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 F3LA99099Rib · crackedDEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE UPPER DOG HOUSE TAIL FAIRING RIB, INNER AFT END. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)Jun 30, 1999 · N207AU · Boeing 737201 · Engine Thrust ReverserSDR F3LA99098Rib · crackedDEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE UPPER DOG HOUSE TAIL FAIRING RIB, INNER LOWER SIDE. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)Jun 30, 1999 · N207AU · Boeing 737201 · Engine Thrust ReverserSDR F3LA99097Chord · crackedDEN - DURING C-CHECK INSPECTION, REPORTED THREE CRACKS FOUND IN PRESSURE DECK COMPRESSION CHORD AT STATION 663.75, RBL 25 AND LBL 25. MAINTENANCE FABRICATED AND REPLACED RIB PER EA 51-737-003 AND SRM 51=40-3. (M)Jun 30, 1999 · N207AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA99096Igv · crackedDEN - DURING C-CHECK INSPECTION REPORTED, NR 1 ENGINE INLET GUIDE VANE CRACKED ON WELD AT 'A' FLANGE, 10 O'CLOCK POSITION. MAINTENANCE STOP DRILLED CRACK PER P/W JT8D MM 72-00, PAGES 664A, 664B AND 665. CRACK AREA WELDED PER P/W E/M 72-23-01, PAGES 901 AND 9Jun 30, 1999 · N207AU · Boeing 737201 · Turbine Engine Compressor SectionSDR F3LA99095Igv · crackedDEN - DURING C-CHECK, INSPECTION REPORTED NR 1 ENGINE INLET GUIDE VANE CRACKED ON WELD AT 'A' FLANGE AT 2 O'CLOCK POSITION. MAINTENANCE STOP DRILLED CRACK PER P/W JT8D MM 72-00, PAGES 664A, 664B AND 665. CRACK AREA WELDED PER P/W E/M 72-23-01, REPAIR NR 14, Jun 30, 1999 · N207AU · Boeing 737201 · Turbine Engine Compressor SectionSDR 99ZZZX2744Seat Track · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK RT OUTBOARD STA 344 - STA 380.Jun 30, 1999 · N226US · Boeing 737201 · Fuselage, Seat/Cargo Attach FittingsSDR F3LA99090Shear Tie · crackedDEN - DURING C-CHECK INSPECTION REPORTED, CRACK IN SHEAR TIE, LAST RIVET TO EDGE OF TIE, AT BS 294.5 ABOVE STRINGER 13L. MAINTENANCE REPAIRED CRACKED AT SHEAR TIE PER SRM 53-10-4, FIG 8. (M)Jun 29, 1999 · N207AU · Boeing 737201 · Fuselage Miscellaneous StructureSDR F3LA99088Angle · crackedDEN - DURING C-CHECK, INSPECTION REPORTED CRACK AT NR 2 ENGINE NOSE COWL FAIRING (SUGAR SCOOP) SEAL RETAINER INNER ANGLE. MAINTENANCE FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3. (M)Jun 29, 1999 · N207AU · Boeing 737201 · Engine Cowling SystemSDR F3LA99087Skin · crackedDEN - DURING C-CHECK, INSPECTION REPORTED CRACK IN PYLON INNER SKIN WHERE PANEL 5243 ATTACHES. MAINTENANCE REMOVED AND DAMAGED AREA AND REPAIRED PER SRM 51-40-3. (M)Jun 28, 1999 · N207AU · Boeing 737201 · Nacelle/Pylon, Plate/SkinSDR USAA990625Skin · crackedTPA - DURING A RON, VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 380 BETWEEN STRINGER 28L AND 28R AFT EQUIP COOLING ACCESS ON SKIN. INSTALLED DOUBLER PER TR 53-30-04/SB 737-53-1117/SRM 51-10-01. (M)Jun 27, 1999 · N253AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB99154Connector · brokenBWI - FL2700 - FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT INCIDENT DUE TO THE NR 2 ENGINE FUEL HEAT VALVE OPEN LIGHT FLICKERING AND THE NR 2 ENGINE OIL TEMPERATURE RISING SLIGHTLY HIGHER THAN THE NR 1 ENGINE INTO THE YELLOW RANGE. NO ENGINE SHUT DOWN OJun 25, 1999 · N265AU · Boeing 737201 · Engine Anti-Icing SystemSDR F3LA99094Exhaust Case · crackedDEN - DURING C-CHECK INSPECTION, REPORTED NR 2 ENGIEN EXHAUST CASE CRACKED AT 3 O'CLOCK STRUT, TOP SIDE. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54 PAGE 204 AND BAC 5975. (M)Jun 25, 1999 · N207AU · Boeing 737201 · Engine Collector/Tailpipe/NozzleSDR F3LA99086Stringer · crackedDEN - DURING C-CHECK, INSPECTION REPORTED STRINGER 7R CRACKED ON AFT SIDE OF CIRCUMFERENTIAL FUSELAGE SPLICE AT BS 360. MAINTENANCE REMOVED DAMAGED AREA, AND FABRICATED AND INSTALLED STRINGER PER SRM 51-10-2, 51-30-2 AND 51-20-01. (M)Jun 25, 1999 · N207AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA99084Line · failedPHX - UPON ARRIVAL, FLIGHT CREW REPORTED 'A' SYSTEM HYDRAULIC LIGHT FLICKERED, THEN LOST AL SYSTEM 'A' HYDRAULICS AT ALTITUDE. 'B' SYSTEM AND STANDBY SYSTEM REMAINED NORMAL. REPLACED DEFECTIVE 'A' SYSTEM MAIN HYDRAULIC SUPPLY LINE TO ENGINE DRIVEN HYDRAULIC Jun 25, 1999 · N212US · Boeing 737201 · Hydraulic System, MainSDR USAASB99153Regulator · failedTPA - FLT 2636 - ON CLIMB-OUT FROM TPA, CAPT OBSERVED A DUCT PRESSURE OF OVER 100 PSI ON THE RIGHT SIDE AND 40 PSI ON THE LEFT SIDE. THE NR 5 LEADING EDGE SLAT TRANSIT LIGHT WAS ALSO ILLUMINATED. CREW CYCLED LEADING EDGE SLATS TWICE BUT LIGHT WOULD NOT EXTINJun 23, 1999 · N243US · Boeing 737201 · Pneumatic Distribution SystemSDR F3LA99093Exhaust Case · crackedDEN - DURNG C-CHECK INSPECTION, REPORTED NR 2 ENGINE EXHAUST CASE STRUT CRACKED AT 9 O'CLOCK POSITION AT ROOT. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54, PAGE 204 AND BAC5975. (M)Jun 23, 1999 · N207AU · Boeing 737201 · Engine Collector/Tailpipe/NozzleSDR F3LA99092Exhaust Case · crackedDEN - DURING C-CHECK INSPECTION, REPORTED A 3 INCH CRACK IN THE NR 2 ENGINE EXHAUST CASE UNDER 3 O'CLOCK POSITION STRUT, EXTENDING TOWARD CENTER OF CASE. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54, PAGE 204 AND BAC 5975. (M)Jun 23, 1999 · N207AU · Boeing 737201 · Engine Collector/Tailpipe/NozzleSDR F3LA99091Igv · crackedDEN - DURING C-CHECK INSPECTION REPORTED NR 2 ENGINE INLET GUIDE VANE CRACKED AND STOP DRILLED AT 2 O'CLOCK POSITION, AFT WELD. MAINTENANCE WELDED CRACK IAW P/W E/M 72-23-04, REPAIR 14, PAGES 901 AND 902, SUBTASK 1, 2, 3 AND 4 AND STRESS RELIEVED IAW P/W E/M Jun 22, 1999 · N207AU · Boeing 737201 · Turbine Engine Compressor SectionSDR USAA990624Skin · crackedCLT - DURING METRO MOD, FOUND 1 INCH LONG CRACK ON SKIN AT STATION 378 BETWEEN STRINGER 21L AND STRINGER 22L. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-03 AND EA NR 64917. (M)Jun 21, 1999 · N246US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990623Floorbeam · corrodedCLT - DURING METRO MOD, FOUND 1 INCH BY 2 INCH AREA OF CORROSION ON FLOORBEAM AT BS 294 AT LBL 06- LBL 10. REPAIRED PER T/R 53-10-04B AND EA NR 64946. (M)Jun 21, 1999 · N246US · Boeing 737201 · Fuselage Main, Floor BeamSDR USAA990616Stringer · corrodedTPA - DURING CX-4 CHECK, FOUND CORROSION ON STRINGER .5 INCH BY 3 INCH AT STATION 1006 STRINGER 27L. REMOVED AND REPLACED STRINGER THAT WAS CORRODED, CLEANED AND TREATED SAME PER SRM 53-10-3 AND EA 64746. (M)Jun 20, 1999 · N248US · Boeing 737201 · Fuselage Main, Longeron/StringerSDR F3LA99085Fitting · crackedDEN - DURING C-4 CHECK INSPECTION, REPORTED LEFT UPPER FORWARD STOP FITTING ON AFT AIRSTAIR DOOR CRACKED. MAINTENANCE INSTALLED REPLACEMENT FITTING PER SRM 51-30-2. (M)Jun 18, 1999 · N207AU · Boeing 737201 · Passenger/Crew DoorsSDR USAA990601Skin · crackedTPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK IN FUSELAGE SKIN AT STATION 727A, 2 INCH AT STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M)Jun 16, 1999 · N229US · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990589Skin · crackedTPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STATION 727A, 2 INCH BY STRINGER 15L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Jun 16, 1999 · N229US · Boeing 737201 · Fuselage Main, Plate/SkinSDR F3LA99080Bearing · out of limitsDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXCESSIVE PLAY IN RIGHT MLG FORWARD TRUNNION BEARING, OUT OF LIMITS AT .057. MAINTENANCE REPLACED RIGHT MLG FORWARD TRUNNION BEARING PER MM 32-11-11A AND WORK CARD 7-7007. (M)Jun 16, 1999 · N214AU · Boeing 737201 · Main Landing Gear Attach SectionSDR F3LA99078Bearing · out of limitsDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXCESSIVE PLAY IN LEFT MLG FORWARD TRUNNION BEARING, OUT OF LIMITS AT .052. MAINTENANCE REPLACED LEFT MLG FORWARD TRUNNION BEARING PER MM 32-11-11A AND WORK CARD 7-7006. (M)Jun 16, 1999 · N214AU · Boeing 737201 · Main Landing Gear Attach SectionSDR USAASB99144Valve · failedBWI - FLT2693 - EN ROUTE FROM ROC TO MCO, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPT ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND DISCONNECTED THE NR 1 ENGINE CSD. CAPT THEN ATTEMPTED TO PUT THE APU ON LINE BUT, THE APU FAILED TO START. Jun 14, 1999 · N254AU · Boeing 737201 · APU Bleed Air SystemSDR USAASB99142Charger · failedORD - MAINTENANCE FOUND THE LEFT AND RIGHT FORWARD ENTRY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Jun 14, 1999 · N236US · Boeing 737201 · Emergency LightingSDR 99ZZZM393Oil Cooler · failedBWI - FLT2693 - EN ROUTE FROM ROC TO MCO, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPT ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND DISCONNECTED THE NR 1 ENGINE CSD. CAPT THEN ATTEMPTED TO PUT THE APU ON LINE BUT, THE APU FAILED TO START. Jun 14, 1999 · N254AU · Boeing 737201 · Engine Oil CoolerSDR 99ZZZM392Csd · failedBWI - FLT2693 - EN ROUTE FROM ROC TO MCO, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CAPT ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND DISCONNECTED THE NR 1 ENGINE CSD. CAPT THEN ATTEMPTED TO PUT THE APU ON LINE BUT, THE APU FAILED TO START. Jun 14, 1999 · N254AU · Boeing 737201 · Alternator-Generator DriveSDR USAASB99137Csd · failedPHL - FLT 711 - ON CLIMB-OUT FROM EWR, AT APPROXIMATELY FL150, THE NR 2 GENERATOR TRIPPED OFF LINE WITH THE NR 2 CSD INDICATING LOW OIL PRESSURE AND HIGH OIL TEMPERATURE. WITH THE APU BEING INOPERATIVE AND ON MEL, THE CREW WAS DOWN TO ONE SOURCE OF ELECTRICALJun 4, 1999 · N262AU · Boeing 737201 · Alternator-Generator DriveSDR F3LA99045Valve · failedDEN - FLT 546 - FLIGHT CREW REPORTED CABIN ALTITUDE HORN SOUNDED AT 10,000 FEET. CLOSED OUTFLOW VALVE USING MANUAL DC AT 32,500 FEET. CABIN CONTINUED TO CLIMB AT 1,000 FPM AND A RAPID DESCENT WAS MADE TO 14,000 FEET. OXYGEN MASKS WERE AUTOMATICALLY DEPLOYEDJun 4, 1999 · N217US · Boeing 737201 · Cabin Pressure Control SystemSDR F3LA99043Drag Brace · crackedDEN - DURING SERVICE CHECK, INSPECTION REPORTED NOSE LANDING GEAR UPPER DRAG BRACE BEARING MIGRATING AT ACTUATOR ATTACH POINT. UPON FURTHER INSPECTION, FOUND 1 INCH CRACK IN NOSE GEAR UPPER DRAG BRACE A-FRAME ON RT SIDE OF WEB. MAINTENANCE INSTALLED NEW DRAJun 4, 1999 · N205AU · Boeing 737201 · Nose/Tail Landing GearSDR USAASB99132Ballast · failedALB - FL 548 - AFTER TAKEOFF, AT APPROXIMATELY 2,000 FEET, CREW NOTICED SMOKE IN THE COCKPIT. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FIELD AT ALB. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE BALLAST FOR THE ENMay 30, 1999 · N233US · Boeing 737201 · Passenger Compartment LightingSDR USAA990485Skin · crackedTPA - DURING RON, FOUND 2 INCH CRACK IN FUSELAGE SKIN AT STATION 756 AND STRINGER 13R. INSTALLED DOUBLER MADE OF 2023T3 - .072 INCH THICK PER SRM 53-30-3, FIG 6. (M)May 30, 1999 · N255AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990483Stringer · corrodedTPA - DURING CX-4 CHECK, FOUND 8 INCHES OF STRINGER WEB CORRODED AT STRINGER 27R AT STATION 967 THROUGH 975. REPLACED STRINGER PER SRM 53-00-03. (M)May 30, 1999 · N265AU · Boeing 737201 · Fuselage Main, Longeron/StringerSDR USAASB99129Battery Pack · dischargedGSO - MAINTENANCE FOUND THE AISLE SEAT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A WIRE SPLICE AND TWO BATTERY PACKS. OPERATIONAL CHECK GOOD. (M)May 24, 1999 · N226US · Boeing 737201 · Emergency LightingSDR USAASB99128Seal · failedRDU FL324 - ON CLIMB-OUT FROM CLT, JUST PRIOR TO PASSING RDU, CAPTAIN REPORTED HEARING TWO LOUD BANGS FROM THE FORWARD CABIN/MAIN ENTRY DOOR AREA. FLGIHT DIVERTED TO RDU AND LANDED WITHOUT FURTHER INCIDENT. RDU MAINTENANCE HAD DIFFICULTY OPENING THE DOOR, SOMay 23, 1999 · N223US · Boeing 737201 · Passenger/Crew DoorsSDR USAA990436Skin · crackedTPA - DURING UNSCHEDULED MAINTENANCE, FOUND .125 INCH CRACK IN SKIN AT STATION 947 AND STRINGER 14R. INSTALLED DOUBLER MADE OF .063 INCH STAINLESS STEEL .5 HARD PER SRM 53-30-3 FIG 21A. (M)May 10, 1999 · N252AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAASB99119Adc · failedTPA - FLT 2636 - AT ROTATION ON TAKEOFF FROM TPA, CREW RECEIVED THE FOLLWING INDICATIONS, FIRST OFFICER ALTIMETER INDICATED STANDBY AND COULD NOT BE RESET, FIRST OFFICER MACH INOPERATIVE, FIRST OFFICER VSI FLAG, ACARS INOPERATIVE, MACH TRIM FAIL AND ALTITUDE AMay 3, 1999 · N245US · Boeing 737201 · Air Data ComputerSDR USAASB99116Fan · failedRIC - FLT 517 - EN ROUTE FOR CLT-DCA AT FL250, FLIGHT ATTENDANT REPORTED THAT A PASSENGER SMELLED SMOKE IN THE FIRST THREE ROWS OF CABIN. CAPTAIN TURNED GALLEY POWER OFF AND THE FLIGHT ATTENDANT WENT BACK AND CONFIRMED SMOKE COMING OUT OF THE AIR CONDITIONINGApr 30, 1999 · N242US · Boeing 737201 · Air Distribution FanSDR USAASB99113Battery Pack · dischargedBDL - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHT OVER THE AFT ENTRY DOOR REMAINS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Apr 27, 1999 · N251AU · Boeing 737201 · Emergency LightingSDR USAASB99110Power Supply · inoperativeCLE - MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. ALSO, FOUND THE INTERIOR LOWER EXIT SIGNS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD.Apr 26, 1999 · N228US · Boeing 737201 · Emergency LightingSDR 99ZZZM358Battery Pack · dischargedCLE - MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHTS INOPERATIVE. ALSO, FOUND THE INTERIOR LOWER EXIT SIGNS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD.Apr 26, 1999 · N228US · Boeing 737201 · Emergency LightingSDR USAASB99109Hydraulic Line · leakingRDU - FL2604 - AIRCRAFT WAS EN ROUTE FROM FLL TO BWI, WHEN IT WAS DIRECTED TO HOLD SHORT OF RDU DUE TO AIR TRAFFIC CONTROL AT DCA. WHILE HOLDING AT 2,500 FEET, THE 'A' HYDRAULIC SYSTEM GAUGE READ ZERO AND WHILE TURNING DURING THE HOLD, THE 'A' SYSTEM LOW PREApr 23, 1999 · N246US · Boeing 737201 · Hydraulic System, MainSDR USAASB99107Circuit Card · malfunctionedTPA - FL2707 - CREW DID NOT RECEIVE ANY LANDING GEAR LIGHTS WHEN GEAR HANDLE WAS LOWERED. CIRCUIT BREAKERS WERE CHECKED, GEAR WAS CYCLED AND VISUAL CHECK THAT GEAR WAS DOWN WAS ACCOMPLISHED. CREW DECLARED AN EMERGENCY. FLIGHT LANDED AT TPA WITHOUT INCIDENT Apr 23, 1999 · N255AU · Boeing 737201 · Landing Gear Position and WarningSDR F3LA99033Bolt · crackedDEN - FLT 857 - DURING SERVICE CHECK, EO 71-20-737-002 WAS ACCOMPLISHED WHICH FOUND THE NR 2 ENGINE OUTBOARD LUG BEARING LOOSE AND DISPLACED. AN ULTRA SOUND INSPECTION REVEALED THE FORWARD ENGINE MOUNT BOLT CRACKED. MAINTENANCE REPLACED NR 2 ENGINE MOUNT ASSApr 23, 1999 · N217US · Boeing 737201 · Engine Mount SectionSDR USAA990396Skin · crackedTPA - DURING EDDY CURRENT INSPECTION, FOUND A .875 INCH SKIN CRACK AT BS 727B PLUS 9 INCHES AT STRINGER 17L. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 1. (M)Apr 22, 1999 · N227AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990395Skin · crackedTPA - DURING EDDY CURRENT INSPECTION, FOUND A 2 INCH SKIN CRACK AT BS 727A PLUS 13 INCHES AT STRINGER 18L. INSTALLED REPAIRED DOUBLER PER SRM 53-30-3 FIG 1. (M)Apr 22, 1999 · N227AU · Boeing 737201 · Fuselage Main, Plate/SkinSDR USAA990394Skin · crackedTPA - DURING EDDY CURRENT INSPECTION, FOUND A 1.25 INCH SKIN CRACK AT BS 727A PLUS 6 INCHES AT STRINGER 19L. INSTALLED REPAIR DOUBLER PER SRM 53-30-3 FIG 1. (M)Apr 22, 1999 · N227AU · Boeing 737201 · Fuselage Main, Plate/Skin
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