N587FE
Service difficulty reports · 399
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 = 'N587FE' 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 = 'N587FE' 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 FDEA202110282648Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK ALONG X = 8.5 FLANGE AT STATION 1527 FOUND CORRODED. MAIN DECK CARGO COMPARTMENT FLOOR AT SEAT TRACK FLANGE STATION 1527 X = 8.5 CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLSDR FDEA202110272642Bracket · corrodedLEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CSDR FDEA202110272641Bracket · corrodedLEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR FDEA202110272640Bracket · corrodedLEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT HOLE BORE (#10 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 09. OVERSIZESDR FDEA202110272639Bracket · corrodedLEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- 44-0SDR FDEA202110272638Bracket · corrodedLEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44- 0SDR FDEA202110272637Bracket · corrodedLEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57- SDR FDEA202110272636Bracket · corrodedLEFT WING- WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-09. OVERSISDR FDEA202110262616Skin · crackedRIGHT HAND AFT LOWER FUSELAGE - APU EXHAUST DOOR CUTOUT UPPER FORWARD CORNER SKIN STATION 2140 AT LONGERON - 36 RIGHT CRACKED. RIGHT HAND AFT LOWER FUSELAGE - APU EXHAUST DOOR CUTOUT UPPER FORWARD CORNER AT STATION 2140 LONGERON - 36 RIGHT CRACKED SKIN ARESDR FDEA202110232597None · noneLEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 731. LEFT HAND WING FIXED LEADING EDGE INTERNAL DOUBLER AT STATION XOS 731 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PERSDR FDEA202110232598None · noneRIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 645. RIGHT HAND WING FIXED LEADING EDGE INTERNAL DOUBLER AT STATION XOS 645 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PSDR FDEA202110232596None · noneLEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 610. LEFT HAND WING FIXED LEADING EDGE INTERNAL DOUBLER AT STATION XOS 610 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PESDR FDEA202110222589Track · crackedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK ALONG X = 8.5 FOUND WITH CROWN CRACKED AT STATION 1541. MAIN DECK CARGO COMPARTMENT FLOOR , CRACKED SEAT TRACK AT STATION 1541 X = 8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AT EXISTING SPLICES STATION 157SDR FDEA202106011430Battery · failedEMERGENCY LIGHTING BAT LO ALERT ON PREFLIGHT REPLACED FWD EMERGENCY LIGHTING POWER SUPPLY. OPS CHECKS SATISFACTORYSDR FDEA202105181287Engine · flamed outENGINE 2 FLAMEOUT AFTER ADDING POWER FOR TAKEOFF. RAN QRH CONTACTED MOCC , NORMAL RELIGHT AND TAKEOFF. SHGN 18MAY21 08:18 MEM U STARTED AND RAN ENGINE #2 FOR 5 MINUTES IN REFERENCE PER MD11 JRH, ENGINE #2 STARTED GOOD AND ALL THE PARAMETERS ARE WITHIN SDR FDEA202105181286Engine · flamed outNUMBER TWO ENGINE FLAMED OUT WITH THROTTLE ADVANCE FOR TAKE OFF. RAN QRH CONTACTED MOCC, RESTARTED ENGINE, NORMAL START AND CLIMB OUT. SHGN 18MAY21 08:25 MEM U STARTED AND RAN ENGINE #2 FOR 5 MINUTES IN REFERENCE PER MD11 JRH, ENGINE #2 STARTED GOOD ANDSDR FDEA201910292773Seat Track · corrodedCABIN - SEAT TRACK AT STATION 455 TO STATION 475 X = 0 FOUND CORROSION . CABIN AT SEAT TRACK STATION 455 TO STATION 475 X = 0 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRACK REMOVED SDR FDEA201910252747Seat Track · corrodedREWORK : MAIN DECK FLOOR SEAT TRACK FOUND CORROSION AT STATION 1821 X = - 75.25 . MAIN DECK FLOOR AT SEAT TRACK STATION 1821 X = - 75.25 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CORRODED SEAT TRASDR FDEA201910252748Seat Track · corrodedREWORK: MAIN DECK FLOOR SEAT TRACK FOUND CORROSION AT STATION 1620 - 1661 , X = 75.25 . MAIN DECK FLOOR AT SEAT TRACK STATION 1620 TO STATION 1661 X = 75.25 , CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGESDR FDEA201910252745Doubler · crackedLEFT WING LEADING EDGE COMPARTMENT APPROXIMATELY AT STATION XOS 761 , BEADED DOUBLER FOUND WITH CRACKS. LEFT WING LEADING EDGE COMPARTMENT STATION XOS 761 BEADED DOUBLER CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MSDR FDEA201910242742Intercostal · crackedEMPENNAGE LEFT HAND REAR CENTER SPAR TO REAR SPAR INTERCOSTAL FOUND CRACK. EMPENNAGE LEFT HAND REAR CENTER SPAR TO REAR SPAR INTERCOSTAL CARRIED OUT REPAIR AS PER EA #1-5330-T0350369P1. TITLE: STABILIZERS- VERTICAL STABILIZER- REAR CENTER SPAR TO REAR SPARSDR FDEA201910222723Seat Track · damagedCABIN , FOUND SEAT TRACK AT STATION 5-6 , X = 47.5 CROWN DAMAGED . CABIN AT SEAT TRACK STATION 5-6 , X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SSDR FDEA201910222722Seat Track · damagedCABIN , FOUND COMPARTMENT SEAT TRACK AT STATION 1425 , X = 47.5 CROWN DAMAGED . CABIN AT SEAT TRACK STATION 1425 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK RSDR FDEA201910222721Seat Track · damagedCABIN , SEAT TRACK AT STATION 1408 , X = 47.5 CROWN DAMAGED . CABIN , SEAT TRACK AT STATION 1408 , X = 47.5 DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BY SECTISDR FDEA201910222720Seat Track · damagedCABIN , FOUND SEAT TRACK AT STATION 1289 X = 47.5 CROWN DAMAGED . CABIN AT SEAT TRACK STATION 1289 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DMAGED SEAT TRACK REPAIRED BY SECSDR FDEA201910222719Seat Track · damagedCABIN , FOUND SEAT TRACK AT STATION 1545 , X = 47.5 CROWN DAMAGED . CABIN , SEAT TRACK AT STATION 1545 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK REPAIRED BSDR FDEA201910222718Seat Track · damagedCABIN , FOUND SEAT TRACK AT STATION AT STATION 1151 , X = 47.5 CROWN DAMAGED . CABIN AT SEAT TRACK STATION 1151 X = 47.5 , DAMAGED CROWN EVALUATED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1 . CROWN DAMAGED SEAT TRACK RESDR FDEA2019101762654Web · crackedCOCKPIT, RIGHT OBSERVER SEAT BASE WEB AT BS 360 FOUND TO HAVE A CRACKED LIGHTENING HOLE. THE WEB WAS REPAIRED IAW SRM 53-10-51-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2019101762661Frame · dentedCABIN - LEFT HAND FRAME AT STATION 1721 LONGERON 12 FOUND DENTED. CABIN - DENTED LEFT HAND FRAME AT STATION 1721 LONGERON 12 LEFT REPAIRED AS PER SRM 53-00-07-2R FIGURE 201 REPAIR 2 . REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPETITIVESDR FDEA2019101762656Spar · crackedHFEC INSPECTION CARRIED OUT AT PSE SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT LEFT HAND FORWARD FLANGE OF THE REAR UPPER SPAR LEFT HAND REAR SPAR CAP FORWARD FLANGE LOCATED AT UPPER SECTION OF THE #4 BANJO FITTING OF LOWER VERTICAL STABISDR FDEA2019101762655Spar · crackedHFEC INSPECTION CARRIED OUT AT PSE, LOWER VERTICAL STABILIZER SPAR. FOUND A CRACK INDICATION AT THE RIGHT FORWARD FLANGE OF THE REAR UPPER SPAR. THE RIGHT REAR SPAR CAP FORWARD FLANGE LOCATED AT UPPER SECTION OF THE NR 4 BANJO FITTING OF LOWER VERTICAL STABISDR FDEA2019101762653Doubler · crackedRIGHT WING FIXED LEADING COMPARTMENT STATION XOS 764 BEAD DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2019101762652Doubler · crackedRIGHT WING FIXED LEADING COMPARTMENT, STATION XOS 790 BEAD DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2019101762651Doubler · crackedRIGHT WING, FIXED LEADING COMPARTMENT STATION XOS 648 BEAD DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201910162650Doubler · crackedRIGHT WING, FIXED LEADING COMPARTMENT STATION XOS 820 BEAD DOUBLER FOUND CRACKED. REPAIRED THE BEADED DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2019101762649Stringer · crackedRIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 906 STRINGER FOUND CRACKED. REPAIR CARRIED OUT AT RIGHT HAND WING FIXED LEADING COMPARTMENT STATION XOS 906 STRINGER AS PER SRM 57-40-03-2R FIGURE 202 REPAIR 2 .REPAIR CLASSIFIED AD MAJOR PER GMM 6SDR FDEA201908282037Indicator · failedR1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYSTEM, INOPERATIVE. R & R THE REMOTE PRESSURE INDICATOR ASSEMBLY FOR R1 DOOR, OPS CHECK GOOD IAW AMM 25-61-04-4.SDR FDEA201904231017Not Reported · cracked2IN CRACK ON LT LOWER CENTER VERTICAL ON NR 2 ENG. COMPLIED WITH FINAL EA# 1-5530-T0346813 A.SDR FDEA201903210696Bearing · seizedWHEN CHANGING THE NR 7 BRAKE FOUND THE BEARINGS SEIZED UP ON NR 7 MAIN TIRE. REMOVED AND REPLACED NR 7 MAIN LANDING GEAR TIRE ASSEMBLY.SDR FDEA201903210695Brake · draggingDURING TAXI AFTER LANDING THE NR 7 MAIN WHEEL BRAKE WAS HANGING UP AND OVERHEATING. TEMP GOT AS HIGH AS 475 WHILE ALL OTHER BRAKES WERE AT 220. CALLED FOR FIRE SUPPORT AS A PRECAUTION. MAINTENANCE TOWED US IN WITH THE BRAKE STILL HANGING UP. TEMP HAD DROPPED TSDR FDEA201903150637Ecu · faultyPDIS 587 73-22 7630 15MAR19 MEM OPEN U LOGPAGES:3028560 ON TAKEOFF JUST AFTER DEPARTING THE RUNWAY THE RED ENGINE FAIL LIGHT ILLUMINATED. A FEW SECONDS LATER AN ODD BOOMING NOISE WAS HEARD FOR ABOUT THREE SECONDS. THERE WERE NO ABNORMALITIES SHOWN ON ANYSDR FDEA2018090652356Tire · separatedPOSTFLIGHT FOUND NR 9 TIRE WITH THROWN TREAD AND TREAD SEPARATION. PER AMM 32-40-00-6 INSPECTION CHECK OF TIRE THAT HAS THROWN TREADS, R&R TIRE. INSPECTED CENTER GEAR TIRE AND WHEEEL PER AMM 32-41-01, NO OTHER DEFECTS FOUND. REMOVED AND REPLACED NR 9 CENTER TISDR FDEA201802060306Power Supply · inoperativeEMERGENCY LIGHT BATTERY 6 LOW LEVEL 1. REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-51-01-4. OPS TESTED GOOD.SDR FDEA201712193412Wire · cutLEVEL 1 ALERT FOR EMERGENCY LIGHT BATTERY AFTER EMERGENCY LIGHT SWITCHED TO TEST. FOUND A WIRE CUT AT 905R GROUND TERMINAL IAW WDM 33-52-01. CRIMPED & SECURED THE TERMINAL IAW SWPM 20-20-01. ALL EMERGENCY LIGHTS ILLUMINATED AND OPS CHECKED NORMAL IAW AMM 33-SDR FDEA201711013120Hinge · wornMAIN DECK CARGO DOOR MOST HINGE SECTION ON FUSELAGE SIDE FOUND FWD 12EA HINGE LOBE HOLES WORN EXCEEDED LIMITS AT STA 635 -STA 652. HOLES REWORKED AND FOUND NR 1 - NR 7 HOLES EXCEED LIMIT AS PER SRM 52-30-16-1A FIGURE 101, NR 1 EXISTING HOLES DIA 0.452''-0.455'SDR FDEA201711013119Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 1780, X= -8.5 FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEEDED ALLOWABLE DAMAGE LIMIT OF SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT REPAIR PER SRM 53-00-52SDR FDEA201711013118Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 1760, X= 27.5 FOUND CORROSION MAIN DECK FLOOR AT SEAT TRACK STA 1760, X= 27.5. CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM SDR FDEA201711013117Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STA 5-83, X= 8.5 FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEEDED ALLOWABLE DAMAGE LIMIT OF SRM 53-00-52-1A FIG 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT REPAIR PER SRM 53-00-52-SDR FDEA201710303111Cargo Track · corrodedCABIN MAIN DECK CARGO TRACK CORROSION AT BS 1169 RBL 47.5. REPLACED THE CARGO TRACK IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201710303108Skin · corrodedEMPENNAGE AFT ACCESSORY COMPT RT STA 2164 SKIN FOUND CORROSION AS MARKED. CORROSION REMOVED FOUND EXCEEDED LIMIT PER SRM 53-00-00-2R FIG 202. ORIGINAL THICKNESS : 0.100", MATERIAL REMOVED : 0.090" AND REMAINING THICKNESS : 0.010". AFT ACCESSORY COMPT RT STA 21
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