# Service difficulty reports: N685FE

A list on [N685FE](https://openairdocs.org/aircraft/N685FE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 6 · 276 reports

- [SDR FDEA202504020554](https://openairdocs.org/sdr/FDEA202504020554.md): Overheat Sensor · malfunctioned · Apr 2, 2025 · N685FE · Airbus A300F4605R · Engine Thrust Reverser
  > INFLIGHT 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. MAI
- [SDR FDEA202405170683](https://openairdocs.org/sdr/FDEA202405170683.md): Angle · damaged · May 17, 2024 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CHECK 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)
- [SDR FDEA202405110747](https://openairdocs.org/sdr/FDEA202405110747.md): Spacer · cracked · May 11, 2024 · N685FE · Airbus A300F4605R · Cargo/Baggage Doors
  > THE 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 06-2-100
- [SDR FDEA202405100749](https://openairdocs.org/sdr/FDEA202405100749.md): Rib · worn · May 10, 2024 · N685FE · Airbus A300F4605R · Spoilers
  > RH 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-ATT
- [SDR FDEA202405100748](https://openairdocs.org/sdr/FDEA202405100748.md): Rib · worn · May 10, 2024 · N685FE · Airbus A300F4605R · Spoilers
  > RH 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:
- [SDR FDEA202405090681](https://openairdocs.org/sdr/FDEA202405090681.md): Header · bent · May 9, 2024 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFT 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, PARA
- [SDR FDEA202405090662](https://openairdocs.org/sdr/FDEA202405090662.md): Bracket · damaged · May 9, 2024 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > #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 &
- [SDR FDEA202405070764](https://openairdocs.org/sdr/FDEA202405070764.md): Fitting · cracked · May 7, 2024 · N685FE · Airbus A300F4605R · Fuselage Main, Structure
  > THE 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 BEARI
- [SDR FDEA202405070682](https://openairdocs.org/sdr/FDEA202405070682.md): Strap · bent · May 7, 2024 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > THSA 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.
- [SDR FDEA202404300732](https://openairdocs.org/sdr/FDEA202404300732.md): Stop Fitting · cracked · Apr 30, 2024 · N685FE · Airbus A300F4605R · Fuselage Main, Structure
  > AVIONICS 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 6-2-100
- [SDR FDEA202404300674](https://openairdocs.org/sdr/FDEA202404300674.md): Angle · cracked · Apr 30, 2024 · N685FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AVIONICS 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 6
- [SDR FDEA202404270762](https://openairdocs.org/sdr/FDEA202404270762.md): Fitting · cracked · Apr 27, 2024 · N685FE · Airbus A300F4605R · Cargo/Baggage Doors
  > THE 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 REPLACEMENT
- [SDR FDEA202308231478](https://openairdocs.org/sdr/FDEA202308231478.md): Unknown · unknown · Aug 23, 2023 · N685FE · Airbus A300* · Hydraulic Power System
  > A/C CAME INTO BLOCKS WITH RAT DEPLOYED. BOTH HANDLES IN COCKPIT HAVE COPPER WIRE STILL INSTALLED.
- [SDR FDEA202307301335](https://openairdocs.org/sdr/FDEA202307301335.md): Valve · failed · Jul 30, 2023 · N685FE · Airbus A300* · Hydraulic Power System
  > APPROACHING 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 OVE
- [SDR FDEA202304130641](https://openairdocs.org/sdr/FDEA202304130641.md): Unknown · unknown · Apr 13, 2023 · N685FE · Airbus A300* · Leading Edge Slat Control System
  > PDIS 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 TROUB
- [SDR FDEA202111182924](https://openairdocs.org/sdr/FDEA202111182924.md): Seat Track · gouged · Nov 18, 2021 · N685FE · Airbus A300* · Fuselage Structure (General)
  > MAIN 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.201
- [SDR FDEA202111142928](https://openairdocs.org/sdr/FDEA202111142928.md): Floor Panel · damaged · Nov 14, 2021 · N685FE · Airbus A300* · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA202111142902](https://openairdocs.org/sdr/FDEA202111142902.md): Floor Panel · damaged · Nov 14, 2021 · N685FE · Airbus A300* · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA202111142901](https://openairdocs.org/sdr/FDEA202111142901.md): Floor Panel · damaged · Nov 14, 2021 · N685FE · Airbus A300* · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA202111142900](https://openairdocs.org/sdr/FDEA202111142900.md): Floor Panel · damaged · Nov 14, 2021 · N685FE · Airbus A300* · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA202111112917](https://openairdocs.org/sdr/FDEA202111112917.md): None · gouged · Nov 11, 2021 · N685FE · Airbus A300* · Fuselage Structure (General)
  > MDCC 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.
- [SDR FDEA202111112894](https://openairdocs.org/sdr/FDEA202111112894.md): Seat Track · gouged · Nov 11, 2021 · N685FE · Airbus A300* · Fuselage Main, Structure
  > SEAT 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.
- [SDR FDEA202111102809](https://openairdocs.org/sdr/FDEA202111102809.md): None · worn · Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/Structures
  > N00399 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.
- [SDR FDEA202111102808](https://openairdocs.org/sdr/FDEA202111102808.md): None · worn · Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/Structures
  > N00398 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.
- [SDR FDEA202111102807](https://openairdocs.org/sdr/FDEA202111102807.md): None · worn · Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/Structures
  > N00397 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.
- [SDR FDEA202111102806](https://openairdocs.org/sdr/FDEA202111102806.md): None · worn · Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/Structures
  > N00396 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.
- [SDR FDEA202111102805](https://openairdocs.org/sdr/FDEA202111102805.md): None · worn · Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/Structures
  > N00395 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.
- [SDR FDEA202111102804](https://openairdocs.org/sdr/FDEA202111102804.md): None · worn · Nov 10, 2021 · N685FE · Airbus A300* · Standard Practices/Structures
  > N00394 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.
- [SDR FDEA202111082907](https://openairdocs.org/sdr/FDEA202111082907.md): None · unknown · Nov 8, 2021 · N685FE · Airbus A300* · Rudder Structure
  > AIRCRAFT 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 EXI
- [SDR FDEA202111082906](https://openairdocs.org/sdr/FDEA202111082906.md): None · unknown · Nov 8, 2021 · N685FE · Airbus A300* · Wing, Plate/Skin
  > AIRCRAFT 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 FA
- [SDR FDEA202111082905](https://openairdocs.org/sdr/FDEA202111082905.md): None · unknown · Nov 8, 2021 · N685FE · Airbus A300* · Wing, Plate/Skin
  > AIRCRAFT 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
- [SDR FDEA202111082879](https://openairdocs.org/sdr/FDEA202111082879.md): None · none · Nov 8, 2021 · N685FE · Airbus A300* · Wing, Control Surfaces
  > AIRCRAFT 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 APPROVED
- [SDR FDEA202111072893](https://openairdocs.org/sdr/FDEA202111072893.md): Floor Panel · damaged · Nov 7, 2021 · N685FE · Airbus A300* · Fuselage Floor Panel
  > AFT 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.
- [SDR FDEA202111072897](https://openairdocs.org/sdr/FDEA202111072897.md): Floor Panel · damaged · Nov 7, 2021 · N685FE · Airbus A300* · Fuselage Floor Panel
  > AFT 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.
- [SDR FDEA202111072896](https://openairdocs.org/sdr/FDEA202111072896.md): Floor Panel · damaged · Nov 7, 2021 · N685FE · Airbus A300* · Fuselage Floor Panel
  > AFT 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.
- [SDR FDEA202111072895](https://openairdocs.org/sdr/FDEA202111072895.md): Floor Panel · damaged · Nov 7, 2021 · N685FE · Airbus A300* · Fuselage Floor Panel
  > FWD 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.
- [SDR FDEA202111062878](https://openairdocs.org/sdr/FDEA202111062878.md): None · cracked · Nov 6, 2021 · N685FE · Airbus A300* · Wing, Control Surfaces
  > 2 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
- [SDR FDEA202111062877](https://openairdocs.org/sdr/FDEA202111062877.md): None · cracked · Nov 6, 2021 · N685FE · Airbus A300* · Wing, Control Surfaces
  > 2EA 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 STRINGERS
- [SDR FDEA202111062876](https://openairdocs.org/sdr/FDEA202111062876.md): None · cracked · Nov 6, 2021 · N685FE · Airbus A300* · Wing, Control Surfaces
  > 2EA 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 STRINGE
- [SDR FDEA2019102542746](https://openairdocs.org/sdr/FDEA2019102542746.md): Windshield · cracked · Oct 24, 2019 · N685FE · Airbus A300F4605R · Flight Compartment Windows
  > F/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 OK
- [SDR FDEA201908081814](https://openairdocs.org/sdr/FDEA201908081814.md): Valve · malfunctioned · Aug 8, 2019 · N685FE · Airbus A300F4605R · Engine Thrust Reverser
  > ON 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 78
- [SDR FDEA2019080971819](https://openairdocs.org/sdr/FDEA2019080971819.md): Regulator Valve · failed · Aug 7, 2019 · N685FE · Airbus A300F4605R · Engine Thrust Reverser
  > ON 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 DEACT
- [SDR FDEA2019060311204](https://openairdocs.org/sdr/FDEA2019060311204.md): Warning Message · false activation · Jun 1, 2019 · N685FE · Airbus A300F4605R · Door Warning System
  > MAIN 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.
- [SDR FDEA2019042650924](https://openairdocs.org/sdr/FDEA2019042650924.md): Floor Panel · cracked · Apr 25, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 241TJ FLOOR PANEL BROKEN FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.
- [SDR FDEA2019042650923](https://openairdocs.org/sdr/FDEA2019042650923.md): Floor Panel · broken · Apr 25, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 232GG FLOOR PANEL BROKEN FABRICATED A NEW FLOOR PANE IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIR.
- [SDR FDEA2019042540900](https://openairdocs.org/sdr/FDEA2019042540900.md): Seat Track · cracked · Apr 24, 2019 · N685FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 REPAIR
- [SDR FDEA2019042540899](https://openairdocs.org/sdr/FDEA2019042540899.md): Floor Panel · damaged · Apr 24, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOOR PANEL R532B113600000 IS DAMAGED FWD PIT FABRICATED NEW FLOOR PANEL R532B113600000 ON TRAVELER T19/1412584 IAW SRZ-25-005 MAJOR REPAIR
- [SDR FDEA2019042540898](https://openairdocs.org/sdr/FDEA2019042540898.md): Floor Panel · cracked · Apr 24, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT 262WF FLOOR PANEL CRACKED. FABRICATED FLOOR PANEL 262WF ON VT MAE TRAVELER T19/1411071 PER SRZ-25-005 CAT "A" MAJOR REPAIR
- [SDR FDEA2019042540893](https://openairdocs.org/sdr/FDEA2019042540893.md): Floor Panel · broken · Apr 24, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 242GJ FLOOR PANEL BROKEN FABRICATED 242GJ FLOOR PANEL ON VTMAE TRAVELER # T19/1411075 PER DWG SRZ -25-005 CAT "A" MAJOR REPAIR
- [SDR FDEA2019042540892](https://openairdocs.org/sdr/FDEA2019042540892.md): Floor Panel · broken · Apr 24, 2019 · N685FE · Airbus A300F4605R · Fuselage Floor Panel
  > MDCC 241NJ FLOOR PANEL BROKEN FABRICATED FLOOR PANEL 241NJ ON VTMAE TRAVELER # T19/1411077 PER DWG SRZ -25-005 CAT "A" MAJOR REPAIR

Next page: https://openairdocs.org/aircraft/N685FE/reports.md?page=2

## 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 = 'N685FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N685FE/reports

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