Airbus A320-233

Service difficulty reports · 254

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A320233'
  ORDER BY difficulty_date DESC"

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SDR 2003F00488Access Panel · delaminatedAT C-CHECK, FOUND RIGHT BELLY FAIRING ACCESS PANEL, 198GB, DELAMINATED STATION 2456. REPAIRED PANEL IAW SRM 51-77-12, PAR 3B, FIGURE 3. (M)May 16, 2003 · N951LF · Airbus A320233 · Aerodynamic FairingsSDR 2003F00487Skin · erodedAT C-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE WITH EROSION STATION 4869. REPAIRED VERTICAL STABILIZER IAW SRM 55-30-00, PATE 123. (M)May 16, 2003 · N951LF · Airbus A320233 · Vertical Stabilizer, Plate/SkinSDR 2003F00495Skin · crackedAT C-CHECK, FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE CRACKED AND SEVERAL DENTS. REPAIRED CRACK IAW SRM 55-14-11, FIGURE 205. DENTS WERE REPAIRED PER PER SRM 51-77-11, REV 61. (M)May 15, 2003 · N951LF · Airbus A320233 · Horizontal Stabilizer, Plate/SkinSDR 2003F00504Track · damagedAT C-CHECK, FOUND OUTBOARD FLAP RIGHT FAIRING TRACK 632CB, DAMAGED ON RIGHT SIDE STATION 3059. REPAIRED TRACK IAW SRM 51-77-12, PAGE 10, FIGURE 3. (M)May 15, 2003 · N951LF · Airbus A320233 · Trailing Edge FlapsSDR 2003F00494Bearing · wornAT C-CHECK, FOUND OUTBOARD FLAP, RIGHT FAIRING TRACK 632CB, WITH FREEPLAY AT STATION 3059. REPLACED BEARINGS OF STAY ASSEMBLY IAW PMS 01-05-27. (M)May 15, 2003 · N951LF · Airbus A320233 · Trailing Edge FlapsSDR 2003F00503Acoustic Panel · deterioratedAT C-CHECK, FOUND NR 2 ENGINE AIR INTAKE ACOUSTIC PANEL WITH DETERIOATION. REPAIRED ACOUSTIC PANEL IAW SRM V2500, 54-10-00, PAGE 100, SEC11. (M)May 15, 2003 · N951LF · Airbus A320233 · Engine Cowling SystemSDR 2003F00502Access Panel · delaminatedAT C-CHECK,F OUND LEADING EDGE ROOT WING 192DT ACCESS PANEL DELAMINATED. REPAIR PANEL IAW SRM 51-73-00, PAGES 1 AND 2. (M)May 15, 2003 · N951LF · Airbus A320233 · Wing, Plate/SkinSDR 2003F00501Duct · corrodedAT C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER C-DUCT, LEFT, WITH CORROSION ON UPSIDE. REPAIRED LEFT THRUST REVERSER IAW RE 2078006, REF CV03-0917-01. (M)May 15, 2003 · N951LF · Airbus A320233 · Engine Thrust ReverserSDR 2003F00500Duct · corrodedAT C-CHECK, FOUND NR 1 ENGINE THRUST REVERSER C-DUCT, RIGHT, WITH CORROSION ON UPSIDE. REPAIRED RIGHT THRUST REVERSER IAW ENGINEER REPORT 2078002, REF, CV03-0799. (M)May 15, 2003 · N951LF · Airbus A320233 · Engine Thrust ReverserSDR 2003F00499Duct · delaminatedAT C-CHECK, FOUND NR 2 ENGINE LEFT THRUST REVERSER COWLING, OUTER SKIN C-DUCT DELAMINATED. C-DUCT REPAIRED IAW SRM V2500 54-30-00, REPAIR NR 4. (M)May 15, 2003 · N951LF · Airbus A320233 · Engine Thrust ReverserSDR 2003F00498Acoustic Panel · dentedAT C-CHECK FOUND NR 1 ENGINE AIR INTAKE ACOUSTIC PANEL DENTED. REPAIRED ACOUSTIC PANEL IAW SRM 54-10-00, PAGE 110, SEC 11. (M)May 15, 2003 · N951LF · Airbus A320233 · Engine Cowling SystemSDR 2003F00497Cover · brokenAT C-CHECK, FOUND OUTBOARD FLAP, RIGHT FAIRING TRACK, 633AR, BROKEN COVER. REPLACED COVER IAW SRM 51-76-00. (M)May 15, 2003 · N951LF · Airbus A320233 · Trailing Edge FlapsSDR 2003F00492Cover · brokenAT C-CHECK, FOUND OUTBOARD FLAP, RIGHT FAIRING TRACK, 632R, BROKEN COVER. REPLACED COVER IAW SRM 51-76-00, REV 60. (M)May 15, 2003 · N951LF · Airbus A320233 · Trailing Edge FlapsSDR 2003F00496Track · dentedAT C-CHECK, FOUND LEFT WING FAIRING TRACK, 533CB INTERIOR, DENTED. REPAIRED FAIRING TRACK IAW SRM 51-77-12 PAGE 10, FIGURE 3. (M)May 15, 2003 · N951LF · Airbus A320233 · Trailing Edge FlapsSDR 2003F00491Liner · erodedAT C-CHECK FOUND NR 2 ENGINE AIR INTAKE ATTRITION LINING WITH EROSION. REPAIRED ATTRITION LINING IAW EM 72-32-85 PAGE 6, FIGURE 72-32-85-990-016. (M)May 15, 2003 · N951LF · Airbus A320233 · Turbine Engine Air Inlet SectionSDR 2003F00484Angle · brokenAT C-CHECK, FOUND BROKEN ANGLE BEHIND SLAT NR 3 STOP, LEADING EDGE LEFT WING. REPAIRED ANGLE IAW SRM 51-20-00. (M)May 15, 2003 · N951LF · Airbus A320233 · Wing Miscellaneous StructureSDR 2003F00483Cowling · puncturedAT C-CHECK FOUND NR 2 ENGINE INTAKE UP WITH TWO PUNCTURES AT THE 7 AND 2 O'CLOCK POSITIONS. REPAIRED AIR INTAKE COWL IAW EM 71-11-11-300-015. (M)May 15, 2003 · N951LF · Airbus A320233 · Engine Cowling SystemSDR 2003F00478Duct · delaminatedAT C-CHECK, FOUND NR 2 ENGINE RIGHT THRUST REVERSER COWLING OUTER SIDING C-DUCT DELAMINATED. REPAIRED DAMAGE IAW SRM V2500, PAGE 201-206, FIGURE 201. (M)May 15, 2003 · N951LF · Airbus A320233 · Engine Thrust ReverserSDR 2003F00477Skin · dentedAT C-CHECK, FOUND DENT ON REAR CONE SKIN FS 82, STATION 38035. REPAIRED DENT IAW SRM 53-51-11 FIGURE 203 PAGE 217-218. (M)May 15, 2003 · N951LF · Airbus A320233 · Aerodynamic FairingsSDR 2003F00423Window · crackedDURING DESCENT, THE PILOTS REPORT THAT L3 WINDOW WAS CRACK DURING DESCENT PROCEDURE. THE AIRCRAFT LANDED WITHOUT INCIDENT. AT BZE STATION WINDOW-MIXED CHECK WAS PERFORMED ACCORDING TO AMM 56-11-22 AND FOUND IT WITHIN LIMITS. AT THE SAME TIME PRESSURIZATION WApr 13, 2003 · N483TA · Airbus A320233 · Flight Compartment WindowsSDR 2004F00253Transducer · inoperativeSJO - FLT 640 - DURING CLIMB, THE CAPTAIN REPORTED THAT NR 2 ENGINE HYD PUMP FAILED. THE AIRCRAFT RETURNED TO SJO STATION. AT SJO, NR 2 ENGINE HYDRAULIC PUMP WAS REMOVED AND REPLACED IAW AMM 29-13-31, BUT IT WAS FOUND THE HYDRAULIC PRESSURE TRANSDUCER INOPERMar 1, 2003 · N462TA · Airbus A320233 · Hydraulic Pressure SensorSDR 2002F00925Sense Line · looseSAL - FLT TA315 - DURING CLIMB, THE CAPTAIN REPORTED LOW OIL PRESS INDICATION FROM ENGINE NR 2. THE AIRCRAFT RETURNED TO EL SALVADOR STATION FOR MAINTENANCE. AFTER LANDING, MAINTENANCE PERSONNEL PERFORMED AMM 79-31-00-810-816 OIL LEAK CHECK, AND FOUND A LEAKSep 26, 2002 · N981LR · Airbus A320233 · Engine Oil PressureSDR 2002F00913Engine · bird ingestionSAP - DURING LANDING, ENGINE NR 2 EXPERIENCED A BIRD STRIKE. AFTER LANDING MAINTENANCE PERSONNEL PERFORMED INSPECTION OF THE ENGINE NR 2. AT THE MOMENT, AIRCRAFT REMAINS ON GROUND AT SAP STATION FOR INSPECTION AND MAINTENANCE. (M)Aug 29, 2002 · N462TA · Airbus A320233 · Engine (Turbine/Turboprop)SDR 2002F00800Relief Valve · damagedJFK - FLT 580 - DURING CLIMB, AN IN FLIGHT FUEL TRANSFER WAS EXPERIENCED FROM RIGHT TANK TO THE CENTER TANK. AIRCRAFT RETURNED TO JFK STATION FOR MAINTENANCE. AT JFK STATION, TECHNICIANS PERFORMED INSPECTION AND FOUND THE OVERPRESSURE PROTECTOR 96 QM DAMAGEDMay 20, 2002 · N484TA · Airbus A320233 · Fuel StorageSDR 2002F00493Valve · damagedFLT GU970 - SJO-GUA - DURING CRUISE, AN IN FILGHT FUEL TRANSFER WAS EXPERIENCED FROM RIGHT TANK TO THE LEFT, AND CENTER TANK. AIRCRAFT DIVERTED ITS FLIGHT TO EL SALVADOR STATION FOR MAINTENANCE. AFTER LANDING, TECHNICIANS PERFORMED INSPECTION TO THE LEFT WINMay 5, 2002 · N483TA · Airbus A320233 · Fuel StorageSDR 2002F00364Manifold · leakingAT THE ARRIVAL OF FLT 221, FLIGHT CREW REPORTED THE YELLOW RESERVOIR LOW LEVEL. ON GROUND TECHNICIANS FOUND A LEAK AT THE PTU MANIFOLD. THE PTU MANIFOLD WAS REPLACED AS PER AIRCRAFT MM 29-13-15 AND OPERATIONAL TEST WAS PERFORMED IAW AIRCRAFT MM 29-23-00. REMar 21, 2002 · N454TA · Airbus A320233 · Hydraulic System, MainSDR 2002F00341Disk · brokenSJO - FLT 660 - DURING THE FLIGHT, THE CAPTAIN REPORTED FUEL IMBALANCE INDICATION, THE AIRCRAFT RETURNED TO SJO STATION FOR MAINTENANCE. AFTER LANDING, MAINTENANCE PERSONNEL PERFORMED OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-11, AND DISCREPANCIES WERE NOT Mar 8, 2002 · N481TA · Airbus A320233 · Fuel StorageSDR 2002F00239Gasket · missingFLT TPU020 - UOI/GYE - DURING CLIMB, CABIN PERSONNEL DETECTED A NOISE AT THE PAX CABIN, NEAR THE EMERGNCY OVERWING EXIT DOORS. THE AIRCRAFT CONTINUE ITS FLIGHT TO GYE STATION. AFTER LANDING AT GYE STATION, TECHNICIANS PERFORMED INSPECTION OF THE AIRCRAFT, ANFeb 24, 2002 · N463TA · Airbus A320233 · Aerodynamic FairingsSDR 2002F00042Fmu · malfunctionedSJO - FLT 660 - DURING TAKEOFF CLIMB, ENGINE NR 2 HAVE EGT OVERLIMIT BEFORE 1,000 FEET, THIS CONDITION WAS FOR 13 SECONDS EGT PARAMETER WAS 639'C AND N2 98.2 PERCENT. PERFORMED TROUBLESHOOTING IAW AMM 77-00-810, INSPECTED ENGINE INLET AND EXHAUST, FOUND NO DAJan 6, 2002 · N464TA · Airbus A320233 · Fuel Controlling SystemSDR 2001F00472Fan · malfunctionedGUA - FLT 581 - DURING CRUISE, MESSAGE ON ECAM PAGE SHOWN VENT BLOWER FAULT/EXTRACT FAN FAULT, VENT SKIN VALVE FAULT ECAM ACTION WAS PERFORMED AND THE AIRCRAFT RETURNED TO GUA STATION FOR INSPECTION. AFTER LANDING, THE EXTRACT FAN MESSAGE ON ECAM WAS ENTERED Oct 4, 2001 · N462TA · Airbus A320233 · Air Distribution FanSDR AWXA0002212Pump · leakingPHX - AIR TURNBACK - FLT 536 - ABOUT 10 MIN AFTER DEPARTURE FROM PHX EN ROUTE TO CLE THE BLUE HYD SYS PRESS AND QUANTITY DROPPED TO ZERO AND ASSOCIATED WARNING INDICATIONS WERE DISPLAYED. THE AIRCRAFT RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCESep 4, 2001 · N825AW · Airbus A320233 · Hydraulic Pump (Electric/Engine), MainSDR 2001F00230Pressure Switch · failedSAL - FLT 390 - DURING CLIMB, THE CAPTAIN REPORTED AIR ENGINE 1 BLEED ABNORMAL PRESSURE, AIR ENGINE 1 BLEED FAULT AND HYD GREEN ENG 1 PUMP LOW PRESSURE. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING, MAINTENANCE TECHNICIAN PERFORMED FAULTAug 16, 2001 · N941LF · Airbus A320233 · Hydraulic Pressure SensorSDR 2001F00229Harness · damagedSAL - FLT 390 - DURING CLIMB, THE CAPTAIN REPORTED AIR ENGINE 1 BLEED ABNORMAL PRESSURE, AIR ENGINE 1 BLEED FAULT AND HYD GREEN ENG 1 PUMP LOW PRESSURE. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING, MAINT TECH PERFORMED FAULT ANALYSIS, Aug 16, 2001 · N941LF · Airbus A320233 · Bleed Air Indicating SystemSDR 2001F00231Pump · failedSAL - FLT 390 - DURING CLIMB, THE CAPTAIN REPORTED AIR ENG 1 BLEED ABNORMAL PRESSURE, AIR ENG 1 BLEED FAULT AND HYD GREEN ENG 1 PUMP LOW PRESSURE. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING, MAINTENANCE TECHNICIAN PERFORMED FAULT ANAAug 15, 2001 · N941LF · Airbus A320233 · Hydraulic Pump (Electric/Engine), MainSDR 2001F00073Indicator · failedLIM - FLT 641 - DURING FLIGHT, WHILE AIRCRAFT TURNED, STANDBY HORIZON TILTED 22 DEGREES RIGHT BANK. AFTER TURN, THE INDICATOR DID NOT RECOVER, IT REMAINED IN THAT POSITION, AND NO FLAG APPEARED. AIRCRAFT RETURNED TO LIMA AIRPORT. AFTER LANDING, MAINTENANCE Jun 16, 2001 · N951LR · Airbus A320233 · Attitude Gyro and Indicating SystemSDR 20010213CW012Brake · malfunctionedDURING LANDING OF FLIGHTAT HONDURAS AIRPORT, CREW REPORTED AT SPEED OF 80 KNOTS, THE BRAKING BECAME VERY POOR, DUE TO THIS SITUATION, HIGH SPEED EXIT OF RUNWAY WAS PERFORMED, BUT LEFT MAIN LANDING GEAR GOT STUCK OUTSIDE OF TAXIWAY. NOTE: FIRST REVENUE FLIGHT Feb 3, 2001 · N465TA · Airbus A320233 · Landing Gear Brake SystemSDR 20010111CW003Bearing · failedDURING FLT, OIL QNTY IND BEGAN TO DROP, ENG NR2 . LOW OIL QNTY LEVEL WARN ON ECAN MON. ENGINE SHUT DWN. AC DIVERTED, MAIN TECH CKD, NR5 BRG TO BE CHANGED. BRG CHGD, ENG RUN UP, CK OK, AC RETURNED TO NORMAL OPERATION.Dec 19, 2000 · N453TA · Airbus A320233 · Turbine Engine Compressor SectionSDR 20001227SH019Control Unit · smokePTY - FLT 622 - DURING CRUISE, COCKPIT CREW OBSERVED SMOKE COMING FROM THE FLIGHT CONTROL UNIT. AIRCRAFT RETURNED TO PANAMA STATION FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING AT PTY STATION, MAINTENANCE TECHS PERFORMED AN INSPECTION OF THE FCU SYSTEM, THE Dec 19, 2000 · N461TA · Airbus A320233 · Auto Flight SystemSDR 20001227SH018Engine · leakingBZE - FLT 573 - DURING CRUISE, ENGINE NR 2 OIL QUANTITY INDICATOR BEGAN TO DROP DOWN. A LOW OIL QUANTITY LEVEL WARNING WAS SHOWN ON THE ECAM MONITOR. ENGINE WAS SHUT DOWN. AIRCRAFT DIVERTED ITS NORMAL FLIGHT TO BELIZE STATION FOR MAINTENANCE. AFTER AN UNEVDec 19, 2000 · N453TA · Airbus A320233 · Turbine Engine Oil SystemSDR 20001227SH021Shutoff Valve · damagedHAV - FLT 622 - DURING CRUISE, AIRCRAFT LOST THE GREEN HYDRAULIC SYTEM QUANTITY, FLIGHT CREW PERFORMED ABNORMAL PROCEDURES FOR GREEN HYDRAULIC SYSTEM LOSS. THE AIRCRAFT RETURNED TO LA HAVANA, CUBA, FOR MAINTENANCE. AT LA HAVANA STATION, MAINTENANCE TECHS FOUDec 15, 2000 · N461TA · Airbus A320233 · Engine Thrust ReverserSDR 20010112SG007Structure · bird strikeSAL-TGU-SAP-MIA- FLT 390 - DURING THE APPROACH, A BIRD IMPACTED THE SLAT NR 4 ON THE LEFT WING. MAINTENANCE TECHS REMOVED AND REPLACED SLAT NR 4 DUE TO DAMAGE TO THE LIMITS. OPERATIONAL TESTED AS PER AMM 27-84-66. THE AIRCRAFT RETURNED TO NORMAL OPERATION. Nov 7, 2000 · N451TA · Airbus A320233 · Leading Edge DevicesSDR 20001113SH016Structure · damagedIAD/SAL - FLT 581 - AT THE GATE, PREVIOUS TO FLIGHT, A TRACTOR HIT THE ENGINE NR 1. A HOLE OF 6 INCHES BY 3 INCHES WAS DONE ON THE FAN COWL AND A HOLE OF 2 INCHES BY 1 INCH WAS DONE ON THE INBOARD FAN COWL. THE AIRCRAFT REMAINED ON GROUND AT IAD STATION FOR Oct 6, 2000 · N458TA · Airbus A320233 · Nacelle/Pylon, Main FrameSDR 20000908SH014Structure · damagedJFK/SJO - FLT LR661 - DURING DEPARTURE - AIRCRAFT WAS PARKED AT THE DELTA TERMINAL NR 2, GATE 27. WHILE THE TRACTOR DRIVER WAS POSITIONING TO PUSH-BACK, HE HIT THE TOW BAR AND IT BOUNCED INTO THE AIRCRAFT CAUSING A 3.5 INCH HOLE ON THE BOTTOM LEFT HAND SIDE OJun 20, 2000 · N941LF · Airbus A320233 · Fuselage Main, StructureSDR 20001004AP004Skin · damagedJFK - FLT 661 - DURING DEPARTURE OF THE FLIGHT LR661 (JFK-SJO), THE AIRCRAFT WAS PARKED AT THE DELTA TERMINAL NR 2, GATE 27, WHILE THE TRACTOR DRIVER WAS POSITIONING TO PUSH-BACK HE HIT THE TOW BAR AND IT BOUNCED INTO THE AIRCRAFT, CAUSING A 3.5 INCH HOLE ON TJun 20, 2000 · N941LF · Airbus A320233 · Fuselage Main, Plate/SkinSDR 20000908SH016Strut · dischargedSJO/UIO - FLT TA661 - THE LANDING GEAR SHOCK ABSORBER FAULT AND L/G LGCIU NR 1 FAULT ECAM WARNING MESSAGES APPEARED ON THE ECAM, AIRCRAFT RETURNED TO SAN JOSE STATION FOR MAINTENANCE. AFTER AN UNEVENTFUL LANDING, MAINT TECHS PERFORMED SERVICING OF THE NOSE LAJun 3, 2000 · N991LR · Airbus A320233 · Nose/Tail Landing Gear Strut/AxleSDR 20000703AP009Pressure Switch · looseJFK-SAL - FLT 571 - THE AIRCRAFT LOST THE GREEN HYDRAULIC SYSTEMS QUANTITY, FLIGHT CREW PERFORMED ABNORMAL PROCEDURES FOR GREEN HYDRAULIC SYSTEM LOSS. THE AIRCAFT PERFORMED AN UNEVENTFUL LANDING AT EL SALVADOR STATION. AT EL SALVADOR STATION MAINTENANCE TECHMay 22, 2000 · N460TA · Airbus A320233 · Hydraulic System, MainSDR 20000908SH015Strut · damagedSJO/CCS/SJO - FLT LR610 - DURING TAKEOFF, GROUND CREW OBSERVED SEPARATION OF THE WHEEL NR 1 THREAD RECAP. AIRCRAFT WAS CONTACTED BY SJO GROUND MAINTENANCE AND ADVISED TO RETURN TO SAN JOSE STATION FOR MAINT. AFTER UNEVENTFUL LANDING, MAINT TECHS INSPECTED THMay 3, 2000 · N240TA · Airbus A320233 · Nose/Tail Landing Gear Strut/AxleSDR 20000420AP001Cowling · damagedJFK - FLT 570 - DURING TAXIING GATE, ENG NR 2 INTAKE COWL BARREL AND RT ENG FAN COWL RE HIT BY A BELT LOADER. STAYED AT JFK FOR MX. PERFORMED INSPECTION THE FOLLOWING DAMAGE WAS FOUND: TWO CRACKS ON THE EXTERIOR LOWER SKIN OF THE ENG INTAKE COWL BARREL, AFT Apr 3, 2000 · N459TA · Airbus A320233 · Engine Cowling SystemSDR 20000420AP009Pump · failedSJO - FLT 641 - DURING CLIMB, 30 MINUTES AFTER TAKEOFF, GREEN ENGINE NR 1 PUMP FAULT AND OVERWEIGHT LANDING PROCEDURE ACCOMPLISHED AS PER QRH 221. THE AIRCRAFT RETURN TO SJO STATION AND LANDING WAS SUCCESSFULLY. AIRCRAFT IS ON GROUND SUBJECT TO INVESTIGATIONFeb 17, 2000 · N460TA · Airbus A320233 · Hydraulic Pump (Electric/Engine), MainSDR 20000420AP005Intake Duct · damagedSAL - FLT 390 - DURING TAKEOFF (SAL-TGU-SAP-MIA) A LARGE BIRD IMPACTED THE ENGINE NR 1, HOWEVER THE ENGINE PARAMETERS REMAINED NORMAL, DUE TO THIS SITUATION THE AIRCRAFT RETURNED TO EL SALVADOR STATION FOR MAINTENANCE. AT EL SALVADOR, MAINTENANCE TECHNICANS PDec 16, 1999 · N460TA · Airbus A320233 · Engine Cowling System
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