N573FE

Service difficulty reports · 220

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 = 'N573FE' 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 FDEA201307081506Skin · puncturedLT WING FIXED L/E EXTERIOR SKIN, XOS 615 - 640, FOUR PUNCTURES. REPAIRED IAW EA 1-5730-T0301138 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.Jul 8, 2013 · N573FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201307021457Skin · delaminatedRT OTBD AILERON T/E WEDGE FOUND DELAMINATED AS MARKED AT INBD CORNER BETWEEN XOA 848.3 TO XOA 866. REPAIRED IAW EA 1-5750-T0300983A, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 116.Jul 2, 2013 · N573FE · Doug MD11F · AileronsSDR FDEA201307021456Vane · delaminatedRT INBD T/E FLAP VANE FOUND DELAMINATION AT LOWER SURFACE, BETWEEN INBD TRACK AND CENTER TRACK AREA. STATION XIFH 141.375 TO XIFH 183.300. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP VANE AS PER AMM 27-50-22-4, REV. 76.1. CARRIED OUT FLAP VANE ADJUSTMENT TJul 2, 2013 · N573FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201306271407Frame · chafedMAIN DECK CARGO COMPARTMENT BS 535, LONGERON NR 19L TO NR 21L AT YOKE ATTACHED FITTING EXISTING REPAIR OUTER ANGLE FOUND CHAFED. REMOVED AND REPLACED IAW SRM 53-20-07, FIGURE 202, REPAIR 1, REV. 52. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REV 116.Jun 27, 2013 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201306251392Doubler · crackedLT WING L/E LOWER COMPARTMENT, CRACK FOUND ON BEADED DOUBLER STIFFENER, XOS= 668 AND ZOS 35, OTBD OF SLAT TRACK NR 10. IAW DWG ARB3954, REV K AND SRM 51-33-01, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Jun 25, 2013 · N573FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201306251390Skin · dentedCENTER CARGO DOOR CUTOUT LOWER AFT FOUND DENTED BS 1781 RT BETWEEN LONGERON 40R TO 41R. REPAIRED IAW SRM 53-00-15, REPAIR 8, FIG. 202, REV. 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV. 116. TO CARRY OUT INSPECTION AS PER SRM 53-00-15, TABLE 201, FJun 25, 2013 · N573FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201306251389Beam · corrodedCENTER WHEEL WELL RT DIAGONAL BOOT STRAP HAS CORROSION. BS 1461 TO 1490, WL 100. REMOVED AND REPLACED PER SRM 51-31-01, REV. 52. NEW BOOT STRAP FABRICATED PER EA 1-5310-T0300908, PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV. 116.Jun 25, 2013 · N573FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201306251388Beam · corrodedCENTER WHEEL WELL LT DIAGONAL BOOT STRAP HAS CORROSION BS 1461 TO 1490, WL 100. REMOVED AND REPLACED IAW SRM 51-31-01, REV. 52. STRAP FABRICATED IAW EA 1-5310- T0300892, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 116.Jun 25, 2013 · N573FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201211244148Battery · inoperativeDURING SERVICE CHECK, FOUND L1 DOOR ESCAPE SLIDE PRESS TO TEST LIGHT NOT ILLUMINATING. GAINED ACCESS TO L1 SLIDE PRESS TO TEST BATTERIES. REPLACED BATTERIES, RESECURED SLIDE COVER, OPS CK GOOD REF AMM 25-61-15-4.Nov 24, 2012 · N573FE · Doug MD11F · Escape SlideSDR FDEA201205211914Retainer · brokenDOOR EMERGENCY EXIT LIGHT LENS ASSY WILL NOT STAY IN PLACE. REPLACED BROKEN RETAINERS IAW SMP. OPS CKS OK. OK FOR SERVICE.May 21, 2012 · N573FE · Doug MD11F · Emergency LightingSDR FDEA201203170990Seal · leakingNR 2 ENGINE OIL QUANTITY DECREASED TO ZERO OVER SEVERAL HOURS, OIL PRESSURE AND TEMPRATURE GOOD UNTIL SHUTDOWN, ENROUTE WHEN OIL PRESSURE DROPPED TO 10 PSI AT IDLE THRUST. SHUTDOWN ENGINE AT THAT TIME. AFTER BLOCKIN, FOUND OIL DRIPPING FROM NR 2 ENG EXHAUSTMar 17, 2012 · N573FE · Doug MD11F · Turbine Engine Oil SystemSDR FDEA201111194984Brake · contaminatedAFTER LANDING TOWER REPORTED SMOKE FROM LT GEAR AREA. INSPECTED BY ANC AIRPORT STAFF, ALL LOOKED OK, TAXIED TO RAMP. APPARENTLY EXCESS LUBRICATION ON LANDING GEAR DEPOSITED ONTO BRAKE ASSY INSPECTED LT GEAR NO LEAKS OR DEFECTS NOTED OK FOR SVC. (FINAL CLOSENov 19, 2011 · N573FE · Doug MD11F · BrakeSDR FDEA201107293017Panel · crackedEMPENNAGE - NR 2 ENGINE RT AIR INTAKE REAR INTERIOR SUPPORT STRUCTURE (364RR) FOUND SUSPECTED CRACKED. REPAIRE CARRIED OUT AS PER EA 1-5530-143624. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.Jul 29, 2011 · N573FE · Doug MD11F · Engine Air Intake SystemSDR FDEA201107262957Skin · crackedRT WING L/E TELESCOPIC DUCT CUTOUT OTBD CORNER SKIN AT XOS 470 FOUND CRACKED. REPAIR CARRIED OUT PER SRM 57-40-01 FIG. 202 REV.47 .REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV.112Jul 26, 2011 · N573FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201107262977Stop Fitting · crackedFWD CABIN - R1 ENTRY DOOR AFT STOP FITTING NR 2 FROM BOTTOM, FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201107262976Frame · dentedFUSELAGE FRAME DENTED AT STA 1741 L12R/L. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262975Frame · dentedMAIN DECK FUSELAGE FRAME DENTED AT STA 1701, L12R. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262974Frame · dentedMAIN DECK FUSELAGE FRAME DENTED AT STA 1681, L12L. REPAIRED AS PER SRM 53-00-07 FIG.201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262973Frame · crackedFUSELAGE FRAME CRACKED AT STA 1721, L12R. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262972Frame · dentedFUSELAGE FRAME DENTED AT STA 1701, L12L. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262971Frame · dentedFUSELAGE FRAME DENTED AT STA 1641 L12L. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262970Frame · damagedFUSELAGE FRAME AT STA 535 L24L, FOUND WITH TOOL MARKS. REPAIRED AS PER DWG SG10530002. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV.112Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262968Frame · damagedFUSELAGE FRAME AT STA 535 L20L, FOUND WITH TOOL MARKS. REPAIRED AS PER DWG SG10530002. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-10 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262966Frame · dentedFUSELAGE FRAME DENTED AT STA 1721, LT L12. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262965Frame · dentedFUSELAGE FRAME DENTED AT STA 1661, LT L12. REPAIRED AS PER SRM 53-00-07 FIG.201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262964Frame · crackedFUSELAGE FRAME CRACKED AT STA 1712, RT L12. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262963Frame · dentedMAIN DECK FUSELAGE FRAME DENTED AT STA 1741, LT L12. REPAIRED AS PER SRM 53-00-07 FIG 201 REV 47. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262961Seat Track · wornMAIN DECK SEAT TRACK LOBE WORN AT STA 755 X=-8. REPAIRED AS PER SRM 53-00-52 FIG 201 REV 47. SEAT TRACK FABRICATED AS PER DRAWING ADA7321. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.Jul 26, 2011 · N573FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107262960Skin · dentedRT WING INBD FLAP, INBD SEGMENT UPPER SKIN FOUND SEVERAL DENTS. DENTED AREAS ARE ACCEPTABLE AND WITHIN ALLOWABLE DAMAGED LIMIT OF 0.060" AS PER SRM 51-80-01 REV 47 AT RIGHT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SKIN. HFEC INSPECTION CARRIED OUT AS PERJul 26, 2011 · N573FE · Doug MD11 · Trailing Edge FlapsSDR FDEA201107262959Skin · dentedLT WING INBD FLAP, INBD SEGMENT UPPER SKIN FOUND SEVERAL DENTS. DENTED AREAS ARE ACCEPTABLE AND WITHIN ALLOWABLE DAMAGED LIMIT OF 0.060" PER SRM 51-80-01 REV 47 AT LEFT HAND WING INBOARD FLAP INBOARD SEGMENT UPPER SKIN. HFEC INSPECTION CARRIED OUT AS PER DAJul 26, 2011 · N573FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201107262958Skin · dentedLT WING INBD FLAP, OTBD SEGMENT UPPER SKIN FOUND SEVERAL DENTS. DENTED AREAS ARE ACCEPTABLE AND WITHIN ALLOWABLE DAMAGED LIMIT OF 0.060" AS PER MD-11 SRM 51-80-01 REV 47 AT LEFT HAND WING INBOARD FLAP OUTBOARD SEGMENT UPPER SKIN. HFEC CARRIED OUT AS PER DACJul 26, 2011 · N573FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201107262969Frame · dentedFUSELAGE FRAME DENTED AT STA 1661 L12R. REPAIRED IAW SRM 53-00-07, FIG 201, REV 47. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107262967Frame · dentedFUSELAGE FRAME DENTED AT STA 1661, RT L12. REPAIRED IAW SRM 53-00-07, REV 47. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 112.Jul 26, 2011 · N573FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201107072605Engine · failedNR 3 ENGINE N1 STOPPED AT APPROX 101 PERCENT. OTHERS ALREADY STABILIZED AT 111.4 PERCENT. PUSHED NR 3 THROTTLE UP AND GOT SLOW CONTINUOUS ACCELERATION. REJECT T/O FOR NR 3 ENGINE N1 TOO LOW. NR1 AND NR2 N1 AT 111.4 , NR3 N1 AT 101.2 . TRIED PUSHING NR 3 Jul 7, 2011 · N573FE · Doug MD11F · Engine (Turbine/Turboprop)SDR FDEA201101090104Indicator · intermittentLT L1 DOOR SLIDE TEST LIGHT ASSY, INTERMITTENT. REMOVED AND REPLACED THE REMOTE PRESSURE INDICATOR ASSEMBLYJan 9, 2011 · N573FE · Doug MD11F · Escape SlideSDR FDEA201012034557Switch · malfunctionedCAN OPEN R L1 PASSENGER DOOR CAN NOT OPEN ELECTRICALLY , UNLESS MANUALLY HOLD THE ARM HANDLE AT DISARM POSITION. MEL 03DEC10 19:03, CAN R RELEASED FOR SERVICE IAW MEL: 52-10-01. R & R DOOR CONTROL INTERLOCK SWITCH S1-1090, AND GIRT BAR ARMED WARNING SWITCDec 3, 2010 · N573FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA200909143298Door · out of alignmentDURING LWR AFT CARGO DOOR OPERATION FOUND DOOR UNABLE TO CLOSE DUE TO INTERFERENCE AT FWD LWR CORNER. AFT CARGO DOOR REMOVED AND REINSTALLED IAW AMM 52-33-04-4 REVISION 64. AFT CARGO DOOR HINGE REPAIR BUSHING FABRICATED AND INSTALLED IAW SRM 52-30-16 FIG 1Sep 14, 2009 · N573FE · Doug MD11 · Cargo/Baggage DoorsSDR FDEA200909143297Skin · erodedLT WING - NR 5 SPOILER T/E LWR SURFACE FOUND 02 EACH LOCATIONS, ERODED. REPAIR CARRIED OUT IAW EA 1-5770-132216. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 107.Sep 14, 2009 · N573FE · Doug MD11 · SpoilersSDR FDEA200908243075Skin · gougedFUSELAGE SKIN ADJACENT TO NOSE JACK POINT FOUND WITH DEEP SCRATCH MARK, SKIN. REPAIR CARRIED OUT IAW SRM 53-20-01 REPAIR 2, FIG 201, REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 107.Aug 24, 2009 · N573FE · Doug MD11 · Fuselage Main, Plate/SkinSDR FDEA200908193047Seat Track · corrodedCABIN - LT SEAT TRACK CROWN AREA AT STA 6-10 TO STA 6-30, X = -8.5 FOUND SURFACE CORROSION. REMOVED AND FOUND EXCEEDED LIMIT IAW SRM 53-00-52, FIG 201, REVISION 41. SEAT TRACK SPLICE REPAIR CARRIED OUT FROM STA 6-0 TO STA 6-25, X = -8.5 IAW SRM 53-00-52, Aug 19, 2009 · N573FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200908193046Skin · corrodedAFT ACCESSORY COMPARTMENT RT SKIN BETWEEN STA 2140 AND STA 2163 (ACCESS PANEL NR347DF LWR ANCHOR NUT MOUNTING AREA) FOUND WITH SEVERE CORROSION. REPAIRED AS PER SRM 53-70-01 FIGURE 201 REVISION 41. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.Aug 19, 2009 · N573FE · Doug MD11 · Fuselage Main, Plate/SkinSDR FDEA200908173033Structure · unknownRT HORIZONTAL STABILIZER AFT OPERATING BULKHEAD TRIMMED FOR BARREL NUT HOLE NR 35R REWORK ACCESS AND FOUND EXCEEDED EO LIMITS. COMPLIED WITH EA NR 1-5510-131640, TITLE: STABILIZER - HORIZ (AD 2003-22-08, EO 1-5510-7-5000) - RT OPERATING BULKHEAD FITTING TRIAug 17, 2009 · N573FE · Doug MD11 · Horizontal Stabilizer StructureSDR FDEA200908173032Hinge Bracket · corrodedLT WING OTBD FLAP, OTBD HINGE (WING SIDE) SIDELINK LWR HOLE FOUND CORRODED. COMPLIED WITH EA 1-5750-132180. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 17, 2009 · N573FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA200908163026Support Fitting · crackedCRACK INDICATION FOUND DURING HEFC OPEN HOLE INSPECTON ON LEFT WING OUTBOARD FLAP HINGE SUPPORT FITTING, MOST OUTBOARD FASTENER HOLE AT 3 O' CLOCK POSITION LOOKING AFT. REPAIR CARRIED OUT IAW EA NR 1-5750-132199. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMMAug 16, 2009 · N573FE · Doug MD11 · Wing Miscellaneous StructureSDR FDEA200908163025Support Fitting · crackedCRACK INDICATION FOUND DURING HEFC OPEN HOLE INSPECTON ON RIGHT WING OUTBOARD FLAP HINGE SUPPORT FITTING MOST OUTBOARD FASTENER HOLE AT 7 O'CLOCK POSITION LOOKING AFT. REPAIR CARRIED OUT IAW EA NR 1-5750-132200. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-Aug 16, 2009 · N573FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR FDEA200908163024Skin · damagedLEFT WING NR 8 SLAT INTERIOR SURFACE SKIN INBOARD TOP CORNER FOUND CHIPPED-OFF AT XOS 1005. CARRIED OUT REPAIR IAW SRM 57-40-01 FIG 201 REPAIR 3, REV 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Aug 16, 2009 · N573FE · Doug MD11 · Leading Edge DevicesSDR FDEA200908153021Skin · corrodedHORIZONTAL STABILIZER LEFT PLANK 36L BARREL NUT BORE BEARING AREA CORROSION REWORK EXCEEDED E.O. 1-5510-7-5000D1 PART 1 LIMITATIONS. REPAIR CARRIED OUT AS PER E.A. 1-5510-131639, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.Aug 15, 2009 · N573FE · Doug MD11 · Horizontal Stabilizer, Plate/SkinSDR FDEA200908132997Skin · misrepairedEXISTING EXTERNAL REPAIR DOUBLER FOUND AT RT WING NR 5 SLAT L/E EXTERIOR SKIN. EXISTING EXTERNAL REPAIR DOUBLER AT RT WING NR 5 SLAT L/E EXTERIOR SKIN EVALUATED AND FOUND NOT IAW SRM REPAIR. REPAIR CARRIED OUT IAW EA NR 1-5750-133822, TITLE: WINGS - FLIGHTAug 13, 2009 · N573FE · Doug MD11 · Leading Edge DevicesSDR FDEA200908132996Skin · misrepairedEXISTING EXTERNAL REPAIR DOUBLER FOUND AT RT WING SLAT NR 7 L/E EXTERIOR SKIN. EXISTING EXTERNAL REPAIR DOUBLER AT RT WING SLAT NR 7 L/E EXTERIOR SKIN EVALUATED AND FOUND NOT IAW SRM REPAIR. RT WING NR 7 SLAT ASSY REMOVED AND REPLACED IAW AMM 27-80-30-4, RAug 13, 2009 · N573FE · Doug MD11 · Wing, Plate/SkinSDR FDEA200908133003Skin · corrodedHORIZONTAL STABILIZER LEFT HAND UPPER PLANK 02L BARREL NUT BORE BEARING AREA CORROSION REWORKED EXCEEDED E.O. 1-5510-4-5000D1 PT1 LIMITATION. REPAIR CARRIED OUT AS PER E.A. 1-5510-131652, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.Aug 13, 2009 · N573FE · Doug MD11 · Horizontal Stabilizer, Plate/Skin
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