N495UA
Service difficulty reports · 112
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 = 'N495UA' 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 = 'N495UA' 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 CALA2026082418862Fmc · faultedFMGC 2 KEEPS FAILING FO MAP LOST LOCKING FOR POSITIVE FIX UNLOCKED PERFORMED AFS TEST IAW AMM 22-96-00. TEST OK NO FAULTS NOTED. LAND CAT 3 TEST WAS PERFORMED, IAW AMM 22-97-00, LAND TEST OK, NO FAULTS FOUND. SUSPECT FMGC 2 INSTALLED BAD FROM STOCK CHKD SCESDR CALA2026081318583Pin · corrodedFOUND CORRODED ROLLER PIN ON RIGHT FWD EXIT HATCH LOWER AFT ATTACH POINT LOCKING THIS LOG FOR MAINTENANCE FERRY FLIGHT UNLOCKED FOR SIGNOFF LOCKED FOR FERRY UNLOCKED FOR MAINTENANCE ACTION UPDATE REMOVED FWD RH EMERGENCY EXIT HATCH UPTO AND INCLUDING STEP 4. NSDR CALA2026022614113Valve · faultedMLG NOT UPLOCKED ECAM PROC DID NOT RESOLVE ISSUE. GEAR REPORTED TO HAVE RETRACTED, BUT DID NOT STAY UPLOCKED TO ALLOW GEAR DOORS TO CLOSE. PERFORMED FIM 32-31-00-810-836-A. MLG DOORS OPENED CORRECTLY BUT GEAR DID NOT PERFORM CORRECTLY. PERFORMED CHECK OF THESDR CALA2025110310844Power Supply · no testOPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK IAW EA2500-03960 AND EA2500-08031. R & R EPSU BATTERY AT AFT L LOCATION. REF: AMM 33-51-38/401 CONFIG 00. OP CHECK GOOD.SDR CALA2025110310843Power Supply · no testOPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS BY BITE-CHECK IAW EA2500-03960 AND EA2500-08031. R & R RT EMERGENCY EXIT EPSU, IAW AMM 33-51-38/401 CONFIG 00. OP CHECK IS GOOD.SDR CALA2025080107204Fuel Cap · missingDURING WALK AROUND FOUND FUEL CAP MISSING. INSTALLED NEW FUEL CAP IAW AMM TASK 28-25-41-400-005-A.SDR CALA2025052905065Unknown · odorCOCKPIT SMELLED LIKE FUMES AND STAYED LIKE THAT FOR A WHILE AFTE R TAKEOFF AND THEN WENTOFF CREW DEBRIEFING: CAPTAIN SAID WHEN THEY START #2 ENGINES , FUEL PRESSURE WAS FLUCTUATING, WHEN ENGINE STARTED THEY SMELL FUMES, AND LINGERS TILL THEY TOOK OFF, ONCE AISDR CALA2025050704534Fmc · faultedAP1 WAS NOT RELIABLE IN REGARDS TO SPEED OR ALTITUDE. ATTEMPTED TWICE. PERFORMED POST FLIGHT REPORT, NO FAULTS LOGGED. PERFORMED AFS TEST, FMGC 1 FAILED TEST. RESET FMGC1 SYS & PERFORMED AFS TEST A SECOND TIME, ALL TEST PASSED. PERFORMED LAND TEST, TEST FAILEDSDR CALA2025012201962Door · out of adjustINFORMATION ONLY REPORT . CLIMBING THRU 16K WE GOT LEFT AND RIGHT OVERWING EXIT INDICATING OPEN. F/ AS SECURED BOTH COVERS TWO WRITE UPS ON ONE LOG PAGE. CREATED ONE LOG PAGE FOR EACH. REF L/P 3571987 LEFT FWD OVERWING EMERGENCY EXIT DOOR INDICATES OPEN . INTSDR CALA2025012301984Battery · faultedOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS FOUND ESPU BATTERY FORWARD LEFT (ABOVE DOOR 1L) BAD. REMOVED AND REPLACED L1 ESPU BATTERY REF AMM 33-51-38. SYSTEM TEST PASSEDSDR CALA2025012201966Handle · detachedCOVER ON LH FWD OVERWING EXIT HANDLE FELL OFF ADJUSTED AND TIGHTENED GAP ON FASTENER ARMS ON LEFT FWD OVERWING EMERGENCY EXIT HATCH COVER FLAP. REF AMM 52-21-11-400-001-A. OPS CHECK GOODSDR CALA2025012101951Power Supply · faultedEPSU INT LOAD EMER L/R FAULT PERFORMED EPSU RESET. FAULT STILL STANDS. FOUND RIGHT HAMD EMERGENCY EXIT LIGHT INOP FOUND LIGHT ELECTRICAL CONNECTOR DISCONNECTED. RECONNECTED IAW AMM 33-51-00. RESET SYSTEM AGAIN. OPS CHECK GOOD. FAULT STILL STANDS. VOLT CHECKED SDR CALA2025011601916Lens · missingL SIDE OVERWING EXIT SLI DE ARMED LENS COVER MISSING. REPLACED LEFT SIDE OVERWING SLIDE ARM INDICATOR LENS COVER PER AMM-52-73-21-000-003-A.SDR CALA2024122601653Cover · detachedECAM MSG DOOR FWD EMER EXIT AFTER LANDING CREW REPORT EMERGENCY EXIT COVER FLAP FOR FWD RIGHT OVERWING EXIT FELL OFF, RE ATTATCHED COVER FLAP, OPS CHECK GOOD, DOOR INDICATIONS NORMAL REF AMM 52-21-11 ADD EMP: U115923SDR CALA2024122001600Sensor · faultedDOOR R AFT EMER EXIT CABIN PRESSURE NORMAL ECAM OCCURED CLIMB OU T 7000FT CREW REPORTS R FWD OPEN ECAM INTERMITTENT ALSO THEN THEY GO OUT WHEN AIRCRAFT IS FULLY PRESSURIZED APPLIED MEL 5270AZ. MEL 5270AZ ACCOMPLISHED REPAIR TROUBLESHOT SENSOR MONITORING FAULT SDR CALA2024122001597Cover · detachedDOOR L EMER EXIT ECAM UPON ENTERING AIRCRAFT NOTICED EMER EXIT HANDLE COVER WAS OFF AND SITTING ON GROUND INCORRECTLY LABELED AS TRIM (LOGPAGE# 3241711). REINSTALLED FWD DOOR L EMER EXIT HANDLE COVER AND OPS CHECKED EMER DOOR PROX SWITCH REF AMM 52-22-00. FAULSDR CALA2024122001592Warning Light · intermittentDOOR R AFT EMER EXIT CREW STATED MOMENTARY RH FWD AND AFT EMERGENCY EXIT LITE ON WITH NO NOISE, VIBRATION OR PREASSURIZATION PROBLEM. INSPECTED DOOR AND FOUND PROPERLY CLOSED PER AMM 52-22-00-410 AND INDICATIONS ARE NORMAL. NO HISTORY OK TO CONTINUESDR CALA2024060701737Frame · crackedFR16RH DOUBLE JOGGLE HOLE #5 HAS A CRACK INDICATION IN THE OUTER FRAME LAYER ONLY 5311-0320 DEVIATION TO EA 5311-02442 OPS 002 TO USE AIRBUS DWG LAYER POST REAMING PER NTM 51-10-01 & 51-10-18 WITH NO DEFECT SIZE 7.142 (.2811), INSP THRESHOLD FROM TIME OF EMBODSDR CALA2023052601647Battery · no testPER PRODUCTION REQUEST, ESPU BATTERY "L" FAILED OPS TEST. REMOVED AND REPLACED IIWL EPSU BATTERY PER A320 AMM 33-51-39-000 -007-C2 / 33-51-39-400-007-C2. PERFORMED OP CHECKS PER A320 AMM 33-51-00-710-001-A / 3351-00-710-002-62. SYSTEM CHECKS GOOD.SDR CALA2023020100308None · noneFWD EMERGENCY BATTERY FAILED CAPACITY TEST. R+R FWD EMERGENCY LIGHT BATTERY REF 33-51-38. OPS CHECK GOOD.SDR CALA2023020100307Light · failedRH OVERWING EMERGENCY BATTERY FAILED CAPACITY TEST. R+R RH OVERWING EMERGENCY LIGHT REF 33-51-38. OPS CHECK GOOD. SUPPOSED TO READ EMERGENCY LIGHT BATTERY.SDR CALA2022121903440Pump · low pressureCTR TK PUMP 1 LO PR DISPLAYED ON UPPER ECAM SCREEN. - FUEL SHORTLY AFTER DEPARTURE CENTER TANK FUEL PUMP 1 WAS REPLACED.SDR CALA2021101801918Stringer · corrodedCORROSION ON AFT CARGO COMPT BILGE AREA, FR56, STRINGER 41L SPLICE AT FR52. RECEIVED NEW STRINGER D5347042020800, BATCH INITIAL INSPECTION TO OCCUR 60,000 FC OR 120,000 FH FROM REPAIR # 0003843117, AND REPAIR COUPLING R5307111220800, BATCH EMBODIMENT AND SUBSESDR CALA2021101801910None · corrodedCORROSION ON AFT CARGO COMPT BILGE AREA, FR56, STRINGER 41L. CORRECTED ON DUPLICATE ELB LOGPAGE 7247641SDR CALA2021101801905None · corrodedCORROSION ON BULK CARGO COMPT. BILGE AREA, STGR41R, FWD AND AFT OF FR59. REMOVED CORROSION FROM S41R FR59 AT BULK CARGO IAW SRM 51-74-00 L=12" D=0.03" FOUND TO BE OUT OF LIMITS IAW SRM 53-41-13-283-602 FIG 001 SHEET 01. REMOVED AND REPLACED S41R FROM FR58 TO FSDR CALA2021101801898None · corrodedCORROSION ON STRINGER AT AFT FUSELAGE OUTFLOW VALVE CUT-OUT AREA , FR65 STRINGER 31R. REMOVED AND INSTALLED OUTFLOW VALVE IAW AMM 21-31-51 OPS TEST GO OD IAW AMM 21-31-00-710. BLENDED AREA ON S31R FR65 IAW SRM 51-74 -00 L=4.110" W=0.940" ORIGINAL THICKNESS 0.1SDR CALA2021101801887None · corrodedCORROSION ON BULK CARGO COMPT STGR 42R BETWEEN FR63 AND FR64 (A3 NB-53-3-6185) REMOVED CORROSION IAW SRM 51-74-00, CHECKED LIMITS L=18" D=.050" , OUT OF LIMITS IAW A320 SRM 53-41-13-283-002, REMOVED AND REPLA CED STRINGER 42R, BETWEEN FR60 TO FR64 P/N D5347041SDR CALA2021101401881None · noneDURING ROTO PROBE INSPECTION OF THE LH DOOR STOP FITTING #7 AT F R16, CRACK INDICATION WAS NOTED IN LOWER I/B HOLE FWD LAST TWO L AYERS, REPAIR BEFORE NEXT FLIGHT. (AD2019-20-10) REPLACED L/H DOOR STOP #7 FITTING INTERCOSTAL BY C/W EC/RA 5311- 02649, REPLACEMESDR CALA2021101401880Stringer · noneCORROSION ON BULK CARGO COMPT STGR41 LH BETWEEN FR63 AND FR64. REPLACED STRINGER 41L BETWEEN FR60 TO FR64. P/N: D5347041821600 BTCH: 0003849002 IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-11. SFR# 1026673. MAINTENANCE ACCOMPLISHED BY V934700 ON WC 0014944 AT SSDR CALA2021101401879Stringer · noneCORROSION ON BULK CARGO COMPT STGR 42L/H BETWEEN FR63 AND FR64 REPLACED STRINGER 42L, BETWEEN FR60 TO FR64, P/N: D5347041821800 BATCH: 0003848975 IAW A320 SRM 51-72-11-911-001 AND SRM 51-42-1 1. SFR# 1026673 MAINTENANCE ACCOMPLISHED BY V934585 ON WC 001494 3 ASDR CALA2021101101845None · corrodedCORROSION ON BULK CARGO COMPT STGR41 LH BETWEEN FR63 AND FR64.SDR CALA2021101101844None · corrodedCORROSION ON BULK CARGO COMPT STGR 42L/H BETWEEN FR63 AND FR64SDR CALA2021101101846Intercostal · noneDURING ROTO PROBE INSPECTION OF THE LH DOOR STOP FITTING #7 AT F R16, CRACK INDICATION WAS NOTED IN LOWER I/B HOLE FWD LAST TWO L AYERS, REPAIR BEFORE NEXT FLIGHT. (AD2019-20-10)SDR CALA2021100401766Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y512.5 AT FR68. (A3NB-53-3-622 2) CORROSION ON FLOOR BEAM Y512.5 FR68 BLENDED OUT IAW SRM 51-74-00 SFR# 1026596. MAINTENANCE ACCOMPLISHED BY V933868 ON WC 0014619 , BLENDED AREA MEASURES LENGTH 1.5" WIDTH 0.15" ORIGINAL THICKNSDR CALA2021100401765Beam · corrodedCORROSIN ON AFT CABIN FLOOR BEAM Y-1292 AT FR66. (A3NB-53-3-6222 ) BLENDED OUT CORROSION ON AFT CABIN BEAM Y-1292 AT FR66 IAW SRM 5 ING BFM 1-74-00 FIG 1. FLOOR BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-0 0-15-283-002 L=4.0" W=2.0" D=.046". REMOVED AND REPLACESDR CALA2021100401764Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y-765 BETWEEN FR67 AND FR68 (A 3NB-53-3-6222) BLEND OUT CORROSION ON AFT CABIN FLOOR BEAM Y-765 BETWEEN FR67 A E ACCOMPLISHED BY V933486 ON WC 0014617 AT ST ENGINEERING BFM ND FR68IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SSDR CALA2021100401763Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y-1162.5 AT FR68. (A3NB-53-3-6 222) BLENDED OUT CORROSION ON AFT CABIN FLOOR BEAM Y-1162.5 IAW SRM 5 ENGINEERING BFM 1-74-00 FIG 1. FLOOR BEAM FOUND TO BE OUT LIMITS IAW SRM 53-00-1 5-283-002 L=0.80" W=0.5" D=0.150". REMOVED ASDR CALA2021092901726Flap Track · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y 160.5 BETWEEN FR68 AND FR70. (SDR REQUIRED) A3NB-53-3-6222 EVALUATED FLOOR BEAM IAW A320 SRM 53-00-15-283-002 AND FOUND OUT OF LIMITS, RECEIVED NEW FLOOR BEAM. REPLACED IAW A320 SRM 51-42 -11. SFR# 1026536. MAINTENANCE ACCOMSDR CALA2021092901725Fitting · corrodedCORROSION ON R2 DOOR CUTOUT LOWER AFT CORNER FITTING AT FR68. (S DR REQUIRED) A3NB-53-3-6299 NO ESTABLISHED LIMITS FOUND IN SRM. REPLACED FR68R DOOR CUTOUT C ORNER FITTING WITH NEW PART IAW SRM 53-41-69-02-A, ITEM 200-A. L OCATED AND DRILLED IAW SRM 51-44-11. SDR CALA2021092701693Beam · corrodedCORROSION ON CABIN FLOOR BEAM Y-765 AT FR20 (A3NB-53-3-6038) EVALUATED FLOOR BEAM AND FOUND OUT OF LIMITS IAW A320 SRM 53-11- 14-283-007, REMOVED AND REPLACED BEAM P/N D5311278220207, BATCH 00037288690 Y-765 IAW A320 SRM 51-42-11. MAINTENANCE ACCOMPLISHE D BY SDR CALA2021092701692Beam · corrodedCORROSION ON CABIN FLOOR BEAM Y-1292 AT FR20. (A3NB-53-3-6038) CORROSION ON CABIN FLOOR BEAM Y-1292 FOUND OUT OF LIMITS IAW SRM 53-11-14-283-007. REMOVED AND REPLACED FLOOR BEAM Y-1292 FROM F R12 TO FR20 IAW SRM 51-42-11. MAINTENANCE ACCOMPLISHED BY V93386 6 OSDR CALA2021092701691Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y1162.5 AT FR68. (A3NB-53-3-62 22) FLOOR BEAM EVALUATED AND FOUND OUT OF LIMITS IAW A320 SRM 53-41- 15-283-002 AND REPLACED FOR NEW FLOOR BEAM PN: D5347218820400 BA TCH: 0002716527 IAW SRM 51-52-11/001. MAINTENANCE ACCOMPLISHESDR CALA2021092701679Door Frame · crackedDURING ROTO PROBE OF RH FR16 #7 DOOR STOP FITTING FASTENER HOLES A CRACK WAS NOTED IN THE BOTTOM I/B HOLE. THE CRACK IS IN THE I NTERCOSTAL AT 9 O''CLOCK. REMOVED INTERCOSTAL FITTING P/N: D531-12307-201-00 AND REPLACED INTERCOSTAL FITTING P/N: D53114236-201-91SDR CALA2021092401665Beam · corrodedCORROSION ON CABIN FLOOR BEAM Y-765 AT FR20 (A3NB-53-3-6038)SDR CALA2021092401664Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM Y1162.5 AT FR68. (A3NB-53-3-62 22)SDR CALA2021092401666Seat Track · corrodedCORROSION ON CABIN FLOOR BEAM Y-1292 AT FR20. (A3NB-53-3-6038)SDR CALA2021092401660Beam · corrodedCORROSION ON AFT CABIN FLOOR BEAM UPPER INBD SPLICE ANGLE (LOWER SURFACE) AT Y-1162.5 FR68 (A3NB-53-3-6222) (SDR) AFT CABIN FLOOR BEAM UPPER INBD SPLICE ANGLE WAS AVALUATED IAW S RM 53-00-15 AND FOUND OUT OF LIMITS, L=0.620" W=0.400" D=0.110", RECEIVED, LOCATESDR CALA2021092401658Beam · corrodedCORROSION ON CABIN FLOOR DUMMY RAIL AT APPRX Y-150 BETWEEN FR20 AND FR23. (A3NB-53-3-6038) REPLACED RAIL BETWEEN FR20 TO FR23 Y-150 IAW A320 SRM 51-72-11- 911-001 AND SRM 51-42-11. P/N: D5311141420200 BTCH: 0003838983. SFR# 1026487. MAINTENANCE ACCOMPLISHED BSDR CALA2021092001606Shear Plate · corrodedAFT CABIN R/H SIDE FLOOR STRUCTURE LATERAL SHEAR PLATE CRACKED A PPRX 5" AFT FR69. INSTALLED NEW SHEAR PLATE AFT FR69 AND ANGLE IAW SRM 51-75-11 AN D SRM 51-42-11. SFR# 1026424. MAINTENANCE ACCOMPLISHED BY V93387 0 ON WC 0014622 AT ST ENGINEERING BFMSDR CALA2021091701599Floor Support · corrodedCORROSION ON CABIN FLOOR SUPPORT AT APPRX Y-1673 AT FR20 REMOVED CORROSION ON CABIN FLOOR SUPPORT AT Y-1673 FR20 IAW SRM 51-74-00 FOUND OUT LIMITS IAW SRM 53-11-14-07 ORIGINAL THICKNESS 0.080" REMAINING THICKNESS 0.030" D=0.050". REMOVED AND REPLACE D FLOOR S
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