N586FE
Service difficulty reports · 500
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 = 'N586FE' 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 = 'N586FE' 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 FDEA201909232320Seat Track · corrodedCABIN - RIGHT HAND STATION 1942 X = - 107 SEAT TRACK FOUND CORROSION. CABIN AT RIGHT HAND SEAT TRACK STATION 1942 X = - 107 CORROSION FOUND EXFOLIATED AND EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIOSDR FDEA2019092432325Stiffener · crackedRIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 542 STIFFENER CRACKED. STIFFENER ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 542 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100. STIFFENER FASDR FDEA2019092432324Doubler · crackedRIGHT HAND WING- FIXED LEADING COMPARTMENT STATION XOS 785 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 785 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOSDR FDEA2019092432318Doubler · crackedRIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 790 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 790 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOSDR FDEA201909222306Doubler · corrodedRIGHT HAND WING - UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION AT STATION YW 467. RIGHT HAND WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER STATION YW 467 AREA CORROSION REMOVED FOUND EXCEED LIMIT AS PER SRM 57-20SDR FDEA201909222314Seat Track · corrodedCABIN - LEFT HAND STATION 1861 X = 8.5 SEAT TRACK FOUND CORROSION. CABIN AT LEFT HAND SEAT TRACK STATION 1861 X = 8.5, CORROSION REMOVED AND FOUND TO EXCEED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SSDR FDEA201909222305Doubler · crackedLEFT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 993 RIB DOUBLER CRACKED. LEFT WING - FIXED LEADING COMPARTMENT STATION XOS 993 RIB CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G, DOUBLER FABRICATED AS PER DRAWING ARB 1249 REV AA, AND INSTALLED AS PER SRSDR FDEA2019092422313Doubler · crackedRIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 691 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 691 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOSDR FDEA2019092422312Doubler · crackedRIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 739 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 739 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOSDR FDEA2019092422311Doubler · crackedRIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 731 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 731 BEADED DOUBLER AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOSDR FDEA2019092422310Doubler · crackedRIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 759 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 759 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOSDR FDEA2019092422309Doubler · crackedRIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 756 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING FIXED LEADING COMPARTMENT AT STATION XOS 756 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR SDR FDEA2019092422308Doubler · crackedRIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 543 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 543 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOSDR FDEA2019092422307Doubler · crackedRIGHT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 666 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON RIGHT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 666 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOSDR FDEA2019092422304Doubler · crackedLEFT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 906 RIB DOUBLER CRACKED. RIB DOUBLER ON LEFT HAND WING-FIXED LEADING COMPARTMENT AT STATION XOS 906 REMOVED AND REPLACED AS PER SRM 51-31-01-0G . DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 3954 REVISDR FDEA2019092422303Doubler · crackedLEFT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 669 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON LEFT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 669 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR SDR FDEA2019092422302Doubler · crackedLEFT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 586 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON LEFT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 586 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR SDR FDEA2019092422301Doubler · crackedLEFT HAND WING - FIXED LEADING COMPARTMENT STATION XOS 592 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT ON LEFT HAND WING - FIXED LEADING COMPARTMENT AT STATION XOS 592 BEADED DOUBLER AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR SDR FDEA2019092422300Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE AFT INBOARD CORNER OF SLAT TRACK NUMBER 10 CUTOUT AND FOUND CRACK INDICATION APPROXIMATE 1/4 INCHES LENGTH AT STATION XOS 657. REPAIR CARRIED OUT ON LEFT HAND WING FIXESDR FDEA201909172267Spar · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT PRINCIPAL STRUCTURAL ELEMENT SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT RIGHT HAND STATION 2164 FORWARD FLANGE OF THE REAR UPPER SPAR. LOWER VERTICAL STABILIZER AT RIGHT HAND STATION 2164SDR FDEA201909172266Spar · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT PRINCIPAL STRUCTURAL ELEMENT SPAR, LOWER VERTICAL STABILIZER AND FOUND CRACK INDICATION AT LEFT HAND STATION 2164 FORWARD FLANGE OF THE REAR UPPER SPAR. LOWER VERTICAL STABILIZER AT LEFT HAND STATION 2164 FSDR FDEA201906051219Skin · cracked#3 PACK BAY CUT-OUT APPEARS TO HAVE A CRACK AT THE UPPER AFT CORNER. COUNTER SUNK HOLES AS REQUIRED IN DOUBLER AND TRIPLER. ALODINED AND PRIMED, IAW MD-11 SRM 53-20-15-2R. AND OK TO INSTALL EXTERNAL ALUMINUM REPAIR DOUBLER AND TRIPLER. SHGN 06JUN19 20:39 SDR FDEA201810082812Skin · dentedNR 1 SLAT LT WING L/E DENT AT NR 3 SLAT TRACK CUT-OUT COMPLIED WITH EA 1-5730-T0342552 PT1.SDR FDEA201810042784Skin · crackedL/H WING L/E SKIN CRACK AT AXIS 247-0280 EA 1-5730-T0342552 CUT OUT DAMAGE AND INSTALLED L/E DOUBLER.SDR FDEA2018100542784Skin · crackedLT WING L/E SKIN CRACK AT AXIS 247-0280 EA 1-5730-T0342552 CUT OUT DAMAGE AND INSTALLED L/E DOUBLER.SDR FDEA2018062971588Target · shearedON RAISING GEAR AFTER TAKEOFF, NOSE GEAR SHOWED AN UNSAFE INDICATION ON PRIMARY AND SECONDARY DISPLAY. FOLLOWED CHECKLIST, VERIFIED GEAR DOWN BY TOWER AND MX, LANDED UNEVENTFULLY. UNSAFE INDICATION PERSISTED AFTER LANDING. INSPECTED NOSE GEAR AND FOUND TARGSDR FDEA201806161509Indicator · inoperativeL1 DOOR SLIDE PUSH TO TEST INOP. REMOVED & REPLACED PTT IND ASSY & OPS NORMAL PER AMM 25-61-04-4. A/C OK FOR SVC.SDR FDEA201806021379Wire Harness · damagedRECEIVED A FIRE LIGHT ON ENGINE 3 AT T/O 3 MIN. CLIMBING THRU 12,000 FT ENGINE WAS SECURED WITH CHECKLIST, FIRE BOTTLE BLOWN. REMOVED AND REPLACED RT NR 2 FIRE EXTINGUISHER BOTTLE UP TO AND INCLUDING STEP 3 G (1)G REF AMM 32-21-01-4. MANIFOLD DISCHARGE PORTSSDR FDEA201804281142Lamp · inoperativeDURING A POST FLIGHT INSPECTION, THE L1 DOOR OVERHEAD AFT EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-52-04-2. EMERGENCY LIGHTS TESTED GOOD. OK FOR SERVICE.SDR FDEA201804010820Iru · failedANTISKID FAIL ALERT AFTER PUT GEAR DOWN, RECYCLED ONCE , STILL FAILED. GO AROUND, 20 MIN FLYING, 3RD GEAR DOWN WITH NO ANTI SKID FAIL. NO WHEEL BRAKES ISSUES NO HOT BRAKES. R & R ANTISKID CONTROL UNIT AS PER AMM 32-45-01-4. OPS TEST CHK'D GOOD. AIRCRAFT SDR FDEA201709162584Panel · missingLEFT DETACHABLE ELEVATOR PANEL 335CZ FOUND MISSING. REPAIRED IAW EA 1-5510-T0335323, PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709162583Panel · missingLEFT DETACHABLE ELEVATOR PANEL 335HZ FOUND MISSING CARRIED OUT A REPAIR IAW EA 1-5510-T0335323, PT 1. INSTALLED THE PANEL IAW AMM 20-50-02. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709162582Panel · missingLEFT DETACHABLE ELEVATOR PANEL 335AZ FOUND MISSING. REPAIRED IAW EA 1- 5510-T0335323, PT 1. INSTALLED IAW AMM 20-50-02. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2017091922504Hinge Bracket · corrodedTHE BORE WAS REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-08. EXISTING HOLE DIA: 0.873", FINAL HOLE DIA: 0.983", MAXIMUM ALLOWABLE HOLE DIA: 0.983". RIGHT WING OUTBD FLAP INBD FWD HINGE REMOVED AND REPLACED AS PER AMM 57-53-01-4. REPAIR CLASSIFIESDR FDEA201709122509Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (FLAP SIDE) PIVOT INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335333, PART 1, STEP 3A, AND 3C.SDR FDEA201709122508Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122507Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122506Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED, AND FOUND OUT OF LIMIT IAW CMM 57-44-08. THE OTBD FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122505Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122503Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE RIGHT WING OTBD FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.SDR FDEA201709122502Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1D.SDR FDEA201709122501Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1D.SDR FDEA201709122500Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1C, AND STEP 1.SDR FDEA201709122499Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1C AND STEP 1.SDR FDEA201709122498Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) UPPER MOUNT OUTBD HOLE SPOT SURFACE FOUND CORRODED. THE SPOT SURFACE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. REPAIRED THE AREA IAW EA 1-5750-T0335291A, PART 1, STEP 1.SDR FDEA201709122497Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED, AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1A.SDR FDEA201709122496Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335291A, PART 1, STEP 1B.SDR FDEA201709122495Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR OUTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2D.SDR FDEA201709122494Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2D.SDR FDEA201709122493Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD HINGE (WING SIDE) BARREL NUT LOWER HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-TO335331, PART 1, STEP 2C.
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