N609FE
Service difficulty reports · 475
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 = 'N609FE' 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 = 'N609FE' 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 FDEA201804070905Unknown · odorFUMES IN THE COCKPIT, SMELLED LIKE RUBBER BURNING, NO SMOKE. WENT MAX BRIGHT ON ALL FLT DECK RHEOSTATS AND COURIER AREA LIGHTS WITH NO ODORS OR DEFECTS NOTED. OPENED SEVERAL FLT DECK, COURIER, AND ELEX BAY PANELS, NO ODORS OR DEFECTS NOTED. RAN ALL ENGINSDR FDEA201710052859Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. REWORKED IAW CMM 57-44-09. OUT OF LIMITS, A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335621, PART 1, STEP 2.SDR FDEA201709282777Tee Fitting · corrodedLT WING O/B FLAP VANE T FITTING 'B' FWD HOLE CORROSION. REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02- 2R FIG 201.EXISTING SLOT HOLE:L=0.858Ï¿½ X W=0.558Ï¿½, FINAL SLOT HOLE:L=0.957Ï¿½ X W=0.657Ï¿½, MAXIMIMUM ALLOWABLE SLOT HOLE; LSDR FDEA201709282776Tee Fitting · corrodedRT WING O/B FLAP VANE 'T' FITTING 'F' FWD HOLE CORROSION. REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIG 201.EXISTING SLOT HOLE:L=0.864Ï¿½X W=0.608Ï¿½, FINAL HOLE:L=0.950Ï¿½ X W=0.650Ï¿½, MAXIMIMUM ALLOWABLE SLOT HOLE; L=0.9SDR FDEA201709282775Tee Fitting · corrodedRT WING O/B FLAP VANE 'T' FITTING 'E' FWD HOLE CORROSION. REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R FIG 201.EXISTING SLOT HOLE:L=0.889Ï¿½X W=0.638Ï¿½, FINAL SLOT HOLE:L=0.9745Ï¿½ X W=0.680Ï¿½, MAXIMIUM ALLOWABLE SLOT HOLE; SDR FDEA201709282774Hinge · corrodedRT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B LUG SURFACE CORROSION. RH WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE LUG SURFACE CORROSION REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04 EXISTING THICKNESS 0.447", MATERIAL REMOVSDR FDEA201709282773Hinge · corrodedRT WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. RH WING O/B FLAP I/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-04 EXISTING HOLE 1.195", FINAL HOLE 1.200", MAXIMUM ALLOWABLE HSDR FDEA201709282772Hinge · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. RH WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08 EXISTING HOLE: 1.224", FINAL HOLE: 1.229SDR FDEA201709282771Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 1.2235", FINAL HOLE 1.229", MAXIMUM ALLOWABLE HOLE 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-SDR FDEA201709282770Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE 0.708", FINAL HOLE 0.712", MAXIMUM ALLOWABLE HOLE 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750-T0SDR FDEA201709282769Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.709", FINAL HOLE: 0.712", MAXIMUM ALLOWABLE HOLE: 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750SDR FDEA201709282768Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING THICKNESS: 760", MATERIAL REMOVED: 0.050", REMAINING THICKNESS: 0.710", MINIMUM ALLOWABLE THICKNESS: 0.720", REPAIR SDR FDEA201709282767Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT I/B BORE SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING THICKNESS: 0.729", MATERIAL REMOVED: 0.026" REMAINING THICKNESS: 0.703". REPAIR SHIM FABRICATED AND INSTALLED AS PERSDR FDEA201709282766Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.948", FINAL HOLE: 0.951", MAXIMUM ALLOWABLE HOLE: 0.944". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-575SDR FDEA201709282765Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.9535", FINAL HOLE: 0.957", MAXIMUM ALLOWABLE HOLE: 0.944". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-57SDR FDEA201709282764Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 2.317", FINAL HOLE: 2.321", MAXIMUM ALLOWABLE HOLE: 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750-T033562SDR FDEA201709282763Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT, OTBD BORE SURFACE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PT 1, STEP 1.SDR FDEA201709282762Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) FWD MOUNT, OTBD LUG SURFACE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0335603, PART 1, STEP 1.SDR FDEA201709282761Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1E.SDR FDEA201709282760Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1E.SDR FDEA201709282759Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) BARREL NUT HOLE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1F.SDR FDEA201709282758Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709282757Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709282756Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) UPPER MOUNT INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1A.SDR FDEA201709272750Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) UPPER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1A.SDR FDEA201709272749Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1C.SDR FDEA201709272748Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE: DIA: 1.222", FINAL HOLE: DIA: 1.228", MAXIMUM ALLOWABLE HOLE: DIA: 1.220". OVERSIZED BUSHING FABRICATED AND INSTASDR FDEA201709272747Hinge Arm · corrodedLT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE: DIA: 1.224", FINAL HOLE: DIA: 1.228", MAXIMUM ALLOWABLE HOLE: DIA: 1.220". OVERSIZED BUSHING FABRICATED AND INSTASDR FDEA201709272746Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD BORE CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709272745Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) LOWER MOUNT INBD BORE CORRODED. THE BORE CORROSION WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. FABRICATED AND INSTALLED A REPAIR IAW 1-5750-T0335583, PART 1, STEP 1B, AND STEP 1.SDR FDEA201709272744Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. CORROSION WAS WORKED IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1.SDR FDEA201709272743Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. CORROSION FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1A.SDR FDEA201709272742Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 1.253", FINAL HOLE: 1.259", MAXIMUM ALLOWABLE HOLE; 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1SDR FDEA201709272741Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 1.252", FINAL HOLE: 1.259", MAXIMUM ALLOWABLE HOLE: 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1SDR FDEA201709272740Hinge Arm · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.692", FINAL HOLE: 0.702", MAXIMUM ALLOWABLE HOLE: 0.667". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T03SDR FDEA201709272739Hinge · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.3255", FINAL HOLE: 0.408", MAXIMUM ALLOWABLE HOLE: 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER ESDR FDEA201709272738Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.390", FINAL HOLE: 0.408", MAXIMUM ALLOWABLE HOLE: 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EASDR FDEA201709272737Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.586", FINAL HOLE: 0.597", MAXIMUM ALLOWABLE HOLE: 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750SDR FDEA201709272736Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.586", FINAL HOLE: 0.597", MAXIMUM ALLOWABLE HOLE: 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750SDR FDEA201709272735Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 2.3165", FINAL HOLE: 2.322", MAXIMUM ALLOWABLE HOLE: 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T03356SDR FDEA201709252710Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T033099 A, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201709252709Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OTBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533C-PT5, STEP 2B, AND 2A. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2SDR FDEA201709252708Hinge Bracket · corrodedRIGHT WING INBD FLAP, OTBD AFT HINGE (FLAP SIDE) PIVOT INBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533C-PT5, STEP 2B, AND 2A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6SDR FDEA201709252707Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OTBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533E-PT6, STEP 2B, AND 2A. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GSDR FDEA201709252706Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD AFT HINGE (FLAP SIDE) PIVOT INBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533E-PT6, STEP 2B, AND 2A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-1SDR FDEA201709252705Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH OTBD BORE CORRDED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330993 A, PART 1, STEP 1F. REPAIR CLASSIFEID AS MAJOR IAW SDR FDEA201709252704Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD HINGE (WING SIDE) ACTUATOR ATTACH INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330993, PART 1, STEP 1F. REPAIR CLASSIFEID AS MAJOR IAW GMSDR FDEA201709252703Rib · crackedLEFT WING, ON REPLACEMENT OF THE NR 2 SLAT, THE OTBD EDGE ANGLE RIB WAS FOUND CRACKED. REMOVED AND REPLACED THE RIB IAW SRM 51-31-01-OG.SDR FDEA201709192629Access Panel · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON RT WING LEADING EDGE CUTOUT AND ACCESS DOORS, FOUND 01 EA CRACK AT REFUELING PANEL INBD CORNER, 0.5 INCH IN LENGTH. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 18. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-1SDR FDEA201709192628Access Panel · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON LT WING LEADING EDGE CUTOUT AND ACCESS DOORS, FOUND ONE CRACK AT REFUELING PANEL INBD CORNER, FIVE INCHES IN LENGTH. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 18. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-1
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