Airbus A320-232

Service difficulty reports · 32,653

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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 = 'A320232'
  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 AALA202302225968Control Unit · defectiveAIRCRAFT WAS GROUNDED: INFLIGHT, THE FLIGHT DECK DOOR HANDLE STUCK IN LOCKED POSITION FROM INSIDE. UNABLE TO MOVE IT OR EXIT FLIGHT DECK. MAINTENANCE REPLACED FLIGHT DECK DOOR CONTROL UNIT 24MQ PER AMM 52-51-14-400-001-A AND TASK CARD 26L20052001. A SATISFACTOFeb 18, 2023 · N663AW · Airbus A320232 · Fixed Inner DoorsSDR AALA202302226585Wire · brokenAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT SEAT ROW 9 ABC IS INOPERATIVE. MAINTENANCE REPAIRED EMERGENCY LIGHT WIRE PER ESPM 20-48-14 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.Feb 18, 2023 · N673AW · Airbus A320232 · Emergency LightingSDR AALA202302221459Light · inoperativeAIRCRAFT WAS NOT GROUNDED: FORWARD EMERGENCY LIGHT AT AFT LEFT HAND LAVATORY IS INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT PER AMM 33-51-18 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.Feb 18, 2023 · N673AW · Airbus A320232 · Emergency LightingSDR YENA2023023100182Slide Raft · failedFLT#1134, SJU-MCO. ' EMERGENCY LIGHTS TEST FAILED INT AND EXT LOAD FAULT FWD LEFT, R1 DOOR SLIDE REQUIRES REPLACEMENT; REMOVED AND REPLACED R1 DOOR SLIDE PACK ASSY PER AMM 25-62-44. PERFORMED OPS TEST OF EMERG LIGHT SYS PER AMM 33-51-00. TEST OK. A/C OK FOR COFeb 17, 2023 · N633JB · Airbus A320232 · Emergency EquipmentSDR CALA2023022000477None · corrodedR.H. FWD. ENTRY DOOR R-1 CUTOUT FR.16-20 STGR 22-23 HAS CORROSIO N AT MULTIPLE LOCATIONS (A3NB-53-3-6298) GENERATED AT HAECO LCQ BY V921658 PER NR 9292736(40736) REPAIRED RH AND FWD ENTRY DOOR CUT OUT FR16-20, STRG 22-23 IAW A AND METLANDS TBD PERFORMED BY V06Feb 17, 2023 · N447UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2023022000476Fitting · corrodedAFT WET AREA CORROSION WEB FITTING RH BETWEEN FR 69-70 A3NB-53-3 -6279 GENERATED AT HAECO LCQ BY V926223 PER NR 9292676(40676) REMOVED AND REPLACE DISCREPANT AFT WET AREA RH SHEAR WEB IAW A32 0 DWG 53471124 AND SRM 51-42-71-001 PER MECH V061616 INSP V06162 9Feb 17, 2023 · N447UA · Airbus A320232 · Flight Compartment EquipmentSDR CALA2023022000475None · corrodedFWD CARGO PIT FR28 BETWEEN STRINGERS 43L-44 CORROSION ON CLEAT D OT MO64 A3NB-53-3-6105 GENERATED AT HAECO LCQ BY V919150 PER NR 9292684(40684) REMOVED AND REPLACED FWD CARGO PIT CLEAT AT FR28 STR43L-44 IAW A 320 SRM 51-42-11-001 PER MECH V061616 INSP V061629Feb 17, 2023 · N447UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2023022000474Torsion Box · corrodedFWD CARGO PIT TORSION BOX HAS SPOTS OF CORROSION ON UPPER SURFAC E DOT M062 A3NB-53-3-6330 GENERATED AT HAECO LCQ BY V929150 PER NR 9292559(40559) REMOVED AND REPLACED TORSION BOX PLATE FRONT FR24 TO FR28 IAW SR M 51-42-11-001 BY MECH V932196 INSP BY V927281Feb 17, 2023 · N447UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2023022000473None · corrodedFWD CARGO PIT R/H FR29 BETWEEN STRINGERS 40R-41R HAS CORROSION O N CLEAT DOT M069 A3NB-53-3-6105 GENERATED AT HAECO LCQ BY V91915 0 PER NR 9292692(40692) REMOVED AND REPLACED DISCREPANT FWD CARGO CLEAT AT R/H FR29 STR 40R-41R IAW A320 SRM 51-72-11-911-002 BY MFeb 17, 2023 · N447UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2023022000472Shear Plate · corrodedAFT WET AREA SHEAR PLATE AT FR70 OUTER SKIN TIE HAS CORROSION A3 NB-53-3-6279 GENERATED AT HAECO LCQ BY V926223 PER NR 9292673 (4 0673) REMOVED AND REPLACED DISCREPANT L/H AFT SHEAR WEB FR69-70 IAW A3 20 DWG 5387124 AND SRM 51-4271-001 PER MECH V061616 INSP V0Feb 17, 2023 · N447UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2023022000480Stop · crackedEA 5340-01724 REV C, STEP 3.1-- FR 66 LEFTHAND AFT DOORSTOP #1 LOWER INBOARD FITTING HOLE CRACKED IN 2 PLACES "REPAIR BEFORE NE XT FLIGHT"Feb 17, 2023 · N448UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2023022000479Stop · crackedDURING ROTO INSP ON LH FR68 DOOR STOP #1. CRACK INDICATION NOTED IN LWR I/B HOLE. REPAIR BEFORE NEXT FLIGHT, REPAIRED LH FR68 DOOR STOP #1 LOWER I/B HOLE PER SRM 53-41-12-30 0-011. EMP: V934143 WC: 45467 STA: ST ENG BFMFeb 17, 2023 · N448UA · Airbus A320232 · Fuselage Main, Attach FittingsSDR CALA2023022000478Door Sill · corrodedAFT L2 PAX DOOR SILL CORRODED I/B OF FR68 PER HAECO LCQ N/R 9292 593/40593 GEN BY V937268 REMOVED AND REPLACED DISCREPANT L2 PAX DOOR SILD IAW A320 SRM 51 -42-11-001 PERFORMED BY V061616Feb 17, 2023 · N447UA · Airbus A320232 · Fuselage Structure (General)SDR GTIA2023022036977Pylon · chafed"DURING PYLON NO 2 EWIS INSPECTION FOUND COMBO SEAL DUCT CLAMP CHAFFING WITH THE PYLON RIB 08-09 WALL SKIN -VERIFIED LTPR NR # 5001214933-0020 HAS BEEN ACCOMPLISHED. "Feb 16, 2023 · N627NK · Airbus A320232 · Nacelle/Pylon StructureSDR GTIA2023022036976Megaphone · inoperativeMEGA PHONE INOP (FWD)-R/R MEGAPHONE IAW SPIRIT ACFT EMER EQUIPMENT DRAWING A320-EMER EQUIPFeb 16, 2023 · N619NK · Airbus A320232 · Emergency EquipmentSDR AALA202302177174Sliding Window · bindingAIRCRAFT IN BASE MAINTENANCE: FIRST OFFICERS SLIDING WINDOW DOES NOT OPERATE SMOOTHLY BINDS IN FRAME. MAINTENANCE REMOVED, INSTALLED CORRECTLY AND ADJUSTED THE FIRST OFFICERS SLIDING WINDOW PER AMM 56-12-11-000-001-A AND AMM 56-12-11-400-001-A. A SATISFACTORYFeb 16, 2023 · N655AW · Airbus A320232 · Flight Compartment WindowsSDR YENA2023021700175Control Unit · failedFLT#706, FLL-EWR. 'ON TAKE OFF AROUND 70KTS WE GOT A BRAKE AUTOBRAKE FAULT BRAKE RELEASED; AS PER TSM 32-42-00-810-819A. PERFORMED BITE TEST OF BSCU IAW AMM 32-46-00 AND FUNCTIONAL TEST OF #2 TACHOMETER IAW AMM 32-42-00-720-002. ALL CHECKS ARE GOOD, COULD NOT Feb 16, 2023 · N563JB · Airbus A320232 · Landing Gear Brake SystemSDR CALA2023021600468Safety Valve · unknownGEAR WOULD NOT EXTENDNORMALLY. GRAVITY EXTPER ECAM. REPLACED PRIORITY VALVE, GREEN SYSTEM REF AMM 29-11-33. LEAK CHECKED NO HELP. GEARS AND GEAR DOORS WOULD NOT RETRACT. REPLACED HYD SYTEM SAFETY VALVE. NEED OPERATIONAL TEST. ACCOMPLISHED RII INSPECTION. REPLAFeb 16, 2023 · N478UA · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR CALA2023021600456None · corrodedGEN BY NRC: SUPPORT TASK: DURING CLEANING OF AFT CABIN UNDER FLO OR FOUND CORROSION AT BILGE AREA FR67 AFT FACE BETWEEN STGR42L T O STGR42R. REMOVED & REPLACED FR67 P/N:D5348021221002 IAW SRM 51-42-11 D534802212 ST ENG BFM WC:49846 V935774Feb 16, 2023 · N402UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2023021600455Seat Track · corrodedCABIN SEAT TRACK -Y765 FR20 HAS CORROSION. REMOVED AND REPLACED CABIN SEAT TRACK -Y765 FROM FR12 TO FR24 IA W SRM 51-72-11-911. EMP: V933866 WC: 50690 STA: ST ENG BFMFeb 16, 2023 · N451UA · Airbus A320232 · Fuselage Main, StructureSDR GTIA2023021636971Door · false activationIN FLT WATER SERVICE DOOR INDICATED OPEN ( ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE 133AL - 171AL - 192NB )--Feb 14, 2023 · N652NK · Airbus A320232 · DoorsSDR CALA2023021400440Floor Support · corroded(A3NB-53-3-6038) CABIN FLOOR SUPPORT BY DOOR R1 FR20 HAS CORROSION. CABIN FLOOR SUPPORT BY DOOR R1 FR 20, REMOVED CORROSIONIAW SRM 5 NEW WEB IAW SRM 51-42-11. NEW WEB IAW SRM 51-42-11. NEW WEB IAW SRM 51-42-11. 1-74-00, CHECKED LIMITS L-20, W-.14 D=0.070 FOUNDFeb 14, 2023 · N451UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2023021400439Floorbeam · corrodedAFT CABIN FLOORBEAM +Y765 HAS CORRDED HARD POINT AT FR68. AFT CABIN FLOOR BEAM +Y765 HARD POINT AT FR68 OUT OF LIMITS. REMOVED, REPLACED NEW SUPPORT BEAM PART # D5347219220000 BATCH# 00 03916319 IAW SRM 51-42-11. EMP: V934337 WC: 50825 STA: ST ENG BF MFeb 14, 2023 · N451UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2023021400437Floor Support · corroded(A3NB-53-3-6038) CABIN FLOOR SUPPORT BY DOOR R1 FR20 HAS CORROSION. CABIN FLOOR SUPPORT BY DOOR R1 FR 20, REMOVED CORROSIONIAW SRM 5 NEW WEB IAW SRM 51-42-11. NEW WEB IAW SRM 51-42-11. NEW WEB IAW SRM 51-42-11. 1-74-00, CHECKED LIMITS L-20, W-.14 D=0.070 FOUNDFeb 14, 2023 · N451UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2023021400435Beam · corrodedAFT CABIN FLOORBEAM +Y765 HAS CORRDED HARD POINT AT FR68. AFT CABIN FLOOR BEAM +Y765 HARD POINT AT FR68 OUT OF LIMITS. REM OVED, REPLACED NEW SUPPORT BEAM PART # D5347219220000 BATCH# 00 03916319 IAW SRM 51-42-11. EMP: V934337 WC: 50825 STA: ST ENG BF MFeb 14, 2023 · N451UA · Airbus A320232 · Fuselage Main, StructureSDR AALA202302156619Bulb · burned outAIRCRAFT WAS NOT GROUNDED: MULTIPLE BULBS OUT IN EXIT SIGN OVER ENTRY AND SERVICE DOORS. MAINTENANCE REPLACED EXIT SIGN BULBS AS REQUIRED AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.Feb 13, 2023 · N657AW · Airbus A320232 · Emergency LightingSDR AALA202302154695Oven · odorAIRCRAFT WAS NOT GROUNDED: LEFT HAND INBOARD OVEN HAS EITHER ELECTRICAL OR PLASTIC SMELL AFTER COOKING. MAINTENANCE REPLACED OVEN PER AMM 25-33-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.Feb 13, 2023 · N601AW · Airbus A320232 · Buffet/GalleysSDR GTIA2023021336969None · noneL2 AND R2 DOOR ASSIST BOTTLE REQ SERVICING. -SERVICED L2 AND R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00.Feb 13, 2023 · N694NK · Airbus A320232 · Passenger/Crew DoorsSDR CALA2023021300426Stop · crackedLEFT FR66 DOORSTOP #1 INBD LOWER HOLE HAS CRACK INDICATIONS IN F RAME 1 POSITION. GEN BY V061671 ON HAECO LCQ NR 9298406/42406 CRACKS NOTED.REQUIRES INSP AT 31,600 FC FROM RPR EMBODIMENT WITH 53-41-12-205-010 TABLE 001.THIS IS A CLASS B RPR. ALL WORK ACMP SUBSFeb 13, 2023 · N427UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2023021300427Fuel Cap · missingPDA 2 FUEL CAP MISSING. INSTALLED NEW FUEL CAP. PARTS USED: 31-2825-9-0001,QTY :1Feb 13, 2023 · N435UA · Airbus A320232 · Aircraft Fuel SystemSDR YENA2023021300157None · noneFLT#1075, PVD-MCO. ' DESCENT FROM FL 350, AT FL230 DOWN TO 13000 WE HAD ODOR SMELL OF CHEMICAL, WET BURNT WOOD. HP VALVES OPEN CABIN FWD/AFT ALSO HAD A SMELL ON THE GROUND AFTER LANDING SINGLE ENG APU ON BLEED. IT SMELLS AGIN BUT MORE OF BURT PLASTIC; COMPLIEDFeb 12, 2023 · N638JB · Airbus A320232 · Air Conditioning SystemSDR CALA2023021300417Stop · crackedLEFT FR66 DOORSTOP #1 OTBD UPPER HOLE HAS A CRACK INDICATION IN FRAME AT 8:30 POSITIONS. GEN BY V061671 ON HAECO LCQ NR 9298407( 42407) AMED BUSHING TO FINAL ID OF .2815? IAW SRM 53-41-12-300-010. LEF UIRES INSPECTION AT 33,000 FC AND SUBSEQUENT INSPECTION AT Feb 12, 2023 · N427UA · Airbus A320232 · Fuselage Main, FrameSDR AALA202302140538Bulb · inoperativeAIRCRAFT IN BASE MAINTENANCE: LIGHT BULBS INOPERATIVE AT L1 DOOR UPPER EXIT SIGN. MAINTENANCE REPLACED LIGHT BULBS AT L1 DOOR UPPER EXIT SIGN PER AMM 33-51-19-400-003-A AND PERFORMED SATISFACTORY OPERATIONAL CHECK OF EMERGENCY LIGHTS PER AMM 33-51-00-710-805A.Feb 11, 2023 · N652AW · Airbus A320232 · Emergency LightingSDR YENA2023021300156Cids · failedFLT#1464, SJD-LAX. (AIRCRAFT PERFORMED AN AIR TURN ABCK TO SJD) ' SHORTLY AFTER TAKE OFF WE HAD A FWD AND AFT CARGO SMOKE DET FAULT INDICATION( CIDS SYSTEM - DIRECTOR (N703-UP) ); REMREP CIDS 2 DIRECTOR PER AMM 23-73-34. OPS CHECK NORMAL. THIS CLEARS MDDR 5007Feb 11, 2023 · N708JB · Airbus A320232 · Communications SystemSDR CALA2023021300416Coupling · detachedPDA 2 FUELER REPORTED ACFT ARIVED WITH FUEL CAP MISSING. SN OFF CAP MISSING C192092 NOTIFIED TOMC ABOUT FUEL CAP PDAFeb 11, 2023 · N465UA · Airbus A320232 · Aircraft Fuel SystemSDR CALA2023021300414Stop · crackedLEFT FR66 DOORSTOP #1 INBD LOWER HOLE HAS CRACK INDICATIONS IN F RAME AT 6 POSITION. GEN BY V061671 ON HAECO LCQ NR 9298406/42406 EMBODIMENT AT 60,000 FC IAW SRI 53-41-12-205-010 TABLE 001 AREA 3.THIS IS A CAT B RPR.ALL WRK ACMP ON HAECO NR 9298406. ACMP BATHTFeb 11, 2023 · N427UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2023021300413Unknown · crackedFUSELAGE FR68 (RH) CRACKED BETWEEN FRAME WEB AND FRAME STIFFENER (STR 22RH) AND CORROSION DAMAGE NOTED IN THE FRAME FWD FACE & INNER CAP AREA BETWEEN STR23R-24R. REF HAECO LCQ NR 9296525 AND NR 9296374. BETWEEN STR23R-24R PER HAECO REO-L242211 REV IR AND ECRAFeb 11, 2023 · N449UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2023021300411Unknown · corrodedFRAME 68 R/H FWD FACE HAS CORROSION AROUND ANCHOR NUT AND ALONG FLOOR LINE. GENERATED AT HAECO LCQ PER NR 9296525 (40525) BY V07 7960 {A3NB-53-3-6222} IR AND ECRA 5341-01367. WORK ACCOMPLISHED BY LCQ EMP V080280. LATEST REVISION OF EC/RA 5341-01367 ON OR BEFORFeb 11, 2023 · N449UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2023021300410Door · corrodedR1 DOOR FR 20 STGR 22R- STGR 23R PER HAECO LCQ N/R 9296513/40513 GEN BY V061629 ACCOMPLISHED BY LCQ EMP V080280. ACCOMPLISH INITIAL INSPECTIONS LEVEL PER PART 2 OF THE LATEST REVISION OF ECRA 5311-02946 ON OR ON THE REPAIR AT THE RH FR20 LOWER FWD WEB FACE AT Feb 11, 2023 · N449UA · Airbus A320232 · Fuselage Structure (General)SDR YENA2023021400173None · noneDURING HEAVY MAINTENANCE: OVERPRESSURE OFFWING SLIDE RESERVOIR RH; REF: ARM W/O 2022-453/1 NR 2022-676108 REMOVED AND REPLACED OFFWING RESERVOIR RH (7507MM) IAW AMM 25-62-46-000-001-A STEP 1 THRU 4.A AND AMM 25-62-46-400-001-A. FUNCTIONAL AND OPS TEST OK. TECHFeb 10, 2023 · N508JL · Airbus A320232 · Emergency EquipmentSDR YENA2023021400172None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON CENTER FRONT WINDSHIELD FRAME, CENTER POST, AROUND UPPER BOLT LH SIDE IN COCKPIT. REF: ARM W/O 2022 453/1 N/R 2022-676202; REF: ARM W/O 2022-453/1 NR 2022-676202 ACCOMPLISHED PERMANENT REPAIR ON LH WINDSHIELD FRAMEFeb 10, 2023 · N508JL · Airbus A320232 · Fuselage Structure (General)SDR YENA2023021400171None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FR36 VERTICAL STRG FLOOR BEAM 4 ZONE 1. THE CRACK DIRECTION IS 12 O'CLOCK. REF: ARM W/O 2022-453/1 N/R 2022-676216; REF: ARM W/O 2022-453/1 NR 2022-676216 PERFORMED REPAIR LOCATED ON Y-254 (BEAM 4) ZONE 1, VERTICALFeb 10, 2023 · N508JL · Airbus A320232 · Fuselage Structure (General)SDR YENA2023021400170None · noneDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR55 AND FR56 IN AFT CARGO COMPARTMENT (CPC P RELATED REFER TO MPD TASK 534107-01); (RESOLVED ON W/O: 1176129 TASKCARD: NR-00027 ) ALL WORK ACCOMPLISHED REF AEROMAN NRC 2022-676486. REMOVED AND REPLACED STFeb 10, 2023 · N508JL · Airbus A320232 · Aerodynamic FairingsSDR YENA2023021400169None · noneDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR57 AND FR58 IN AFT CARGO COMPARTMENT (CPC P RELATED REFER TO MPD TASK 534107-01); (RESOLVED ON W/O: 1176129 TASKCARD: NR-00028 ) ALL WORK ACCOMPLISHED ON AEROMAN NR 2022-676482, REMOVED AND REPLACED STRINFeb 10, 2023 · N508JL · Airbus A320232 · Aerodynamic FairingsSDR YENA2023021400168None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE HORIZONTAL FLANGE RADIUS AT STGR 22 AFT WEB FACE, CRACK LENGTH IS 1.500 INCH APPROX, AT AFT GALLEY AREA (1EA); ACCOMPLISHED PERMANENT REPAIR IAW AEROMAN WO 2022-453/1, NR 2022-676465 AND JETBLUE ECFeb 10, 2023 · N508JL · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2023021400167None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON VERTICAL STRG FLOOR BEAM 3 ZONE 2. THE CRACK DIRECTION IS 12 O'CLOCK. REF AEROMAN NRC 2022-676209; REF: ARM W/O 2022 453/1 N/R 2022-676209 REPAIRED IAW EC NO. A23-034-01 AND EA 53-0635-22, REV 0 (COVER, PART 1 AND Feb 10, 2023 · N508JL · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA2023021400166None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON VERTICAL STRG FLOOR BEAM 4 ZONE 2. CRACK DIRECTIONS ARE 12 O'CLOCK AND 8 O'CLOCK. REF AEROMAN NRC# 2022-676210; REF: ARM W/O 2022 453/1 N/R 2022-676210. REPAIRED PER EC NO. A23-034-01 AND EA 53-0635-22. ITEM IS CATFeb 10, 2023 · N508JL · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA2023021400165None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FR36 VERTICAL STRG FLOOR BEAM 5 ZONE 2. THE CRACK DIRECTION IS 11 O'CLOCK. REF AEROMAN NRC 2022-676220; REF: W/O 2022 453/1 N/R 2022-676220 REPAIRED PER EC A23-034-01 AND EA 53-0635-22 REV 0 (COVER PART 1 AND PARTFeb 10, 2023 · N508JL · Airbus A320232 · Fuselage Main, Attach FittingsSDR YENA2023021400164None · noneDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR57 AND FR58 IN AFT CARGO COMPARTMENT (CPCP RELATED REFER TO MPD TASK 534107-01); ALL WORK ACCOMPLISHED ON AEROMAN NR 2022-676482, REMOVED AND REPLACED STRINGER 43L BTW FR57 AND FR58 IN AFT CARGO COMPARTMENFeb 10, 2023 · N508JL · Airbus A320232 · Fuselage Structure (General)SDR YENA2023021400163None · noneDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FR55 AND FR56 IN AFT CARGO COMPARTMENT (CPC P RELATED REFER TO MPD TASK 534107-01); ALL WORK ACCOMPLISHED REF AEROMAN NRC 2022-676486. REMOVED AND REPLACED STRINGER 43L BTW FR54 AND FR60 IN AFT CARGO COMPARTFeb 10, 2023 · N508JL · Airbus A320232 · Fuselage Structure (General)
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