N185FE
Service difficulty reports · 19
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 = 'N185FE' 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 = 'N185FE' 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 FDEA202604030398Skin · delaminatedDELAMINATION IN LEADING EDGE AT 25" OF OUTER END ON INBD MAIN FLAP, LT WING IN LEADING EDGE AT 25" OF OUTER END ON INBOARD MAIN FLAP, LT WING WAS EVALUATED AND REQUIRED REPAIR IAW SRM 57-53-01-1A AND SRM 51-70-17-OG, REPAIR 4.A, REV. 94.SDR FDEA202604020395Floor Panel · crackedFOUR CRACKS ON FLOOR PANEL 241WFF FLOOR PANEL 241WFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG 201 (SHEET 3) REV 94 DEC 15/2025SDR FDEA202604020394Floor Panel · crackedCRACK ON AFT EDGE LOWER SURFACE OF FLOOR ACCESS PANEL 241XFF OF MAIN CARGO COMPARTMENT FLOOR ACCESS PANEL 241XFF OF MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4-B FIG 201 SHEET2 REV. 94 DEC 15/2025SDR FDEA202603300387Skin · delaminatedDELAMINATION ON LEADING EDGE OF OUTBOARD FLAP AT 60" FROM INBD EDGE LEADING EDGE OF OTBD FLAP AT 60" FROM INBOARD EDGE WAS REPAIRED IAW SRM 51-70-17-0G REV 94 DEC 15/2025SDR FDEA202603300386Skin · dentedDENT ON LOWER SURFACE OF OUTBOARD FLAP AT 12" FROM INBOARD EDGE AND 16" FROM LOWER EDGE, LEFT WING LOWER SURFACE OF OUTBOARD FLAP AT 12" FROM INBOARD EDGE AND 16" FROM LOWER EDGE LEFT WING WAS REPAIRED IAW B767 SRM 51-70-06-0G REV 94SDR FDEA202603300385Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231AFF AT MAIN CARGO COMPARTMENT FLOOR PANEL 231AFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 DEC15/2025SDR FDEA202603300384Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231DFF AT MAIN CARGO COMPARTMENT FLOOR PANEL 231DFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4-B FIG 201 SHEET 2 REV.94 DEC15/2025SDR FDEA202603300383Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231EFF AT MAIN CARGO COMPARTMENT FLOOR PANEL 231EFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 .SDR FDEA202603280380Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241HFF AT MAIN CARGO COMPARTMENT. FLOOR PANEL 241HFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET2 REV.SDR FDEA202603280379Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 232KFF AT MAIN CARGO COMPARTMENT. FLOOR PANEL 232KFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50.2R PAR 4-B FIG 201 SHEET2 REV. 94 DEC 15/2025SDR FDEA202603280378Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 231UFF AT MAIN CARGO COMPARTMENT. FLOOR PANEL 231UFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET2 REV 94 DEC 15/2025SDR FDEA202603280377Floor Panel · damagedPUNCTURE ON FLOOR PANEL 231MFF AT MAIN CARGO COMPARTMENT. FLOOR PANEL 231MFF AT MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202509061633Skin · chafedLH WING #5 SLAT HAS GOUGE IN LOWER SKIN AT WING STA 441 NEAR TRAILING EDGE REPAIRED LH WING L/E # 5 SLAT TRAILING EDGE WEDGE AT WS 433.1 IN REF TO 767 SRM 57-43-02- 2R FIG.201 SHEET 2 AND 767 SRM 51-70-10-2R. SEE JPF FOR WORK ACCOMPLISHED.THIS IS A MAJOR RESDR FDEA202406260870Skin · crackedLOWER FUSELAGE SKIN CRACKED APPROX 1" LOCATED 10" FWD OF BS 1654.5 AND OTBD OF S36L. COMPLIED WITH E.A. # H-5310-T0379685 PT 11808. TITLE - FUSELAGE - MAINFRAME - REPAIRS DUE TO CONTAINER STRIKE, FUSELAGE SKIN, ST 1629-1702, S-36L TO S-36R AND STA 1678 FRASDR FDEA202406260869Frame · damagedFOUND DAMAGE TO FRAME BS 1678 OTBD OF S36R. COMPLIED WITH E.A. # H-5310-T0379685 PT 2. TITLE - FUSELAGE - MAINFRAME - REPAIRS DUE TO CONTAINER STRIKE, FUSELAGE SKIN, ST 1629-1702, S-36L TO S-36R AND STA 1678 FRAME.SDR FDEA202404120459Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222CFF . FLOOR PANEL 222CFF WAS REPAIRED IAW SRM 53-00-50-2R PARAG 4B FIG 201 SHEET 2. REV 88.SDR FDEA202404120458Floor Panel · dentedDENTS ALONG UPPER SURFACE OF FLOOR PANEL 222BFF ON MDC. FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PARAG 4B FIG 201 SHEET 2. REV 88.SDR FDEA202204271061Slat · dentedLEFT WING SLAT 4 WITH DENT T/E WEDGE LH WING SLAT #4 WEDGE AT POSITION OSS(648.9-657) UPPER SKIN WAS REPAIRED IAW SRM 57- 43-02-2R PAG. 1-2 FIG. 201 AND SRM 51-70-10-2R REP. 4 PAG. 149, 159-163 FIG. 202 REV. 82 DEC15/2021SDR FDEA202110052477Slat · damagedRH WING #11 SLAT HAS WHAT APPEARS TO BE A BULLET HOLE IN TOP SURFACE REPAIRED R/H WING #11 SLAT REF 767 SRM 57-43-02-2R AND 51-70-10.
Back to N185FE