N474UA
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 = 'N474UA' 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 = 'N474UA' 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 CALA2025110510916Fairing · damagedHUMMING NOISE COMING FROM ENG 2 SIDE EXIT ROW AT CRUISE. ENG AND PRESS INDICATIONS NORMAL, OK TO PLACE ON CARRY PER MT -53-004 ACCOMPLISHED INTERIM REPAIR AND APPLIED SPEED TAPE TO WING TO BODY PANEL RIGHT SIDE 192DT.SDR CALA2025102010284None · noneFA EMERGENCY MANUAL NEEDS REPLACEMENT NOTIFIED SCRUBS, NO MAINTENANCE REQUIRED.SDR CALA2025102010253Fuel Cap · missingFUEL CAP LANYARD MISSING. REQUEST MEL 2522HK FOR MISSING FUEL CAP LANYARD CAP IS NOT DAMGD ANDIS SECURE 2522HK APPROVED PLACED ON MEL.SDR CALA2025102110351Packing · damagedHYD B RSVR LO LVL AT FL200 FOUND LEAK AT BLUE PRESSURE SWITCH 2074GJ, SUSPECT SEAL LEAKING. BLUE SYSTEM PRESSURE SWITCH WAS FOUND LOOSE AND HAD A CUT O-RING. INSTALLED A FRESH SEAL, REINSTALLED THE SWITCH, AND A PRESSURE CHECK CONFIRMS THERE IS NO MORE LEAK. SDR CALA2025093009425Cover · misinstalledDOOR L FWD EMER EXIT ON ECAM SCREEN AT 16000 FT VERIFIED LH FWD EMERGENCY EXIT HATCH HANDLE FLAP COVER IS IN ITS CORRECT INSTALLATION POSITION, LOWER ECAM EMERGENCY EXIT SYMBOL LIGHT EXTINGUISHED AND NO ACTIVE FAULTS PRESSENT. REF TSM 52-21-00-810-801-A.SDR CALA2025093009439Intercostal · crackedLEFT FRAME 16 DOUBLE JOGGLE AREA HOLE 18 HAS CRACK INDICATION IN FRAME LAYER AT 5 O`CLOCK, DIRECTION 50%. REMOVED FASTENERS COMMON TO #18 (LEADER), #19 (ASSOCIATED). REF SRM 51-42-11/001. HOLE #18, #19 DIA. = NOMINAL. REAMED HOLE 18 TO MAX DIA. OF .34220? INSDR CALA2025092909374Pin · corrodedNUMBER 2 ENG AFT MOUNT INNER AND OUTER PINS ARE PITTED. REMOVED AND REPLACED NR 2 ENGINE AFT MOUNT INNER AND OUTER PINS IAW AMM 71-22-11-000-803-A/400-803-A.SDR CALA2025092909373Pin · corrodedNUMBER 1 ENG AFT MOUNT INNER AND OUTER PINS ARE PITTED. REMOVED AND REPLACED #1 ENGINE AFT MOUNT INNER AND OUTER PINS IA W A320 AMM 71-22-11-000-803-A/400-803-A.SDR CALA2025092509259Rib · corrodedUPON REMOVAL OF UPPER SPAR AFT WEB FIVE HAS CORROSION. LOCATED AND DRILLED NEW #1 AFT FAIRING FOR #1 AFT MOVABLE FAIRING IAW SRM 51-44-11 TO INSTALLED ON NR 375421/24337/9292337.SDR CALA2025092209112Spar · corrodedLH WING AFT MOVEABLE FAIRING IS CORRODED. REMOVED AND REPLACED NO. 1 MOVABLE FAIRING UPPER SPAR IAW A320 SRM 54-42-11-P. 5-25SDR CALA2025091608960Spar · corrodedRH WING AFT MOVABLE FAIRING IS CORODDED. REMOVED AND REPLACED UPPER SPAR IAW A320 SRM 51-42-11 P5-25 SRM 51-44-11 P.3 SRM 54-55-12-283-007 FIG 4 SRM 51-57-12-911-001.SDR CALA2025091508904Door Frame · crackedLEFT FWD EMERGENCY EXIT DOOR AFT VERT BEAM CRACKED. REMOVED AND REPLACED LT FWD EMER EXTI DOOR AFT FRAME SEGMENT IAW SRM 51-42-11/001 AND DRAWING D52279010010, D52279040004.SDR CALA2025091508903Door Frame · crackedAFT EMERGECY EXIT DOOR AFT VERT BEAM CRACKED. REMOVED AND REPLACED THE LT AFT EMER EXIT DOOR AFT FRAME SEGMENT IAW SRM 51-42-11/001 AND DRAWINGS D52279010010, D52279040004.SDR CALA2025091508902Door Frame · crackedRIGHT FWD EMERGENCY EXIT DOOR AFT VERT BEAM CRACKED. REMOVED AND REPLACED RT FWD EMER EXIT DOOR AFT FRAME SEGMENT IAW SRM 51-42-11/001 AND DRAWING D5227900010, D5227040004.SDR CALA2025091508901Door Frame · crackedRIGHT AFT EMERGENCY EXIT DOOR FWD VERT BEAM CRACKED. REMOVED AND REPLACED RT AFT AMER EXIT DOOR FWD FRAME SEGMENT IAW SRM 51-42-11/001 AND DRAWINGS D52279010010, D52279040004.SDR CALA2025091508900Door Frame · crackedRIGHT AFT EMERGENCY EXIT DOOR & AFT VERT BEAMS CRACKED A3NB-MP-2100-52 2102-01-1-AFT-R. REMOVED AND REPLACED RT AFT EMER EXIT AFT FRAME SEGMENT IAW SRM 51-42-11/001 AND DRAWING D52279010010, D52279040004.SDR CALA2025091208831Door Frame · crackedLT FWD EMER EXIT DOOR FWD AND VERT BEAMS CRACKED. REMOVED AND REPLACED LH FWD EMER EXIT DOOR FWD FRAME SEGMENT IAW A320 DRM 51-42-11/001 AND DRAWING D52279010010, D52279040004. P ERFORMED BY V061630 AND INSP BY N078625SDR CALA2025091208827Door Frame · crackedLT AFT EMER EXIT DOOR FWD AND VERT BEAMS CRACKED. REMOVED AND REPLACED LH AFT EMER EXIT DOOR FWD VERT BEAM IAW A32 0SRM 51-42-11/001 AND DRAWINGS D52279010010 AND D52279040004.SDR CALA2025091208825Door Frame · crackedRT FWD EMER EXIT DOOR FWD VERT BEAMS CRACKED. REMOVED AND REPLAED RT FWD EMER EXIT DOOR'S FWD VERT DRAIN IAW A 320 SRM 51-42-11/001 AND DRAWINGS D52279010010 AND D52279040004 ESFR #1827.SDR CALA2025091108779Floorbeam · corrodedAFT CABIN FLOORBEAM, -Y1292 GOUGED AT FR68. REMOVED AND REPLACED BEAM -Y1292, FR 68 IAW SRM 51-72-11-911-001, SRM 51-42-11/001, CMM 51-21-11/001, SRM 53-41-14- 283-009, SRM 53-41-14-01A, & SRM 51-11-12/001.SDR CALA2025073107141Seal · missingUPON REMOVAL OF PANEL 191DT FOUND BOTTOM SEAL MISSING, WILL BE REPLACING BOTTOM SEAL WHEN PANEL GETS REPLACED.SDR CALA2025072806959Light · damagedPROCEDURE - ROW 10 EMERGENCY SEAT MOUNTED LIGHT. INOP R&R ROW 10 SEAT MOUNTED EMERGENCY LIGHT ASSY. OPS TEST OK. REF AMM 33-51-19-000-002-A/ -400-002-A PARTS USED: 99-3350-3-0008,QTY :1SDR CALA2024120201373Battery Pack · dischargedOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - TEST SHOWS EPSU BATTERY AFT LEFT PREFORMED SELF TEST ON AFT EPSU, SHOWS BATTERY FAULT REMOVED AND REPLACED AFT EPSU BATTER REF AMM: 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK OK, OK FOR SSDR CALA2024061101768Actuator · bindingFLP 1/2 SYSTEM JAM ECAM MESSAGE. JAM OCCURED DURING APPROACH. PERFORMED OPERATIONAL TEST OF FLAP SYSTEM. NO FAULTS NOTED DURING TEST. FOLLOWED TSM 27-51-00-810-810-A UP TO PARAGRAPH 4(D). FOUND LH FLAP TRACK 1 REMOVED LH FLAP TRACK #1 ACTUATOR REF MM 27-54-4SDR CALA2022102702976Plate · bentUPPER AFT CABIN DOOR WAS BENT FROM CONTACT WITH MANLIFT. REMOVED PLATE AFT. UPPER CABIN DOOR I.A.W. S.R.M. 51-42-11, LOCATED AND DRILLED I.A.W. S.R.M. 51-44-11 AND INSTALLED PLATE AFT. UPPER CABIN DOOR I.A.W. S.R.M. 51-42-11. EMP: V933986 WC: 36199 STA: ST ENGSDR CALA2022102702958Slat · dentedRIGHT NUMBER ONE SLAT HAS DENTS DUE TO HAIL. REF. SRM 57-40-00 PB.101 TASK 283-001 THIS ITEM LOCKED FOR MX FERRY ROW TO BFM. THIS ITEM UNLOCKED FOR MAINTENANCE TO DOCUMENT SPECIFIC DEPTHS AND DIMENSIONS OF ALL DENTS. ALSO. THIS ITEM NEEDS A STATEMENT CONFIRMINSDR CALA2022102702953Frame · crackedRHS FR 20 DOUBLE JOGGLE HOLE #6 CRACKED IN FRAME LAYER AT 10 O?CLOCK POSITION. 35,177 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM INSPECTION OF FR20 F EC 5311-02907. THERE AFTER REPEAT INSPECTION AT 6,700 FLIGHT C PLOYEE V934700. RHS HOLES #5 AND #6, PER PART 2 STEPSDR CALA2022102702952Skin · crackedRHS FR 16 DOUBLE JOGGLE HOLES #8 CRACKED AT 2 O?CLOCK POSITION AND #D CRACKED AT 3 O?CLOCK POSITION. UMULATES 33,077 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM INSPECTION F THE LATEST REVISION OF EC 5311-02907. THERE AFTER REPEAT INSPE K PERFORMED BY VTMAE EMPLOYEESDR CALA2022102702951Frame · damagedLHS FR 20 DOUBLE JOGGLE HOLE #A AND #B DAMAGED. UMULATES 35,177 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM INSPECTION ISION OF EC 5311-02907. THERE AFTER REPEAT INSPECTION AT 6,700 F RFORMED BY VTMAE EMPLOYEE V934700. OF FR20 LHS HOLES #A AND #B PER PART 2 STEP 2 OSDR CALA2022102402931None · noneRH WING, T/E LWR SKIN SUPPORT PLATE FOR HYD LINE CONNECTIONS FROM PYLON IS WORN-OUT REMOVED AND REPLACED SUPPORT PLATE IAW SRM 57-21-11-300-005. EMP : V933863 WC: 36421 STA: ST ENG BFM ESFR# 1030227SDR CALA2022101802854Frame · crackedLH FRAME FOOT AT FR43 CRACKED IN OUTBOARD POSITION 3:00 FACING A FT. REPAIR BEFORE NEXT FLIGHT. REMOVED AND REPLACED FR43 IAW EA 5330-06692. EMP: V935774 WC: 36 048 STA: ST ENG BFM INSPECTION ACCOMPLISHED ON ST ENGINEERING NRC# 36048SDR CALA2022101802833Support Plate · wornLH WING T/E LWR SKIN SUPPORT PLATE FOR HYD LINE CONNECTIONS FROM PYLON IS WORK-OUT. REMOVED OLD LH WING T/E LWR SKIN SUPPORT PLATE IAW SRM 51-42-11. EMP: V933866 WC: 35978 STA: ST ENG BFM SFR# 1030170 FABRICATED NEW SUPPORT PLATE IAW DRAWING D57251216. NEW SUPSDR CALA2022101802832Stringer · corrodedAFT FUSELAGE LOWER SKIN UPPER SURFACE STRINGER 41R HAS CORROSION ON SEVERAL LOCATIONS BETWEEN FR64 AND FR58. REMOVED AND REPLACED STRINGER 41R AT AFT FUSELAGE BETWEEN FR58 A ND FR64 IAW SRM 51-42-11 AND 51-72-11. EMP: V934340 WC: 36202 ST A: ST ENG BFM SFR# 10SDR CALA2022101802831Panel · damagedUPPER AFT CABIN DOOR WAS BENT FROM CONTACT WITH MANLIFT.SDR CALA2022101802830Frame · crackedL/H FR20 DOOR STOP #7 TOP I/B HOLE HAS A CRACK INDICATION IN FRA ME AND INTERCOSTAL LAYERS. REPAIR BEFORE NEXT FLIGHT. REMOVED CRACK ON LH FR20, DOOR STOP 7, IN HOLE #1, ON FRAME AND INTERCOSTAL, IAW AIRBUS DRAWING R53113118, FLOWCHART 4, REPAIR C ODE A AND ECSDR CALA2022101802827Frame · crackedL/H FR16 DOOR STOP #7 TOP I/B AND BOTTOM I/B HOLES HAVE CRACK IN DICATIONS IN FRAME AND INTERCOSTAL LAYERS. REPAIR BEFORE NEXT FL IGHT. REMOVED CRACK ON LH FR16 DOOR STOP 7, IN HOLES #1 AND #3 ON FRAM E AND INTERCOSTAL, IAW AURBUS DRAWING R531B118, FLOWCHART 4SDR CALA2022101802824Fitting · damagedRH FR43 FOOT BTACKED AT 3:00 POSITION FACING FWD (OUTBOARD). REP AIR BEFORE NEXT FLIGHT. REPAIRED RH FR43 FOOT WITH INSTALLATION OF FREEZE PLUG IAW AIRBU S R53370233. EMP: V933863 WC: 36049 STA: ST ENG BFM SFR# 1030161 INPECTION ACCOMPLISHED ON ST ENGINEERING SDR CALA2022101802823Frame · crackedRH FRAME 16 DOOR STOP FITTING #7 TOP INBOARD HOLE CRACKED AT 7:0 0 POSITION IN THE FRAME LAYER AND DOOR STOP FITTING #7 BOTTOM IN BOARD HOLE CRACKED AT 8:00 POSITION IN THE FRAME LAYER. REPAIR B EFORE NEXT FLIGHT. REMOVED AND INSTALLED INTERCOSTAL AND DOOR STOSDR CALA2022101402815None · crackedWHILE WORKING EA 5340-01724 REV C OP002 STEP 3.1. NDT NOTED A CRACK INDICATION IN DOORSTOP FITTING 1 BOTTOM IB HOLE AT 4:00 POSITION FACING AFT FRAME 68 LH. (REF LP 9682403 ? PREVIOUSLY CLEARED IN ERROR) -12-300-008. INSTALLED FITTING PER SRM 52-13-31-400-022-SDR CALA2022100602697Stop Fitting · crackedWHILE WORKING EA 5340-01724 REV C OP002, STEP 3.1 NDT NOTED A CRACK INDICATION IN DOOR STOP FITTING 1 BOTTOM IB HOLE AT 4:00 POS ITION FACING AFT. FRAME 68 LH REPAIRED LWR I/B HOLE AT L/H FR68 DOOR STOP FITTING #1 IAW SRM 5 3-41-12-300-010. AND INSTALLED DOOR SDR CALA2022100602696Fitting · crackedLH FRAME FOOT AT FR43 CRACKED IN OUTBOARD POSITION 3:00 FACING A FT. REPAIR BEFORE NEXT FLIGHT.SDR CALA2022093002581Panel · crackedCTR FUSELAGE LH FR 36 PRESSURE PANEL CRACKED I/B HOLES #9, #20, #26 ACCOMPLISHED ON VTMAE NR 36413 BY VTMAE EMPLOYEE V933870. N PRESSURE PANEL HOLES AREA PER PART 2 OF THE LATEST REVISION OF OR BEFORE MARCH 23, 2023, PERFORM AN INSPECTION OF THE LH FR 36 ECRA SDR CALA2022091602374Seat Track · corrodedCABIN SEAT TRACK -Y765 FR20-22 IS CORRODED ON TOP SURFACE. CABIN SEAT TRACK REMOVED AND INSTALLED NEW SEAT TRACK P/N 531127 822020A I.A.W SRM 51-72-11 AND 51-42-11. (T#87305) WORK ACCOMPLI SHED AT ST ENGINEERING OF MOBILE AT BFM ON N/R#: 36182SDR CALA2022090702307Seat Track · corrodedCABIN SEAT TRACK -Y1292 FR20 IS CORRODED ON TOP SURFACE. REMOVED CORROSION FROM CABIN SEAT TRACK -Y1292 FR20 IAW SRM 51-7 4-00 FOUND TO BE OUT OF LIMITS. REMOVED NAD INSTALLED NEW SEAT T RACK P/N 5311298220201 IAW SRM 51-42-11. EMP: V934335 WC: 36183 STA: ST ESDR CALA2022090202244None · noneFORWARD CARGO THRESHOLD SILL PLATE HAS CORROSION FR25-FR28 REMOVED CORROSION AT DOOR SILL PLATE AT FWD CARGO IAW SRM 51-74- 51-42-11. EMP: V935834 WC: 36166 STA: ST ENG BFM 00 CHECK LIMITS ORIG. MAT 0.063" D=0.019" L=3.5" W=1" MAT. REMAI NING 0.042" (T93968) FSDR CALA2022090202243Beam · nonePASSENGER CABIN, BETWEEN FR16 AND Y518, RAIL DUMMY HAS CORROSION RMEOVED CORROSION ON RAIL DUMMY AT FR16 T518 IAW SRM 51-74-00, F SRM 51-75-12. EMP: V933986 WC: 36250 STA: ST ENG BFM OUND WITHOUT OF LIMITS IAW SRM 51-11-14-203-007, MEASURE: L=1.90 0", W=1.4", SDR CALA2022082902200Doubler · noneDURING AASR SURVEY TO COMPLY WITH 14 CFR 121.1109, FOUND DOUBLER REPAIR AT FR65 BETWEEN STRG26L AND STGR29L NO DOCUMENTS COULD B E FOUND OF REPAIR IN RECORDS REMOVED OLD REPAIR DOUBLER AT FR65 BETWEEN STR26L AND STGR29L. M EMP: V933866 WC: 36354 STA: ST ENG BFSDR CALA2022082902197Seat Track · corrodedAFT CABIN FLOOR STRUCTURE: SEAT TRACK INBOARD LH (Y765) HAS CORR OSION IN FR66 REMOVED AND REPLACED SEAT TRACK IAW SRM 51-42-11. EMP: V934614 W C: 36262 STA: ST ENG BFM SFR# 1029532SDR CALA2022082602184Floor Support · nonePASSENGER CABIN, BETWEEN FR20 AND Y-1732, FLOOR STR HAS CORROSIO N. REMOVED CORROSION ON FLOOR STR WEB IAW 51-74-00, FOUND TO BE OUT STA: ST ENG BFM OF LIMITS L=0.849", W=0.550", D=0/060", REMOVED WEB BETWEEN FR2 0 AND Y-1732 IAW SRM 51-42-11 AND INSTALLED NEWSDR CALA2017100203422Lamp · inoperativeRED EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-18. OPS CHECKED GOOD.
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