N100UX
Service difficulty reports · 94
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N100UX' AND registry_match = 'registration' 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.
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 = 'N100UX' AND registry_match = 'registration' ORDER BY difficulty_date 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 GLBA20110303FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE FUSELAGE FRAME CRACKED AT FS 273.25 & STR 2R, CRACKS ON INBD & OTBD SIDE OF STRINGER CUTOUT, .7", .8" & .6" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. SDR GLBA20110303JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE FUSELAGE FRAME AT FS 456 CRACKED .3" IN LENGTH AT STRINGER 9AR CUTOUT. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-015. MATERIALS UTILIZED ARE INCLUDSDR GLBA20110228FAKeel · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND LT WHEEL WELL KEEL ATTACH HOLES ARE OVERSIZED, WHERE IB FENDER BRAKET ATTACHES.SDR GLBA20110228FKeel · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND LH WHEEL WELL GRAVEL FENDER HAS LOOSE RIVETS AND IS CRACKED AROUND THE LOOSE RIVETS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-54-SDR GLBA201102231Cap · leakingPILOT REPORTED THAT FUEL WAS LEAKING OUT OF LT MAIN FUEL CAP DURING FLIGHT. MAINTENANCE REPLACED THE LT FUEL CAP IAW BMM 28-20-00.SDR GLBA201009061Autofeather Sys · malfunctionedCYCLED IN DURING APPROACH LT ENGINE ENTERED FEATHER & OUT OF FEATHER. MX TROUBLESHOT AUTOFEATHER SYS, SYS FOUND TO OPERATE NORMALLY IAW BMM 61-21-00.SDR GLBA20090507AUplock Switch · malfunctionedTHE PILOTS REPORTED THAT UPON GEAR RETRACTION OUT OF "LWT" THE GEAR INTRANSIT LIGHT DID NOT EXTINGUISH. VERIFIED THAT ALL GREEN LIGHTS WERE OUT AS WELL. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR UPLOCK SWITCH PERFORMED LANDING GEAR. RETRACTION TEST OPS CSDR GLBA20090506AUplock Switch · dirtyPILOTS REPORTED THAT AFTER TAKEOFF THEY RETRACTED THE GEAR AND THE GEAR HANDLE REMAINED ILLUMINATED. MAINTENANCE TROUBLESHOT THE SYSTEM AND INSPECTED AND CLEANED THE NOSE GEAR UP LOCK SWITCH AND OPS CK WAS GOOD IAW MM 32-60-00. PERFORMED EXTENSION/RETRACTIONSDR GLBA2009042009AController · malfunctionedFLT.5187 WHILE AT FLIGHT LEVEL 25000, LOST CABIN PRESSURE, DEPLOYED O2 MASKS AND RETURNED TO FMN. INFLIGHT EMERGENCY DECLARED. AIR TURNBACK PILOTS REPORTED THAT DURING CRUISE THEY EXPERIENCED A LOSS OF CABIN PRESSURIZATION AT 25000 FT. CABIN WENT TO ZERO SDR GLB2008F00028Skin · crackedMAJOR REPAIR CONFORMITY CHECK OF REPAIR ABOVE AIRSTAIR DOOR PERFORMED. MX FOUND STOP DRILLED CRACKS AROUND 2 RIVETS BOTH 1.25 FROM LT AND RT CENTERLINE OF STRINGER 1 AT 163.975. MX REMOVED OLD PATCH, REMOVED DAMAGED AREAS BY CUTTING OUT .75" SKIN IN BOTH ARESDR GLB2008F00031Motor · burnedPILOTS REPORTED A STRONG ODOR OF SMOKE WITH EYE IRRITATION PRESENT ON TAXI. TURNING OFF BLEEDS TO ENVIRO OFF AS WELL AS TURNING OFF MODE CONTROL, DID NOT CHANGE ODOR . THERE WAS NO VISIBLE SMOKE. MAINT TROUBLESHOT AND FOUND THE SMOKE ODOR TO BE A FLAP MOTOR THSDR GLB2008F00017Bleed Valve · malfunctionedON DEPARTURE FROM "STL" PILOTS REPORTED THAT WHILE FLYING LEVEL AT 7000, AS PILOTS ACCELERATED THROUGH 200KIAS, LT ENG TORQUE BEGAN TO FLUTTER CONSTANTLY 50FT/LBS AND EXPERIENCED MULTIPLE DROPS OF +/-100 FT/LBS. ALL OTHER ENG INDICATIONS NORMAL, +300 FT LB SUSDR GLB2008F00003Skin · crackedPOPPED RIVET HEADS AND CRACK FOUND AT STATION 163.975 ABOVE AIRSTAIR DOOR. MAINTENANCE STOP DRILLED AROUND RIVETS AND REPAIRED THE AFFECTED AREA IAW B1900D SRM 53-90. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. (K)SDR GLBA20060929Unknown · odorPILOTS REPORTED 30 MINUTES INTO THE FLIGHT THAT A BURNING SMELL WAS EVIDENT WITH BLOWERS IN AUTO. PILOTS SELECTED THE BLOWERS OFF AND THE SMELL WENT AWAY. MAINTENANCE INSPECTED BLOWER MOTORS FORWARD AND AFT, FLAP MOTOR, CIRCUIT BREAKER PANELS UNDER THE FLOOR SDR GLBA20060922Skin · delaminatedAIRSTAIR DOOR EXTERIOR SKIN DELAMINATING AROUND DOOR HANDLE AREA. MX REMOVED CORROSION IN AFFECTED AREA AND REPAIRED PER B1900 SRM 52-10-05 FIGURE NR 1.RII INSPECTION COMPLIED WITH PER TC 8.2.1.SDR GLBA20060667Motor · shortedELECTRICAL SMELL IN CABIN - INSPECTED FOUND FLAP MOTOR SHORTED, PLACED ON MEL.SDR 2003788Spar · crackedDURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1 INCH LONG EACH UNDER PANEL 332 ATC. REPAIR WAS MADE AND AIRCRAFT RETURNED TO SERVICE.SDR GLBA20030525Windshield · crackedFO'S CRACKED WINDSHIELD, REMOVED AND REPLACED FO'S WINDSHIELD.SDR GLBA2003525Windshield · crackedFO'S CRACKED WINDSHIELD, REMOVED AND REPLACED FO'S WINDSHIELD.SDR GLBA2003040Actuator · failedLEFT I/B FLAP FAILED TO RETRACT COMPLETELY. REMOVED AND REPLACED FLAP ACTUATOR , OPS CHECK GOOD.SDR GLBA2003015Uplock Switch · out of adjustLANDING GEAR IN-TRANSIT LIGHTS FLICKER WITH GEAR UP, ADJUSTED RT MLG UPLOCK SWITCH OPS CHECKED GOODSDR GLBA2002201O-Ring · failedCLIMBING THROUGH 16000 FT, ALTITUDE HIGH ANNUNCIATOR ILLUMINATED, R&R O-RINGS AND RESECURED CLAMPS OPS CHECK GOODSDR GLBA2002132Engine · overtempLEFT ENGINE OVERTEMPED ON TAKEOFF ROLL, PERFORMED FULL POWER PERFORMANCE RUN UP TQ WITHIN LIMITS.SDR GLBA2002085Tube · damagedRT BLEED AIR FAILED IN FLIGHT. FOUND CHAFED HOLE IN EVA TUBING RT WING. REPAIRED HOLE.SDR GLBA2002068Control Head · stripped#1 NAV SELECT BUTTON STRIPPED, REPLACED CONTROL HAEDSDR GLBA2002064Door · out of rigEMERGENCY EXIT HANDLE NEEDED CHECK. RIGGED DOOR, OPS CHECKED SATISFACTORY.SDR GLBA2002067Rivet · shearedPILOT REPORTED THAT RUDDER PEDAL WAS VERY DIFFICULT TO ADJUST. INSPECTION FOUND THE TORQUE TUBE BEARING HOLDER OUTBOARD SIDE HAD ALL BUT ONE RIVET FASTENER SHEARED (3EA). REPLACED RIVETS AND RETURNED TO SERVICE.SDR GLBA2002047Altimeter · inaccurateCAPTAINS ALTIMETER INDICATION OFF, REPLACED ALTIMETER OPS CHECKED SYSTEM SATISFACTORYSDR GLBA2002034Motor · inoperativeLANDING GEAR RELAY C/B POPPED, REPLACED HYDRAULIC MOTOR OPS CHECKED SYSTEM SATISFACTORYSDR GLBA2001127Connector · looseNR 2 ENGINE OIL FLUX IN FLIGHT. RESECURED OIL PRESSURE SWITCH CANNON PLUG; ADDED 2 QTS OIL TO NR 2 ENGINE. OP'S CHECKED GOOD.SDR GLBA2001109Power Lever · faultyLT POWER LEVER WILL NOT GO INTO GROUND FINE, RT POWER LEVER WILL NOT COME OUT OF GROUND FINE. REMOVED AND REPLACED BOTH POWER LEVERS.SDR GLBA2001086Controller · inoperativeWOULD NOT PRESSURIZE ON CLIMBOUT. REPLACED PRESSURE CONTROLLER.SDR GLBA9137Altimeter · failedCAPTAINS ALTIMETER FAILED AFTER TAKEOFF. REMOVED AND REPLACED CAPTAINS ALTIMETER. SYSTEMS TESTS GOOD. (M)SDR 20000703AP002Circuit Breaker · failedAFTER ENGINE START, CREW SMELLED ELECTRICAL SMOKE ODOR (NO SMOKE VISIBLE) THAT ORIGINATED AT THE CABIN BRIEFER CIRCUIT BREAKER. POWER WAS REMOVED FROM TEH CABIN BRIEFER AND THE AIRCRAFT WAS SHUT DOWN. CABIN BRIEFER CIRCUIT BREAKER WAS REPLACED AND THE CABIN SDR GLBA99014Boost Panel · shortedAIR RETURN FOR SMOKE SMELL IN COCKPIT, FOUND YAW DAMP RUDDER BOOST PANEL CAUSING BURNING SMELL. DISCONNECTED PANEL AND DEFERRED. REPLACED RUDDER BOOST PANEL. (M)SDR GLBA97176Switch · ouf of adjustFRM - FLAPS SELECTED AT 17 DEGREES FOR TAKEOFF. FLAPS WENT TO 35 DEGREES WITHOUT BEING SELECTED. RETURN TO GATE. RIGGED FLAP LIMIT SWITCH. (M)SDR GLBA96103Solenoid Valve · failedDEN - LEFT ENVIRONMENTAL FAIL ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL AND CREW RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED LEFT SOLENOID VALVE. OPS CHECK WAS GOOD. (X)SDR GLBA96063Beta Collar · wornSPW - CREW REPORTED, THE RIGHT PROP WENT INTO GROUND FINE DURING FLAIR, MAINTENANCE REMOVED AND REPLACED RIGHT PROP AND ADJUSTED ENGINE RIGGING FOR TORQUE. OPS CHECKS WERE GOOD. (M)SDR GLBA96031Uplock Switch · lack of lubeFSD - CRWE REPORTED AUTOFEATHER CB POPPED ON FINAL WHEN GEAR WAS SELECTED DOWN. MAINTENANCE LUBRICATED RIGHT GEAR UPLOCK SWITCH. SYSTEM OPS CHECK GOOD. (M)SDR GLBA96030Flap Pos Trans · failedFSD - CREW REPORTED THE FLAPS WOULD NOT RETRACT FOLLOWING TAKEOFF. CREW MADE AN AIR TURN BACK FOLLOWED BY AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED FLAP POSITION INDICATOR TRANSMITTER. SYSTEM OPS CHECK GOOD. (M)SDR 95ZZZM511Ehsi · inopFAR - THE CREW ELECTED AN AIR TURN BACK AFTER THE NR 2 EADI AND EHSI WENT BLANK/INOP FOLLOWED BY A SMALL AMOUNT OF ELECTRICAL SMOKE IN THE COCKPIT. THE LANDING WAS UNEVENTFUL. THE NR 2 VERT GYRO AND NR 2 EHSI WERE SATISFACTORILY REPLACED. (M)SDR 95ZZZM510Vert Gyro · inopFAR - THE CREW ELECTED AN AIR TURN BACK AFTER THE NR 2 EADI AND EHSI WENT BLANK/INOP FOLLOWED BY A SMALL AMOUNT OF ELECTRICAL SMOKE IN THE COCKPIT. THE LANDING WAS UNEVENTFUL. THE NR 2 VERT GYRO AND NR 2 EHSI WERE SATISFACTORILY REPLACED. (M)SDR 95ZZZM142Eva Tube · leakingISN - AFTER NOTING THAT THE LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED, THE CREW ELECTED AN AIR TURN BACK AND ACCOMPLISHED AND UNEVENTFUL LANDING. MAINTENANCE FOUND AND REPAIRED EVA TUBING IN LEFT LEADING EDGE. LEAK CHECKED OK.SDR 95ZZZX2510O-Ring · leakingISN - CREW REPORTED FUMES IN THE COCKPIT. MAINTENANCE FOUND AN O-RING UNDER THE RUDDER BOOST TRANSMITTER LEAKING OIL. THE O-RING WAS REPLACED AND LEAK CHECKED GOOD.
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