Boeing 737-201

Service difficulty reports · 2,471

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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 = '737201'
  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 F3LA98026Stringer · corrodedPAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 14-R, BS 440-500, AND CRACK IN STRINGER 14-R, BS 440-448. MAINTENANCE REPAIRED CORRODED AREAS, PER SRM 51-30-2, 53-30-1,53-30-3 AND 51-40-2. FABRICATED REPLACEMENT PARTS AND REPAIRED CRACK PER SApr 10, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA98025Stringer · crackedPAE - DURING C-CHECK, INSPECTION REPORTED STRINGER 16-R CRACKED AT BS 500B PLUS 8 INCHES, FORWARD OF WING ILLUMINATION LIGHT. MAINTENANCE REMOVED A 1 INCH BY 1.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, AND ER 98-0277. (M)Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA98024Stringer · crackedPAE - DURING C-CHECK INSPECTION, FOUND STRINGER 16L CRACKED AT BS 500B PLUS 19 INCHES, AFT OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, SRM 51-10-1 AND ER 98-0277. (M)Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA98022Frame · crackedPAE - DURING C-CHECK INSPECTION REPORTED, FRAME CRACKED AT BS 360 BETWEEN STRINGER 20R AND 21R. MAINTENANCE REMOVED A 1. INCH BY 3.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-1 AND 51-40-3. (M)Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, FrameSDR F3LA98021Skin · crackedPAE - DURING C-CHECK INSPECTION REPORTED, CRACK AT BS 950 BELOW STRINGER 14R AT EDGE OF SKIN LAP. MAINTENANCE REMOVED A 1 INCH BY 3 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3. (M)Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA98019Stringer · crackedPAE - DURING C-CHECK INSPECTION REPORTED CRACK IN STRINGER 16R AT BS 500B PLUS 16 INCHES, AFT OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0275. (M)Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA98018Stringer · crackedPAE - DURING C-CHECK INSPECTION REPORTED, CRACK IN STRINGER 16L AT BS 500B PLUS 8 INCHES, FORWARD OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0277. (M)Apr 9, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA98014Skin · corrodedDEN - FLT 43 - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD92-25-09), INSPECTION REPORTED BULGING OF SKIN (CORROSION) AT STATION 901, S23R AND S24R, AND STATION 895, STRINGER 25R. MAINTENANCE REPAIRED CORRODED AREAS PER SRM 53-30-1, PAGE 3 (Apr 9, 1998 · N217US · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA98013Skin · crackedDEN - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD 92-25-09, INSPECTION REPORTED .625 INCH CRACK SIX INCHES FORWARD OF L-1 DOOR IN FUSELAGE SKIN AT STRINGER 7. MAINTENANCE REPAIRED CRACK PER SRM 53-30-3, PAGES 7 AND 8. (M)Apr 9, 1998 · N217US · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA98015Skin · delaminatedPAE - DURING C-CHECK, MAINTENANCE REPORTED DISBONDING ON NR 4 SLAT TRAILING EDGE WEDGE OUTBOARD UPPER END. MAINTENANCE REMOVED 52.0 INCHE OF DELAMINATED SKIN FROM OUTBOARD LOWER SURFACE, 13 INCHES OF DELAMINATED SKIN FROM OUTBOARD UPPER SURFACE AND 15 INCHES Apr 7, 1998 · N207AU · Boeing 737201 · Leading Edge DevicesSDR F3LA98010Frame · crackedDURING C-CHECK, MAINTENANCE REPORTED FRAME CRACKED AT STA 7472, STR 9L. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3. (X)Apr 7, 1998 · N207AU · Boeing 737201 · Fuselage Main, FrameSDR F3LA98023Stringer · corrodedPAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 10-L, BS 450-459. MAINTENANCE REMOVED A 3 INCH BY 2.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, PAGES 3 AND 4, SRM 53-30-3, FIGURE 16, SRM 53-30-3, PAGES 51-53, AND SRApr 6, 1998 · N207AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA98020Skin · corrodedPAE - DURING C-CHECK INSPECTION REPORTED, CORROSION ON STRINGER 4L SKIN LAP AT BS 500A PLUS 10 INCHES. MAINTENANCE REMOVED A 1.2 INCH BY 2 INCH CORRODED AREA, FABIRCATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3. (M)Apr 6, 1998 · N207AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980165Skin · crackedROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND A 2 INCH CRACK FUSELAGE SKIN BS 807 STR 19L. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIG 6. (X)Apr 3, 1998 · N244US · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA98011Floorbeam · corrodedDURING C-CHECK, MAINTENANCE REPORTED CORROSION ON UPPER CHORD BS 328 FLOORBEAM, LBL 30-4, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF BS 328 BEAM UPPER CHORD FROM LBL 28 TO LBL 65. FABRICATED REPAIR PARTS AND INSTALLED WET WITH FASTENERS PER SRM 53-10-9, Apr 3, 1998 · N207AU · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980147Stringer · corrodedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORRODED AREA BS 920 TO BS 932 STRINGER 25L STRINGER. REMOVED CORRODED AREA, INSTALLED REPAIR PARTS, REPAIRED PER T/R 53-202-01, CORROSION LEVEL 2. (M)Apr 2, 1998 · N227AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980146Angle · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 663 RBL 25 WL 202 UPPER CHORD ANGLE. INSTALLED DOUBLER, REPAIRED PER DRAWING 65C37732. (M)Apr 2, 1998 · N227AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA980145Skin · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STA 727 A PLUS 10 INCHES BELOW S17R SKIN. REMOVED TWO PREVIOUS DOUBLERS, CUT OUT DAMAGED SKIN. FABRICATED FILLER AND INSTALLED. REPAIRED PER SRM 53-30-3 FIG 6. (X)Apr 2, 1998 · N227AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980144Skin · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CRACK .125 INCH SKIN RT AFT SERVICE DOOR CUTOUT FORWARD LOWER CORNER. CUTOUT CRACK FABRICATED AND INSTALLED DOUBLER, REPAIRED PER BOEING DRWING 65C27287. (M)Apr 2, 1998 · N227AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980143Frame · crackedINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 520 INBOARD OF CHORD LBL 21 FRAME. INSTALLED DOUBLER, REPAIRED PER SRM 51-40-3. (M)Apr 2, 1998 · N227AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980142Skin · crackedINT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK AT STA 759 S17R, 3 INCH LONG SKIN. REMOVED PRE-DOUBLER AND BLIND FASTENERS, FABRICATED DOUBLER AND INSTALLED PER SRM 53-30-3 FIG 25 AND EA 30778. (X)Apr 2, 1998 · N227AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980141Frame · corrosionINT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH AREA CORRODED AT STATION 360, BETWEEN S28L AND STRINGER 28R FRAME. INSTALLED FRAME REPAIR SECTION AND REPAIRED PER SRM 53-10-04 FIG 10. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Apr 2, 1998 · N227AU · Boeing 737201 · Fuselage Main, FrameSDR F3LA98012Skin · crackedDEN - PRIOR TO DEPARTURE, MAINTENANCE REPORTED ONE .25 INCH CRACK IN LEFT WING LEADING EGE SKIN AT WBL 165.0. MAINTENANCE REPAIRED DAMAGED AREA PER SRM 57-30-4, PAGE 4. (M)Apr 1, 1998 · N205AU · Boeing 737201 · Wing, Plate/SkinSDR USAA980137Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 4 INCH BY 4 INCH STATION 908, STRINGER 21L. CUT OUT DAMAGE AND INSTALLED STRINGER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980136Stringer · corrosionINT - DURING 'Q-4' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCHES, STA 967 TO STA 987, STR 25R. INSTALLED REPAIR ANGLES AND REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X)Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980135Beam · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AROUND NUT PLATES STATION 235 BL '0' TO RBL 15 NOSE W/W CEILING TRANSVERSER BEAM. REMOVED AND INSTALLED NEW PREFAB TRANSVERSER BEAM, FABRICATED AND INSTALLED ZEE STRAPS. REPAIRED PER Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Miscellaneous StructureSDR USAA980134Stringer · corrosionINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 30 INCH CORRODED AREAS CORROSION ON STRINGER 24L FROM BS 294.5 TO BS 325.3 STRINGER. INSTALLED DOUBLER REPAIR ANGLE, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980133Stringer · corrodedINT - DURING 'Q-4' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORROSION STA 1006 STR 26L. INSTALLED REPAIR ANGLES, REPAIRED PER SRM 53-10-3. CORROSION TAKE NR: C53-202-01. CORROSION LEVEL: 2. (X)Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980132Stringer · corrodedINT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 30 INCH STATION 294 TO 325 STRINGER 24L. SPLICED IN NEW STRINGER SECTION, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (M)Mar 27, 1998 · N242US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR 98ZZZX1365Housing Assy · crackedHYDRAULIC MODULE PACK HOUSING WALL BETWEEN TWO SHUT-OFF VALVES CRACKED. HOUSING CRACKED DURING NORMAL OPERATION. SUBMITTER STATED THIS IS A RECURRING PROBLEM AND RECOMMENDED A STRONGER HOUSING BE MANUFACTURED AS A REPLACEMENT.Mar 19, 1998 · Boeing 737201 · Landing Gear Retraction/Extension SystemSDR F3LA98009Wire · loosePHX - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 4 A, B, C INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SECURED WIRING HARNESS AND SYSTEM CHECKED OK. (M)Mar 17, 1998 · N205AU · Boeing 737201 · Light System WiringSDR USAASB98066Circuit Breaker · failedCLT - FLT 1503 - ON CLIMB-OUT FROM CLT, THE NR 1 GENERATOR WAS LOST AT APPROXIMATELY 6,000 FEET. CREW PUT THE APU GENERATOR ON LINE AND IT CEASED AT 11,000 FEET. WITH ONLY ONE POWER SOURCE LEFT, CREW RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENMar 16, 1998 · N243US · Boeing 737201 · AC Generation SystemSDR USAASB98063Csd · out of adjustBOS - FLT 1683 - AT 5,000 FEET, THE NR 2 GENERATOR DROPPED OFF LINE. CAPTAIN HAD A BRAND NEW FIRST OFFICER ON BOARD AND WAS NOT CERTAIN ABOUT THE RELIABILITY OF THE APU. CAPTAIN ELECTED TO RETURN TO FIELD AT BOS AFTER STARTING APU AND PLACING APU'S GENERATORMar 12, 1998 · N246US · Boeing 737201 · Alternator-Generator DriveSDR USAASB98060Light Assy · failedLGA - FLT 956 - PRIOR TO DEPARTURE, MAINTENANCE WAS CALLED TO FIX AND INOP AFT EMERGENCY LIGHT. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. (M)Mar 11, 1998 · N248US · Boeing 737201 · Emergency LightingSDR F3LA98006Line · failedSFO - ON INBOUND FLIGHT TO SFO, FLIGHT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULIC PRESSURE AND FLUID. USED ALTERNATE FLAP SYSTEM AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE 'A' SYSTEM HYDRAULIC PRESSURE LINE IN AFT FLAP WELL, BOTH 'A' SYSTEM HMar 8, 1998 · N205AU · Boeing 737201 · Hydraulic System, MainSDR USAASB98057Battery Pack · dischargedROC - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND POWER SUPPLY IN THE FORWARD CABIN. OPS CHECK GOOD. (M)Mar 2, 1998 · N262AU · Boeing 737201 · Emergency LightingSDR 98ZZZM339Power Supply · inoperativeROC - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND POWER SUPPLY IN THE FORWARD CABIN. OPS CHECK GOOD. (M)Mar 2, 1998 · N262AU · Boeing 737201 · Emergency LightingSDR USAA980114Stringer · corrosionINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 15 INCH CORROSION ON STR 25R FROM STA 360 - STA 340. INSTALLED NEW STRINGER, REPAIRED PER SRM 53-10-3 FIG 1. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980113Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .0625 INCH CRACK BS 304 BETWEEN S9L AND S10L SKIN. (EDDY CURRENT). INSTALLED DOUBLER, REPAIRED PER EA 43634. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980112Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .0625 INCH CRACK FORWARD ENTRY DOOR FUSELAGE LOWER AFT CORNER WL 207, STA 344 SKIN. INSTALLED DOUBLER, REPAIRED PER BOEING DWG 65C27257. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980111Floorbeam · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK BS 663 BL ZERO WL 205 FLOORBEAM WEB. INSTALLED DOUBLER, REPAIRED PER BAC DRAWING NR 65C34537. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA980110Frame · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK IN BODY FRAME RADIUS BS 294.5, 5 INCHES BELOW S26R. INSTALLED FRAME REPAIR, REPAIRED PER SRM 51-40-3. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, FrameSDR USAA980109Stringer · crackedINT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT 2 SKIN ATTACH FASTENER HOLES 5 INCHES TO 11 INCHES FOWARD OF BS 540 FRAME S15L STRINGER (FUSELAGE). INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1 AND EA 43631. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980108Stringer · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT 2 EACH SKIN ATTACH FASTENER HOLES 7 INCHES AND 8 INCHES FORWARD OF BS 540 FRAME S15R STRINGER FUSELAGE. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3 FIG 1 AND EA 43631. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980107Skin · crackedINT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 379 BETWEEN BL ZERO AND S28L SKIN (FUSELAGE). INSTALLED DOUBLER, REPAIRED PER TR 53-30-04. (X)Feb 28, 1998 · N233US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980105Skin · crackedINT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK ON EXTERNAL FUSELAGE SKIN AT FORWARD RT SERVICE DOOR LOWER HINGE CUTOUT FORWARD EDGE SKIN. REMOVED SECTION OF SKIN AND INSTALLED REPAIR DOUBLER. REPAIRED PER SB 737-53-1074 FIG 3 AND SRM 5Feb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA980104Frame · corrosionINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION BS 787 BETWEEN STRINGER 26R AND STRINGER 27R. CUTOUT CORRODED AREA AND INSTALLED REPAIR SKIN ATTACH ANGLE, REPAIRED PER SRM 53-10-4 FIG 7. CORROSION TASK NR C53-208-01, CORROSION LEVEFeb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980103Stringer · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 12 INCH SECTION OF CORROSION STRINGER 27L, BS 967 AND BS 987 STRINGERS. CUTOUT STRINGER, FABRICATED REPAIR SECTIONS AND SPLICED AND INSTALLED ON A/C BS 947 PLUS 10 INCHES TO BS 1016, REPAIRED PER SRM 5Feb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAA980102Frame · corrodedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 4 INCH CORROSION BS 286, STRINGER 28L FRAME WEB. CUTOUT CORRODED SECTION OF FRAME WEB AND INSTALLED NEW SECTION, REPAIRED PER SRM 51-40-02. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M)Feb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, FrameSDR USAA980101Stringer · crackedINT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK IN STRINGER, S18R BS 333. SPLICED STRINGER 65-45800-189, REPAIRED PER EA 43633. (M)Feb 23, 1998 · N259AU · Boeing 737201 · Fuselage Main, Longeron/Stringer
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