N458UA

Service difficulty reports · 150

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 = 'N458UA' 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.

SDR CALA2019010200004Fitting · corrodedCARGO COMP DOOR SURROUND FWD CORNER FITTING HAS CORROSION. REMOVED AND REPLACED CORNER FITTING PER SRM 51-72-11-911-00 1 PARA 2.A.Dec 31, 2018 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019010200003Stringer Splice · corrodedA3NB-53-3-6105 FWD CARGO COMPT BETWEEN FR30-31 STR42L SPLICER HA S CORROSION SPOT ON UPPER SURFACE 18-5321-1-2706 AT PER REF NO.9295285 REMVOED AND REPLACED 1EA CORRODED STR SPLICE IN THE FWD CARGO CO MP BETWEEN FR30-31 STR42L IAW SRM 51-72-11-911-001.Dec 31, 2018 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019010200002Stringer · corrodedAFT CARGO BILGE BETWEEN FRAMES 63 AND 64 STRINGER 42 LEFT IS CORRODED. (A3NB-53-3-6185 18-5341-2905. PER REF. NO. 9295 264 (41264). GENERATED. CORRECTION FOR PREVIOUS ENTRY. A3NB-05-3-6022 AFT CARGO BILGE BETWEEN FR63 AND 64 STR42 LEFT IS CORRODED REMOVED AND Dec 31, 2018 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019010200001Splice Plate · corrodedFORWARD CARGO COMPARTMENT BETWEEN FR30-31 STRINGER 41L & SPLICER HAVE CORROSION SPOTS ON UPPER SURFACE ON REF 9295284 SPEC A3NB-53-3-6105. NR GENERATED REMOVED AND REPLACED (FISH PLATE) SPLICER IN FWD CARGO COMPT BETWEEN FR30-31 STR41L IAW SRM 51-72-11-001 STEDec 31, 2018 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018123102688Cleat · corrodedFORWARD CARGO COMPARTMENT BETWEEN FR30-31 & BETWEEN STRINGERS 43 L-44 CLEAT HAS CORROSION SPOT ON UPPER SURFACE ON HAECO LCQ REF 9295286 SPEC A3NB-24-3-6046. NR GENERATED BY V919150 REMOVED AND REPLACED CORRODED CLEAST BETWEEN FR30 TO FR31 AND BE TWEEN STR43 LDec 30, 2018 · N458UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR CALA2018122872667Repair · not reportedAD RELATED 2016-18-09 UPON REMOVAL OF FR34 BELLY FAIRING BETWEEN STR43L-43R REPAIR DOUBLER WAS FOUND. DOUBLER REQ''S PREVIOUS REP AIR INFO AT HAECO LCQ PER REF NO.9294479 BY MECH V913402 REMOVED AND REPLACED SKIN DOUBLER AT FR34,STR43L TO STR43R IAW S RM 53-00Dec 27, 2018 · N458UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2018122872658Shear Plate · corrodedR/H AFT CABIN AFT SHEAR PLATE SUPPORT HAS CORROSION ON LOWER SUR FACE BETWEEN FR 69-70 - EA 5346-01001 REV B OPS 007 - GENERATED BY V077960 AT HAECO LCQ PER N/R 9295327 REMOVED AND REPLACED SHEAR PLATE SUPPORT IN AFT CABIN R/H SIDE FR69-70 IAW A320 SRM 51-42-1Dec 26, 2018 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018122872657Hinge Fitting · misalignedA3NB-55-3-6022; RUDDER HINGE FITTING #6 MISALIGNED BY MECH V0802 85 AT HAECO LCQ PER REF NO.9295346 REMOVED AND REPLACED #6 HINGE FITTING IAW A320 SRM 55-36-42-300- 001 PARG 2.A. AND AMM 55-36-41-000-001-A PARG 4.B. WORK ACCOMPLI SHED BY TECH V061630 AND INSP Dec 26, 2018 · N458UA · Airbus A320232 · Rudder StructureSDR CALA2018122872656Fitting · corroded(A3NB-53-3-6222) L-2 DOOR LOWER CUTOUT AFT CORNER FITTING CORROS ION AT HAECO LCQ BY MECH N078570 REMOVED AND REPLACED L2 DOOR LWR AFT CORNER FITTING IAW A320 SRM 51-72-11-911-001 MECH V915153 INSP LC-61Dec 26, 2018 · N458UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR CALA2018122872652Doubler · corrodedLAV EXHAUST VENT INTERIOR MATING SURFACE AT FR70 HAS CORROSION O N HAECO LCQ REF 9295110 SUPPORT TASK. NR GENERATED BY V901092 REMOVED AND REPLACED LAV EXHAUST VENT REINFORCEMENT PLATE DOUBLE R FR70 IAW A320 SRM 51-42-11-001 PARA E AND DRAWING #D5348019100 0 BDec 26, 2018 · N458UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018122872646Hinge · misalignedA3NB-55-3-6022; RUDDER HINGES #3 ARE MISALIGNED AT HAECO LCQ PE R REF NO.9295256 BY MECH V061757 REMOVED AND REPLACED NO. 3 HINGE FITTING IAW A320 SRM 55-36-42-3 00-001 PARG 2A AND AMM 55-36-41-400-001-A PAR 6H. BY MECH V08028 5 AND INSP BY LC-66.Dec 23, 2018 · N458UA · Airbus A320232 · Rudder StructureSDR CALA2018122872645Fitting · misalignedA3NB-55-3-6022; RUDDER HINGE ARM FITTING #7 MISALIGNED AT HAECO LCQ PER REF NO.9295347 BY MECH V080285 REMOVED AND REPLACED NO. 7 HINGE FITTING IAW A320 SRM 55-36-42-3 00-001 PARG 2A AND AMM 55-36-41-400-001-A PAR 4. BY MECH V08028 5 AND INSP BY LC-66.Dec 23, 2018 · N458UA · Airbus A320232 · Rudder StructureSDR CALA2018122402637Frame · corrodedFORWARD CARGO COMPARTMENT FR30 BETWEEN STRINGERS 40R-41R CLEAT H AS CORROSION SPOT ON UPPER SURFACE SPEC A3NB-53-3-6105 GEN BY V9 19150. REMOVED CORRODED CLEAT AND REPLACED NEW CLEAT IAW AIRBUS A320 51 -42-11-001. ALODINE,TREATED,PRIMED AND TOPCOATED IAW A320 Dec 23, 2018 · N458UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2018122402636Intercostal · damagedA3NB-53-4-6304 R1 DOOR FR20 #4 STOP FITTING UPPER PTBD BOLT HOLE PRODUCES REJECTABLE INDICATIONS DURING RFHEC INSP AT HAECO LCQ PER REF NO.9294679 BY MECH V061690 REMOVED AND REPLACED R1 FR20 #4 INTERCOASTAL IAW A320 SRM 51-42- 11 BY MECH V913402 INSP LC-99Dec 23, 2018 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018121762585Door Sill · corrodedSPEC #A3NB-53-3-6222 L2 DOOR SILL FASTNER HOLES HAVE CRROSION AT FR68 AT HAECO LCQ BY MECH V061642 REMOVED AND REPLACED L2 DOOR SILL IAW A320 SRM 51-72-11-911-001 BY MECH V915153 INSP BY LC-61Dec 13, 2018 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018121402561Threshold · corrodedAFT CARGO PIT DOOR THRESHOLD UPPER SHEET METAL I/B OF FISH PLATE FROM, FR52R TO FR56R UPPER SURFACE HAS CORROSION (A3NB-53-4-6179 ) PER HAECO LCQ REF. NO. 9294873(40873) GENERATED BY V902249. REMOVED AND REPLACED AFT PIT CARGO THRESHOLD COVER SHEET IAW A32 0 SDec 11, 2018 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018121762584Fitting · corrodedR-2 DOOR LOWER CUTOUT AFT CORNER FITTING HAS CORROSION - {A3NB-5 3-3-6222} - GENERATED BY TECH V061603 AT HAECO LCQ PER N/R 92952 28 REMOVED AND REPLACED CORNER FITTING AT FR68 IAW A320 SRM 51-72-1 1-001, SRM 51-42-11-001. RECEIVED NEW CORNER FITTING PN D53480Dec 10, 2018 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018121762583Door Sill · corrodedR2 DOOR SILL FASTENER HOLES HAVE CORROSION AT FR 68 A3NB-53-3-62 22 GENERATED BY V061642 ON HAECO LCQ NR 9294753 REMOVED AND REPLACED DOOR SILL AT R2 DOOR FR66-FR68 IAW A320 SRM 51-42-11-001,SRM 51-72-11-001. RECEIVED NEW R2 DOOR SILL IAW A3 20 53-41-14-001 PNDec 10, 2018 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2018121762582Fitting · corrodedR-2 DOOR LOWER CUTOUT FWD CORNER FITTING HAS CORROSION - {A3NB-5 3-3-6222} - GENERATED BY TECH N078570 AT HAECO LCQ PER N/R 92951 12 REMOVED AND REPLACED CONER FITTING AT FR66 IAW A320 SRM 51-72-11 -001, SRM 51-42-11-001 RECEIVED NEW CORNER FITTING IAW A320 SRDec 10, 2018 · N458UA · Airbus A320232 · Service DoorsSDR CALA2018120702497Stop Fitting · not reportedR1 DOOR FR16 NO.7 STOP FITTING BOTH INBD BOLT HOLES PRODUCE REJE CTABLE INDICATIONS DURING RFHEC INSPECTION A3NB-53-4-6304 GENERA TED BY V061690 ON HAECO LCQ NR 9294675 REMOVED AND REPLACED #7 INTERCOASTAL @ R1 DOOR FR16 IAW A320 SRM 51-72-11 BY MECH V913402 IDec 1, 2018 · N458UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2018120702491Stop Fitting · crackedL1 DOOR FR16 NO.7 STOP FITTING BOTH UPPER BOLT HOLES AND THE LOW ER INBD BOLT HOLE PRODUCES REJECTABLE INDICATIONS DURING RFHEC I NSPECTION AD 2017-22-03 A3NB-53-4-6304 GENERATED BY V061690 ON H AECO LCQ NR 9294683 REMOVED AND REPLACED LH FR 16 NO.7 INTERCOASTNov 30, 2018 · N458UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2017120304302Lens · unsecureDOOR 2L EMERG SIGN COVER FELL OFF. REPLACED LENS ASSY.Dec 3, 2017 · N458UA · Airbus A320232 · Emergency LightingSDR CALA2017091803250Proximity Sensor · out of adjustLOWER ECAM SCREEN SHOWS THE R2 DOOR SLIDE NOT ARMED. FOUND DOOR ARMING PROXIMITY SENSOR 7WN2 OUT OF ADJUSTMENT. ADJUSTED THE SENSOR IAW AMM 52-71-00-820-002-A01. VERIFIED COCKPIT ECAM AND HANDLE OPS GOOD. VERIFIED THE R2 DOOR OPERATION ,SAFETY AND SECURITY.Sep 18, 2017 · N458UA · Airbus A320232 · Escape SlideSDR CALA2017090102970Door Sill · corrodedR2 DOOR SILL PLATE INBD EDGE HAS CORROSION AT SCREW HOLE UPPER AND LWR SURFACE FRAMES 68 8-35. CUTOUT DAMAGED AREA ON R2 DOOR CUTOUT SILL PLATE SCREW HOLE AND INSTALLED REPAIR PER A320 SRM 53-41-14 FIG 20101 REPAIR PRINCIPLE NO.5Sep 1, 2017 · N458UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2017051901488Cover · missingEMER EXIT LT AT 1B MISSING COVER. REPLACED EMERGENCY EXIT LIGHT MODULE IAW AMM 33-51-18 PB 401. TEST OK.May 19, 2017 · N458UA · Airbus A320232 · Emergency LightingSDR CALA2016081295642Battery Pack · no testEMERGENCY LIGHT FAILED OPS TEST, EPSU BATTERY. RESET EPSU BATTERY, OPS TESTED OKAug 7, 2016 · N458UA · Airbus A320232 · Emergency LightingSDR CALA2016081195625Battery Pack · no testEMERGENCY LIGHT SYSTEM TEST FAILED. REPLACED EPSU AND BATTERY AT DOOR 1L, OPS CHECKED GOODJun 5, 2016 · N458UA · Airbus A320232 · Emergency LightingSDR CALA2016051295350Power Supply · faultyEMERGENCY POWER SUPPLY UNIT FWD LT MSG ON PTP PANEL AT DOOR 1L. REPLACED EMER POWER SUPPLY UNIT 10WL IAW MM 33-51-38-401. OPERATIONS NORMAL.May 11, 2016 · N458UA · Airbus A320232 · Emergency LightingSDR CALA2015121494891Frame · corrodedFRAME 65, BETWEEN STRINGERS 33R & 34R, ELONGATED HOLE UNDER FASTENER. REMOVED FASTENER & FRAME CLIP FROM STRINGER 35R TO 40R, FWD SIDE IAW SRM 53-00-1 2. RESTORED PROTECTIVE FINISH IAW SRM 51-75-12, NO SRI REQUIRED.Dec 11, 2015 · N458UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2015121494890Stringer · corrodedSTRINGER 39R, FROM FRAME 65 - 66.5, HAS CORROSION IN MULTIPLE AREAS. REMOVED CORROSION BEYOND LIMITS. PROCURED REPLACEMENT STRINGER PAR D5348012521400. LOCATED, DRILLED, DEBURRED & RESTORED PROTECTIVE FINISH IAW SRM 51-44-11.Dec 11, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015121494889Doubler · corrodedWASTE PANEL INTERNAL DOUBLER CORRODED. REMOVED WASTE SERVICE PANEL, REMOVED FRAME CLIPS & STRINGER CLIPS AT REQUIRED & REMOVED WASTE PANEL INT DOUBLER. FABRICATED REPLACEMENT DOUBLER, LOCATED, DRILLED & DEBURRED. INSTALLED DOUBLER, FRAME CLIPS & STRINGER CLDec 11, 2015 · N458UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2015121494888Stringer · damagedSTRINGER 35R, FRAME 65 - 66 HAS OUT OF ROUND HOLES. REMOVED DAMAGED STRINGER 35R FROM FRAME 65 - 66. FABRICATED REPLACEMENT STRINGER. LOCATED, DRILLED & DEBURRED, INSTALLED & REST ORD SURFACE PRO IAW SRM 51-75-12.Dec 11, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015121494885Stringer · corrodedSTRINGER 39 RT, BETWEEN FRAME 65 - 65 HAS CORROSION. R & R IAW SRM 51-72-11.Dec 9, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015121494884Stringer · corrodedSTRINGER 38 RT, BETWEEN FRAME 65 & 65 HAS CORROSION. REMOVED DAMAGED STRINGER 38 RT, BETWEEN FRAME 65 & 65. FABRICATED REPLACEMENT STRINGER & LOCATED, DRILLED & DEBURRED REPLACEMENT PART. INSTALLED & RESTORED PROTECTIVE FINISH IAW SMR 51-42-11.Dec 9, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015121494883Stringer · corrodedCORROSION ON STRINGER 40R, BELOW FRAME 65 IN AFT CARGO COMPARTMENT. R & R STRINGER 40R, BELOW FRAME 65 IN AFT CARGO COMPARTMENT. LOCATED & DRILLED NEW HOLES, INSTALLED NEW STRINGER SHEAR TIE & SPLICED IAW SRM 51-72-11 & SPLICED PROTECTIVE COAT IAW SRM 51-23-Dec 9, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015121494882Stringer · damagedFRAME 64 - 65, STRINGER 36R, HAS OUT OF ROUND HOLES. R & R IAW SMR 51-42-11.Dec 9, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015121494881Stringer · damagedFRAME 64 - 65, STRINGER 37R, HAS OUT OF ROUND HOLES. REMOVED DAMAGED STRINGER 37R & SPLICE. FABRICATED REPLACEMENT STRINGER & SPLICE. LOCATED, DRILLED & DEBURRED REPLACEMENT PARTS. INSTALLED & RESTORED PROTECTIVE FINISH IAW SRM 51-42-11.Dec 9, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015121494880Stringer · damagedFRAME 66 - 67, STRINGER 38R, HAS OUT OF ROUND HOLES. REMOVED OLD STRINGER & INSTALLED NEW FABRICATED STRINGER. LOCATED, DRILLED & DEBURRED, PRIMED & TOP COATED IAW SRM 51-42-11.Dec 9, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015121494879Stringer · damagedFRAME 66 - 67.5, STRINGER 36R, HAS OUT OF ROUND HOLES. REMOVED OLD STRINGER & INSTALLED FABRICATED STRINGER IAW SRM 51-42-11. ALLOCATED, DRILLED & DEBURRED IAW SRM 51-44-11. TOP COATED TREATED & PRIMED IAW SRM 51-21-11.Dec 9, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015120894876Stringer Splice · corrodedCORROSION STRINGER 41R, FRAME 58 SPLICE. REMOVED CORRODED SPLICE FRAME 58. FABRICATED REPLACEMENT SPLICE. LOCATED, DRILLED & DEBURRED & INSTALLED SPLICE IAW SRM 51-42-11.Dec 7, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015120894875Stringer · corrodedUPON REMOVAL OF FLOOR PANELS IN AFT CARGO PIT FOR SKYDROL LEAK FOUND, CORROSION ON STRINGER 41RT, FRAME 58 - 60. REMOVED CORRODED STRINGER 41RT FROM FRAME 58 - 64, PROCURED REPLACEMENT STRINGER LOCATION, DRILLED & DEBURRED STRINGER & INSTALLED IAW SRM 51-42-Dec 7, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015120894874Stringer Splice · corrodedCORROSION ON STRINGER SPLICE IN AFT CARGO COMPARTMENT C64 FRAME & STRINGER 41R. REMOVED STRINGER 41R, FRAME 64 SPLICE. FABRICATED REPLACEMENT SPLICE & INSTALLED IAW SRM 51-42-11.Dec 7, 2015 · N458UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2015070794069Epsu · faultyFOUND THE EPSU BATTERY AFT LT FAULTED, INOPERATIVE WHILE PERFORMING THE EMER LIGHTS OPERATIONAL TEST FROM THE NR 2 SVC. R & R THE EPSU 13WL AS REQUIRED IAW AMM 33-5 1-38. OPERATIONS CHECKED GOOD.Jul 7, 2015 · N458UA · Airbus A320232 · Emergency LightingSDR CALA2015050793683Access Panel · unsecureLEFT FWD EMER EXIT DISPLAYED ON UPPER ECAM SCREEN. FOUND ACCESS PANEL TO LT OVERWING EXIT INSIDE PLANE FELL OFF. RE-INSTALLED PANEL LIGHT ON OVERWING EXIT WENT OUT.May 7, 2015 · N458UA · Airbus A320232 · Emergency LightingSDR CALA2014032490679Target · faultyDOOR 2R SLIDE ARMED, INTERMITTENT DURING FLIGHT. LOST SLIDE INDICATION ON ECAM DOOR OXY PAGE. REPLACED DOOR ARMED SENSOR TARGET IAW PTT 2992009.Mar 23, 2014 · N458UA · Airbus A320232 · Emergency EquipmentSDR CALA2014012490230Engine · shutdownNR 2 ENG ACCELERATED THRUST IDLE AT 60 PERCENT N 1 SHUT ENG DOWN.Jan 22, 2014 · N458UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2014010990112Hydraulic Line · leakingON ARRIVAL TO GATE FOUND HYD FLUID LEAKING FROM NR 2 ENG. REPLACED HYD LINE TO THE THRUST REVERSER SHUT OFF VLV, LEAK CHECKED OK.Jan 6, 2014 · N458UA · Airbus A320232 · Hydraulic System, MainSDR CALA2014010790055Apu · shutdownMX REPORTS APU AUTO SHUTDOWN AT GATE. LOCAL FBO AMT REPORTS APU AUTO SHUTDOWN. CYCLED CB'S L41 & L42 & RETRIED START. EGT REACHED 85 & RPM MAXIM AT 20%.Jan 3, 2014 · N458UA · Airbus A320232 · APU Core EngineSDR CALA2013120293343Doorbell · inoperativeDOORBELL TO FLIGHT DECK INOPERATIVE.Dec 1, 2013 · N458UA · Airbus A320232 · Communications SystemSDR CALA2013112593245Sealant · damagedAMBIENT NOISE LEVEL TOO HIGH APPEARS TO EMANATE FROM RT WINDSHIELD LOWER QUADRANT. FOR SEALANT IAW MT 56-005, PCN 841-0098. ACCOMPLISHED APPLICATION OF SEALANT IN AREA AS DESCRIBED IN SMC01 SEQ 5272007 FOR DETAILED CORRECTIVE ACTION.Nov 23, 2013 · N458UA · Airbus A320232 · Flight Compartment Windows
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