N823AS, cancelled Nov 13, 2017

Service difficulty reports · 217

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 = 'N823AS' AND deregistration_id = 'N823AS-2017-11-13'
  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 ASOA2012121302642Skin · crackedLT WING LOWER SKIN PLANK CRACKED AT WS 148.019 FWD OF REAR SPAR. CRACK IS 1.025". UPON REMOVAL OF SKIN PANEL AT WS 127-25 -WS 148.019 FOUND JOINT STRAP AT WS 148.019 BROKEN. STRAP REQUIRES REPLACEMENT. LOCATED, DRILLED, SEALED AND INSTALLED A NEW JOINT STRNov 26, 2012 · N823AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2012121302641Post · crackedFS 409+128 VERTICAL POST LBL 18 AFT OTBD (UPPER) RADIUS FAILS NDT WITH AN INDICATION GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-53-41-1643.Nov 26, 2012 · N823AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA2012072001950Door · lack of lubeSERVICE DOOR CANNOT BE OPENED FROM THE OUTSIDE. LUBED SERVICE DOOR, OPS CHECKED GOOD, REF MM 52-41-00.Jul 18, 2012 · N823AS · Cndair CL6002B19 · Service DoorsSDR ASOA2012071901931Engine · failedON DEPATURE, NR 1 ENGINE ITT EXCEEDED 900 DEGREES C. PULLED ENGINE TO IDLE. FELT SEVERE VIBRATION AND PROCEEDED TO RUN SEVERE ENGINE DAMAGE QRH AND SHUTDOWN ENGINE. ACFT RETURNED TO DEPARTURE, AND AN EMERGENCY DECLARED. REPLACED LT ENGINE. ACFT OK FOR SJul 15, 2012 · N823AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA201201771Light · inoperativeLEFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.Jun 6, 2012 · N823AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201201665Light · malfunctionedEMERGENCY LIGHTS ILLUMINATED WHEN SWITCH IN AUTO. RESET & OPS CHECKED EMEGENCY LIGHTS IAW AMM 33-51-01. CIRCUIT BREAKER PULLED. CHECKED GOOD.May 18, 2012 · N823AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201201625Lamp · burned outFWD LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.May 11, 2012 · N823AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201201307Lens · missingEMERGENCY LIGHT IS MISSING LENS. INSTALLED EMERGANCY LIGHT LENS IAW AMM 33-51-16. OPS CHECKS GOOD.Apr 19, 2012 · N823AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201102040Lens · looseBOARDING DOOR EMERGENCY LIGHT LENS COVER LOOSE. R & R EMERGENCY LIGHT FOR LT SIDE FWD OF PAX DOOR. OPS CHECKED GOOD IAW AMM 33-51-21, FIG.1, ITEM 16.Oct 25, 2011 · N823AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201101672Door · lack of lubePASSENGER DOOR DIFFICULT TO OPEN. LUBED PAX DOOR AND PERFORMED OPS CK OF PAX DOOR IAW AMM 52-10-00. NO DEFECTS NOTED. (SDR CLOSED)Sep 8, 2011 · N823AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201101671Door · bindingUNABLE TO OPEN THE PASSENGER DOOR OR THE GALLEY SERVICE DOOR FROM OUTSIDE. SERVICE DOOR OPERATED NORMALLY IAW AMM 52-41-00 PAX DOOR OPERATED NORMALLY IAW AMM 52-11-00. ACFT OK FOR SERVICE.Sep 8, 2011 · N823AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201101609Door · bindingMAIN CABIN DOOR DIFFICULT TO OPEN OR CLOSE. CYCLED PAX DOOR OPS CHECKED GOOD IAW AMM 52-11-00. ACFT OK FOR SERVICE.Aug 26, 2011 · N823AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201101536Door · unknownF/A REPORTS MAIN PAX DOOR WILL NOT FULLY EXTEND TO OPEN POSITION WITHOUT ASSISTANCE FROM GROUND. OPS CHECKED PAX DOOR UNABLE TO DUPLICATE PROBLEM IAW AMM 52-11-00.Aug 19, 2011 · N823AS · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201101211Door · bindingRAMP REPORTS PAX DOOR WILL NOT OPEN OR CLOSE COMPLETELY OUTER HANDLE WILL NOT PUSH IN. OPENED AND CLOSED PASSENGER DOOR SEVERAL TIMES, OPS CHECKED OUTER HANDLE IAW AMM 52-11-03-710-802. OPS CHECK NORMAL. ACFT OK FOR SERVICE.Jun 22, 2011 · N823AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201101155Door · bindingPASSENGER DOOR WOULD NOT OPEN PROPERLY, IT GETS STUCK. PERFORMED OPS TEST OF THE PASSENGER DOOR IAW AMM 52-11-00, OPS CHECK GOOD. NO DEFECTS NOTED.Jun 10, 2011 · N823AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201100855Light · malfunctionedDURING CRUISE FLT, EMERGENCY LIGHTS CAME ON NO ORH PROCEDURE FOR THIS SELECTED EMERGENCY LIGHTS OFF. RESET CIRCUIT BREAKER AND PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CK GOOD ACFT OK FOR SERVICE.Apr 29, 2011 · N823AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201100172Lamp · burned outSERVICE DOOR EMERGENCY LIGHT INOPERATIVE. LAMPED EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.Jan 26, 2011 · N823AS · Cndair CL6002B19 · Emergency LightingSDR ASOA201001800Skin · crackedSUSPECT TWO CRACKS ON PAX DOOR SIKN UNDER TOP STEP ONE FWD AND AFT. REPAIRED IAW SRM 51-42-06, 51-42-13 AND 51-45-00.Nov 17, 2010 · N823AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201001644Door · bindingSERVICE DOOR CAN NOT BE OPENED FROM OUTSIDE, REPORTED BY RAMP AGENT. INSPECTED & C/W OPS CK OF SERVICE DOOR NO DEFECTS FOUND IN REF TO AMM CHAP 52-41-00.Oct 23, 2010 · N823AS · Cndair CL6002B19 · Service DoorsSDR ASOA201001492Pressure Panel · crackedFOUND FS 460 PRESSURE FLOOR HAS 2 INDICATIONS NOTED. 1 BETWEEN BL 0 AND RBL 9.0 2.8" LENGTH 50 PERCENT FSH AND 2ND BETWEEN BL 0.0 AND RBL 9.0 2.8" LENGTH 50 PERCENT FSH. FAILED NDT INSP. REO 601R-53-41-1279 REV. HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEOct 2, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201001486Seat Track · corrodedALL 6 CARGO BAY SEAT TRACKS ARE CORRODED. TREAT, PRIME, PAINT AND INSTALL TRACKS -49 AND -5 REQUIRED. TREATED PARTS IAW SRM 51-21-11, PRIMED PARTS IAW SRM 51-21-06, TOPCOAT PART IAW SRM 51-25-16 & INSTALLED -49 AND -5 PARTS IAW AMM 20-21-00-910-801 & REO 601Sep 27, 2010 · N823AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001437Floor Support · corrodedCONTINUATION OF MWC 347. FLOOR SUPPORT OTBD OF RBL 36 IS CORRODED FROM FS 621.00 TO FS 559.00+80. 26 EA NUTPLATES NEED INSTALLED. REINSTALLED 26 EA NUTPLATES IAW SRM 51-42-10.Sep 22, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001431Angle · cracked2 EA ANGLES COMMON WITH CARGO DOOR LOWER FWD/AFT DOOR STOPS (ANGLES ARE UNDER SILL PLATE) ARE CRACKED FS 590 AND FS 605. REMOVED 2 CRACKED ANGLES AT FS 590 AND FS 605 UNDER SILL PLATE THAT ARE COMMON WITH CARGO DOOR LOWER FWD AND AFT DOOR STOPS IAW SRM 51-42-Sep 22, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001419Placard · deterioratedPAX DOOR "EXIT" PLACARD IS DETERIORATED. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-00-000-801 AND 11-30-00-400-801.Sep 20, 2010 · N823AS · Cndair CL6002B19 · Placards and MarkingsSDR ASOA201001418Cargo Track · corrodedCARGO BAY SEAT TRACK ARE CORRODED. APPLIED DINITROL ON FS 409+16 FRAME SECTOR IAW SRM 51-21-11.Sep 20, 2010 · N823AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001484Sill · corrodedRT CABIN SIDE SILL CORROSION AT FS 578.00 EXCEEDED ALLOWABLE BLENDING LIMITS 1.0" WIDE, 1.1" LONG, .040 DEEP AROUND NUTPLATE HOLE. C/W STEPS 1, 2, 4, 5 AND 6 OF REO 601R-53-00-383. C/W REO 601R-53-00-383A. PERFORMED EDDY CURRENT OF RT CABIN FLOOR SIDE SILL.Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001346Seat Track · corrodedSEAT TRACK SEGMENT AT RBL 9 FS 409+112 TO FS 559 IS CORRODED BEYOND LIMITS. REMOVED SEAT TRACK SEGMENT AT RBL 9 FS 409+112 TO FS 559 IAW AMM 53-01-11-000-802. START WITH DRILLING OF NEW SEAT TRACK IAW SRM 51-40-11. LOCATED, DRILLED AND COUNTERSUNK ALL NEW Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001345Seat Track · corrodedRT SEAT TRACK SEGMENT AT RBL 9 FS 394.00 TO FS 409+112 IS CORRODED BEYOND LIMITS. REMOVED RT SEAT TRACK SEGMENT AT RBL 9 FS 394 TO FS 409+112 IAW AMM 53-01-11-000-802. RT SEAT TRACK REQUIRES INSTALL. LOCATED AND DRILLED HOLES ON NEW SEAT TRACK IAW SRM 51-40-Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001344Seat Track · corrodedLT SEAT TRACK SEGMENT AT LBL 9 FS 409+112 TO FS 559 IS CORRODED BEYOND LIMITS. REMOVED LT SEAT TRACK SEGMENT AT RBL 9 FS 409+112 TO FS 559 IAW AMM 53-01-11-000-802. LOCATED, DRILLED AND COUNTERSUNK ALL NEW HOLES ON NEW SEAT TRACK IAW SRM 51-40-11. INSTALLED LSep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001343Seat Track · corrodedLT SEAT TRACK SECTION AT LBL 9, FS 394.00 TO FS 409+112 IS CORRODED BEYOND LIMITS. REMOVED LT SEAT TRACK SECTION AT LBL 9 FS 394.00 TO FS 409+112 IAW SRM 53-01-11-000-802. LT SEAT TRACK REQUIRES INSTALL. LOCATED, DRILLED AND COUNTERSINK SEAT TRACK IAW SRM 5Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001342Seat Track · corrodedLT SEAT TRACK SEGMENT ON FLOOR LBL 9 FROM FS 364.00 TO FS 394.00 IS CORRODED BEYOND LIMITS. R & R LT SEAT TRACK SEGMENT ON FLOOR LBL 9 FROM FS 364 TO FS 394 IAW MM 53-01-11-000/400-802.Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001341Floorbeam · corrodedFLOOR SUPPORT CHANNEL LOCATED AT FS 349.00, RBL 36.00, WL 73.50 IS CORRODED ON OTBD SIDE MAX DEPTH .030". REPAIRED TRANSVERSE BEAM BY COMPLYING WITH STEPS 1-11 OF REO 601R-53-21-1178. ECTC REQUIRED. REO 601R-53-21-1178 REV HAS BEEN ACCOMPLISHED AND ALL STEPS Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001340Support Angle · corrodedRT FLOOR SILL SUPPORT ANGLE LOCATED BETWEEN FS 310.00 AND FS 319.70 IS CORRODED BEYOND REPAIRABLE LIMITS PN 601R38669-49. LOCATED & DRILLED SERVICEABLE DOUBLER FOR GALLEY MOUNT BETWEEN FS 310 & FS 319 IAW SRM 51-40-11. INSTALLED DOUBLER ON THRESHOLD IAW SRM Sep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001339Attach Angle · corrodedSERVICE DOOR SILL FWD ATTACH ANGLE LOCATED ON AFT SIDE OF FS 319.70 IS CORRODED AND REQUIRES REPLACEMENT, PN 601R3838-1. REMOVED SERVICE DOOR FWD ANGLE AT FS 319.70 IAW SRM 51-42-21 AND SRM 51-41-02. SERVICEABLE ANGLE REQ'S INSTALL. LOCATED & DRILLED NEW SERSep 15, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201001338Glowstrip · inoperativeRT EMER TRACK PHOTOLUMINESCENT INSERT FAILED TO WHITE COLOR AND NO LONGER LUMINATES IN ONE SECTION. R & R RT FADED EMER TRACK INSERT IAW AMM SUPPLEMENT ASA 33-51-00. (CLOSED)Sep 15, 2010 · N823AS · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201001316Fitting · corrodedSERVICE DOOR SILL FITTING AT FS 319.70, RBL 42 CORRODED. REMOVED SILL FITTING IAW SRM 51-42-21. DRILLED & LOCATED NEW SERVICEABLE STRAP BRACKET IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE STRAP BRACKET IAW SRM 51-42-21. APPLIED PROTECTIVE PAINT IAW SRM 51-2Sep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001315Floor Support · corrodedCLIP ON AFT SIDE OF FLOOR SUPPORT CROSSMEMBER AT 319.70 RBL 42 CORRODED. REMOVED CLIP ON AFT SIDE OF FLOOR SUPPORT IAW SRM 51-42-06, 51-42-26. REMOVED CORROSION ON CLIP IAW SRM 51-21-06 AREA ON CLIP WITHIN LIMITS IAW SRM 53-00-00, MATERIAL REMOVED .003, REMAISep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001314Floor Support · corrodedTHE FLOOR SUPPORT CROSSMEMBER IS CORRODED AT THE RT END AT FS 349.Sep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001313Floor Support · corrodedCLIP ON FWD SIDE OF FLOOR SUPPORT CROSSMEMBER AT FS 349, RBL 42 IS CORRODED. REMOVED FWD CLIP IAW SRM 51-42-06 AND 51-42-21. LOCATED AND INSTALLED SERVICEABLE CLIP AT FS 349, RBL 42 IAW SRM 51-42-06.Sep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001312Floor Support · corrodedCLIP ON THE AFT SIDE OF FLOOR SUPPORT CROSSMEMBER AT FS 349, RBL 42 IS CORRODED. REMOVED AFT CLIP IAW SRM 51-42-06 AND 51-42-21. CLIP REQUIRES REPLACED. REPLACED DAMAGED CLIP WITH SERVICEABLE CLIP IAW SRM 51-42-21. PAINTED IAW SRM 51-25-01.Sep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001311Support · corrodedTHE SILL SUPPORT JUST IN FRONT OF SVC DOOR FS 310-319 IS CORRODED. REMOVED SILL PLATE IAW SRM 51-42-06. SILL PLATE REQUIRES INSTALLATION. INSTALLED NEW SERVICEABLE SILL PLATE IAW SRM 51-42-06. APPLIED PROTECTIVE TREATMENT IAW SRM 51-25-01.Sep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001310Support Angle · corrodedSUPPORT ANGLE FOR RT WARDROBE FITTING AT FS 349 BETWEEN BL 36-42R IS CORRODED. REMOVED SUPPORT ANGLE IAW SRM 51-42-06. CORRODED SUPPORT ANGLE IS BEYOND REPAIRABLE LIMITS IAW SRM 53-00-00, FIG 102, SHEET 2, LOCATED, DRILLED UP NEW SERVICEABLE SUPPORT ANGLE ISep 12, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001300Intercostal · corrodedINTERCOSTAL AT FS 559.00+80 BETWEEN RBL 9 AND RBL 27 IS CORRODED. REMOVED CAP STRIP AT FS 559.00+80 INTERCOSTAL BETWEEN RBL 9-27 IAW SRM 51-42-06 AND 51-42-10. AFTER FURTHER INVESTIGATION OF DAMAGE AT FS 559.00+80 BETWEEN RBL 9 AND RBL 27, FOUND DAMAGE TO BSep 9, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001299Skin · corrodedSKIN CORRODED BETWEEN FS 409+16 AND 409+32 AT STR 27 AROUND STROBE LIGHT. REMOVED BEACON LIGHT REINFORCEMENT ANGLE CHANNEL IAW SRM 51-42-06. LOCATED BETWEEN FS 409+16 AND 409+32 FOUND SKIN UNDER CHANNEL TO BE FREE OF CORROSION. CHANNEL IS CORRODED BEYOND RESep 9, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201001298Stringer · corrodedSTRINGER 27 CORRODED BETWEEN FS 319.00 AND FS 349.00. CUT STRINGER 27 AT FS 325 AND REMOVED AFT CORRODED SECTION IAW REO 601R-53-21-1183 REV & SRM 53-00-03. CUT EDGES OF STR 27 AFT FS 325. COMPLIED WITH SRM 53-00-03. PERFORMED EDDY CURRENT OF CUT EDGES IAW NSep 9, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA201001285Fitting · crackedFITTING AT LOWER LT 621 BULKHEAD OTBD IS CRACKED. FOUND TO BE CRACKED, LT FS 621 BULKHEAD FLOOR SUPPORT ANGLE. REMOVED CRACKED LT FS 621 FLOOR SUPPORT ANGLE AND FOUND TO BE PREVIOUSLY REPAIRED IAW REO 601R-53-61-117 AND FOUND 11EA ELONGATED FASTENER HOLES THROSep 5, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA201001284Angle · corrodedANGLE AT CARGO DOOR SILL PLATE IS CORRODED. REMOVED ANGLE, LOCATED, DRILLED, AND DEBURRED NEW IAW SRM 51-42-06 AND 51-40-11. INSTALLED ANGLE IAW SRM 51-42-06 & 51-42-21.Sep 5, 2010 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201001283Post · crackedFOUND FS 409.0+128, RBL 18.0 INBD SIDE VERT POST HAS INDICATION NOTED APPROX .3" IN LENGTH 60 PERCENT FSH AT WL 69.0 AFT FLANGE RADIUS. FAILED NDT INSP. REMOVED INBD AND OTBD POSTS AT FS 409, RBL 18 IAW SRM 51-42-06. DRILLED SERVICEABLE INBD POST IAW SRM 51Sep 5, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA201001274Floorbeam · crackedFS 280.090 FLOORBEAM WEB IS CRACKED LOWER RADIUS, AT LBL 11 AND BOTH FWD & AFT J CHANNELS ARE CORRODED ACROSS COCKPIT ENTRANCE. REPAIRED AND COMPLIED WITH REO 601R-53-11-926 IAW REO 601R-53-11-926, REV B. CLOSEOUT AND OPS CHECK REQ'ED. COMPLIED WITH CLOSEOUTSep 4, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201001273Fitting · crackedFS 202.75 BULKHEAD HAS EVIDENCE OF A CRACK AT PARKING BRAKE CABLE BULKHEAD FITTING. PERFORMED EDDY CURRENT INSP OF FS 202.75 BULKHEAD AT PARKING BRAKE CABLE SUSPECTED AREA IAW NDTM 51-20-06. FOUND FS 202.75 BULKHEAD WEB HAS INDICATION NOTED APPROX 150 INCHESSep 4, 2010 · N823AS · Cndair CL6002B19 · Fuselage Main, Bulkhead
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