N431FE

Service difficulty reports · 69

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 = 'N431FE' 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 06FDEA03873Fitting · unknownPREVIOUS REPAIR FOUND LOCATED RT FS 2105-2208, FS 38(1)-38(2) AND STR 49-55, EXTERNAL DOUBLER AROUND AFT AIR CONDITIONING ACCESS HOLE. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FITTINNov 4, 2006 · N431FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 06FDEA03869Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED RT FS 1236-1260, FS 15A-16 AND STRINGER 39-40 EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFNov 4, 2006 · N431FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 06FDEA03875Skin · damagedPREVIOUS REPAIR FOUND LOCATED LT FS 1019-1061, FS 11-12 AND STR 27-29 EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR COVERED BY RAS/AS/185/97. REPAIR EVANov 4, 2006 · N431FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 06FDEA03844Seat Track · misrepairedPREVIOUS MCD SEAT TRACK REPAIR FOUND LT SIDE, FS 3104-3181, FS 54.3-55/58 AND Y195.9. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM PENov 2, 2006 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA03446Engine · leakingDURING CRUISE, NR 2 ENGINE TRIM LIGHT/ECAM ILLUMINATED NR 2 ENGINE, NOTICED N1 AND N2 INOP, OIL QUANTITY ZERO, OIL PRESSURE IN YELLOW, 14 PSI. ECAM ALERT FOR ENGINE SHUTDOWN, OIL PRESSURE ZERO. FLIGHT TIME ON ONE ENGINE -2 5 MINUTES. HYD LOW PRESS LIGHTS AOct 13, 2005 · N431FE · Airbus A310203 · Turbine Engine Oil SystemSDR 05FDEA00290Skin · damagedELONGATED HOLES IN THE RT LWR WING SKIN AT 1 FASTENER HOLE FOR MANHOLE COVER 650KB.Feb 15, 2005 · N431FE · Airbus A310203 · Wing, Plate/SkinSDR 04FDEA02921Display · intermittentON TAKEOFF ROLL BOTH SGU`S WENT BLANK AT APPROX 85 KNOTS, THEN REAPPEARED AT 105-110 KNOTS THEY WENT BLANK AGAIN EXCEPT FOR SYSTEM DATA NOT AVAILABLE CAUTION ON EACH DISPLAY, SGU'S HAD BEEN RESET ON PRE FLIGHT DUE TO SAME PROBLEM T/O AT 110KNOTS WITH NO ADOct 12, 2004 · N431FE · Airbus A310203 · Central DisplaySDR 04FDEA02435Fuel Tank · crackedAT BLOCK IN, FOUND LT OUTER WING FUEL TANK LEAKING FROM BOTTOM OF WING JUST OUTBD OF RIB NR 20, JACK 05, TRACK 08. FUEL COMING OUT OF DRAIN HOLE ON BOTTOM OF WING JUST FWD OF OVAL ACCESS PANEL. MX FOUND LT NR 8 SLAT TRACK CANISTER TO HAVE APPROX 1 - 2 INCH CAug 6, 2004 · N431FE · Airbus A310203 · Fuel StorageSDR 04FDEA01374Angle · damagedAFT PRESSURE BULKHEAD FR80 OUTER ANGLE LABELED LEFT NR 8 HAS INCOMING ELONGATED HOLES. FABBED REPLACEMENT ANGLE P/N A5398182321000 IAW ACFT DRAWING A53981823 ANGLE TO BE INSTALLED ON N CARD N00035 REF SDR 04-1346.May 20, 2004 · N431FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA01351Pressure Blkhd · corrodedAFT PRESSURE BULKHEAD FR 80 LEFT WEB ASSY HAS AREAS OF EXCESSIVE CORROSION. FABRICATED NEW WEB IAW AIRBUS DRWG A53981860, INSTALLED NEW WEB ASSY IAW A310 SRM 51-40-21 ON ATTACH ANGLE. WORK PERFORMED ON NRC N00269.May 19, 2004 · N431FE · Airbus A310203 · Fuselage Main, BulkheadSDR 04FDEA01349Fitting · damagedSTRINGER 57 O/B END FITTING AT FRAME 80 HAS TWO ELONGATED HOLES. .300 X .280. .225 X .190. FABBED REPLACEMENT PART IAW AIRBUS DWG A53981973 ANGLE (END FITTING). ANGLE INSTALLED ON WORK CARD NON ROUTINE N00035.May 19, 2004 · N431FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA01350Fitting · damagedSTRINGER 57 I/B END FITTING AT FRAME 80 HAS TWO ELONGATED HOLES. .300 X .200. .225 X .190. NO ACTION REQUIRED OLD PART IS BEING REPLACED AT STR 57 FR 80 REF DRAWING R53970100 ITEM 40 PART A5398020620300 REF N00035 FOR INSTALLATION OF END FITTING.May 19, 2004 · N431FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA01347Angle · corrodedAFT PRESSURE BULKHEAD FR 80 INNER ANGLE LABELED LT NR 2 AND SHIM ARE CORRODED [EXFOLIATED]. REPLACED ANGLE AND SHIM ON FR 80 INNER ANGLE LT NR 2 IAW A310 SRM 51-72-10 AND 53-19-17.May 19, 2004 · N431FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA01343Angle · corrodedAFT PRESSURE BULKHEAD FR 80 INNER ANGLE {LABELED NR 3} HAS EXFOLIATED CORROSION. REPLACED ANGLE ON FR 80 INNER ANGLE NR 3 LT IAW A310 SRM 51-72-10 AND 53-19-17.May 19, 2004 · N431FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA01348Web · damagedWEBBING AT FRAME 80 HAS THREE ELONGATED HOLES COMMON TO STRINGER 57. .300 X .280 HOLE WITH ED OF .250 FROM CENTER. ELONGATED HOLE .225 X .190. ELONGATED HOLE .225 X .180.May 19, 2004 · N431FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 04FDEA01346Pressure Blkhd · corrodedREAR PRESSURE BULKHEAD FWD FACE ON THE AFT SIDE OF FR 82 FROM S38L TO S38R HAS AREAS OF CORROSION. LEVEL 2 CORROSION. REF N CARD N00035. COMPLIED WITH EA 6-5310-78353 PT1May 19, 2004 · N431FE · Airbus A310203 · Fuselage Main, BulkheadSDR 04FDEA01287Bulkhead · corrodedAFT PRESSURE BULKHEAD FR 80 RIGHT WEB ASSY HAS AREAS OF CORROSION. INSTALLED NEW WEB ON ATTACH ANGLE IAW SRM 51-40-21. WORK PERFORMED ON NRC N00272.May 18, 2004 · N431FE · Airbus A310203 · Fuselage Main, BulkheadSDR 04FDEA01252Bulkhead · corrodedREAR PRESSURE BULKHEAD FWD FACE ON THE AFT SIDE OF FR 80/82 FROM S38L TO S38R HAS AREAS OF CORROSION. COMPLIED WITH EA 6-5310-78353 PT1.May 13, 2004 · N431FE · Airbus A310203 · Fuselage Main, BulkheadSDR 04FDEA01234Spar · corrodedRIGHT HORIZONTAL UPPER TRAILING EDGE SPAR I/B OF RIB 5 HAS LEVEL 2 CORROSION, APPROX 6 INCHES L X .800 INCH W, NOTE: PREVIOUS STRAP REPAIR INSTALLED I/B OF DAMAGE TO RIB 3. REMOVED PREVIOUS REPAIR, REMOVED CORROSION, MAT'L LOSS GREATER THAN 10 PERCENT, FABRIMay 12, 2004 · N431FE · Airbus A310203 · Horizontal Stabilizer, Spar/Rib
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