Airbus A320-233

Service difficulty reports · 254

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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 aircraft_model_key = 'A320233'
  ORDER BY difficulty_date DESC"

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SDR 2004F00419Control Unit · malfunctionedDURING CLIMB, AFTER FLAPS RETRACTION A/C DID NOT ACCELERATE MORE THAN 235 KNOTS. BOTH PFDS AND STANDBY AIRSPEED SHOWED THE SAME MESSAGE. AIRCRAFT RETURNED TO SAL FOR MAINTENANCE. AFTER LANDNG, THE WIRING ON THE VMO/MMO SWITCH WAS CHECKED AND TROUBLESHOOTINGSep 12, 2004 · N482TA · Airbus A320233 · Landing Gear Retraction/Extension SystemSDR 2004F00321Fan · stuckDURING CRUISE, VIBRATION UNDER CABIN FLOOR TO AFT GALLEY AREA, & BURNED ODOR AROUND COCKPIT & FORWARD GALLEY AREA FELT. AS PREVENTATIVE ACTION CREW OXYGEN USED. ECAM MESSAGE OF VENT BLOWER FAULT CAME ON. A/C DEVIATED FROM ITS NORMAL SCHEDULE FLT TO CUL. AFAug 17, 2004 · N486TA · Airbus A320233 · Air Distribution FanSDR TL9R200400002Brake · bindingTHE A320 NR 1 BRAKE WAS REMOVED AS WORN TO LIMITS. THERE WERE NO OPERATIONAL PROBLEMS OR UNUSUAL INDICATIONS LEADING UP TO THE REMOVAL. WHILE ATTEMPTING TO REMOVE THE NR 1 MAIN WHEEL TO FACILITATE REMOVAL OF THE BRAKE, IT WOULD NOT COME OFF AS THE BRAKE WAS JJul 24, 2004 · Airbus A320233 · BrakeSDR 2004F00318Inlet · departedAFTER TAKEOFF, NR 1 ENGINE INBOARD AND OUTBOARD FAN COWL DEPARTED AIRCRAFT. A SHUTTER WAS FELT BY THE AIRCREW AND THE NR 1 ENGINE INSTRUMENT LIGHTS FLASHED AMBER AND THEN WENT TO NORMAL. THE NR 1 ENGINE OIL QUANTITY LIGHT REMAINED AMBER. AN EMERGENCY WAS DECJul 13, 2004 · N951LF · Airbus A320233 · Engine Air Intake SystemSDR 2004F00177Skin · delaminatedDURING GROUND INSPECTION, FOUND PANEL 191DT DAMAGED, WITH MATERIAL LOST AND DELAMINATED. AIRCRAFT REMAINS AT MIA STATION FOR REPAIR. (M)Jun 20, 2004 · N463TA · Airbus A320233 · Fuselage Main, Plate/SkinSDR 2004F00176Warning Light · false activationDURING CLIMB, AN ECAM MESSAGE OF DOOR AVIONIC OPEN CAME ON. CREW DIVERTED THE FLIGHT TO SAP STATION FOR MAINTENANCE. AFTER LANDING, INSPECTION OF THE AVIONICS DOOR WAS PERFORMED, WHICH IT WAS FOUND CLOSED. THE ECAM MESSAGE OF THE DOOR OPEN INDICATION WAS ENJun 20, 2004 · N470TA · Airbus A320233 · Door Warning SystemSDR 2004F00175Panel · delaminatedMIA-SJO - DURING GROUND INSPECTION OF FLIGHT LR627, IT WAS FOUND PANEL 191DT DAMAGED, WITH MATERIAL LOST AND DELAMINATED. AT MIA STATION, REPLACEMENT OF THE PANEL 191DT WAS PERFORMED, PER AMM 53-35-11. AIRCRAFT RETURNED TO NORMAL OPERATION. (M)Jun 20, 2004 · N463TA · Airbus A320233 · Fuselage Main, Plate/SkinSDR 2004F00178Proximity Sensor · malfunctionedDURING CLIMB, NLG REMAINED UNLOCKED & A/C RETURNED TO STATION FOR MX. AFTER LANDING, INSPECTION OF NLG PERFORMED PER AMM, & REMOVED TWO NLG PROXIMITY SENSORS PER AMM. PERFORMED BITE TEST PER AMM, & FOUND NORMAL. A VERIFICATION OF NLG HINGE BEARING CLEARANCEJun 19, 2004 · N451TA · Airbus A320233 · Landing Gear Position and WarningSDR SOKF2341AAElement · contaminatedDURING TAKEOFF RUN, ENGINE NR 2 DID NOT SPOOL UP BEFORE 80 KNOTS. AIRCRAFT RETURNED TO GATE. TECHS PERFORMED ANALYSIS IAW TSM AND AMM., REPLACED MAIN ELEMENT OF FUEL FILTER IAW AMM 73-1242, INSPECTED VSV MECHANISM IAW 73-32-42. CLEANED P 4.9, P2/T2 TUBES SYJun 10, 2004 · N482TA · Airbus A320233 · Aircraft Fuel Filter/StrainerSDR 2004F00269Fmu · erraticDURING TAKEOFF, AN ECAM WARNING MESSAGE, ENGINE NR 2 OVERSPEED PROTECTION FAULT CAME ON, AT LOW SPEED. WHEN MOVING TRUST LEVERS TO FLX MCT POSITION ENGINE NR 1 RESPONDED NORMAL, WHILE ENGINE NR 2 REMAINED AT LOW POWER. THE PLANE YAW TO THE RT AND THE TAKEOFFMay 24, 2004 · N991LR · Airbus A320233 · Fuel Controlling SystemSDR 2004F00185Structure · vibrationDURING CRUISE, AIRCRAFT DIVERTED TO MIAMI, DUE PILOT REPORTED MODERATED STRUCTURAL VIBRATION. THE AIRCRAFT LANDED WITHOUT ANY OTHER DISCREPANCY, AND STILL ON GROUND FOR MAINTENANCE. (M)May 11, 2004 · N477TA · Airbus A320233 · Fuselage Main, StructureSDR 2004F00312Computer · failedSJO - FLT 631 - DURING CLIMB, ANTI-ICE ON NR 1 CAPTAIN PITOT PROBE WENT INOPERATIVE, AND AIRCRAFT RETURNED TO SAN JOSE. AT SJO, TECHS PERFORMED ANALYSIS PER AMM AND FOUND UNSERVICEABLE THE NR 1 PHC. NR 1 PHC WAS REPLACED PER AMM 30-31-34, AND AS PREVENTATIVEMay 4, 2004 · N483TA · Airbus A320233 · Pitot/Static Anti-Ice SystemSDR 2004F00183Warning Light · false indicationDURING CRUISE FLIGHT WHILE FLYING THROUGH MODERATE RAIN, THERE WAS AN AOA DISCREPANCY. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO DFW. AIRCRAFT LANDED IN DFW WITHOUT INCIDENT. INSPECTED AOA VANES AND TESTED AUTOMATIC FLIGHT SYSTEM AFS. RAN BITE CHECKS OF Apr 13, 2004 · N941LF · Airbus A320233 · Stall Warning SystemSDR 2004F00221Windshield · bird strikeDURING CLIMB, A BIRD STRUCK THE LEFT WINDSHIELD, CRACKING THE OUTER PLY OF THE WINDSHIELD. THE AIRCRAFT DIVERTED ITS NORMAL FLIGHT TO EL SALVADOR STATION. AFTER LANDING AT SAL STATION, TECHNICIANS PERFORMED INSPECTION DUE BIRD STRIKE PER AMM 05-51-14. THE LApr 6, 2004 · N981LR · Airbus A320233 · Flight Compartment WindowsSDR 2004F00198Computer · malfunctionedSAL-TGU-SAP - FLT TA390 - DURING CLIMB, MULTIPLE ECAM WARNING MESSAGES ON SCREEN CAME ON, CABIN PRESSURE, LANDING ELEVATION, NAV ILS R FAULT, AUTO FLT, NAV GPWS, UNABLE CAPTAIN SIDE TO SELECT VOR ON RMP NR 1 AND THEN ON NR 2 ALSO ND NR 1 INOP, FIRST OFFICER ANMar 30, 2004 · N991LR · Airbus A320233 · Flight Management Computing Hardware SystemSDR 2004F00164Computer · malfunctionedSJO - FLT 641 - DURING APPROACH DUAL FMGC MESSAGE CAME ON, DUE TO THIS CONDITION AIRCRAFT RETURNED TO SAN JOSE AIRPORT. ON GROUND MAINTENANCE, RESET BOTH FMGC SYSTEMS PER AMM 22-83-00, AND FOUND NORMAL, THEM RETURNED THE AIRCRAFT TO SERVICE. (M)Mar 26, 2004 · N486TA · Airbus A320233 · Autopilot SystemSDR RYNA54233Transducer · faultyDURING CRUISE FLIGHT, ECAM DISPLAYED (LEFT WING AIR LEAK) MESSAGE. PERFORMED ECAM ACTION. RETURNED, AS A HEAVY WEIGHT LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE BLEED PRESSURE TRANSDUCER.Mar 3, 2004 · N941LF · Airbus A320233 · Bleed Air Indicating SystemSDR 2004F00162Fitting · leakingCREW REPORTED HYD G+Y LOW PRESSURE. A/C RETURNED TO STATION FOR INSP. A/C LANDED WITHOUT INCIDENT. MAINT TECHS VERIFIED HYD SYS & PERFORMED INSP ON AFT BLKHD AREA PER AMM & FOUND LEAD SOURCE ON YELLOW SYS FITTING AT REAR BULKHEAD, PART CRACKED. ELBOW FITTIFeb 13, 2004 · N453TA · Airbus A320233 · Hydraulic System, MainSDR 2004F00289Transducer · malfunctionedFLT LR622 - DURING CRUISE, BOTH ENGINES BLEED SYSTEMS FAULT ECAM WARNING CAME ON. BOTH BLEED SYSTEMS WENT TO CLOSED POSITION AND THE AIRCRAFT RETURNED TO SAL STATION. AFTER LANDING, INSPECTION WAS PERFORMED TO THE BLEED SYSTEM AND REPLACED ENGINE NR 1 TRANSDJan 23, 2004 · N462TA · Airbus A320233 · Pneumatic Distribution SystemSDR 2004F00211Packing · leakingSAP - FLT TAI390, DURING GROUND INSPECTION, FOUND A HYDRAULIC LEAK IN THE RIGHT WHEEL WELL. TECHS PERFORMED AN INSPECTION OF THE WHEEL WELL AREA AND FOUND THAT THE LEAK SOURCE WAS ON A FITTING ON THE AUTOMATIC BRAKE SELECTOR VALVE AND TWO SEALS WERE REPLACED Jan 18, 2004 · N451TA · Airbus A320233 · Hydraulic System, MainSDR 2004F00315Pump · failedDURING CRUISE, ECAM WARNING MESSAGE HYDRAULIC YELLOW ENGINE NR 2 PUMP LOW PRESS SHOWED ON SCREEN. THE AIRCRAFT RETURNED TO SAL STATION. AFTER LANDING AT SAL, TECHNICIANS VERIFIED ENGINE HYDRAULIC PUMP PRESSURE PER AMM 29-13-00. A FALSE INDICATION WAS DETECTJan 16, 2004 · N453TA · Airbus A320233 · Hydraulic Pump (Electric/Engine), MainSDR 2004F00213Rod End · looseBZE - FLT 410 - DURING CLIMB FLIGHT, EXPERIENCED A STRONG VIBRATION IN ALL PHASES OF FLIGHT ABOVE 300 KNOTS. THE AIRCRAFT WAS RETURNED TO SAL STATION FOR MX. AT EL SALVADOR STATION, THE ELEVATORS FREE PLAY WERE INSPECTED PER AMM 27-34-00, AND FOUND A PLAY ONDec 21, 2003 · N981LR · Airbus A320233 · Elevator Control SystemSDR 2004F00210Structure · vibrationDURING CLIMB, IT WAS EXPERIENCED A STRONG VIBRATION IN ALL PHASES OF FLIGHT ABOVE 300 KNOTS. THE AIRCRAFT WAS DEVIATED FROM ITS NORMAL FLIGHT SCHEDULE TO SAL STATION FOR MAINTENANCE. THE AIRCRAFT REMAINS ON GROUND AT SAL STATION FOR MAINTENANCE. (M)Dec 21, 2003 · N981LR · Airbus A320233 · Aircraft StructuresSDR 2004F00003Engine · fireDURING ENGINE NR 2 TESTS AFTER THE ENGINE FIRE, IAW NORMAL PROCEDURE BOTH ENGINE FIRE EXTINGUISHING BOTTLES WERE USED AND SOME OTHER CHEMICAL EXTINGUISHERS WERE USED ON ENGINE NR 2. THE ENGINE WAS REPLACED AND SENT TO A REPAIR STATION FOR REPAIRS. ENGINE WASDec 1, 2003 · N455TA · Airbus A320233 · Engine (Turbine/Turboprop)SDR 2004F00363Control Panel · inoperativeFLT TA525 - SAL-DFW, DURING CLIMB, CAPTAIN AUDIO CONTROL PANEL WENT INOPERATIVE, AFFECTING AUDIO PLUS SELECTION OF THE SYSTEM. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENANCE. AFTER LANDING, PERSONNEL REPLACED AND TESTED OF THE ACP PANEL NR 1 PER AMM 23Nov 22, 2003 · N981LR · Airbus A320233 · Communications SystemSDR 2004F00025Compressor · stalledHAV - FLT 130 - DURING TAKEOFF FLIGHT CU130, HAV-MEX, AN ENGINE STALL OCCURRED ON ENGINE NR 2. TAKEOFF PROCEDURE WAS ABORTED, AIRCRAFT RETURNED TO GATE. AT THE PRESENT AIRCRAFT REMAINS ON GROUND FOR MAINTENANCE. (M)Nov 13, 2003 · Airbus A320233 · Engine (Turbine/Turboprop)SDR RYN2004F00011Floor Support · corrodedAT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 34 ABOVE STRINGER 34 IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 34 JUST ABOVE 34L IN FORWARD CARGO COMPARTMENT.Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR RYN2004F00005Floor Support · corrodedAT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 31 TO 34 AT STRINGER 34L IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT FROM FRAME 31 TO 34, STRINGER 34L IN FORWARD PIT.Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR RYN2004F00004Floor Support · corrodedA (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 28 TO 31 AT STRINGER 34R.Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR RYN2004F00003Floor Support · corrodedAT (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT FROM FRAME 31 TO 33 AT STRINGER 34R IN FORWARD CARGO COMPARTMENT. FABRICATED NEW FLOORBOARD SUPPORT. TREATED, PRIMED, TOP COATED AND INSTALLED FLOORBOARD SUPPORT FROM FRAME 31 TO 33 AT STRINGER 34R.Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR RYN2004F00002Floor Support · corrodedA (C) CHECK, FOUND CORROSION ON FLOORBOARD SUPPORT AT FRAME 34 AND STRINGERS 34R TO 34L IN FORWARD CARGO COMPARTMENT. REMOVED AND REPLACED FLOORBOARD SUPPORT AT FRAME 34 FROM STRINGER 34R TO 34L IN FORWARD PIT.Oct 19, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00262Warning Light · illuminatedDURING TAKEOFF, THE LANDING GEAR DOOR NOT CLOSED INDICATION WAS SHOWN AND THE LANDING GEAR UPLOCK SYSTEM OF THE NOSE LANDING GEAR SYSTEM HAD AN INCORRECT INDICATION OF THEIR POSITION IN THE COCKPIT INSTRUMENTS. THE AIRCRAFT RETURNED TO SAL STATION FOR MAINTENOct 14, 2003 · N457TA · Airbus A320233 · Landing Gear Position and WarningSDR 2004F00242Intercostal · corrodedAT C-CHECK, OFUND AFT CARGO COMPARTMENT FLOOR INTERCOSTAL CORRODED AT FRAME 54 AND RBL 17. REMOVED CORROSION FROM INTERCOSTAL AT FRAME 54, RBL 17. NO MEASUREABLE MATERIAL LOSS. TREATED, PRIMED AND APPLIED TOPCOAT. (M)Oct 2, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00383Intercostal · corrodedAT C-CHECK, OFUND AFT CARGO FLOOR INTERCOSTAL IS CORRODED AT FRAME 56 AND RBL 22-24. REMOVED CORROSION FROM INTERCOSAL AT FRAME 56, RBL 22-24. NO MEASUREABLE MATERIAL LOSS. TREATED, PRIMED AND APPLIED TOPCOAT. (M)Oct 2, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00181Intercostal · corrodedAT C-CHECK, FOUNDINTERCOSTAL AT FORWARD CARGO COMPARTMENT BETWEEN FRAME 51 AND 52 RBL 27 HAS SURFACE CORROSION. REMOVED AND REPLACED INTERCOSTAL AT AFT CARGO COMPARTMENT BETWEEN FRAME 51 AND FRAME 52, RBL 27. (M)Oct 2, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00094Floorboard · puncturedAT C-CHECK, FOUND AFT CABIN FLOORBOARD NR 261DF HAS MULTIPLE PUNCTURES. REPAIRED AFT CABIN FLOORBOARD PANEL NR 261DF. (M)Oct 2, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR 2004F00089Floor Support · corrodedAT C-CHECK, FOUND AFT CABIN FLOOR SUPPORT HAS CORROSION AT STATION 3850 AND RBL 32. REMOVED LIGHT CORROSION AT NUT PLATE AT STATION 3850 AND RBL 32. FOUND TO BE WITHIN LIMITS. TREATED, PRIMED AND TOPCOAT APPLIED. (M)Oct 2, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00228Intercostal · corrodedAT C-CHECK, FOUND INTERCOSTAL LOCATED BETWEEN FRAME 50 AND 51 RBL 27 AT AFT CARGO COMPARTMENT IS CORRODED AT FORWARD END. (M)Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00091Mount · damagedAT C-CHECK, FOUND NR 1 ENGINE FORWARD MOUNT STOP SERIAL NR 0313-PTE HAS GOUGING IN BOLT HOLES. CLEANED NR 1 ENGINE FORWARD MOUNT STOP, S/N 0313. NO GOUGING NOTED. DIMENSIONS CHECKED AND FOUND TO BE WITHIN LIMITS. (M)Sep 26, 2003 · N951LF · Airbus A320233 · Engine Mount SectionSDR 2004F00068Plate · corrodedAT C-CHECK, FOUND INTERCOSTAL AT AFT CARGO COMPARTMENT FRAME 48 TO 49, LBL 27 WITH SURFACE CORROSION. REMOVED AND REPLACED INTERCOSTAL PLATE AT AFT CARGO COMPARTMENT, FRAME 48 TO FRAME 49, LBL 27. (M)Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00067Crossbeam · damagedAT C-CHECK, FOUND NR 1 ENGINE FORWARD MOUNT CROSSBEAM HAS NICKS, SCRATCHES, AND GOUGING. INSPECTED AND CLEANED DAMAGED AREA. REPAIRED NR 1 ENGINE FORWARD MOUNT CROSSBEAM BY REMOVING AND REPLACING BUSHING. (M)Sep 26, 2003 · N951LF · Airbus A320233 · Engine Mount SectionSDR 2004F00066Fitting · corrodedAT C-CHECK, FOUND FLOOR SUPPORT FITTING AT AFT CARGO COMPARTMENT FRAME 56, LBL 12 IS CORRODED AROUND 2 EACH FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT FITTING AT FRAME 56, LBL 12, IN AFT CARGO PIT. (M)Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Main, Attach FittingsSDR 2004F00065Fitting · corrodedAT C-CHECK, FOUND FLOOR SUPPORT FITTING AT AFT CARGO COMPARTMENT FRAME 56 BL 0 IS CORRODED AROUND 2 EACH FASTENER HOLES. REMOVED AND REPLACED FLOOR SUPPORT FITTING AT FRAME 56, BL 0 IN AFT CARGO PIT. (M)Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Main, Attach FittingsSDR 2004F00064Skin · damagedAT C-CHECK, FOUND UPPER FUSELAGE CROWN AREA BETWEEN FRAMES 52 AND 53 STRINGER 1 LT AND 1 RT VHF ANTENNA MOUNT SURFACE HAS TOOL MARKS AROUND PERIPHERY. UPON FURTHER EVALUATION OF UPPER FUSELAGE CROWN AREA BETWEEN FRAME 52 AND FRAME 53, STRINGER 1L AND 1R, VHF Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Main, Plate/SkinSDR 2004F00063Stringer · corrodedAT C-CHECK, FOUND AFT CABIN FUSELAGE STRINGER FLOOR LEVER UPPER SURFACE CORRODED BETWEEN FRAMES 68-69 AT STATION 3280. REMOVED AND REPLACED STRINGER 21L BETWEEN FRAMES 68 AND 69 STATION 3280. (M)Sep 26, 2003 · N951LF · Airbus A320233 · Fuselage Main, Longeron/StringerSDR 2004F00138Sill · corrodedAT C-CHECK, FOUND CORROSION AT L2 DOOR INBOARD OF AFT GIRT BAR ATTACH PLATE AT FRAME 68 AND LBL 50. REMOVED AND REPLACED L2 DOOR SILL, LOWER FORWARD CORNER FITTING, DRAINS AND ANGLE AT FRAME 67, LEFT LOWER, UNDER SILL. (M)Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Miscellaneous StructureSDR 2004F00137Floorboard · corrodedAT C-CHECK, FOUND CORROSION ON MAIN CABIN FLOORBOARD PANEL NR 222FF. REPAIRED MAIN CABIN FLOORBOARD NR 222FF. (M)Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR 2004F00135Floorboard · corrodedAT C-CHECK, FOUND CORROSION ON MAIN CABIN FLOORBOARD PANEL NR 221FF. REMOVED SURFACE CORROSION FROM FLOORBOARD 221FF. MATERIAL LOSS FOUND TO BE WITHIN LIMITS. TREATED AND PRIMED. (M)Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR 2004F00123Pan · corrodedAT C-CHECK, FOUND CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY ATTACH POINTS FOR BLOW-OUT DOOR FRAME, 8 PLACES. AFTER EVALUATION, FOUND NO CORROSION ON LEFT AFT LAVATORY FLOOR PAN ASSEMBLY, ATTACHMENT POINTS FOR BLOW OUT DOOR FRAME. (M)Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Floor PanelSDR 2004F00120Floorbeam · corrodedAT C-CHECK, FOUND CORROSION AT R2 DOOR FLOORBEAM 8 INCHES INBOARD OF DOOR CUT OUT FROM FRAMES 66 TO 68 RBL 50. REPAIRED CORRODED AREA AT R2 DOOR FLOORBEAM, 8 INCHES INBOARD OF DOOR CUTOUT FROM FRAMES 66 TO 68, RBL 50. (M)Sep 17, 2003 · N951LF · Airbus A320233 · Fuselage Main, Floor Beam
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