N610FE
Service difficulty reports · 497
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 = 'N610FE' 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 = 'N610FE' 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 FDEA201203140933Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP HINGE, CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. REPAIR CARRIED OUT IAW STEP 1, 2, 9, 10, 11 AND 12 OF EA 1-5750-150447, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201203140931Vane · corrodedRT WING OTBD FLAP VANE FITTING, FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02, FIG 201, REV 48. REPAIR BUSHING FABRICATED AND INSTALLED IAW EA1-5750-150450. PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201203140934Bushing · wornRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, OTBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIA 1.224" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-04, REV 72 , MAX ALLOWABLE DIA 1.220", BUSHING FABRICATED AND INSTALLED IAW SDR FDEA201203140932Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIA 1.223", FINAL HOLE DIA. 1.249" , MAX ALLOWABLA DIA 1.220" REPAIR CARRIED OUT IAW STEP 1,2,9,10,11 ASDR FDEA201203130912Fitting · corrodedRIGHT WING OTBD FLAP VANE FITTING F ECCENTRIC HOLE FOUND CORRODED. FOUND EXCEEDED LIMITS IAW SRM 57-50-02 FIG 201, REV 48 EXISTING HOLE:0.851"(LENGTH), 0.557"(WIDTH). FINAL HOLE 0.944"(LENGTH), 0.660"(WIDTH). MAXIMUM HOLE 0.940"(LENGTH), 0.670"(WIDTH).REPAIR SDR FDEA201203130911Fitting · corrodedLEFT WING OTBD FLAP VANE FITTING B ECCENTRIC HOLE FOUND CORRODED. FOUND EXCEEDED LIMITS IAW SRM 57-50-02, FIG 201, REV 48 EXISTING HOLE:0.873"(LENGTH), 0.623"(WIDTH). FINAL REWORK HOLE 0.930"(LENGTH), 0.706"(WIDTH). MAXIMUM REWORK HOLE 0.940"(LENGTH), 0.640"SDR FDEA201203120888Hinge · damagedRT WING OTBD FLAP, OTBD HINGE BUSHING ON PIVOT HOLE REMOVED IAW CMM 20-20-07, REV 72 . BORE MEASURED DIA 2.315" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 MAX ALLOWABLE, DIA 2.3135". NEW BUSHING FABRICATED AND INSTALLED IAW STEP 10 AND 11 OF EA 1-57SDR FDEA201203120894Skin · chafedLT WING NR 3 L/E SLAT TELESCOPIC DUCT CUTOUT FOUND CHAFED. REPAIRED IAW SRM 51-31-01, REV 48. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201203120893Hinge Fitting · damagedLT WING (FLAP SIDE) INBD FLAP OTBD HINGE INBD PIVOT HOLE FOUND STEP HOLE. MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 72 . EXISTING HOLE DIA 1.190", /1.253" , MAXIMUM HOLE DIA 1.220" BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-150446, PART 1 SDR FDEA201203120892Bushing · wornLT WING (FLAP SIDE) INBD FLAP OTBD HINGE OTBD PIVOT HOLE BUSHING WORN. REMOVED IAW CMM 20-20-07, REV 72 EXISTING HOLE DIA 1.283", MAX ALLOWABLE HOLE DIA 1.220" HOLE MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 72 . BUSHING FABRICATED AND INSTALLEDSDR FDEA201203120890Bushing · wornRT WING (FLAP SIDE) INBD FLAP, OTBD HINGE INBD PIVOT HOLE BUSHING WORN. BUSHING REPAIRED IAW EA 1-5750-160001, PART 1. EXISTING HOLE DIA 1.283", MAX HOLE DIA 1.220", NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-160001 PART 1, STEP 4 AND 5. REPAIR CLSDR FDEA201203120889Hinge Fitting · damagedRT WING (FLAP SIDE) INBD FLAP OTBD HINGE OTBD PIVOT HOLE FOUND STEP HOLE. REPAIRED IAW EA 1-5750-160001, PART 1. EXISTING HOLE DIA.1.282" /1.192", MAX ALLOWABLE HOLE DIA 1.220". NEW BUSHING FABRICATED AND INSTALLED IAW EA 1-5750-160001 PART 1, STEP 4 ANSDR FDEA201203120885Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE PIVOT HOLE FOUND EXCEEDED CMM LIMITS AFTER BUSHING REMOVAL FOR NDT ACCESS. MEASURED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 EXISTING HOLE DIA 2.315" MAX ALLOWABLE DIA 2.3135'. REPAIR CARRIED OUT IAW EA 1-57SDR FDEA201203120883Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP OTBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 EXISTING HOLE DIA 0.582', FINAL HOLE DIA 0.598", MAX. ALLOWABLE DIA 0.584' REPAIR CARRIED OUT IAW EA 1-5750-150447, PARSDR FDEA201203120882Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP OTBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72 . EXISTING HOLE DIA 0.585", FINAL HOLE DIA. 0.598", MAX ALLOWABLE HOLE DIA.0.584" REPAIR CARRIED OUT IAW STEP 3 OF EA 1-5SDR FDEA201203120881Hinge Fitting · corrodedRT WING (WING SIDE) OTB FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 57-44-09, REV 72. EXISTING THK UPPER:0.412", LOWER:0.408". REMAINING THK UPPER:0.407", LOWER:0.403'. MATERIAL REMOVED: UPPER: 0.005", LOWER:0.005" IAW STEP SDR FDEA201203120880Bushing · wornRT WING (WING SIDE) OTBD FLAP INBD HINGE INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED CMM 20-20-07, REV 72. BORE MEASURED DIA 1.223", AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. MAX ALLOWABLE DIA 1.220", WASHER INSTALLED IAW EA 1-5750-160003, PARSDR FDEA201203120879Hinge Fitting · wornRT WING (WING SIDE) OTBD FLAP INBD HINGE OTBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED CMM 20-20-07, REV 72 BORE MEASURED DIA 1.222", AND FOUND EXCEEDED LIMIT IAW 1 CMM 57-44-08 REV 72. MAX ALLOWABLE DIA.1.220" .BUSHING FABRICATED AND INSTALLED IAW STEP 5 SDR FDEA201203120878Hinge Fitting · corrodedRIGHT WING (WING SIDE) OTBD FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 57-44-08, REV 72. EXISTING THICKNESS UPPER: 0.375", LOWER: 0.355", REMAINING THICKNESS UPPER: 0.365", LOWER: 0.345", MATERIAL REMOVED UPPER: 0.010", LOWER SDR FDEA201203090844Longeron Splice · crackedDURING X-RAY INSPECTION, FOUND A CRACK ON STA 5-123, LONGERON SPLICE 2 LT. LONGERON REMOVED IAW SRM 51-31-01, REV 48. NEW LONGERON SPLICE FABRICATED IAW DWG A5A7111-501, REV C. NEW FABRICATED LONGERON SPLICE INSTALLED IAW SRM 51-31-01, REV 48. REPAIR CLASSDR FDEA201203090843Bushing · migratedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE PIVOT HOLE REPAIR BUSHING FOUND MIGRATED. REPAIRED IAW EA 1-5750-160002 STEP 3, 7, 8 AND 9 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201203090842Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5750-160002, STEP 4 AND 5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201203090841Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-160002, PART 1, STEP 2,7,8,9 AND 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201203090840Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP INBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-160002, PART 1, STEP 2.SDR FDEA201203090839Bushing · wornLEFT WING (WING SIDE) OTBD FLAP INBD HINGE, INBD ACTUATOR, HOLE BUSHING WORN. REPAIRED IAW EA 1-5750-160002, PART 1, STEP 1, 7, 8 AND 9 .SDR FDEA201203090838Bushing · wornLEFT WING (WING SIDE) OTBD FLAP INBD HINGE OTBD ACTUATOR HOLE BUSHING WORN. REPAIRED IAW EA1-5750-160002, PART 1 STEP 1, 7, 8 AND 9 .SDR FDEA201203090837Bushing · wornLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE INBD ACTUATOR HOLE BUSHING WORN. MEASURED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72. EXISTING HOLE DIA 1.254", MAX HOLE DIA 1.220", BUSHING FABRICATED AND INSTALLED IAW STEP 9 AND 10. WASHER FABRICATED IAW SSDR FDEA201203090836Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72 . EXISTING HOLE DIA. 0.398", FINAL HOLE 0.4095", MAX HOLE DIA. 0.391", BUSHING FABRICATED AND INSTALLED PER STEPSDR FDEA201203090835Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE SIDE LOAD FITTING LOWER HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72 EXISTING HOLE DIA. 0.398", FINAL HOLE DIA. 0.4095", MAX HOLE DIA. 0.391", BUSHING FABRICATED AND INSTALLED IAW SDR FDEA201203090834Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW REV 72 UPPER FACE EXISTING THICKNESS: 0.413", MATERIAL REMOVED :0.003", REMAINING THICKNESS :0.410", LOWER FACE EXISTING THICKNESS: 0.410", MATERIAL REMOVED :0SDR FDEA201203090833Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP OTBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72. MAX ALLOWABLE DIA.0.584", EXISTING HOLE DIA 0.538", FINAL HOLE DIA 0.595", BUSHING FABRICATED AND INSTALLED IAW STEP SDR FDEA201203090832Hinge Fitting · corrodedLEFT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09, REV 72. EXISTING HOLE DIA 0.585", FINAL HOLE DIA.0.597", MAX HOLE DIA 0.584". BUSHING FABRICATED AND INSTALLED AS IAW STESDR FDEA201203070796Attach Fitting · crackedRIGHT WING T/E OTBD FLAP L/E STOP BOLT ATTACHMENT FITTING FOUND CRACKED. ATTACH FITTING REMOVED AND REPLACED AS PER EA 1-5750-160011.SDR FDEA201203070795Attach Fitting · crackedLEFT WING T/E OTBD FLAP L/E STOP BOLT ATTACHMENT FITTING FOUND CRACKED. FITTING REMOVED AND REPLACED AS PER EA 1-5750-160010. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 114.SDR FDEA201203060790Skin · crackedRIGHT WING FIXED L/E SKIN FOUND CRACKED AT NR 8 SLAT TRACK CUTOUT INBD SIDE, LOWER CORNER. REPAIR CARRIED OUT AS PER SRM 57-40-02 REPAIR 7 FIG.201 REV 48. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 114.SDR FDEA201203050779Roller Tray · corrodedCENTER CARGO COMPARTMENT STA 1701, X=-58 (APPROX) FOUND ROLLER TRAY WITH SURFACE CORROSION. NEW ROLLER TRAY REWORKED AS PER DRAWING AFJ7063 REV. A NEW ROLLER TRAY INSTALLED AS PER AMM 20-50-02 REV 72 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 114.SDR FDEA201203050778Beam · crackedL3 DOOR NR 2 STOP BEAM FOUND CRACKED. STOP BEAM REMOVED AND REPLACED AS PER SRM 51-31-01 REV 48. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 114.SDR FDEA201203050777Skin · crackedLT WING NR 5 L/E SLAT OTBD TRACK CUTOUT LOWER OTBD CORNER FOUND CRACKED. REPAIR CARRIED IAW SRM 57-40-02 REPAIR 7 FIG.201 REV 48 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 114.SDR FDEA201203050776Access Panel · crackedLT WING L/E LOWER SURFACE ACCESS PANEL 519CB FWD INBD CORNER, FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 REPAIR 7 FIG.201 REV 48. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV.114SDR FDEA201012014530Pressure Switch · failedDUE TO ENG NR 3 FUEL FILTER AND MASTER CAUTION LIGHT . SPEED 50 KTS. NO MAX BREAKING RECEIVED. R & R FUEL FILTER PRESSURE SWITCH.SDR FDEA201003220955Bushing · damagedLT HORIZ STABILIZER INBD L/E 2 EACH BUSHING FOUND DAMAGED. REPAIRED AS PER EA1-5510-132389.SDR FDEA201003200945Panel · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = 55 CTR TANK UPPER SURFACE AFT PANEL FOUND WITH SURFACE CORROSION. REPAIR AS PER EA 1-5710-132380.SDR FDEA201003200944Panel · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = 10 CTR TANK UPPER SURFACE AFT PANEL FOUND WITH SURFACE CORROSION. REPAIR AS PER EA 1-5710-132380.SDR FDEA201003200943Panel · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = 8 CTR TANK UPPER SURFACE AFT PANEL FOUND WITH SURFACE CORROSION ON (2) LOCATIONS. REPAIR AS PER EA 1-5710-132380.SDR FDEA201003200942Fuel Tank · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = -35 CTR TANK UPPER SURFACE AFT PANEL FOUND WITH SURFACE CORROSION. REPAIRED AS PER EA 1-5710-132380.SDR FDEA201003200941Panel · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = -37 CTR TANK UPPER SURFACE AFT PANEL FOUND WITH SURFACE CORROSION. REPAIR AS PER EA 1-5710-132380.SDR FDEA201003200940Fuel Tank · corrodedMAIN DECK CARGO - STA 1229, APPROX 'X' = -55 CTR TANK UPPER SURFACE AFT PANEL FOUND SURFACE CORROSION AT (3) LOCATIONS. REPAIR AS PER EA 1-5710-132380.SDR FDEA201003200939Fuel Tank · corrodedMAIN DECK CARGO - STA 1229, APPROX. 'X' = -60 CTR TANK UPPER SURFACE AFT PANEL FOUND SURFACE CORROSION AT THREE (3) LOCATIONS. REPAIR AS PER EA 1-5710-132380.SDR FDEA201003200938Fuel Tank · corrodedMAIN DECK CARGO - STA 1229, APPROXIMATELY 'X' = -90 CENTER TANK UPPER SURFACE AFT PANEL FOUND SURFACE CORROSION AT ONE (1) LOCATION. REPAIR AS PER EA 1-5710-132380.SDR FDEA201003200937Fuel Tank · corrodedMAIN DECK CARGO - STA 1229 'X' = -100 CTR TANK UPPER SURFACE AFT PANEL FOUND SURFACE CORROSION AT (2) LOCATIONS. REPAIR AS PER SRM 51-21-01 REV 43 AND SRM 57-10-01 REV 43.
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