N685FE

Service difficulty reports · 276

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 = 'N685FE' 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 FDEA202504020554Overheat Sensor · malfunctionedINFLIGHT GOT ECAM: HOT AIR SUPPLY OVERHEAT, THEN GOT: MAIN DECK CARGO SMOKE - MID DECK B, THEN GOT BLEED VALVE ENG 2 FAULT. COMPLIED WITH ECAM CHECKLIST AND DECLARED EMERGENCY. WHILE LANDING GOT ENG 2 REV CONTROL CB POPPED (V74). EMERGENCY DECLARED. MAIApr 2, 2025 · N685FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA202405170683Angle · damagedCHECK FOUND 1 EA ANGLE MOUNTING BROKEN BETWEEN FR79 AND FR 80 AT AFT OF BULK CARGO. REPLACED THE NEW SECTION I.A.W A300-600F SRM 51-72-10-001, P.2. THE REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100. (BTW FR79 AND FR80 AFT OF BULK CARGO)May 17, 2024 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202405110747Spacer · crackedTHE MDC DOOR ACTUATOR SPACER WAS FOUND CRACK AT FR24. REPLACED THE NEW SPACER I.A.W A300-600F SRM 51-72-10-001, P.2 (POS:MDC DOOR AT FR24). THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100May 11, 2024 · N685FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202405100749Rib · wornRH WING #5 SPOILER ACTUATOR O/B JACK RIB I/B FACE SURROUNDING BOLT HOLE LOCATION 3 (O/B LWR) AREA FOUND NICK ACCOMPLISHED THE REINFORCED REPAIR AT RH WING #5 SPOILER O/B JACK RIB LOWER HOLE I.A.W FEDEX EA NO:T6-5740-T0379208 P1, SEQ NO:769, TITLE: WING-ATTMay 10, 2024 · N685FE · Airbus A300F4605R · SpoilersSDR FDEA202405100748Rib · wornRH WING #5 SPOILER ACTUATOR O/B JACK RIB I/B FACE SURROUNDING BOLT HOLE LOCATION 1 (O/B UPR) AREA LOSS OF PROTECTION ACCOMPLISHED THE REINFORCED REPAIR AT RH WING #5 SPOILER O/B JACK RIB UPPER HOLE I.A.W FEDEX EA NO:T6-5740-T0379208 P1, SEQ NO:769, TITLE: May 10, 2024 · N685FE · Airbus A300F4605R · SpoilersSDR FDEA202405090681Header · bentAFT CGO DOOR CUTOUT UPPER FWD CORNER FOUND A PLATE DEFORMED, POS: FR59A-FR61 STGR28R REPLACED THE DEFORMED HEADER WITH NEW PART ON AFT CGO DOOR CUTOUT UPPER FWD CORNER AT FR59A~FR61, STGR28R I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARAMay 9, 2024 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202405090662Bracket · damaged#4 SUPPORT BRACKET BROKEN FOR AFT CARGO COMP'T DOOR AT FR61A~FR62,S-43R POSITION. REPLACED THE BRACKET WITH NEW PART AND FASTENERS AT AFT CARGO DOOR FR61A~FR62 S- 43R, THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 I.A.W A300-600F SRM 51-72-10-001, PAGE.2 &May 9, 2024 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202405070764Fitting · crackedTHE MDC DOOR ACTUATOR AFT SUPPORT FRAME WAS FOUND CRACK AFTER MDC DOOR REMOVED FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA: T6-5230- T0379032 P1, SEQ NO:774 TITLE: DOORS - CARGO DOOR/HYD SYS - MAIN CARGO DOOR ACTUATOR BEARIMay 7, 2024 · N685FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202405070682Strap · bentTHSA COMPT FOUND 1EA SUPPORT WEB GOT DEFORM AT FR85-86 S-33R REPLACED THE DAMAGE SUPPORT WEB AT THSA COMPT FR85-86 S-33R I.A.W A300-600F SRM 51- 72-10-001, PAGE.2, REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.May 7, 2024 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202404300732Stop Fitting · crackedAVIONICS COMP'T ACCESS DOOR STOP FITTING "OMEGA"CRACK AT FR6,Z-1497 POSITION. ACCOMPLISHED THE REPLACEMENT OF OMEGA AT AVIONICS ACCESS DOOR STOP FR6 Z-1497 Y0 I.A.W A300-600F SRM 51-72-10-001, PAGE.2, THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100Apr 30, 2024 · N685FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202404300674Angle · crackedAVIONICS COMP'T CABIN FLOOR STRUCTURE CROSSBEAM 1EA ANGLE FITTING CRACK AT FR10,Y- 953 POSITION. REPLACED THE NEW ANGLE WITH RIVETS I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21- 001, PARA.6, PAGE.7B-PAGE.23,THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6Apr 30, 2024 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202404270762Fitting · crackedTHE MDC DOOR ACTUATOR YOKE FWD SUPPORT FRAME WAS FOUND CRACK. FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA: T6-5230- T0379032 P1, SEQ NO:774 TITLE:DOORS - CARGO DOOR/HYD SYS - MAIN CARGO DOOR ACTUATOR BEARING FITTING REPLACEMENTApr 27, 2024 · N685FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202308231478Unknown · unknownA/C CAME INTO BLOCKS WITH RAT DEPLOYED. BOTH HANDLES IN COCKPIT HAVE COPPER WIRE STILL INSTALLED.Aug 23, 2023 · N685FE · Airbus A300* · Hydraulic Power SystemSDR FDEA202307301335Valve · failedAPPROACHING RWY23R KTYS FOR TAKEOFF, INDICATING SMOKE IN COURIER AREA. STOPPED ACFT. CONFIRMED SMOKE IN COURIER AREA. NO SMOKE IN COCKPIT. DECLARED EMERGENCY WITH KTYS TOWER. CONDUCTED EMERG EVAC, EXITING VIA L1 SLIDE. PERCEIVED SMOKE COMING FROM VENTS OVEJul 30, 2023 · N685FE · Airbus A300* · Hydraulic Power SystemSDR FDEA202304130641Unknown · unknownPDIS 685 27-80 2192 13APR23 YEG OPEN U WHILE ON APPROACH AT 8000 FT MSL AND 210KIAS, RECEIVED A SLAT SYS 1&2 FAULT. COMPLIED WITH ECAM AND QRH. FAULT NOT CLEARED. ***EMERGENCY DECLARED*** TSM: 27-80-02 JRH: CHAPTER 6 AMM: 12-22-27-00 TROUBApr 13, 2023 · N685FE · Airbus A300* · Leading Edge Slat Control SystemSDR FDEA202111182924Seat Track · gougedMAIN DECK FLOOR STRUCTURE SEAT TRACK FOUND GOUGE AT FR72 2" Y0 REPAIR THE DAMAGED SEAT TRACK I.A.W A300-600F SRM 53-10-16-201 PARA4C PAGE201- PAGE207/208 FIG201 & 53-18-16-201-2 P.201Nov 18, 2021 · N685FE · Airbus A300* · Fuselage Structure (General)SDR FDEA202111142928Floor Panel · damagedMAIN DECK CAGRO COMPT #231AH FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.Nov 14, 2021 · N685FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202111142902Floor Panel · damagedMAIN DECK CAGRO COMPT #232NG FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.Nov 14, 2021 · N685FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202111142901Floor Panel · damagedMAIN DECK CAGRO COMPT #231HH FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.Nov 14, 2021 · N685FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202111142900Floor Panel · damagedMAIN DECK CAGRO COMPT #231CF FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, FIG. 201, P. 201-205.Nov 14, 2021 · N685FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202111112917None · gougedMDCC SEAT TRACK CROSS BEAM ADAPTER FND GOUGE AT FR54 BTN Y-1959 AND Y-2452 REMOVED THE DAMAGED CROSS BEAM AND INSTALLED THE NEW CROSS BEAM I.A.W A300-600F SRM 51-72-10-001 PAGE2 AND 51-40-21-001 PARA7 PAGE24-PAGE50.Nov 11, 2021 · N685FE · Airbus A300* · Fuselage Structure (General)SDR FDEA202111112894Seat Track · gougedSEAT TRACK Y-953 FND GOUGE AT FR44 40MM REPLACED THE DAMAGED SEAT TRACK WITH NEW ONE BY FASTENERS I.A.W. A300-600F SRM 51- 72-10-001 P. 2 AND 51-4-21-001 PARA. 7 P. 24-50.Nov 11, 2021 · N685FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202111102809None · wornN00399 FR54/FR54.2 LH NO.5 DUMMY SEAT TRACK GAP VALUE(A) OVER 1.0MM. REPAIRED THE DUMMY SEAT TRACK AND CHECK OK FOR SERVICE I.A.W A300-600 SRM 53-15-16- 201 & AMM:20-21-12-00.Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/StructuresSDR FDEA202111102808None · wornN00398 FR54/FR54.2 LH NO.4 DUMMY SEAT TRACK GAP VALUE(A) OVER 1.0MM. REPAIRED THE DUMMY SEAT TRACK AND CHECK OK FOR SERVICE I.A.W A300-600 AMM:20-21-12- 00 & SRM 53-15-16-201 .Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/StructuresSDR FDEA202111102807None · wornN00397 FR54/FR54.2 RH NO.4 DUMMY SEAT TRACK GAP VALUE(A) OVER 1.0MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P.201~P210 FIG.201 PFM REPAIR ACCOMPLISHED.Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/StructuresSDR FDEA202111102806None · wornN00396 FR38.2/FR40 LH NO.5 DUMMY SEAT TRACK GAP VALUE(A) OVER 1.0MM. REPAIRED THE DUMMY SEAT TRACK AND CHECK OK FOR SERVICE I.A.W A300-600 SRM: 53-15-16- 201 & AMM:20-21-12-00.Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/StructuresSDR FDEA202111102805None · wornN00395 FR38.2/FR40 LH NO.4 DUMMY SEAT TRACK GAP VALUE(A) OVER 1.0MM. REPAIRED THE DUMMY SEAT TRACK WITH CHECK OK FOR SERVICE I.A.W A300-600 SRM 53-15- 16- 201 &AMM:20-21-12-00.Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/StructuresSDR FDEA202111102804None · wornN00394 FR38.2/FR40 NO.1 DUMMY SEAT TRACK GAP VALUE(A) OVER 1.0MM. REPAIRED THE DUMMY SEAT TRACK WITH CHECK OK FOR SERVICE I.A.W A300-600 SRM 53-15- 16- 201 & AMM:20-21-12-00.Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/StructuresSDR FDEA202111082907None · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON RUDDER TRAILING EDGE APEX AREA LOCATED BTW T/E SCREW LINE NO.20 AND NO.21 FASTENER COUNTED FROM LOWER SIDE POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXINov 8, 2021 · N685FE · Airbus A300* · Rudder StructureSDR FDEA202111082906None · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON L/H WING LWR SURFACE L/E PANEL 513AB CUTOUT FWD O/B AREA POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FANov 8, 2021 · N685FE · Airbus A300* · Wing, Plate/SkinSDR FDEA202111082905None · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR SURFACE L/E PANEL 613AB CUTOUT FWD O/B AREA POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA Nov 8, 2021 · N685FE · Airbus A300* · Wing, Plate/SkinSDR FDEA202111082879None · noneAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON L/H WING I/B FLAP UPR SURFACE SKIN LOCATED BTW RIB3-4 AND STGR 1.1 10.4" POSITION.. REF TO EO:E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR FOUND IT TO BE NOT CURRENT WITH FAA APPROVEDNov 8, 2021 · N685FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202111072893Floor Panel · damagedAFT CARGO COMPT #151 UF FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201 PARA. 8B FIG. 203 SHEET 1 P. 209-211.Nov 7, 2021 · N685FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202111072897Floor Panel · damagedAFT CARGO COMPT #151 PF FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203, SHEET 1, P. 209-211.Nov 7, 2021 · N685FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202111072896Floor Panel · damagedAFT CARGO COMPT #151 WF FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203, SHEET 1, P. 209-211.Nov 7, 2021 · N685FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202111072895Floor Panel · damagedFWD CARGO COMPT #131 LG FLOOR PANEL WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8B, FIG. 203, SHEET 1, P. 209-211.Nov 7, 2021 · N685FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202111062878None · cracked2 EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB 26AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE WORK: LH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB 26 BETWEEN STRINGERS 2.7 AND 2.8 - ALI 575306-01 I.A.W. EA: T6-5750-T0365383 P1 (SEQ 1146) AND Nov 6, 2021 · N685FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202111062877None · cracked2EA CRACKS WERE FOUND AT RH WING CENTER FLAP RIB 26AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE RIB FLANGE REPAIR I.A.W. EA: T6-5750-T0365382 P1 (SEQ 1147) WORK TITLE: RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIBS 26 AND 27 BETWEEN STRINGERSNov 6, 2021 · N685FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202111062876None · cracked2EA CRACKS WERE FOUND AT RH WING CENTER FLAP RIB 27AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE RIB FLANGE REPAIR I.A.W. EA: T6-5750-T0365382 P1 (SEQ 1147) WORK TITLE: RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIBS 26 AND 27 BETWEEN STRINGENov 6, 2021 · N685FE · Airbus A300* · Wing, Control SurfacesSDR FDEA2019102542746Windshield · crackedF/O FRONT WINDSHIEL WINDOW HEAT FAULT FOLLOWED BY CRACKING , APPEARS TO BE CRACKED OUTER LAYER . FOUND CRACK FROM LEFT BOTTOM TO RIGHT UPPER OF F/O WINDSHIELD F/O WINDSHIELD AND WINDSHIELD TEMPERATURE CONTROLLER REPLACED PER MM, OPS CHECK OKOct 24, 2019 · N685FE · Airbus A300F4605R · Flight Compartment WindowsSDR FDEA201908081814Valve · malfunctionedON ROTATION, NR 2 REVERSER UNLOCK AMBER LIGHT ILLUMINATED WITH ECAM AND THRUST REVERSER PRESSURIZED ON ECAM. COMPLIED WITH ECAM AND QRH THRUST REVERSER UNLOCKED. ENG REV UNLK PROCEDURE LIGHT AND ECAM REMAINED UNTIL SHUTDOWN. FOLLOWING MOCC MTSI, AND FIM 78Aug 8, 2019 · N685FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA2019080971819Regulator Valve · failedON ROTATION, NR 2 REVERSER UNLOCK AMBER LIGHT ILLUMINATED WITH ECAM AND THRUST REVERSER PRESSURIZED ON ECAM. COMPLIED WITH ECAM AND QRH THRUST REVERSER UNLOCKED. ENG REVERSER UNLK PROCEDURE LIGHT AND ECAM REMAINED UNTIL SHUTDOWN. THRUST REVERSER IS DEACTAug 7, 2019 · N685FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA2019060311204Warning Message · false activationMAIN DECK DOOR NOT CLOSED INFLIGHT INDICATION ON ECAM CLEANED ALL TARGET AND PERFORMED SEVERAL OPS CHECK OF MAIN DECK DOOR IAW MM 52-36-00-00. UNABLE TO DUPLICATE. NO HISTORY LAST 99 DAYS, SUSPECT INTERMITTENTE FAULT. A/C OK TO CONTINUE.Jun 1, 2019 · N685FE · Airbus A300F4605R · Door Warning SystemSDR FDEA2019042650924Floor Panel · crackedMDCC 241TJ FLOOR PANEL BROKEN FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.Apr 25, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2019042650923Floor Panel · brokenMDCC 232GG FLOOR PANEL BROKEN FABRICATED A NEW FLOOR PANE IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.Apr 25, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2019042540900Seat Track · crackedMAIN DECK FLOOR STRUCTURE LBL 1959 BETWEEN FR60 AND FR61 SEAT TRACK CRACKED IN RADIUS OF SCALLOP REPLACED SEAT TRACK USING P/N DAN 2001T79511 BATCH #0003037298 IAW AIRBUS DWG 17A53274786 SRM 51-40-21. MAJOR REPAIRApr 24, 2019 · N685FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2019042540899Floor Panel · damagedFLOOR PANEL R532B113600000 IS DAMAGED FWD PIT FABRICATED NEW FLOOR PANEL R532B113600000 ON TRAVELER T19/1412584 IAW SRZ-25-005 MAJOR REPAIRApr 24, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2019042540898Floor Panel · crackedMAIN DECK CARGO COMPT 262WF FLOOR PANEL CRACKED. FABRICATED FLOOR PANEL 262WF ON VT MAE TRAVELER T19/1411071 PER SRZ-25-005 CAT "A" MAJOR REPAIRApr 24, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2019042540893Floor Panel · brokenMDCC 242GJ FLOOR PANEL BROKEN FABRICATED 242GJ FLOOR PANEL ON VTMAE TRAVELER # T19/1411075 PER DWG SRZ -25-005 CAT "A" MAJOR REPAIRApr 24, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA2019042540892Floor Panel · brokenMDCC 241NJ FLOOR PANEL BROKEN FABRICATED FLOOR PANEL 241NJ ON VTMAE TRAVELER # T19/1411077 PER DWG SRZ -25-005 CAT "A" MAJOR REPAIRApr 24, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor Panel
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