N632VA, cancelled Mar 26, 2024

Service difficulty reports · 46

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N632VA' AND deregistration_id = 'N632VA-2024-03-26'
  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 ASAA2024030248273Slide · unwanted deployRH OVERWING SLIDE DEPLOYED. GROUNDED - YES. REMOVED AND REPLACED RH OVERWING SLIDE S/N A156832 IAW A320 AMM 25-62-42-000-001-A AND AMM 25-62-42-400-001-A.Mar 2, 2024 · N632VA · Airbus A320214 · Escape SlideSDR ASAA2024011747371Unknown · unknownSMOKE IN COCKPIT DURING MANEUVERS AT APPROX 15,000 FT. HAD SLIGHT ELECTRICAL SMELL. RAN SMOKE EVACUATION CHECKLIST WHICH SEEMED TO RESOLVE THE ISSUE. MOST NOTICEABLE ON RIGHT SIDE UNDER F/O SLIDING WINDSCREEN. ALSO WAS NOTICEABLE IN MID TO AFT CABIN. GROUNDEDJan 12, 2024 · N632VA · Airbus A320214 · Windshield/Door Rain/Ice RemovalSDR ASAA2023083146146Floor Panel · puncturedAFT CABIN 251CF HAS REPAIR NOT LISTED IN REPAIR LISTINGS GROUNDED - YES. REPAIRED AFT MAIN CABIN FLOOR PANEL 251CF IAW A320 SRM 53-02-00-283-001 AND 53-02-00-300-001.Aug 31, 2023 · N632VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023083146144Floor Panel · puncturedAFT CABIN FLOOR PANEL 241JF HAS A REPAIR NOT LISTED IN REPAIR LISTINGS. GROUNDED - YES. ACCOMPLISHED REPAIR ON AFT CABIN FLOOR PANEL 241FJ IAW A320 SRM53-02-00-283-001 REV 145 AND SRM 53-02-00-300.0010 ZONE A.Aug 31, 2023 · N632VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023061743629Angle · corrodedACCESS DOOR 312AR FWD AT FUSELAGE FR71 AND DOOR JAMB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED DOOR JAMB ANGLE AT ACCESS DOOR 312AR AT FR71 IAW A320 SRM 51-42-11-001 REV 145.Jun 17, 2023 · N632VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA2023060644386Floorboard · delaminatedMAIN CABIN FLOOR BOARD 231FF HAS INSERT DAMAGE AT L/H. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR BOARD 231FF IAW A320 AMM 53-12-12-420-001-A.Jun 6, 2023 · N632VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023060544059Seat Track · wornMAIN CABIN SEAT INBD TRACK CROWN LATERAL AREA IS WORN AT FR42. GROUNDED - YES. REMOVED AND REPLACED SEAT TRACK P/N: D5337111000800 IAW A320 SRM 51-42-11/001 AND SRM 51-72-11-911-001 REV. 145 AT MAIN CABIN L/H INBD FR41 TO FR47 Y = 765.Jun 5, 2023 · N632VA · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2023060544058Seat Track · wornMAIN CABIN OUTBD SEAT TRACK CROWN LATERAL AREA IS WORN BETWEEN FR43 AND FR44. GROUNDED - YES. REMOVED AND REPLCAED MAIN CABIN SEAT TRACK BETWEEN FR41 AND FR47 Y=1292. P/N D5337111200400 IAW A320 SRM 51-42-11 AND SRM 51-72-11-911-001.Jun 5, 2023 · N632VA · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2023051846503Skin Panel · corrodedFOUND MULTIPLE AREAS OF CORROSION ON L/H WING TOP SKIN PANEL 2 T/E OVERHANG BETWEEN RIB 14-18 GROUNDED - YES. ACCOMPLISHED EA A320-57EA-01874 REV. 00 MINOR REPAIRMay 18, 2023 · N632VA · Airbus A320214 · Wing, Plate/SkinSDR ASAA2023051743345Door Sill · corrodedAFT CABIN R/H LWR SILL AT FR68 HAS CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" PERMANENT REPAIR ON AFT CABIN R/H LWR SILL AT FR68, Y=1732 IAW A320 SRM 53-41-14-300-001, REV 144.May 17, 2023 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2023051645209Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251RF HAS MISSING MATERIAL GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 251RF IAW A320 AMM 53-00-00-400-801-A AND 53-00-00-000-801-A.May 16, 2023 · N632VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023051345989Skin Panel · corrodedR/H WING TOP SKIN PANEL 2 T/E OVERHANG HAS EXTENSIVE CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY B PERMANENT REPAIR OF R/H WING TOP SKIN PANEL 2 TEOH RIBS 9-27 IAW ASA EA A320-57EA-0187 REV 00 AND AIRBUS RDAF 81250074/004/2023 ISSUE A DATED 25-OCT-2023.May 13, 2023 · N632VA · Airbus A320214 · Wing, Plate/SkinSDR ASAA2023051345909Skin Panel · corrodedL/H WING/TOP SKIN PANEL 2 TRAILING EDGE OVERHANG HAS EXTENSIVE CORROSION THROUGHOUT GROUNDED - YES. REPAIRED L/H WING TOP SKIN OVERHANG AT RIBS 9-27, STRINGER 16 IAW ASA EA A320-57EA-01874 REV 00 AND AIRBUS RDAF 81253170/031/2023 ISSUE A DATED 23-OCT-2023 CATEMay 13, 2023 · N632VA · Airbus A320214 · Wing Miscellaneous StructureSDR ASAA2023051345908Skin Panel · corrodedL/H WING/TOP SKIN PANEL 2 OVERHANG BETWEEN RIB 6 AND 27 CORROSION. GROUNDED - YES. REPAIRED L/H WING TOP SKIN TRAILING EDGE OVERHANG IAW ASA EA A320-57EA-01874 REV 00 AND AIRBUS RDAF 81253170/059/2023 ISSUE A DATED 24-OCT-2023 CATEGORY B PERMANENT REPAIR.May 13, 2023 · N632VA · Airbus A320214 · Wing Miscellaneous StructureSDR ASAA2023051345907Skin Panel · corrodedL/H WING/TOP SKIN PANEL 2/TRAILING EDGE OVERHANG BETWEEN RIB 6 AND 27 CORROSION. GROUNDED - YES. REPAIRED L/H WING/TOP SKIN PANEL 2 REAR SPAR AT RIB 15-18 IAW ASA EA A320-57EA-01874 REV 00 AND AIRBUS RDAF 81253170/060/2023 ISSUE A DATED 21-OCT-2023 CATEGORY BMay 13, 2023 · N632VA · Airbus A320214 · Wing, Plate/SkinSDR ASAA2023042046700Floor Panel · corrodedR1 DOOR THRESHOLD PLATE HAS RUST ON 3EA ATTACHING SCREW HOLES. GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 222FF AT FR16 TO FR20 P/N E5367147800700 IAW A320 AMM 53-12-12-400-001-AApr 20, 2023 · N632VA · Airbus A320214 · Fuselage Floor PanelSDR ASAA2023042043410Door Sill · corrodedAFT CARGO COMPARTMENT DOOR SILL UPPER SURFACE HAS CORROSION FROM FR55 TO FR56. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO COMPARTMENT DOOR SILL/THRESHOLD SHEET AT FR52A TO FR56, Y=-609.6 TO Y=-723.9 IAW A320 SRM 51-72-11-911-001.Apr 20, 2023 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2023042043333Web · corrodedAFT CARGO DOOR CUTOUT TORQUE BOX UPPER WEB IS CORRODED IN NUMEROUS AREA. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO DOOR CUTOUT TORQUE BOX WEB P/N: D5347556522200 AT FR52A TO FR56, STR 39R IAW A320 SRM 51-42--11/001 PARA. 2E AND 2F.Apr 20, 2023 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2023042043178Floor Support · corrodedAFT PIT FLOOR STRUCTURE HAS CORROSION FROM C56 TO C58 ON LEFT SIDE AFT LOOKING FWD. GROUNDED - YES. REMOVED AND REPLACED AFT PIT FLOOR SUPPORT AT FR56 TO FR58 STR37L TO STR38L IAW A320 SRM 51-42-11/001 REV. 144.Apr 20, 2023 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2023041543306Skin · corrodedR/H FUSELAGE ACCESS DOOR 312AR INNER SKIN IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED INNER SKIN ON ACCESS DOOR 312AR IAW A320 SRM 51-42-11-001Apr 15, 2023 · N632VA · Airbus A320214 · Service DoorsSDR ASAA2019041429230Shear Tie · corrodedMAIN CABIN FLOOR LEVEL BETWEEN FR69-FR70 STR23R LATERAL SHEAR TIE WEB CORRODED GROUNDED - YES. REMOVED CORRODED LATERAL SHEAR TIE WEB IN MAIN CABIN FLOOR LEVEL BETWEEN FR69-FR70 STR 23R (CORROSION WAS 100% MATERIAL LOSS PLUS 2 INCHES LENGTH) PER AIRBUS DWG 18DApr 14, 2019 · N632VA · Airbus A320214 · Fuselage Internal Mounting StructureSDR ASAA2019041429229Shear Tie · corrodedMAIN CABIN FLOOR LEVEL BETWEEN FR69-FR70 STR23R LATERAL SHEAR TIE WEB CORRODED GROUNDED - YES. REMOVED CORRODED LATERAL SHEAR TIE WEB IN MAIN CABIN FLOOR LEVEL BETWEEN FR69-FR70 STR23R (CORROSION WAS 100% MATERIAL LOSS PLUS 2 INCHES LENGTH) PER AIRBUS DWG 18D5Apr 14, 2019 · N632VA · Airbus A320214 · Fuselage Internal Mounting StructureSDR ASAA2019042382913Beam · corrodedMAIN CABIN LWR DOOR SILL SUPPORT AT R-2 DOOR, FWD OF FR68 HAS A CORRODED EXISTING REPAIR GROUNDED - YES. REMOVED DAMAGED REPAIR IAW A320 SRM 51-42-11. FABRICATED NEW REPAIR AND 2 EACH FILLERS IAW A320 SRM 53-41-14-300-001. INSTALLED REPAIR AND 2 EACH FILLERMar 28, 2019 · N632VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA2019032979147Web · corrodedMAIN CABIN FLOOR @ FR69-FR68 R/H OUTBOARD CUSP WEB CORRODED GROUNDED - YES. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW A320 SRM 53-41-14. ORIG .063 REMOVED .057 REMAINING .006. LOCATED AND DRILLED NEW WEB IAW A320 SRM 51-42-11. INSTALLED NEW WEB IAW A320 SMar 27, 2019 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2019042372998Door Sill · corrodedAFT PASSENGER/CREW RT/SIDE DOOR LOWER FWD GIRT BAR FITTING CORRODED. GROUNDED - YES. REMOVED CORROSION IAW A320 SRM 53-41-14-283-002. ORIG MAT .098, REMAINING MAT .069 MAT LOSS OF .029. REPAIRED AREA IAW A320 SRM 53-41-14-300-001. THIS IS A CATEGORY A REPMar 27, 2019 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2019042372991Door Frame · corrodedL1 DOOR LOWER FRAME AT GIRT BAR LOCATION FWD HAS CORROSION (MARKED IN RED) GROUNDED - YES. REMOVED CORROSION ON L1 LOWER DOOR FRAME AT FWD GIRT BAR PER A320 SRM 53-11-14-283-005, A320 SRM 51-74-00, A320 SRM 51-74-00. ORIG. THICK .197 REMAINING .181 REMOVED .01Mar 27, 2019 · N632VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA2019042372990Door Frame · corrodedR1 DOOR LOWER FRAME AT GIRT BAR304 LOCATION FWD AND AFT HAS CORROSION (MARKED IN RED) GROUNDED - YES. REMOVED CORROSION ON R1 DOOR LOWER FRAME AT FWD AND AFT GRIT BAR LOCATIONS PER A320 SRM 53-11-14-283-005, A320 SRM 51-74-00, A320 SRM 51-74-00. ORIG THICK .18Mar 27, 2019 · N632VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA2019042372989Floor Support · corrodedMAIN CABIN FLOOR @FR68 RBL30 BEAM UPPER SURFACE CORRODED GROUNDED - YES. REMOVED CORROSION OUT OF SRM 53-00-14 LIMITS - DAMAGE WAS 2" LONG - ORIG THK .150", REMAINING THK .130" REMOVED .020 ", REMOVED DAMAGED BEAM BETWEEN FR67-FR70 @ Y-765, LOCATED, DRILLED ANMar 27, 2019 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2019032729087Fitting · corrodedAFT PASSENGER/CREW LT/SIDE DOOR LOWER FWD GIRT BAR FITTING CORRODED. GROUNDED - YES. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW A320 SRM 53-41-174. ORIG .098 REMOVED .013. REMAINING .085. ALODINED AND PRIMED IAW A320 SRM 51-75-12. TOPCOATED IAW A320 51-75-1Mar 27, 2019 · N632VA · Airbus A320214 · Emergency EquipmentSDR ASAA20190429148Shear Tie · corrodedMAIN CABIN, AFT, LEFT SIDE, LATERAL SHEAR TIE STR 23L BETWEEN FRAME 69 AND 68 CORROSION GROUNDED - YES. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW A320 SRM 53-41-14. ORIG .065, REMOVED .058 REMAINING .005. REMOVED AND REPLACED WEB IAW A320 SRM 51-42-11 AND Mar 25, 2019 · N632VA · Airbus A320214 · Fuselage Internal Mounting StructureSDR ASAA2019042352912Beam · corrodedAFT MAIN CABIN, R-2 DOOR THRESHOLD. DOOR SILL SUPPORT BEAM CORROSION AFT END. GROUNDED - YES. BLENDED CORROSION IAW A320 SRM 53-41-14-283-002. ORIG MAT .071 REMAINING MAT .0. 100% MAT. LOSS. REPAIRED AREA IAW A320 SRM 53-41-14-300-001. THIS IS A CATEGORYMar 25, 2019 · N632VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA2019042352988Beam · corrodedAFT MAIN CABIN, FLOOR BEAM, BUTT LINE 8 L. JUST FORWARD OF FRAME 70, CORROSION ON TOP GROUNDED - YES. CORROSION LOCATED AT A HARD POINT AREA WHICH IS A EXCLUDED AREA REQUIRING BEAM REPLACEMENT, REF. A320 SRM 53-00-14-283-002, FIG 001 (SHT 1) REMOVED DAMAGED BEMar 25, 2019 · N632VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA201902529061Bracket · corrodedMAIN CABIN, AFT, LEFT SIDE, LATERAL SHEAR TIE STR 23L BETWEEN FRAME 69 AND 70 CORROSION GROUNDED - YES. REMOVED AND REPLACED MAIN CABIN AFT LEFT SIDE LATERAL SHEAR TIE, STR69-70 STR 23L IAW A320-DWG D53474180 - LATE ENTRY - REMOVED CORROSION ON SHEAR TIE IMar 25, 2019 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR ASAA2019042252957Support Beam · corrodedAFT MAIN CABIN, L-2 DOOR THRESHOLD. DOOR SILL SUPPORT BEAM CORROSION AFT END. GROUNDED - YES. BLENDED CORRODED AREA. ORIGINAL MAT. THICKNESS .071, REMOVED .016, REMAINING .055. FOUND TO BE OUT OF LIMITS AS PER SRM 53-41-14-283-002. FABRICATED REPAIR ANGLE IAWMar 25, 2019 · N632VA · Airbus A320214 · Fuselage Main, StructureSDR ASAA2018112617046Oil System · depletedON CLIMBOUT RECEIVED ENG 2 STALL ECAM MSG. IT WENT AWAY. 30 SECONDS LATER IT SHOWED UP AGAIN. THEN OIL QUANTITY WAS DEPLETING. ENG 2 FAILED FAIL ECAM THEN SHUT DOWN ENGINE TWO. GROUNDED - YES. EMERGENCY LANDING DECLARED - AOG IN SEANov 21, 2018 · N632VA · Airbus A320214 · Turbine Engine Oil SystemSDR 2013FA0000312Seat Track · corrodedFORWARD CABIN SEAT TRACK FROM FR12-24 AT Y765 HAD AN AREA OF CORROSION AT FR16 BEYOND LIMITS. EXTENT OF THE DAMAGE WAS 1" IN LENGTH X 2" IN WIDTH X .032 DEPTH. THE SEAT TRACK WAS REPLACED IAW SRM 51-42-11.Apr 14, 2013 · N632VA · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR 2013FA0000311Sill · corrodedRIGHT AFT PASSENGER DOOR SILL BETWEEN FR 66-68, ST 23-24 AT RBL 56 HAD AN AREA OF CORROSION BEYOND LIMITS. EXTENT OF DAMAGE WAS 1" IN LENGTH X 1" IN WIDTH X .050" DEPTH. THE DOOR SILL WAS REPAIRED IAW SRM 53-41-14, FIG 201, VIEW K, PRINCIPLE 5.Apr 11, 2013 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR 2013FA0000260Support · corrodedLEFT AFT SHEAR PLATE SUPPORT, FR 69-70, ST 23L-24L HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 2" L X 2" W X .020 DEPTH. SUPPORT BELOW A SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 51-42-11.Apr 10, 2013 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR 2013FA0000259Shear Plate · corrodedRIGHT AFT SHEAR PLATE BETWEEN FR 69-70, S23R HAS CORROSION BEYOND LIMITS. EXTENT OF DAMAGE 2" L X 2" W X .040 DEPTH. SHEAR PLATE WAS R & R IAW SRM 51-40-00 AND 51-42-11.Apr 10, 2013 · N632VA · Airbus A320214 · Fuselage Miscellaneous StructureSDR VQIA2012F00000Unknown · odor(APPROX 3.5 HRS INTO THIS FLIGHT) THE FLIGHT CREW "DETECTED STRONG CHEMICAL ODOR WHILE IN CRUISE, UNABLE TO DETERMINE ORIGIN, DIVERTED". THE FLT CREW DONNED 02 MASK AND DECLARED AN EMERGENCY WITH ENROUTE-ATC AND FOLLOWED PROCEDURES FOR A TPA DIVERSION. ONCE Jan 7, 2012 · N632VA · Airbus A320214 · Air Distribution SystemSDR VQI2012F00003Guide · out of positionAFTER THE FLIGHT, DURING THE TURN, IT WAS NOTED THAT THE L1 DOOR WOULD NOT REMAIN LOCKED OPEN. MX WAS AT THE STATION AND FOUND THE GUIDE AND BUSHING OUT OF POSITION, REF AIPC 52-11-01-09D, ITEMS 240 AND 260. THE 2 PARTS WERE RE-INSERTED AND THE DOOR UNLOCKINDec 22, 2011 · N632VA · Airbus A320214 · Passenger/Crew DoorsSDR VQI2012F00002Bushing · out of positionAFTER THE FLIGHT, DURING THE TURN, IT WAS NOTED THAT THE L1 DOOR WOULD NOT REMAIN LOCKED OPEN. MX WAS AT THE STATION AND FOUND THE GUIDE AND BUSHING OUT OF POSITION, REF AIPC 52-11-01-09D, ITEMS 240 AND 260. THE 2 PARTS WERE RE-INSERTED AND THE DOOR UNLOCKIDec 22, 2011 · N632VA · Airbus A320214 · Passenger/Crew DoorsSDR VQI2010F00001Actuator · unserviceableACFT WAS UNDERGOING A C2 CHECK. DURING THE ACCOMPLISHMENT OF MPD TASK CARD 274451-04-1, 2 DIFFERENT GREASE TYPES WERE FOUND. THE GREASES WERE WIPED CLEAN OFF THE TRIMMABLE HORIZONTAL STABILIZER ACTURATOR (THSA) AND JACKSCREW. FURTHER INSP REVEALED A METALLISep 10, 2010 · N632VA · Airbus A320214 · Elevator Control SystemSDR VQI2009F00003Engine · failedFLIGHT PUSHED BACK 6 MINUTES EARLY AT 1624Z AND TOOK OFF AT 1639Z. AT 1903Z, CUSTOMER SUPPORT CONTACTED MX, ADVISING THAT THE NR 1 ENG SHUTDOWN AT APPROX 1853Z. AT 1906Z MX SENT AN ACAR MESSAGE TO THE ACFT REQUESTING THE CONDITION OF THEIR ENG PARAMETERS WITNov 13, 2009 · N632VA · Airbus A320214 · Engine (Turbine/Turboprop)SDR 2009FA0000012Ecu · faultyFLIGHT 515 LAX TO JFK. DURING CRUISE 3 ECAM WARNINGS, THRUST LEVER FAULT, CTL VALVE FAULT, AND ENG2 FADEC A FAULT. AN ASSOCIATED LAND ASAP AMBER ECAM ADVISORY MSG ALSO APPEARED. CREW ADVISED DISPATCH THAT THEY WERE DIVERTING TO LAS. MX FOLLOWED THE TSM FORDec 30, 2008 · N632VA · Airbus A320214 · Fuel Control/Turbine EnginesSDR VQI2008F00005Unknown · odorFLT DIVERTED DUE TO ODOR IN CABIN AROUND SEAT ROWS 4 TO 7. AT ABOUT 10,000 FT & CLIMBING ODOR FIRST NOTICED BY FLT TEAM MEMBER & THEN DISAPPEARED. LATER, AT ABOUT 30,000 FT ODOR RETURNED. REPORTED IT TO BE LIKE ELECTRIC OR PLASTIC ODOR & THAT IT WAS STRONG. Oct 30, 2008 · N632VA · Airbus A320214 · Air Distribution System
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