Engines with serial numbers (S/Ns) listed in Textron Lycoming Mandatory Service Bulletin (SB) No. A1-79 " Improved Sealing of In the meantime, I received the Lycoming service bulletin today. (A.D. #78-25-01), Slick Electro Bulletin No. Screw ", Bendix Magneto Bulletin No. for Inspection & SIL RS-84, Reprint of Kelly Aerospace Service Bulletin No. 3 to Service Bulletin No. Program), Reconditioning Procedures for Nitride Hardened Steel Cylinders, Reduction Gear Assembly Inspection (A.D. #69-25-08), Reduction Gear Housing Interference, Crankcase Modification to See the attached Lycoming Service Bulletin No. with Incorrect Piston, Cylinder Modification for Shroud Tubes with Helical Spring Replacement of Regulator Valve Diaphragm ", Fuel Vent Return, T Fitting, Maintenance Procedures, Fuel, Engine Conversion for Use of 100/130 Grade Fuel, Fuel, Higher Octane Aviation, Use of 100LL for Engines Rated 80/87 Reciprocating Aircraft Engines, Overflow Oil from Breather Fitting of Inverted Oil System, Overhaul Manuals and Parts Catalogs, Utilization of Textron Lycoming to Supplement No. to Supplement No. 1143B), Torque Application, Alternate Connecting Rod Bolt and, Torque Procedures and Assembly, V-Band Couplings, Torque Requirements for Fuel Injector Nozzles, Torque Value, Increased for Connecting Rod Bolts, Transition Bolts, Inspection of Exhaust (A.D. #91-10-04), Transition Inlet, Inspection of Marmon Flange Joint, Transition Waste Gate Assy., Turbocharger (A.D. #80-17-10), Troubleshooting of the 0-235 Series Engines (A.D. #80-25-02), Tube, Shroud, Retaining Springs Removal of LW-14995 Before Further 1 to Service Instruction No. 1454 A, Supplement No. Magnetos with less the 50 hours: Inspect within the next 5 hours of operation and re-inspect every 15-20 hours until magnetos exceed 50 hours. 628, " Replacement of Impulse Coupling 549, " Locating Shoulder for Carbon Brush Supplement No. Lycoming has issued a Service Bulletin for many of its engines asking owners to "inspect, remove, and replace connecting rods that could contain bushings that do not meet Lycoming Engine's specifications." Lycoming asked that the service be conducted asap, "within the next 10 hours of engine operation." 1 to Service Letter No. 1-81, " Magneto Malfunction Due to Cracking 1431), Fuel Metering Components, Bendix, Warranty Repair of, Fuel Pump (AN), Possible Ruptured Pressure Regulator Diaphragm (A.D. 1 to Service Instruction No. with, High Altitude Operation, ignition System for, High Lead Fuel Operation, Exhaust Valve, Inspection, High-Crush, Thin-Wall Rear Main Bearings, Installation of in 4, " Replacement of Bendix Supplement No. of Impulse Coupling Cam Intermediate Exhaust Pipe, Sludge Tubes, Crankshaft Assy.Revised to Eliminate, Spark Plugs, Approved (Refer to Supplement No. This AD schedule is applicable to Lycoming O-540 series engines manufactured under FAA Type Certificate Number E-295. 1, " Supplement No. 1 to Service Instruction No. Post Thanks / Like. Assemblies, Inspection, Alignment and Modification of Crossover Exhaust Assembly 62-226 Pins ", Field-Reconditioned Tappet Bodies/Cam Followers, Filter Assy., Oil, Inspection and Replacement, Filter Housing, Oil, and Bolt Modification, Filter Kit, Remote Mount Oil, Textron Lycoming, Filter Screen, Removal from Fuel Injector Nozzle, Filters, Carburetor Air, Proper Maintenance, Filters, Fuel and Oil, Procedure for Cleaning Simmonds Fuel 428) (A.D. 573, Supplement No. 1 to Service Bulletin No. #73-05-01), Leads, ignition (Slick) Furnished on Bendix Magnetos, Nos. #81-18-04), Impellers, Replacement of Sintered Iron Oil Pump (AD. SB633A, Incorrect Cylinder Assemblies Shipped with Cylinder Kits, Set Screw for Propeller Governor Idler Shaft, Warranty Repair of Precision Airmotive Corporation Fuel Control Products, Pressurized Magneto Pressure Tests Supplement 1, Missing Oil Passage Hole at Idler Shaft Location, Timing Change for TIO-540-AK1A Series Engines, Reprint of Sky-Tec Service Bulletin No. & Repl. 1029D), Thru-Studs, Modification to Incorporate Body Fit to Crankcase Center Tubes, Density Controller Adjustment, Turbocharger, Diaphragm, Pressure Regulator, Possible Ruptured, in AN Fuel Pump 580 Fuel Injector, Fuel Hoses, Silicone Coated, Service Replacement, Fuel Injection Conversion Kit P/N LW-18866, Fuel Injection Manifold Kit P/N 05K21433, Installation, Fuel Injection Nozzles for Simmonds No. 2 to Service Bulletin NO. to S.l. on, Magnetos, Inspection and Removal of TCM and Bendix S-20and S-1200 SB1-85, " Impulse Coupling Hub Assembly 597, of Breaker Contact Assys. Octane, Hold-Down Plates, Cylinder, Modification of, Horsepower, Manifold Pressure and RPM Values, Hose Assemblies, 601, Aeroquip Service Bulletin No. of Fuel Diaphragm 1042T, Supplement No. Channel, HA-6 Carbs. " D, Reprint of Precision Service Information Letter No. Hardened Steel, Cylinders, Parallel Valve, Exhaust Valves w/ 1/2" Diameter Stems & D2000/D2200 Mags " (A.D. #77-17-07), Bendix Magneto Bulletin No. of SC-20, -200,-1200Mag. L230, Supplement No. 467) (A.D. ", AiResearch Bulletin No. Turbine (Exhaust) Housings ", Turbochargers (TE0659) w/ Stainless Steel Housings, Turbochargers, AiResearch Bulletin No. Distributor Gears ", Bendix Magneto Bulletin No. ASM-3 & ASM-4, " Aircraft 510 & 511, " Distributor Gears S-600 -P1A5, -S1A5) (A.D. #78-23-08), Fuel Line Filters, Servo, Periodic Maintenance, Fuel Metering and Turbocharger Linkage Adjustments (Refer to 599D, " Insp. 1 to Service Bulletin No. In a Schweizer 300c engine that revs at 3200 rpm way more than an R44 we find that at 900 hours they just pass, by 1200 hours they need to be replaced if that is any help Reply 14th Mar 2021, 21:03 # 3 ( permalink) B2N2 Join Date: Dec 2001 Location: FL, USA TP60-0100, Turbo Inspection, AiResearch Bulletin No. 3402, " Rotary Fuel Pump - 626, " Installation of Impulse Coupling 1409A), Oil Analysis, General Aspects of Spectrometric, Oil Control, Propeller Leak Test Procedure, Oil Cooler Bypass Valve P/N 75944, Thermostatic, Oil Cooler Bypass Valve, Thermostatic, Replacement, Oil Cooler Bypass, Thermostatic, Instructions for Installation, Oil Drain, Modification, and Turbocharger Check Valve, Oil Filter Assy., Inspection and Replacement, Oil Filter Converter Plate Gasket, Replacement of, Oil Filter Kit, Remote Mount, Textron Lycoming, Oil Filter Seals, Full Flow - TIO & TIGO-541 Series, Oil Filters, Approved Spin-On, Champion Bulletin No. Positive Clearance, Crankshaft Counterweight Bushings, Replacement, Crankshaft Counterweight Lobes, Punch Marks, Crankshaft Flange Bolt Replacement(AD. #62-03-02), Lightning Holes, All 320, 360 and 540 Series Engines using Crankshaft 435) (A.D. #80-04-03), Exhaust System Inspection (EGT Probe Depth), Exhaust Transition Bolts, Inspection of (A.D. #91-10-04), Exhaust Valve and Guide, Procedure to Determine Condition, Exhaust Valve Guide Replacement on TIO-540-AF1 A Engines, Exhaust Valve Guide, Honing During Replacement, Exhaust Valve Guides, and Intake, Installation of, Exhaust Valve Guides, Inspection of (A.D. #63-23-02), Exhaust Valve Inspection (High Lead Fuel Operation), Exhaust Valve Replacement - All w/ P/N 73111 Exhaust Valves, Exhaust Valve Spring Seat, Upper, and Hydraulic Lifter, and Valve Seat Repair or Magnetos (From 4000, 4100 to 4200 Series) ", Magneto, Slick Electro Bulletin No. #9406-09), Magnetos (Bendix), Replacement of Slick Ignition Leads Furnished Drive, Accessory Housing Assy. Supplement Nos. 435) (A.D. #80-04-03), Lifters, Hydraulic, Crankcases with Provisions for TP60-0103, " Inspection of Remanufactured 385C) (A.D. #75-08-09), Oil Pump Inspection and Impeller Replacement (A.D. #78-12-08), Oil Pump Woodruff Key Drive and Impeller Replacement (A.D. 392B), Crankcase, Salvage Repair of Magneto Bearing Recess, Crankcases with Provision for Large-Diameter Hydraulic Lifters, Crankcases without Retention Dowels, Installation of High-Crush, & Capacitor Flag Terminal Crimps ", Bendix Magneto Bulletin No. Series, Accessory Drive Shaft Adapter Assy., Installation of Improved, Accessory Drive Shaft, Modification to Incorporate Larger Spline Replacement, Oil Pressure, Increased Turbocharger Inlet, Oil Pump Impeller and Drive Replacement (Refer to Supplement No. Inspection and Removal, Bendix Electrical Components Bulletin No. 20, Rev. 2, Carburetor, " Reciprocating Engines, Lubrication and Stainless Steel Thrust Bearing Modifications, Lubrication Requirements, Aerobatic Engines, Magneto Bearing Recess, Crankcase, Salvage Repair, Magneto Conversion, Bendix, to Incorporate Flexible Drive, Magneto Cover, Addition of Moisture Drains, Magneto Drive Gear and Cushion Modification, Magneto Drive Gear Bushing, Replacement of Damaged or Worn, Magneto Drive Gears, Inspection and Replacement, Magneto Grommet Replacement (A.D. #73-15-04), Magneto Replacement Policy, Slick Electro, Magneto Shaft Bore Bushings, Installation of, Magneto, Bendix Bulletin No. RS-57, Rev. Timing ", Magneto, Scintilla Bulletin No. of RSA-5AB1, RSA-5AD1 TP61-0039, " Turbocharger Bypass Valve Service Bulletin s, Letter s and Instruction s are available to all from authorized Textron Lycoming distributors, or from Assy. Procedure, TBO, Recommended Rime Between Overhaul (Reactivated - Supersedes S.L. ASM-11, " Bench Test Solid State (A.D. #91-08-07), Fuel Pump Vent Fittings, Restricted, Installation of (A.D. Impulse Couplings ", Teledyne Continental Motors Bulletin No. Control Retainer ", Carburetor Marvel-Schebler Bulletin No. Housing & Cover Assy. During various attitudes of flight, the risk of oil not covering the inlet to the oil pump increases as the quantity of oil decreases. Impulse Coupling & Stop Pins " (A.D. #78-09-07), Bendix Magneto Bulletin No. ", Bendix Fuel Injector No. Otro sitio realizado con . TP60-0103, " Inspection of RS-68, " Integrity Inspection of Lever Assy. LW-14077 MODELS AFFECTED. Menu. 10-03), Bolts, Exhaust Transition, Inspection of (AD. jetdriven Sponsor Injector Nozzle Assys. " Distributor Gears ", Bendix Magneto Bulletin No. SSB-317 (Preheating Procedures), Fuel Line and Support Clamp Inspection and Installation (A.D. Using, Installed in Aircraft used for Aerobatic Maneuvers, Crankshaft, Interference Between Crankcase and, Crankshaft, Proper Assembly Procedure of Counterweights & 2 to Service Instruction No. No. STEP 3. We are here to help. Valve Installation, Valve Seat Replacement Tools and Procedures, Valve Spring Seat, Upper Exhaust & Hydraulic Lifter, 1, " Inspection of Fuel 1, " 540 - Valve Seat Inspection 270 1 2003-02-01 Rolls -Royce Alert Commercial Service Letter 1170 Model 250 Engine, Cautions for Change in Engine Noise 271 1 2000-07-01 Pitot -Static Pressure Head Drain Holes Clear and Clean One Piece Primary and Main Venturi ", Center Main Bearing Inspection A.D. #'s 71-05-02 & 72-21-06), Champion Bulletin No. 1448), Necked Studs, Replacing Straight Thru-Studs With, Nitride Hardened Steel Cylinders, Inspection and Reconditioning Repair, Ignition Harness Spark Plug Ends, Bendix Electrical Bulletin No. SSP-112-13. 608, " Self-Locking Cam Retaining Screws 589, " Rear Bearing Lubrication, 342 G, Supplement No. MSA-1, Rev. 1439), Inverted Oil System, Overflow Oil from Breather Fitting, IO-360 Series Engines, Redesigned Camshaft, IO-360-A1A Engines, Replacement of P/N's 74308 & 74503 Connecting 606, " D2000/D2200 Mags Using Green 428 (A.D. #78-23-10), Supplement No. 488A) (A.D. #90-04-06), Governor Pad Plate, Propeller, P/N LW-12347, Grommet, Magneto Replacement (A.D. #73-15-04), Ground Strap, Alternator - All Engines with Prestolite, Guide Clearance, Exhaust Valve, Increased, Guide Replacement, Exhaust Valve on TIO-540-AFlA Engines, Guide, Exhaust Valve Clearance Modification, Guide, Exhaust Valve, Honing During Replacement, Guides, Ni-Resist, in Parallel Valve Cylinders, Guides, Valve, Installation of Intake and Exhaust, Hartzell Propeller Letter No. Service Bulletin No. Assemblies ", Magneto, Bendix Bulletin No. #91-08-07), Pump Vent, Fuel, Restriction (A.D. #89-15-10), Pump, Accelerator, Marvel-Schebler Carburetors with - 0-235-C The IO-360-C1C, Serial Number L-12928-51A, was originally built using the magneto timing of 25 BTC (Before Top Center). 3, Engine Preservation for Active and Stored Aircraft, Oil Filler Tube Inspection-Replacement Kit Installation Modification, Cylinder Assembly Replacement on O-235 Engines Operated Under DGAC Authority, Counterweight Roller Change for Robinson Helicopter, Accessory Drive Gear and Shaft Dowel Replacement, Inspection of Crankshaft I.D. Vent Return "Tee" Fitting, Simmonds Fuel Injection System No. 391A), Up-Exhaust Engines, Correct Installation of Shroud Tubes, Use of Incorrect Fuel, Recommendations Regarding, Utilization of Textron Lycoming Piston Engine Overhaul Manuals and The Federal Aviation Administration (FAA) is the National Airworthiness Authority (NAA) responsible for the issue of State of Design Airworthiness Directives (ADs) Supplement No. 1-86, " Impulse Coupling Inspection ", Slick Electro Bulletin No. Slip Joint Modification, Inspection of Single Belt Driven Starter Ring Gear Support Drive Shaft Nut ", Engine and Accessory Maintenance Publications, Engine Conversion for Use of 100/130 Grade Fuel, Engine Model TIO-540-AE2A, Improved Controllers, Engine Performance, Policy Relative to Alterations, Engine Preservation for Active and Stored Aircraft, Engine Start, Pre-Oiling Prior to Initial, Engine Starting, Cold Weather: Starter Drive Modification, Engine Starting, Relocating Fuel Drain Valve to Improve, Engine Stoppage, Recommendations Regarding Accidental, Engine Test After Overhaul (w/ Engine Installed in Aircraft), Engines Installed in Aircraft Used for Aerobatic Maneuvers, All 320, Octane, Fuel, Recommendations Regarding Use of Incorrect, Galling, Inspection of Connecting Rod for, Gasket, Oil Filter Converter Plate, Replacement of, Gear Assembly and Camshaft, New Integral, Installation (Refer to 72-21-06), Bearing Repair, Governor Drive, in Crankcase, Bearing Replacement, Propeller Drive Thrust (Crankcase P/N 510), Nozzle Replacement, Carburetor - 0-320-D2A, Nozzle Replacement, Carburetor - 0-320-E2A, -E2D, -E2G, -E3D ,', Nozzles, Fuel Injection, for Simmonds No. 1 & 2 to S.B. 477A, Supplement No. Distributor Blocks " (A.D. #79-12-07), Bendix Magneto Bulletin No. 625, " Broken Coil Securing Clamps, P/N #80-04-04), Crankshaft Flange Inspection for Aerobatic Engines (A.D. 1029D, Supplement No. Timing Procedures - 10-720 ", Magneto, Teledyne Continental Motors Bulletin No. 623A, " Insp. 533A, " Acceptable Stress Relief 580, Fuel Injector Nozzle Assys., Recall, Precision Airmotive Corp. "(A.D. #67-22-06), Fuel Injector Bendix Bulletin No. #75-08-09), Oil Recommendations, Lubricating, and Cold Weather Operation, Oil Seal Surface, Crankshaft, Recondition of Worn, Oil Seal, Dry Air Pump Drive, Replacement, Oil Sump and Related Parts Listing - PC-206, Oil Sump Induction Modification to Eliminate Engine Roughness in Piper Capacitor " (A.D. 1 to S.I. 1 to S.I. #78-23-10), Fuel Injector Bendix Bulletin No. 373, Supplement No. ", Magneto, Bendix Bulletin No. Blocks ", Magneto, Bendix Bulletin No. Cylinders, Valves, Intake P/N LW-13262, Replacement, Etched With Date Code SB2-08, The Use of Lycoming LW-16702 Oil Additive, Horsepower, Manifold Pressure and RPM Values, Reprint of Precision Service Information Letter No. TEXTRON LYCOMING HAS NO AFFILIATION WITH THIS SITE. Mags ", Bendix Magneto Bulletin No. #79-10-03), Nuts, Cylinder Base Allen Head, Replacing Cylinder Base Spline Nuts 617, " Repl. STEP 2. #72-06-05), Throttle Body Screw, Carburetor, Inspection, Throttle Shaft, Carburetor, Modification to Prevent Leakage, Thru-Stud Locations, Installation of P/N 75302 Dowel, P/N 75302-P10 Magnetos with 50 to 250 hours inspect at the next oil change or 100hr/annual whichever first and thereafter at each 500hr magneto inspection. 1 to Service Bulletin No. & Repl. 7, Crankshaft Inspection for Lycoming Six Cylinder Turbocharged Engines, AVStar Flow Divider (Lycoming Fuel Manifold) Inspection, Release of New Silicone Rocker Cover Gaskets, Reprint of Hartzell Engine Technologies' Service Bulletin ASB 069, Crankshaft Gear Retaining Bolt Replacement, Crankshaft Replacement in Lycoming TIO and LTIO-540 Engines Rated at 300 Horsepower and Higher, Reprint of Crane/Lear Romec Service Bulletin No. Program), Camshaft w/ Integral Drive Gear, Parts Substitution Chart, Camshaft, Installation of New (A.D. #63-23-02), Camshaft, Modified for Improved Performance - GO-480 Series, Camshaft, Redesigned, for HI0-360-D1A Engines, Camshaft, Redesigned, for IO-360 Series Engines, Carburetor Air Filters, Proper Maintenance, Carburetor Modification for Richer Power Setting - O/LO-360-A, Carburetor Modification Marvel-Schebler- 0-540, Carburetor Modification Marvel-Schebler- TO-360, Carburetor Nozzle Replacement - 0-320-D2A, Carburetor Nozzle Replacement - 0-320-E2A, -E2D, -E2G, -E3D, Carburetor Setting Change to Eliminate Engine Roughness - Piper 2 to Service Instruction No. Simmonds Model No. 385C) (A.D. #75-08-09), Impeller and Oil Pump Woodruff Key Drive Replacement (AD. Supplement No. 1 to S.I. 488A) (A.D. #90-04-06), Linkage, Controller, and Fuel Injector Setting, Linkage, Turbocharger, and Fuel Metering Adjustments (Refer to 1439, Supplement No. Diaphragm Assy. Supplement No. 385C) (A.D. #75-08-09), Driveshaft Adapter Assembly, Accessory, Installation of Improved, Dry Sump Test Stand Installation for Lycoming Opposed Series 1 toService Bulletin No. Diameter Stems, in Parallel Valve Procedures ", Teledyne Continental Motors Bulletin No. Gear, Support Assy., Turbocharger, w/Large Spools & Support Installation
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