos and Ignition Timing for proper timing procedure Replace points and condenser Replenish Clean thoroughly Remove cooler and flush thoroughly This troubleshooting chart is provided as a guide ...

Page 120: ...alkaline solids is dueto a previous clean ing with alkaline materials Replace pump Check gage Clean plumbing Replace if required Replace spring Adjust pressure to 30 60 psi by adjusting screw This troubleshooting chart is provided as a guide Review all probable causes given check other listings of troubles with similar symptoms Items are presented in sequence of the approximate ease of checking no...

Page 121: ...t gage connection Engine getting fuel 10 11 CORRECTION Loosen one line at nozzle If no fuel shows with fue1 ftow on gage replace fuel manifold valve Remove nozzles and clean Adjust fuel air control unit in accordance with adjustment procedures Adjust fuel air control unit in accordance with adjustment procedures Lower unmetered fuel pressure Replace worn elements of Remove and clean all nozzles Im...

Page 122: ... TROUBLE Engine Lacks Power Reduction in Maximum Manifold Pressure Or Critical Altitude White Smoke Exhaust PROBABLE CAUSE Improperly Adjusted Wastegate valve Loose or damaged exhaust system Malfunctioning turbocharger Exhaust system gas leakage Turbo coking oil forced through seal turbine housing 10 12 CORRECTION To check the adjustment of the fixed wastegate valve refer to the airframe seivice m...

Page 123: ... Section Page 11 1 Engine Preservation After Overhaul 11 1 11 2 Flyable Storage 7 to 30 days 11 2 11 3 Temporary Storage up to 90 days 11 2 11 4 Indefinite Storage 11 3 11 5 Returning Engine to Service 11 4 11 6 Indefinite Storage Inspection Procedures 11 4 ...

Page 124: ...cts of combustion In consideration of the circumstances mentioned TCM has listed three reasonable minimum preservation procedures that if implemented will minimize the detriments of rust and corrosion It is the owner s responsibility to choose a program that is viable to the particular aircraft s mission Aircraft engine storage recommendations are broken down into the following categories A Flyabl...

Page 125: ...vative oil approximately two ounces through the oil filler tube e Seal all engine openings exposed to the atmosphere using suitable plugs or moisture resistant tape f Engines installed in aircraft that are preserved for storage in accordance with this section should have a tag affixed to the propeller in a conspicuous place with the following notation on the tag DO NOT TURN PROPELLER ENGINE PRESER...

Page 126: ...an 25 hours 4 Re install the spark plugs and rotate the propeller by hand several revolutions to check for possible liquid lock Start the engine 5 Give the aircraft a thorough visual inspection and test flight per airframe manufacturer s instructions 11 6 INDEFINITE STORAGE INSPECTION PROCEDURES Aircraft prepared for indefinite storage should have the cylinder dehydrator plugs visually inspected e...

Page 127: ...CHAPTER 12 AIRWORTHINESS LIMITATIONS 12 1 ...

Page 128: ...00 hour inspections as described in the TSI0 520 BE series overhaul manual and inspections mandated by the FAA under Part 43 and 91 of the Federal Aviation Regulations are required for type certification 3 Other Related Procedures Subject to additional information contained in FAA Approved Mandatory Service Bulletins issued after the date of certification the TSI0 520 BE erigine does not have any ...

Page 129: ...CHAPTER 13 ENGINE PERFORMANCE AND CRUISE CONTROL Section Index Section Page 13 1 Cruise Control By Performance Curve 13 2 13 2 Cruise Control By T l T 13 3 13 3 Performance Charts 13 4 13 1 ...

Page 130: ... inlet temperature indicator is used as an aid to leaning proceed as follows 1 Adjust RPM for desired cruise setting 2 Slowly move mixture control toward lean while observing T l T gage Note position on the instrument where the needle peaks or starts to drop as mixture is leaned further 3 The maximum recommended cruise setting is 235 HP at 2400 RPM and 31 0 Hg MAP with the mixture set at 25 F to 5...

Page 131: ...Mixture Ratio Curve 80 2500 RPM and 32 8 Hg ADMP 13 8 13 6 Mixture Ratio Curve 75 2400 RPM and 32 5 Hg ADMP 13 9 13 7 Mixture Ratio Curve 65 2300 RPM and 30 0 Hg ADMP 13 10 13 8 Mixture Ratio Curve 50 2200 RPM and 25 8 Hg ADMP 13 11 13 9 Fuel Flow Vs Brake Horsepower 13 12 13 10 Metered Fuel Pressure Vs Fuel Flow 13 13 13 11 Fuel Injection Fuel Pump Pressure PSIA Vs Rated Horsepower 100 F AVGAS 13...

Page 132: ... 4 220 I UJ t I 200 ffi 8 t 1 r 1 1 1 r 1 1so t w a 160t8 i 75 f t 1 t 140 r r JI I w Full Throttle BSFC i I I 09 70 i J j i t 120 t u I l fJ 0 w 65 a c f 2 UJ Q I 60 i l t 11 t t I iii Pro Load BSFC 155 i FIGURE 13 1 SEA LEVEL PERFORMANCE 13 4 ...

Page 133: ...ir temperature at throttle body 115 F 3 420 avg CHT 180 200 F oil RPM 320 2600 300 2500 280 2400 260 2300 I a I CL UJ I 240 I 2200 1 0 l L L _ _ i __ l __ 1 J_21 00 220 j 12 18 20 22 24 26 28 30 32 34 36 38 2000 200 180 0 I FIGURE 13 2 CONSTANT SPEED SEA LEVEL PERFORMANCE FULL RICH MIXTURE 13 5 ...

Page 134: ...on air temperature at throttle body 115 F 3 420 F Avg CHT 180 200 oil i RECOMMENDED q__ J cRu ISE RANGE I 22 24 I 26 28 I 32 34 RPM 340 2600 320 2500 300 2400 280 2300 2200 260 2100 240 2000 220 200 180 160 140 120 36 38 FIGURE 13 3 CONSTANT SPEED SEA LEVEL PERFORMANCE BEST POWER MIXTURE 13 6 ...

Page 135: ...3 MIN FUEL GRADE 100 1OOLL COMP RATIO 7 5 1 INLE STD ATMOSPHERE WITHOUT RAM 320 MAX CONT 2600 RPM 38 IN HG ADMP 300 5 280 c rl m a 260 240 0 c 220 a c 0 200 m 180 m rl 0 160 D r 1 I l I i 36 0 IN HG I I v i RFCO MENDED CRUISE 2400 RPM 31 IN HG ADMP v I I l_ r I K I I s 140 z I I 0 1 120 I I 100 I I I w PRESSURE AlTITUOE IN FEET ...

Page 136: ... 400 375 350 I UJ f i f H L 1 Z I o1 i 1 a I w w t t ol f UJ z o 1 I 1 I 260 240 Standard Day Test Cell _ 1 1 Data Sea Level 90 100 110 120 130 140 FIGURE 13 5 MIXTURE RATIO CURVE 80 2500 RPM AND 32 8 Hg ADMP 13 8 ...

Page 137: ... I I a w 1600 a Avg T rbine Inlet Temp E w I I J 1500 w J z w z en a I Standard Day Test Cell Data Sea Level i 1 1 i 80 90 100 110 120 130 140 150 I 11 FIGURE 13 6 MIXTURE RATIO CURVE 75 2400 RPM AND 32 5 Hg ADMP 13 9 ...

Page 138: ... 0 w a r 60 J a UJ l I J CD u 55 I m I I 1 U 200 a 0 I w 180 a lil w z 50 O Q WI 45 J a co z o Ao I 1 NOTE Standard day test cell data sea level l 75 85 90 95 100 105 I I I I FUEL FLOW LBS HR I FIGURE 13 7 MIXTURE RATIO CURVE 65 2300 RPM AND 3o o Hg ADMP 13 10 ...

Page 139: ... 1500 I _EMPERATURE i z a l i ___ 1 _wt1 m 1400 o e i I ffi I w 1 a t 1300 L CL G t t 4 a I ffi _ _ i _II 60 __ __ ___ __a 1 f 1 J 170 1 1 BHP uJ I fu i ro U 55 160 00 i 0 ro I I 2 UJ __ftl 1 50 I 150 l CL z II vvBSFC a I Q ro E i 45 t i 4 1 I C I _ I a 1 E ID B z _ ___ 40 1 i _ J I NOTE STAN OARD DAY TEST CELL 1 1 i 8 60 65 70 I DATA I AT SEA LEVEL I I I FUEL FLOW LBS HR I I I I I 1 1 1 11111 111...

Page 140: ...B GAL 1 l 7 t t f _ r 1 l 160 m r l l 1 140 0 R l l h oi_ t f f lf l l 1 J i 120 r BEST POWER APPROXIMATE I I I I i PEAK T LT APPROXIMATEt 100 5j I I I I BEST ECONOMY APPROX R o J _ t jf 25 SO F LEAN OF PEAK EGT i i i 80 I 140 150 190 200 230 240 250 260 270 280 290 300 310 ...

Page 141: ...ITHOUT INFLUENCE OF DIFFERENTIAL FUEL HEAD IN GAGE LINE i5 c 20 NOMINAL TOLERANCE 30 PSI XI m AVGAS 78 F m I m XI m 0 c m r w ti XI m CJ CJ c XI m c m r Tl r 0 E 16 v m I m l v 0 _c _ 12 m r U D m U en v c n 8 m I 0 l L 4 i E _E r 0 40 80 120 160 200 240 280 c I I I I FUEL FLOW LBS HR l I I I I I 11111 111111111 111111111 1111111111 111111111 111111111 1111111111 1111111111111111111111111111111111...

Page 142: ...0 0 1 1 q 0 j 1 0 J LL J w IJ Cl w I a x Cl r m a J m J s I 0 J IJ 0 0 0 0 0 U v C C I FIGURE 13 11 FUEL INJECTION FUEL PUMP PRESSURE PSIA VS RATED HORSEPOWER 100 F AVGAS 13 14 0 a 0 v 0 I w J 0 i tri Cl w I a ...

Page 143: ...1 111111111 11111111 111111111 111111111 11111 I I I I I I E E v I v I v i I E MAXIMUM PRESSUR DROP ALLOWABLE ACROSS A SUITABLE FLOW TRANSDUCER I E I E _ 5 1 0 1 5 2 0 2 5 3 0 3 5 4 0 4 5 5 0 5 5 6 0 E I I I I I I 111111111 111111111 111111111 111111111 111111111 11111111 111111111 111111111 111111111 111111111 111111111 11111 PRESSURE PSIG FIGURE 13 12 FUEL FLOW VS PRESSURE DROP 13 15 ...

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