Airbus A320-232

Service difficulty reports · 32,653

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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 YENA2021102500715Battery · failedFLT 2080, FLL-DCA. FWD ENTRY DOORS EMERGENCY EXIT LIGHTS NOT COMING ON ; R/R EMERGENCY LIGHT BATTERY AT FWD EPSU IAW AMM 33-51-38, LIGHTS OPERATE NORMALLY NOW.Oct 22, 2021 · N554JB · Airbus A320232 · Emergency LightingSDR CALA2021102501958Bulkhead · noneLH FR 68 #1L X4 DOOR STOP FITTING MOUNT HOLES IN FRAME HAVE AN OUT OF ROUND INDICATION, AS PER NTM 51-10-01-250-801-A-01, SUBTAS K 51-10-1-253-001-A, ITEM C. (7)(C) TABLE 5. DOT #11-07 - EA 534 0-01724 002 - NR 9294294 (28294) GENERATED BY V062335 AT HAECO L COct 22, 2021 · N436UA · Airbus A320232 · Fuselage Main, FrameSDR YENA2021102100710Battery · failedFLT # 2080, FLL-DCA. FWD ENTRY DOORS EMERGENCY EXIT LIGHTS NOT COMING ON ; R/R EMERGENCY LIGHT BATTERY AT FWD EPSU IAW AMM 33-51-38, LIGHTS OPERATE NORMALLY NOW.Oct 22, 2021 · N554JB · Airbus A320232 · Emergency LightingSDR CALA2021102201956None · none(A3NB-53-3-6222) FLOOR BEAM -Y765 BETWEEN FR 66/70 HAS CORROSIO N. DOT 52-40 () REMOVED AND REPLACED FLOOR BEAM BETWEEN FR66 TO 70 AT -Y765 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V933438 AT BFM ST AEROSPA CE MOBILE. NR 0015803Oct 22, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2021102201955None · missingPDA 3 RIGHT LANDING LIGHT BULB AND RETAINING RING MISSING AFTER LANDING AT MSY, LIGHT ASSEMBLY REPLACED REPLACED LANDING LIGHT ASSYOct 22, 2021 · N448UA · Airbus A320232 · Lighting SystemSDR CALA2021102201952None · failedFLIGHT CREW REPORTED VIA AIRINC L/G DOOR NOT CLOSED FAULT ON ECAM, FLIGHT CREW ATTEMPTED TO RECYCLE GEAR AS CALLED OUT FOR IN QRH FAULT REMAINED. NLG DOOR UPLOCK ACTUATOR LEAKING. REMOVED NOSE GAER UPLOCK ACTUATOR REF AMM 32-31-14-000-002-A. PULLED AND COLLAREOct 22, 2021 · N404UA · Airbus A320232 · Landing Gear SystemSDR AALA202111105191Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER BETWEEN FR 64 AND FR 67 AT S31R. REPLACED STRINGER PER SRM 51-42-11.Oct 21, 2021 · N649AW · Airbus A320232 · Fuselage Main, Longeron/StringerSDR AALA202110254144Panel · crackedAIRCRAFT IN BASE MAINTENANCE: R2 DOOR FLAP ASSEMBLY PANEL CRACKED. REPAIRED DOOR FLAP ASSEMBLY PANEL PER AMM 25-20-00-340-803-A.Oct 21, 2021 · N679AW · Airbus A320232 · Passenger/Crew DoorsSDR AALA202110222416Power Supply · faultyAIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT LIGHTS STAY ON WITH EMERGENCY EXIT SWITCH OF FLIGHT ATTENDANT PANEL AND COCKPIT IN OFF POSITION. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (11WL) PER AMM 33-51-38.Oct 21, 2021 · N647AW · Airbus A320232 · Emergency LightingSDR YENA2021102100712Web · corrodedDURING HEAVY MAINTENANCE, FROM AEROMAN NR 2021-428652 CORROSION WEB LOCATED BTW FR 69 TO FR 70 STRG 23R AT AFT GALLEY AREA ( CPCP RELATED 534195-01) ; (RESOLVED ON W/O: 1121241 TASK CARD: NR-00015) FROM AEROMAN NR 2121-428652, WORK DONE BY H.MENDEZ 8601415, RIOct 21, 2021 · N594JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2021102100711Web · corrodedDURING HEAVY MAINTENANCE, FROM AEROMAN NR 2021-428652 CORROSION WEB LOCATED BTW FR 69 TO FR 70 STRG 23R AT AFT GALLEY AREA ( CPCP RELATED 534195-01)Oct 21, 2021 · N594JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2021102201951Beam · noneA3NB-53-3-6038 CABIN FWD FLOOR STRUCTURE SUPPORT BAM HAVE CORROS ION FR20 Y254 DOT 42-047 () REPLACED SUPPORT BAM P/N D5311146100200 BATCH:0003854609 IAW A32 0 SRM 51-42-11 AND SRM 51-72-11-911-001. Y254 BETWEEN FR 12 TO F R 24. ACCOMPLISHED BY EMP#V935834 AT Oct 21, 2021 · N486UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021102201950Beam · none(A3NB-53-3-6222) FLOOR BEAM Y254 BETWEEN FR 66/68 HAS CORROSION DOT 52-39 REMOVED AND REPLACED FLOOR BEAM Y254 BETWEEN FR 66/68 P/N D53472 17320100 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V935833 AT S T AREORSPACE MOBILE. NR#0015802Oct 21, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2021102201949Seat Track · noneA3NB-53-3-6038 CABIN FLOOR SEAT TRACK Y-1292 FR20 HAVE WEAR MARK S AND GOUGES. DOT 42-053 EVALUATED FLOOR BEAM IAW SRM A320 53-00-15-283-002 FOUND OUT OF LIMITS, REPLACED BY NEW FLOOR BEAM PN:D5311278220201 BATCH:00038 6549, REPLACED IAW A320 SRM 51-42-11-001.Oct 21, 2021 · N486UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021102201948Beam · none(A3NB-53-3-6222) FLOOR BEAM -Y765 BETWEEN FR 66/70 HAS CORROSIO N. DOT 52-40 () REMOVED AND REPLACED FLOOR BEAM BETWEEN FR66 TO 70 AT -Y765 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V933438 AT BFM ST AEROSPA CE MOBILE. NR 0015803Oct 21, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2021102201947Beam · crackedLH FRAME 43 FOOT AFT INBOARD ATTACHMENT HOLE IS CRACKED IN THE C ENTER WING BOX UPPER MOST LAYER AT 2:00 - SUPPORT TASK AD 2020-1 8-06 - NR 9294751 (28751) GENERATED BY V061633 AT HAECO LCQ. REPLACED FRAME AND REAMED HOLE TO .4060 TO REMOVE INDICATION IAW EC/ROct 21, 2021 · N436UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR GTIA2021102136063None · noneAFT MEGAPHONE INOP.-R/R AFT MEGAPHONE IAW SPIRIT DRAWING NO. A320-EMER EQUIPMENTOct 21, 2021 · N620NK · Airbus A320232 · Escape SlideSDR YENA2021102100708Apu · odorFLT # 648, SLC-BOS. FA'S STATED THAT MUSTY FUMES WERE PRESENT IN THE MID TO AFT CABIN DURING LOW ALT DESCENT AND REMAINED UNTIL THE ENGINES WERE SHUT DOWN ; DETERMINED APU TO BE AT FAULT FOR CABIN ODOR. REFERENCE LP 3242713 ITEM 1 FOR APU DEFECT. DECONTAMINATIOct 20, 2021 · N563JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR CALA2021102201946None · noneAFT CARGO FR50 STRGT41RT STRINGER CORRODED. GENERATED BY N078592 ON HAECO LCQ NR 9294560/28560 0-13-205-002 TABLE 5 INSPECTION THRESHOLD FROM TIME OF EMBODIMEN T FC 60,000 OR FH 120,000 WHICHEVER VALUE IS ACHIEVED FIRST. SUB SEQUENT INSPECTIONS TBD. INSPECTIONOct 20, 2021 · N436UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021102201945None · weakFORWARD EMERGENCY LIGHTS BATTERY PACK 10WL FAILS TO ILLUMINATE W ITH THE CONTROL SWITCH IN ARM AND C/B''S PULLED - SUPPORT TASK - NR 9294241 (28241) GENERATED BY V061627 AT HAECO LCQ. REMOVED AND REPLACED 10WL EPSU BATTERY AND OP CHECKS GOOD IAW A3 20 AMM 33-5Oct 20, 2021 · N436UA · Airbus A320232 · Lighting SystemSDR CALA2021102201944Fitting · crackedPER NR 9292941/26941 LH WING TE SPAR AILERON ATTACH FITTING IS C RACKED. GENERATED BY V061680 ACP RPR ON LH WING TE SPAR AILERON ATTACH FITTING SUPPORT DIAPHR INSP V077960 AM LOWER IB AFT FLANGE PER HAECO REO-L23461 REV A PART 3 WITH N O DEVIATIONS ACP RMVL AOct 20, 2021 · N441UA · Airbus A320232 · Wing, Attach FittingsSDR CALA2021102201942None · weakEMERGENCY LIGHTS FAIL TO ILLUMINATE FOR THE BATTERY PACKS AT THE BATTERY PACKS AT THE L/H AND R/H OVERWING (11WL & 12WL) WITH THE CONTROL SWITCH IN ARMED AND THE C/B''S PULLED - SUPPORT TASK - N R 9294239 (28239) GENERATED BY V061627 AT HAECO LCQ. REMOVED AND Oct 20, 2021 · N436UA · Airbus A320232 · Lighting SystemSDR CALA2021102201941Fitting · corrodedL2 DOOR LOWER AFT CORNER FITTING HAS CORR. PER HAECO LCQ NR 9294 490/28490. GENERATED BY V061334 REMOVED AND REPLACED WITH NEW L-2 DOOR LOWER AFT CORNER FITTING A320 UAL SRM 51-42-11-001. PER MECH V061737. REMOVED AND REPLACED WITH NEW L-2 DOOR LOWER AFT CORNEOct 20, 2021 · N436UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2021102201940Fitting · corrodedL2 DOOR LOWER AFT CORNER FITTING HAS CORR. PER HAECO LCQ NR 9294 490/28490. GENERATED BY V061334 REMOVED AND REPLACED WITH NEW L-2 DOOR LOWER AFT CORNER FITTING A320 UAL SRM 51-42-11-001. PER MECH V061737. REMOVED AND REPLACED WITH NEW L-2 DOOR LOWER AFT CORNEOct 20, 2021 · N436UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2021102001936Floorbeam · corrodedA3NB-53-3-6038 CABIN FWD FLOOR STRUCTURE SUPPORT BAM HAVE CORROS ION FR20 Y254 DOT 42-047 () REPLACED SUPPORT BAM P/N D5311146100200 BATCH:0003854609 IAW A32 0 SRM 51-42-11 AND SRM 51-72-11-911-001. Y254 BETWEEN FR 12 TO F R 24. ACCOMPLISHED BY EMP#V935834 AT Oct 20, 2021 · N486UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021102001935None · none(REPAIR BEFORE NEXT FLT) ROTO PROBE OF LH FR16 #7 DOOR STOP FITT ING HOLES FOUND CRACKS AT THE I/B UPPER AND I/B LOWER HOLES. CRA CKS ARE IN THE INTERCOSTAL ONLY. () REPAIRED L/H FR16 #7 DOOR STOP FITTING HOLES BY REPLACING INTERC OSTAL FITTING ON EC/RA 5311-0Oct 20, 2021 · N486UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021102001934Floorbeam · corroded(A3NB-53-3-6222) FLOOR BEAM Y254 BETWEEN FR 66/68 HAS CORROSION DOT 52-39 REMOVED AND REPLACED FLOOR BEAM Y254 BETWEEN FR 66/68 P/N D53472 17320100 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V935833 AT S T AREORSPACE MOBILE. NR#0015802Oct 20, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR GTIA2021102136062None · noneAFT F/A FLASH LIGHT HOLDER BROKEN R2 POS ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R&R R2 F/A FLASHLIGHT IAW CMM 25-60-13. THHIS CLEARS DMI # 287357601. PLACARD REMOVED. DMI LOG UPDATED. MOC NOTIFIED.Oct 19, 2021 · N697NK · Airbus A320232 · Escape SlideSDR AALA202111107895Hinge Arm · gougedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER #5 HINGE ARM UPPER SURFACE HAS WORN / GOUGED AREA. REPAIRED HINGE ARM PER EA 331564.Oct 18, 2021 · N649AW · Airbus A320232 · Horizontal Stabilizer StructureSDR AALA202110292366Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #12 UPPER AFT ATTACHMENT BOLT BETWEEN WS13464 AND WS14459, BETWEEN RIB 25 TO RIB 27. REPLACED BOLT PER AMM 27-84-64-400-002-A.Oct 18, 2021 · N649AW · Airbus A320232 · Leading Edge DevicesSDR AALA202110283974Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #5 LOWER ATTACHMENT BOLT BETWEEN WS5512 AND WS6699, BETWEEN RIB 10 TO RIB 12. REPLACED BOLT PER AMM 27-84-64-400-002-A.Oct 18, 2021 · N649AW · Airbus A320232 · Leading Edge DevicesSDR AALA202110274658Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORRODED AREA FOUND ON FLOOR BEAM Y1162.5. LENGTH = 0.446 INCHES, WIDTH = 0.306 INCHES, DEPTH = 0.025 INCHES. REPLACED FLOOR BEAM Y1162.5 LOCATED FROM FR68 TO FR69 AT AFT GALLEY AREA PER SRM 51-72-11-911-001.Oct 18, 2021 · N652AW · Airbus A320232 · Fuselage Main, Floor BeamSDR GTIA2021102136059None · inoperativeWX RADAR INOP.-R&R TRU (13SQ1) OPS CHECK OK REF AMM 34-41-51Oct 18, 2021 · N692NK · Airbus A320232 · Inertial Guidance SystemSDR YENA2021101900683Outflow Valve · fault messageFLT # 501, BOS-MSY(AIR RETURN BACK TO BOS). VENT BLOWER FAULT ECAM DURING FLIGHT , SKIN AIR OUTLET VALVE ( SKIN AIR OUTLET VALVE ) ; RESET AVEC C/B'S PER AMM 21-26-00. NO FAULTS., (ITEM RESOLVE UNDER MDDR: 452866) REM/REP SKIN OUTLET VALVE REF AMM 21-26-53.Oct 18, 2021 · N789JB · Airbus A320232 · Air Distribution SystemSDR AALA202111307981Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON SHEAR PLATE LOCATED AT FR69 AND STR 23R. LENGTH= 0.929 IN. REPLACED SHEAR PLATE AT AFT GALLEY AREA PER SRM 51-42-11-801.Oct 17, 2021 · N652AW · Airbus A320232 · Fuselage Main, Plate/SkinSDR AALA202111160095Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: AFT GALLEY AREA CRACKED SHEAR PLATE LOCATED FROM FR 69 TO FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11-911-001, SRM 51-42-11-801 AND DWG D53470100.Oct 17, 2021 · N652AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202111161283Dummy Rail · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD GALLEY AREA RAIL DUMMY LOCATED AT LEVEL FR 16 AND Y503.2. REPLACED RAIL DUMMY PER SRM 51-72-11-911-001 AND DRAWING D53112825.Oct 17, 2021 · N652AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202111094265Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM BETWEEN FR 12 AND FR 24 AT +Y765. REPLACED FLOOR BEAM PER SRM 51-42-11.Oct 17, 2021 · N652AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202111020245Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION, MEASURING L=0.914 IN, W=0.646 IN, D=0.047 IN, ON AFT GALLEY AREA FLOOR BEAM LOCATED BETWEEN FR 68 TO FR 70 AT -Y160.5. REPLACED FLOOR BEAM PER SRM 51-42-11-801, SRM 51-72-11-911-001 AND DRAWINGS D21270904, D53472000.Oct 17, 2021 · N652AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202111020141Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION, MEASURING L=1.666 IN, W=0.988 IN, D=0.025 IN, ON AFT GALLEY AREA FLOOR BEAM LOCATED BETWEEN FR 64 TO FR 66 AT -Y765. REPLACED FLOOR BEAM PER SRM 51-72-11-911-001, SRM 51-42-11-801, AND DWG D53472000, D53472816.Oct 17, 2021 · N652AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202110298959Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 70 AND -Y765. REPLACED FLOOR BEAM PER SRM 51-72-11Oct 17, 2021 · N652AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202110276502Coupling · corrodedAIRCRAFT IN BASE MAINTENANCE: CORRODED AREA FOUND ON COUPLING LOCATED AT STA FR68 AND RIGHT BUTT LINE -Y-1162.5. LENGTH = 1.22 INCHES, WIDTH = 0.650 INCHES, DEPTH = 0.065 INCHES. REPLACED SPLICE LOCATED INBOARD UPPER POSITION AT FR 68 AND -Y1162.5 RIGHT SIDE AOct 17, 2021 · N652AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202110271452Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORRODED AREA FOUND ON FLOOR BEAM Y1292 LOCATED AT FR66, LEFT BUTT LINE Y1292. LENGTH = 0.935 INCHES, WIDTH = 0.611 INCHES, DEPTH = 0.044 INCHES. REPLACED FLOOR BEAM Y1292 LOCATED FROM FR64 TO FR66 AT AFT GALLEY AREA PER SRM 51-72Oct 17, 2021 · N652AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202110277348Coupling · corrodedAIRCRAFT IN BASE MAINTENANCE: CORRODED AREA FOUND ON COUPLING LOCATED AT FR66, RIGHT BUTT LINE Y765. LENGTH= 1.120 INCHES, WIDTH= 0.640 INCHES, DEPTH= 0.068 INCHES. REPLACED SPLICE LOCATED INBOARD UPPER POSITION AT FR 66 AND -Y765 PER SRM 51-72-11-911-001.Oct 17, 2021 · N652AW · Airbus A320232 · Fuselage Main, StructureSDR GTIA2021101836054None · noneL1 AND R2 DOOR ASSIST ACCUMULATORS REQUIRES SERVICE.-L1 AND R2 DOORS WERE SERVICED IAW AMM 52-10-00Oct 17, 2021 · N603NK · Airbus A320232 · Passenger/Crew DoorsSDR CALA2021101801918Stringer · corrodedCORROSION ON AFT CARGO COMPT BILGE AREA, FR56, STRINGER 41L SPLICE AT FR52. RECEIVED NEW STRINGER D5347042020800, BATCH INITIAL INSPECTION TO OCCUR 60,000 FC OR 120,000 FH FROM REPAIR # 0003843117, AND REPAIR COUPLING R5307111220800, BATCH EMBODIMENT AND SUBSEOct 17, 2021 · N495UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2021101801917Intercostal · cracked(REPAIR BEFORE NEXT FLT) ROTO PROBE OF LH FR16 #7 DOOR STOP FITT ING HOLES FOUND CRACKS AT THE I/B UPPER AND I/B LOWER HOLES. CRA CKS ARE IN THE INTERCOSTAL ONLY. ()Oct 17, 2021 · N486UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021101801916None · noneLARGE LAVATORY SPILLAGE DETECTED 10/16/2021 FROM FWD BULKHEAD TO APB BELOW AFT CARGO FLOOR PANELS DRIPPING FROM BILGE DRAIN BELOW AFT CARGO DOOR COMING FROM WASTE DRAIN VALVE UPPER FLANGE. WASTE DRAIN VALVE REPLACED THIS CHECK ON N/R 000463110.Oct 17, 2021 · N489UA · Airbus A320232 · Water and Waste SystemSDR CALA2021101801915Intercostal · cracked(REPAIR BEFORE NEXT FLT) ROTO PROBE OF RH FR16 #7 DOOR STGOP FIT TIING HOLE FOUND CRACKS AT THE I/B TOP AND I/B BOTTOME HOLES. CR ACKS ARE IN THE INTERCOSTAL ONLY. ()Oct 17, 2021 · N486UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021101801914Beam · corroded(A3NB-25-3-6221) FLOOR BEAM Y1162.5 BETWEEN FR 68/69 HAS CORROSI ON. DOT 52-32 () REMOVED AND REPLACE FLOOR BEAM Y1162.5 FR 68-69 AND HARD POINT I AW SRM 51-42-11. ACCOMPLISHED BY EMP#V933438 AT ST AEROSPACE MOB ILE. NR#0015797Oct 17, 2021 · N486UA · Airbus A320232 · Cabin Equipment/Furnishings
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