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 05FDEA03264Stringer · crackedFOUND CRACK INDICATION ON LEFT HAND TANK AT END OF STRINGER 9 (UPPER STRINGER).SDR 05FDEA03263Seat Track · crackedCABIN SEAT TRACK LOWER FLANGE ADJACENT TO STATION 755, X=-8.5 FOUND CRACK. REPAIR CARRIED OUT AS PER SRM 53-70-00.SDR 05FDEA03248Seat Track · crackedMAIN DECK CARGO COMPARTMENT: LEFT HAND SEAT TRACK FOUND CRACKED AT STATION 939, X=28.5. MAIN DECK CARGO COMPARTMENT: LEFT HAND SEAT TRACK AT STATION 939, X=28.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 VOL I FIG 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-SDR 05FDEA03247Seat Track · gougedMAIN DECK CARGO COMPARTMENT: LEFT HAND SEAT TRACK MOUNTING EDGE FOUND GOUGE AT STATION 939, X=47.5. MAIN DECK CARGO COMPARTMENT: LEFT HAND SEAT TRACK AT STATION 939, X=47.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 VOL I FIG 1. REPAIR CLASSIFIED AS MASDR 04FDEA02566Isolator · defectiveMANIFOLD NR 2 FAILURE. INFLIGHT QRH COMPLIED WITH. LANDED CDG. PERFORMED DECAY CHECK IAW MM 36-00-02 WITH ALL OK, PERFORMED FLIGHT FAULT, REVIEW ON THE MFC FOUND (SENSOR ZONE 15 ELE A). DURING TEST FOUND BAD ISOLATION ON LOOP D1-98 REMOVED AND REPLACED MASDR 04FDEA01872Strap · corrodedRIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, OUTBOARD STRAP BORE HOLE AT PIVOT POINT BADLY CORRODED. RIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, OUTBOARD STRAP P/N ARC2518U502, REMOVED AND NEW STRAP REPLACED AS PER DRAWING ARC2512 AND SSDR 04FDEA01770Hinge Bracket · corrodedRIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE HOLE CORRODED. RIGHT HAND AFT (FLAP SIDE) INBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. ORIGIGINAL DIAMETER=1.SDR 04FDEA01776Floor Support · corrodedMAIN CARGO DECK RIGHT HAND STA 1891 FLOOR SUPPORT HAS CORROSION BETWEEN SEAT TRACK REF X=75.25 AND X=102.5. REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA3814 & INSTALLED AS PER SRM 51-35-01 VOL II.SDR 04FDEA01775Floor Support · corrodedMAIN CARGO DECK STA 1890 TO STA 2007 RIGHT HAND LONGITUDINAL FLOOR SUPPORT X=59 HAS CORROSION. CORROSION REMOVED AS PER SRM 51-35-01 VOL II. FABRICATED NEW FLOOR SUPPORT AS PER DRAWING AGA7551 AND FPI CARRIED OUT AS PER DPS 4-707 AND FOUND NO CRACK AND INSTSDR 04FDEA01774Floor Support · corrodedMAIN CARGO DECK RIGHT HAND STA 1851 BETWEEN SEAT TRACK REF X=102.5 AND X=75.25 FLOOR SUPPORT HAS EVIDENCE OF CORROSION. FLOOR SUPPORT REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOOR SUPPORT FABRICATED AS PER DRAWING AGA3814 & INSTALLED AS PER SRM 51-35-01 VOL IISDR 04FDEA01773Floor Support · corrodedMAIN CARGO DECK RT STA 1821 BETWEEN SEAT TRACK REF X=102.5 AND X=75.25 FLOOR SUPPORT HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED AS PER SRM 51-35-01 VOL II.SDR 04FDEA01772Floor Support · corrodedMAIN CARGO DECK RT STA 1741 BETWEEN SEAT TRACK REF X=102.5 AND X=75.25 FLOOR SUPPORT HAS CORROSION. REMOVED AS PER SRM 51-35-01 VOL II. NEW FLOOR PANEL SUPPORT FABRICATED AS PER DRAWING AFA3853 AND INSTALLED AS PER SRM 51-35-01 VOL II.SDR 04FDEA01771Seat Track · corrodedMAIN CARGO DECK RIGHT HAND STA 1741 TO STA 2007 SEAT TRACK REF X=102.5 SEAT TRACK HAS CORROSION. SEAT TRACK REMOVED AS PER SRM 51-21-01 VOL II, FOUND EXCEEDED LIMIT: ORIG. THICKNESS =0.080, MATERIAL REMAINED=0.043", MATERIAL REMOVED =0.037 AS PER SRM 53-70-SDR 04FDEA01768Fitting · crackedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE INTERNAL RIB FITTING (FORWARD OUTBOARD SIDE) FOR HINGE ATTACHMENT CRACKED APPROXIMATELY 2 INCHES IN LENGTH. RIGHT HAND WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27- 50-30-4 AND FLAPS RIGGING AND OPERATIONAL SDR 04FDEA01767Angle · crackedCENTER LANDING GEAR WHEEL WELL LOWER LEFT HAND SIDE FOUND ANGLE PLATE CRACKED AT STATION 1381.SDR 04FDEA01766Angle · crackedCENTER LANDING GEAR WHEEL WELL LOWER RIGHT HAND SIDE FOUND ANGLE PLATE CRACKED AT STATION 1381.SDR 04FDEA01765Floor Support · corrodedCABIN FLOOR PANEL SUPPORT CORRODED AT STA 1741 RBL 63.SDR 04FDEA01764Housing · crackedGLIDE SLOPE HOUSING MOUNTING BRACKET FOUND CRACKED. GLIDESLOPE HOUSING MOUNTING BRACKET REMOVED AND REPLACED AS PER AMM 32-21-34-4 AND GLIDESLOPE FUNCTIONAL TEST CARRIED OUT AS PER AMM 34-32-02-2, FOUND SATIS.SDR 04FDEA01740Hinge Bracket · corrodedLEFT FWD (WING SIDE) I/B FLAP O/B HINGE PIVOT BORE SPOTFACE CORRODED. LEFT FWD (WING SIDE) I/B FLAP O/B HINGE PIVOT BORE SPOTFACE CORROSION. REMOVED AND EXCEED LIMITS AS PER CMM 57-44-07 PAGES 403-404. ORIGINAL THICKNESS = 0.483 INCH, REMAINING THICKNESS = SDR 04FDEA01739Hinge Bracket · corrodedRT FWD (WING SIDE) I/B FLAP O/B HINGE, PIVOT BORE SPOTFACE CORRODED. RT FWD (WING SIDE) I/B FLAP O/B HINGE, PIVOT BORE SPOTFACE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-07 PAGES 403-404. ORIGINAL THICKNESS=0.493 INCH, REMAINING THICKNESS=0.442 SDR 04FDEA01737Vane · corrodedRIGHT WING O/B FLAP VANE, OVAL SHAPE HOLE ON NR 2 TEE FITTING SECOND FROM I/B SIDE FOUND CORRODED. REMOVED AS PER CMM 20-10-02; ORIGINAL OVAL HOLE=0.860 X 0.566; REWORKED OVAL HOLE=0.870 X 0.610; FPI CARRIED OUT IAW CMM 20-30-02 REV 42 FOUND NO CORROSION AND NSDR 04FDEA01738Vane · corrodedLEFT WING O/B FLAP VANE - OVAL SHAPE HOLE ON NR 1 TEE FITTING (FIRST FROM I/B SIDE) FOUND CORRODED. LT WING OUTBOARD FLAP VANE REMOVED AS PER CMM 20-10-02; ORIGINAL HOLE OVAL SIZE=0.860 X 0.560, REWORKED TO SIZE=0.870 X 0.600; FPI CARRIED OUT IAW CMM20-30-02 RSDR 04FDEA01732Hinge Bracket · corrodedLEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, I/B PIVOT BORE HOLE CORROSION REMOVED AND EXCEEDED LIMITS PER CMM 57-52-03, PAGES 442 - 443. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.25SDR 04FDEA01731Hinge Bracket · corrodedLEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER=1.187 INCH, FINAL DIAMETER=1.282 INSDR 04FDEA01730Hinge Bracket · corrodedRT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B ACTUATOR LUG HOLE CORROSION. REMOVED AND EXCEED LIMITS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.SDR 04FDEA01729Hinge Bracket · corrodedRT FWD (WING SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, I/B ACTUATOR LUG HOLE CORROSION. REMOVED AND EXCEED LIMITS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1.22SDR 04FDEA01728Hinge Bracket · corrodedRT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, LOWER MOUNT SPOTFACE CORROSION REMOVED AND EXCEED LIMITS PER CMM 57-44-08, ORIGINAL THICKNESS = 0.500 INCH, MATERIAL REMOVED = 0.012 INCH, REMAININGSDR 04FDEA01727Hinge Bracket · corrodedRT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B LOWER MOUNT BORE HOLE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, O/B LOWER MOUNT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER=0.641 INCH, FINAL DIAMETER SDR 04FDEA01726Hinge Bracket · corrodedRT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SPOTFACE CORRODED. RT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SPOTFACE CORROSION. REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.427 INCH, MATERIAL REMOVED = 0.006 INSDR 04FDEA01725Hinge Bracket · corrodedRT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORRODED. RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL THICKNESS=0.652 INCH, REMAINING THICKNESS=0.5SDR 04FDEA01724Hinge Bracket · corrodedRT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORRODED. RT AFT (FLAP SIDE) I/B FLAP O/B HINGE, O/B PIVOT BORE HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIA 1.187 INCH, FINAL DIA 1.282 INCH. REPAIR CASDR 04FDEA01716Bracket · corrodedRIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORRODED. RIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09, PAGES 402 - 407. ORIGINAL THICKNESS = 0.452 INCH, MATERIAL REMOVED = 0.00SDR 04FDEA01713Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. LT FWD (WING SIDE) O/B FLAP I/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIASDR 04FDEA01712Bracket · corrodedLT FWD (WING SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIASDR 04FDEA01711Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE - LOWER MOUNT SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.495 INCH, MATERIAL REMOVED = 0SDR 04FDEA01710Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SURFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, BARREL NUT HOLE SURFACE CORROSION REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL THICKNESS = 0.405 INCH, MATERIAL REMOVED = 0.003 INSDR 04FDEA01709Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP I/B HINGE, PIVOT BORE HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP I/B HINGE, PIVOT BORE HOLE CORROSION REMOVED AS PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 2.252 INCH, FINAL DIAMETER = 2.323 INCH. COMPLIED WITH FESDR 04FDEA01733Seat Track · corrodedMAIN CARGO DECK RT STA 1741 TO STA 2007 SEAT TRACK REF X=102.5 SEAT TRACK HAS CORROSION. SEAT TRACK REMOVED AS PER SRM 51-21-01 VOL II, FOUND EXCEEDED LIMIT: ORIG. THICKNESS =0.080, MATERIAL REMAINED=0.043, MATERIAL REMOVED =0.037 AS PER SRM 53-70-00 FIG 3 PSDR 04FDEA01715Hinge · corrodedRIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED.SDR 04FDEA01714Hinge · corrodedRIGHT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORRODED.SDR 04FDEA01700Hinge · corrodedLEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE - I/B STRAP BORE HOLE AT PIVOT POINT BADLY CORRODED. LEFT AFT (FLAP SIDE) I/B FLAP O/B HINGE - I/B STRAP P/N ARC2517U501 REMOVED AND NEW STRAP REPLACED AS PER DRAWING ARC2512 AND SRM 51-33-01 VOL 2.SDR 04FDEA01699Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - O/B ACTUATOR LUG HOLE CORROSION REMOVED AND EXCEED LIMIT PER CMM 57-44-08, PAGES 402 - 407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = 1SDR 04FDEA01698Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - I/B ACTUATOR LUG HOLE CORROSION REMOVED AND EXCEED LIMITS AS PER CMM 57-44-09 PAGES 402-407. ORIGINAL DIAMETER = 1.187 INCH, FINAL DIAMETER = SDR 04FDEA01697Hinge Bracket · corrodedLEFT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORRODED. LEFT FWD (WING SIDE) O/B FLAP O/B HINGE - BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-09, PAGES 402-407. ORIGINAL THICKNESS = 0.427 INCH, MATERIAL REMOVED = 0.002 INSDR 04FDEA01691Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.502, REMAINING THICKNESS = 0.500, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT SDR 04FDEA01690Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.063, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRACKESDR 04FDEA01689Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.500, REMAINING = THICKNESS = 0.472, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGSDR 04FDEA01688Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE I/B PIVOT BORE HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.148. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND RIGHT OUTBOARD FLAP - INBOARD HINGE BRASDR 04FDEA01687Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL THICKNESS = 0.399, REMAINING = THICKNESS = 0.397, MATERIAL REMOVED = 0.002. COMPLIED WITH FEDEX EA 1-5750-76738, LEFT AND SDR 04FDEA01686Hinge · corrodedLEFT AFT (FLAP SIDE) O/B FLAP I/B HINGE O/B ACTUATOR BORE HOLE CORRODED.
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