N582FE

Service difficulty reports · 370

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 = 'N582FE' 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 FDEA201407021601Skin · damagedAGING ACFT LT WING LE UPPER SURFACE FOUND EXISTING REPAIR AT APPROXIMATELY STATION XIS 247. EVALUATED AND FOUND DAMAGED LEFT WING LEADING EDGE UPPER SURFACE AT STA XIS 247. CARRIED OUT REPAIR AS PER SRM 57-40-02 FIGURE 201 REPAIR 8 REV 55 EO 1-5100-7-5001 B4Jul 2, 2014 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201406301593Doubler · crackedLEFT WING LEADING EDGE LOWER ACCESS CUTOUT FOUND DOUBLER CRACKED AT APPROXIMATE STATION XOS 602. CRACKED DOUBLER R&R IAW DRAWING ARB2933 REV T AND SRM 51-31-01 REV 55. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.Jun 30, 2014 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201406301591Frame · dentedCABIN MAIN CARGO COMPARTMENT LT STATION 1741, LONGERON 12LH SIDEWALL FRAME DENTED. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 55. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.Jun 30, 2014 · N582FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201406301590Frame · dentedCABIN MAIN CARGO COMPARTMENT RT STATION 1641 LONGERON 12RT SIDEWALL FRAME DENTED. FRAME REPAIRED AS PER SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 55. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.Jun 30, 2014 · N582FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201406301586Doubler · crackedRIGHT WING LE CAVITY BEADED DOUBLER FOUND CRACKED AT APPROXIMATE STATION XOS 669. CARRIED OUT REPAIR AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 55. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.Jun 30, 2014 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201406301585Doubler · crackedRIGHT WING LE CAVITY BEADED DOUBLER FOUND CRACKED AT APPROXIMATE STATION XOS 910. CARRIED OUT REPAIR AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 55 REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 122.Jun 30, 2014 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201406301584Skin · delaminatedRIGHT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM STATION XIFH 127.800 TO XIFH 216.300. RT WING INBOARD FLAP VANE ASSEMBLY R&R AS PER AMM 27-50-22-4 REVISION 79 ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-830-801 REVISION 79. FOUND SATISJun 30, 2014 · N582FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201406271560Skin · crackedRIGHT WING DROOP LE UPPER SURFACE FOUND CRACKED APPROXIMATELY 1.5 INCH IN LENGTH AT FASTENER HOLE AT STATION XDLE 329.774. CRACKED ON UPPER SURFACE AT RT WING DROOP LE AT STATION XDLE 329.774. CARRIED OUT REPAIR IAW SRM 57-40-01 FIGURE 201 REPAIR 5 REVISION Jun 27, 2014 · N582FE · Doug MD11F · Leading Edge DevicesSDR FDEA201405110980Skin · crackedDURING WALK AROUND FOUND SUSPECTED CRACK IN RT WING AROUND SLAT DRIVE MECHANISM ACCESS DOOR. HFEC INSPECTED CRACK INDICATED IAW SOPM 20-30-00. REMOVED DAMAGE IAW SRM 57-40-02 REPAIR 7. PERFORMED HFEC OF CUT OUT AREA ON RT WING TO ENSURE CRACK REMOVAL IAW NTMay 11, 2014 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201404170745Guide · brokenDURING CLIMB OUT 250 KIAS, RECEIVED RED WARNING LIGHTS ON NOSE GEAR & LT MAIN PRIMARY LIGHTS. SLOWED TO 230KIAS RECEIVED LIGHTS PRIMARY & SECONDARY. ACCOMPLISHED CHECKLIST, CYCLED GEAR, ALL LIGHTS EXTINGUISHED. ON POST FLIGHT INSPECTION FOUND BRAKE HOSE GUApr 17, 2014 · N582FE · Doug MD11F · Main Landing GearSDR FDEA201308011741Light · inoperativeR1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST, HAS NO INDICATION.Aug 1, 2013 · N582FE · Doug MD11F · Escape SlideSDR FDEA201308011734Button · inoperativeR1 ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST, NO INDICATION. R & R AND OPS CHECKED OK IAW MM 25-61-04-4.Aug 1, 2013 · N582FE · Doug MD11F · Escape SlideSDR FDEA201306011195Cooling Fan · burnedHEARD A LOUD FAN SOUND UNDER COCKPIT FLOOR (AVIONICS). SOUND SUDDENLY STOPPED AND A SLIGHT BURNING ODOR IN COCKPIT. NO OTHER INDICATIONS. R & R NR 3 AVIONIC COOLING FAN ASSY IAW AMM 21-26-02-2-1.Jun 1, 2013 · N582FE · Doug MD11F · Air Distribution FanSDR FDEA201302240424Anti-Ice Valve · failedON DEPARTURE GOT LEVEL 2 WING A/I DISAGREE. COMPLIED WITH QRH FIM 30-11-02 AND FOUND BAD RT WING DE-ICE VALVE. REMOVED INOP VALVE AND INSTALLED A SERVICEABLE VALVE IAW THE AMM 30-11-01-4. PERFORMED OPERATION CHECKS IAW 30-11-00-5 AND NOTED OPS GOOD. NO LEAKFeb 24, 2013 · N582FE · Doug MD11F · Airfoil Anti/De-ice SystemSDR FDEA201301270200Downlock · crackedRECEIVED HYD 3 ELEV ALERT AT 1 14 ENROUTE (FL 350). HYD QTY WAS 4.8 QTY CONTINUED DECREASING UNTIL RECEIVING HYD 3 OFF ALERT. (QTY 2.8) QRH REFERENCED AND CONTACTED MOCC. LOST 3 HYD WHEN EXTENDING GEAR. LANDED AND CLEARED RWY. TOWED TO PARKING. FOUND THREJan 27, 2013 · N582FE · Doug MD11F · Landing Gear Retraction/Extension SystemSDR FDEA201210123599Coalescer Bag · odorDURING PREFLIGHT WITH EXTERNAL AIR CONNECTED, THERE APPEARED AN OILY SMOKE ODOR ENTERED THE COCKPIT. NR 1 PACK TEMP CLIMBED TO 182 FACT. R & R NR 1 PACK COALESCER BAG REF AMM 21-54-05-2. OPERATED NR 1 PACK AND NO OIL ODOR FOUND REF AMM 21-53-20-5. LEAK/OPOct 12, 2012 · N582FE · Doug MD11F · Humidity Control SystemSDR FDEA201209113279Skin · wornLEFT WING INBD AILERON ASSY LOWER FORWARD RUB STRIP WORN. SKIN FABRICATED AS PER DRAWING ARC1250 REVISION D. RUBSTRIP (SKIN) REMOVED AND REPLACED AS PER E.A. 1-5750-162367. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Sep 11, 2012 · N582FE · Doug MD11F · AileronsSDR FDEA201208233138Seat Track · wornMAIN DECK SEAT TRACK WORN AT BS 1531 X=-8. REPAIRED AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Aug 23, 2012 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208223106Seat Track · crackedMAIN DECK CARGO SEAT TRACK AT BS 1501 TO 1511 X=-75.25, FOUND CRACKED. REPAIR CARRIED OUT AND INSTALLED AS PER AS PER SRM 53-00-52 FIGURE 201 REPAIR 1 REVISION 50. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.Aug 22, 2012 · N582FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208223105Longeron · crackedCENTER CARGO BS 1790, LONGERON 47R FOUND CRACKED. REPAIRED IAW SRM 53-00-05, REPAIR 1, FIG 202, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Aug 22, 2012 · N582FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA201208223103Panel · corrodedRT WING T/E PANEL NR 641JB CUT OUT LOWER SURFACE FOUND CORRODED. R & R IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Aug 22, 2012 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201208223102Panel · corrodedLT WING T/E PANEL 541JB CUTOUT FOUND CORRODED. R & R IAW SRM 51-31-01, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.Aug 22, 2012 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201112235437Access Panel · missingON POST FLIGHT INSPECTION, NOTED ACCESS PANEL MISSING FROM NR1 ENGINE PYLON OTBD SIDE, ACCESS PANEL IS DIRECTLY ABOVE AFT ENGINE MOUNT BOLTS. INSTALLED MISSING ACCESS PANEL AND NUTPLATES AND FASTENERS AS REQUIRED REF SRM 51-31-01.Dec 23, 2011 · N582FE · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR FDEA201105251986Fire Loop · malfunctionedLEVELING AT FL 250 RECEIVED LEVEL 3, ENG NR 2, FIRE INDICATION. COMPLETED PHASE 1 PROCEDURES, DUMPED FUEL AND RETURN TO DEPARTURE. R & R LWR TURB LOOP A RESPONDER IAW MM 26-11-03-4. FINAL CLOSED.May 25, 2011 · N582FE · Doug MD11F · Fire DetectionSDR FDEA201009293780Doubler · corrodedLT WING UPPER WING SURFACE MLG SUPPORT UPPER DOUBLER AT XORS 290 FOUND CORROSION. CARRIED OUT RECTIFICATION AS PER EA 1-5710-143434. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Sep 29, 2010 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201009293779Doubler · corrodedLT WING UPPER WING SURFACE MLG SUPPORT UPPER DOUBLER AT XORS 288 FOUND CORROSION. CARRIED OUT RECTIFICATION AS PER EA 1-5710-143434. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Sep 29, 2010 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201009273734Skin · crackedLEFT WING LEADING EDGE LOWER ACCESS PANEL 519CB CUT OUT, INBOARD CORNER SKIN FOUND CRACKED. CARRIED OUT REPAIR AS PER SRM 57-40-02 FIGURE 201, REPAIR 7, REVISION 44. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.Sep 27, 2010 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201009273732Skin · crackedRIGHT WING LOWER SKIN PANEL OUTER WING ACCESS DOOR CUT OUT AT APPROXIMATELY BETWEEN XORS 683.400 AND XORS 713.600, 01 EACH FASTENER HOLE FOUND WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSPECTION. CARRIED OUT REPAIR BY INSTALLATION OF BUSHING IN REWORK FASep 27, 2010 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201009273731Skin · crackedLEFT WING LOWER SKIN PANEL, OUTER WING ACCESS DOOR CUT OUT AT APPROXIMATELY BETWEEN XORS 683.400 AND XORS 713.600, 03 EACH FASTENER HOLE FOUND WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSPECTION. 03 EACH FASTENER HOLE AT LEFT HAND WING LOWER SKIN FUEL TANSep 27, 2010 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201009263726Floorbeam · crackedFORWARD AVIONICS COMPARTMENT FLOORBEAM AREA FROM CABIN CENTER LOWER CHORD AT STA 392, RBL 15 FOUND CRACKED. HFEC INSPECTION CARRIED OUT AS PER NDT SPM REVISION 13 PART 06-10-01.001, RESULT NO CRACK EVIDENT.Sep 26, 2010 · N582FE · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA201009243700Rib · crackedRIGHT WING NR 1 LEADING EDGE SLAT INBOARD PERFORMANCE FILLET OUTBOARD EDGE RIB FOUND CRACKED AROUND AFT FASTENER HOLE. CARRIED OUT REPAIR AS PER SRM 57-40-71 FIGURE 201, REPAIR 1, REVISION 44. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.Sep 24, 2010 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201009243698Skin · corrodedRIGHT WING UPPER SURFACE, MAIN LANDING GEAR SUPPORT UPPER DOUBLER AT XORS 277 FOUND CORROSION. CARRIED OUT RECTIFICATION AS PER E.A. 1-5730-143750. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100, REVISION 111.Sep 24, 2010 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201009243699Frame · crackedUPPER AFT FUSELAGE FRAME CLIP AT CANT STA Y = 2069 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01, REVISION 44. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.Sep 24, 2010 · N582FE · Doug MD11F · Fuselage Main, FrameSDR FDEA200910243659Pilot Valve · inoperativeON TAKE OFF BLEED AIR 2 OFF ALERT. TRIED MANUAL AND 2ND AUTO CHANNEL COULD NOT RESTORE (BLEED AIR 3 PREVIOUSLY DEFERRED) AIR TURNBACK PHNL 90,000 LBS FUEL DUMPED. REPLACED NR 2 PRESSURE REGULATOR PILOT VALVE IAW AMM 36-12-20-4. RAN NR 2 ENG IAW JRH. NR 2 POct 24, 2009 · N582FE · Doug MD11F · Pneumatic Distribution SystemSDR FDEA200909153301Pressure Switch · failedON TAKEOFF RUN APPROX 50KTS HAD A NR 3 ENG LEVEL 2 "ENG OIL FILTER". REJECTED TAKEOFF AND COMPLIED WITH QRH. REMOVED AND REPLACED THE OIL FILTER DIFFERENTIAL PRESSURE SWITCH.Sep 15, 2009 · N582FE · Doug MD11F · Engine Oil Indicating SystemSDR FDEA200903100883Support · damagedRT WING REAR SPAR NR 4 SPOILER HINGE SUPPORT HOLE FOUND ELONGATED. RT WING REAR SPAR NR 4 SPOILER HINGE SUPPORT HOLE REPAIR CARRIED OUT AS PER E.A. 1-5750-127474. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Mar 10, 2009 · N582FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA200903100882Skin · corrodedCABIN, RT STA 1229 X= -43 TO X= -53, CENTER WING UPPER PANEL FOUND CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-127463: WINGS, CENTER WING UPPER AUXILLIARY FUEL TANK SKIN CORROSION, REPAIR.Mar 10, 2009 · N582FE · Doug MD11F · Wing, Center BoxSDR FDEA200903100880Skin · corrodedCABIN - R/H STA 1229, X= -70 CENTER WING UPPER PANEL FOUND CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-127463: WINGS, CENTER WING UPPER AUXILIARY FUEL TANK SKIN CORROSION, REPAIR.Mar 10, 2009 · N582FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200903020785Support Frame · corrodedAFTER REMOVAL OF LT MAIN LANDING GEAR RETRACT CYLINDER SUPPORT FRAME MOUNTING BOLTS PER SNRM N01194 FOUND MOUNTING BORE HOLES WITH CORROSION. REPAIRED AS PER EA 1-5740-127470. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Mar 2, 2009 · N582FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA200903020783Support · corrodedAFTER REMOVAL OF FRAME SUPPORT MOUNTING BOLTS PER SNRM N01267 FROM RT MAIN LANDING GEAR RETRACT CYLINDER ASSY FOUND MOUNTING HOLES WITH CORROSION. REPAIRED AS PER EA 1-5740-127479. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Mar 2, 2009 · N582FE · Doug MD11F · Main Landing GearSDR FDEA200903020781Attach Fitting · corrodedRT WING OTBD FLAP VANE NR 2 FROM INBD TRACK FITTING ATTACH BORE FOUND WITH CORROSION. COMPLIED WITH E.A. 1-5750-127473. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Mar 2, 2009 · N582FE · Doug MD11F · Wing, Attach FittingsSDR FDEA200903020778Attach Fitting · corrodedLT WING OTBD FLAP VANE NR 2 TRACK FITTING ATTACH BORES FOUND WITH CORROSION. COMPLIED WITH EA 1-5750-127466. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Mar 2, 2009 · N582FE · Doug MD11F · Wing, Attach FittingsSDR FDEA200903010774Shear Tie · crackedCENTER CARGO, UPON REMOVED EXISTING REPAIR DOUBLER BILGE AREA FRAME SHEAR CLIP CRACKED AT STA 1841, LONGERON- 51L. REMOVED AND REPLACED WITH NEW SHEAR TIE AS PER SRM 51-33-01 VOL. II.Mar 1, 2009 · N582FE · Doug MD11F · Fuselage Internal Mounting StructureSDR FDEA200902240680Skin · misrepairedEXISTING REPAIR, LT WING NR 7 LEADING EDGE EXTERIOR OTBD SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING NR 7 LEADING EDGE SLAT EXTERIOR OTBD SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IAW ANY SRM REPAIR SCHEME. REPAIR CARRIED OUT PER FEDEX EA Feb 24, 2009 · N582FE · Doug MD11F · Leading Edge DevicesSDR FDEA200902240678Skin · misrepairedEXISTING REPAIR, LT WING, INBD FLAP INBD SEGMENT, INBD UPPER LEADING EDGE SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP INBD SEGMENT, INBD UPPER LEADING EDGE SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IAW ANY SRM REPAIR SCHEME. LT WINFeb 24, 2009 · N582FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200902240675Skin · misrepairedFUSELAGE, EXISTING REPAIR DOUBLER AT SKIN STATION 1841, AROUND LONGERON-52L. EXISTING REPAIR DOUBLER AT FUSELAGE SKIN AT STA 1841, AROUND LONGERON 52L EVALUATED AND FOUND NOT ACCOMPLISHED IAW SRM 53-20-00 FIG 2 VOL I. EXISTING REPAIR DOUBLER REMOVED AND NEW Feb 24, 2009 · N582FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA200902240679Skin · misrepairedLT WING, INBD FLAP INBD SEGMENT, MIDDLE AFT UPPER SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP INBD SEGMENT MIDDLE AFT UPPER AFT UPPER SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IAW SRM 57-10-00 FIG 38 VOL I. EXISTING REPAIR DOUBLER Feb 24, 2009 · N582FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200902240677Skin · misrepairedRT WING, INBD FLAP INBD SEGMENT UPPER MIDDLE AFT SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING INBD FLAP INBD SEGMENT UPPER MIDDLE AFT SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IAW SRM 57-10-00 FIG 38 VOL I. EXISTING REPAIR DOUBLER REMOVED AFeb 24, 2009 · N582FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200902240676Skin · misrepairedLT WING, INBD FLAP INBD SEGMENT OTBD AFT UPPER SURFACE FOUND EXISTING REPAIR. EXISTING REPAIR AT LT WING INBD FLAP INBD SEGMENT OTBD AFT UPPER SURFACE EVALUATED AND FOUND NOT ACCOMPLISHED IN ACCORDANCE WITH SRM 57-10-00 FIG 38 VOL I. EXISTING REPAIR DOUBLEFeb 24, 2009 · N582FE · Doug MD11F · Trailing Edge FlapsSDR FDEA200902230673Hinge Bracket · corrodedRT WING, OTBD FLAP OTBD HINGE BRACKET SIDE LOAD LOWER HOLE SURFACE CORROSION. COMPLIED WITH EA 1-5750-128580. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Feb 23, 2009 · N582FE · Doug MD11F · Wing, Control Surface Attach Fittings
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