N608FE
Service difficulty reports · 370
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 = 'N608FE' 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 = 'N608FE' 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 FDEA201902080280Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 541 - 546 FOUND WITH CRACK REPAIR CARRIED OUT ON LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 541 - XOS 546 AS PER SRM 57-40-02-2R FIG SDR FDEA201902080277Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 652 - 657 FOUND WITH CRACK REPAIR CARRIED OUT ON LEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 652 - XOS 657 AS PER SRM 57-40-02-2R FIG SDR FDEA201902080273Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 747 - 752 FOUND WITH CRACK REPAIR CARRIED OUT ON LEFT AHND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STA XOS 747 - XOS 752 AS PER SRM 57-40-02-2R FIG 203 SDR FDEA201902080279Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 554 - 558 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201902080278Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 616 - 621 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201902080276Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 673 - 679 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201902080275Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 685 - 691 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201902080274Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 727 - 733 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201902080272Doubler · crackedLEFT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 767 - 772 FOUND WITH CRACK. REPAIR CARRIED OUT ON BEADED DOUBLER PER SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201902080293Skin · crackedLEFT HAND WING LEADING EDGE NR 12 SLAT TRACK CUTOUT FOUND CRACKED AT APPROXIMATE XOS 776.8. REPAIR CARRIED OUT ON LEFT HAND WING LEADING EDGE #12 SLAT TRACK CUTOUT AT APPROXIMATELY STATION XOS 776.8 AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7 .REPAIR CLASSSDR FDEA201902080292Seat Track · damagedCABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 1290, X = 8.5. MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 1290 X= 8.5 MEASURED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE SDR FDEA201902080291Seat Track · damagedCABIN MAIN DECK CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT LEFT HAND STATION 705, X = 75.25. SEAT TRACK CROWN AREA DAMAMGED MEASURED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FOG 101 ALLOWABLE DAMAGE. SEAT TRACK CARRIED OUT REPAIR AS PER SRMSDR FDEA201902080290Skin · chafedRIGHT HAND WING LEADING EDGE INBOARD EDGE FOUND WITH CHAFFING AT APPROXIMATE XDLE 309.9. REPAIR CARRIED OUT ON RIGHT HAND WING DROOP LEADING EDGE INBOARD EDGE AT XDLE 309 AS PER SRM 57-40-01-2R FIGURE 202 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2SDR FDEA201902080286Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 879 - 883 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 879-883 AS PER SRM 57-40-02-2R FIG 203 SDR FDEA201902080285Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 647 - 652 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 647- 652 AS PER SRM 57-40-02-2R FIG 203SDR FDEA201902080284Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 728 - 734 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 728-734 AS PER SRM 57-40-02-2R FIG 203 SDR FDEA201902080283Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 734 - 740 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 734-740 AS PER SRM 57-40-02-2R FIG 203 SDR FDEA201902080282Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 753 - 759 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STATION XOS 753-759 AS PER SRM 57-40-02-2R FIG 203 SDR FDEA201902080281Doubler · crackedRIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATE STATION XOS 610 - 616 FOUND WITH CRACK. REPAIR CARRIED OUT ON RIGHT HAND WING LEADING EDGE COMPARTMENT BEADED DOUBLER AT APPROXIMATELY STA 610 - 616 AS PER SRM 57-40-02-2R FIG 203 REPAISDR FDEA2019020530245Seat Track · crackedMAIN DECK COMPARTMENT SEAT TRACK FOUND CRACK AT STATION 635 X = - 8.5 MAIN DECK COMPARTMENT FLOOR SEAT TRACK CRACKED AT STATION 635 X = -8.5 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1 FROM STATION 625 TO STATION 645 X = -8.5. REPAIR CLASDR FDEA2019020530244Seat Track · crackedMAIN DECK COMPARTMENT FLOOR SEAT TRACK FOUND CRACK AT STATION 695 X = 27 MAIN DECK COMPARTMENT SEAT TRACK CARRIED OUT REPAIR FROM STATION 685- STATION 705 X = 27 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201804100957Light · unknownEMERGENCY LIGHT SYSTEM INOPERATIVE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM, OPS CHECKED NORMAL IAW MM 33-51-01-5.SDR FDEA201712283462Bushing · looseDURING A CURRENT B-CHECK, BUSHINGS WERE FOUND LOOSE. MX REPORTED LUG HOLE SIZES ARE THE SAME AS PREVIOUSLY REPORTED. COMPLIED WITH EA 1-5230-143587 REV C.SDR FDEA201708022093Autobrake Sys · malfunctionedDURING TAKE OFF ROLL, BRAKES BEGAN TO GRAB AND RUDDER PEDALS DISPLACED (LEFT RUDDER) AUTOBRAKES HAD BEEN DEFERRED DUE TO AUTOBRAKE FAIL. CYCLED BRAKE PEDALS NUMEROUS TIMES WITH NO DEFECTS NOTED WITH BRAKE APPLICATION. INSPECTED BRAKES WHILE CYCLING PEDASDR FDEA201702120527Skin · detachedLEFT WING INBD TRAILING EDGE LOWER PANEL 541KB FOUND SKIN DETACHED. REPAIRED IAW SRM 51-71-00-0G, PARA 19, AND EA 1-5720-T0331275, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201702120526Hinge Bracket · corrodedRIGHT WING, INBD FLAP, FWD (WING SIDE) OTBD HINGE PIVOT HOLE BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07 AND EA 1-5750-73360 D, PART 3, STEP 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201702120525Hinge Bracket · corrodedLEFT WING INBD FLAP FWD (WING SIDE) OTBD HINGE PIVOT HOLE BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-07 AND PER EA 1-5750-T0328840 D, PART 1, STEP 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201702060435Hinge Fitting · corrodedRIGHT WING OTBD FLAP INBOARD AFT HINGE (FLAP SIDE) INBOARD PIVOT BORE FOUND WITH CORROSION. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-04. BUSHING FABRICATED AND INSTALLED IAW EA 1-5750- T0331077, PART 1, STEP 1B. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2SDR FDEA201702020341Vane · corrodedRIGHT WING OTBD FLAP VANE NR 2 FITTING BUSHING HOLE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 57-50-02-2R FIG 201. A SLOT BUSHING WAS FABRICATED IAW EA 1-5750-T0331241, PART 1, STEP 2 AND INSTALLED IAW AMM 27-50-32-4.SDR FDEA201702020340Hinge Bracket · corrodedRIGHT WING OTBD FLAP AFT HINGE, FLAP SIDE, PIVOT OUTBD HOLE BORE FOUND CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132706 D, PART 4, STEP 2 & 3.SDR FDEA201702020339Hinge Bracket · corrodedRIGHT WING OTBD FLAP AFT HINGE, FLAP SIDE, PIVOT INBD HOLE BORE FOUND CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-132706 D, PART 4, STEP 2 & 3.SDR FDEA201702020338Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR INBD HOLE SURFACE CORRODED. REMOVED THE CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.SDR FDEA201702020337Hinge · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR OUTBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1C.SDR FDEA201702020336Hinge · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE, WING SIDE, ACTUATOR INBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1C.SDR FDEA201702020335Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE SURFACE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.SDR FDEA201702020334Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE SURFACE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1.SDR FDEA201702020333Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE CORRODED. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1, AND STEP 1B.SDR FDEA201702020332Hinge Bracket · corrodedRIGHT HAND WING OUTBD FLAP FWD INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE CORRODED. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1, AND STEP 1B.SDR FDEA201702020331Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD INBD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133, PART 1, STEP 1A.SDR FDEA201702020330Hinge Bracket · corrodedRIGHT WING OUTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT HOLE BORE CORROSION. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331133 PART 1, STEP 1A.SDR FDEA201702020329Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1B.SDR FDEA201702020328Hinge Bracket · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1B.SDR FDEA201702020327Hinge · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT OUTBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1, AND STEP 1A.SDR FDEA201702020326Hinge · corrodedRIGHT WING OTBD FLAP FWD OTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331132, PART 1, STEP 1, AND STEP 1A.SDR FDEA201702020325Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1B.SDR FDEA201702020324Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1B.SDR FDEA201702020323Hinge Bracket · corrodedLEFT WING OTBD FLAP FWD INBD HINGE (WING SIDE) UPPER MOUNT OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1A.SDR FDEA201702020322Hinge Bracket · corrodedLEFT WING OTBD FLAP FWD INBD HINGE (WING SIDE) UPPER MOUNT INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331077, PART 1, STEP 1A.SDR FDEA201702020321Hinge Bracket · corrodedLEFT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR INBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP 1B.SDR FDEA201702020320Hinge · corrodedLEFT WING OUTBD FLAP OUTBD FWD HINGE (WING SIDE) ACTUATOR OUTBD HOLE BORE CORRODED. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0331076, PART 1, STEP 1B.
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