N686FE

Service difficulty reports · 181

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 = 'N686FE' 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 FDEA202402200191Autothrottle Sys · faultedSHORTLY AFTER LIFTOFF ON THE ATS OFF, NON-PROFILE TAKEOFF, THE RIGHT THROTTLE REDUCED ITSELF BY APPROXIMATELY 1.5 KNOB WIDTHS. ADVANCED THE RIGHT THROTTLE TO MATCH AND THE PROBLEM NEVER RETURNED. THE CAPTAIN STATED THAT THIS ISSUE IS THE SAME ISSUE THATFeb 20, 2024 · N686FE · Airbus A300F4605R · Auto Throttle SystemSDR FDEA202402130157Power Supply · failedDURING MX. PREFLIGHT: COURIOR AREA EMERGENCY LIGHTS ARE INOP. REPLACED EPSU BATTERY IAW A300-600 AMM CH. REF. LISTED ABOVE. OPS CKS GOO. A/C OK FOR SERVICE. AMM: 33-51-14-04. PAR. B REPLACED EPSU BATTERY IAW A300-600 AMM CH. REF. LISTED ABOVE. OPS CKS Feb 13, 2024 · N686FE · Airbus A300F4605R · Emergency LightingSDR FDEA202304050564Seat · crackedAPPEARS FRONT OF CAPTAINS SEAT IS LOOSE. ROCKS EXCESSIVELY. AMM 25-XX-XX-XX FOUND CAPT SEAT CRACKED AT BOTH FRONT ATTACH POINTS REF AMM 25-11-11-06. AMM: 25-11-11-04 REMOVED AND REPLACED CAPT SEAT REF AMM 25-11-11-04, OP'S CHECK GOODApr 5, 2023 · N686FE · Airbus A300* · Flight Compartment EquipmentSDR FDEA202208082051Skin · dentedFOUND A DENT AT RH O/B FLAP UPPER SURFACE I/B T/E. CUT OUT THE DAMAGE AREA AND REPAIR WITH EXTERNAL DOUBLER I.A.W EA NO:6-5750-T0370136 P1, SEQ NO:000767, TITLE:WING - FLIGHT SURFACES - RH OUTER FLAP TRAILING EDGE UPPER SKIN REPAIR BETWEEN RIBS 3A AND 3B &Aug 8, 2022 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202208051895Dummy Rail · wornFR54/FR54.2 LH NO.5 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.5MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202208051894Dummy Rail · wornFR54/FR54.2 RH NO.5 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.5MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202208051893Seat Track · wornFR54/FR54.2 RH NO.4 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.4MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202208051892None · wornFR54/FR54.2 RH NO.3 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.15MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202208051891None · wornFR38.2/FR40 LH NO.2 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.15MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202208051890None · wornFR38.2/FR40 RH NO.5 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.12MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202208051889None · wornFR38.2/FR40 RH NO.3 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.46MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PERFORM REPAIR. REPAIR ACCOMPLISHED.Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202208021926None · noneAIRCRAFT REPAIR ASSESSMENT:EXISTING CROSSBEAM REPAIR FOUND ON MAIN DECK AT FR58,BTW -Y450~-Y953. COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTING REPAIR DETERMINED IT TO BAug 2, 2022 · N686FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202208021925None · noneAIRCRAFT REPAIR ASSESSMENT:EXISTING SPLICE REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR56~FR57.2,-Y450 POSITION. COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTING REPAIR DETAug 2, 2022 · N686FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202208021924None · noneAIRCRAFT REPAIR ASSESSMENT:EXISTING SPLICE REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR57-57.2,Y450 POSITION. COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTING REPAIR DETERMAug 2, 2022 · N686FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202207282043Rib · cracked1EA CRACK(7MM) WAS FOUND AT L/H WING CENTER FLAP RIB 27 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE WORK WITH REPAIR ANGLE AND EXTERNAL DOUBLER I.A.W EA NO:6-5750- T0369804 P1, SEQ NO:000760, TITLE:WING-FLIGHT SURFACES-LH CENTER FLAP, CRACKS IN Jul 28, 2022 · N686FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202207282042Rib · cracked3EA CRACKS(MAX18MM) WERE FOUND AT L/H WING CENTER FLAP RIB 26 FWD AND AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE WORK WITH REPAIR ANGLES AND EXTERNAL DOUBLER I.A.W EA NO:6-5750- T0369804 P1, SEQ NO:000760, TITLE:WING-FLIGHT SURFACES-LH CENTER FLAPJul 28, 2022 · N686FE · Airbus A300B4605R · Wing, Rib/BulkheadSDR FDEA202207281842Floor Panel · damagedFWD CARGO COMPT #131MG FLOOR PANEL WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005Jul 28, 2022 · N686FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202207281841Floor Panel · damagedFWD CARGO COMPT #131RG FLOOR PANEL WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005Jul 28, 2022 · N686FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202207272023Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 27AFT AREA. ACCOMPLISHED THE WORK WITH REPAIR ANGLE AND EXTERNAL DOUBLER I.A.W EA NO:6-5750- T0369907 P1 ,SEQ NO:000761 ,TITLE:WING-FLIGHT SURFACES-RH CENTER FLAP ,CRACKS IN UPPER FLANGES OF RIBS 25,26 AND 27 BJul 27, 2022 · N686FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202207272022Rib · cracked2EA CRACKS WERE FOUND AT RH WING CENTER FLAP RIB 26AFT AREA. ACCOMPLISHED THE WORK WITH REPAIR ANGLE AND EXTERNAL DOUBLER I.A.W EA NO:6-5750- T0369907 P1 ,SEQ NO:000761 ,TITLE:WING-FLIGHT SURFACES-RH CENTER FLAP ,CRACKS IN UPPER FLANGES OF RIBS 25,26 AND 27Jul 27, 2022 · N686FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202207272021Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 25AFT AREA. ACCOMPLISHED THE WORK WITH REPAIR ANGLE AND EXTERNAL DOUBLER I.A.W EA NO:6-5750- T0369907 P1 ,SEQ NO:000761 ,TITLE:WING-FLIGHT SURFACES-RH CENTER FLAP ,CRACKS IN UPPER FLANGES OF RIBS 25,26 AND 27 BJul 27, 2022 · N686FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202207272020Seat Track · corrodedMAIN DECK WAS FOUND SEAT TRACK CORROSION AT FR14 7"~ FR15B 9",Y 450 REPLACED THE SEAT TRACK WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2Jul 27, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202207272019Seat Track · corrodedMAIN DECK WAS FOUND SEAT TRACK CORROSION AT FR14C~ FR17,Y-450 REPLACED THE SEAT TRACK WITH NEW ONE I.A.W A300-600F SRM 51-72-10-001, PAGE.2Jul 27, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202207271960Floor Support · corrodedMAIN DECK FLOOR LONGERON SUPPORT STRUCT UPR SURFACE FOUND CORROSION NEAR FR12A 2",Y 730 REMOVED SUPPORT STRUCT AND INSTALLED NEW SUPPORT STRUCT I.A.W A300-600F SRM 51-72- 10-001, PAGE2 AND 51-40-21-001, PARA 6 , PAGE7B - PAGE23.Jul 27, 2022 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202207262050Seat Track · noneFOUND EXISTING SPLICE REPAIR ON MAIN DECK SEAT TRACK BTW FR 56~57.2, Y1456 POSITION NOT I.A.W SRM 53-10-16-201 PARA.4 FIG.201. ACCOMPLISHED THE REPAIR WORK I.A.W. A300-600F SRM 53-10-16-201 PARA.4 FIG.201 P.203-208.Jul 26, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202207262041Seat Track · noneFOUND EXISTING SPLICE REPAIR ON MAIN DECK SEAT TRACK BTW FR 52~53, -Y450 POSITION NOT I.A.W SRM 53-10-16-201 PARA.4 FIG.201. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO:T6-5310-T0370079 P1,TITLE:FUSELAGE- MAINFRAME-EXISTING SEAT TRACK REPAIR BETWEEN FR52 ANJul 26, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202207262010Seat Track · noneFOUND EXISTING SPLICE REPAIR ON MAIN DECK SEAT TRACK BTW FR61-65, Y450 POSITION NOT I.A.W SRM 53-10-16-201 PARA.4 FIG.201. REMOVED THE UNQUALIFIED EXISTING REPAIR & PERFORMED SEAT TRACK SPLICE REPAIR I.A.W A300-600F SRM 53-10-16-201 PARA.4 FIG.201 PAGE.203Jul 26, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202207262009Seat Track · noneFOUND EXISTING SPLICE REPAIR ON MAIN DECK SEAT TRACK BTW FR 36~37, -Y1456 POSITION NOT I.A.W SRM 53-10-16-201 PARA.4 FIG.201. REMOVED THE INCORRECT INSTALLED FASTENERS & REPAIRED PER A300-600F SRM 53-10-16-201 PARA.4 FIG.201 PAGE.203-208, THIS REPAIR IS CLJul 26, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202207261923Skin · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON FUSELAGE SKIN AT FR59A,BTWSTGR41R-43R. COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1,TITLE:A300/A310 RPR IDENT & SUPPLEMENTAL MX REQ(SMR)TRK,INSPECTION OF EXISTING REPAIR DETERMIJul 26, 2022 · N686FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202207212085None · noneTHIS NRC IS FOR REWORK, REF TO N00121 FOR REPAIR ASSESSMENT, FOUND EXISTING DOUBLER REPAIR BTW FR20-20A STGR 39R-42R NOT TO BE CURRENT WITH FAA APPROVED SRM DATA 53-13-12-201 PARA.5 PAGE.206-211 FIG.201(SHEET.1).Jul 21, 2022 · N686FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202201140520Epsu · inoperativeMDIS 686 33-50 1477 14JAN22 BUR FACT U EMERGENCY LIGHTS FOR L1 AND L2 DOORS AND COURIER AREA INOP. R/I 14JAN22 15:14 BUR U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: AD-3214-30 POS: 3 SRL: 88700 Jan 14, 2022 · N686FE · Airbus A300F4605R · Emergency LightingSDR FDEA202012033019Slide · detachedFOUND R-1 DOOR ESCAPE SLIDE SEPARATED FROM DOOR ATTACH BRACKET. CREW ENTRY DOOR ESCAPE SLIDE R1- REMOVED. INSTALLED ESCAPE SLIDE ON R1 DOOR, IN REF TO AMM 25-61-21-04-0. A/C OK FOR SERVICE.Dec 3, 2020 · N686FE · Airbus A300F4605R · Escape SlideSDR FDEA202012023016Slide · detachedFOUND R-1 DOOR ESCAPE SLIDE SEPARATED FROM DOOR ATTACH BRACKET. INSTALLED ESCAPE SLIDE ON R1 DOOR IN REF TO AMM 25-61-21-04-0. A/C OK FOR SERVICE.Dec 2, 2020 · N686FE · Airbus A300F4605R · Escape SlideSDR FDEA2020071091483Module · inoperativeNR 2 ENGINE FIRE HANDLE UPPER ROW LIGHT DOES NOT ILLUMINATE DURING FIRE TEST AND LIGHT TEST. R & R THE NR 2 ENGINE FIRE CONTROL MODULE IAW AMM 26-12-20-04. OPS NORMAL.Jul 9, 2020 · N686FE · Airbus A300F4605R · Fire DetectionSDR FDEA2020072311185Wire Harness · malfunctionedON DESCENT INTO AFW AT 6000' AND 250 KTS, SMOOTH AIR, ENG #1 LOOP A FAULTED, COMPLIED WITH QRH. RELEASED FOR SERVICE PER MEL : 26-12-01-01-A CATEGORY : C EXPIRATION : 21JUN20 "MEL 26-12-01-01-A: ENG 1 LOOP A - INOP. FLIGHT CREW MUST PERFORM FUNCTIONAL Jun 11, 2020 · N686FE · Airbus A300F4605R · Fire DetectionSDR FDEA2020061211185Fire Loop · faultedON DESCENT INTO AFW AT 6000' AND 250 KTS, SMOOTH AIR, ENG NR 1 LOOP A FAULTED, COMPLIED WITH QRH. RELEASED FOR SERVICE PER MEL : 26-12-01-01-A CATEGORY : C EXPIRATION : 21JUN20 "MEL 26-12-01-01-A: ENG 1 LOOP A - INOP. FLIGHT CREW MUST PERFORM FUNCTIONAL TEST Jun 11, 2020 · N686FE · Airbus A300F4605R · Fire DetectionSDR FDEA202006111184Wire Harness · faultedDURING CLIMB OUT, NUMEROUS BRIEF ECAM WARNINGS OF NR 2 ENG B LOOP FAULT. ONCE LEVEL AT CRUISE AND POWER REDUCED, WARNINGS STOPPED. CLOSED AND SECURED NR 2 ENGINE FAN, REVERSER AND CORE COWLS IAW MM 71-10-00, RAN NR 2 ENGINE IAW JRH FOR OVER 20 MINUTE'S AND Jun 11, 2020 · N686FE · Airbus A300F4605R · Fire Protection System WiringSDR FDEA2020060531128Pitot Line · obstructedABORTED TAKEOFF AT 100KIAS ON CAPT'S PFD. FIRST OFFICERS AIRSPEED INDICATION READ 70KIAS. FLUSHED CAPT AND FIRST OFFICER`S PITOT PRESSURE LINES IAW AMM 34-10-00-03. FOUND DEBRIS (BURNT FLYING BUG NEST AND BUGS) PURGED FROM FIRST OFFICERS LINE FUNCTIONAL TESJun 3, 2020 · N686FE · Airbus A300F4605R · Pitot/Static SystemSDR FDEA202001230211Spar · crackedINSPECTION OF CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE, RH SIDE, FOUND HOLE D WITH CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE, RH SIDE, CRACKED HOLE D PER EA: 6-5710-T0352050 PJan 23, 2020 · N686FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202001230210Angle · crackedINSPECTION OF CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE, LH SIDE, FOUND HOLE G WITH CRACK SIGNAL REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE, LH SIDE, CRACKED HOLE G PER EA: 6-5710-T0352050 PJan 23, 2020 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202001160142Web · crackedMAIN DECK FR47 UNDERFLOOR WEB BETWEEN Y0 AND -Y450 CRACKED REPAIRED THE CRACKED WEB OF MAIN DECK FR47 UNDERFLOOR BETWEEN Y0 AND -Y450 PER A300-600F SRM53-15-15-C2-201 PARA.5. THE REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-Jan 16, 2020 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202001160141Web · crackedMAIN DECK FR47 UNDERFLOOR WEB BETWEEN Y0 AND Y450 CRACKED REPAIRED THE CRACKED WEB OF MAIN DECK FR47 UNDERFLOOR BETWEEN Y0 AND Y450 PER A300-600F SRM53-15-15-C2-201 PARA.5. THE REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-60Jan 16, 2020 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202001160140Web · crackedMAIN DECK FR47 UNDERFLOOR WEB BETWEEN Y953 AND Y1456 CRACKED REPAIRED THE CRACKED WEB OF MAIN DECK FR47 UNDERFLOOR BETWEEN Y953 AND Y1456 PER A300-600F SRM53-15-15-C2-201 PARA.5. THE REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER AJan 16, 2020 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202001090081Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN Y1456 AND Y1959 REPAIRED THE CRACKED CROSSBEAM OF MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR64 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15 FIG211. MAJOR REPAIRJan 9, 2020 · N686FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202001090080Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR57.3, BETWEEN Y1456 AND Y1959 REPAIRED THE CRACKED CROSSBEAM OF MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR57.3 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15 FIG211. MAJOR REJan 9, 2020 · N686FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202001090079Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR31, BETWEEN -Y450 AND -Y953 REPAIRED THE CRACKED CROSSBEAM OF MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR31 BETWEEN -Y450 AND -Y953 PER A300-600F SRM53-10-15 FIG212 AND EA: 6-531Jan 9, 2020 · N686FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202001090078Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR30, BETWEEN -Y450 AND -Y953 REPAIRED THE CRACKED CROSSBEAM OF MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR30 BETWEEN -Y450 AND -Y953 PER A300-600F SRM53-10-15 FIG212 AND EA: 6-531Jan 9, 2020 · N686FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201909142243Filter · odorPDIS 686 21-50 9237 14SEP19 MEM FACT U LOGPAGES:3143852 AFTER TALE-OFF @ KSDF, FUMES/ODORS FROM A/C PACKS WITH ECON SELECTED ON OVHD PANEL, DESELECTED ECON FLOW BUT STILL LINGERING FUMES/ODORS. FACT 14SEP19 16:40 MEM U R/R FILTER FOR THE FLIGHT COMPSep 14, 2019 · N686FE · Airbus A300F4605R · Air Distribution SystemSDR FDEA2019032760734Support · damagedGEAR WOUL NOT RETRACT ON T/O SYS1. SWITCHED TO SYS 2 AND GEAR WOULD NOT RETRACT. GEAR LEVER WOULD NOT MOVE PAST CENTER DETENT. TSM: 32-30-00 FIG.109 AND FOUND NO CONTINUITY BETWEEN PIN H AND PIN K, LANDING GEAR CONTROL LEVER TO BE REPLACED. LANMar 26, 2019 · N686FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201807121693None · noneMAIN CABIN UNDER FLOOR PANEL 232UG SEAT TRACK HAS A SPOT OF CORROSION ON THE SIDE JUST AFT OF THE SEAT TRACK SPLICE, FR26 TO 27, O/B TRACK REMOVED DAMAGE ABD EVALUATED DAMAGE AREA IAW A300-600 SRM 51-10-16. MAX RE-WORK DEPTH PER SRM IS .012", DEPTH ON AIRCRADec 7, 2018 · N686FE · Airbus A300* · Fuselage Main, Longeron/Stringer
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