Airbus A320-231

Service difficulty reports · 3,758

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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 = 'A320231'
  ORDER BY difficulty_date DESC"

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SDR AWXA200200104Doubler · dentedPHX - GROUND DAMAGE - "O" - DURING WALK AROUND DAMAGE TO THE FUSELAGE SKIN WAS FOUND JUST AFT OF THE RADOME ON BELLY OF AIRCRAFT AT FS 01. MAINTNENANCE PERFORMED HFEC INSPECTION ON OUTSIDE SKIN AND INTERNAL SURROUNDING STRUCTURE, NO DEFECTS WERE NOTED. TEMPORAFeb 3, 2002 · N636AW · Airbus A320231 · Fuselage Main, Plate/SkinSDR CA020204001Hose · ruptured(CAN) LOST HYDARULIC QUANTITY IN GREEN SYSTEM AND LOW PRESSURE WARNING ON ENGINE 1 HYDRAULIC SYSTEM(GREEN). CREW SWITCHED OFF THE EDP AND PTU AT FIRST INDICATION OF FLUID LOSS AND USED THE EMERGENCY FREE FALL GEAR EXTENSION HANDLE. MAINTENANCE FOUND A RUPTUREDFeb 2, 2002 · Airbus A320231 · Hydraulic System, MainSDR AWXA200200095Fire Loop · chafedPHX - ABORTED T/O - FLT 0317 - C - WHILE PREPARING TO TAKEOFF FROM PHX EN ROUTE TO CMH WHEN THROTTLE WERE ADVANCED FLIGHT CREW RECEIVED A NR 1 ENGINE FIRE LOOP-A FAULT. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT AND FOUND Feb 1, 2002 · N627AW · Airbus A320231 · Fire DetectionSDR AWXA200200084Lens · missingCMH - EEL - "C" - EMERGENCY ESCAPE PATH LIGHT RED LENS COVER MISSING AT SEAT 9A. MAINTENANCE INSTALLED RED EMERGENCY ESCAPE PATH LIGHT LENS COVER AT SEAT 9A.Jan 27, 2002 · N634AW · Airbus A320231 · Emergency LightingSDR AWXA200200145Floor Support · corrodedYWG - MAJOR REPAIR - C - DURING C-08 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT Y1292 AT FR 66 RT. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW DWG D53472090, AND SRM 51-42-11.Jan 25, 2002 · N646AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200200167Floor Support · corrodedYWG - MAJOR REPAIR - "C" - DURING C-08 CHECK CORROSION WAS FOUND AROUND SCREW HOLES ON FLOOR SUPPORT AT Y1162R, BETWEEN FR 68 & 69. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT Y1162R, BETWEEN FR 68 & 69; FABRICATED A NEW FLOOR SUPPORT AND INSTALLED REPAIRS IJan 25, 2002 · N646AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA200200166Floor Support · corrodedYWG - MAJOR REPAIR - "C" - DURING C-08 CHECK CORROSION WAS FOUND ON FORWARD AND AFT FLOOR SUPPORT IN FORWARD CABIN AT Y254, FR 15-19. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER SRM 53-11-14; REMOVED CORRODED FLOOR SUPPORT; FABRICATJan 22, 2002 · N646AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR CA020118006Handle · malfunctioned(CAN) AT APPRXIMATELY 10,000 FT ALTITUDE THE FWD CARGO DOOR INDICATED UNSAFE ON ECAM. THE AIRCRAFT DIVERTED AND WAS INSPECTED BY A COMPANY ACA. THE DOOR HANDLE WAS FOUND TO BE OUT OF THE DETENT BY ABOUT 1/4 OF AN INCH. THE HANDLE ASSY AND DOOR LOCKING MECHANISJan 17, 2002 · Airbus A320231 · Cargo/Baggage DoorsSDR AWXA200200042Battery · dischargedSAN - EEL - C - DURING TEST OF EMERGENCY EXIT LIGHTING ALL OF THE FWD AND AFT SECTION EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS 10WL (ZONE 221) AND 13WL (ZONE 263) IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD IJan 16, 2002 · N637AW · Airbus A320231 · Emergency LightingSDR AWXA200200014Decoder · inoperativePHX - EEL - C - DURING INSPECTION EMERGENCY LIGHT SYSTEM FAILED TEST WITH FAULTS INDICATING EMERGENCY COMM LT. MAINTENANCE TROUBLESHOT AND REPLACED DEU-B 300RH4 PER AMM 23-73-47-401.Jan 9, 2002 · N636AW · Airbus A320231 · Entertainment SystemSDR CA020109008Brake · overheated(CAN) SHORTLY AFTER POWER WAS APPLIED AT TAKEOFF, BOTH BRAKE TEMPERATURE INDICATIONS ON LEFT SIDE EXCEEDED 300 DEG.C, FLIGHT CREW REJECTED TAKEOFF. MAX BRAKE TEMP INDICATION ON LEFT SIDE WAS 610 DEG.C. BRAKES STARTED TO SMOKE. REJECTED TAKEOFF INSPECTION Jan 6, 2002 · Airbus A320231 · BrakeSDR AWXA200200007Battery · dischargedPHX - EEL - C - DURING INSPECTION ALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. NOTE: AIRCRAFT HAS BEEN PARKED SINCE 30 NOVEMBER, 2001. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS 10WL-13WL, ZONES 221, 241, 242, AND 263 IAW AMM 33-51-38,Jan 5, 2002 · N646AW · Airbus A320231 · Emergency LightingSDR AWXA200200001Power Supply · dischargedPHX - EEL - C - EMERGENCY ESCAPE LIGHTS INOPERATIVE ON THE LEFT SIDE OF THE AIRCRAFT. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL, OPERATIONAL CHECK WAS GOOD.Jan 1, 2002 · N627AW · Airbus A320231 · Emergency LightingSDR AWXA200100681Cable · brokenPHX - EEL - "C" - DURING INSPECTION MAINTENANCE FOUND EMERGENCY SEAT LIGHT WIRE BROKEN AT ROW 13. MAINTENANCE REPAIRED BROKEN WIRE AT ROW 13 IAW ESPM 20-53-20.Dec 29, 2001 · N634AW · Airbus A320231 · Emergency LightingSDR AWXA200100677Handle · not seatedLAX - ABORTED TAKEOFF - FLT 702 - "C" - WHEN INITIATING TAKEOFF FLIGHT CREW RECEIVED AN AFT CARGO DOOR WARNING LIGHT INDICATION, TAKEOFF WAS ABORTED WITHOUT INCIDENT AND AIRCRAFT RETURNED TO THE GATE. AT THE GATE MAINTENANCE INSPECTED THE AFT CARGO DOOR AND FODec 29, 2001 · N629AW · Airbus A320231 · Door Warning SystemSDR AWXA200100655Flap · puncturedYWG - MAJOR REPAIR - "C" - DURING C-02 CHECK MAINTENANCE DISCOVERED THE L/H OUTBOARD TRAILING EDGE FLAP HAS A PUCTURE ON THE LOWER SURFACE JUST INBOARD OF THE #3 CANOE. MAINTENANCE CUTOUT THE DAMAGED AREA OF SKIN AND FABRICATED, FITTED, AND INSTALLED A HONEYCODec 18, 2001 · N633AW · Airbus A320231 · Trailing Edge FlapsSDR AWXA200100653Power Supply · faultyPHX - EEL - C - FLIGHT ATTENDANT PANEL INDICATED EMERGENCY LIGHT POWER SUPPLY FAULT LT FWD (10WL). MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY 10WL IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD.Dec 18, 2001 · N644AW · Airbus A320231 · Emergency LightingSDR AWXA200100650Seat Track · corrodedYWG - MAJOR REPAIR - C - DURING C-02 CHECK MAINTENANCE FOUND CORROSION AT NR 3 SEAT TRACK BS FRAME 20, RBL 1292. MAINTENANCE REMOVED, FABRICATED AND INSTALLED 8 INCH SECTION OF TRACK 4 INCHES FORWARD TO 4 INCHES AFT OF FRAME 20, RBL 1292, IAW SRM 53-00-15, FIDec 14, 2001 · N633AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200100649Seat Track · corrodedYWG - MAJOR REPAIR - C - DURING C-02 CHECK MAINTENANCE FOUND CORROSION AT NR 4 SEAT TRACK BS FRAME 20, RBL 765. REMOVED, FABRICATED AND INSTALLED 8 INCH SECTION OF TRACK 4 INCHES FORWARD TO 4 INCHES AFT OF FRAME 20, RBL 765 IAW SRM 53-00-15, FIG 201, PG 202-2Dec 14, 2001 · N633AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200100641Power Supply · dischargedSAN - EEL - "C" - RT OVERWING EXIT SIGN 42WL INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY UNIT 12WL AT ZONE 242 IAW AMM 33-51-38-000-001, OPERATIONAL CHECK WAS GOOD.Dec 14, 2001 · N644AW · Airbus A320231 · Emergency LightingSDR AWXA200100639Power Supply · dischargedCMH - EEL - "C" - SEVERAL EMERGENCY LIGHTS INOPERATIVE MID CABIN LT SIDE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT AT 11WL, ZONE 241 IAW AMM 33-51-38-000-001.Dec 12, 2001 · N627AW · Airbus A320231 · Emergency LightingSDR AWXA200100640Battery Pack · dischargedLAX - EEL - "C" - TWO SEAT LIGHTS OUT LEFT FORWARD CABIN. MAINTENANCE REPLACED FORWARD EMERGENCY BATTERY PACK 10WL AT ZONE 221 PER T/C F1C33301, OPERATIONAL CHECK WAS GOOD.Dec 11, 2001 · N620AW · Airbus A320231 · Emergency LightingSDR AWXA200100609Warning System · malfunctionedLAS - ABORTED TAKEOFF - FLT 0193 - C - ON TAKEOFF ROLL RUNWAY 22R AT 60 KTS AFT CARGO DOOR OPEN INDICATION APPEARED ON ECAM; TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED UNEVENTFULLY TO THE GATE. AT THE GATE MAINTENANCE VISUALLY CONFIRMED CARGO DOOR WAS CLOSED ADec 1, 2001 · N629AW · Airbus A320231 · Door Warning SystemSDR AWXA200100613Power Supply · defectiveLAS - EEL - FLT 0116 - "C" - CAPTAIN REPORTED L2 AND R2 EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY 13WL IAW AMM 33-51-38, OPERATIONALLY CHECKED GOOD.Nov 30, 2001 · N621AW · Airbus A320231 · Emergency LightingSDR AWXA200100594Switch · failedPHX - EMERGENCY LANDING - FLT 614 - 10 MIN AFTER TAKEOFF FROM SAN TO PHX ECAM MESSAGE APPEARED FOR YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL. FLIGHT CONTINUED TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCE VERIFIED NO FLUID LOSS AND TROUBLESHOT SYSTEM RENov 25, 2001 · N643AW · Airbus A320231 · Hydraulic Quantity SensorSDR AWXA200100595O-Ring · leakingCLE - EMERGENCY LANDING - FLT 534 - C - EN ROUTE FROM PHX TO CLE RECEIVED YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL QUANTITY INDICATION WITH PRESSURE INDICATING NORMAL, 1 HR 30 MIN LATER SYSTEM LOST ALL PRESSURE. DECLARED EMERGENCY LANDING INTO CLE, LANDINGNov 25, 2001 · N627AW · Airbus A320231 · Hydraulic System, MainSDR AWXA200100590Pump · failedCMH - DIVERTED FLIGHT - FLT 683 -C- EN ROUTE FROM PHX TO EWR DURING CLIMB THE FLIGHT DECK CREW OBSERVED ECAM MESSAGE CTR TK PUMP 1 LO PRESS, FOLLOWED BY PUMP 2 LO PRESS. THE CREW CONTACTED MAINTENANCE CONTROL AND WERE INSTRUCTED TO TRY MANUAL MODE, BUT STILL Nov 16, 2001 · N634AW · Airbus A320231 · Fuel Boost PumpSDR AWXA200100566Service difficultyPHX - DIVERTED FLIGHT - FLT 613 - "C" - ON LEVEL OFF AT FL 370 ENROUTE FROM LAS TO ATL, ECAM MESSAGE APPEARED FOR LEFT PACK OVER PRESSURE FOLLOWED BY #2 BLEED OVER PRESSURE FAULT. CREW WAS UNABLE TO CONTROL CABIN PRESS AND DESCENDED TO FL 200 WHERE THEY REGAINNov 2, 2001 · N621AW · Airbus A320231 · Pneumatic Distribution SystemSDR AWXA200100563Relay · failedLanding gear failed to extend when commanded. Crew used manual extension system and landed without further problems. gear swing and trouble shooting per 32-31-00-810 indicated the hydraulic relay 48GA bad. Replaced relay and functional tested per task 31-31-0Oct 29, 2001 · N637AW · Airbus A320231 · Landing Gear Retraction/Extension SystemSDR AWXA200100522Pump · overheatedPHX - AIR TURNBACK - FLT 794 - C - ON CLIMBOUT THE CREW GOT ECAM MESSAGE FOR BLUE HYD SYS ELECTRIC PUMP OVERHEAT. THE CREW FOLLOWED ECAM PROCEDURES AND RETURNED TO PHX. THE ECAM MESSAGE WAS DISPLAYED ENTIRE FLIGHT. MAINTENANCE TROUBLESHOT AND REPLACED THE BOct 9, 2001 · N635AW · Airbus A320231 · Hydraulic Pump (Electric/Engine), MainSDR AWXA200100517Valve · leakingPHX - AIR TURNBACK - FLT 27 - AFTER T/O THE LANDING GEAR WOULD NOT RETRACT. CREW RESET LGCIU 1 & 2 PER MAINTENANCE CONTROL, NO HELP. THE AIRCRAFT APPEARED TO REMAIN IN GROUND MODE. THE AIRCRAFT RETURNED TO PHX, MAKING AN UNEVENTFUL LANDING. MAINTENANCE TROUBLEOct 6, 2001 · N645AW · Airbus A320231 · Main Landing Gear Strut/Axle/TruckSDR AWXA200100512Nipple · loosePHX - ENG FIRE/SMOKE - FLT 14 - "C" - AFTER LANDING, WHEN TAXING OFF RUNWAY, ECAM MESSAGE APPEARED, NO. 2 ENG. FIRE AND CREW SHUTDOWN #2 ENG. OVERHEAD #2 FIRE PUSHBUTTON DID NOT ILLUMINATE. ALL ENG PARAMETERS WERE NORMAL, SMOKE WAS OBSERVED BY THE FIRE DEPT FROct 1, 2001 · N626AW · Airbus A320231 · Turbine SectionSDR AWXA200100479Valve · failedPHX - AIR TURNBACK - FLT 77 - ON CLIMBOUT THE CREW GOT AN ECAM MESSAGE FOR INLET SKIN FAULT AND WERE UNABLE TO PRESSURIZE THE AIRCRAFT. THE AIRCRAFT RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE AVI VENT CONT C/B POPPED. THEY RESET THE C/Sep 30, 2001 · N633AW · Airbus A320231 · Cabin Pressure Control SystemSDR AWXA200100514Seat Track · corrodedYWG - C1 CK -NR 4 SEAT TRACK CORRODED AT FR 20R, Y-1292. BEYOND LIMITS AFTER CORROSION REMOVAL. MAINTENANCE REMOVED DAMAGED SECTION OF TRACK, FABRICATED REPAIR SECTION AND SPLICES AND INSTALLED REPAIR PARTS IAW SRM 53-00-15, FIG 201.Sep 25, 2001 · N635AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200100513Seat Track · corrodedYWG - C1 CK -NR 3 SEAT TRACK AT FR 20R, Y-765, CORRODED. BEYOND SRM LIMITS AFTER CORROSION REMOVAL. MAINTENANCE REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED REPAIR SECTION AND SPLICES AND INSTALLED REPAIR IAW SRM 53-00-15, FIG 201.Sep 25, 2001 · N635AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA200100476Packing · brokenLAX - ABORTED APPROACH - FLT 37 - "C" - ON FINAL APPROACH ECAM INDICATED YELLOW HYDRAULIC SYSTEM LOW PRESSURE, SYSTEM FLUID DEPLETED AND THE CREW PERFORMED A GO AROUND. THE SUBSEQUENT APPROACH AND LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED THE AIRCRAFT ANDSep 25, 2001 · N627AW · Airbus A320231 · Hydraulic System, MainSDR AWXA200100447Fuel Line · damagedPHX-FLT 299-FUEL SMELL IN CABIN-C-WHILE THE AIRCRAFT WAS SITTING AT THE GATE WITH THE APU RUNNING AND AIR CONDITIONING PACKS ON THERE WAS A SMELL OF FUEL IN THE CABIN, STRONGEST OVERWING. WITH THE PACKS TURNED OFF THE SMELL DISSIPATED. MAINTENANCE TROUBLESHOSep 17, 2001 · N636AW · Airbus A320231 · APU Engine Fuel and ControlSDR AWXA200100448Actuator · leakingLAS-FLT 238-FUEL SMELL IN CABIN- C -WHILE APPROACHING THE GATE AFTER LANDING THE CABIN CREW AND SOME PASSENGERS NOTED A FUEL SMELL. THE FLIGHT DECK CREW STARTED THE APU AFTER LANDING, NO FUEL ODOR WAS NOTICED PRIOR TO STARTING THE APU. AT THE GATE THE CREW TURSep 14, 2001 · N643AW · Airbus A320231 · APU Core EngineSDR AWXA0002260Odor · detectedPHX - AIR TURNBACK - FLT 751 - AFTER TAKEOFF THE FLIGHT DECK CREW SMELLED AN ELECTRICAL ODOR IN THE COCKPIT AND RETURNED TO PHX MAKING AN UNEVENTFUL LANDING. EMERGENCY EQUIPMENT HAD BEEN CALLED OUT. BY THE TIME THE AIRCRAFT LANDED THE ODOR HAD DISSIPATED. PSep 13, 2001 · N620AW · Airbus A320231 · Air Distribution SystemSDR AWXA0002202Controller · failedPHX- ABORTED TAKEOFF - FLT 239 - ON TAKEOFF ROLL CREW HAD NO INDICATION OF TOGA AND ABORTED THE TAKEOFF AT 70 KTS AND RETURNED TO THE GATE. MAINTENANCE TROUBLESHOT AND REPLACED THE FLIGHT CONTROL UNIT PER AMM 22-81-12-401, SYSTEM CHECKS WERE GOOD. NO FURTHERAug 24, 2001 · N628AW · Airbus A320231 · Flight ControllerSDR CA010823005Tire · deflated(CAN) L/H NOSE WHEEL ASSEMBLY DEFLATED DURING TAXI TO GATE. MECHANICS ON SITE NOTED, OVER PRESSURE VALVE WAS LOOSE WHICH CONTRIBUTED TO THE LOSS OF PRESSURE IN THE TIRE. L/H AND R/H NOSE WHEEL ASSEMBLIES WERE CHANGED.Aug 22, 2001 · Airbus A320231 · TireSDR AWXA0002213Packing · brokenD: Las - L/H plyon /engine fire - Flt 69 - while taxing in to the gate personnel observed smoke and flame at the top of the #1 ENG. and pylon area. Ground crew advised the pilots who followed QRH procedures. Maintenance opened the thrust reversers / core cowlsAug 18, 2001 · N629AW · Airbus A320231 · Aircraft Fuel Distribution SystemSDR AWXA0002178Floor Support · corrodedFR 20 TO FR 21 Y-1732 RT FLOOR SUPPORT CORRODED. REPAIRED AS PER AWA ER 26-5311-01277DL1.Aug 17, 2001 · N626AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA0002177Floor Support · corrodedFR 16-20 Y 254 LT FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT RAIL FROM FR 12 TO 24 AS PER SRM 53-11-14 PG 37, 205-210 FIG 8 AND 202.Aug 16, 2001 · N626AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA0002176Floor Support · corrodedFR 16-20 Y-254 RT FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT RAIL AS PER SRM 53-11-14 PG 37 AND DWG D53110858.Aug 16, 2001 · N626AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA0002175Seat Track · corrodedFR 20 Y-754 RT SEAT TRACK CORRODED. REPLACED SEAT TRACK/FLOOR SUPPORT RAIL AS PER SRM 53-11-14 PG 37 AND DWG D53110858.Aug 16, 2001 · N626AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA0002163Seat Track · corrodedFR 20 Y -754 RT SEAT TRACK CORRODED. REPLACED SEAT TRACK/FLOOR SUPPORT RAIL AS PER SRM 53-11-14 PG 37 AND DWG D53110858.Aug 16, 2001 · N626AW · Airbus A320231 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA0002162Floor Support · corrodedFR 16-20 Y -254 RT FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT RAIL AS PER SRM 53-11-14 PG 37 AND DWG D53110858.Aug 16, 2001 · N626AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA0002161Floor Support · corrodedFR 16-20 Y 254 LT FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT RAIL FROM FR12 TO 24 AS PER SRM 53-11-14 PG 37, 205-210 FIG 8 AND 202.Aug 16, 2001 · N626AW · Airbus A320231 · Fuselage Miscellaneous StructureSDR AWXA0002174Skin · dentedDENT IN FUSELAGE AT FRAME 23 BETWEEN STRINGERS 25L & 24L. REMOVED PREVIOUS REPAIR. FABRICATED AND INSTALLED SKIN DOUBLER AS PER A320 SRM 53-00-10 FIGURE 203 PAGES 206C TO 208B.Aug 14, 2001 · N626AW · Airbus A320231 · Fuselage Main, Plate/Skin
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