N673FE

Service difficulty reports · 360

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 = 'N673FE' 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 FDEA202609181362Gearbox · failedFLAPS STUCK LESS THAN 20 DEGRESS. DURING DETENTION PRIOR TO LANDING, DECLARED EMERGENCY, UNEVENTFUL LANDING RUNWAY 28 LEFT AT KBOI. AMM 27-51-19-04, AMM 27-55-12-04, AMM 27-54-00-05, AMM 27-54-13-04, & AMM 27-50-00-03. FOUND COUPLING SHEARED FROM RT FLAP SISep 18, 2026 · N673FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA202609041263Jackscrew · leakingON APPROACH, PUT THE SLATS OUT, GOT SLATS 1 & 2 FAULTS. PER ECAM, CYCLED HANDLE. DID NOT EXTEND. FOLLOWED QRH. DECLARED EMERGENCY. UNEVENTFUL NO SLAT LANDING. PRI.0 DUE TO CAUSING DELAY, SFCC 1 SLAT FAIL INDS SHOW JAM. FLAP FAIL, INDS SHOW SUPPLY P. SW. SFCSep 4, 2026 · N673FE · Airbus A300F4605R · Leading Edge Slat ActuatorSDR FDEA202605150599Bottle · low pressureMAIN CABIN DOOR 2R EMERGENCY OPERATION CYLINDER REQUIRES SERVICING. SERVICED R1 FORWARD DOOR EMERGENCY OPERATION CYLINDER IAW AMM 52-10-14-03-02. ACFT OK TO CONTINUE.May 15, 2026 · N673FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202602190244Safety Wire · wrong partWHILE WORKING FEA 6-2560-F0386375 A PT1 FOUND INCORRECT SAFETY WIRE ON EJECTOR BAG RELEASE CABLE. AMM: 25-61-20-05-01 REPLACED EJECTOR BAG RELEASE CABLE SAFETY WIRE WITH CORRECT WIRE MS20995CY16 CAD PLATED COPPER WIRE. REF. AMM 25-61-20-05-01. OK FOR SERVFeb 19, 2026 · N673FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202504090584Door · out of alignmentWHILE ATTEMPTING TO DISARM L1, RAMP PERSONNEL WAS ATTEMPTING TO OPEN L1 DOOR BEFORE THE SLIDE WAS ABLE TO BE DISARMED. MECHANICAL DISARM FEATURE WAS UNABLE TO MOVE TO DISARM POSITION, SLIDE FELL OUT OF DOOR WITH NO (INTENDED) DEPLOYMENT. RELEASED FOR SERVApr 9, 2025 · N673FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202503180441Fitting · damagedCOMPLY WITH EO 6-5230-E0378588 B P5 FOR MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS REPLACEMENT. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCC) ACTUATOR BEARING FIMar 18, 2025 · N673FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202503180440Shear Tie · crackedCOMPLY WITH EO 6-5310-E0330747 D P26 FOR FUSELAGE FRAME BASE FITTING AT FR46 BETWEEN STGR36RH AND STGR38RH CRACK REPAIR COMPLIED WITH EO 6-5310-E0330747 D P26. TITLE: FUSELAGE - MAIN FRAME - INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 AND 46, Mar 18, 2025 · N673FE · Airbus A300F4605R · Fuselage Internal Mounting StructureSDR FDEA202503180439Shear Tie · crackedCOMPLY WITH EO 6-5310-E0330747 D P24 FOR FUSELAGE FRAME BASE FITTING AT FR45 BETWEEN STGR36RH AND STGR38RH CRACK REPAIR COMPLIED WITH EO 6-5310-E0330747 D P24. TITLE: FUSELAGE - MAIN FRAME - INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 AND 46, Mar 18, 2025 · N673FE · Airbus A300F4605R · Fuselage Internal Mounting StructureSDR FDEA202503180438Shear Tie · crackedCOMPLY WITH EO 6-5310-E0330747 D P23 FOR FUSELAGE FRAME BASE FITTING AT FR45 BETWEEN STGR36LH AND STGR38LH CRACK REPAIR COMPLIED WITH EO 6-5310-E0330747 D P23. TITLE: FUSELAGE - MAIN FRAME - INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 AND 46,Mar 18, 2025 · N673FE · Airbus A300F4605R · Fuselage Internal Mounting StructureSDR FDEA202503180437Shear Tie · crackedCOMPLY WITH EO 6-5310-E0330747 D P22 FOR FUSELAGE FRAME BASE FITTING AT FR44 BETWEEN STGR35RH AND STGR37RH CRACK REPAIR COMPLIED WITH EO 6-5310-E0330747 D P22. TITLE: FUSELAGE - MAIN FRAME - INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 AND 46, Mar 18, 2025 · N673FE · Airbus A300F4605R · Fuselage Internal Mounting StructureSDR FDEA202503180436Shear Tie · crackedCOMPLY WITH EO 6-5310-E0330747 D P21 FOR FUSELAGE FRAME BASE FITTING AT FR44 BETWEEN STGR35LH AND STGR37LH CRACK REPAIR COMPLIED WITH EO 6-5310-E0330747 D P21. TITLE: FUSELAGE - MAIN FRAME - INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 AND 46,Mar 18, 2025 · N673FE · Airbus A300F4605R · Fuselage Internal Mounting StructureSDR FDEA202503110354None · noneEXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR30 BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR30 BETWEEN -Y450 AND -Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5321-54628 A, UPGRADED TO Mar 11, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503110353None · noneEXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR29 BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR29 BETWEEN -Y450 AND -Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5321-54628 A, UPGRADED TO Mar 11, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503110352None · noneEXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR28 BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR28 BETWEEN -Y450 AND -Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5321-54628 A, UPGRADED TO Mar 11, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503100351None · noneEXISTING REPAIR ON FWD CARGO DOOR FWD CUTOUT FRAME 20A BETWEEN STGR33RH AND STGR45RH REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FWD CARGO DOOR FWD CUTOUT FRAME 20A BETWEEN STGR33RH AND STGR45RH WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6Mar 10, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503090349Hinge Arm · delaminatedLH WING #5 SPOILER CENTER O/B HINGE ARM LWR SURFACE, CENTER O/B HINGE ARM INSIDE & OUTSIDE SURFACES FOUND DELAMINATION. SIZE: (1)25MM*25MM, DEPTH: 2.10MM (2)15MM*15MM, DEPTH: 0.83MM (3)20MM*15MM, DEPTH: 1.57MM COMPLIED WITH EA: 6-5750-T0369910 A P2. TITLE:Mar 9, 2025 · N673FE · Airbus A300F4605R · SpoilersSDR FDEA202503090348Hinge Arm · delaminatedRH WING #4 SPOILER CENTER I/B HINGE ARM INSIDE SURFACE FOUND DELAMINATION. SIZE: 20MM*15MM, DEPTH: 0.71MM COMPLIED WITH EA: 6-5750-T0382425 P1. TITLE: WING - FLIGHT SURFACES - RH #4 SPOILER CENTER HINGE ARM SURFACE DELAMINATION - SB A300-57-6082 R03 - MOD Mar 9, 2025 · N673FE · Airbus A300F4605R · SpoilersSDR FDEA202503090347Seat Track · noneEXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y1456 BETWEEN FR30 AND FR32 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y1456 BETWEEN FR30 AND FR32 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIG2Mar 9, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503090346Seat Track · noneEXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y450 BETWEEN FR74 AND FR76 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y450 BETWEEN FR74 AND FR76 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIMar 9, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503090345Seat Track · noneEXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y1456 BETWEEN FR55 AND FR57.2 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y1456 BETWEEN FR55 AND FR57.2 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201 Mar 9, 2025 · N673FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202503090344Seat Track · noneEXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y450 BETWEEN FR55 AND FR57.2 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y450 BETWEEN FR55 AND FR57.2 WAS EVALUATED AND FOUND IN COMFORMITY WITH A300-600F SRM 53-10-16-201 FIMar 9, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503090343Seat Track · noneEXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y1456 BETWEEN FR26 AND FR31 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y1456 BETWEEN FR26 AND FR31 WAS EVALUATED AND FOUND IN COMFORMITY WITH A300-600F SRM 53-10-16-201 FIMar 9, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503090342Seat Track · noneEXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y2462 BETWEEN FR18 AND FR22 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y2462 BETWEEN FR18 AND FR22 WAS EVALUATED AND FOUND IN COMFORMITY WITH A300-600F SRM 53-10-16-201 FIG Mar 9, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503090341Seat Track · unknownEXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y852.4 BETWEEN FR73 AND FR80/82 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y852.4 BETWEEN FR73 AND FR80/82 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53279238 (ISSUMar 9, 2025 · N673FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202503070336Seat Track · noneEXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y1221.2 BETWEEN FR74 AND FR77 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y1221.2 BETWEEN FR74 AND FR77 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM 53-10-16-201Mar 7, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503040325Seat Track · misrepairedEXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y450 BETWEEN FR64 AND FR72 REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y450 BETWEEN FR64 AND FR72 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIMar 4, 2025 · N673FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202503040324Seat Track · misrepairedEXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y450 BETWEEN FR75 AND FR79 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y450 BETWEEN FR75 AND FR79 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIMar 4, 2025 · N673FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202503040323Seat Track · misrepairedEXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y1456 BETWEEN FR55 AND FR57.2 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y1456 BETWEEN FR55 AND FR57.2 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-10-16Mar 4, 2025 · N673FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202503040322Crossbeam · misrepairedEXISTING REPAIR ON FWD CARGO DOOR FWD CUTOUT FRAME 20A BETWEEN STGR33RH AND STGR45RH REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FWD CARGO DOOR FWD CUTOUT FRAME 20A BETWEEN STGR33RH AND STGR45RH WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6Mar 4, 2025 · N673FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202503040321Seat Track · misrepairedEXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR64 BETWEEN Y953 AND Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR64 BETWEEN Y953 AND Y1456 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-10-15-201 FIGMar 4, 2025 · N673FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202503040319Seat Track · misrepairedEXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR64 BETWEEN -Y953 AND -Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR64 BETWEEN -Y953 AND -Y1456 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-10-15-201Mar 4, 2025 · N673FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202503040318Floor Support · corrodedEXISTING REPAIR ON MAIN DECK FLOOR SUPPORT AT Y730 BETWEEN FR11 AND FR13A REQUIRES EVALUATION FOR CONFORMITY EXISITING REPAIR ON MAIN DECK FLOOR SUPPORT AT Y730 BETWEEN FR11 AND FR13A WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53612214 (ISSUE.V00) ANMar 4, 2025 · N673FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202503040317Seat Track · misrepairedEXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y953 BETWEEN FR30 AND FR32 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y953 BETWEEN FR30 AND FR32 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIGMar 4, 2025 · N673FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202503040316Repair · misrepairedEXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y450 BETWEEN FR29 AND FR34 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y450 BETWEEN FR29 AND FR34 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIGMar 4, 2025 · N673FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202503040315Seat Track · misrepairedEXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y0 BETWEEN FR26 AND FR31 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y0 BETWEEN FR26 AND FR31 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM 53-10-16-201 FIG201Mar 4, 2025 · N673FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202503040314Panel · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "F" HOLE FOUND CRACK SIGNAL COMPLIED WITH EA 6-5710-T0382800 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK HOLE F AT FR47 RHS DURING SB57-6068 EMBMar 4, 2025 · N673FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202502270303Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR66, BETWEEN -Y953 AND -Y1456 REPAIRED THE CRACKED CROSSBEAM AT MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE FR66 BETWEEN -Y953 AND -Y1456 PER A300-600F SRM53-10-15-201 FIG.211. THIS IS Feb 27, 2025 · N673FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202502270302Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR67, BETWEEN Y1456 AND Y1959 REPAIRED THE CRACKED CROSSBEAM AT MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE FR67 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 FIG.211. THIS IS CAFeb 27, 2025 · N673FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202502260296Floorbeam · noneEXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-15-201 Feb 26, 2025 · N673FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202502260295Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED AT FR32, BETWEEN Y1456 AND Y1959 COMPLIED WITH EA:6-5310-T0382537 P1. TITLE: FUSELAGE - MAINFRAME - CRACK ON FR32 CROSSBEAM, BETWEEN Y1456 AND Y1959. REPAIRED THE CRACKED CROSSBEAM AT MAIN DECFeb 26, 2025 · N673FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202502260294Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR30, BETWEEN Y1456 AND Y1959. COMPLIED WITH EA:6-5310-T0382538 P1. TITLE: FUSELAGE - MAINFRAME - CRACK ON FR30 CROSSBEAM, BETWEEN Y1456 AND Y1959. REPAIRED THE CRACKED CROSSBEAM AT MAIN DFeb 26, 2025 · N673FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202502050176Sensor · faultedENROUTE TO KSHV IN CLIMB AT APPROX FL 240 THE ECAM SHOWED R FUEL LO LEVEL. WE DID ALSO GET THE RED LIGHT ON THE OVERHEAD. RETURNED TO MEM AND THE INDICATION WENT AWAY AT 5000 FEET. THE INDICATION DID NOT RETURN. EMERGENCY DECLARED. AMM 28-42-00-05-02Feb 5, 2025 · N673FE · Airbus A300F4605R · Fuel Indicating SystemSDR FDEA202409111309Door · unsecureDURING POST FLIGHT INSPECTION FOUND RIGHT AFT NOSE GEAR DOOR ASSY. LOOSE AND NOT SECURE. FOUND HARDWARE MISSING (ITEMS 190) FROM ITEM #10 THAT ATTACHES DOOR TO NOSE LANDING GEAR. INSTALLED NEW HARDWARE, REF IPC 32-22-01-02 ITEM 190 FROM ITEM 10 THAT ATSep 11, 2024 · N673FE · Airbus A300F4605R · Landing Gear DoorsSDR FDEA202404170526Adapter · damagedRAMP REPORTED 8R SEATTRACK EAR BROKEN AT KINK TRANSATION AREA STA 1571 POSITION 8R . LOBE DAMAGE POS 8R FR60, OK PER SR30-53-003. IPC: 25-57-01-03 TRACK EAR BROKE AT STA. 1571 /8R. OIL REFERENCE: SR30-53-003. REMOVED BROKEN SEAT TRACK ADAPTER AT FRApr 17, 2024 · N673FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202209122307Skin · crackedCRACKS WERE FOUND ON INNER SKIN AND CONNECTING CLIP OF MDCD AT PT1, BETWEEN C23A AND C24 PERFORMED THE REPAIR ON MDC DOOR AS PER FEDEX EA # : 6-5230-T0370454 P1 , TITLE: DOORS - CARGO DOOR / HYD SYS - MAIN DECK CARGO DOOR , AFT BEARING FITTING , INNER SKSep 12, 2022 · N673FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202209122305Skin · crackedCRACKS WERE FOUND ON INNER SKIN AND CONNECTING CLIP OF MDCD AT PT1, BETWEEN C23A AND C24 PERFORMED THE REPAIR ON MDC DOOR AS PER FEDEX EA # : 6-5230-T0370454 P1 , TITLE: DOORS - CARGO DOOR / HYD SYS - MAIN DECK CARGO DOOR , AFT BEARING FITTING , INNER SKSep 12, 2022 · N673FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202209122308Skin · crackedCRACKS WERE FOUND ON INNER SKIN AND CONNECTING CLIP OF MDCD AT PT1, BETWEEN C23A AND C24 PERFORMED THE REPAIR ON MDC DOOR AS PER FEDEX EA # : 6-5230-T0370454 P1 , TITLE: DOORS - CARGO DOOR / HYD SYS - MAIN DECK CARGO DOOR , AFT BEARING FITTING , INNER SKINSep 12, 2022 · N673FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202209072225Skin · crackedCRACKS WERE FOUND ON INNER SKIN AND CONNECTING CLIP OF MDCD AT PT1, BETWEEN C23A AND C24 PERFORMED THE REPAIR ON MDC DOOR AS PER FEDEX EA # : 6-5230-T0370454 P1 , TITLE: DOORS - CARGO DOOR / HYD SYS - MAIN DECK CARGO DOOR , AFT BEARING FITTING , INNER SKINSep 7, 2022 · N673FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202208202008Skin · delaminatedRH WING #5 SPOILER TOP SKIN FOUND DELAMINATION(AREA:35MM*32MM,DEPTH:1.8MM) AND CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION(AREA:25MM*40MM,DEPTH:0.85MM) PERFORMED THE REPAIR ON RH WING #5 SPOILER AS PER A300-600F SRM57-72-11-201 PARA12 AND FEDEX EA 6-5Aug 20, 2022 · N673FE · Airbus A300F4605R · SpoilersSDR FDEA202208192005Frame · crackedRH FWD CREW DOOR - FRAME SEGMENT CRACKED AT FR14C PERFORMED THE REPAIR ON RH FWD CREW DOOR - FRAME SEGMENT AT FR14C AS PER FEDEX EA 6-5210-T0370105 P1 TITLE:DOORS-PASSENGER/CREW-LOCAL FABRICATION AND REPLACEMENT OF FRAME SEGMENT ON R1 DOOR-RSC TRACKING.THIAug 19, 2022 · N673FE · Airbus A300F4605R · Doors
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