Airbus A300 F4-605R

Service difficulty reports · 9,199

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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 aircraft_model_key = 'A300F4605R'
  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 FDEA202611011712Smoke Detector · failedMDIS 657 26-12 9422 01NOV26 19:41 MEM FACT AVIONICS SMOKE DETECTION ALERT DURING MX PRE-FLT FACT 01NOV26 20:34 MEM AMM 26-15-12-04 WITH REF ABOVE. REMOVED AND REPLACED AVIONICS COMPARTMENT SMOKE DETECTOR UNIT 13WA. OPS CHECK GOOD. A/C OK FONov 1, 2026 · N657FE · Airbus A300F4605R · Smoke DetectionSDR FDEA202610231680Switch · damagedSELECTED LANDING GEAR HANDLE DOWN AT 170KTS, 2300FT, DESCENDING ON THE 16R GLIDE SLOPE AT SLC, & NOTHING HAPPENED. NO AIR NOISE, NO LANDING GEAR DOOR INDICATION, RECEIVED 3 RED UNLK LIGHTS ON THE LANDING GEAR INDICATOR. PERFORMED A DISCONTINUED APPROACH, WIOct 23, 2026 · N672FE · Airbus A300F4605R · Landing Gear SelectorSDR FDEA202610151590Hydraulic System · low quantityDURING TAKEOFF ROLL AT 65 KNOTS, MASTER CAUTION WITH BLUE HYD SYS RSVR LO. REJECTED TAKEOFF AT 75 KIAS. COMPLIED WITH ECAM AND QRH. AMM 12-12-29-00, BLUE HYD QTY LOW. SERVICED BLUE HYD SYS IAW AMM 12-12-29-00.Oct 15, 2026 · N665FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA202610041482Structure · crackedMAIN DECK CARGO DOOR UPPER EDGE AT PT1 BTWN FR 22 & 25, FOUND CRACK SIGNAL AT 2 EA FASTENER HOLES. COMPLIED WITH EA 6-5230-T0388992 P1 REPAIR MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 2EA CRACK HOLES. EA TITLE: DOORS - CARGO DOOR/HYD SYS -Oct 4, 2026 · N670FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202609281443Fitting · damagedCOMPLY WITH EO 6-5230-E0378588 C P5. DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOSep 28, 2026 · N670FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202609221405Stiffener · corrodedTOILET SERVICE ACCESS PANEL FWD LOWER CUTOUT CORRODED. REPLACED THE CORRODED STIFFENER AT TOILET SERVICE ACCESS PANEL FWD LOWER CUTOUT PER A300-600F SRM51-40-21 & DWG.A53612375(ISSUE.K). THIS IS CAT A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.Sep 22, 2026 · N670FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202609221403Rib · crackedRIGHT WING CENTER FLAP RIB UPR FLANGE FOUND CRACK AT RIB15 BETWEEN STRINGERS 2.6, 2.7, & 2.8. CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100 I.A.W EA T6-5750-T0378801 P1, SEQ 1119, LT CENTER FLAP WITH OVERSIZED HOLE ON UPPER SKIN AT RIB 11. REPAIRED IAW GMM6-2Sep 22, 2026 · N670FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202609221402Rib · crackedLEFT WING CENTER FLAP RIB UPPER FLANGE FOUND CRACKED AT RIB 26 BETWEEN STGR2.6 AND STGR2.7. COMPLIED WITH EA 6-5750-T0388894 P1 REPAIR LT WING CENTER FLAP UPR FLANGE CRACK. THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.Sep 22, 2026 · N670FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202609211390Stringer Splice · crackedMDCC FR 47, S-18L STRINGER SPLICE CRACKED. REPLACED THE STRINGER SPLICE AT MDCC FR47, S-18L PER A300-600F SRM51-40-21 & DWG.A53833157(ISSUE:F00). THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2026 · N670FE · Airbus A300F4605R · Fuselage Main, Longeron/StringerSDR 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 FDEA202609171360Gfi · failedAUTO FUEL FEED FAULTED. USED QRH PROCEDURES TO RESET SYS. NR 2 PUMP FAULTED & WOULD NOT RESET. NR 1 INNER TANK PUMP DEFERRED, LEAVING NO OPERATING PUMP IN RT TANK & APPROX 25,000 POUNDS IN RT TANK UNUSABLE. DECLARED EMERGENCY & TRIED TO ESTABLISH A WAY TO BURNSep 17, 2026 · N677FE · Airbus A300F4605R · Fuel Boost PumpSDR FDEA202609151338Pitot Tube · inoperativeDURING TAKEOFF CA AIRSPEED INDICATOR INDICATED 0. ABORTED TAKEOFF AND TAXIED BACK TO RAMP. REMOVED AND REPLACED CAPT'S PITOT TUBE EF AMM 34-11-15-04. LEAK CHECK GOOD. ACFT OK FOR CONTINUED SERVICE.Sep 15, 2026 · N667FE · Airbus A300F4605R · Pitot/Static SystemSDR FDEA202609081286Bottle · low pressureLEFT FWD CREW ENTRY DOOR DAMPER AND EMERGENCY OPERATION CYLINDER REQUIRES SERVICING. SERVICED LEFT FWD DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AS REQUIRES.Sep 8, 2026 · N672FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202609061267Frame · crackedINSPECTION OF FRAME 40 LT, LOWER WING JUNCTION, FOUND A CRACK SIGNAL AT FASTENER HOLE NR 1. COMPLIED WITH EA: 6-5710-T0388595 P1. REPAIRED FRAME 40 LT LOWER JUNCTION, CRACKED FASTENER HOLE NR 1. THIS IS CATEGORY B REPAIR. FOLLOW UP INSPECTION IAW EA 6-5710-Sep 6, 2026 · N661FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202609061266Seat Track · corrodedMAIN DECK SEAT TRACK AT Y1959 BETWEEN FR53 AND FR54 CORRODED. REPAIRED THE CORRODED MAIN DECK SEAT TRACK AT Y1959 BETWEEN FR53 AND FR54 PER SRM53-10-16-201 FIG.201 & EA: 6-5310-T0388627 P1. CATEGORY -A- MAJOR REPAIR IAW GMM6-2-100.Sep 6, 2026 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 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 FDEA202609031261Elec Connector · looseR1 DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL, ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. VERIFIED R1 DOOR ARMING HANDLE OPS AND THAT INDICATIOSep 3, 2026 · N681FE · Airbus A300F4605R · Door System WiringSDR FDEA202609011253Seat Track · wornMAIN DECK SEAT TRACK AT Y1959 BETWEEN FR 62 AND FR 63 FOUND WORN. SEAT TRACK SECTION AT Y1959 BETWEEN FR62 AND FR63 PER A300-600F SRM51-40-21 & SRM53-10-16-201 FIG.201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.Sep 1, 2026 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202608261228Attach Fitting · crackedFWD CARGO DOOR ACTUATOR ATTACH FITTING FOUND 2EA CRACKS BY HFEC INSPECTION. REPLACED THE CRACKED FWD CARGO DOOR ACTUATOR ATTACH FITTING WITH FABRICATED PART PER SRM51-40-21 & DWG: F52370695(ISSUE. J), A52370501(ISSUE. J) & A52370534(ISSUE. F). RSC TRACKING Aug 26, 2026 · N661FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202608181142Processor · faultedTAKEOFF AT IND, MLG WOULD NOT RETRACT. C-W QRH. RETURNED. EMERG DECLARED. AMM 32-31-00-05, NLG RETRACT FULLY, GREEN ON BOTH MLG INDS, BOTH LT & RT MLG STAYED GREEN DOWN ON INDS. PERFORMED MLG EXTEND & RETRACT AT GATE & VERIFIED ALL MLG DOORS EXTEND & REAug 18, 2026 · N689FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA202607301074Restraint · brokenMAIN CARGO DECK RESTRAINT MC1487 IN 8L HAS A BROKEN TIP. REMOVED DAMAGED RESTRAINT FROM AIRCRAFT COAT CLOSET AND SHIPPED FOR REPAIR. AIRCRAFT HAS SEAT TRACK DAMAGE AND FLOOR PANEL DAMAGE AT RESTRAINT ATTACH POINTS AND WILL REQUIRE SHEETMETAL REPAIR PRIOR Jul 30, 2026 · N679FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202607220984Power Supply · inoperativeRIGHT FORWARD DOOR SLIDE WILL NOT ARM. RELEASED FOR SERVICE PER MEL. ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. VERIFIED R1 DOOR SLIDE GIRT BAR LOCKS INTJul 22, 2026 · N658FE · Airbus A300F4605R · Door Warning SystemSDR FDEA202607200951Pressure Deck · corrodedFWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE FR40, Y-450 CORRODED. REPAIRED THE CORRODED AREA AT FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR39 - FR40, BETWEEN Y0 AND Y450. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100. SEE WRI 5310911Jul 20, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202607200950Pressure Deck · crackedFWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE FR40, Y1456 CRACKED. REPAIR. REPAIRED THE CORRODED AREA AT FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR39 - FR40, BETWEEN Y0 AND Y450. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM6-2-100.Jul 20, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202607170941Fcu · failedDURING CLIMB OUT PASSING 5000 ATS LEVER TRIPPED OFF AND WE LOST POWER TO THE ENTIRE FCP. NO FLIGHT DIRECTORS, NO FMAS. TRIED RESETTING ATS LEVER AND PITCH TRIM AND YD LEVERS. NO LUCK. AIR TURN BACK. MANUALLY FLOWN AND NO AUTO THROTTLES. AMM: 22-15-12-04Jul 17, 2026 · N656FE · Airbus A300F4605R · Flight Control SystemSDR FDEA202607140936Repair · no discrepancyEXISTING REPAIR ON LH WING SLAT NR 1 INNER SKIN BETWEEN RIB 10 & RIB 11 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON LT WING SLAT NR 1 INNER SKIN BETWEEN RIB10 AND RIB11 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5740-133777 A. PERFORMED Jul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202607140935Repair · no discrepancyEXISTING REPAIR ON MAIN DECK CROSSBEAM FR60,-Y1456~-Y2462 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CROSSBEAM FR60,-Y1456~-Y2462 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5310-43476 A.UPGRADED TO MAJOR REPAIR. CLASSIFIED Jul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202607140934Repair · inaccurateEXISTING REPAIR ON MAIN DECK SEAT TRACK FR32-FR38.2,Y450 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR32-FR38.2,Y450 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16 FIG.201.DUE TO ONE FASTENER MIJul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202607140933Repair · inaccurateEXISTING REPAIR ON MAIN DECK SEAT TRACK FR30-FR34,Y0 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR30-FR34,Y0 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16 FIG.201.DUE TO TWO FASTENERS MISSING INJul 14, 2026 · N678FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202607140932Seat Track · misrepairedEXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR22,Y2462 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR22,Y2462 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16 FIG.201A.DUE TO 4 FASTENERS MISSINJul 14, 2026 · N678FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607140931Repair · no discrepancyEXISTING REPAIR ON BULK CARGO DOOR SKIN BETWEEN FR67-FR69,BEAM4-LOWER EDGE REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON BULK CARGO DOOR SKIN BETWEEN FR67-FR69,BEAM4-LOWER EDGE WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5234-102006. .THE Jul 14, 2026 · N678FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202607140920Hinge Arm · delaminatedLH WING #3 SPOILER O/B CENTER HINGE ARM O/B DELAMINATION (AREA: 25MM*15MM,DEPTH: 1.40MM), I/B CENTER HINGE ARM O/B DELAMINATION ( AREA: 30MM*12MM, DEPTH: 1.50MM). PERFORMED THE REPAIR ON LH WING #3 SPOILER CENTER HINGE ARM PER FEDEX EA:6-5750- T0387988 P1 Jul 14, 2026 · N678FE · Airbus A300F4605R · SpoilersSDR FDEA202607130923Skin · misrepairedEXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR54.2-FR54.3,STGR46L-STGR49L REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR54.2-FR54.3,STGR46L-STGR49L. NO RECORD FOUND. REMOVED THE EXISTING REPAIR AND PERFORMED THE NEW REPAIR Jul 13, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202607100915Warning System · malfunctionedR1 DOOR WON T SHOW SLIDE WHEN DOOR IS ARMED. MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. AMM 52-73-13-04-02 AMM 31-55-22-04 SLAVED IN SWITCH 1Jul 10, 2026 · N681FE · Airbus A300F4605R · Door Warning SystemSDR FDEA202607100898Glide Slope · malfunctionedON RNAV APPROACH RW 21, ON GLIDEPATH AND CONFIGURED FOR LANDING GOT GLIDESLOPE GLIDESLOPE REPEATEDLY STARTING AT 100 FEET UNTIL TOUCHDOWN.Jul 10, 2026 · N654FE · Airbus A300F4605R · Glide Slope SystemSDR FDEA202607100896Sensor · faultedGREEN SYSTEM OVERHEAT LIGHT FLASHING AND CHIME WARINING.Jul 10, 2026 · N662FE · Airbus A300F4605R · Hydraulic Reservoir, MainSDR FDEA202607100884Floorbeam · corrodedEXISTING REPAIR ON BULK CARGO COMPARTMENT FLOOR BEAM FR66, Y1456 - Y1456 REQUIRES EVALUATION FOR COMFORMITY. EVALUATED AND FOUND NOT IN CONFORMITY WITH DWR:A53974322(ISSUE:T).FOUND CORROSION ON THE FLANGE SURFACE.PERFORMED THE NEW REPAIR PER EA 6-5321-T03Jul 10, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202607100883Floor Panel · crackedMDCC UNDER FLOOR PANEL FR47, Y-953 - Y-1456 FOUND 1EA WEB CRACKED. REPAIRED THE CRACKED WEB AT MDCC UNDER FLOOR PANEL FR47, Y-953 - Y-1456 PER A300-600F SRM53-15-15-201-C2 FIG.201 & SRM51-40-21. THIS IS CAT B REPAIR. INSPECTION THRESHOLD FROM REPAIR: 2400Jul 10, 2026 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202607100882Web · crackedMDCC UNDER FLOOR PANEL FR47, Y0 - Y450 FOUND 1EA WEB CRACKED. REPAIRED THE CRACKED WEB AT MDCC UNDER FLOOR PANEL FR47, Y-953 - Y-1456 PER A300-600F SRM53-15-15-201-C2 FIG.201 & SRM51-40-21. THIS IS CAT B REPAIR. INSPECTION THRESHOLD FROM REPAIR: 24000FC, Jul 10, 2026 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202607050840Crossbeam · crackedMDCC FR64, Y1456 - Y1959 CROSSBEAM CRACKED. REPAIRED THE CRACKED CROSSBEAM AT MDCC FR64, Y1456 - Y1959 PER SRM 53-10-15- 201 PARA.14 & SRM51-40-21. THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.Jul 5, 2026 · N678FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202607030830Pressure Switch · leakingON TAKEOFF ROLL AT ABOUT 60KTS ECAM ALERT OF GREEN HYDRAULIC SYSTEM LOW PRESSURE. WE GOT TWO ECAM WARNINGS, ONE RIGHT AFTER THE OTHER. RTO, AUTO BRAKES DID NOT ENGAGE BEC OF LOW SPEED. TSM 29-32-00 FIG 105 AMM 29-14-00-03 JRH CH5 WITH REF ABOVE RAN NR 1 AJul 3, 2026 · N690FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA202606280938Spoiler · delaminatedLH WING #3 SPOILER CENTER HINGE OUTBD ARM OUTBD WEB FOUND DELAMINATION. SIZE:40MM*25MM, DEPTH: 1.1MM COMPLIED WITH EA 6-5750-T0387764 P1, EA TITLE:WING - FLIGHT SURFACES - LH #3 SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE DELAMINATIJun 28, 2026 · N680FE · Airbus A300F4605R · Wing, Control SurfacesSDR FDEA202606280930Spoiler · delaminatedRH WING #5 SPOILER CENTER OUTBD HINGE ARM OUTBD WEB FOUND DELAMINATION. SIZE: A:40MM*25MM,B:30MM*20MM, DEPTH: A:1.6MM,B:1.2MM COMPLIED WITH EA 6-5750-T0387765 P1, EA TITLE:WING - FLIGHT SURFACES - RH #5 SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATIONJun 28, 2026 · N680FE · Airbus A300F4605R · SpoilersSDR FDEA202606240829Seat Track · damagedEXISTING REPAIR ON MAIN DECK SEAT TRACK FR62-FR65,-Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR62-FR65,-Y953 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F SRM53-10-16-201 FIG.201 DUE TO FOUND SEAT TRACK Jun 24, 2026 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202606240799Frame · damagedEXISTING REPAIR ON FUSELAGE FRAME FR0 BETWEEN 8-9 O'CLOCK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FUSELAGE FRAME FR0 BETWEEN 8-9 O'CLOCK WAS EVALUATED AND CANNOT BE IDENTIFIED TO A REPAIR IN THE SRM.NO RECORD FOUND.RE-REPAIRED PER EA 6-Jun 24, 2026 · N680FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202606240798Pressure Deck · not reportedEXISTING REPAIR ON HORIZONTAL PRESSURE DECK UPPER SURFACE BETWEEN FR51-FR52,Y0~- Y450 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON HORIZONTAL PRESSURE DECK UPPER SURFACE BETWEEN FR51- FR52,Y0~-Y450 WAS EVALUATED AND CANNOT BE IDENTIFIED TO A RJun 24, 2026 · N680FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202606230797Seat Track · noneEXISTING REPAIR ON MAIN DECK SEAT TRACK FR40-FR45,Y1456 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR40-FR45, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53832020(ISSUE: J00), NO RECORD FOUND. EO: 6-5100-7- Jun 23, 2026 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202606230796Crossbeam · not reportedEXISTING REPAIR ON MAIN DECK CROSSBEAM FR20,Y1959~Y2462 REQUIRES EVALUATION FOR CONFORMITY.Jun 23, 2026 · N680FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202606200788Cvr · malfunctionedCVR WOULD NOT TEST PROPERLY DURING PREFLIGHT. RELEASED FOR SERVICE PER MEL : 23-71-01 CATEGORY : A EXPIRATION : 23JUN26 MEL 23-71-01: CVR - INOP.AMM: 23-71-00-05 PERFORMED ADJ/TEST OF CVR IAW AMM 23-71-00-5 AND OPS CHECK WAS GOOD. NO FAULT FOUND.Jun 20, 2026 · N679FE · Airbus A300F4605R · Audio/Video MonitoringSDR FDEA202606190795Seat Track · no discrepancyEXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR21,-Y1959 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR18-FR21,Y1959 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH EA 6-5313-69642.Jun 19, 2026 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
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