N801FX

Service difficulty reports · 223

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 = 'N801FX' 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.

SDR COEA2011111723801Skin · damagedHEAVY CK COE / MAJOR REPAIR: SKIN UNDER RT CREASE BEAM WEB BETWEEN FR 28D-29 HAS TOOLING DAMAGE. FABRICATED AND INSTALLED DOUBLER AND RT CREASE BEAM BETWEEN FR 28D - 29 IAW SRM.Nov 17, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, Plate/SkinSDR COEA2011111722801Structure · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: 521DT PANEL CUTOUT IS CORRODED.(LENGTH 7.625 X 6.62, WIDTH .394", DEPTH .031"). SUBMITTED TO ATR. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.Nov 17, 2011 · N801FX · Aerosp ATR72212 · Wing, Plate/SkinSDR COEA2011111721801Structure · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: 522CT ACCESS DOOR CUTOUT HAS CORROSION (LENGTH 7.437 X 10.75, WIDTH .394", DEPTH .066"). SUBMITTED TO ATR. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.Nov 17, 2011 · N801FX · Aerosp ATR72212 · Wing, Plate/SkinSDR COEA2011111720801Structure · corrodedHEAVY CK COE / LEVEL 2 CORROSION: 622CT ACCESS DOOR CUTOUT HAS CORROSION (LENGTH 7.43 X 10.75, WIDTH .394", DEPTH .067"). SUBMITTED TO ATR / REPAIR PER SRI AND SRAS FROM ATR.Nov 17, 2011 · N801FX · Aerosp ATR72212 · Wing, Plate/SkinSDR COEA2011111619801Frame · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: FRAME 36 AT STR 15R HAS CORROSION (LENGTH 4.234", WIDTH .343", DEPTH .062"). SUBMITTED TO ATR / REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS AND SRAS FROM ATR.Nov 17, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, FrameSDR COEA2011111618801Failsafe · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: FRAME 39 FAIL SAFE IS CORRODED AND HAS MISSING SURFACE PROTECTION STR 20R-20L (LENGTH 40", WIDTH 1", DEPTH .016"). SUBMITTED TO ATR / REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS & SRAS.Nov 16, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, FrameSDR COEA2011111517801Skin · damagedHEAVY CK COE / MAJOR REPAIR: DENT WITH GOUGE IN SKIN EXTERNAL FUSELAGE 2.7" AFT OF FR 39 AND .9" ABOVE STRINGER 19R. REPAIR PER ATR SRAS AND SRI.Nov 15, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, Plate/SkinSDR COEA2011111516801Rib · damagedHEAVY CK COE / MAJOR REPAIR: RT WING WHERE FUEL FEEDER JET PUMP MOUNTS TO RIB 5 BOTTOM AFT HOLE BETWEEN STIFFENERS 8 & 9 DAMAGED. REPAIR PER ATR72 SRAS AND SRI.Nov 15, 2011 · N801FX · Aerosp ATR72212 · Wing, Rib/BulkheadSDR COEA2011111515801Rib · damagedHEAVY CK COE / MAJOR REPAIR: LT WING FUEL FEEDER JET PUMP MOUNTS TO RIB 5 BOTTOM AFT HOLE BETWEEN STIFFENERS 8 AND 9 DAMAGED. REPAIR PER ATR SRAS AND SRI.Nov 15, 2011 · N801FX · Aerosp ATR72212 · Wing, Rib/BulkheadSDR COEA2011111514801Bulkhead · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: AFT PRESSURE BULKHEAD HAS CORROSION IN MULTIPLE AREAS 29.75 INCHES RIGHT OF BL 0 (SKIN DOUBLER PN S53871408206 LENGTH 1", WIDTH 1", DEPTH .055" / SKIN DOUBLER PN S53871408203 LENGTH 1.22", WIDTH .9", DEPTH .019Nov 15, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, BulkheadSDR COEA2011111113801Floor Support · corrodedHEAVY CK COE / LEVEL 2 CORROSION: LT AFT CARGO DOOR THRESHOLD FLOORBOARD SUPPORT FR 36-38 UPPER SURFACE HAS TOOLING MARKS, CORROSION AND MISSING SURFACE PROTECTION (LENTH 12", WIDTH 2", DEPTH .009"). REMOVE AND REPLACE WITH OEM PART PER ATR72 STRUCTURAL REPANov 11, 2011 · N801FX · Aerosp ATR72212 · Fuselage Miscellaneous StructureSDR COEA2011111112801Floor Support · corrodedHEAVY CK COE / LEVEL 2 CORROSION: LT AFT CARGO DOOR THRESHOLD FLOOR SUPPORT INBOARD INTERCOSTAL HAS BARE METAL AND CORROSION ON LOWER AFT SURFACE (LENGTH 8", WIDTH 2", DEPTH .009"). REMOVED AND REPLACED SUPPORT BEAM WITH OEM PART PER ATR72 STRUCTURAL REPAIR Nov 11, 2011 · N801FX · Aerosp ATR72212 · Fuselage Miscellaneous StructureSDR COEA2011111111801Threshold · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: AFT CARGO DOOR THRESHOLD HAS AREAS OF CORROSION ON THE UPPER AND LOWER SURFACES (LENGTH 27", WIDTH 1", DEPTH .012"). AREA BLENDED; FABRICATED WEB AND INSTALLED PER STRUCTURAL REPAIR MANUAL.Nov 11, 2011 · N801FX · Aerosp ATR72212 · Fuselage Miscellaneous StructureSDR COEA2011111110801Crease Beam · corrodedHEAVY CK COE / LEVEL 2 CORROSION: RT CREASE BEAM WEB FR 35 - 36 IS CORRODED AND HAS TOOLING MARKS ON UPPER SURFACE (LENGTH 4', WIDTH 3.5", DEPTH .009"). REMOVE AND REPLACE WEB PER STRUCTURAL REPAIR MANUAL.Nov 11, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, StructureSDR COEA2011111109801Stringer · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: STRINGER 20R HAS EXFOILIATED CORROSION AT FRAME 28 - 28A (LENGTH 3", WIDTH 2", DEPTH .036"). REMOVED AND REPLACED WITH FABRICATED STRINGER SPLICE IAW STRUCTURAL REPAIR MANUAL.Nov 11, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, Longeron/StringerSDR COEA2011111008801Closeout Panel · corrodedHEAVY CK COE / LEVEL 2 CORROSION: RIGHT CLOSE OUT PANELS BETWEEN CREASE BEAM AND RIGHT OUTBOARD SEAT TRACK CORRODED AND AREA MISSING SURFACE PROTECTION FR35-36. (LENGTH 12", WIDTH 3", AND DEPTH .030"). REMOVED AND REPLACED PLATE WITH OEM PART.Nov 10, 2011 · N801FX · Aerosp ATR72212 · Fuselage Miscellaneous StructureSDR COEA2011111007801Stringer Clip · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: STRINGER FRAME CLIP AT FRAME 22 STR 19R HAS CORROSION. REMOVED, FABRICATED AND REPLACED STRINGER CLIP SRM.Nov 10, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, Attach FittingsSDR COEA2011111006801Stringer · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: STRINGER 18R AFT OF FR 27 HAS EXFOLIATING CORROSION (LENGTH 29.25", WIDTH 2"). REMOVED AND REPLACED STRINGER 18R AFT OF FRAME 27.Nov 10, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, Longeron/StringerSDR COEA2011111005801Closeout Panel · corrodedHEAVY CK COE / LEVEL 2 CORROSION: LEFT CLOSE OUT PANEL BETWEEN CREASE BEAM AND LEFT OUTBOARD SEAT TRACK HAS CORROSION AND MISSING SURFACE PROTECTION FR 35-36 (LENGTH 12", WIDTH 3", DEPTH .013"). REMOVE CORROSION AND REMOVED AND REPLACED PLATE WITH OEM PART INov 10, 2011 · N801FX · Aerosp ATR72212 · Fuselage Miscellaneous StructureSDR COEA2011110904801Skin · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: SKIN AREA AROUND LT BLEED AIR INLET AT FRAME 24 STR 19-20L HAS CORROSION (LENGTH 6", WIDTH 8", DEPTH .021"). REPAIR PER SRAS FROM ATR.Nov 9, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, Plate/SkinSDR COEA2011100903801Skin · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: SKIN AREA AROUND RT BLEED AIR INLET TUBE AT FRAME 24 STR 19-20R HAS CORROSION. (LENGTH 7.32", WIDTH 5.9", DEPTH .0016"). REPAIR PER SRAS FROM ATR.Nov 9, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, Plate/SkinSDR COEA2011110902801Stringer Clip · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: STRINGER/FRAME CLIP AT FRAME 23 STR 21R HAS LEVEL 2 CORROSION. REMOVED CORROSION; FABRICATED AND INSTALLED STRINGER CLIP PER ATR STRUCTURAL REPAIR MANUAL.Nov 9, 2011 · N801FX · Aerosp ATR72212 · Fuselage Main, Attach FittingsSDR COEA2011091401801Skin · corrodedHEAVY CK COE / LEVEL 2 CORROSION: DISCREPANCY: LT ELEVATOR TOP SURFACE AROUND NR 2 STATIC WICK BASE HAS LEVEL 2 CORROSION. FOUND TRAILING EDGE WEDGE LIGHTNING STRIP CHANNEL CORRODED. (LENGTH 1", WIDTH 1", DEPTH ALL THE WAY THROUGH). REMOVED AND REPLACED TRSep 14, 2011 · N801FX · Aerosp ATR72212 · Elevator, Plate/Skin
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