# Service difficulty reports: N802FD, cancelled Mar 5, 2025 A list on [N802FD, cancelled Mar 5, 2025](https://openairdocs.org/deregistered/N802FD-2025-03-05.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR FDEA200908143019](https://openairdocs.org/sdr/FDEA200908143019.md): Floor Support · corroded · Aug 14, 2009 · N802FD · Airbus A310 · Fuselage Miscellaneous Structure > FWD CABIN FLOOR STRUCTURE - SUPPORT FLOOR AT Y730 BTW FR12A AND 13A FOUND CORRODED. SUPPORT FLOOR REPLACED IAW SRM 51-72-10. - [SDR FDEA200908133009](https://openairdocs.org/sdr/FDEA200908133009.md): Floorbeam · corroded · Aug 13, 2009 · N802FD · Airbus A310324 · Fuselage Main, Floor Beam > AFT CARGO BAY- FLOORBEAM CORROSION AT FR60 AT POSITION Y-140. BEAM REPLACED IAW SRM 51-40-21. - [SDR FDEA200908133008](https://openairdocs.org/sdr/FDEA200908133008.md): Floorbeam · corroded · Aug 13, 2009 · N802FD · Airbus A310324 · Fuselage Main, Floor Beam > AFT CARGO BAY- FLOORBEAM CORROSION AT FR60 AT POSITION Y1470. REPLACED IAW SRM 51-40-21. - [SDR FDEA200908073165](https://openairdocs.org/sdr/FDEA200908073165.md): Skin · delaminated · Aug 7, 2009 · N802FD · Airbus A310324 · Trailing Edge Flaps > LT WING FLAP INBD WITH DEBONDING ON T/E. T/E WAS REPLACED IAW EA 6-5710-131046 AND SRM 51-72-10. - [SDR FDEA200908033100](https://openairdocs.org/sdr/FDEA200908033100.md): Structure · cracked · Aug 3, 2009 · N802FD · Airbus A310324 · Fuselage Main, Structure > COCKPIT 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. - [SDR FDEA200907303099](https://openairdocs.org/sdr/FDEA200907303099.md): Structure · cracked · Jul 30, 2009 · N802FD · Airbus A310324 · Fuselage Main, Structure > COCKPIT 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. - [SDR FDEA200907293007](https://openairdocs.org/sdr/FDEA200907293007.md): Fitting · corroded · Jul 29, 2009 · N802FD · Airbus A310324 · Fuselage Main, Structure > FWD 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. - [SDR FDEA200907292910](https://openairdocs.org/sdr/FDEA200907292910.md): Skin · corroded · Jul 29, 2009 · N802FD · Airbus A310324 · Wing, Plate/Skin > RIGHT 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. - [SDR FDEA200907273108](https://openairdocs.org/sdr/FDEA200907273108.md): Beam · corroded · Jul 27, 2009 · N802FD · Airbus A310324 · Fuselage Main, Structure > AFT 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. - [SDR FDEA200907233102](https://openairdocs.org/sdr/FDEA200907233102.md): Trunnion · damaged · Jul 23, 2009 · N802FD · Airbus A310324 · Wing, Landing Gear Attach Fittings > LT WING - NR 3 EXTERIOR TRUNNION FOUND DAMAGED. TRUNNION NR 3LH WAS REPAIRED IAW CMM 57-53-12. - [SDR FDEA200907233101](https://openairdocs.org/sdr/FDEA200907233101.md): Trunnion · damaged · Jul 23, 2009 · N802FD · Airbus A310 · Wing, Landing Gear Attach Fittings > LT WING - NR 1 EXTERIOR TRUNNION FOUND DAMAGED. THE AFFECTED TRUNNION WAS REPAIRED IAW CMM 57-53-12. - [SDR FDEA200907032470](https://openairdocs.org/sdr/FDEA200907032470.md): Brake · burned · Jul 3, 2009 · N802FD · Airbus A310324 · Landing Gear Brake System > NR 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 A - [SDR 08FDEA00047](https://openairdocs.org/sdr/08FDEA00047.md): Window · cracked · Jan 6, 2008 · N802FD · Airbus A310324 · Flight Compartment Windows > CAPT 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. - [SDR 07FDEA04722](https://openairdocs.org/sdr/07FDEA04722.md): Skin · delaminated · Oct 11, 2007 · N802FD · Airbus A310324 · Trailing Edge Flaps > LT WING, FLAP INBD W/ DBONDS AT THE T/E BETWEEN RIB 2 AND RIB 8 REPLACE TRAILING EDGE IAW FEDEX EA 6-5710-115293. - [SDR 07FDEA04735](https://openairdocs.org/sdr/07FDEA04735.md): Arm · corroded · Oct 10, 2007 · N802FD · Airbus A310324 · Rudder Structure > NR 4 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 6-5510-115292. - [SDR 07FDEA04733](https://openairdocs.org/sdr/07FDEA04733.md): Arm · corroded · Oct 10, 2007 · N802FD · Airbus A310324 · Rudder Structure > NR 3 RUDDER HINGE ARM WITH CORROSION AT LUG BORES. REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA 6-5510-115292. - [SDR 07FDEA04732](https://openairdocs.org/sdr/07FDEA04732.md): Arm · corroded · Oct 10, 2007 · N802FD · Airbus A310324 · Rudder Structure > NR 2 RUDDER HINGE ARM WITH CORROSION IN LUG BORE. REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5510-115292. - [SDR 07FDEA04723](https://openairdocs.org/sdr/07FDEA04723.md): Skin · debonded · Oct 9, 2007 · N802FD · Airbus A310324 · Trailing Edge Flaps > RT WING INBD FLAP T/E W/ VARIOUS DEBONDS TRAILING EDGE WAS REPLACED IAW SRM 51-72-10 AND EA 6-5710-115293. - [SDR 06FDEA1027](https://openairdocs.org/sdr/06FDEA1027.md): Skin · damaged · Mar 13, 2006 · N802FD · Airbus A310324 · Nacelle/Pylon, Main Frame > ACCOMPLISH 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. - [SDR 06FDEA1026](https://openairdocs.org/sdr/06FDEA1026.md): Skin · cracked · Mar 13, 2006 · N802FD · Airbus A310324 · Nacelle/Pylon, Plate/Skin > ACCOMPLISH 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. - [SDR 06FDEA0372](https://openairdocs.org/sdr/06FDEA0372.md): Converter · no test · Jan 24, 2006 · N802FD · Airbus A310 · DC Rectifier/Converter > REMOVED AND REPLACED SDAC IAW AMM 31-55-22-4. OPERATIONAL TEST FOUND SATISFACTORY. A/C OK TO CONTINUE. PREMATURE REMOVAL/INSTALLATION. - [SDR 05FDEA01221](https://openairdocs.org/sdr/05FDEA01221.md): Spoiler · damaged · May 6, 2005 · N802FD · Airbus A310324 · Spoilers > DURING C2 CHECK, FOUND AN EXISTING REPAIR ON LEFT WING NR 1 SPOILER TRAILING EDGE. REPAIRED PER SRM 57-70-00. - [SDR 05FDEA01220](https://openairdocs.org/sdr/05FDEA01220.md): Skin · damaged · May 6, 2005 · N802FD · Airbus A310324 · Trailing Edge Flaps > DURING C2 CHECK, 2 EXISTING FLUSH COMPOSITE REPAIRS WHERE FOUND ON LEFT INBOARD FLAP TRAILING EDGE. REPAIRED IAW EA 6-5750-84119. - [SDR 05FDEA01219](https://openairdocs.org/sdr/05FDEA01219.md): Skin · damaged · May 6, 2005 · N802FD · Airbus A310324 · Elevator, Plate/Skin > DURING C2 CHECK, AN EXISTING REPAIR WAS FOUND ON LEFT ELEVATOR TOP SURFACE OUTBOARD OF RIB 17. NEW REPAIR ACCOMPLISHED PER SRM 55-20-00. - [SDR 05FDEA01218](https://openairdocs.org/sdr/05FDEA01218.md): Flap · damaged · May 6, 2005 · N802FD · Airbus A310324 · Trailing Edge Flaps > DURING C2 CHECK, FOUND AN EXISTING REPAIR ON RIGHT INBOARD FLAP LOWER TRAILING EDGE. NEW REPAIR WAS PERFORMED IAW FEDEX EA 6-5710-84120. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N802FD-2025-03-05/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.