N590FE
Service difficulty reports · 555
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 = 'N590FE' 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.
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 = 'N590FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202509121689Web · crackedAGING AIRCRAFT - EXISTING REPAIR AT COCKPIT FLOOR WEB OBSERVER SEAT AREA STATION 360 X = -13.250 RIGHT HAND SIDE. EXISTING REPAIR AT COCKPIT FLOOR WEB OBSERVER SEAT AREA STATION 360 X =-13.250 RIGHT HAND SIDE EVALUATED AND FOUND WITH CRACK LENGTH AT EDGE OSDR FDEA202410051428Lamp · no test1L DOOR EMERGENCY SLIDE CIRCUIT TEST PUSH BUTTON DOES NOT ILLUMINATE. RELEASED FOR SERVICE PER MEL : 25-61-02. L1 EVAC SLIDE REMOTE PRESS INDICATOR - INOP. PER MEL 25-61-02, VERIFY AND RECORD IN THE AML, EVAC SLIDE SYS PRESS ADEQAUTE ONCE EACH FLIGHT DAYSDR FDEA202404260298Indicator · failedR1 DOOR PRESSURE TO TEST INOPERATIVE. REMOVED AND REPLACED THE R1 DOOR INDICATOR ASSEMBLY, REMOTE PRESSURE AND OPS CHECKED NORMAL. AC OK FOR SERVICE.SDR FDEA202404100453Battery · inoperativeEMER LT BAT 1 LO DURING PREFLIGHT REPLACED EMERGENCY LIGHT BATTERY. OPS CHECK GOOD. AMM 33-51-01-4.SDR FDEA202401220103Door · crackedAFT BULK DOOR LOWER AFT SKIN HAS DAMAGE REPAIRED AFT LWR CORNER IN REF TO E.A. 1-5230-T0377851 PART 1 AND 2.SDR FDEA202401252103Door · crackedAFT BULK DOOR LOWER AFT SKIN HAS DAMAGE REPAIRED AFT LWR CORNER IN REF TO E.A. 1-5230-T0377851 PART 1 AND 2.SDR FDEA202305110854Skin · chafedLOWER FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT DOOR JAMB STATION 1009, LONGERON 39 RIGHT TO LONGERON 42 RIGHT EXISTING DOUBLER REPAIR FOUND WITH EDGE CHAFE. LOWER FORWARD CARGO COMPARTMENT DOOR CUT OUT AFT DOOR JAMB AT STATION 1002 TO STATION 1009 LONSDR FDEA202305110853Skin · chafedLOWER CENTER CARGO COMPARTMENT DOOR CUT OUT FORWARD DOOR JAMB LONGERON 38 RIGHT TO LONGERON 42 RIGHT DOUBLER REPAIR FOUND WITH EDGE CHAFE. LOWER FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD DOOR JAMB STATION 895 LONGERON 38 RIGHT TO LONGERON 42 RIGHT EXSDR FDEA202305110851Skin · chafedLOWER CENTER CARGO COMPARTMENT DOOR CUT OUT AFT DOOR JAMB LOWER EXISTING DOUBLER REPAIR FOUND WITH EDGE CHAFE AT STATION 1781 TO STATION 1801, LONGERON 38 RIGHT TO LONGERON 44 RIGHT. LOWER CENTER CARGO COMPARTMENT DOOR CUT OUT AFT JAMB LOWER EXISTING DOUBSDR FDEA202305110850Skin · chafedLOWER CENTER CARGO COMPARTMENT DOOR CUT OUT FORWARD DOOR JAMB STATION 1704 , LONGERON 40 RIGHT TO LONGERON 42 RIGHT DOUBLER REPAIR FOUND WITH EDGE CHAFE. LOWER CENTER CARGO COMPARTMENT DOOR CUT OUT FORWARD DOOR JAMB AT APPROXIMATELY STATION 1708 LONGERON SDR FDEA202305090828Floor Panel · corrodedUPON REMOVAL RCB FOR ACCESS FOUND CORROSION ON RCB FLOOR PANEL AT STATION 475 - 515 , X = 0 TO X = - 8.5. REMOVED AND REPLACED AS PER AMM 53-21-10-2. RIGID CARGO BARRIER FLOOR PANEL FABRICATED BY MACHINING AS PER DOUGLAS DRAWING WSP 0785 REVISION B. REPSDR FDEA202305090827Floor Panel · corrodedUPON REMOVAL RCB FOR ACCESS FOUND CORROSION ON RCB FLOOR PANEL AT STATION 475 - 515 , X = 8.5 TO X = 0. REMOVED AND REPLACED AS PER AMM 53-21-10-2. RIGID CARGO BARRIER FLOOR PANEL FABRICATED BY MACHINING AS PER DOUGLAS DRAWING WSP0785 REVISION B. REPAIRSDR FDEA202305090826Floor Panel · corrodedUPON REMOVAL RCB FOR ACCESS FOUND CORROSION ON RCB FLOOR PANEL AT STATION 475 - 515 , X = 20.5 TO X = 8.5. REMOVED AND REPLACED AS PER AMM 53-21-10-2. RIGID CARGO BARRIER FLOOR PANEL FABRICATED BY MACHINING AS PER DOUGLAS DRAWING WSP 0786 REVISION B. RESDR FDEA202305090825Floor Panel · corrodedUPON REMOVAL RCB FOR ACCESS FOUND CORROSION ON RCB FLOOR PANEL AT STATION 475 - 515 , X = 27.5 TO X = 20. REMOVED AND REPLACED AS PER AMM 53-21-10-2. RIGID CARGO BARRIER FLOOR PANEL FABRICATED BY MACHINING AS PER DOUGLAS DRAWING WSP 0785 REVISION B. REPSDR FDEA202305010792Unknown · unknownCABIN - STATION 1621, X = - 107.25 SEAT TRACK ASSEMBLY FOUND WITH CORROSION.SDR FDEA202305010791Seat Track · corrodedCABIN: SEAT TRACK STATION 1149, X = - 8.5 FOUND CORROSION. FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1169 TO EXISTING SPLICE STSDR FDEA202305010790Seat Track · corrodedCABIN: SEAT TRACK STATION 1159, X = 8.5 FOUND CORROSION. FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1189 TO EXISTING SPLICE STATSDR FDEA202305010789Seat Track · wornCABIN - SEAT TRACK AT STATION 755 X = - 8.5 CROWN AREA WORN. WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES FROM STSDR FDEA202305010788Seat Track · wornCABIN - SEAT TRACK AT STATION 725 X = - 8.5 CROWN AREA WORN. CROWN AT SEAT TRACK STATION 725 X = - 8.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMSDR FDEA202305010787Seat Track · wornCABIN - SEAT TRACK AT STATION 755 X = 27.5 CROWN AREA WORN. WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION SDR FDEA202305010786Seat Track · wornCABIN - SEAT TRACK AT STATION 755 X = 47.5 CROWN AREA WORN. EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 725 TO STSDR FDEA202305010785Seat Track · wornSEAT TRACK AT BS 505 X = 8.5 CROWN AREA WORN. CROWN EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 525 TO END OF PART STATION 440, SDR FDEA202305010784Cap · corrodedRIGHT WING - TRAILING EDGE REAR SPAR UPPER CAP AT XORS 1043 FOUND CORROSION. RIGHT WING TRAILING EDGE REAR SPAR UPPER CAP AT XORS 1043 CORRODED AREA REPAIR CARRIED OUT AS PER EA# 1-5710-T0374279 PART 1, TITLE : WINGS - BASIC WING STRUCTURE - RH WING - CORSDR FDEA202305010783Seat Track · wornCABIN: SEAT TRACK STATION 6-90, X = 8.5 CROWN AREA FOUND WORN. SEAT TRACK STATION 6-90 , X = 8.5 EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN WORN SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FRSDR FDEA202304190700Doubler · corrodedRIGHT WING - UPPER SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER AT STATION XW 229.5 FOUND CORROSION. MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN INNER REAR SPAR AND YW467 AREA CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-20-01-1ASDR FDEA202304190699Doubler · corrodedLEFT WING - UPPER SURFACE MAIN LANDING GEAR SUPPRT UPPER DOUBLER AT STATION XW 229.5 FOUND CORROSION. UPPER SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER BETWEEN AUXILIARY SPAR AND YW 467 AREA CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-20-SDR FDEA202304190696Skin · crackedDURING HFEC INSPECTION ON RIGHT HAND WING FUEL ACCESS DOOR FORWARD INBOARD CORNER AT STATION XOS 610 FOUND 01 EACH CRACK APPROXIMATELY 0.3 INCHES. REPAIR CARRIED OUT AS PER MD - 11 SRM 57-40-01-2R REPAIR 18 FIGURE 201. INITIAL INSPECTION TO BE CARRIED OUTSDR FDEA202304190695Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 627 FOUND CRACK. BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190694Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 613 FOUND CRACK. BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190693Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 663 FOUND CRACK. BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190692Fitting · crackedDURING INSPECTION ON #4 BANJO LEFT HAND SIDE OF LOWER VERTICAL STAB AFT FLANGE OF UPPER REAR SPAR CAP ON THE LOWEST FASTENER #1 LEFT AS SHOWN ON SHEET 10.1 FIGURE, COME ACROSS CRACK ON THE EDGE OF AFT FLANGE ABOVE FASTERNER #1 LEFT AS MARKED AT STATION 2164.SDR FDEA202304190691Stringer · crackedUPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW -17 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.SDR FDEA202304190690Stringer · crackedUPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW 17 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.SDR FDEA202304190689Stringer · crackedUPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW 46.5 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.SDR FDEA202304190688Stringer · crackedUPPER AUXILIARY TANK - STRINGER 46 AT STATION XCW -17 FOUND CRACK. REPAIR CARRIED OUT AS PER EA# 1-5710-T0374206 PART 1. TITLE: WINGS - BASIC WING STRUCTURE - CENTER WING LOWER PANEL CRACK FOUND ON STRINGER S-46 BETWEEN XCW 17.000 AND XCW -17.000. REPASDR FDEA202304190687Stringer · crackedUPPER AUXILIARY TANK - STRINGER 46 AT STATION XCW 17 FOUND CRACK. REPAIR CARRIED OUT AS PER EA# 1-5710-T0374206 PART 1 TITLE: WINGS - BASIC WING STRUCTURE - CENTER WING LOWER PANEL CRACK FOUND ON STRINGER S-46 BETWEEN XCW 17.000 AND XCW -17.000. REPAIRSDR FDEA202304190686Stringer · crackedUPPER AUXILIARY TANK - STRINGER 42 AT STATION XCW 46.5 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190685Fitting · crackedDURING HFEC SURFACE INSPECTION ON THE RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND 01 EACH CRACK WITH LENGTH APPROXIMATELY 1.1 INCHES AT STATION 583 AS MARKED. RIGHT HAND NOSE LANDING GESDR FDEA202304190684Fitting · crackedDURING HFEC SURFACE INSPECTION ON THE LEFT HAND NOSE LANDING GEAR TRUNION FITTING AFT OF NOSE LANDING GEAR DOOR AFT HINGE FITTING SLOT OUT AREA FOUND 01 EACH CRACK WITH LENGTH APPROXIMATETLY 0.1 INCHES AT STATION 583 AS MARKED. LEFT HAND NOSE LANDING GEAR SDR FDEA202304190683Stringer · crackedUPPER AUXILIARY TANK - STINGER 51 AT STATION XCW 46.5 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190682Former · crackedLEFT WING - LEADING EDGE COMPARTMENT LOWER FORMER AT XOS 559 FOUND CRACK. FORMER REMOVED AND REPLACED AS PER MD - 11 SRM 51-31-01-0G. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 1162 REVISION S. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190681Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 623 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190680Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 670 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190679Skin · crackedLEFT WING - NUMBER 16 SLAT TRACK LOWER CUTOUT SKIN AT XOS 1004.5 FOUND CRACK. REPAIR CARRIED OUT AS PER MD -11 SRM 57-40-02-2R REPAIR 7 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190678Skin · damagedRIGHT WING - TRAILING EDGE INBOARD ISLAND UPPER SKIN LOWER SURFACE FORWARD EDGE FINGER DOUBLER AT XW 398 FOUND DETACHED. REPAIR CARRIED OUT AS PER MD-11 SRM 57-50-01- 2R REPAIR 6 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190677Finger Doubler · detachedLEFT WING - TRAILING EDGE INBOARD ISLAND UPPER SKIN LOWER SURFACE FORWARD EDGE FINGER DOUBLER AT XW 398 FOUND DETACHED. REPAIR CARRIED OUT AS PER MD-11 SRM 57-50-01- 2R REPAIR 6 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202204020823Battery · dischargedMDIS 590 33-50 0749 02APR22 YYZ OPEN U DURING PRE FLIGHT, EMERGENCY LIGHTING SYSTEM TEST FAILS AND SHOWING MSG BAT 1 LO. REMOVED AND REPLACED POWER SUPPLY, EMERGENCY LIGHTING BATTERY REF. AMM 33-51-01-4. PERFORMED SDR FDEA202203180584Computer · failedELEVATOR CONTROLLER FEEL LOST AT FL 390 WITH LOSS OF FO AIRSPEED. PERFORMED ORH PROCEDURE UNRELIABLE AIRSPEED FO. REMOVED AND REPLACED #2 CENTRAL AIR DATA COMPUTER IAW MD-11 AMM 34-16-01-4 OPS CHECK NORMAL, PERFORM SDR FDEA202108172022Control Valve · leakingON CLIMBOUT AFTER RETRACTION RECIEVED A LEVEL 1 HYD 1 OFF. HSC SHUT OFF SYSTEM AND WE CONTINUED TO KIX ON ARRIVVAL AFTER FLAPS IS RECIEVED HYD 1 FAIL. PRESSURE AND QTY SYSTEM1 0 AND 0.3. PERFORMED HYDRAULIC SYSTEM EXTERNAL LEAKAGE IAW MM 29-00-00-6 HYD LESDR FDEA202103230748Seat Track · corrodedCABIN - STATION 1761 TO STATION 1781 , X = 8.5 SEAT TRACK FOUND CORRODED AROUND FASTENER HOLES . CABIN AT STATION 1761 TO STATION 1781 X = 8.5 CORROSION AT FASTENER HOLES EVALUATED EVALUATED AND FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A
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