N926PA

Service difficulty reports · 19

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 n_number = 'N926PA'
  ORDER BY difficulty_date 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.

SDR FQAR20190226005Rib · crackedDURING A SCHEDULED INSPECTION, WING RIBS AT STATIONS 86.03 AND 64.59 WERE FOUND TO BE CRACKED AT THE END RIVIT HOLE UPPER SIDE, REPLACED RIBS WITH NEW.Feb 22, 2019 · N926PA · Piper PA28181 · Wing, Rib/BulkheadSDR FQAR20190226004Rib · crackedDURING A SCHEDULED INSPECTION, WING RIBS AT STATIONS 86.03 AND 64.59 WERE FOUND TO BE CRACKED AT THE END RIVIT HOLE UPPER SIDE, REPLACED RIBS WITH NEW.Feb 22, 2019 · N926PA · Piper PA28181 · Wing, Rib/BulkheadSDR FQAR201807240043Channel · crackedDURING A SCHEDULED INSPECTION, THE DOOR CHANNEL WAS FOUND TO BE CRACKED. THE CHANNEL IS THE MOUNTING LOCATION FOR THE CABIN DOOR HINGES AND CRACKS DUE TO IMPROPER ADJUSTMENTS OF THE DOOR, CREWS PULLING ON THE DOOR GETTING INTO AND OUT OF THE CABIN, AND INCORREJul 23, 2018 · N926PA · Piper PA28181 · Fuselage Miscellaneous StructureSDR FQAR20180501028Bracket · crackedDURING A ROUTINE INSPECTION, FOUND THE FORWARD FLAP HANDLE MOUNTING BRACKET CRACKED, BRACKET IS LOCATED IN THE TUNNEL AND IS THE MOUNTING POINT FOR THE TWO FORWARD BOLTS FOR THE FLAP HANDLE ASSEMBLY, BELIEVE CRACKING IS CAUSED BY FLIGHT CREWS INADVERTENTLY STApr 29, 2018 · N926PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR FQAR20170922090Channel · crackedDURING A ROUTINE INSPECTION A CHANNEL IN THE RIGHT WING WAS FOUND CRACKED. THE CHANNEL IS THE AFT OF TWO CHANNELS RIVETED TO A SKIN ASSY LOCATED INBOARD ON THE RIGHT WING BETWEEN THE LEADING EDGE AND MAIN SPAR.Sep 22, 2017 · N926PA · Piper PA28181 · Wing Miscellaneous StructureSDR FQAR20170922089Channel · crackedDURING A ROUTINE INSPECTION, A CHANNEL IN THE RIGHT WING WAS FOUND CRACKED. THE CHANNEL IS THE FWD OF TWO CHANNELS RIVETED TO A SKIN ASSY LOCATED INBOARD ON THE RIGHT WING BETWEEN THE LEADING EDGE AND MAIN SPAR.Sep 22, 2017 · N926PA · Piper PA28181 · Wing Miscellaneous StructureSDR FQAR20170922088Channel · crackedDURING A ROUTINE INSPECTION, A HAT CHANNEL IN THE LEFT WING WAS FOUND CRACKED. THE CHANNEL IS THE FWD OF TWO CHANNELS RIVETED TO A SKIN ASSY LOCATED INBOARD ON THE LEFT WING BETWEEN THE MAIN SPAR AND THE WING LEADING EDGE.Sep 22, 2017 · N926PA · Piper PA28181 · Wing Miscellaneous StructureSDR FQAR20170619049Angle · crackedDURING A ROUTINE INSPECTION, AN ANGLE IN THE RIGHT WING THAT IS CO-LOCATED WITH THE OUTBOARD FLAP MOUNTING BRACKET WAS FOUND TO BE CRACKED THROUGH THE RIVETS.Jun 19, 2017 · N926PA · Piper PA28181 · Wing Miscellaneous StructureSDR FQAR20170601029Doubler · damagedTHE AIRCRAFT WAS UNDERGOING INSPECTION OF THE WING SPAR IAW SB 978A. DAMAGE TO THE RIGHT WING LOWER AFT SPAR DOUBLER WAS NOTED DURING VISUAL INSPECTION. THE DAMAGE IS A RESULT OF IMPROPER WASHERS INSTALLED WHEN WINGS WERE LAST REINSTALLED ON AIRCRAFT. THE CORJun 1, 2017 · N926PA · Piper PA28181 · Wing SparSDR FQAR20161121060Bracket · crackedWHEN THE ELT WAS BEING REMOVED FOR INSPECTION, THE TECH DISCOVERED TWO, 2 INCH CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET.Nov 21, 2016 · N926PA · Piper PA28181 · Fuselage Main, Attach FittingsSDR FQAR20151121103Carburetor · leakingAFTER ENGINE START, THE ENGINE BEGAN RUNNING VERY ROUGHLY. THE ENGINE RPM BEGAN TO DECREASE STEADILY UNTIL THE ENGINE DIED COMPLETELY. THE PILOTS EXITED THE ACFT AND NOTED FUEL WAS STREAMING FROM OUT OF THE ENGINE COWLING. PILOTS IN ANOTHER AIRCRAFT REPORTENov 21, 2015 · N926PA · Piper PA28181 · Fuel Control/Reciprocating EnginesSDR FQAR20150823091Carburetor · failedWHEN THE CREW ATTEMPTED TO SHUTDOWN THE ENGINE, THE ENGINE REMAINED RUNNING, JUST ROUGHLY; INSPECTION REVEALED THE CARBURETOR WAS THE SOURCE OF THE MALFUNCTION.Aug 23, 2015 · N926PA · Piper PA28181 · Fuel Control/Reciprocating EnginesSDR FQAR20150406026Throttle Cable · damagedDURING INSPECTION, THE THROTTLE CABLE WAS FOUND TO BE COMING APART AT THE SWAGE NEAR THE CARBURETOR. ALL THAT HELD THE CABLE END TOGETHER WAS A RUBBER BOOT; HAD THE CABLE END COME APART, IT WOULD HAVE RESULTED IN A LOSS OF THROTTLE CONTROL. THE SWAGES ARE INCApr 2, 2015 · N926PA · Piper PA28181 · Power LeverSDR FQAR20140129001Tube · failedNLG TIRE DEFLATED WHILE PARKED AND TIED DOWN. THE WHEEL ASSEMBLY WAS REPLACED WITH A SERVICEABLE BUILT UP WHEEL ASSY. THE AFFECTED TUBE WAS INSTALLED AS PART OF A BUILT-UP WHEEL ASSY ON 11/13/2013 AND HAD SINCE ACCRUED 174 HOURS TIME IN SERVICE. THIS REPAIR SJan 21, 2014 · N926PA · Piper PA28181 · Tire TubeSDR FQAR20140129002Tube · leakingBETWEEN FLIGHTS, THE LT MAIN TIRE WAS FOUND FLAT. THE WHEEL ASSY WAS REPLACED WITH A SERVICEABLE BUILT UP WHEEL ASSEMBLY. THE AFFECTED TUBE WAS INSTALLED AS PART OF A BUILT-UP WHEEL ASSY ON 11/13/2013 AND HAD SINCE ACCRUED 174 HOURS TIME IN SERVICE. THIS REPAIJan 19, 2014 · N926PA · Piper PA28181 · Tire TubeSDR FQAR20140129012Tube · failedTHE RIGHT MAIN TIRE WENT FLAT AS THE ACFT WAS EXECUTING A TOUCH-AND-GO LANDING. THE WHEEL ASSY WAS REPLACED WITH A SERVICEABLE BUILT UP WHEEL ASSY WHILE STILL ON THE RUNWAY. THE AFFECTED TUBE WAS INSTALLED AS PART OF A BUILT-UP WHEEL ASSY ON 11/13/2013 AND HAJan 3, 2014 · N926PA · Piper PA28181 · Tire TubeSDR FQAR1303021301302Pump · wornENGINE OPERATED AT LOWER POWER SETTINGS ONLY. ENGINE DIED AT HALF TO FULL THROTTLE. FOUND ELECTRIC FUEL PUMP TO BE INOPERATIVE. UPON FURTHER INVESTIGATION FOUND THAT VALVE SEATS IN THE ELECTRIC FUEL PUMP HAD WORN ALLOWING THE VALVES TO WEDGE INTO THE SEAT. Mar 2, 2013 · N926PA · Piper PA28181 · Fuel Boost PumpSDR 20000809SH008Gasket · tornAFTER SHORT PERIOD OF USE, GASKET HAD DETERIORATED AND TORN. SUBMITTER STATED HAVING SEEN NUMEROUS CASES OF THIS IN FLEET OF ARCHER III''S. (X)Jul 11, 2000 · N926PA · Piper PA28181 · Fuel StorageSDR 20000731SH010Gasket · tornTHE FUEL CAP GASKET DETERIORATES AND TEARS AFTER PUTTING THE FUEL CAP ON AND OFF A FEW TIMES. APPROXIMATELY 10 TIMES OF TAKING THE FUEL CAP ON AND OFF. (X)Jun 20, 2000 · N926PA · Piper PA28181 · Fuel Storage
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