N125FE
Service difficulty reports · 25
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 = 'N125FE' 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 = 'N125FE' 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 FDEA202608211212Skin · dentedDURING INSPECTION FOUND EVIDENCE OF STRIKE AT BS 368, STRINGER 5R, DOOR STA 108 3/4" INBD OF STR 5R, REPAIRED SKIN USING COMPLING WITH EA.H-5330-T0388341P1 (PART 1 OF THIS EA PROVIDES INSTRUCTIONS TO ACCOMPLISH SRM 53-00-01-2R, REPAIR 29, WITH CLARIFICATION SDR FDEA202608201196Panel · delaminatedRIGHT WING UPPER L/E PANEL ABOVE PYLON AT ISS 337.60 HAS EROSION ACROSS L/E, WITH NUMEROUS FASTENER HEADS PULLING THROUGH SKIN. ALSO FOUND SEVERAL DOUBLE DRILLED HOLES ON THE RT WING LEADING EDGE RIBS AND CHORDS BETWEEN WS 337 & 356. THERE ARE NO PUBLISHEDSDR FDEA202608061090Skin · dented#4 SLAT T/E WEDGE UPPER SURFACE, 22" FROM THE OUTBD END AND 7" FROM THE AFT EDGE HAS SMALL DENT.MWT, REPAIRED DENT ON # 4 SLAT ON UPPER SURFACE 22" FROM OB EDGE AND 7" FROM AFT EDGE. REF B767 SRM 51-70-10-2R REPAIR 2 FIG 201 SHEET (1 OF 5). SEE JPF, THIS ISDR FDEA202608041083Skin · dentedRIGHT WING NR 8 SLAT TOP SIDE APPROX IN THE MIDDLE HAS A DENT. REPAIRED RT WING NR 8 SLAT TRAILING EDGE WEDGE TOP SKIN SURFACE AT WS.465.65 IAW SRM: 57-43-02-2R AND SRM 51-70-10-2R. THIS IS A MAJOR REPAIR, SEE JPF STEPS FOR OTHER WORK ACCOMPLISHED.SDR FDEA202608011075Skin · dentedRIGHT WING, NR 7 SLAT, UPPER SURFACE T/E WEDGE HAS 2EA DENTS APPROX 28" FROM OUTBD EDGE. REPAIRED DENTS ON RT WING, NR 7 SLAT, UPPER SURFACE T/E WEDGE AT ISS 317 IAW SRM 57-43-02-2R AND SRM 51-70-10-2R. SEE JPF FOR WORK PERFORMED. THIS IS A MAJOR REPAIR.SDR FDEA202509141704Warning Message · illuminatedENROUTE MAIN CARGO DOOR LIGHT ILLUMINATED. ON DESCENT PASSING 22K, LIGHT WENT OUT. RELEASED FOR SERVICE PER MEL : 52-71-01-02 CATEGORY : C. MAIN DECK CARGO DOOR INDICATION SYSTEM - INOP. VERIFY AND RECORD IN AML/EAML THAT MAIN DECK CARGO DOOR IS CLOSEDSDR FDEA202508171491Escape Rope · dislodgedESCAPE ROPE FROM MAIN ENTRY DOOR DISLODGED FROM FRAME AMM 25 61-02-2 ESCAPE ROPE REPOSITIONED IN YOUR PLACE A/C OK FOR SVC.SDR FDEA202507031111Slat System · malfunctionedLE SLAT DISAG ON RAISING FLAPS FROM 1 TO UP. RAN QRH. DECLARED EMERGENCY, UPON ARRIVAL. RECONFIGURED SLAT/FLAP SYS TO NORMAL OPS IAW MM 27-81-00-5. PERFORMED FSEU BITETEST IAW FIM 27-51 FT 809, FAULT HISTORY SHOWED: - LEG 0 : TE FLAPS MAINT MSG 27-5110SDR FDEA202408131120Fitting · crackedMAIN CARGO COMPARTMENT BETWEEN STA 977/999 AND RBL 11/33 FLOOR FITTING BROKEN. MAIN CARGO COMPARTMENT BTWN STA 977/999 AND RBL 11/33 FLOOR FITTING WAS REPLACED IAW E.A H-2550-T0380216SDR FDEA202408101108Skin · burnedRH WING, OUTBOARD AILERON BETWEEN WBL 910 AND WBL 890 WITH TWO LIGHTNING STRIKE. RH WING, OUTBOARD AILERON BTW WBL 910 AND WBL 890 WAS REPAIRED IAW B767 SRM 57-60- 02-2R PAG 1 AND SRM 51-70-14-0G REP 11 PAG 17-18 REV 89 APR 15/2024SDR FDEA202408051086Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 251KFF WITH SEVERAL DENTS. MAIN DECK CARGO, FLOOR PANEL 251KFF WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 89 APR 15/2023.SDR FDEA202408051085Floor Panel · crackedMAIN DECK CARGO COMPARTMENT, FLOOR PANEL 241WFF WITH A PUNCTURE. MAIN DECK CARGO, FLOOR PANEL 241WFF WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PAR 4.B FIG. 201 SHEET 2 REV. 89 APR 15/2024.SDR FDEA202408051084Skin · dentedSLAT 11, EXTERNAL SURFACE, UPPER WEDGE WITH DENT NEXT TO INB FRAME. SLAT 11, EXTERNAL SURFACE, UPPER WEDGE WITH DENT NEXT TO INB FRAME WAS REPAIRED IAW B767 SRM 57-43-02-2R REP 1 PAG 1-2 AND SRM 51-70-10-2R REPAIR 4 PAG 150-151 FIG 201 (SHEET 1) REV 89 APRSDR FDEA202307081186Former · failedNOSE FORMER ANGLE CRACKED AT RIGHT WING OSS 565. VISUALLY INSPECTED FORMER AT FLE OSS 565 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 REV F & A WITH SRM TR 57-111 AS REFERENCE.SDR FDEA202307081185Former · failedNOSE FORMER ANGLE CRACKED AT THE RIGHT WING OSS 499.6. PER EA H-5720-T0367172 REV A VISUALLY INSPECTED FORMER AT FLE OSS 499.603 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 REV F WITH SRM TR 57-111 AS REFERENCE.SDR FDEA202211172811Skin · wornRH WING SLAT #8 INNER SKIN WEDGE AREA TWO PREVIUS REPAIR WITH WEAR. RH WING SLAT #8 T/E WEDGE INNER SKIN, ONE PREVIOUS REPAIR WAS REPLACED AND ONE FILLER WAS REPLACED IAW B767 SRM 57-43-02-2R REP. 1 FIG. 201 PAG. 1-2 AND SRM 51-70-10-2R REP. 4 PAG. 10, 11,SDR FDEA202211172810Skin · wornLEFT WING OUTBOARD SLAT NO 5 TRAILING EDGE WITH WEAR (LOWER SURFACE). LEFT WING OUTBOARD SLAT NO 5 TRAILING EDGE WEDGE WAS REPAIRED IAW SRM 51-70-10-2R REPAIR 4 FIG. 202 SHEET 8 AND SRM 57-43-02-2R REP. 1 FIG. 201 PAG. 1-2 REV. 84 15-AUG-2022SDR FDEA202007011419Slat · chafedRW #8 SLAT TE GOUGED TWO PLACES REPAIRED #8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW B767 SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 51-70-10 REPAIR GENERAL REFINISHED REPAIR IAW B767AMM 51-21-04 AND 51-24-21. SEALED DOUBLERS IAWSDR FDEA2020070811419Wedge · chafedRW #8 SLAT TE GOUGED TWO PLACES REPAIRED #8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW B767 SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 51-70-10 REPAIR GENERAL REFINISHED REPAIR IAW B767AMM 51-21-04 AND 51-24-21. SEALED DOUBLERS IAWSDR FDEA2020070211419Wedge · gougedRT WING NR 8 SLAT TE GOUGED TWO PLACES. REPAIRED NR 8 SLAT TRAILING EDGE WEDGE AT TWO EACH LOCATIONS BY BONDING REPAIR IAW SRM 57-43-02-0I, 57-43-02-2R REPAIR 1 AND 51-70-10 REPAIR GENERAL REFINISHED. REPAIR IAW AMM 51-21-04 AND 51-24-21. SEALED DOUBLERS IASDR FDEA2019111522939Brake · damagedPDIS 125 32-43 4006 12NOV19 CDG OPEN U LOGPAGES:2841209 ON LANDING ROLLOUT APPLIED BRAKES MANUALLY FELT VIBRATION. ON SHUTDOWN BRAKE TEMP LIGHT IS ON BRAKE TEMPS 4435 WITH LIGHT BRAKING SHGN 12NOV19 20:11 CDG U UPON CAPTAIN'S FEEDBACK DECSDR FDEA2018081752047Sensor · fod1.25 HOURS INTO FLIGHT, RECEIVED A MAIN CARGO EICAS. COMPLIED WITH QRH. INDICATOR WENT OUT. DECENDING THRU FL220. PRESSURIZATION NORMAL THOUGHOUT. FOUND DEBRIS ON THE SENSOR TARGET S892. REMOVED THE DEBRIS. INSPECTION CHECKED GOOD. PERFORMED PSEUSDR FDEA201806191544Smoke Barrier · damagedCREW REST SMOKE CURTAIN HAS HOLE IN IN LEFT PLASTIC WINDOW. INSTALLED NEW CURTAIN PER IPC 26-29-01-01.SDR FDEA201607312683Unknown · malfunctionedFLAPS STOPPED BETWEEN 20 AND 25 FLAPS ON INITIAL CONFIGURATION FOR LANDING WITH T/E FLAP DISAGREE. COMPLIED WITH QRH FOR REF FLAP 20 LANDING. VERIFIED OVERLOAD TRIP INDICATORS ON LT & RT WINGS AND VERIFIED FLAP TRANSMITTERS TO BE GOOD FOR SERVICE. PERFORMEDSDR FDEA201509132855Controller · malfunctionedAT FL 360 GOT A CABIN ALTITUDE MASTER WARNING. CABIN WAS SHOWING JUST OVER 10,000 FT WITH A 200 FT PER MIN CLIMB. WE WENT TO AUTO 2 BUT CABIN CONTINUED TO CLIMB, COMPLIED WITH QRH. ON DESCENT WE TRIED MANUAL & WERE ABLE TO CONTROL THE CABIN ALTITUDE. TROUB
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