N180FE
Service difficulty reports · 22
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 = 'N180FE' 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 = 'N180FE' 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 FDEA202508251536Skin · damagedPREVIOUS REWORK ON FUSELAGE SKIN, BTW STA 522 AND 544, AT STG 39R FUSELAGE SKIN, BTW STA 522 AND 544, AT STG 39R DAMAGE WAS REPAIRED I.A.W. SRM 53-00-01- 2R FIG 201 REP 29 SHEET 9 REV 92 APR 15, 2025SDR FDEA202508231533Skin · dentedDENT ON INTERNAL SURFACE OF WEDGE, SLAT NO. 11. INTERNAL SURFACE OF WEDGE SLAT NO. 11 WAS REPAIRED IAW B767 SRM 57-43-02-2R AND SRM 51-70-10-2R FIG 202 SHEET 4 REPAIR 4 REV 92 APR 15, 2025.SDR FDEA202508191506Skin · damagedRH WING, INBD MAIN FLAP, UPPER SURFACE, 68" FROM OUTBD EDGE AND 20" FROM TRAILING EDGE, PUCTURE, RH WING, INBD MAIN FLAP UPPER SURFACE, 68" FROM OUTBD EDGE AND 20" FROM TRAILING EDGE WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R, FIGURE 201 SHEET 2 AND SRM 51-SDR FDEA202508181497Skin · damagedPREVIOUS REWORK ON FUSELAGE SKIN, BTW STA 654 66 AND 654 88, STG 39R. FUSELAGE SKIN, BTW STA 654 66 AND 564 88, STG 39R. WAS REPAIRED I.A.W. SRM 53-00-01-2R, REPAIR 1 FIG 201 SHEET 2 REV.92 APR 15 2025.SDR FDEA202508151456Floor Panel · damagedHOLE ON FLOOR PANEL 241KFF ON MAIN DECK. FLOOR PANEL 241KFF ON MAIN DECK, WAS REPAIRED I.A.W. B767 S.R.M. 53-00-50-2R, REP. 4.B., FIG. 201, REV. 92.SDR FDEA202508141452Skin · damagedPUNCTURE ON LEADING EDGE OF OUTBOARD FLAP AT RH WING, AT 72" FROM IMBOARD EDGE. LEADING EDGE OF OUTBOARD FLAP AT RH WING, AT 72" FROM OUTBOARD EDGE WAS REPAIRED I.A.W. B-767, SRM 57-53-01-2R, FIG 201, TABLE I AND SRM 51-70-03-0G, PAR. 5.A, REV. 92, APR-15- SDR FDEA202508141451Skin · delaminatedDELAMINATION ON LEADING EDGE OF OUTBOARD FLAP AT RH WING, AT 135" FROM OUTBOARD EDGE. LEADING EDGE OF OUTBOARD FLAP AT RH WING, AT 135" FROM OUTBOARD EDGE WAS REPAIRED I.A.W. B-767, SRM 57-53-01-2R, FIG 201, TABLE I AND SRM 51-70-03-0G, PAR. 5.A, REV. 92, SDR FDEA202508131447Floor Panel · damagedHOLE ON FLOOR PANEL 241 FFF ON MIAN DECK. FLOOR PANEL 241 FFF ON MIAN DECK, WAS REPAIRED I.A.W. B767 S.R.M. 53-00-50-2R, REP. 4.B. , FIG. 201, REV. 92 APR 15,2025.SDR FDEA202508131446Floor Panel · damagedHOLE ON FLOOR PANEL 241 GFF ON MIAN DECK. FLOOR PANEL 241 GFF ON MIAN DECK, WAS REPAIRED I.A.W. B767 S.R.M. 53-00-50-2R, REP. 4.B. , FIG. 201, REV. 92 APR 15,2025.SDR FDEA202508131445Floor Panel · damagedBROKEN FLOOR PANEL 242 TFA ON MIAN DECK. FLOOR PANEL 242 TFA ON MIAN DECK, WAS REPAIRED I.A.W B767 S.R.M 53-00-50-2R, REP. 4.B. , FIG 201, REV. 92 APR 15, 2025.SDR FDEA202508121416Floor Panel · damagedHOLE ON FLOOR PANEL 252 MFF ON MAIN DECK. HOLE ON FLOOR PANEL 252 MFF ON MAIN DECK WAS REPAIRED I.A.W. B767 S.R.M. 53-00-50-2R REP 4.B. FIG. 201 REV. 92, APR 15, 2025.SDR FDEA202508121414Floor Panel · damagedPUNCTURE ON UPPER SURFACE OF FLOOR PANEL 231 QFF AT SEC. 43 OF MDC. UPPER SURFACE OF FLOOR PANEL 231 QFF, AT SEC. 43 OF MDC, WAS REPAIRED I.A.W. B767 S.R.M. 53-00-50-2R REP 4.B. FIG. 201 REV. 92, APR 15, 2025.SDR FDEA202508121413Floor Panel · crackedCRACK ON UPPER SURFACE OF FLOOR PANEL 232 DFF, SEC. 43, MDC. UPPER SURFACE OF FLOOR PANEL 232 DFF, SEC. 43, MDC, WAS REPAIRED I.A.W. B767 S.R.M. 53- 00-50-2R REP 4.B. FIG. 201 REV. 92, APR 15, 2025.SDR FDEA202508121412Floor Panel · crackedCRACK ON UPPER SURFACE OF FLOOR PANEL 231EFF, SEC. 43, MDC. UPPER SURFACE OF FLOOR PANEL 231EFF, SEC. 43, MDC WAS REPAIRED I.A.W. B767 S.R.M. 53-00- 50-2R, REP. 4.B. FIG. 201, REV. 92 APR 15, 2025.SDR FDEA202508121411Floor Panel · crackedCRACK ON UPPER SURFACE OF FLOOR PANEL 221GFF SECTION 41, MDC. UPPER SURFACE OF FLOOR PANEL 221GFF SECTION 41, MDC, WAS REPAIRED I.A.W. B767 S.R.M. 53-00-50-2R, REP 4B, FIG. 201 REV. 92 APR 15, 2025SDR FDEA202508121415Floor Panel · damagedPUNCTURE ON UPPER SURFACE OF FLOOR PANEL 231 SFF, AT SEC. 43 OF MDC. UPPER SURFACE OF FLOOR PANEL 231 SFF, AT SEC. 43 OF MDC, WAS REPAIRED I.A.W. B767 S.R.M. 53-00-50-2R PAR 4.B. FIG. 201 REV. 92, APR 15, 2025.SDR FDEA202401090156Skin · dentedFOUND DENT ON #11 SLAT AFT EDGE AT APPROX WS 887, MEASURING 14" X 5.5". COMPLIED WITH (EA# H-5740-T 0378114 P 1 REPAIRED LH WING L/E # 11 SLAT TRAINLING EDGE WEDGE AT WS OSS 887 IN REF TO 767 SRM 57-43-02-2R, PG 1-2 DETAIL I & III, FIG.201 SHEETS 1 & 2, AND SDR FDEA202206301631Former · crackedL/E FORMER CRACKED UNDER OTBD END OF #8 SLAT OTBD OF #2 ENGINE. MARKED WITH TAPE REPLACED CRACKED FORMER PER EA H-5720-T0369280 P1.SDR FDEA202206301630Former · crackedL/E FORMER CRACKED UNDER INBD END OF #8 SLAT OTBD OF #2 ENGINE. MARKED WITH TAPE REPLACED CRACKED FORMER PER EA H-5720-T0369280 P1.SDR FDEA202109202350Wedge · wornRH WING, SLAT NO 8 WITH GOUGE ON TRAILING EDGE WEDGE L=30MM, W=18MM, D=1MM. RH WING SLAT #8 TRAILING EDGE WEDGE, LOWER SKIN WAS REPAIRED I.A.W. SRM 57-43-02-2R FIG. 201 (SHEET 1) PAG. 1-2 AND SRM 51-70-10-2R FIG. 202 (SHEET 8) PAG. 15-23,53,71-79,84,162 RSDR FDEA202109172336Wedge · wornLH WING, SLAT NO 5 TRAILING EDGE WEDGE WITH WEAR. LH WING, SLAT NO 5 TRAILING EDGE WEDGE, LOWER SKIN WAS REPAIRED IAW SRM 57-43-02-2R FIG. 201 (SHEET 1) PAG. 1-2 AND SRM 51-70-10-2R FIG.202 (SHEET 8) PAG. 15-23, 53, 71, 79-84, 162 REV. 81 AUG 15/2021SDR FDEA202010242632Escape Rope · looseF/O'S ESCAPE ROPE PANEL IS LOOSE. REINSTALLED ESCAPE ROPE COVER, PER MM 25-61-02-2. A/C OK FOR SERVICE.
Back to N180FE