N454UA
Service difficulty reports · 126
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 = 'N454UA' 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 = 'N454UA' 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 CALA2026091419405Battery · faultedPROCEDURE - EPSU BAT CAP AFT L FAULT. REMOVED AND REPLACED BATTERY AMM REF 33-51-38-400-002-A. OPS CHECK OK, OK FOR SERVICE.SDR CALA2026080218149Spoiler · damagedLEFT WING NR 2 SPOILER DAMAGED, REMOVED NR 2 LT SPOILER IAW AMM 27-64-42-000-001-A, TRIMMED OUT DAMAGED SKIN SECTION SIZE= 1.0" DIA. CLEANED, INSTALLED COMPOSITE REPAIR, CURED, RESTORED PAINT FINISH AND REINSTALLED PREVIOUSLY REMOVED SEAL AND SEAL RETAINER ISDR CALA2026061717163Uplock · faultedNOSE LANDING GEAR DOORS DID NOT CLOSE UPON RETRACTING GEAR ON TAKEOFF. CYCLED NO JOY. NLG DOORS DID NOT LOSE UPON RETRACTING GEAR ON TAKEOFF. CYCLED NO JOY. PERFORMED REMOVAL OF THE NLG DOOR-UPLOCK ASSY IAW AMM 32-31-14-000-001. CHECKED MATING SURFACES & SDR CALA2026031014455Unknown · odorAIRCRAFT HAD AN ODOR IN BACK, AFTER LIGHTNING STRIKE. C/W TSM TASK 21-00-00-615-802-A, NO SMELL FOUND. .NO LIGHTNING STRIKE EVIDENCE FOUND. OK TO CONTINUESDR CALA2025102010308Bottle · low pressureDOOR 2L PRESSURE IS LOW. PRESSURE IS 1650. DOOR PRESSURE IS SERVICABLE PER AMM 52-13-14-200-001-A.SDR CALA2025093009426Tire · bulgedNR 3 MLG TIRE FOUND BEYOND AMM LIMITS. MUST BE REPLACED PRIOR TO T HE NEXT FLIGHT. RAMP REPORT: NR 3 TIRE HAS A LARGE BULGE AT THE 6 O'OCLOCK POSITION. WILL NEED REPLACEMENT REPLACED #3 MLG TIRE REF. AMM 32-41-11-400-006-A.SDR CALA2025081507803Filter · odorSECOND HALF OF FLT NOTICED AN ACCRID OR SMELLY GYM SOCKS WITH PACKS ON. NO SMOKE PRESENT. PER CREW ODOR CONTINOUS WITH APU RUNNING & IN FLIGHT DECK, REF TSM 05-50-810-831-A. APU NEEDS INSPECTION IAW AMM 49-00-00-200-816. NOTED BY MAINT. NO PRIOR HISTORY. SDR CALA2025042504219Aoa · faultedGRAPHIC DISPLAY OF VLS ON ND IS 5 KNOTS HIGHER THAN FMGC. ND SHO WS VLS SAME AS APP SPEED CREW STATED DISCREPANCY WAS VISIBLE IN BOTH PFDS. FOLLOWED TSM 22-66-00-810-889-A LAST LEG CLASS 3 FAULTS DISPLAYS AOA SENSOR1 ( 3FP1 )", ADR1 TEST SHOWS MSG AOA SENSORSDR CALA2025010601819Battery · no testOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSU BATTERY EMER L 33-51-38 12WL FAILS BATTERY TEST. LOWER FLOOR PANEL REMOVED ROW 21A REMOVED AND REPLACEDEPSU BATTERY MERL, PER 33-51-11, TEST OK. PARTS USED: 18-3351-3-0001,QTY :1SDR CALA2024110801080None · noneFA EMERGENCY CHECKLIST BEHIND SEAT 3B NEEDS TO BE REPLACED. VERIFIED F/A EMERGENCY CHECKLIST WAS REPLACED IN THE BACK OF SEAT 3B.SDR CALA2024090302367Blowout Panel · missingTEST FLIGHT, RIGHT WING BLOW OUT PANEL 622AB MISSING.SDR CALA2024083000513Blowout Panel · missingPDA 2 UPON RETURN OF TEST FLIGHT 3836 IN LCQ. FOUND PANEL # 622AB MISSING FROM RT WING LEADING EDGE REF LOG PAGE 9081839. IAW GMM 02-30-95. UPDATED TO ATTACH IMAGE. RT WING PANEL 622AB FOUND MISSING AFTER TEST FLIGHT.SDR CALA2024082602282Hinge Arm · crackedRIGHT HORIZONTAL STAB NR 3 HINGE ARM CRACKED. REMOVED AND REPLACED RT HORIZONTAL STAB NR 3 HINGE ARM IAW SRM 51-42-11/0 01.SDR CALA2024082102248Flange · damagedEA 5310-07639 REQUIRES UPDATED ECRA. CLEARING LP.RII INSPECTION C/W BY HAECO LCQ INSP LC-66 QC RECORDS UPDATE PLANNING TO CONTACT ENGINEERING AFTER 68,165 TOTAL AIRCRAFT FLIGHT CYCLES BUT BEFORE 69,165 TOTAL AIRCRAFT FLIGHT CYCLES FOR THE PART 2B INSPECTION RSDR CALA2024081202197Threshold · corrodedFWD PIT THRESHOLD FR 27 CORROSION NOTED AT TIE DOWN LOCATION PER HAECO LCQ 9298941/36941.SDR CALA2024072602114Floor Support · crackedFLIGHT DECK HAS 1 EA CRACKED FLOOR WEBS 1 ON CAPT. SIDE. GENERAT ED BY PER HAECO LCQ NR9298360/36360 REMOVED AND REPLACED WEB IN FLIGHT DECK L/H FR 8-11 IAW A320 SRM 51-72-11. ACCOMPLISHED BY INSPECTED BYSDR CALA2024072602113Floor Support · crackedRH FLIGHT DECK CRACKED FLOORBEAM AT FR8-11. GENERATED BY ON HAECO LCQ NR 9298874/36874 REMOVED AND REPLACED WEB IN FLIGHT DECK R/H FR 8-11 IAW A320 SRM 51-72-11. PERFORMED BY INSPECTED BYSDR CALA2024072902118Torque Box · corrodedAFT PIT TORSION BOX COVER CORRODED. REMOVED AND REPLACED TORSION BOX COVER AT AFT PIT IAW A320 SRM 5 1-42-11-001SDR CALA2024071902065Skin · abnormalR/H ELEVATOR TOP SIDE HAS LIQUID INGRESS AT 91 INCHES FROM I/B 5 1/2 INCHES FROM TRAILING EDGE 2 INCHES IN DIAMETER. DRILLED WITNESS HOLES ON RH ELEVATOR UPPER SURFACE 91 IN FROM VB 5.5 IN FROM T/E 1.5 IN DIA ZONE C IAW A320 AMM 55-20-00-200-006 A PAR 4 A(6) SDR CALA2024071502036Profile · gougedEMERGENCY EXIT INTERNAL STRUCTURE R/H FWD HATCH GOUGES ON AFT LO AD TRANSMITTING PROFILE. REMOVED AND REPLACED AFT FRAME SEGMENT ON FWD O/W HATCH RH IAW A 320 SRM 51-72-11-911-001SDR CALA2024071502035Profile · gougedEMERGENCY EXIT INTERNAL STRUCTURE R/H FWD GOUGES ON FWD LOAD TRA NSMITTING PROFILE. REMOVED AND REPLACED FWD FRAME SEGMENT ON FWD O/W HATCH IAW A320 SRM 51-72-11-911-001SDR CALA2024052201558Battery · dischargedOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - EPSI BATTERY EMER R AND EPSU BATTERY AFT L MSGS PRESENT R&R EMER R AND AFT L EPSU BATTERY PACKS REF AMM 33-51-38. OPS CK GOOD OF BOTH PARTS USED: 18-3351-3-0001,QTY :1SDR CALA2024040901008Computer · intermittentSLAT SYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL FOLLOW TSM 27-51-00-810-806-A C/W 27-51-00-810-06A NO FAULTS FOUND. LOOK IN LAST LEG REPORT FOR SLAT FOUND DE POWER INTERRUPT WITH NO T/S DATA REF TSM 27-81-00-810-811A. CLEARS DEFECT. DUE TO HISTORY WSDR CALA2024010200005Fuel Cap · missingDURING WALK AROUND FOUND REFUELING CAP COUPLING MISSING CAP COUPLING NIS AT SFO, REQ DEFERRAL INSTALLED NEW REFUEL COUPLING CAP PER AMM 28-25-41-400-005-A. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1555928 SN OFF 2814 CAP, COUPLING R OFF 31-2825-9-0001 281SDR CALA2022121903423Fitting · crackedF.O LOWER WINDHISELD CONTINUITY FITTING AT LOWER CENTER POST PRODUCED A CRACK INDICATION DURING THE HFEC INSPECTION. GENERATED A T HAECO LCQ PER NR 9298244 (32244) BY V061690 EA 5310-07675 AD 2 020-17-03. THE FRONT WINDSHIELD FRAME RH CONTINUITY FITTING, ACCOMSDR CALA2022112503216Frame · crackedFR 68 RH AT STR 22 HAS CRACK INDICATION IN RADIUS ABOVE LOWER IB BOLT. (EA RELATED). GENERATED BY V892444 AT HAECO LCQ PER NR 92 98138(32138). INITIAL INSP AT RH FR68 STR22 RPR PART HORZ FLANGE & INNER CAP N OR BEFORE 49,080 TOTAL ACFT FC. ACMP REPEAT INSP NOTSDR CALA2022111703156Floor Support · corrodedAFT CABIN, R-2 DOOR ENTRYWAY SILL PLATE CORRODED. GEN BY V913126 ON HAECO LCQ NR 9298338/32338 REMOVED AND REPLACED R2 DOOR SILL IAW A320 SRM 51-72-11-911-001 AND A320 SRM 51-42-11-001. ACMP BY MECH V077956 INSP BY N078570SDR CALA2022110203009Skin · contaminatedR/H ELEVATOR UPPER PANEL PRODUCED INDICATIONS OF WATER INGRESS D URING THERMOGRAPHY INSPECTION. INDICATION LOCATION IS 16.25IN FR OM INBD EDGE AND 8.75IN FWD OF THE T/E. 1.25 INCH WIDTH BY 1.5IN LENGTH. GENERATED AT HAECO LCQ PER NR 9298181 (32181) BY V06169 0SDR CALA2022110203008Skin · contaminatedR/H ELEVATOR UPPER PANEL PRODUCED INDICATIONS OF WATER INGRESS D URING THERMOGRAPHY INSPECTION. INDICATION LOCATION IS 15.5 IN FR OM INBD EDGE AND 24.5IN FWD OF THE T/E. 1 IN WIDTH BY 1.5 IN LEN GTH. GENERATED AT HAECO LCQ PER NR 9298182 (32182) BY V061690. {ESDR CALA2022110203007Skin · contaminatedR/H ELEVATOR UPPER PANEL PRODUCED INDICATIONS OF WATER INGRESS D URING THERMOGRAPHY INSPECION. INDICATION LOCATION IS 13.5 IN FRO M INBD EDGE AND 9 IN FWD OF THE T/E. 1 INCH WIDTH BY 1.5 INCH LE NGTH. GENERATED AT HAECO LCQ PER NR 9298180 (32180) BY V061690. {SDR CALA2022050601161Accumulator · overservicedLOWSPEED ABORT DUE TO BLUE HYD LO AIR PR ECAM VERBAL FROM CAPTAIN : THERE WAS NOT "HYD B RSVR LO AIR PR" MSG. T/S PER TSM 29-12-00-810-801A FOUND BLUE SYS OVERSERVICED AND ACCUMLATOR PRESS LOW. SERVICED ACCUMLATOR AND DRAINED RES IAW AMM 29-10-00-680-003A ANDSDR CALA2019052700839Battery · failed(SUPPORT TASK) L-58 NO DOT. THE RT EPSU (12WL) FAILS IT'S BATTERY WHEN TESTED FROM THE PTP. NONROUTINE 9619154 REMOVED AND REPLACED RT EPSU BATTERY IAW AMM 33-51-38-000- 002-A AND 33-51-38-400-002A. PERFORMED TEST OF EPSU BATTERY IAW AMM 33-51-38-000-002-A SUBSDR CALA2018081731790Relay · inoperativeDOOR WARNING FAILED STEP 8, CLOSED CIRCUIT BREAKER P11 AND OPEN CIRCUIT BREAKER P10 OF THE DOOR WARNING CARD. REMOVED AND REPLACED THE RELAY 12WN IAW ESPM 20-46-50, FOUND FAULTY WHEN TROUBLESHOT IAW TSM 52-11-00. AFFIRMED THE OPS TEST OF THE DOOR WARNING ISDR CALA2018081701801Fitting · crackedLEFT WINDSHIELD SIDE POST AT FRAME 4, UPPER ATTACHMENT FITTING HAD A CRACK INDICATION. REPAIRED THE WINDSHIELD POST IAW ECRA 5311-01984, PART 3.SDR CALA2018081761796Skin · crackedINTERNAL FUSELAGE SKIN, FRAME 35, STRINGER 30L, AFT LOWER FASTNER HOLE HAD A CRACK INDICATION. REPAIRED IAW PART 3 OF ECRA 5311-01981.SDR CALA2018080601760Floorbeam · corrodedAFT CARGO BAY FLOORBEAM AFT SIDE OF FRAME 64, BETWEEN STRINGERS 44R TO 43R WAS CORRODED. REPAIRED IAW EC/RA 5341-01125.SDR CALA2018080601751Rib · crackedCRACKS WERE FOUND ALONG THE RIVET HEADS AT THE AFT INNER VERTIVAL RIB IN THE RT AFT EMERGENCY EXIT HATCH. REMOVED AND REPLACED THE RIB IAW SRM 51-42-11-001, AND SRM 51-72-11-911-001.SDR CALA2018080601750Rib · crackedCRACKS WERE FOUND ALONG THE RIVET HEADS AT THE FWD INNER VERTICAL RIB IN THE LT FWD EMERGENCY EXIT HATCH. REMOVED AND REPLACED THE RIB IAW SRMS 51-42-1 1-001, AND 51-72-11-911-001.SDR CALA2018080601749Rib · crackedCRACKS FOUND ALONG THE RIVET HEADS AT LOWER AFT INNER VERTICAL RIB IN THE RT FWD EMERGENCY EXIT HATCH., REMOVED AND REPLACED THE RIB IAW SRM 51-42-11-001, AND 51-7 2-11-911-001.SDR CALA2018080601748Rib · crackedCRACKS FOUND ALONG THE RIVET HEADS AT THE FWD INNER VERTICAL RIB ON THE RT AFT EMERGENCY EXIT HATCH. REMOVED AND REPLACED THE VERTICAL RIB IAW SRM 51-42-11-001, AND 51-72-11-911-001.SDR CALA2018080601747Rib · crackedFOUND CRACKS ALONG RIVET HEAD AT UPPER AFT INNER VERITCAL RIB ON THE LT FWD EMERGENCY EXIT HATCH. REMOVED AND REPLACED THE RIB IAW SRMS 51-42-11-001, AND 51-72-1 1-911-001.SDR CALA2018073001731Wire Harness · damagedDURING REMOVAL OF THE EEP HARNESSES, IT WAS NOTED THAT ROWS 7-8 HAVE A BROKEN WIRE. REMOVED AND REPLACED EEPL HARNESSES AT SEAT ROWS 7-8 WITH NEW ONES IAW AMM 33-51-22-400-802CL. OPS CHECK TO BE PERFORMED ON WORK CARD.SDR CALA2018073001730Seal · blownL2 DOOR FLEXABLE CONTROL CABLE HAS BLOWN SEAL. REMOVED AND REPLACED L2 DOOR FLEXABLE CABLE IAW AMM-52-13-2 2-400-001-A SUBTASK 52-13-22-420-052-C. LUBRICATED CABLE IAW SUBTASK 52-13-22-640-051-A. RIGGING PERFORMED ON ROUTINE CARD.SDR CALA2018073001726Roller · seizedSIDE ROLLER SEIZED ON LT AFT EMERGENCY EXIT. HATCH REMOVED AND REPLACED SIDE ROLLER (FWD) ON LT AFT EMERGENCY EXIT HATCH IAW CMM-52-21-11 SUBTASK 52-21-11-400-004-A01.SDR CALA2018073001725Hinge Fitting · wornL1 DOOR UPPER HINGE ARM BEARING MIGRATING OUT OF HOUSING. REMOVED AND REPLACED L1 DOOR UPPER HINGE ARM FITTING ASSEMBLY IAW 52-11-31-400-002-A SUBTASK 52-11-31-420-054-A.SDR CALA2018073001724Wire Harness · damaged(DURING REMOVAL OF THE EEPL HARNESS ES, IT WAS NOTED THAT ROWS 32-35 HAVE A DAMAGED WIRE NEAR THE SWD CONNECTOR. REMOVED AND REPLACED EEPL HARNESSES AT SEAT ROWS 32-35 WITH NEW HARNESSES IAW AMM 33-51-22-400-802C1. OPS CHECK PERFORMED ON WORK CARD.SDR CALA2018071901659Plate · corrodedREMOVED, MATCH DRILLED & REPLACED CORRODED FISH PLATE AT FR 32 STR 43-44 LT, RESTORED SURFACE PROTECTION IAW SRM 51-72-11 -911-001 IAW ER5100R01017 REV E. FWD CARGO COMPARTMENT FROM FR32 FROM STRG 43-44 ON LT SIDE FISH PLATE & RIVETS HAVE CORROSION. INSP COMPLSDR CALA2018071901658Plate · corrodedFWD CARGO COMPARTMENT FROM FR 30 FROM STR 43-44 ON LT SIDE. FISH PLATE & RIVETS HAVE CORROSION. REMOVED, MATCH DRILLED & INSTALLED FISH PLATE AT FR 30 STR 43L TO 43R DUE TO CORROSION, RESTORED SURFACE PROTECTION IAW SRM 51-72-11-911-001, ER 5100R01017 REV E. ISDR CALA2018071901657Plate · corrodedFWD CARGO COMPARTMENT FROM FR 26 FROM STG 43-44 ON RT SIDE FISHPLATE & RIVETS HAVE CORROSION. REMOVED, MATCHDRILLED & REPLACED CORRODED FISH PLATE AT FR 26 STG 43-44 RT, RESTORED SURFACE PROTECTION IAW SRM 51-72-11-9 11-001 IAW ER 5100R01017 REV E. INSP COMPLISDR CALA2018071901656Plate · corrodedFWD CARGO COMPARTMENT FROM FR 30 FROM STR 40-41 ON LT SIDE. FISH PLATE & RIVETS HAVE CORROSION. REMOVED, MATCHDRILLED & REPLACED CORRODED FISHPLATE AT FR 30 STR 40-41 LT RESTORED SURFACE PROTECTION IAW SRM 51-72-11-911- 001, ER5100R01017 REV E. INSP COMPLIED W
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