N580FE, cancelled Mar 2, 2024

Service difficulty reports · 128

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 = 'N580FE' AND deregistration_id = 'N580FE-2024-03-02'
  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 FDEA201505081433Bottle · dischargedL1 DOOR EMER DOOR OPENING BOTTLE WAS DISCHARGED & SLIDE WAS DISCONNECTED FROM DOOR DURING THE L1 DOOR EMER OPENING. THE SLIDE DID NOT INFLATE.May 8, 2015 · N580FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201502190547Bottle · low pressureL1 DOOR ASSIST BOTTLE INDICATES LOW PRESS. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 12-25-04-3-0. OK FOR SERVICE.Feb 19, 2015 · N580FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201409232715Hydraulic Line · leakingLEVEL ONE HYD 3 OFF PASSING FL 200 LEVEL TWO HYD 3 FAIL AT FL 370, LOWERED GEAR MANUALLY. FOUND HYD PRESS HOSE THAT CONNECTS FROM THE PYLON TO THE ENG HYD MANIFOLD BLOWN APART AT THE PYLON B NUT. REMOVED THE DAMAGED HOSE. DUE TO NR 3 SYS HYD AT 0 QTY, REQUSep 23, 2014 · N580FE · Doug MD11F · Hydraulic System, MainSDR FDEA201404080697Control Unit · failedON TAXI OUT RECEIVED LVL 1, FIRE DET 2 FAIL. AFTER STOPPING ACFT, RAN A FIRE TEST & THEN RECEIVED LVL 3, ENG 2 FIRE, ALERT. RAN QRH PROCEDURES, FOR ENG FIRE SEVERE DAMAGE CHECKLIST. FIRED FIRST BOTTLE & ALERT REMAINED ON, AFTER 30 SEC STILL HAD FIRE ALERT OApr 8, 2014 · N580FE · Doug MD11F · Fire DetectionSDR FDEA201305070928Skin · misrepairedFUSELAGE SKIN, BS 979, LONGERON 47-48R MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 1 REV 52. EO 1-5100-7- 5001B3, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 7, 2013 · N580FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201305060915Skin · crackedNR 3 AIRCONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN FOUND CRACKED. NR 3 AIRCONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN CARRIED OUT REPAIR IAW SRM 53-20-15, REPAIR 3, FIG 201, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 6, 2013 · N580FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201305060919Skin · corrodedRIGHT WING UPPER SURFACE FOUND CORROSION AT XORS 255 DURING SPOILER, UPPER SURFACE INSPECTION. CORROSION REMOVED AND FOUND EXCEED LIMITS IAW SRM 57-20-01, FIG 101, REV 52. DOUBLER REPAIR CARRIED OUT IAW EA 1-5730-167610. REPAIR CLASSIFIED AS MAJOR IAW GMM May 6, 2013 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201305060916Rib · wornRT WING NR 4 L/E SLAT INBD SLAT TRACK RIB FWD HOLE FOUND WORN AFTER REMOVAL OF NR 3 SLAT. NR 4 SLAT REWORKED IAW SRM 57-40-02 REPAIR 10, FIGURE 201, REVISION 52. FINAL HOLE DIAMETER 1.125" AND THE CHAFING MARK STILL EXIST, REPAIR ACCOMPLISHED IAW EA 1-5750-May 6, 2013 · N580FE · Doug MD11F · Leading Edge DevicesSDR FDEA201305040910Cap · misrepairedLT WING T/E LOWER ACCESS PANEL 541JB CUT-OUT FWD EDGE LOWER CAP MISREPAIRED. REPAIRED IAW EA 1-5710-167609. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 4, 2013 · N580FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201305030903Rib · crackedRIGHT WING NR 5 SLAT FOUND INBD INNER RIB CRACKED. NR 5 SLAT FABRICATED AND INSTALLED IAW EA 1-5750-166127, STEP 2 AND 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 3, 2013 · N580FE · Doug MD11F · Leading Edge DevicesSDR FDEA201305030902Support Fitting · damagedMAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 6 HOLE DIAMETER (D ) ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 3, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201305030901Support Fitting · damagedMAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 1 HOLE DIAMETER ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 3, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201305030900Support Fitting · damagedMAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 7 HOLE DIAMETER (A & C ) ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.May 3, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201305030899Skin · crackedNR 3 AIR CONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN FOUND CRACKED. REPAIRED IAW SRM 53-20-15, REPAIR 3, FIG 201 REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 116.May 3, 2013 · N580FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201305010893Beam · corrodedCENTER WHEEL WELL BS 1461 TO 1490 RT DIAGONAL I-BEAM FOUND CORRODED. R & R WITH NEW FABRICATED I-BEAM IAW SRM 51-31-01, REV 52 AND EA 1-53-167608. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 1, 2013 · N580FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201305010892Bulkhead · canningOIL CANNING AT CENTER LANDING GEAR RT VERTICAL WEB BETWEEN BS 1401 TO 1441, Z= -119 TO Z= -83. REPAIRED IAW EO 1-5100-7- 5001B3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 1, 2013 · N580FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201305010891Bulkhead · canningOIL CANNING AT CENTER LANDING GEAR LT VERTICAL WEB BETWEEN BS 1401 TO 1441, Z= -119 TO Z= -80. CARRIED OUT INSPECTION IAW EA 1-5310-167604, REPAIRED IAW EO 1-5100-7-5001B3 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.May 1, 2013 · N580FE · Doug MD11F · Fuselage Main, BulkheadSDR FDEA201304280879Skin · crackedRIGHT WING - L/E LOWER SURFACE NR 12 SLAT TRACK CUT-OUT SKIN FOUND CRACKED AT XOS 777. DURING OTBD SLAT DRIVE CABLES INSPECTION. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7 REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 28, 2013 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201304280878Frame · dentedBS 1661 LONGERON 12R FRAME FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201304280877Door Frame · crackedL3 DOOR FORWARD FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201304280876Door Frame · crackedR3 DOOR AFT FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201304280875Door Frame · crackedR3 DOOR FORWARD FRAME WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 28, 2013 · N580FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201304260865Skin · crackedLEFT WING INBD FLAP UPPER SURFACE FOUND CRACKED AT XIFH 177 AND 58" FROM T/E. REPAIRED IAW EA 1-5750-166124. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.Apr 26, 2013 · N580FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201304260863Skin · looseLEFT WING INBD FLAP UPPER SURFACE, SEVERAL FASTENERS AT XIFH 159 FOUND LOOSE. R & R WITH NEW FASTENERS IAW SRM 51-35-01, REV 52. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.Apr 26, 2013 · N580FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201304260862Seat Track · corrodedEXFOLIATION CORROSION FOUND ON SEAT TRACK BASE AT BS 491 TO 502, X= -27.5. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 26, 2013 · N580FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201304240840Skin · misrepairedRT WING FIXED L/E SURFACE TELESCOPIC DUCT CUT-OUT AREA MISREPAIRED. REPAIRED IAW SRM 57-40-01, REPAIR 10, FIGURE 201, REV 52 AND EA 1-5730-166121. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 24, 2013 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201304240843Skin · delaminatedRIGHT WING OTBD FLAP T/E WEDGE INBD EDGE FORM DELAMINATED FROM XOFH 458.690 TO XOFH 468.690. REPAIRED IAW EA 1-5750-166120. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.Apr 24, 2013 · N580FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201304240842Skin · crackedLT WING INBD FLAP UPPER SKIN AT XIFH= 171, 52" FROM T/E FOUND WITH 1 INCH CRACK. REPAIRED IAW EA 1-5750-166124. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 24, 2013 · N580FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201304240841Skin · crackedRT WING NR 5 SLAT LOWER SURFACE FOUND CRACK ABOUT 5 INCHES LONG AT XOS 717. REPAIRED IAW EA 1-5750-166127, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 24, 2013 · N580FE · Doug MD11F · Leading Edge DevicesSDR FDEA201304240839Access Panel · corrodedRT WING T/E LOWER ACCESS PANEL 641JB CUT-OUT FWD EDGE LOWER CAP SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5710-166116. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 24, 2013 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201304230831Frame · misrepairedFRAME MISREPAIRED AT CABIN BS 535, L24L. REPAIRED IAW SRM 53-20-07, FIG 201, REPAIR 1, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 23, 2013 · N580FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201304230830Frame · misrepairedFRAME MISREPAIRED AT CABIN STATION 535, L19L. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 52. EO 1-5100-7-5001B3, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.Apr 23, 2013 · N580FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201201260347Pressure Switch · failedMAX POWER TAKE OFF, NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE INDICATED NORMAL ON GAUGES. ABORT WAS ACCOMPLISHED AT 20 KIAS. LIGHT WENT OUT WHEN POWER MOVED TO IDLE. ALL OIL INDICATIONS REMAINED NORMAL. R & R LOW OIL PRESSURE SWITCH IAWJan 26, 2012 · N580FE · Doug MD11F · Engine Oil QuantitySDR FDEA201108243450Hinge · crackedRIGHT MLG DOOR-CENTER HINGE ASSY FOUND CRACKED. CRACKED HINGE REMOVED AND REPLACED WITH NEW HINGE AT RIGHT HAND DOOR CENTER AREA AS PER SRM 51-35-01 REV 47. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.Aug 24, 2011 · N580FE · Doug MD11F · Fuselage, Door HingeSDR FDEA201108173313Skin · corrodedRT FUSELAGE SKIN BENEATH AFT BODY FAIRING (UPPER SIDE) FROM BS 2155 TO 2164, FOUND CORRODED AT SEVERAL LOCATIONS. CORROSION REMOVED IAW SRM 51-70-01, FIG 201. REPAIR 3 REV 47. ORIGINAL THICKNESS 0.0125", MATERIAL REMOVED 0.085", REMAINING THICKNESS 0.040"Aug 17, 2011 · N580FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201108173312Skin · corrodedRT FUSELAGE BENEATH AFT BODY FAIRING (LOWER SIDE) FROM STA 2155 TO 2164 FOUND CORRODED AT SEVERAL LOCATIONS. CORROSION REMOVED, ORIGINAL THICKNESS 0.095", MATERIAL REMOVED 0.045", REMAINING THICKNESS 0.050". REPAIR CARRIED OUT IAW SRM 53-70-01, FIG 201, REPAug 17, 2011 · N580FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201006262195Probe · failedAT LEVEL OFF CALM AIR GOT A FUEL QTY/FUEL USED LEVEL 2 POSSIBLE FUEL LEAK ALERT. FOLLOWED QRH PROCEEDURE S AND ISOLATED PROBLEM TO NR 2 MAIN TANK ERRONEOUS QTY OF - 4500. QTY IN TANK 2 WOLD FLUCTUATE IN MANUAL AND AUTO. NO LEAK NOTED. REMOVED AND REPLACED Jun 26, 2010 · N580FE · Doug MD11F · Fuel Indicating SystemSDR FDEA201002170442Brake · failedAFTER TAKEOFF NR 8 BRAKE TEMP CLIMBED TO OVER 400 DEGREES BEFORE DECREASING. AFTER LANDING NR 8 BRAKE RAN HOTTER THAN THE OTHERS. GEAR WAS LOWERED TO COOL BRAKE AND RETRACTED. ACFT LANDED OK WITHOUT INCIDENT. R & R NR 8 BRAKE IAW MM 32-43-20-4. OPS CHECK Feb 17, 2010 · N580FE · Doug MD11F · Landing Gear Brake SystemSDR FDEA200909183325Skin · corrodedCORROSION - RT UPPER WING SURFACE AT XORS197. REPAIRED IAW EA 1-5710-132215.Sep 18, 2009 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909063264Skin · corrodedLT WING UPPER SKIN AT STA, XORS 378 FOUND CORROSION. REPAIR IAW EA 1-5710-132212 TITLE: "WINGS-LT WING UPPER SKIN SURFACE CORROSION - REPAIR"Sep 6, 2009 · N580FE · Doug MD11 · Wing, Plate/SkinSDR FDEA200909063263Skin · corrodedLT WING UPPER SKIN AT STA, XORS 130 TO XORS 197 FOUND CORROSIONS. REPAIR IAW EA 1-5710-132213 TITLE: "WINGS-LT WING UPPER SKIN SURFACE CORROSION - REPAIR"Sep 6, 2009 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909063262Skin · corrodedLT WING UPPER SKIN AT STA. XORS 402 TO XORS 433 FOUND CORROSIONS. REPAIR IAW EA 1-5710-132212.Sep 6, 2009 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909013226Skin · corrodedRIGHT UPPER WING SKIN HAS CORROSION AT STA XORS 150. REPAIRED IAW EA 1-5750-132215.Sep 1, 2009 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909013225Skin · corrodedRIGHT UPPER WING SKIN HAS CORROSION, STA XORS 163. REPAIRED IAW EA 1-5710-132215.Sep 1, 2009 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909013224Skin · corrodedRIGHT UPPER WING SKIN HAS CORROSION, STA XORS 298. REPAIRED IAW EA 1-5710-132215. MAJOR REPAIR.Sep 1, 2009 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909013223Skin · corrodedLEFT UPPER WING SKIN STA XORS 317 TO 360 HAS CORROSION. REPAIR IAW EA 1-5750-132209.Sep 1, 2009 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200909013222Longeron · corrodedLONGERON 45R BS879 LWR OTBD SURFACE CORRODED IN FWD CARGO. COMPLIED WITH EA 1-5310-132210: FUSELAGE - LONGERON 45R CRACK AT APPROX STA 879 - REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 107.Sep 1, 2009 · N580FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200909013201Longeron · corrodedFWD CARGO - LONGERON 45R AT BS 879 LWR OTBD SURFACE CORRODED. COMPLIED WITH EA 1-5310-132210: FUSELAGE - LONGERON 45R CRACK AT APPROX STA 879 - REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 107Sep 1, 2009 · N580FE · Doug MD11F · Fuselage Main, Longeron/StringerSDR FDEA200908313193Skin Panel · cracked25EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN INSP AT RT LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. REPAIR IAW EA 1-5710-133858 TITLE: "AD2007-07-04 - WINGS - RT LWR SKIN PLANK CUTOUT AT 636AB - REPAIR TO ACCESS DOOR AAug 31, 2009 · N580FE · Doug MD11F · Wing, Plate/SkinSDR FDEA200908313192Skin Panel · cracked21 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT W LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. REPAIR IAW EA 1-5710-133857 TITLE: "AD2007-07-04 - WINGS - LT LWR SKIN PLANK CUTOUT AT 536AB - REPAIR TO AAug 31, 2009 · N580FE · Doug MD11F · Wing, Plate/Skin
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