N341UA
Service difficulty reports not matched to an aircraft · 55
They name N341UA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N341UA' AND registry_match IS NULL 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 = 'N341UA' AND registry_match IS NULL 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 2008UALA02589Control Panel · no testAFT PIT A DET LIGHT DOES NOT ILLUMINATE WITH CARGO SYS FIRE TEST OR LIGHTS TEST. REPLACED FIRE TEST CONTROL PANEL, CHECKS NORMAL. AC OK FOR SERVICE.SDR 2008UALA02588Control Panel · no testFWD PIT A DETECTOR LIGHT DOES NOT ILLUMINATE WITH CARGO FIRE SYS TEST OR WITH LIGHTS TEST. REPLACED TEST PANEL SYSTEMS CHECK GOOD.AC OK FOR SERVICE.SDR 2008UALA02418Warning Light · illuminatedABORTED TAKEOFF AT 100 KTS DUE TO A FUEL FILTER BYPASS LIGHT ON NR 2 ENGINE.SDR 2008UALA00997Bracket · looseDOOR 1R BRACKET THAT HOLDS GIRT BAR ON DOOR LOOSE. GIRT BAR COMES OUT TOO EASILY. ADJUSTED BRACKET.SDR 2008UALA00030Dump Valve · obstructedFLIGHT DIVERTED DUE TO FORWARD LAVATORY OVERFLOW. FOUND FOREIGN OBJECT IN DUMP VALVE ALLOWING FLUID TO BYPASS VALVE. REMOVED OBJECT.SDR 2008UALA0030Lavatory · unknownFLIGHT DIVERTED DUE TO FORWARD LAVATORY OVERFLOW.SDR 2007UALA04404Fire Bottle · low pressureFWD ENGINE FIRE BOTTLE PRESSURE AT LIMIT. REPLACED BOTTLE OF FWD ENG SYS.
SDR 2007UALA04380Skin · crackedNR 6 SLAT (RT WING) CRACKED, LOCATED ON BOTTOM SURFACE. REMOVED DAMAGED AREA AND PERFORMED A REPAIR TO THE NR 6 SLAT (BOTTOM SURFACE).
SDR 2007UALA04352Clamp · brokenAIRCRAFT UNABLE TO MAINTAIN PRESSURE WITH SINGLE PACK OPERATION. FOUND APU BELLOWS CLAMP WAS FOUND LOOSE/BROKEN AND LEAKING PRESSURE. REPLACED CLAMP. PERFORMED SINGLE PACK PRESSURIZATION OF A/C. ALL CHECKS GOOD.SDR UALA2008111304215Skin · damagedFUEL LEAKING AT AFT SPAR JUST OUTBOARD OF LT MAIN GEAR, FROM UPPER REAR SPAR CORD REINFORCEMENT DOUBLER LOCK FASTENER. BEAM LT SUPPORT FTG HAS 6 ELONGATED HOLES IN UPPER SKIN. BEAM LT SUPPORT FTG HAS 6 ELONGATED HOLES IN UPPER SKIN. EG APPROVAL TO USE LG DSDR 2007UALA04215Support Fitting · damagedFUEL LEAKING AT AFT SPAR JUST OUTBOARD OF LEFT MAIN GEAR, FROM UPPER REAR SPAR CHORD REINFORCEMENT DOUBLER LOCK FASTENER. BEAM LEFT SUPPORT FITTING HAS 6 ELONGATED HOLES IN UPPER SKIN.SDR 2007UALA03014Light · contaminatedFLOOR PROXIMITY LIGHTING INOP FROM ROW 16 AFT TO AFT GALLEY. CLEANED & DRIED PROXIMITY LIGHTS. TESTED GOOD.SDR 2007UALA02220Detector · faultyCARGO FIRE DETECTION FAIL LIGHTS ALL 4 ARE ILLUMINATED. REPLACED 3 DETECTORS IN AFT PIT A SYSTEM AND 3 IN FWD PIT 2 EACH FOR B SYSTEM AND 1 FOR A SYSTEM.SDR 2007UALA02199Light · out of positionCREW REPORTS EEL LIGHTS COMING OFF THE LAST THREE FEET. LIGHTS INOP FROM ROW 16 BACK. REPLACE EEL AFT STRIP OPS CKS OK.SDR 2007UALA00790Bearing · failedRECIRC FAN ABOVE 7 IS GRINDING & HAS A BURNING ODOR. [SUP 05-29-07] RECIRCULATION FAN INOP. REPLACED RECIRCULATION FAN AND FILTER. UNIT HAD BAD BEARINGS. REPLACED BEARING AND BALANCED ROTOR AND IMPELLER.SDR 2007UALA00544Filter · dirtyCREW REPORTS MAIN CABIN FLIGHT ATTENDANTS AND PASSENGERS HAVING DIFFICULTY BREATHING AND SNEEZING. SUPPLEMENTAL DATA UPDATE CAUSE: HEPA FILTER. REPLACED RIGHT PACK RECIRCULATION FAN HEPA FILTER.SDR 2006UALA01302Wire · inoperativeFOUND AFT CABIN EEL LIGHTS INOP FROM ROW 15 AFT TO AND INCLUDING EEL STRIP IN FRONT OF AFT GALLEY CART STOWAGE COMPARTMENT. REPLACED EEL TRACK CABLE.SDR 2006UALA01301Wire · inoperativeFOUND EEL LIGHTS INOP AT ROWS 1-2 AND EEL STRIP IN FRONT OF FWD GALLEY CART STOWAGE COMPARTMENT. REPLACED EEL TRACK CABLE.SDR 2006UALA01259Fan · odorBURNING ELECTRICAL ODOR OR ACRID SMOKE ODOR DETECTED IN CABIN DURING APPROACH. EMERGENCY DECLARED. REPLACED THE INSTRUMENT COOLING SUPPLY FAN. REPLACED BEARINGS AND ALL WORN AND PRECAUTIONARY ITEMS.SDR 2006UALA00747Door Frame · corrodedAFT CARGO DOOR CUTOUT FWD FRAME HAS CORROSION AT STA 794 BETWEEN STR 24R & 27R. INSTALLED EXTERNAL ANGLE DOUBLER REPAIR PER SRM 51-70-11 FIG 1.SDR 2006UALA00716Stringer · corrodedAFT CARGO COMPARTMENT STATION 847 STRINGER 22R HAS CORROSION ON STRINGER. CUT OUT DAMAGED STR AND REPLACED WITH NEW SECTION PER SRM 53-00-03.SDR 2006UALA00660Stringer Clip · crackedDURING BELLY SKIN REPLACEMENT 4 EA STRINGER CLIPS WERE FOUND CRACKED AT STA 787 STR 21R, STA 787 STR 22R, STA 867 STR 20R & STA 887 STR 20R. REPLACED STRINGER CLIPS REF SRM 51-40-02.SDR 2006UALA00657Frame · crackedROUND OVERWING FRAME STA 616 RT SIDE IS CRACKED. INSTALLED STIFFENING ANGLE PER MM53-11-89.SDR 2006UALA00645Frame · crackedLT WW BS 695 FRAME AT STR 18A IS CRACKED IN THE RADIUS. REPLACED ANGLE PER SRM51-4 0-02.SDR 2006UALA00630Web · crackedSTRINGER 7L ATTACH WEB AT STA 294.5 IS CRACKED AT INBD CORNER. REPLACED WEB PER SRM51-40- 02.SDR 2006UALA00272Light · inoperativeLEFT OVERWING EMERGENCY SLIDE LIGHT INOP.SDR 2005UALA00257Overheat Loop · malfunctionedRETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. CREW REPORTED NR 2 ENGINE OVERHEAT INDICATION AT CLIMB. CREW SHUT DOWN NR 2 ENGINE PER QRC. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM. FOUND NR 2 ENGINE CORE DETECTOR M1122, LOOPSSDR 2005UALA00078Skin · dentedSTA 341-359 HAS 3 DENTS ABOVE STR 21R. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR.SDR 2005UALA00077Skin · dentedLT FUSE SKIN IS DENTED AT STA 897 BETWEEN STR 24L AND 25L. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. CUT-OUT DAMAGE AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER.SDR 2003UALA00745Switch · failedUNABLE TO SELECT NOSE DOWN ELEVATOR TRIM FROM BOTH YOKES. MAINTENANCE TECHNICIANS DUPLICATED THE PROBLEM ON GROUND. THE PROBLEM WAS TRACED TO A FAULTY FLAPS UP SWITCH (S245). THE SWITCH WAS REPLACED. OPERATIONAL CHECKS WERE PERFORMED SATISFACTORILY.SDR 2003UALA00746Autopilot Sys · malfunctionedWITH EITHER AUTO PILOTS ENGAGED AND ATTEMPTING TO ACCELERATE THE AIRCRAFT PITCHES UP. UPDATE DURING BITE CHECK OF THE AUTOPILOT BITE, FOUND FCC-B FAULTED, DADC2 FAULTED. DURING FULL TEST OF AUTOPILOT, OBSERVED FAULT WITH AFAU. REPLACED FCC-B, DADC, AND AFAUSDR 2002UALA01376Light · inoperativeEMERGENCY FLOOR LIGHTING SYSTEM INOPERATIVE. DEFECTIVE EEL LIGHT ASSEMBLY. REPLACED EEL STRIP. OPERATIONAL CHECK GOOD.SDR 2002UALA00773Circuit Breaker · failedDIVERTED TO DEN DUE TO LOSS OF GENERATOR. THE AIRCRAFT WAS DIVERTED TO DENVER WITHOUT INCIDENT. AMT CREW ISOLATED CAUSE OF FAILURE DUE TO NR 2 TRANSFER BUS NORMAL CIRCUIT BREAKER (C821) AS BAD. THE CIRCUIT BREAKER WAS REPLACED, AND THE AIRCRAFT WAS RETURNEDSDR 2002UALA00584Keelbeam · wornRIGHT HAND KEEL BEAM LOWER FLANGE UPPER SURFACE WEAR AREA AROUND FASTENER HOLE BODY STATION 700-727. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2002UALA00535Frame · crackedSTATION 178 LEFT HAND VERTICAL SIDE CHORD CRACKED AT STRINGER 17. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE.SDR 2002UALA00533Frame · corrodedAFT PIT FRAME UPPER SURFACE BODY STATION 727E STRINGER 25R TO STRINGER 26R HAS EXCESS MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR.SDR 2002UALA00532Frame · misdrilledAFT STABILIZER COMPARTMENT STATION 1108 STRINGER 1R FORWARD FACE OF FRAME HAS MISDRILLED HOLE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2002UALA00524Stringer · crackedFUSELAGE STRINGER 16 LH IS CRACKED AT BODY STATION 500C + 18 INCHES. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHEDINSTALLED NEW STRINGER AND SPLICE.SDR 2002UALA00520Pressure Panel · crackedMAIN LANDING GEAR WHEEL WELL HORIZONTAL BULKHEAD WEB IS CRACKED BS 665, LBL 32 WL 202. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.SDR 2002UALA00513Frame · crackedCABIN, BODY STATION 887 FRAME, BETWEEN S8R & S9R, FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE-CHANNEL DOUBLER.SDR 2002UALA00507Stringer · crackedCABIN STATION 360 STRINGER 14L TAIL CRACKED AT FASTENER JUST FORWARD OF FRAME. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW U-CHANNEL.SDR 2002UALA00506Stringer · crackedFORWARD CABIN STATION 294.5 STRINGER 17R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR.SDR 2002UALA00472Bulkhead · crackedSTATION 178 BULKHEAD WEB AFT SIDE CRACKED AT BL 0 WL 188. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2002UALA00471Bulkhead · crackedSTATION 178 BULKHEAD AFT SIDE WEB CRACKED RBL 5 WL 200. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2002UALA00470Frame · crackedCABIN, BODY STATION 867 FRAME, BETWEEN STRINGER 8R AND 9R FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE (CHANNEL) NESTED ON INBOARD FRAME FLANGE.SDR 2002UALA00466Frame · crackedBODY STATION 887 FUSELAGE FRAME IS CRACKED BETWEEN STRINGER 8L AND STRINGER 9L AT UPPER FASTENER FOR VENT BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2002UALA00439Frame · crackedCABIN BODY STATION 867 FRAME, BETWEEN 8L & 9L FRAME IS CRACKED AT FASTENER HOLE FROM VENT BRACKET, AFT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED CHANNEL REPAIR ANGLE.SDR 2002UALA00399Frame · crackedCABIN BODY STATION 827 FRAME BETWEEN STRINGER 8R AND STRINGER 9R, FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET (AFT SIDE). MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR CHANNEL (ANGLE) DOUBLER.SDR 2002UALA00398Frame · crackedCABIN BODY STATION 847 BETWEEN STRINGER 8R AND 9R FRAME IS CRACKED AT FASTENER HOLE FOR VENT BRACKET. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR CHANNEL (ANGLES) DOUBLER.SDR 2002UALA00397Floorbeam · damagedAFT CABIN STATION 947 LBL 5 AND LBL 15 HAS EXCESSIVE MATERIAL LOSS. MAJOR REPAIR ACCOMPLISHED. REPAIRED FLOORBEAM UPPER CAP WITH SINGLE FLANGE BLEND OUT REPAIR. INSTALLED SINGLE REPAIR ANGLE.
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