N807FX
Service difficulty reports · 177
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 = 'N807FX' 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 = 'N807FX' 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 2010F00162Attach Fitting · corrodedPAX CREW DOOR LOWER CLEAT ON 4TH INTERCOSTAL FROM FRONT BETWEEN BEAM 3 AND 4 IS CORRODED BEYOND SRM LIMITS. REMOVED CLEAT IAW SRM 51-25-01 REV 77. REMOVED CORROSION FROM CLEAT IAW SRM 51-21-42 REV 77 AND ATR 72 SRM 51-21-58 REV 77. FOUND CLEAT TO BE OUT OF SDR 2010F00161Intercostal · corrodedPAX DOOR SECOND FROM FRONT INTERCOSTAL ABOVE BEAM 6 IS CORRODED BEYOND SRM LIMITS AT LOWER INBD CORNER. REMOVED CLEAT FOR ACCESS IAW ATR 72 SRM 51-25-01 REV 77. REMOVED CORROSION FROM INTERCOSTAL IAW SRM 51-21-42 REV 77 & SRM 51-21-58 REV 77. MEASURED AFFECSDR COER2010FA0000711Skin · corrodedREMOVED CORROSION IAW ATR 72 SRM 57-14-12 PB400 REV 77. FINAL DIMENSION OF .732" - .738" WAS FOUND TO BE OUT OF LIMITS. INSTALLED NEW FOIL + SPACERS ON 521DT ACCESS PNL FOR REWORKED DOOR CUTOUT AS PER SRI DO/TS-3754/10-13808. NOTE: APPLICATION OF SRI DO/TSDR 2010F00153Stringer · corrodedCORROSION FOUND ON STRINGER 19 LT BETWEEN FR 24- FR 25 BEYOND SRM LIMITS. (LEVEL II)SDR 2010F00152Skin · corrodedREMOVABLE PANEL CUTOUT FOR PANEL 622CT IS CORRODED BEYOND SRM LIMITS. (LEVEL II) REMOVED CORROSION IAW ATR 72 SRM 57-14-12, PB 400 REV 77. FINAL DIMENSIONS AT .713 - .717 WAS FOUND TO BE OUT OF LIMITS. INSTALLED NEW FOIL + SPACERS ON ACCESS PNL 622CT FOR RESDR 2010F00151Skin Panel · corrodedREMOVABLE PANEL CUTOUT FOR PANEL 522CT IS CORRODED BEYOND SRM LIMITS. REMOVED CORROSION IAW SRM 57-14-12, PB 400, REV 77. FINAL DIMENSIONS OF .691"- .696" WAS FOUND TO BE OUT OF LIMITS. INSTALLED NEW FOIL & SPACERS ON PANEL 522CT FOR REWORKED DOOR CUTOUT IAW SDR 2010FA0000711Skin Panel · corrodedREMOVABLE PANEL CUTOUT FOR PANEL 521CT IS CORRODED BEYOND SRM LIMITS. (LEVEL II)SDR 2010F00150Doubler · corrodedFUSELAGE SKIN (FACTORY DOUBLER) UNDER TAIL BUMPER AFT SEAL IS CORRODED. LEVEL II. REMOVED CORROSION IAW ATR 72 SRM 51-21-42 EFF APR 01/01. REMOVED FUSELAGE SKIN DOUBLER ITEM 70 OF SRM 53-61-26 FIG 102 REV 77 PER ATR 72 SRM 51-25-01, 51-25-04 REV 77. FABRICASDR 2010F00149Stringer · corroded(COER) CORROSION FOUND ON STRINGER 20LT BETWEEN FR 24- FR 25 BEYOND SRM LIMITS. (LEVEL II) REMOVED CORROSION REF ATR72 SRM 51-21-58 REV 77 .010IN MATERIAL REMOVAL. ALLOWABLE IS .0027IN REF 51-10-10, SECTION IS OUT OF LIMITS. REPAIRED STRINGER IAW SRM.SDR 2010F00148Crease Beam · corrodedRT INNER CREASE BEAM CORD BETWEEN FR 16-17 HAS CORROSION OUTSIDE SRM LIMITS. (LEVEL II)SDR 2010FA0000708Crease Beam · corroded(COER) RT CREASE BEAM INNER CHORD SPLICE (JOINT) CORROSION BEYOND SRM LIMITS (LEVEL II).SDR 2010FA0000707Crease Beam · corroded(COER) RT CREASE BEAM WEB BETWEEN FRAMES 22 AND 23 CORROSION OUTSIDE SRM LIMITS (LEVEL II).SDR 2010F00147Crease Beam · corrodedRT CREASE BEAM INNER CHORD AT FR 23A, CORRODED BEYOND SRM LIMITS. (LEVEL II)SDR 2010F00146Skin · corrodedLONGITUDINAL BUTT SPLICE AT BL-0 FWD OF FRAME 13 HAS CORROSION OUT OF SRM LIMITS. (LEVEL II) REPLACED LONGITUDINAL BUTT SPLICE IAW ATR72 SRM.SDR 2010F00145Skin Panel · corrodedFUSELAGE SKIN UNDER UPPER ADF ANTENNA AT BL0 BETWEEN FR 28B AND 28C HAS AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-21-42 REV 77. MEASURED AFFECTED AREA MIN REMAINING THICKNESS .027" REF ATR NTM 51-40-00 REV 34. REMAINING UT THICKNESS IS RECORDED AND MASDR COER2010F00153Stringer · damagedBLENDED AREA ON STRINGER 20 IAW SRM 51-21-58, REV 77. MEASURED AFFECTED AREA MIN MATERIAL REMAINING .040" REF NTM 51-40-00, REV 34. FOUND OUT OF LIMITS IAW SRM 53-51-00, FIG 301, ORIG MAT .051 IAW SRM 53-51-26 IT 20 PERCENT MAT LOSS. CUT DAMAGED SECTION OUT SDR 2010F00144Crease Beam · corrodedLT CREASE BEAM INNER CORD AT FR 23 HAS CORROSION. (LEVEL II) PART NOT LISTED IN SRM. SRKM SHOWS PN S5307020820251 FOR RT SIDE ONLY. THERE IS NOT A SYMMETRICAL PART IN THE MANUALS FOR THE LT SIDE, BUT AC HAS ONE INSTALLED. REMOVED CORROSION REFERENCING ATR 72 SDR 2010FA0000703Crease Beam · corrodedPITTING CORROSION ON RT CREASE BEAM WEB FRAME 23-23A. LEVEL II CORROSION. REMOVED 4 EA FASTENERS TO ALLOW FOR CORROSION REMOVAL IAW ATR 72 SRM 51-25-01 AND 51-25-04 REV 77. REMOVED CORROSION FROM CREASE BEAM WEB AS MARKED IAW ATR 72 SRM 51-21-42 REV 77. MEASDR 2010FA0000702Skin Panel · corrodedSKIN FWD OF FRAME 12 AT BL 0 RT SIDE OF BUTT SPLICE HAS CORROSION OUTSIDE OF SRM LIMITS. (LEVEL II) REMOVED CORROSION IAW ATR 72 SRM 51-21-42 REV 77. CUT OUT DAMAGED SECTION OF SKIN REF ATR 72 SRM 53-11-00 FIG 401 REV 77. FABRICATED DOUBLER & FILLER AND INSSDR 2010F00143Seat Track · corrodedLT OTBD SEAT TRACK BETWEEN FRAME 23 AND 29 HAS LEVEL II CORROSION BEYOND SRM LIMITS.SDR 2010F00142Seat Track · corrodedRT OTBD SEAT TRACK BETWEEN FRAMES 23 AND 29 HAS LEVEL II CORROSION BEYOND ALLOWABLE SRM LIMITS. REMOVED CORROSION IAW ATR 72 SRM 51-21-42 REV 77 ON RT OUTBOARD SEAT TRACK BETWEEN FRAMES 23 AND 29. FOUND AREAS TO BE OUT OF LIMITS. REMOVED SEAT TRACK SECTION SDR COER2010F00140Crease Beam · corrodedREMOVED 4 EA FASTENERS TO ALLOW FOR CORROSION REMOVAL IAW SRM 51-25-01 AND 51-25-04 REV 77. REMOVED CORROSION FROM CREASE BEAM WEB AS MARKED IAW SRM 51-21-42 REV 77. MEASURED AFFECTED AREA MIN MATERIAL REMAINING .038" REF ATR NTM 51-40-00 REV 34. MATERIAL LSDR COERFA0000708Crease Beam · corrodedREMOVED 1 EA HI-LOC TO ALLOW FOR CORROSION REMOVAL IAW ATR 72 SRM 51-25-04 REV 77. REMOVED CORROSION FROM SPLICE IAW ATR 72 SRM 51-21-42 REV 77. MEASURED AFFECTED AREA MIN MAT REMAINING THICKNESS .064" REF ATR NTM 51-40-00 REV 34. (NOTE: MAX THICKNESS NOTEDSDR 2010FA0000665Angle · crackedINTERIOR FUSELAGE, RT WING PRESSURE DECK RE-ENFORCEMENT ANGLE AT STRINGER 4R IS CRACKED AFT OF FRAME 27. NO REPAIR ACTION IS REQUIRED OTHER THAN THE APPLICATION OF PR 1436GB. APPLIED BEAD ALONG THE CRACK WITH PR 1436GB PER DO/TS-3855/10-13855 E-MAIL INSTRUCTISDR 2010F00140Angle · crackedINTERIOR FUSELAGE, LT WING PRESSURE DECK RE-ENFORCEMENT ANGLE AT STRINGER 4L IS CRACKED AFT OF FRAME 27. NOTE AC N807FX IS RESERVED REGISTRATION, AC FORMERLY N673AS.SDR 2010F00139Keelbeam · corrodedKEELBEAM LOWER PLATE/ SKIN HAS CORROSION ON BOTTOM BETWEEN SPECIAL STRINGERS. LEVEL II CORROSION, ORIGINAL MATERIAL .063", REMAINING MATERIAL IS 048", 21 PERCENT TOTAL MATERIAL LOSS. FOUND UPPER SUPPORT BRACKET CORRODED BEYOND LIMITS PER ATR 72 SRM 53-51-00 FSDR 2010F00138Skin · dentedDENT BEYOND ALLOWABLE LIMITS. CUT OUT DAMAGED AREA IAW ATR 72 SRM 53-00-00 FIG 403 REV 77. INSTALLED REPAIR PER ATR 72 SRM 53-00-00 FIG 403. APPLIED FILLET SEAL TO DOUBLER AND TOP COATED PER ATR 72 SRM 51-22-02 AND SRM 51-21-27 REV 77.
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