N802FD, cancelled Mar 5, 2025

Service difficulty reports · 25

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 = 'N802FD' AND deregistration_id = 'N802FD-2025-03-05'
  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 FDEA200908143019Floor Support · corrodedFWD CABIN FLOOR STRUCTURE - SUPPORT FLOOR AT Y730 BTW FR12A AND 13A FOUND CORRODED. SUPPORT FLOOR REPLACED IAW SRM 51-72-10.Aug 14, 2009 · N802FD · Airbus A310 · Fuselage Miscellaneous StructureSDR FDEA200908133009Floorbeam · corrodedAFT CARGO BAY- FLOORBEAM CORROSION AT FR60 AT POSITION Y-140. BEAM REPLACED IAW SRM 51-40-21.Aug 13, 2009 · N802FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA200908133008Floorbeam · corrodedAFT CARGO BAY- FLOORBEAM CORROSION AT FR60 AT POSITION Y1470. REPLACED IAW SRM 51-40-21.Aug 13, 2009 · N802FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA200908073165Skin · delaminatedLT WING FLAP INBD WITH DEBONDING ON T/E. T/E WAS REPLACED IAW EA 6-5710-131046 AND SRM 51-72-10.Aug 7, 2009 · N802FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA200908033100Structure · crackedCOCKPIT FLOOR STRUCTURE - UPPER PANEL AT RT TORSION BOX FOUND CRACKED BETWEEN FR1 AND FR2 AT Y1004. THE TORSION BOX WAS REPAIRED IAW EA 6-5310-131043.Aug 3, 2009 · N802FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200907303099Structure · crackedCOCKPIT FLOOR STRUCTURE - UPPER PANEL AT RT TORSION BOX FOUND CRACKED BETWEEN FR1 AND FR2 AT Y-1004. THE TORSION BOX WAS REPAIRED IAW EA 6-5310-131043.Jul 30, 2009 · N802FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200907293007Fitting · corrodedFWD CARGO COMPT - MANHOLE FITTING - CORROSION FOUND BTW FR38.1&FR38.2. CORROSION REMOVED IAW SRM 51-74-10. MANHOLE WAS REPAIRED IAW A310 SRM 53-14- 12 FIG.203.Jul 29, 2009 · N802FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200907292910Skin · corrodedRIGHT WING - SPOTS OF CORROSION AT UPPER SKIN SURFACE AT REAR SPAR LOCATION, BTW RIBS 4 AND 5. CORROSION WAS BLENDED OUT AND REMAINING THICKNESS FOUND ACCEPTABLE AS PER EA 6-5710-131042.Jul 29, 2009 · N802FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA200907273108Beam · corrodedAFT CARGO COMPT, CORROSION ON BEAM OF CARGO COMPT FLOOR AT FRAME 63 BTW Y805 AND Y1740. THE BEAM WAS REPLACED IAW SRM 51-72-10.Jul 27, 2009 · N802FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200907233102Trunnion · damagedLT WING - NR 3 EXTERIOR TRUNNION FOUND DAMAGED. TRUNNION NR 3LH WAS REPAIRED IAW CMM 57-53-12.Jul 23, 2009 · N802FD · Airbus A310324 · Wing, Landing Gear Attach FittingsSDR FDEA200907233101Trunnion · damagedLT WING - NR 1 EXTERIOR TRUNNION FOUND DAMAGED. THE AFFECTED TRUNNION WAS REPAIRED IAW CMM 57-53-12.Jul 23, 2009 · N802FD · Airbus A310 · Wing, Landing Gear Attach FittingsSDR FDEA200907032470Brake · burnedNR 8 BRAKE TAXING INTO GATE WENT ABOVE 300 DEGS WITH ALL OTHER TEMPS BETWN 50-75 DEGS. ON ARRIVAL, WERE INFORMED BY GRD CREW THE BRAKES WERE VERY HOT, SMOKING AND LATER CAUGHT FIRE. ECAM SHOWED TEMP ABOVE 600 DEGREES. BRAKE FANS WERE ACTIVATED BEFORE GATE AJul 3, 2009 · N802FD · Airbus A310324 · Landing Gear Brake SystemSDR 08FDEA00047Window · crackedCAPT FRONT COCKPIT WINDOW CRACKED REMOVED AND REPLACED WINDOW HEAT PROTECTION NR 1 IAW MM 30-42-11-4. PERFORMED OPS CHECK AS PER MM 30-42-00-5. ALL TEST PASSED.Jan 6, 2008 · N802FD · Airbus A310324 · Flight Compartment WindowsSDR 07FDEA04722Skin · delaminatedLT WING, FLAP INBD W/ DBONDS AT THE T/E BETWEEN RIB 2 AND RIB 8 REPLACE TRAILING EDGE IAW FEDEX EA 6-5710-115293.Oct 11, 2007 · N802FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA04735Arm · corrodedNR 4 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 6-5510-115292.Oct 10, 2007 · N802FD · Airbus A310324 · Rudder StructureSDR 07FDEA04733Arm · corrodedNR 3 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5510-115292.Oct 10, 2007 · N802FD · Airbus A310324 · Rudder StructureSDR 07FDEA04732Arm · corrodedNR 2 RUDDER HINGE ARM WITH CORROSION IN LUG BORE. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-115292.Oct 10, 2007 · N802FD · Airbus A310324 · Rudder StructureSDR 07FDEA04723Skin · debondedRT WING INBD FLAP T/E W/ VARIOUS DEBONDS TRAILING EDGE WAS REPLACED IAW SRM 51-72-10 AND EA 6-5710-115293.Oct 9, 2007 · N802FD · Airbus A310324 · Trailing Edge FlapsSDR 06FDEA1027Skin · damagedACCOMPLISH MAINTENANCE B-CHECK. NR 2 ENGINE CRK FOUND WITH ABOUT 4 INCHES ON AIR INLET INTERIOR SKIN SURFACE BETWEEN NR 5 AND NR 6 HOURS. REPAIRED PER CMM 71-11-05 FIG 603. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.Mar 13, 2006 · N802FD · Airbus A310324 · Nacelle/Pylon, Main FrameSDR 06FDEA1026Skin · crackedACCOMPLISH MAINTENANCE B-CHECK. NR 2 ENG SMALL CRACKS FOUND ON AIR INLET EXTERIOR SKIN SURFACE AT ZONE BETWEEN NR 5 AND NR 6 HOURS (LIP INLET). REPAIRED PER CMM 71-11-05 FIG 603. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.Mar 13, 2006 · N802FD · Airbus A310324 · Nacelle/Pylon, Plate/SkinSDR 06FDEA0372Converter · no testREMOVED AND REPLACED SDAC IAW AMM 31-55-22-4. OPERATIONAL TEST FOUND SATISFACTORY. A/C OK TO CONTINUE. PREMATURE REMOVAL/INSTALLATION.Jan 24, 2006 · N802FD · Airbus A310 · DC Rectifier/ConverterSDR 05FDEA01221Spoiler · damagedDURING C2 CHECK, FOUND AN EXISTING REPAIR ON LEFT WING NR 1 SPOILER TRAILING EDGE. REPAIRED PER SRM 57-70-00.May 6, 2005 · N802FD · Airbus A310324 · SpoilersSDR 05FDEA01220Skin · damagedDURING C2 CHECK, 2 EXISTING FLUSH COMPOSITE REPAIRS WHERE FOUND ON LEFT INBOARD FLAP TRAILING EDGE. REPAIRED IAW EA 6-5750-84119.May 6, 2005 · N802FD · Airbus A310324 · Trailing Edge FlapsSDR 05FDEA01219Skin · damagedDURING C2 CHECK, AN EXISTING REPAIR WAS FOUND ON LEFT ELEVATOR TOP SURFACE OUTBOARD OF RIB 17. NEW REPAIR ACCOMPLISHED PER SRM 55-20-00.May 6, 2005 · N802FD · Airbus A310324 · Elevator, Plate/SkinSDR 05FDEA01218Flap · damagedDURING C2 CHECK, FOUND AN EXISTING REPAIR ON RIGHT INBOARD FLAP LOWER TRAILING EDGE. NEW REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-84120.May 6, 2005 · N802FD · Airbus A310324 · Trailing Edge Flaps
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