Und Aerospace
Service difficulty reports · 117
Reports filed under designator OG5R by a repair station, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE submitter_designator = 'OG5R' AND submitter_type_code = 'B' ORDER BY difficulty_date DESC, sdr_id DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE submitter_designator = 'OG5R' AND submitter_type_code = 'B' ORDER BY difficulty_date DESC, sdr_id DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2020FA0000365Seal · debondedDURING PHASE INSPECTION FOUND THE FORWARD CRANKSHAFT SEAL LOOSE AND LEAKING. UPON REMOVAL FOUND THE ADHESIVE USED BY THE MANUFACTURER HAD FAILED TO ADHERE TO THE ENGINE CRANKCASE ALLOWING THE SEAL TO ROTATE WITH THE CRANKSHAFT. THIS HAS BECOME A COMMON PROBLEMSDR OG5R2016FA0000315Washer · brokenENGINE DRIVEN FUEL PUMP PLUNGER RETAINING METAL WASHER AND PLASTIC WASHER BROKE OFF AND WAS FOUND IN THE OIL SCREEN AND OIL SUMP. BOTH PIECES WERE FOUND CRACKED IN HALF.SDR OG5R2016FA0000314Washer · brokenENGINE DRIVEN FUEL PUMP PLUNGER RETAINING METAL WASHER AND PLASTIC WASHER BROKE OFF AND WAS FOUND IN THE OIL SCREEN AND OIL SUMP. BOTH PIECES WERE FOUND CRACKED IN HALF.SDR OG5S2016FA0000139Muffler · crackedMUFFLER CRACKED INTERNALLY ALLOWING EXHAUST GASES TO ENTER HEATING SHROUD, THEREBY ALLOWING FUMES INTO CABIN.SDR OG5R2016FA0000046Muffler · crackedCRACKED MUFFLER ALLOWING EXHAUST FUMES TO ENTER THE CABIN.SDR OG5S2015FA0000356Pump · leakingON POST FLIGHT, PILOT REPORTED FUEL DRIPPING FROM BOTTOM OF COWL. UPON FURTHER INSPECTION BY MAINTENANCE, IT WAS DETERMINED THAT THE ENGINE DRIVEN FUEL PUMP WAS THE SOURCE OF THE LEAK. PUMP WAS REPLACED, OPS AND LEAK CHECK WAS GOOD.SDR OG5R2015040600123Muffler · crackedSPOT WELDS ON MUFFLER SEPARATED RELEASING EXHAUST INTO HEAT EXCHANGER.SDR 2015FA0000061Strut · leakingDURING PHASE INSPECTION MECHANIC NOTED BOTH MLG STRUTS LEAKING FLUID. UPON DISASSEMBLY TO REPACK STRUTS MECHANIC FOUND APPROXIMATELY .5 CUP OF ALUMINUM SHAVINGS IN INNER STRUT. FURTHER INSPECTION FOUND OUTER STRUT INNER BORE GROOVED AND GOUGED IN THE AREA OFSDR OG5S2015FA0000041Distributor Gear · detachedAT RUN-UP, FOUND EXCESSIVE MAGNETO DROP ON LT ENGINE, RT MAGNETO. REMOVED MAGNETO AND FOUND DISTRIBUTOR FINGER LOOSE ON DISTRIBUTOR GEAR. THIS IS A COMMON FAILURE. REPLACED MAGNETO WITH SERVICEABLE MAGNETO.SDR OG5R2014FA0000694Bushing · wornPILOT REPORTED CONTROL YOKES WERE GRINDING, DURING VISUAL INSPECTION FOUND SUPPORT GUIDE, FOR CONTROL YOKE BUSHING, BOTH TO BE WORN WITH SUPPORT GUIDE TO BE PENETRATING MATERIAL MORE THAN 75 PERCENT.SDR OG5S2014FA0000691Longeron · crackedDURING ANNUAL INSPECTION, A LONGERON WAS FOUND CRACKED AT THE AFT MLG ATTACHMENT HOLE ON BOTH SIDES.SDR OG5S2015FA0000042Distributor Gear · detachedRIGHT MAGNETO, RT ENGINE OPERATED INTERMITTENTLY. REMOVED AND DISASSEMBLED. FOUND DISTRIBUTOR FINGER LOOSE ON DISTRIBUTOR GEAR. THIS IS A COMMON PROBLEM. INSTALLED SERVICEABLE MAGNETO.SDR OG5S2014110400651Actuator · failedDURING INSPECTION, DISCOVERED TRIM ACTUATOR WOULD JAM IN BOTH UP AND DOWN TRAVEL. TOTAL ACTUATOR TRAVEL WAS ABOUT .5 OF SPECIFIED TRAVEL. REPLACED TRIM ACTUATOR.SDR OG5R2014110400650Injector · malfunctionedON RUN UP, FOUND THAT THE THROTTLE CONTROL WOULD STICK AT LOW RPM. WHEN ENOUGH FORCE WAS APPLIED TO MOVE PAST THE STICKING POINT THE RPM WOULD JUMP 200-400 RPM. AFTER DISCONNECTING THE THROTTLE CONTROL WE FOUND THE CONTROL WAS SMOOTH. THIS MADE IT DIFFICULTSDR OG5R2015FA0000043Distributor Gear · detachedAIRCRAFT HAD BAD MAGNETO DROP RIGHT ENGINE RIGHT MAGNETO. REMOVED AND DISASSEMBLED MAGNETO. FOUND DISTRIBUTOR FINGER SEPERATED FROM DISTRIBUTOR GEAR. THIS IS A COMMON PROBLEM. INSTALLED SERVICEABLE MAGNETO.SDR OG5R2014100900593Pump · failedDURING PHASE INSPECTION, DISCOVERED FOUR PIECES OF STEEL IN OIL SUCTION SCREEN. PIECES DETERMINED TO BE SWAGED WASHER FROM TOP OF ENGINE DRIVEN FUEL PUMP PISTON ROD. NO ABNORMAL OPERATION NOTED BY PILOTS. REPLACED FUEL PUMP.SDR 2013FA0000255Line · crackedPILOT REPORTED HIGH EGT AND ROUGH RUNNING ENGINE DURING LAST 30 MINUTES OF FLIGHT. DURING POST FLIGHT, FUEL WAS NOTED ON RT ENGINE AND WRITTEN UP. DURING INSPECTION, A FUEL SUPPLY HARD LINE WAS FOUND CRACKED UNDER THE B-NUT AT THE FLAIR. THIS LINE HAD BEEN RSDR 2012FA0000679Bracket · brokenDURING PHASE INSPECTION, THE RT OTBD, INBD FLAP TRACK BRACKET, BROKEN AT UPPER AFT END OF AFT TRACK. FLAP ATTACH POINTS WERE UNDAMAGED. BRACKET REPLACED AND ACFT RETURNED TO SERVICE.SDR 2012FA0000583Cap · migratedDURING SCHEDULED INSPECTION INNER NOSE STRUT TUBE UPPER CAP RIVETS WERE FOUND TO BE MIGRATING. INNER STRUT TUBE REPLACED WITH OLD STYLE TUBE.SDR 2012FA0000561Strut · damagedDURING SCHEDULED INSPECTION, INNER NOSE STRUT TUBE UPPER CAP RIVETS WERE FOUND TO BE MIGRATING.SDR 2012FA0000351Strut · damagedDURING SCHEDULED INSPECTION, INNER NOSE STRUT TUBE UPPER CAP RIVETS WERE FOUND TO BE MIGRATING.SDR 2012FA0000350Manifold · obstructedENGINE ROUGHNESS REPORTED BY CREW. PROBLEM CONFIRMED BY MX AND TROUBLESHOT TO FUEL DISTRIBUTION MANIFOLD NOT DISTIBUTING FUEL EQUALLY TO ALL CYLINDERS. MANIFOLD AND ENGINE ONLY HAD 7.6 HRS TSMOH BY MFG. MANIFOLD WAS REPLACED AND ENGINE RAN SMOOTHLY.SDR 2012FA0000287Tire · deflatedNOSE TIRE DEFLATED ON LANDING.SDR 2012FA0000286Tire · deflatedNOSE TIRE DEFLATED ON LANDING.SDR 2012FA0000282Oil Cap · looseAFTER LEVELING OFF AT 5,500 MSL THE CREW BEGAN LEANING MIXTURES AND THE RT ENGINE RPM BEGAN TO DROP AT A STEADY RATE. NO ENGINE ANNUNCIATORS APPEARED AND ALL ENGINE INSTRUMENTS READ NORMAL AFTER 15 SECONDS THE RT PROP WENT FULL FEATHER AND THE ENGINE WAS SHUTDSDR 2011FA0000645Pin · shearedNLG STRUT PINS SHEARED.SDR 2011FA0000644Pin · shearedNLG STRUT HAS PINS SHEARED INTERNALLY.SDR 2011FA0000643Tube · damagedNLG INNER TUBE SEPARATED.SDR 2011FA0000641Pin · shearedNLG PINS SHEARED ON INNER STRUT TUBE.SDR 2011FA0000642Tube · damagedNLG STRUT TUBE HAS PIN HOLES ELONGATED.SDR 2011FA0000649Pin · brokenNLG STRUT TUBE HAS A BROKEN PIN.SDR 2011FA0000647Pin · missingPINS MISSING.SDR 2011FA0000639Tube · separatedNLG INNER STRUT TUBE PIN MIGRATING LOOSE.SDR 2011FA0000648Tube · separatedINNER TUBE SEPARATED.SDR 2011FA0000646Tube · separatedNLG STRUT INNER TUBE SEPARATING.SDR OG5R20110719001Tire · deflatedFLAT TIRE DURING LANDING ROLL OUT; WHILE TAXIING TO PARK THE ACFT.SDR OG5R20110714001Tire · deflatedLT MAIN TIRE WENT FLAT ON TAXI. RECURRING PROBLEM.SDR 2011FA0000388Tube · flatWHILE TAXIING, ACFT EXPERIENCES A FLAT TIRE ON THE LT MAIN GEAR AT THE END OF THE TAXIWAY. MX WAS NOTIFIED AND THE TIRE WAS REPLACED. HAVE BEEN EXPERIENCING SEVERAL OF THESE PROBLEMS AND WE HAVE BEEN INSTRUCTED BY OUR SAFETY DEPARTMENT TO SUBMIT SDR FORMS.SDR OG5R20110610001Tire · deflatedNOSE LANDING GEAR TIRE FLAT ON TAXI.SDR OG5R20110714002Tire · deflatedLT MAIN TIRE WENT FLAT ON TAXI.SDR OG5R20110714003Tire · deflatedDURING TAXI, NOSE TIRE WENT FLAT.SDR OG5R20110601001Tire · deflatedFLAT NOSE WHEEL DURING TAXI.SDR 2000ZZZX371Baffle · looseAIRCRAFT WAS WRITTEN UP FOR HAVING A ROLL TENDENCY. INVESTIGATION BY MAINTENANCE FOUND INTERNAL BAFFLING ON LEFT FUEL TANK HAD COME LOOSE CAUSING TANK HAD COME LOOSE CAUSING TANK TO BUDGE INCREASING THE CAMBER ON THAT WING. FURTHER INSPECTION OF RT TANK FOUNSDR 99ZZZX1383Bolt · shearedPILOT REPORTED SEVERE VIBRATION ON CLIMB-OUT. UPON INITIAL INSPECTION, FOUND SPINNER CRACKED. UPON REMOVAL OF SPINNER, FOUND 5 OUT OF THE 6 PROP BOLTS SHEARED. AIRCRAFT MANUFACTURER NOTIFIED.SDR 99ZZZX1051Connector · misinstalledAIRCRAFT BROUGHT IN FOR VACUUM PUMP FAILURE. BEFORE REPLACEMENT OF PUMP DURING RUN-UP AND OPS CHECK, THE OIL AREA ANNUNCIATOR WAS INDICATING THE VACUUM SYSTEM AND THE VACUUM ANNUNCIATOR WERE INDICATING THE OIL SYSTEM. TROUBLESHOOTING DISCOVERED THE WIRES IN SDR 99ZZZX933Fuel Pump · failedENGINE STOPPED. IN-FLIGHT INSPECTION FOUND ENGINE DRIVEN FUEL PUMP ACTUATING ARM HAD BROKEN AT PIVOT POINT. BROKEN PIECE WAS RETRIEVED FROM SUMP. NO OTHER CONTAMINATION FOUND. PUMP WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. PUMP HAD BEEN IN PARTS ROOMSDR 99ZZZX284Bracket · brokenOIL FILLER TUBE SUPPORT BRACKET FOUND BROKEN AT 90 DEGREE BEND DURING ACCEPTANCE INSPECTION. SUBMITTER STATED THIS IS THE SECOND ONE FOUND BROKEN DURING AN ACCEPTANCE INSPECTION OF SIMILAR AIRCRAFT. PART REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR 99ZZZX311Bracket · brokenDURING ACCEPTANCE INSPECTION, ALTERNATOR BRACKET, P/N 22-2411-10-00, WAS FOUND BROKEN OFF AT THE TOP ALTERNATOR MOUNTING HOLE UNDERNEATH WELD. LACK OF PENETRATION DURING WELDING MAY HAVE BEEN THE CAUSE. PART REPLACED WITH NEW PART. AIRCRAFT RETURNED TO SERVSDR 99ZZZX285Bracket · brokenDURING ACCEPTANCE INSPECTION OF AIRCRAFT, FOUND OIL FILLER TUBE SUPPORT BRACKET BROKEN AT 90 DEGREE BEND. SUBMITTER STATED LEFT UNCORRECTED, THIS COULD ALLOW FILLER TUBE TO BECOME DISLODGED FROM OIL TANK. CONTINENTAL WAS NOTIFIED. PART REPLACED AND AIRCRAFTSDR 99ZZZX278Fuel Injector · malfunctionedENGINE RAN EXTREMELY RICH IN-FLIGHT. QUIT ON FLAIR/ROLL-OUT, COULD NOT RESTART. MAINTENANCE WAS ABLE TO RESTART, BUT ALSO FOUND MIXTURE EXTREMELY RICH AND WAS UNABLE TO ADJUST TO SPECS. SUSPECT INTERNAL LEAKAGE. NO EXTERNAL EVIDENCE. INJECTOR WAS REPLACED
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