N584FE

Service difficulty reports · 491

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 = 'N584FE' AND registry_match = 'registration'
  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 08FDEA01363Seat Track · corrodedMAIN DECK SEAT TRACK FLANGE AT STA 1500, X = -8 FOUND CORROSION AT UPPER SURFACE. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 9, 2008 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01351Seat Track · corrodedUPON REMOVAL OF MAIN DECK FLOOR PANEL 292BF, FOUND SEAT TRACK AT STA 1831 TO STA 1887, X = -75.5 WITH EXFOLIATION CORROSION. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 8, 2008 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01350Seat Track · corrodedMAIN DECK SEAT TRACK FLANGE BELOW FLOOR PANEL 262AF AT STA 1159 TO 1245, X = -8 FOUND CORROSION ON UPPER SURFACE. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 8, 2008 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01349Seat Track · corrodedMAIN DECK SEAT TRACK FLANGE BELOW FLOOR PANEL NR 263LF AND 263FF AT STA 1310 TO STA 1365, X = -8 FOUND CORROSION AT UPPER SURFACE AT 3 LOCATIONS. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAApr 8, 2008 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01348Skin · corrodedAFT FUSELAGE, RIGHT EXTERNAL SKIN AT STA 2144 TO STA 2164, FOUND EXFOLIATION CORROSION AT LOWER EDGE OF FIXED FAIRING (347DF) MOUNTING AREA. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. ORIGINAL THICKNESS = 0.095", MATERIAL REMOVED = 0.058", REMAINING THApr 8, 2008 · N584FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 08FDEA01321Fitting · crackedMAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 7 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 6, 2008 · N584FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA01320Fitting · crackedMAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 6 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 6, 2008 · N584FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA01319Fitting · crackedMAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 4 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 6, 2008 · N584FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA01318Fitting · crackedMAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 3 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 6, 2008 · N584FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA01317Fitting · crackedMAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 2 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 6, 2008 · N584FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA01316Fitting · crackedMAIN DECK CARGO DOOR LOWER DOOR JAMB SPOOL FITTING NR 1 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 6, 2008 · N584FE · Doug MD11F · Cargo/Baggage DoorsSDR 08FDEA01278Skin · cracked08 EACH FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-120551, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10Apr 3, 2008 · N584FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA01277Access Panel · corroded06 EACH FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-120550, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100Apr 3, 2008 · N584FE · Doug MD11F · Wing, Plate/SkinSDR 08FDEA01276Seat Track · corrodedMAIN DECK SEAT TRACK INBOARD FLANGE AT STA 1481 TO STA 1515, X = -75 FOUND CORROSION. REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 3, 2008 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01275Seat Track · corrodedMAIN DECK SEAT TRACK FLANGE AT STA 1395, X = -75 FOUND EXFOLIATION CORROSION. REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 3, 2008 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01274Seat Track · corrodedMAIN DECK SEAT TRACK FLANGE AT STA 1470, X = -75 FOUND EXFOLIATION CORROSION. REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 3, 2008 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01273Seat Track · corrodedMAIN DECK SEAT TRACK FLANGE BELOW FLOOR PANEL NR 272HF AT STA 5-73, X = -8 HAS EXFOLIATION CORROSION. REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 3, 2008 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01256Stringer · crackedRIGHT WING, AFTER PANEL REMOVAL FOUND LEADING EDGE STRINGER CRACK AT XOS 667. REPAIR CARRIED OUT PER EA 1-5710-120544, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Apr 2, 2008 · N584FE · Doug MD11F · Wing, Longeron/StringerSDR 08FDEA01255Skin · dentedLEFT WING, INBOARD FLAP LOWER SKIN FOUND WITH DENT AT STA XIFH 299. DENT AREA MEASURED AND FOUND OUT OF LIMIT PER SRM 57-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Apr 2, 2008 · N584FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA01253Skin · dentedRIGHT WING, INBOARD FLAP LOWER SURFACE FOUND DENTS AT XIFH 150. DENTED AREA MEASURED FOUND OUT OF LIMIT PER SRM 57-10-00 FIGURE 17 VOLUME I. DEPTH = 0.048" AND DIAMETER = 0.5". REPAIR CARRIED OUT PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOApr 2, 2008 · N584FE · Doug MD11F · Trailing Edge FlapsSDR 08FDEA01250Access Panel · crackedRIGHT WING, LEADING EDGE LOWER SURFACE ACCESS PANEL 619CB INBOARD CORNER CUTOUT AREA FOUND CRACK. REPAIR CARRIED OUT PER SRM 57-10-00 FIGURE 21 VOLUME I. FABRICATED FILLER AND DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMMApr 2, 2008 · N584FE · Doug MD11F · Wing, Plate/SkinSDR 06FDEA03904Fluid · leakingON LANDING, ONCE AUTOBRAKES ENGAGED, A/C HAD VIOLENT SHAKE, DISENGAGED AUTOBRAKES AND GOT UNSAFE CENTER GEAR. MAINTENANCE CONFIRMED HYD LEAK. TOWED TO GATE. NORMAL LANDING. REMOVED AND REPLACED THE CENTER LANDING GEAR, DRAGBRACES, TIRES,BRAKE, ANTI SKID MANov 6, 2006 · N584FE · Doug MD11 · Hydraulic System, MainSDR 06FDEA03641Hinge · damagedWINGS, DURING ACCOMPLISHMENT OF FEDEX EA NR 1-5710-66421A PT2, FOUND LT AND RT INBOARD FLAP OUTBOARD HINGE BORE DIMENSION ARE DIFFERENT FROM THE DATA RECORDED IN THE E.A. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Oct 16, 2006 · N584FE · Doug MD11 · Trailing Edge FlapsSDR 06FDEA03596Seat Track · corrodedMAIN DECK CARGO, FOUND SEAT TRACK FLANGE AT STA 1300 RBL 78 CORRODED. CORRODED SEAT TRACK ON MAIN DECK CARGO, STA 1300 RBL 78 TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG.1, VOL.I. REFER TO SNRM N00966 FOR FURTHER WORK DETAILS. REPAIR CLASSIFIOct 9, 2006 · N584FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03592Floorbeam · corrodedMAIN DECK CARGO, ON FLOOR PANEL OPEN UP FOUND UNDERFLOOR STRUCTURE AT STA 1225 RBL 4 WITH CORROSION. CORROSION ON MAIN DECK CARGO ON FLOOR PANEL UNDERFLOOR STRUCTURE AT STA 1225 RBL 4 REMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND EXCEEDED LIMIT AS PER SOct 4, 2006 · N584FE · Doug MD11 · Fuselage Main, Floor BeamSDR 06FDEA03591Floorbeam · corrodedFOUND CENTER CARGO COMPARTMENT, FLOOR PANEL SUPPORT CORRODED AT STA 1841 RBL 54. REPAIR CARRIED OUT AS PER FEDEX E.A. 1-5310-104803.Oct 4, 2006 · N584FE · Doug MD11 · Fuselage Main, Floor BeamSDR 06FDEA03590Longeron · crackedFOUND CENTER CARGO COMPARTMENT BILGE AREA, LONGERON 50L SUSPECT CRACK AT STA 1709. REPAIR CARRIED OUT AS PER SRM 53-10-00.Oct 4, 2006 · N584FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 06FDEA03582Seat Track · corrodedMAIN DECK CARGO, FOUND SEAT TRACK FLANGE AT STA 1400 LBL 8 CORRODED. TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 53- 70-00 FIG.1, VOL.I FROM STA 1360 TO STA 1440, LBL 8. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Oct 3, 2006 · N584FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03581Seat Track · corrodedMAIN DECK CARGO, FOUND SEAT TRACK FLANGE AT STA 1310 RBL 78 CORRODED. REPAIRED SEAT TRACK FABRICATED AND INSTALLED AS PER SRM 53-70-00, FIG.1, VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 3, 2006 · N584FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03554Seat Track · corrodedMAIN DECK CARGO, FOUND SEAT TRACK FLANGE CORRODED AT STA 1258 RBL 78. SEAT TRACK REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REFER TO SNRM N00898 FOR FURTHER WORK DETAILS. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.Oct 3, 2006 · N584FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA03553Seat Track · corrodedMAIN DECK CARGO, FOUND SEAT TRACK FLANGE CORRODED AT BS 1230 AND 1240 RBL 78. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIG. 1 VOL. I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Oct 3, 2006 · N584FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03551Skin · crackedRIGHT WING, FIXED LEADING EDGE SKIN AT NR 14 TRACK CUTOUT FOUND CRACKED. CUTOUT TRIMMED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR DOUBLER AND FILLER FABRICATED AS PER SRM 57- 10-00 FIGURE 21 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REOct 3, 2006 · N584FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03546Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 765 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT HAND WING FIXED LEADING EDGE AT XOS 698 REPAIRED AS PER FEDEX E.A. 1-5730-104794, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Oct 2, 2006 · N584FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03545Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 730 FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-104794.Oct 2, 2006 · N584FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03544Skin · crackedRIGHT WING, FIXED LEADING EDGE AT TELESCOPIC DUCT CUTOUT SKIN CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-104793.Oct 2, 2006 · N584FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03528Spar Cap · corrodedLEFT WING REAR SPAR LOWER CAP AFT FLANGE FOUND WITH CORROSION AT STA XORS 1045. REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 57-20-00 FIGURE 16 VOLUME I. REPAIR CARRIED OUT ON EXCEEDED LIMIT AREA AS PER FEDEX E.A. 1-5710-104798Oct 2, 2006 · N584FE · Doug MD11 · Wing SparSDR 06FDEA03527Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT STA XOS 623 TO 627 FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-104791.Oct 2, 2006 · N584FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03526Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT STA XOS 630 TO 634 FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-104791.Oct 2, 2006 · N584FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA03475Stringer · crackedCRACK FOUND DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF STRINGER 16 (UPPER STRINGER) AT APPROX XORS 386. REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I AND FEDEX E.A. 1-5710-104796.Sep 29, 2006 · N584FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03474Stringer · crackedCRACK FOUND DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF STRINGER 12 (UPPER STRINGER) AT APPROX XORS 642. REPAIRED AS PER SRM 57-20-00.Sep 29, 2006 · N584FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03473Stringer · crackedCRACK FOUND DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF STRINGER 13 (UPPER STRINGER) AT APPROX XORS 577. REPAIRED AS PER SRM 57-20-00.Sep 29, 2006 · N584FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03472Stringer · crackedCRACK FOUND DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF STRINGER 14 (UPPER STRINGER) AT APPROX XORS 521. REPAIRED AS PER SRM 57-20-00.Sep 29, 2006 · N584FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03471Skin · crackedLEFT WING ANTI-ICING TELESCOPIC DUCT DOOR CUT OUT BOTH CORNER FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-104789.Sep 29, 2006 · N584FE · Doug MD11 · Wing, Plate/SkinSDR 05FDEA01576Static Port · corrodedFUSELAGE, LEFT HAND PRIMARY STATIC PORT (PRESSURE COMPENSATING PLATE ASSEMBLY) EXTERIOR SURFACE FOUND WITH SEVERAL PIT MARKS. FUSELAGE, LEFT HAND PRIMARY STATIC PORT REMOVED AND REPLACED PER AMM 34-11-03-4. CRITICAL WAVINESS CHECK COMPLIED WITH PER WORK CARDJun 10, 2005 · N584FE · Doug MD11 · Flight Environment DataSDR 05FDEA01578Fitting · corrodedCENTER LANDING GEAR WHEEL WELL, RIGHT HAND TRUNNION SUPPORT FITTING GUIDE PIN HOLE BUSHING CORRODED. CENTER LANDING GEAR WHEEL WELL, RIGHT HAND TRUNNION SUPPORT FITTING GUIDE PIN HOLE CORROSION REMOVED PER SRM 53-40-00 VOLUME I, FIGURE 15. FINAL HOLE DIAMETEJun 10, 2005 · N584FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 05FDEA01577Fitting · corrodedCENTER LANDING GEAR WHEEL WELL, LEFT HAND TRUNNION SUPPORT FITTING GUIDE PIN HOLE BUSHING CORRODED. CENTER LANDING GEAR WHEEL WELL, LEFT HAND TRUNNION SUPPORT FITTING GUIDE PIN HOLE CORROSION REMOVED PER SRM 53-40-00 VOLUME I, FIGURE 15. FINAL HOLE DIAMETER Jun 10, 2005 · N584FE · Doug MD11 · Fuselage, Landing Gear Attach FittingsSDR 05FDEA01555Skin · damagedNR 1 ENGINE, NOSE COWL AT APPROXIMATELY SEVEN O' CLOCK POSITION EXTERIOR SURFACE FOUND WAVINESS. NR 1 ENGINE, NOSE COWL REMOVED AND REPLACED PER AMM 71-11-01-4.Jun 9, 2005 · N584FE · Doug MD11 · Nacelle/Pylon, Plate/SkinSDR 05FDEA01552Floorbeam · corrodedUPPER CARGO COMPARTMENT, FLOOR PANEL SUPPORT AT STA 1321, X= -33 TO -75 FOUND CORRODED. (PANEL 262EF AND 262LF). UPPER CARGO COMPARTMENT, FLOOR PANEL SUPPORT AT STA 1321, X= -33 TO -75 REMOVED AS PER SRM 51-35-01 VOLUME II. NEW REWORKED FLOOR PANEL SUPPORT Jun 8, 2005 · N584FE · Doug MD11 · Fuselage Main, Floor BeamSDR 05FDEA01514Support Bracket · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE) OUTBOARD CENTER AND AFT BOLT HOLES FOUND CORRODED DURING ACCOMPLISHMENT OF EA 1-5750-83126. REMOVED AND REPAIRED PER FEDEX EA 1-5750-86625.Jun 2, 2005 · N584FE · Doug MD11 · Trailing Edge FlapsSDR 05FDEA01507Seat Track · corrodedMAIN DECK CARGO, SEAT TRACK AT STA 5-0 TO STA 5-35, X = -9 FOUND CORRODED. MAIN DECK CARGO, SEAT TRACK AT STA 5-0 TO STA 1531, X = -9 REMOVED AND REPLACED AT EXISTING SPLICES PER SRM 53-70-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100Jun 1, 2005 · N584FE · Doug MD11 · Fuselage, Seat/Cargo Attach Fittings
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