# Service difficulty reports: N926PA A list on [N926PA](https://openairdocs.org/aircraft/N926PA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FQAR20190226005](https://openairdocs.org/sdr/FQAR20190226005.md): Rib · cracked · Feb 22, 2019 · N926PA · Piper PA28181 · Wing, Rib/Bulkhead > DURING 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. - [SDR FQAR20190226004](https://openairdocs.org/sdr/FQAR20190226004.md): Rib · cracked · Feb 22, 2019 · N926PA · Piper PA28181 · Wing, Rib/Bulkhead > DURING 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. - [SDR FQAR201807240043](https://openairdocs.org/sdr/FQAR201807240043.md): Channel · cracked · Jul 23, 2018 · N926PA · Piper PA28181 · Fuselage Miscellaneous Structure > DURING 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 INCORRE - [SDR FQAR20180501028](https://openairdocs.org/sdr/FQAR20180501028.md): Bracket · cracked · Apr 29, 2018 · N926PA · Piper PA28181 · Fuselage Main, Attach Fittings > DURING 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 ST - [SDR FQAR20170922090](https://openairdocs.org/sdr/FQAR20170922090.md): Channel · cracked · Sep 22, 2017 · N926PA · Piper PA28181 · Wing Miscellaneous Structure > DURING 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. - [SDR FQAR20170922089](https://openairdocs.org/sdr/FQAR20170922089.md): Channel · cracked · Sep 22, 2017 · N926PA · Piper PA28181 · Wing Miscellaneous Structure > DURING 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. - [SDR FQAR20170922088](https://openairdocs.org/sdr/FQAR20170922088.md): Channel · cracked · Sep 22, 2017 · N926PA · Piper PA28181 · Wing Miscellaneous Structure > DURING 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. - [SDR FQAR20170619049](https://openairdocs.org/sdr/FQAR20170619049.md): Angle · cracked · Jun 19, 2017 · N926PA · Piper PA28181 · Wing Miscellaneous Structure > DURING 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. - [SDR FQAR20170601029](https://openairdocs.org/sdr/FQAR20170601029.md): Doubler · damaged · Jun 1, 2017 · N926PA · Piper PA28181 · Wing Spar > THE 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 COR - [SDR FQAR20161121060](https://openairdocs.org/sdr/FQAR20161121060.md): Bracket · cracked · Nov 21, 2016 · N926PA · Piper PA28181 · Fuselage Main, Attach Fittings > WHEN THE ELT WAS BEING REMOVED FOR INSPECTION, THE TECH DISCOVERED TWO, 2 INCH CRACKS NEXT TO THE NUTPLATES IN THE ELT MOUNTING BRACKET. - [SDR FQAR20151121103](https://openairdocs.org/sdr/FQAR20151121103.md): Carburetor · leaking · Nov 21, 2015 · N926PA · Piper PA28181 · Fuel Control/Reciprocating Engines > AFTER 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 REPORTE - [SDR FQAR20150823091](https://openairdocs.org/sdr/FQAR20150823091.md): Carburetor · failed · Aug 23, 2015 · N926PA · Piper PA28181 · Fuel Control/Reciprocating Engines > WHEN THE CREW ATTEMPTED TO SHUTDOWN THE ENGINE, THE ENGINE REMAINED RUNNING, JUST ROUGHLY; INSPECTION REVEALED THE CARBURETOR WAS THE SOURCE OF THE MALFUNCTION. - [SDR FQAR20150406026](https://openairdocs.org/sdr/FQAR20150406026.md): Throttle Cable · damaged · Apr 2, 2015 · N926PA · Piper PA28181 · Power Lever > DURING 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 INC - [SDR FQAR20140129001](https://openairdocs.org/sdr/FQAR20140129001.md): Tube · failed · Jan 21, 2014 · N926PA · Piper PA28181 · Tire Tube > NLG 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 S - [SDR FQAR20140129002](https://openairdocs.org/sdr/FQAR20140129002.md): Tube · leaking · Jan 19, 2014 · N926PA · Piper PA28181 · Tire Tube > BETWEEN 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 REPAI - [SDR FQAR20140129012](https://openairdocs.org/sdr/FQAR20140129012.md): Tube · failed · Jan 3, 2014 · N926PA · Piper PA28181 · Tire Tube > THE 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 HA - [SDR FQAR1303021301302](https://openairdocs.org/sdr/FQAR1303021301302.md): Pump · worn · Mar 2, 2013 · N926PA · Piper PA28181 · Fuel Boost Pump > ENGINE 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. - [SDR 20000809SH008](https://openairdocs.org/sdr/20000809SH008.md): Gasket · torn · Jul 11, 2000 · N926PA · Piper PA28181 · Fuel Storage > AFTER SHORT PERIOD OF USE, GASKET HAD DETERIORATED AND TORN. SUBMITTER STATED HAVING SEEN NUMEROUS CASES OF THIS IN FLEET OF ARCHER III''S. (X) - [SDR 20000731SH010](https://openairdocs.org/sdr/20000731SH010.md): Gasket · torn · Jun 20, 2000 · N926PA · Piper PA28181 · Fuel Storage > THE 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) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N926PA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.