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 FDEA201708232302Seat Track · corrodedMAIN DECK CARGO SEAT TRACK FLANGE FOUND CORROSIONS AT RT BS 1419, RBL 27.5. OUT OF LIMITS IAW SRM 53-00-52-1A, FIGURE 101, AND REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 23, 2017 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708212290Hinge · corrodedUPPER CARGO DOOR FWD HINGE LOBES EXISTING REPAIR BUSHINGS INSIDE DIAMETER OUT OF LIMITS AND TWO BUSHINGS DAMAGED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 52-34-04.Aug 21, 2017 · N584FE · Doug MD11F · Fuselage, Door HingeSDR FDEA201708172245Fitting · crackedDURING HFEC INSPECTION AT THE LT FWD FLANGE, LOCATED AT THE UPPER SECTION REAR SPAR CAP OF THE NR 4 BANJO FITTING OF THE VERTICAL STABILIZER , BS 2164. A CRACK WAS FOUND APPROXIMATELY 0.50 INCH LENGTH. REPAIRED IAW EA 1-5530-T0335146, P1. CLASSIFIED AS MAJAug 17, 2017 · N584FE · Doug MD11F · Vertical Stabilizer, Attach FittingsSDR FDEA201708172247Web · crackedFUSELAGE: FAC OBSERVER SEAT CUTOUT WEB FOUND CRACKED AT APPROXIMATELY BS 360. REPAIRED IAW SRM 53-10-51-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 17, 2017 · N584FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201708172246Skin · crackedDURING HFEC INSPECTION, A CRACK WAS FOUND APPROXIMATELY 0.50 INCHES IN LENGTH ON THE LT WING CORNER AT THE FUEL ACCESS DOOR FWD INBD CORNER AT XOS 610. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 18. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 17, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708172249Former · crackedRT WING LEADING EDGE CAVITY AT STA XOS 584 FORMER FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB 2931 REVISION H. INSTALLED NEW FORMER AT RT WING LEADING EDGE AT STA XOS 584 AS PER SRM 51-33-01-0G. RAug 17, 2017 · N584FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201708172248Former · crackedRT WING LEADING EDGE CAVITY UPPER FORMER AT STA XOS 584 FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB 2931 REVISION H. INSTALLED NEW FORMER AT RT WING LEADING EDGE CAVITY UPPER AT STA XOS 584 AS PER Aug 17, 2017 · N584FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201708152217Frame · crackedMAIN DECK CARGO BAY R3 DOOR FWD LOWER FUSELAGE FRAME WEB FOUND CRACKED AT RT BS 1255, BETWEEN LONGERONS AND 27R. REPAIRED IAW EA 1-5310-T0335060, P1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Fuselage Main, FrameSDR FDEA201708152219Door Frame · crackedMAIN DECK CARGO BAY L3 DOOR AFT LOWER FRAME WEB CRACKED AT BS 1310, BETWEEN LONGERONS 26L AND 27L. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201708152218Door Frame · crackedMAIN DECK CARGO BAY L3 DOOR FWD LOWER FRAME WEB CRACKED AT BS 1255, BETWEEN LONGERONS 26L AND 27L. REPAIRED IAW SRM 53-40-15-2R, FIGURE 201, REPAIR 3. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Fuselage Main, StructureSDR FDEA201708152213Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 709 - 714 CRACKED. THE DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152211Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 692 - 698 CRACKED. THE DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152209Support · crackedLEFT WING LEADING EDGE LOWER ACCESS PANEL SUPPORT FOUND CRACK AT XOS 543. ACCESS PANEL REMOVED IAW SRM 51-31-01-0G. FABRICATED A NEW SUPPORT IAW DRAWING ARB 2933, REVISION AJ. INSTALLED A NEW SUPPORT IAW SRM 51-33-01-0G. THE REPAIR WAS CLASSIFIED AS MAJOR Aug 15, 2017 · N584FE · Doug MD11F · Wing Miscellaneous StructureSDR FDEA201708152208Former · crackedLEFT WING LEADING EDGE SKIN INTERNAL FRAME SUPPORT BRACKET FOUND CRACK AT XOS 584. FORMER REMOVED IAW SRM 51-31-01-0G. FABRICATED A NEW FORMER IAW DRAWING ARB 2931, REVISION H, AND INSTALLED THE FORMER IAW SRM 51-33- 01-0G. THE REPAIR WAS CLASSIFIED AS MAAug 15, 2017 · N584FE · Doug MD11F · Wing Main, Frame StructureSDR FDEA201708152207Doubler · crackedLEFT WING LEADING EDGE SKIN INTERNAL SUPPORT BEADED DOUBLER FOUND CRACK AT XOS 613. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152206Doubler · crackedLEFT WING LEADING EDGE SKIN INTERNAL SUPPORT BEADED DOUBLER FOUND CRACKED AT XOS 640. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152205Doubler · crackedLEFT WING LEADING EDGE SKIN INTERNAL SUPPORT DOUBLER FOUND CRACKED AT XOS 627 . REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152204Stiffener · crackedLEFT WING LEADING EDGE LOWER SKIN SUPPORT STIFFENER FOUND CRACK AT XOS 547. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-31-01-0G AND DRAWING ARB 2918, REVISION G, AND SRM 51-35-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152215Doubler · crackedRT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 542 - XOS 546 FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 542 - XOS 546 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152214Doubler · crackedRT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 536- XOS 541 FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 536- XOS 541 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152212Doubler · crackedRT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 579 - XOS 584 FOUND CRACKED. REPAIR CARRIED OUT AT RT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 579 - XOS 584 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10Aug 15, 2017 · N584FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201708152210Splice · corrodedCENTER LANDING GEAR, RT FWD UPPER BRACE ATTACH FITTING SPLICE FOUND CORRODED BS 1461. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-00-2R, FIGURE 202. REMOVED IAW SRM 51-33-01-0G, FABRICATED A NEW SPLICE IAW DRAWING AEA 7130, REVISION C, AND INSTAAug 15, 2017 · N584FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201707181990Trunnion · wornCENTERLINE LANDING GEAR LT AND RT TRUNNION SUPPORT FITTINGS CORRODED. COMPLIED WITH EA 1-5340-T0334405A, PT2. MACHINED FAYING SURFACE. AFTER MACHINING, MINIMUM THICKNESS OF FAYING SURFACE WAS LESS THAN SRM LIMITS.Jul 18, 2017 · N584FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201707181989Trunnion · wornCENTERLINE LANDING GEAR LT AND RT TRUNNION SUPPORT FITTINGS CORRODED. COMPLIED WITH E.A. 1-5340-T0334405A PT1. MACHINED FAYING SURFACE. AFTER MACHINING, MINIMUM THICKNESS OF FAYING SURFACE WAS LESS THAN SRM LIMITS.Jul 18, 2017 · N584FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA201703190960Reservoir · emptyFORWARD PASSENGER DOOR WAS PNEUMATICALLY OPENED BY THE EMERGENCY OVERRIDE LEVER. RESET THE L1 DOOR IAW MM 52-11-02-2, SPOTTED THE PRESSURE FOR THE RELATIVE PNEUMATIC RESERVOIR WAS ZERO. CHARGED THE L1 DOOR RESERVOIR IAW AMM 12-25-04-3, ACFT OK FOR SERVICE.Mar 19, 2017 · N584FE · Doug MD11F · Passenger/Crew DoorsSDR FDEA201702250661Control Unit · failedDURING TAKEOFF ROLL, SHORTLY AFTER POWER APPLICATION (60 KNOTS) AIRCRAFT VEERED TO THE LEFT. ATTEMPED TO CORRECT BUT TO NO AVAIL. REJECTED THE TAKE OFF AND RECEIVED A TIRE FAILURE ON NR 4 TIRE. TAXIED BACK TO RAMP. REPLACED ANTI SKID CONTROL UNIT IAW AMM Feb 25, 2017 · N584FE · Doug MD11F · Tire TubeSDR FDEA201612014300Power Supply · failedDURING PREFLIGHT, RECEIVED AN EMERGENCY LIGHT BATTERY 1 LOW. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-01-4. OPS CHECKED NORMAL, OK FOR SERVICE.Dec 1, 2016 · N584FE · Doug MD11F · Emergency LightingSDR FDEA201611023804Screw · looseR1 DOOR SLIDE R1 OUT OF ADJUSTMENT. FOUND FOLLOW UP DOOR ABOVE R1 DOOR WILL NOT RETRACT WHEN R1 DOOR IS RAISED. FOUND LOOSE SCREWS ON AFT OUTBOARD ROLLER. TIGHTNED SCREWS IAW AMM 52-11-11-4. LUBED SLIDING CEILING PANEL IAW AMM 12-25-05-3. OPS CHECKED GNov 2, 2016 · N584FE · Doug MD11F · Service DoorsSDR FDEA201611023803Screw · looseDOOR SLIDE R1 NEEDS ADJUSTING. FOUND LOOSE SCREWS ON AFT OUTBOARD ROLLER. TIGHTNED THE SCREWS IAW AMM 52-11-11-4. LUBED SLIDING CEILING PANEL IAW AMM 12-25-05-3. OPS CHECK GOOD IAW AMM 52-11-02Nov 2, 2016 · N584FE · Doug MD11F · Escape SlideSDR FDEA201610273716Warning System · false activationEMER PWR TEST FAIL ALERT (LEVEL 1) DURING PREFLIGHT. CYCLED BATT CHARGER CONTROL C/B AND RTS OF EPCU SYS. OPS CK NORMAL REF M/M 24-34-02-5Oct 27, 2016 · N584FE · Doug MD11F · Battery/Charger SystemSDR FDEA201610183653Cover · missingCONTROL PANEL AT L1 ENTRY DOOR MISSING 'DOOR DISARM' LIGHT COVER. INSTALLED THE COVER IAW MM 52-11-00-0.Oct 18, 2016 · N584FE · Doug MD11F · DoorsSDR FDEA201511143604Slide · inoperativeR1 DOOR ESCAPE SLIDE PUSH TO TEST LIGHT WILL NOT EXTINGUISH. RELEASED FOR SERVICE IAW MEL 52-10-03-03, CATEGORY B, EXPIRATION 17 NOV 15. 1R MAIN ENTRY SLIDE & RAFT INOPERATIVE. TESTED SLIDE IAW FIM 25-61-02 PG 103 & MEL 25-61-02. SLIDE BOTTLE SHOWS GREEN,Nov 14, 2015 · N584FE · Doug MD11F · Escape SlideSDR FDEA201510033050Skin · corrodedNUMBER 2 ENG LT PICKLE BARREL - LANDING COMMON TO FAN COWL HAS FRETTING CORROSION & WORN PAINT. REMOVED CORRODED & WORN SECTION OF SKIN IAW SRM 54-20-15 FIG 201. INSTALLED NEW SPLICED SKIN IAW SRM 54-20-15 FIG 201. PAINTED LT PICKLE BARREL.Oct 3, 2015 · N584FE · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR FDEA201510033049Seat Track · damagedMAIN CABIN, SEAT TRACK DAMAGED AT STATION 635, RBL 8.5. REPLACED SECTION OF SEAT TRACK IAW SRM 53-00-52 & SRM 51-33-01.Oct 3, 2015 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201509282975Floorbeam · corrodedMAIN CABIN, STATION 770 FLOOR SUPPORT CORRODED BENEATH FLOORBOARD 242GF. R & R FLOOR SUPPORT.Sep 28, 2015 · N584FE · Doug MD11F · Fuselage Main, Floor BeamSDR FDEA201509282974Door · damagedCENTER CARGO DOOR, FWD LOWER CORNER EDGE SHOWING SPLIT. REPAIRED IAW SRM 52-30-16 FIG 201 REPAIR 3.Sep 28, 2015 · N584FE · Doug MD11F · Cargo/Baggage DoorsSDR FDEA201509262967Seat Track · corrodedGALLEY FLOOR RBL 28, STATION 435, JUST AFT OF LAVATORY, CORROSION IN SEAT TRACK. BLENDED AREA OF SEAT TRACK IAW SRM 53-00-52 REPAIR 1. BLENDING IS OUT OF LIMITS IAW SRM 53-00-52 REPAIR 1 FIG 201 SHT 6 NOTE C. REPLACED SECTION OF SEAT TRACK IAW SRM 53-00-52,Sep 26, 2015 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201509252947Floor Support · corrodedGALLEY FLOOR SUPPORT UNDER LAVATORY INBD AFT CORNER CORROSION, STATION 420, RBL 18. R & R LAVATORY FLOOR SUPPORT IAW SRM 51-33-01, PN WSP0668-503.Sep 25, 2015 · N584FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201509252946Seat Track · corrodedMAIN DECK FLOOR STATION 505 LT X=105.00, SEAT TRACK HAS EXFOLIATION CORROSION. R & R SEAT TRACK, COMPLIED WITH EA 1-5320-T0320245 PART 1.Sep 25, 2015 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201509252945Floor Support · corrodedGALLEY FLOOR SUPPORT UNDER LAVATORY, INBD AFT CORNER, CORROSION STATION 420, RBL 18. R & R FLOOR SUPPORT IAW SRM 51-33-01, PN WSP0668-503.Sep 25, 2015 · N584FE · Doug MD11F · Fuselage Miscellaneous StructureSDR FDEA201509252944Seat Track · corrodedMAIN DECK, FLOOR STATION 440, RBL 27.00 SEAT TRACK OTBD EDGE CORRODED. R & R SEAT TRACK IAW SRM 53-20-52.Sep 25, 2015 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201509252943Seat Track · corrodedGALLEY FLOOR, RBL 28, STATION 435, JUST AFT OF LAVATORY, CORROSION IN SEAT TRACK. BLENDED AREA OF SEAT TRACK IAW SRM 53-20-52. BLENDING IS OUT OF LIMITS IAW SRM 53-20-52 REPAIR 1 FIG 201 SHT 6 NOTE C. REPLACED SECTION OF SEAT TRACK IAW SRM 53-20-52.Sep 25, 2015 · N584FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201509252941Floorboard · corrodedAFT AVIONICS COMPARTMENT, APPROX STATION 475, RBL 12-72 ABOVE MAIN AVIONICS RACK. MILD CORROSION FORMING IN BETWEEN FLOORBOARDS & ACFT STRUCTURE IAW SNRM 47. REMOVED MULTIPLE FLOORBOARDS TO FACILITATE REMOVAL OF CORROSIVE LAVATORY FLUID & DETAILED VISUAL INSSep 25, 2015 · N584FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201509252940Floor Panel · corrodedMAIN DECK COURIER AREA, STATION 475 - 500, FLOORBOARD PANEL UNDER RCB WSP0785-501, HAS SURFACE CORROSION. R & R PANEL WSP0785-501 IAW DWG WS0785 & SRM 51-31-01.Sep 25, 2015 · N584FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201509242937Floor Panel · corrodedMAIN CABIN, STATION PANEL WSP0790-502 IS CORRODED. REMOVED, FABRICATED & INSTALLED FLOOR PANEL IAW DWG WSP0790.Sep 24, 2015 · N584FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201509242936Floorboard · corrodedMAIN DECK, COURIER AREA, STATION 475 - 500 FLOORBOARD PANEL UNDER RCB, WSP0786-501 HAS SURFACE CORROSION. REMOVED STRESS PANEL PN WSP0786-501. FABRICATED NEW FLOORBOARD PANEL UNDER RCB, PN WSP0786-501.Sep 24, 2015 · N584FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201509232927Floor Panel · corrodedMAIN CABIN, STATION 495, RBL 5, ALLOY FLOOR PANEL HAS LIGHT SURFACE CORROSION, PANEL WSP0785-502. FABRICATED FLOOR PANEL IAW DWG WSP0785-502. R & R ALLOY FLOOR PANEL WSP0785-502.Sep 23, 2015 · N584FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201509232926Floor Panel · corrodedMAIN CABIN, STATION 495, RBL 11 ALLOY FLOOR PANEL HAS LIGHT SURFACE CORROSION WSP0785-501. FABRICATED FLOOR PANEL IAW DWG WSP0785-501. R & R ALLOY FLOOR PANEL WSP0785-501.Sep 23, 2015 · N584FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201509232925Floor Panel · corrodedMAIN CABIN, BETWEEN STATION 495 - 515, FLOORBOARD SHOWS EVIDENCE OF CORROSION ON PRESS PANEL PN WSP0786-501 AT LBL 20 - 25. FABRICATED FLOOR PANEL IAW DWG WSP0786-501. R & R FLOOR PANEL WSP0786-501.Sep 23, 2015 · N584FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201509232924Floor Panel · corrodedMAIN DECK, STATION 501, ALLOY FLOOR PANEL WSP0785-501 HAS CORROSION BEYOND SRM LIMITS IAW SRM 53-20-50 PARA NR 4. FABRICATED FLOOR PANEL IAW DWG WSP0785. R & R FLOOR PANEL.Sep 23, 2015 · N584FE · Doug MD11F · Fuselage Floor Panel
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