N605FE
Service difficulty reports · 508
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 = 'N605FE' 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 = 'N605FE' 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 05FDEA00085Longeron · dentedMAIN DECK, LONGERON 18L AT STA Y= 535 FOUND WITH DENT. FOUND MOUNTING FASTENER LOOSE LONGERON 18L AT STA Y= 535 - LOOSE FASTENERS REMOVED AND REPLACED PER SRM 51-31-01 VOLUME ISDR 05FDEA00064Stiffener · corrodedMAIN DECK, CENTER TANK, REAR SPAR UPPER CHORD ATTACHED STIFFENER FOUND CORRODED AT STA Y= 1371, X= 117 FORWARD OF SLANT PANEL. MAIN DECK, CENTER TANK, CORROSION ON REAR SPAR UPPER CHORD AT STA Y= 1371, X= 117. REMOVED AND REPROTECTED PER SRM 51-21-01 VOLUME SDR 05FDEA00080Spar Cap · corrodedRT WING, REAR SPAR UPPER CAP AT STA 1044 FOUND WITH CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-81590SDR 05FDEA00063Skin · corrodedRT WING, CORROSION FOUND BETWEEN XOS= 680 TO XOS= 725 UPPER SURFACE SPAR AREA. COMPLIED WITH FEDEX EA 1-5710-81591, CORROSION REMOVAL AND REPAIR. CORROSION REMOVED AT XORS STA 714 AS PER SRM 51-21-01 VOL. II FOUND WITHIN LIMITS AS PER SRM 57-10-00 FIG. 32 VOSDR 05FDEA00060Seat Track · wornMAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1099 TO Y= 1129, X= 27.50V FOUND WORN. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1SDR 05FDEA00056Structure · corrodedLT WING, TRAILING EDGE UPPER CHORD AT XORS= 1042 FOUND CORRODED. REPAIR CARRIED OUT AT LEFT HAND WING, TRAILING EDGE UPPER CHORD AT XORS= 1042 AS PER FEDEX EA 1-5710-81589, FOUND EXCEEDED LIMITS AS PER SRM 57-20-00 VOLUME I, FIGURE 16.SDR 05FDEA00055Seat Track · wornMAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 710 TO Y= 715, X= -8.50 SCALLOP FOUND WORN. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1.SDR 05FDEA00054Seat Track · damagedMAIN DECK, SEAT TRACK HORIZONTAL FLANGE UPPER SURFACE AT STA Y= 5-11 TO Y= 5-53, X= -75.25 FOUND FLOOR PANEL MOUNTING HOLE SHORT OF EDGE MARGIN. REPAIRED IAW SRM 53-70-00 VOLUME I, FIGURE 1.SDR 05FDEA00053Skin · dentedINNER LT WING LOWER SKIN AT XORS= 85 FOUND WITH 3.5 INCH DENT. COMPLIED WITH FEDEX EA 1-5710-81592.SDR 05FDEA00045Seat Track · corrodedMAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1841 TO Y= 1871, X= - 8.50 FOUND CORRODED. REMOVED AND REPAIRED PER SRM SRM 53-70-00 VOLUME I, FIGURE 1.SDR 05FDEA00040Seat Track · wornMAIN DECK, SEAT TRACK BETWEEN STA Y= 1219 TO Y= 1239, X= -47.50 FOUND WORN. SPLICED AND REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1.SDR 05FDEA00042Seat Track · wornMAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1501 TO Y= 5-11, X= 8.50 FOUND WORN. SPLICED AND TRIMMED PER SRM 51-33-01 VOLUME II; AND REPAIRED PER SRM 53-70- 00 VOLUME I, FIGURE 1.SDR 05FDEA00041Seat Track · wornMAIN DECK CARGO, SEAT TRACK BETWEEN STA Y= 1341 TO Y= 1401, X= - 47.50 FOUND WORN. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1.SDR 05FDEA00022Thrust Reverser · crackedNR 3 ENGINE, RT THRUST REVERSER, TRANSLATING COWL, UPPER TRACK, MOST AFT END FOUND WITH CRACKED. THRUST REVERSER P/N 683L221G04, S/N R592-084. NR 3 ENGINE, RT THRUST REVERSER REMOVED AND REPLACED PER AMM 78-33-01-4. THRUST REVERSER DOOR ADJUSTMENT AND CHECK SDR 05FDEA00021Thrust Reverser · crackedNR 3 ENGINE, LT THRUST REVERSER, TRANSLATING COWL, UPPER TRACK, MOST AFT END FOUND WITH CRACKED. THRUST REVERSER P/N 683L220G04, S/N R591-090 NR 3 ENGINE, LT THRUST REVERSER REMOVED AND REPLACED PER AMM 78-33-01-4. THRUST REVERSER DOOR ADJUSTMENT AND CHESDR 05FDEA00009Slat Track · crackedLEFT HAND WING, SLAT TRACK NR 16 INBOARD RIB FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-33-01 AND SRM 51-35-01. NR 16 SLAT TRACK ADJUSTMENT AND TEST CARRIED OUT PER AMM 27-80-00-2. OUTBOARD SLAT OPERATIONAL TEST CARRIED OUT PER AMM 27-80-00-5.SDR 05FDEA00004Seat Track · damagedMAIN DECK CARGO, SEAT TRACK AT STA Y= 791.75 TO Y= 859, X= 8.5 DAMAGED AT FLANGED AREA. REPAIRED PER SRM 53-70-00 VOLUME I, FIGURE 1SDR 04FDEA02814Control Unit · malfunctionedIN CRUISE FLT, AT FL 330, AT APPROX TAKEOFF PLUS FOUR HOURS, RECEIVED (LEVEL 1 TANK 2 FUEL QTY LO) ALERT S.D. FUEL READINGS WERE: 1- 900 2- 0 3-900 AUX- 900 TAIL- 12900. FUEL INDICATIONS AND USAGE TO THAT POINT HAD BEEN NORMAL. FSC WAS IN AUTO, ALSO GOT SDR 04FDEA02567Pitot Tube · obstructedON DESCENT DURING APPROACH GOT IAS ON PFD AND SELECT ELEV FEEL MAN, LVL 2 ALERT. ALSO HAD WINDSHEAR FAIL DET ALERT ON STATUS PAGE. STANDBY A/S SHOWED F/O'S INDICATOR ACCURATE. CAPT'S 10 KNOTS SLOW. RAN READ TAB. B Y TOUCHDOWN, F/O'S INDICATOR READ 156 KNOSDR 04FDEA02562Pitot Head · obstructedON DESCENT DURING APPROACH GOT IAS ON PFD AND SELECT ELEV FEEL MAN LVL 2 ALERT. ALSO HAD WINDSHEAR FAIL DET ALERT ON STATUS PAGE. STANDBY A/S SHOWED F/O'S INDICATOR ACCURATE. CAPT'S 10 KNOTS SLOW. RAN READ TAB. BY TOUCHDOWN, F/O'S INDICATOR READ 156 KNOSDR 03FDEA01200Spar Cap · corrodedHORIZONTAL STAB RT AFT SPAR CAP NR 36R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STABILIZER AFT SPAR CAP NR 36R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69404 - STABILIZERS - HORIZONTAL STABILIZERSDR 03FDEA01192Shim · out of positionRIGHT WING ROOT UPPER SURFACE- STRINGER NR 1 SHIM FOUND SEPARATED INTO 2 VISIBLE PIECES AND EACH WITH MIGRATION OF: (1) 0.7 INCH FWD AND 0.5 INCH DOWN AND (2) 0.6 INCH DOWN. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERSSDR 03FDEA01193Shim · out of positionLEFT WING ROOT- UPPER SURFACE- STRINGER NR 4 SHIM FOUND MIGRATED 0.6 INCH DOWN AND 0.4 INCH FWD. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTION.SDR 03FDEA01194Shim · out of positionLEFT WING ROOT- UPPER SURFACE STRINGER NR 3 SHIM FOUND MIGRATED 0.7 INCH DOWN. PREVIOUS RECORD IS 0.5 INCH. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTISDR 03FDEA01195Shim · out of positionLEFT WING ROOT- STRINGER NR 1 SHIM FOUND MIGRATED 0.3 INCH DOWN. COMPLIED WITH FEDEX EA 1-5710-55626B WINGS - BASIC WING STRUCTURE - LT & RT STRINGERS NR 1, NR 2, NR 3 & NR 4 SHIM MIGRATION PART II, FOLLOW-UP ACTION.SDR 03FDEA01199Skin · corrodedHORIZONTAL STAB RT UPPER CENTER PLANK NR 26R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. HORIZONTAL STABILIZER RT UPPER CTR PLANK NR 26R FITTING REMOVED & REPLACED AS PER FEDEX EA 1-5510-69397 - STABILIZERS - HORIZONTAL STABILIZERSDR 03FDEA01214Fitting · corrodedLT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND WITH CORROSION IN HOLE. LT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71810.SDR 03FDEA01213Fitting · corrodedLT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND WITH CORROSION IN HOLE. LT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71810, TITLE: WINGS TRAILING EDGE AND TRAILING EDGE DEVICES - LTSDR 03FDEA01212Fitting · corrodedRT WING O/B FLAP VANE- TEE FITTING NR 5 FROM INBOARD FOUND WITH CORROSION IN HOLE. RT WING O/B FLAP VANE- TEE FITTING NR 5 FROM INBOARD CORROSION IN HOLE, REPAIRED IAW EA 1-5750-71878.SDR 03FDEA01211Tee Fitting · corrodedSNRM N1007 - RT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND WITH CORROSION IN HOLE. SNRM N1007 - RT WING O/B FLAP VANE- TEE FITTING NR 4 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED IAW EA 1-5750-71878, TITLE: WINGS- TRAILING EDGE AND TRAILINSDR 03FDEA01210Tee Fitting · corrodedRIGHT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND WITH CORROSION IN HOLE. RT WING O/B FLAP VANE- TEE FITTING NR 3 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71878, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVICES- RISDR 03FDEA01209Fitting · corrodedRT WING O/B FLAP VANE- TEE FITTING NR 2 FROM INBOARD FOUND WITH CORROSION IN HOLE. RT WING O/B FLAP VANE- TEE FITTING NR 2 FROM INBOARD FOUND CORROSION IN HOLE REPAIRED AS PER FEDEX EA 1-5750-71878,SDR 03FDEA01175Splice · crackedCTR CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 46L SPLICE FITTING FOUND CRACK. CTR CARGO STA 5-113 THRU STA 1541 CRACK LONGERON 46L SPLICE REMOVED AND NEW SPLICE INSTALLED AS PER DWG A5A7114 AND SRM 51-33-01 VOL II.SDR 03FDEA01179Skin · corrodedRH HOR STAB UPPER AFT PLANK NR 27R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69279 - STABILIZERS - HORIZONTAL STABILIZER - CSDR 03FDEA01191Structure · corrodedRIGHT HORIZONTAL STABILIZER UPPER AFT PLANK NR 35R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-1-5000 LIMITATIONS. RIGHT HORIZONTAL STABILIZER UPPER AFT PLANK NR 35R BARREL NUT BORE REPAIR CARRIED-OUT AS PER FEDEX EA 1-5510-69402 - STABILIZERS - HORIZONTSDR 03FDEA01176Splice · crackedCENTER CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 45L SPLICE FITTING FOUND CRACK. CENTER CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 45L SPLICE FITTING REMOVED & REPLACED AS PER SRM 51-33-01 VOL II.SDR 03FDEA01174Splice · crackedCTR CARGO COMPT BILGE AREA STA 5-113 THRU 1541 LONGERON 49L SPLICE FITTING FOUND CRACK. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II.SDR 03FDEA01167Hinge · looseSNRM N0934 - RT WING- O/B FLAP (FLAP SIDE) O/B HINGE O/B PIVOT HOLE AND I/B AND O/B ACTUATOR ATTACHMENT HOLES FOUND BUSHING LOOSE. ** S/D ** COMINGSDR 03FDEA01169Barrel Nut · corrodedRT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE FOUND CORROSION BEYOND EO 1-5510-7-5000 LIMITATIONS. RT HORIZONTAL STAB UPPER AFT PLANK NR 27R BARREL NUT BORE REPAIR CARRIED- OUT AS PER FEDEX EA 1-5510-69279 - STABILIZERS - HORIZONTAL STABILIZER - SDR 03FDEA01189Hinge · corrodedSNRM N0866 - RT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. CORRECTIVE ACTION: SNRM N0866 - RT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS IAW EA 1-5750-71806, TITLE: WINSDR 03FDEA01168Support · crackedLT WING- O/B FLAP STOP BOLT SUPPORT ISLAND FOUND CRACKED. LT OUTBD FLAP STOP BOLT SUPPORT ISLAND REPAIRED AS PER FEDEX EA 1- 5750-69259 - WINGS - TRAILING EDGE FLAPS - LT OUTBOARD FLAP SECONDARY UP STOP REPAIR.SDR 03FDEA01170Splice · crackedCTR CARGO RT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING FOUND CRACK. CTR CARGO RT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING REMOVED AS PER SRM 51-33-01 VOL II. NEW SPLICE FITTING FABRICATED AS PER DWG A5A7114 AND INSTALLED AS PER SRM 51-33-01 VOL II.SDR 03FDEA01172Splice · crackedCTR CARGO LEFT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING FOUND CRACK. LEFT TUNNEL STA 5-123 LONGERON 37 SPLICE FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.SDR 03FDEA01171Splice · crackedCTR CARGO RT TUNNEL STA 5-123 LONGERON 38 SPLICE FITTING FOUND CRACK. CTR CARGO RT TUNNEL STA 5-123 LONGERON 38 SPLICE FITTING FABRICATED AS PER DWG A5A7114 & INSTALLED AS PER SRM 51-33-01 VOL II.SDR 03FDEA01187Hinge · corrodedRT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. RT WING O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-69405 - WINGS - TRAILING EDGE & TRAILING EDGE DEVICES SDR 03FDEA01216Hinge · corrodedRIGHT WING- I/B FLAP (WING SIDE) O/B HINGE PIVOT LUG I/B SURFACE CORRODED. RIGHT WING- I/B FLAP (WING SIDE) O/B HINGE PIVOT LUG I/B SURFACE REPAIRED AS PER FEDEX AE 1-5750-71880, TITLE: WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES- RT INBOARD FLAP OUTBOARDSDR 03FDEA01215Hinge · corrodedLT WING I/B FLAP (WING SIDE) O/B HINGE PIVOT BORE AND I/B LUG SURFACE CORRODED. LT WING I/B FLAP (WING SIDE) O/B HINGE PIVOT BORE AND I/B LUG SURFACE REPAIRED AS PER FEDEX EA 1-5750-71881 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBD FLAP OSDR 03FDEA01190Hinge · corrodedLEFT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. LEFT WING- O/B FLAP (WING SIDE) I/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-69406, TITLE: WINGS- TRAILING EDGE AND TRAILING EDGE DEVISDR 03FDEA01186Hinge · corrodedLT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES CORRODED. LT WING- O/B FLAP (WING SIDE) O/B HINGE I/B AND O/B ACTUATOR ATTACHMENT HOLES REPAIRED AS PER FEDEX EA 1-5750-71807.SDR 03FDEA01188Hinge · corrodedLEFT O/B FLAP (WING SIDE) I/B HINGE LOWER REAR SPAR MOUNT O/B HOLE AND AFT NUT ATTACHMENT SURFACE CORRODED. LEFT O/B FLAP (WING SIDE) I/B HINGE LOWER REAR SPAR MOUNT O/B HOLE AND AFT NUT ATTACHMENT SURFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08 AN
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