N523FE

Service difficulty reports · 372

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 = 'N523FE' 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 FDEA201502030419Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, ACTUATOR ATTACH OTBD LUG BORE FOUND CORRODED. FOUND TO BE OUT OF LIMITS IAW CMM 57-44-08. REPAIRED IAW EA 1-5750-T0315337 PART 1 STEP 1 AND 1B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201502030418Hinge Bracket · corrodedLEFT WING OTBD FLAP, INBD FWD HINGE BRACKET, ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. REPAIRED IAW EA 1-5750-T0315337 PART 1 STEP 1 AND 1B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201502030416Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET, ACTUATOR ATTACH INBD LUG BORE FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA1-5750-T0315330 REV A PART 1 STEP 1 AND 1B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201502030415Hinge Bracket · corrodedLEFT WING OTBD FLAP, OTBD FWD HINGE BRACKET FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0315330 REV A PART 1 STEP 1 AND 1A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201502030414Hinge Bracket · corrodedLEFT WING OTBD FLAP FWD HINGE BRACKET FOUND CORRODED. FOUND OUT OF LIMITS IAW CMM 57-44-09 . REPAIRED IAW EA 1-5750-T0315330 REV A PART 1 STEP 1 AND 1A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201502030417Angle · crackedLEFT WING FIXED LE FWD INTERIOR ANGLE FOUND CRACKED AT XOS 666. REPAIRED IAW SRM 57-40-03 FIGURE 202 REPAIR 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201502030413Doubler · crackedLEFT WING FIXED LE RIB DOUBLER FOUND CRACKED AT XOS 667. DOUBLER REMOVED IAW SRM 51-31-01. FABRICATED NEW DOUBLER IAW DRAWING ARB3954 REVISION K. INSTALLED THE NEW DOUBLER IAW SRM 51-33-01. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Feb 3, 2015 · N523FE · Doug MD11F · Wing, Rib/BulkheadSDR FDEA201501310402Frame · dentedCABIN RT STATION 1741, LONGERON 12 RT FRAME FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jan 31, 2015 · N523FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201501310401Skin · crackedRIGHT WING SLAT TRACK NR 12 CUT OUT OTBD CORNER CRACKED AT XOS 775. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jan 31, 2015 · N523FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201501300392Seat Track · corrodedCABIN MAIN DECK CARGO BAY BS 1209, X 8.5 SEAT TRACK FOUND CORRODED. SEAT TRACK REPAIRED IAW SRM 53-00-52 FIGURE 201 REPAIR 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jan 30, 2015 · N523FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201407021610Unknown · malfunctionedON 2 SEPARATE ATTEMPTS, EMER POWER TEST FAILED, DURING PREFLIGHT. DOWN POWERED ACFT & RE-POWERED ACFT. PERFORMED EMER POWER TEST IAW AMM 24-00-01-5. OPERATIONS CHECKED NORMAL. NO HISTORY, OK FOR SERVICE.Jul 2, 2014 · N523FE · Doug MD11F · DC Generating SystemSDR FDEA201406251547Engine · failedON DEPARTURE ROLL TPE 23R APPROACHING 100 KTS EXPERIENCED NR 1 ENG FAILURE. REJECT PERFORMED, ACFT TOWED BACK TO GATE TIME 1349. ENG FIRE AGENT DISCHARGED IAW QRH PROCEDURE. NR 1 ENG REMOVAL & REPLACEMENT ACCOMPLISHED.Jun 25, 2014 · N523FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA201404240836Blocker Door · damagedNR 3 ENGINE THRUST REVERSER LT HALF NR 1 & 2 BLOCKER DOORS FROM THE TOP DAMAGED. REMOVED NR 3 THRUST REVERSER IAW WIC 78T1003-L. OPS CHECKED GOOD.Apr 24, 2014 · N523FE · Doug MD11F · Engine Thrust ReverserSDR FDEA201306081229Battery · inoperativeDURING SERVICE CHECK FOUND PUSH TO TEST LIGHT ON R1 DOOR SLIDE REMOTE INDICATOR INOPERATIVE. R & R BATTERIES ON THE PUSH TO TEST LIGHT ON R1 DOOR SLIDE REMOTE INDICATOR ASSY IAW MM 25-61-04-4 INDICATION NORMAL.Jun 8, 2013 · N523FE · Doug MD11F · Escape SlideSDR FDEA201304090746Wire Harness · shortedLEVEL 3, FIRE WARNING NR 3 IN FLIGHT. USED BOTH FIRE EXTINGUISHING BOTTLES. LANDED UNEVENTFULLY. FOUND PYLON LOOP A HARNESS CREATING THE HIGH RESISTANCE READING. R & R WIRE HARNESS. ENGINE RUN OPS CHECKED NORMAL, RAN ENGINE TO HIGH POWER IAW JRH APROXIMAApr 9, 2013 · N523FE · Doug MD11F · Fire Protection System WiringSDR FDEA201303060501Door Frame · misrepairedR2 DOOR LOWER FRAME AFT END LONGERON 27, RT BS 850 MISREPAIRED. REPAIRED IAW EA 1-5310-163599, PART 1.Mar 6, 2013 · N523FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201302270465Bulkhead · corrodedCENTER CARGO COMPARTMENT BULKHEAD PANEL FOUND CORRODED AT BS 1841, "X" = 15 TO "X" =24. BULKHEAD PANEL REMOVED AND REPLACED WITH NEW FABRICATED AS PER SRM 51-35-01 REVISION 51. WEB FABRICATED IAW DRAWING AYG7170 REVISION T. REPAIR CLASSIFIED AS MAJOR AS PER GFeb 27, 2013 · N523FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201302240422Web · crackedAVIONICS COMPARTMENT CEILING - APPROX BS 360, COCKPIT OBSERVER SEAT VERTICAL GEAR FEED THROUGH CUTOUT FOUND WEB CRACKED. REPAIRED IAW SRM 53-10-51 FIGURE 201 REPAIR 1 REVISION 51. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.Feb 24, 2013 · N523FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201302220416Door Frame · crackedMAIN DECK R3 DOOR FORWARD FRAME WEB FOUND CRACKED. REPAIRED AS PER SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.Feb 22, 2013 · N523FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201302220415Longeron Splice · crackedCENTER CARGO COMPARTMENT LONGERON SPLICE 38L BETWEEN BS 5-113 AND 1541 FOUND CRACKED. REMOVED AND REPLACED WITH NEW LONGERON SPLICE AS PER SRM 51-33-01 REVISION 51. LONGERON SPLICE FABRICATED AS PER DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GFeb 22, 2013 · N523FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201302220414Longeron Splice · crackedCENTER CARGO COMPARTMENT LONGERON SPLICE 39L BETWEEN BS 5-113 AND 1541, FOUND CRACKED. REMOVED AND REPLACED WITH NEW, FABRICATED LONGERON SPLICE IAW SRM 51-33-01 REVISION 51 & DRAWING A5A7114 REVISION J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116Feb 22, 2013 · N523FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201302220413Longeron Splice · crackedCENTER CARGO COMPARTMENT LONGERON SPLICE 37R. FOUND CRACKED BETWEEN BS 5-113 AND 1541. REPAIRED IAW SRM.Feb 22, 2013 · N523FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201302220412Frame · dentedMAIN DECK FRAME AT BS 1741, LONGERON 12L, FOUND DENT. REPAIRED AS PER SRM 53-00-07, FIGURE 201, REPAIR 2, REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 116.Feb 22, 2013 · N523FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201302220411Frame · dentedMAIN DECK AT BS 1721 LONGERON 12L, FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.Feb 22, 2013 · N523FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201302220410Frame · dentedMAIN DECK FRAME FOUND DENTED AT BS 1681, LONGERON 12L. REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.Feb 22, 2013 · N523FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201302220409Spar · crackedEMPENNAGE - LOWER VERTICAL STABILIZER NR 2 ENGINE INTAKE DUCT LT REAR CENTER SPAR TO REAR SPAR FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 REPAIR 2 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.Feb 22, 2013 · N523FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201302220407Spar · crackedEMPENNAGE - LOWER VERTICAL STABILIZER NR 2 ENG INLET DUCT RT CENTER SPAR TO REAR SPAR FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 REPAIR 2 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 116.Feb 22, 2013 · N523FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA201302210397Skin · delaminatedLT WING OTBD FLAP INBD LOWER T/E DELAMINATED. REPAIRED IAW EA 1-5750-163594. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115Feb 21, 2013 · N523FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201302210399Skin · crackedFOUND NINE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS 683.4 AND XORS 713.6. REPAIR CARRIED OUT IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 51. REPAIR CLASSIFIED Feb 21, 2013 · N523FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201302210398Skin · crackedFOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS 683.4 AND XORS 713.6. REPAIR CARRIED OUT IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJFeb 21, 2013 · N523FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201111305096Battery · dischargedON PREFLIGHT EMERGENCY POWER TEST FAILED AFTER ABRUPT POWER LOSS AND REINSTATEMENT. "ADG BATTERY CTL RLYINTFC" IN CFDS MESSAGE. POWERED DOWN AND WAITED FOR BATTERY TO BE CHARGED. EMERGENCY POWER TEST PASSED IAW MM 24-34-02-5. ACFT OK FOR SERVICE.Nov 30, 2011 · N523FE · Doug MD11F · Battery/Charger SystemSDR FDEA201108123239Battery · inoperativeR1 DOOR SLIDE PRESSURE INDICATION PRESS TO TEST INOPERATIVE. REPLACED BATTERIES PER MM 25-61-04-0 -- TESTED GOOD.Aug 12, 2011 · N523FE · Doug MD11F · Escape SlideSDR FDEA201107222893Controller · malfunctionedAFTER PUSH BACK AND ALL 3 ENGINES START RECEIVED CARGO FIRE LWR FWD LEVEL 3 ALERT WITH TRITONE SEVERAL TIMES FOLLOWED BY CARGO FIRE AGENT DISCHARGE SWITCH FLASHING. FOLLOWED QRH DISCHARED 1 FIRE BOTTLE. R & R THE MISCELLANEOUS SYSTEMS CONTROLLER AS A PRECAUTJul 22, 2011 · N523FE · Doug MD11F · Fire DetectionSDR FDEA201103211105Channel · crackedLOWER FD CARGO COMPARTMENT STA 919 X 40 CHANNEL ASSY FOUND HOLE PUNCTURED, DAMAGED. LOWER FORWARD CARGO COMPARTMENT STA 919 X 40 CHANNEL ASSEMBLY REMOVED AND REPLACED AS PER AMM 20-50-02 REVISION 69.1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 1Mar 21, 2011 · N523FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201103161028Longeron Splice · crackedLOWER FWD CARGO COMPARTMENT BILGE AREA STA 6-05, LONGERON 52. SPLICE FITTING FOUND CRACKED. REMOVED AND NEW SPLICE FITTING P/N FXADA8424-527 INSTALLED AS PER SRM 51-33-01 REVISION 45. NEW SPLICE FITTING. FABRICATED AS PER DRAWING ADA8424 REVISION A. REPAIR Mar 16, 2011 · N523FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201103161007Doubler · crackedCENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD AREA RIGHT HAND SIDE DOUBLER FOUND CRACKED. CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD AREA RIGHT HAND SIDE DOUBLER FABRICATED AS PER DRAWING AEA0526 REVISION NC. DOUBLER REMOVED AND REPLACED AS PER SRMar 16, 2011 · N523FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201103161006Doubler · crackedCENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD AREA LEFT HAND SIDE DOUBLER FOUND CRACKED. CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD AREA LEFT HAND SIDE DOUBLER FABRICATED AS PER DRAWING AEA0526 REVISION NC. DOUBLER REMOVED AND REPLACED AS PER SRM 51Mar 16, 2011 · N523FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201103161004Frame · corrodedLOWER AFT CARGO COMPARTMENT STATION 1841 X-22 WEB FRAME FOUND CORROSION. AFT CARGO COMPARTMENT STATION 1841 X-22 FRAME WAS FABRICATED AS PER DOUGLAS DRAWING AGA 7170 REVISION R. FRAME WAS REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. REPAIR CLASSIFIEDMar 16, 2011 · N523FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201103140960Vane · delaminatedLEFT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATION. LEFT WING INBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 69.1. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-830-801 REVISION 69.1 SATIS.Mar 14, 2011 · N523FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201103140959Skin · crackedLEFT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE CRACKED TELESCOPIC DUCT CUTOUT CARRIED OUT REPAIR AS PER SRM 57-40-01 FIG 201 REPAIR 10 REVISION 45. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 1Mar 14, 2011 · N523FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201103140957Frame · dentedCABIN RIGHT BS 1701 L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG 201 REVISION 45. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 112. INITIAL INSPECTION TO BE CARRIED OUT AT 14500 CYCLE AND REPETITIVE INSPECTION AT 9500 USING HFEC METHMar 14, 2011 · N523FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200906152099Fuel Tank · corrodedCORROSION - BS 1227 X=-96 AT UPP SURFACE OF CENTER AUX FUEL TANK AT MAIN DECK CARGO FLOOR. CORROSION BLENDED WITHIN LIMIT IAW SRM 57-20-00 FIG 13 VOL 1 REV 40 AND EA 1-5710-132104.Jun 15, 2009 · N523FE · Doug MD11F · Fuel StorageSDR FDEA200906152097Fuel Tank · corrodedCORROSION - STA1227 X=105 AT UPP SURFACE OF CENTER AUX FUEL TANK AT MAIN DECK CARGO FLOOR. CORROSION BLENDED WITHIN LIMIT IAW SRM 57-20-00 FIG 13 VOL 1 REV 40 AND EA 1-5710-132104.Jun 15, 2009 · N523FE · Doug MD11F · Fuel StorageSDR FDEA200906122043Longeron · crackedDURING HFEC INSP CARRIED OUT ON NLG LT TRUNNION FITTING FWD AREA, FOUND CRACK ON THE NEARBY LONGERON. NLG LT TRUNNION FITTING FWD AREA DAMAGED LONGERON REMOVED AND REPLACED IAW SRM 51-31-01 VOL II REV 40, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 107.Jun 12, 2009 · N523FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200906112019Frame · bentBENT FRAME FLANGE AT LT STA 1701 LONGERON 12 IN MAIN DECK CARGO. FRAME REPAIRED IAW SRM 53-30-00 FIG 1 VOL 1 REV 40. CAT B REPAIR REQUIRE INITIAL INSP AT 14500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYCLES (MAJOR REPAIR).Jun 11, 2009 · N523FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200906102001Seat Track · corrodedMAIN DECK CARGO FLOOR SEAT TRACK X= -8.5 CROWN FOUND CORRODED AT STA 1451. REPAIRED IAW SRM 53-70-00 FIG1 VOL1 REV40 (MAJOR REPAIR).Jun 10, 2009 · N523FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906102000Seat Track · corrodedMAIN DECK CARGO FLOOR SEAT TRACK X= -8.5 CROWN FOUND CORRODED AT STA 1521. REPAIRED IAW SRM53-70-00, FIG1, VOL1 REV40 REFER TO SNRM N00347 FOR DETAIL (MAJOR REPAIR).Jun 10, 2009 · N523FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906091986Trunnion · crackedCRACK 1 INCH FOUND AT FUSELAGE STA 580 FWD OF NOSE GEAR RT TRUNNION FITTING. REPAIR CARRIED OUT AS PER SRM 53-40-00 FIG 23 VOL I REV 40, (MAJOR CAT B REPAIR)Jun 9, 2009 · N523FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA200906081964Seat Track · corrodedMAIN DECK CARGO FLOOR, SEAT TRACK X = 8.5 AT STA 1212, CROWN BASE FOUND CORRODED. SEAT TRACK REPAIRED IAW SRM 53-70-00 FIG1 VOL1 REV40 (MAJOR REPAIR).Jun 8, 2009 · N523FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906081963Skin · crackedRT WING - NR 3 L/E SLAT TELESCOPIC DUCT CUTOUT INBD AND OTBD CORNER FOUND CRACKED. REPAIRED IAW SRM57-10-00 FIG43, VOL1 REV40.Jun 8, 2009 · N523FE · Doug MD11F · Wing, Plate/Skin
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