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 07FDEA00666Spar Cap · corrodedRIGHT WING REAR SPAR UPPER CAP FOUND CORROSION AT XORS 1043. SUPPLEMENTAL 21 MARCH 07; CORROSION REMOVED ON RIGHT HAND WING REAR SPAR UPPER CAP XORS 1043 AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS = 0.119", MATERIAL REMOVED = 0.039", REMAINED THICKNESSSDR 07FDEA00642Stringer · crackedCRACK FOUND AT STRINGER END 14R (XORS 521), APPROX 14" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 14R (XORS 521) ON RIGHT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICES AS PER SRM 57-20-00 FIGUSDR 07FDEA00641Stringer · crackedCRACK FOUND AT STRINGER END 13R (XORS 577), APPROX 11" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 13R (XORS 577) ON RIGHT HAND WING TANK TRIMMED OUT 2 BAY AND REPAIRED WITH SPLICES AS PER SRM 57-20-00 SDR 07FDEA00640Stringer · crackedCRACK FOUND AT STRINGER END 12R (XORS 642), APPROX. 9" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 12R (XORS 642) ON RIGHT HAND WING TANK CARRIED OUT REPAIR AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAISDR 07FDEA00639Stringer · crackedCRACK FOUND AT STRINGER END 9R (XORS 819), APPROX 13" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 9R (XORS 819) ON RIGHT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICES AS PER SRM 57-20-00 FIGURSDR 07FDEA00638Stringer · crackedCRACK FOUND AT STRINGER END 10R (XORS 760), APPROX. 13" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 10R (XORS 760) ON RIGHT HAND WING TANK SLOTTED OUT AND ANGLE REPAIR CARRIED OUT AS PER SRM 57-20-00 FSDR 07FDEA00637Stringer · crackedCRACK FOUND AT STRINGER END 11R (XORS 704), APPROX 12.5" LENGTH ON RIGHT WING TANK, DURING HFEC INSPECTION. CRACK AT STRINGER END 11R (XORS 704) ON RIGHT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICES AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSDR 07FDEA00636Stringer · crackedCRACK FOUND AT STRINGER END 44L (XORS 523), APPROX 1" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 44L (XORS 523) ON LEFT HAND WING TANK SLOTTED OUT AND REPAIRED WITH NEW REPAIR SPLICE AS PER SRM 57-SDR 07FDEA00635Stringer · crackedCRACK FOUND AT STRINGER END 14L (XORS 521), APPROX 13" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. CRACK AT STRINGER END 14L (XORS 521) ON LEFT HAND WING TANK TRIMMED OUT AND REPAIRED WITH SPLICE REPAIR AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSDR 07FDEA00634Stringer · crackedCRACK FOUND AT STRINGER END 42L (XORS 629), APPROX 1" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. (SUPPLEMENTAL 23 MARCH 07) CRACK AT STRINGER END 42L (XORS 629) ON LEFT HAND WING TANK SLOTTED OUT AND REPAIRED WITH NEW REPAIR SPLICE AS PER SRM 57-20SDR 07FDEA00633Stringer · crackedCRACK FOUND AT STRINGER END 9L (XORS 819), APPROX 10" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. SUPPLEMENTAL 21 MARCH 07, CRACK ON STRINGER END 9L (XORS 819) SLOTTED OUT AND REPAIRED WITH ANGLES AS PER SRM 57-20 -00 FIGURE 10 VOLUME I. REPAIR CLASSSDR 07FDEA00632Duct · crackedRIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. (SUPPLEMENTAL 23 MARCH 07) CRACK AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57 -10-00 FIGURE 42 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA1579Odor · unknownPDIS: DURING CRUISE ENCOUNTERED ICING CONDITIONS. WHEN WINDOW HEAT WAS TURNED ON A VERY STRONG ELECTRICAL SMOKE SMELL. NO VISIBLE SMOKE. NARROWED SMELL DOWN TO THE F/O (RIGHT) WINDOW HEAT. REPLACED ANTI-ICE CONTROL PANEL PRECAUTIONARY. REPLACED WINDSHIELDSDR 05FDEA02810Skin · damagedWHILE PERFORMING REPEATITIVE INSPECTIONS ON EXISTING SKIN EXTERNAL DOUBLER REPAIR AT STA Y1811 LONGERON 36R, FOUND THE REPAIR DOUBLER WITH SEVERAL SUNK IN FASTENER HEADS. REPAIR DOUBLER REMOVED AS PER SRM 51-31-01 VOLUME II. NEW REPAIR DOUBLER FABRICATED AS SDR 05FDEA02752Seat Track · crackedUPPER CARGO, SEAT TRACK RBL 47 CRACKED AT STA 1019. REPAIRED AS PER SRM 53-70-00.SDR 05FDEA02751Skin · crackedCRACK INDICATIONS ON NR 5 BORE HOLES FOUND DURING HFEC INSPECTION AT LEFT HAND WING LOWER SKIN DOOR CUTOUT OF PANEL 536AB. FOUND HOLES CRACK LENGTH APPROXIMATELY 0.100", 1 HOLE CRACK LENGTH APPROXIMATELY 0.187" ON BORE SURFACE. REPAIR CARRIED OUT AS PER FEDESDR 05FDEA02735Seat Track · corrodedUPPER CARGO, SEAT TRACK RBL 27 CORRODED AT STA 1745. UPPER CARGO STA 1745 RBL 27 SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. THIS REPAIR IS CLASSIFIED AS MAJORE REPAIR AS PER GMM 6-2-100.SDR 05FDEA02733Bulkhead · crackedCENTER WHEEL WELL LEFT FORWARD BULKHEAD SPOILER PUSHROD (MJ) FEED THROUGH CUTOUT REINFORCEMENT DOUBLER FOUND CRACKED. CTR WHEEL WELL LT FWD BULKHEAD SPOILER PUSH ROD (MJ) FEEDTHROUGH CUTOUT REINFORCEMENT DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-01 VOL IISDR 05FDEA02715Seat Track · crackedUPPER CARGO, SEAT TRACK RBL 11 CRACKED AT STA 630. REMOVED AS PER SRM 53-70-00 VOL I FIG 1. NEW TRACK REWORKED AND INSTALLED AS PER SRM 53-70-00 VOL I FIG 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 05FDEA02714Seat Track · crackedUPPER CARGO, SEAT TRACK RBL 27 CRACKED AT STA 630. UPPER CARGO STA 625 TO STA 665 RBL 27 SEAT TRACK REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR 05FDEA02702Seat Track · crackedUPPER CARGO, SEAT TRACK RBL 47 CRACKED AT STA 939 TO STA 979. REMOVED AS PER SRM 53-70-00 VOL1 FIG1. NEW TRACK AND SPLICE REWORKED AS PER SRM 53-70-00 VOL 1 FIG1. NEW TRACK AND SPLICE INSTALLED AS PER SRM 53-70-00 VOL1 FIG 1. REPAIR CLASSIFIED MAJOR AS PSDR 05FDEA02701Seat Track · crackedUPPER CARGO, SEAT TRACK LBL 27 CRACKED AT STA 1169. REPAIRED AS PER SRM 53-70-00 VOLUME I FIGURE 1. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR 05FDEA02700Seat Track · corrodedUPPER CARGO, SEAT TRACK RBL 11 CORRODED AT STA 1121 TO STA 6-10. REMOVED AS PER SRM 51-31-01 VOL 2. NEW SEAT TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOL 1 FIG1. NEW SEAT TRACK AND SPLICE INSTALLED AS PER SRM 51-35-01 VOL 2. REPAIR CLASSIFIED MAJOR SDR 05FDEA02699Seat Track · crackedUPPER CARGO, SEAT TRACK 47 CRACKED AT STA 1095 TO STA 6-51. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. THIS REPAIR CLASSIFED AS MAJOR REPAIR AS PER GMM 6-2-100.SDR 05FDEA02698Seat Track · crackedUPPER CARGO, SEAT TRACK RBL 27 CRACKED AT STA 6-30. REMOVED AS PER SRM 53-70-00 VOLUME I FIGURE 1. NEW TRACK AND SPLICE FABRICATED AS PER SRM 53-70-00 VOLUME I FIGURE 1. NEW TRACK AND SPLICE INSTALLED AS PER SRM 53-70-00 VOLUME I FIGURE 1. REPAIR CLASSIFISDR 05FDEA02697Seat Track · crackedUPPER CARGO, SEAT TRACK LBL 27 CRACKED AT STA 1338. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 04FDEA03236Tube · brokenDURING CRUISE AT F330 LEVEL 2, ALERT"ENG 2 OIL PRESS LOW" OBSERVED OIL PRESS READING 4 IN RED. ALSO, OBSERVED OIL QTY ZERO (0) ON ENG 2. COMPLIED WITH APPROPRIATE QRH PROCEDURES. AFTER SHUT DOWN N1 26.1 EGT 7 N2 22 .1 ENG SHUT DOWN AT 1350Z, LANDED AT 160SDR 04FDEA02657Engine · leakingAFTER START NR 2 ENG OIL WAS APPROX 15 QTYS. AFTER 1 37 OIL QTY DECREASED TO 10 QTYS. MONITORED AND SLOW LEAK OVER THE NEXT 45 MIN DOWN TO 4 QTYS. NR 2 ENG SHUT DOWN AT 6 QTYS. OIL TEMP AND PRESS NORMAL DURING THE LEAK. FND OIL TUBE ASSY P/N 1800M14G01 BROKESDR 04FDEA01640Tee Fitting · corrodedLEFT WING - I/B FLAP VANE O/B TEE FITTING BORE FOUND CORRODED. LEFT WING - I/B FLAP VANE O/B TEE FITTING BORES CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.877 INCH, CENTER=0.878 INCH, AFT=0.8785 INCH. FPI CARRIED OUT, RESULT: NO COSDR 04FDEA01639Tee Fitting · corrodedRIGHT WING - I/B FLAP VANE O/B TEE FITTING BORE FOUND CORRODED. RIGHT WING - I/B FLAP VANE O/B TEE FITTING BORES CORROSION REMOVED PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.8795 INCH, CENTER=0.8775 INCH, AFT=0.8790 INCH. FPI CARRIED OUT, RESULT: NO CORRSDR 04FDEA01638Fitting · corrodedRIGHT WING - I/B FLAP VANE I/B TEE FITTING BORE FOUND CORRODED. RIGHT WING - I/B FLAP VANE I/B TEE FITTING BORES CORROSION REMOVED PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.879 INCH, CENTER=0.880 INCH, AFT=0.880 INCH. FPI CARRIED OUT, RESULT: NO CORROSDR 04FDEA01637Fitting · corrodedLEFT WING - I/B FLAP VANE I/B TEE FITTING BORE FOUND CORRODED. LEFT WING - I/B FLAP VANE I/B TEE FITTING BORES CORROSION REMOVED AS PER SRM 51-21-01 VOL 2. BORES DIAMETER: FWD=0.8765 INCH, CENTER=0.877 INCH, AFT=0.880 INCH. FPI CARRIED OUT, RESULT: NO COSDR 04FDEA01512Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, FINAL DIAMETER: 1.1221, MAX ALLOWABLE DIAMETER: 1.190, EXCEED ALLOWABLE LIMIT AS PERSDR 04FDEA01511Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER:1.187, FINAL DIAMETER: 1.1221, MAX ALLOWABLE DIAMETER: 1.190, EXCEED ALLOWABLE LIMIT AS SDR 04FDEA01510Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), UPPER I/B MOUNTING BOLT BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL DIAMETER: 0.879, FINAL DIAMETER: 0.952, MAX ALLOWABLE DIAMETER: 0.944, EXCEED ALLOWABLE LIMIT AS PERSDR 04FDEA01509Hinge · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE), LOWER MOUNTING SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402 TO 407 FIG 401. ORIGINAL THICKNESS OF LUG: 0.481, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.479, MINIMUM ALLOWABLE THISDR 04FDEA01508Hinge · corrodedRT WING OB FLAP IB HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. RT WING O/B FLAP I/B HINGE (WING SIDE), SIDE LINK SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 FIG 1, PAGES 402 TO 407. ORIGINAL THICKNESS OF LUG: 0.429, MATERIAL REMOVED: 0.002, RESDR 04FDEA01417Frame · chafedMAIN DECK - FRAME FOUND TWO CHAFED MARK AT STA 535 LT BETWEEN 9G NET ATTACH YOKE. MAIN DECK - FRAME AT STA 535 LT BETWEEN 9G NET ATTACH YOKE DISCREPANT AREAS (2 LOCATIONS) TRIMMED OUT AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503.SDR 04FDEA01419Seat Track · corrodedSEAT TRACK LBL 8.5 CORRODED AT STA 1119 TO STA 6-50. REMOVED AND REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I.SDR 04FDEA01418Frame · chafedMAIN DECK - FRAME FOUND TWO CHAFED MARK AT STA 535 RIGHT BETWEEN 9G NET ATTACH YOKE. DISCREPANT AREAS (2 LOCATIONS) TRIMMED OUT AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503.SDR 04FDEA01416Frame · chafedMAIN DECK FRAME FOUND TWO CHAFED MARKS AT STA 535 LEFT BETWEEN 9G NET ATTACH YOKE. DISCREPANT AREAS (2 LOCATIONS) TRIMMED OUT AND REPAIR CARRIED OUT AS PER DWG SRZ-53-503.SDR 04FDEA01395Floor Support · corrodedMAIN DECK, FLOOR SUPPORT CORRODED AT STA 409, RBL 14. FLOOR SUPPORT CORRODED AT STA 409, RBL 14 REMOVED IAW SRM 51-33-01 VOL II, NEW FLOOR SUPPORT HOLES TRANSFERRED IAW SRM 51-31-01-VOL II AND INSTALLED IAW SRM 51-33-01 VOL II.SDR 04FDEA01394Seat Track · corrodedMAIN DECK R1 DOOR WAY SEAT TRACK FOUND CORROSION AT STA 440 RT 86 INCHES. REMOVED IAW SRM 51-33-01 VOL II. NEW SEAT TRACK HOLES TRANSFERRED IAW SRM 51-31-01 VOL II, PROTECTED IAW SRM 51-21-01 VOL II AND INSTALLED IAW SRM 51-33-01 VOL II.SDR 04FDEA01393Seat Track · crackedMAIN DECK - SEAT TRACK FOUND CRACKED AT STA 902-914 RT 28 INCHES. REMOVED AT STA 459 TO STA 535 RBL 27.5 IAW SRM 51-33-01 VOL II, REPAIR TRACK FABRICATED AND INSTALLED IAW SRM 53-70-00 FIGURE 1 VOL I.SDR 04FDEA01391Floor Support · corrodedMAIN DECK FLOOR SUPPORT FOUND CORROSION AT STA 457 LT 87 INCHES. REMOVED IAW SRM 51-31-01 VOL II, NEW SUPPORT MACHINED AS PER DWG ABA8356 AND INSTALLED IAW SRM 51-31-01 VOL II.SDR 04FDEA01390Seat Track · crackedSEAT TRACK FOUND CRACKED AT STA 902-914 RIGHT 28 INCHES. SEAT TRACK CUT AND REMOVED AT STA 869 TO STA 969 RBL 27.5 AND REPAIR CARRIED OUT IAW SRM 53-70-00 FIG 1 VOL I.SDR 04FDEA01373Hinge · corrodedLEFT WING - O/B FLAP O/B HINGE (WING SIDE), SIDE LINK BARREL NUT HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 0.593, MAX ALLOWABLE DIAMETER: 0.667, FINAL DIAMETER: 0.661 WITHIN LIMIT. REPAIRED AS PESDR 04FDEA01372Hinge · corrodedLEFT WING - O/B FLAP O/B HINGE (WING SIDE), SIDE LINK SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL THICKNESS OF LUG: 0.452, MATERIAL REMOVED: 0.002, REMAINING THICKNESS OF LUG: 0.450. REPAIRED AS PER EA 1-SDR 04FDEA01371Hinge · corrodedLEFT WING - O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. BORE CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 1.187, MAX DIAMETER: 1.190, FINAL DIAMETER: 1.250 EXCEEDED LIMIT. REPAIRED AS PERSDR 04FDEA01370Hinge · corrodedLEFT WING - O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. BORE CORROSION REMOVED AS PER CMM 57-44-09 FIG 401 PAGES 402 TO 407. ORIGINAL DIAMETER: 1.187, MAX DIAMETER: 1.190, FINAL DIAMETER: 1.250 EXCEEDED LIMIT. REPAIRED AS PE
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