Airbus A320-232

Service difficulty reports · 32,652

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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 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 CALA2025090408469Fitting · damagedR/H ELEVATOR INBD ACTUATOR FITTING LOCKING LUG GOUGED. REPAIRED RH ELEVATOR I/B ACTUATOR FITTING LOCKING LUG IAW A320 S RM 55-26-47-300-001 THIS REPAIR IS CATEGORY A NO FURTHER ACTION REQUIRED.Aug 28, 2025 · N467UA · Airbus A320232 · Elevator StructureSDR YENA2025082800898Pressure Switch · failedFLT#384, MCO-JFK.(AN EMERGENCY WAS DECLARED) "HYDRAULIC YELLOW RESERVOIR OVERHEAT ECAM MESSAGE AFTER TAKEOFF; COMPLETED OPS CHECK OF YELLOW HYD ELECTRIC PUMP/YELLOW HY PRESSURE SWITCH IAW AMM 29-13-00 REF LG PG 4330481 ITEM 1+2. REMOVED AND REPLACED YELLOW HYAug 28, 2025 · N636JB · Airbus A320232 · Hydraulic System, MainSDR YENA2025082800897Pump · failedFLT#384, MCO-JFK.(AN EMERGENCY WAS DECLARED) "HYDRAULIC YELLOW RESERVOIR OVERHEAT ECAM MESSAGE AFTER TAKEOFF; COMPLETED OPS CHECK OF YELLOW HYD ELECTRIC PUMP/YELLOW HY PRESSURE SWITCH IAW AMM 29-13-00 REF LG PG 4330481 ITEM 1+2. REMOVED AND REPLACED YELLOW HYAug 28, 2025 · N636JB · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR YENA2025082800893Battery · failedFLT#47, LGA-TPA. "EMERG LIGHT BATTERY FIN 11WL FAILED TEST; REMOVED AND REPLACED EMERG LIGHT BATTERY FIN 11WL IAW AMM 33-51-38."Aug 28, 2025 · N796JB · Airbus A320232 · Emergency LightingSDR YENA2025082800890Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON EMERGENCY EXIT DOOR (844) FRAME SEGMENT (1) (1EA), CRACK LENGTH: 0.100 INCH; ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT RH EEH) FRAME / REINFORCE DOOR STRUCTURE - MODIFICATION IAAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800889Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON EMERGENCY EXIT DOOR (834) FRAME SEGMENT (1) (2EA), CRACK LENGTH: 3.100 INCH; ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT LH EEH) FRAME / REINFORCE DOOR STRUCTURE - MODIFICATION IAAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800888Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON EMERGENCY EXIT DOOR (833) FRAME SEGMENT (1) (2EA), CRACK LENGTH: 2.500 INCH; ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (FWD LH EEH) FRAME / REINFORCE DOOR STRUCTURE - MODIFICATION IAAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800887Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON EMERGENCY EXIT DOOR (843) FRAME SEGMENT (1) (2EA), CRACK LENGTH: 3.50 INCH; ACCOMPLISHED DOORS / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (FWD RH EEH) FRAME / REINFORCE DOOR STRUCTURE - MODIFICATION IAAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800885Skin · damagedDURING HEAVY MAINTENANCE: LIGHTNING STRIKE EXTERNAL SKIN LOC. BTW FRAME 26 AND FRAME 27 AND BTW STRINGER 41L AND 42L AT LOWER FUSELAGE; WORK ACCOMPLISHED ON AEROMAN W/O:2025 194/1 NR: 2025 - 471516 REPAIR LOCATED BTW FRAME 26 AND FRAME 27 AND BTW STRINGER 41L Aug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2025082800886Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE ( INBOARD LOWER HOLE ) AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 5 O CLOCK; PERFORMED PERMANENT REPAIR LOCATED ON FRAME 68, L/H SIDE AT LEVEL OF DOOR STOP #1 I.A.W. Aug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800884Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE ( INBOARD LOWER HOLE ) AT DOOR STOP FITTING 4 POSITION,CRACK DIRECTION IS 2 O CLOCK AND 7 O CLOCK; (RESOLVED ON W/O: 1402836 TASKCARD: NR-00034) REF AEROMAN WO # 2025-194/1 NAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025082800883Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE ( INBOARD LOWER HOLE ) AT DOOR STOP FITTING 1 POSITION,CRACK DIRECTION IS 12 O C LOCK AND 6 O CLOCK;(RESOLVED ON W/O: 1402836 TASKCARD: NR-00035) REF AEROMAN WO # 2025-194/1 NAug 28, 2025 · N612JB · Airbus A320232 · Fuselage Main, StructureSDR AALA202509106633Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SLAT 1 LOWER BOLT TRACK #3 ATTACHMENT ON RT WING, MEASURES OF CORROSION L: 0.105 IN, W:0.079 IN, D: 0.001IN. MAINTENANCE REPLACED SLAT 1 LOWER BOLT TRACK #3 ATTACHMENT ON RH WING.Aug 27, 2025 · N664AW · Airbus A320232 · Leading Edge DevicesSDR YENA2025082800892Oil Cooler · leakingFLT#1406, SDQ-MCO. "AFTER LANDING WE CHANGED OVER TO APU BLEED ON TAXIWAY. WE NOTICED A BURNING OIL SMELL UPON DOOR, INFLIGHT MONITORED THE SMELL WAS STRONG IN THE CABIN AS WELL; COMPLIED WITH INFO NOTICE 2017-T015-L SECTION B2. IDENTIFY ODOR SOURCE TO BE THE Aug 27, 2025 · N641JB · Airbus A320232 · APU Oil SystemSDR YENA2025082800882Pump · faultedFLT#1642, BZE-JFK. (AN EMERGENCY WAS DECLARED) "HYD GREEN #1 ENGINE PUMP INOP; REF L/P 4349090 ITEM #2 FOR REMOVED AND REPLACED OF ENG #1 PUMP, ENG #1 PRESSURE SWITCH, P/B SWITCH, RELAY ALSO REF L/P 4349091 ITEM #2 (REMOVED AND REPLACED PRESSURE SWITCH ( 1151GAug 27, 2025 · N558JB · Airbus A320232 · Hydraulic Pump (Electric/Engine), MainSDR YENA2025082800881Unknown · odorFLT#699, LGA-MCO. #3&4 INFLIHT CREW REPORTS A VERY STRONG CHEMICAL SMELL IN AFT GALLEY PRODUCING A METALLIC TASTE IN THE MOUTH, SORE THROAT AND HEADACHE OCCURED ON DESCENT FROM 4500 THROUGH ENGINE SHUTDOWN AT GATE. #3 SEEKING MEDICAL ATTN. ACCOMPLISHED TASK Aug 27, 2025 · N608JB · Airbus A320232 · Air Distribution SystemSDR AALA202508293112Power Supply · fault messageAIRCRAFT WAS NOT GROUNDED: EPSU SYS TEST FOR PS CHECK SHOWS 13WL FAULT. MAINTENANCE REPLACED EPSU 13WL IAW AMM 33-51-38 OPS CHECK GOOD.Aug 26, 2025 · N660AW · Airbus A320232 · Emergency LightingSDR YENA2025082800891Apu · odorFLT#2101, JFK-CHS. "WHILE CRUISING AT FL 340 FLIGHT CREW EXPERIENCED AN ODOR SIMILAR TO A MAGIC MARKER IN THE COCKPIT THAT DEVELOPED INTO BURNING EYES AND THROAT. FA#1 INFORMED THE CA PAX WERE FEELING SICK WITH BURNING THROAT AND ONE VOMITING,. PHYSICAL SYMPTOAug 26, 2025 · N658JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR CALA2025082808218Gauge · out of positionDOOR 2L SLIDE PRESS GAUGE OSCURED AND HARD 2 READ. UNSURE OF PR ESS DOOR 2L SLIDE PRESS GAUGE CLEARLY VISIBLE AND WITHIN RANGE REF AMM TASK 25-62-00-210-001-AAug 26, 2025 · N490UA · Airbus A320232 · Emergency EquipmentSDR CALA2025082708196Seat Track · corrodedCABIN FLOOR STRUCTURE L/H SEAT TRACK Y254 CORRODED AT FRS 21, 22 , 23. REMOVED AND REPLACED SEAT TRACK Y254 FR 12-24 LH IAW A320 SRM 51 -72-11-911-001 AND SRM 51-42-11 ACMP BY MECH V937285 INSP BY V89 2429Aug 26, 2025 · N467UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025082708195Seat Track · corrodedSEAT TRACK AT FR58 Y765 UPPER FLANGE CROWN GOUGED. REMOVED SEAT TRACK FR58-FR64 Y765 IAW A320 SRM 53-41-15-300-003 REV 154 REPLACED SEAT TRACK FR58-FR64 Y765 IAW A320 SRM 53-41-15 -300-003 REV 154.Aug 26, 2025 · N467UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025082808238Hydraulic System · leakingHYD Y SYS LO LVL ECAM APPEARED AFTER TAKEOFF. CREW STATED THEY LOST YELLOW SYS ON TAKEOFF. SHUT YELLOW HYD ELECT PUMP OFF IMMEDIATELY. FLT WAS JUST OVER A HOUR. CONFIRMED YELLOW SYS EMPTY ON LOWER SERVICE PANEL QTY GAUGE & ON PANEL. MET ACFT ON TAXIWAY, ACFT Aug 25, 2025 · N463UA · Airbus A320232 · Hydraulic System, MainSDR CALA2025082708192Floor Support · corrodedFWD CARGO COMPT, FRAME 28 STR33 LH TO 33 RH FLOOR PROFILE PANEL HAS CORROSION. REMOVED AND REPLACED FWD CARGO PROFILE PANEL AT FR28 STR33 LH TO 33 RH IAW A320 SRM 51-42-11.Aug 25, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025082708191Floor Support · corrodedAFT CABIN WET AREA FLOOR BEAM Y765 FR 66-70 L/H HAS CORROSION. REMOVED CORRODED FLOOR BEAM AND REPLACED WITH NEW FLOOR BEAM AT Y765 FR 66-70 LH IAW A320 SRM 51-42-11/001.Aug 25, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025082600880A/C Pack · odorFLT#373, BOS-AUA. PERSISTENT OIL SMELL ODOR ROW 20 AND AFT WITH PACK 1+2 ON ( PACKS ); COMPLIED WITH INFORMATION NOTICE 2017-T015, SECTION B2. IDENTIFIED ODOR TO APU (FOUND OIL IN INLET, LOAD COMPRESSOR & DRAIN). DECONTAMINATION LEVEL "A" WAS ACCOMPLISHED PEAug 25, 2025 · N659JB · Airbus A320232 · Air Distribution SystemSDR GTIA2025082539055Megaphone · no testFWD MEGAPHONE NOT WORKING. REMOVED AND REEPLACED MEGAPHONE IAW AMM 25-65-01. OPS CHECK GOOD.Aug 25, 2025 · N646NK · Airbus A320232 · Emergency EquipmentSDR YENA2025082500877Unknown · odorFLT 1962, PBI-LGA, DURING CLIMB, STRONG PERSISTENT & INCREASING INDICATION OF OIL FUMES. LEVEL 3 DETERMINED USING FOM AND ISOLATION CHECKLIST. PACK 1 ISOLATED. CAPTAIN & FO AFFECTED. IRRITATED BURNING EYES, SCRATCHY THROAT, HEAVY RAIN DURING TAKEOFF AND CLIMAug 24, 2025 · N715JB · Airbus A320232 · Air Distribution SystemSDR CALA2025082708178Warning Light · false activationFWD CARGO DOOR ECAM ON LANDING ROLLOUT PLACING BACK ON MEL BECAUSE OF EXTENSIVE HISTORY. REQUESTING MEL 5270J NOC MEL 5270J APPROVED PLA APPLIED. DDP C/W. *DM* AWM 31-54-46 INSPECT WIRES TO PROX SWITCH FOR CONDITION. CHECK WIRES WITHIN HARNESS 4613VB. ALSO SEEAug 23, 2025 · N430UA · Airbus A320232 · Door Warning SystemSDR CALA2025082708164Elec Connector · disconnectedROW 38 ABC ON SEAT EMERGENCY LIGHT INOP FOUND CONNECTOR ON SEAT DISCONNECTED, RECONNECTED & PERFORM EMERGENCY LIGHTING TEST PER AMM 33-51-00-710-804-A, OPS TEST GOODAug 23, 2025 · N484UA · Airbus A320232 · Light System WiringSDR CALA2025082508087Rivet · missingSERVICE CHECK EXTERIOR WALK-AROUND PROCEDURE - 2, MISSING RIVETS ON CNA T/E, 12 CLOCK POSITION OF FWD ROW ON INNER SKIN SIDE. .NO OTHER RIVETS FELT OR LOOK LOOSE. REPLACED THE CNA AS PER EC/RA: 7811-01400 STEP: G.1. OKAY FOR 78-DIP FOR ENG 1 CNA TRAILING EAug 23, 2025 · N446UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR CALA2025090208387Skin · dentedUPPER FUSELAGE DENT APROX .5" FWD OF FR 12 & 1" ABOVE STGR 1L. PERFORMED A DOUBLER REPAIR TO EXTERNAL SKIN AT LOCATION OF DAMAGE FR12 STRG 1L IAW SRM 53-11-11-300-054. THIS IS A CATEGORY B REPAIR.Aug 22, 2025 · N438UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR AALA202508257255Light · no testAIRCRAFT WAS GROUNDED: ROW 17 ABC AISLE EMERGENCY LIGHT INOP. MAINTENANCE REPAIRED WIRING IAW ESPM 20-48-14 OPS CHECK NORMAL IAW 33-51-11.Aug 22, 2025 · N656AW · Airbus A320232 · Emergency LightingSDR AALA202508254549Sign · inoperativeAIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHT BURNED OUT AIRCRAFT RIGHT SIDE AT THE OVERWING EXIT. MAINTENANCE REPLACE RH EMER DOOR EXIT SIGN IAW AMM 33-51-15.Aug 22, 2025 · N656AW · Airbus A320232 · Emergency LightingSDR CALA2025082508081Power Supply · no testEMERGENCY LIGHTING TESTS SHOWS THE FOLLOWING FAULTS: EPSU COMM FWD L, EPSU COMM AFT L, EPSU ARMED/ON EMER R, EPSU ARMED/ON L. T/S & FOUND FAULTY FWD ESPU 10WL IAW TSM 33-51-00-810-806A. REMOVED & REPLACED ESPU 10WL IAW AMM 3-51-38-000-001A & 33-51-3 4-400-00Aug 22, 2025 · N478UA · Airbus A320232 · Emergency LightingSDR YENA2025082200869A/C Pack · odorFLT# 696, ATL-BOS. PACK 1 FUME EVENT ON TAKE OFF PACK 1 SECURED IAW FCOM CH 7, OPENAug 22, 2025 · N656JB · Airbus A320232 · Cabin Cooling SystemSDR CALA2025082708188Seat Track · corrodedR/H WET AREA SEAT TRACK -1292 AT FR64-66 IS CORRODED. REMOVED SEAT TRACK, -1292 FR 64-66 IAW A320 SRM 51-42-11/0 01 REV 154 REPLACED BEAM-SEAT TRACK -1292 FR64-66 IAW A320 SRM 5 1-42-11/001 REV 154Aug 21, 2025 · N467UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025082508094Frame · crackedRH FRAME 16 DOUBLE JOGGLE FASTENER HOLE #6 HAS A CRACK INDICATION IN THE FRAME LAYER, AT 1 OCLOCK (VIEWED FROM THE OUTSIDE) 60% S.H. ACCOMPLISHED INTERIM REPAIR AT RH FR 16 DBL JOGGLE HOLE # 6 IAW ECRA 5311-03392 PART 1.1. ACCOMPLISH INITIAL INSP OF RH FR16 DAug 21, 2025 · N477UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2025082508078Support Angle · crackedEXTERNAL RT FUSELAGE FAIRING OUTER VERTICAL SUPPORT AT FR 34 IS CRACKED. REMOVED AND REPLACED FR 34 VERTICAL ANGLE IAW SRM 51-42-11 P 18-25.Aug 21, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025082200866Oil Cooler · failedFLT# 814, FLL-HPN(DIVERTED TO MCO).EXCESSIVE OIL CONSUPTION OBSERVED IN #1 ENGINE .5 QTS EVERY 4 MIN. LANDED 1.5 QTS 7.0 QTS AFTER ENGINE SHUTDOWN. OIL PRESSURE WAS 250-260 PSI; RAR IDG DRIVE SEAL ASSY IAW AMM 72-60-28. OPC GOOD AT THIS TIME NO LEAKS NOTED. REAug 21, 2025 · N760JB · Airbus A320232 · Turbine Engine Oil SystemSDR YENA2025082200865Ecs · contaminatedFLT # 2051. BOS-MCO. LEVEL 2 PERSISTANT ENVIROMENTAL SYSTEM ODOR IN FLIGHT DECK AND FWD CABIN (OBSERVED BY 3 CREWMEMBERS) CAUSING EYE IRRITATION. SMELL SIMILAR TO DIRTY SOCKS. APU AND PACKS ON. NO EXTERNAL AIR CONNECTION.; COMPLIED WITH INFO NOTICE 2017 - T15 Aug 21, 2025 · N520JB · Airbus A320232 · Cabin Cooling SystemSDR CALA2025082208046Battery · faultedBITE FAULT: EPSU BATTERY EMER R REPLACED EPSU BATTERY AT POSITION BATT. EMER R IAW AMM 33-51-38, OPS TEST GOOD.Aug 21, 2025 · N466UA · Airbus A320232 · Emergency LightingSDR CALA2025082208045Battery · faultedBITE FAULT: AFT L REPLACED EPSU BATTERY AT POSITION AFT L IAW AMM 33-51-38, OPS TEST GOOD .Aug 21, 2025 · N466UA · Airbus A320232 · Emergency LightingSDR CALA2025082108013Floor Support · corrodedAFT CABIN WET AREA FLOOR SUPPORT -Y765 RT FR 66-70 SHOWS EVIDENCE OF CORROSION. R & R THE FLOOR SUPPORT IAW SRM 51-42-11/001, REV 154.Aug 20, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025082108012Floor Support · corrodedMAIN CABIN AFT WET AREA FLOOR SUPPORT AT FR 68-69 LT Y1292 IS CORRODED. R & R THE FLOOR SUPPORT IAW SRM TASK 51-72-11-911-001.Aug 20, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025082108011Floor Support · corrodedCABIN FLOOR AFT WET AREA AT FR68-70 L/H FLOOR SUPPORT Y254 IS CORRODED. R & R THE FLOOR SUPPORT IAW SRM 51-42-11/001, REV 154.Aug 20, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025082108010Shear Plate · corrodedSHEAR PLATE AT L/H FR69-70 WET AREA HAS SHEARED FASTENERS & POSS IBLE CORROSION. REMOVED AND REPLACED SHEAR PLATE AT LH FR 69-70 WET AREA IAW A32 0 SRM TASK 51-72-11-911-001.Aug 20, 2025 · N467UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025082000853Unknown · odorFLT # 944, BZN-JFK. ODRO EVENT ON DESCENT OUT OF 11,000 FEET UNTIL LANDING SMELL DESCRIBED AS A CHEMICAL SMELL, BOTH FORWARD AND AFT CABIN; RAN APU, ENG 1 & ENG 2 WITH BOTH PACKS ON, NO ODOR NOTED, A/C OK FOR SVCAug 20, 2025 · N658JB · Airbus A320232 · Air Distribution SystemSDR YENA2025082100859Frame · damagedDURING HEAVY MAINTENANCE, PARTIAL REPLACEMENT OF FRAME 16 IAW TC A23-042-02. PERFORMED PERMANENT REPAIR WITH PARTIAL REPLACEMENT TO FRAME 16, S8R - 13R IAW SRM 51-42-11, DWG R531-13279-002, ISSUE E, AND EC A23-042-02.Aug 19, 2025 · N627JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2025082100858Frame · deformedDURING HEAVY MAINTENANCE: DEFORMATION ON FRAME 74 BTW STR 20R TO STR 20L AREA REAR FUSELAGE ; REMOVED AND REPLACED FRAME 74 LOC. BTW STR20R TO STR 20L AREA REAR FUSELAGE I.A.W A320 SRM 51-42-11, A320 SRM 51-72-11 AND DRAWING D53572510.Aug 19, 2025 · N627JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2025082100857Bushing · looseDURING HEAVY MAINTENANCE: SECONDARY FINDINGS LOOSE REPAIR BUSHING (1 EA), LOCATED BETWEEN RIB 16 TO RIB 17 FUEL TAN K AREA LH WING.; (RESOLVED ON W/O: 1391229 TASKCARD: NR-00039 ) PERFORMED BUSHING HOLE REPAIR AND REPLACED BRIDGING PLATE LOCATED BTW RIB16 TO RAug 19, 2025 · N627JB · Airbus A320232 · Wing Main, Frame Structure
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