# Service difficulty reports: N686FE

A list on [N686FE](https://openairdocs.org/aircraft/N686FE.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 4 · 181 reports

- [SDR FDEA202402200191](https://openairdocs.org/sdr/FDEA202402200191.md): Autothrottle Sys · faulted · Feb 20, 2024 · N686FE · Airbus A300F4605R · Auto Throttle System
  > SHORTLY 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 THAT
- [SDR FDEA202402130157](https://openairdocs.org/sdr/FDEA202402130157.md): Power Supply · failed · Feb 13, 2024 · N686FE · Airbus A300F4605R · Emergency Lighting
  > DURING 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
- [SDR FDEA202304050564](https://openairdocs.org/sdr/FDEA202304050564.md): Seat · cracked · Apr 5, 2023 · N686FE · Airbus A300* · Flight Compartment Equipment
  > APPEARS 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 GOOD
- [SDR FDEA202208082051](https://openairdocs.org/sdr/FDEA202208082051.md): Skin · dented · Aug 8, 2022 · N686FE · Airbus A300F4605R · Trailing Edge Flaps
  > FOUND 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 &
- [SDR FDEA202208051895](https://openairdocs.org/sdr/FDEA202208051895.md): Dummy Rail · worn · Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FR54/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.
- [SDR FDEA202208051894](https://openairdocs.org/sdr/FDEA202208051894.md): Dummy Rail · worn · Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FR54/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.
- [SDR FDEA202208051893](https://openairdocs.org/sdr/FDEA202208051893.md): Seat Track · worn · Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FR54/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.
- [SDR FDEA202208051892](https://openairdocs.org/sdr/FDEA202208051892.md): None · worn · Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FR54/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.
- [SDR FDEA202208051891](https://openairdocs.org/sdr/FDEA202208051891.md): None · worn · Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FR38.2/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.
- [SDR FDEA202208051890](https://openairdocs.org/sdr/FDEA202208051890.md): None · worn · Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FR38.2/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.
- [SDR FDEA202208051889](https://openairdocs.org/sdr/FDEA202208051889.md): None · worn · Aug 5, 2022 · N686FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > FR38.2/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.
- [SDR FDEA202208021926](https://openairdocs.org/sdr/FDEA202208021926.md): None · none · Aug 2, 2022 · N686FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT 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 B
- [SDR FDEA202208021925](https://openairdocs.org/sdr/FDEA202208021925.md): None · none · Aug 2, 2022 · N686FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT 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 DET
- [SDR FDEA202208021924](https://openairdocs.org/sdr/FDEA202208021924.md): None · none · Aug 2, 2022 · N686FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT 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 DETERM
- [SDR FDEA202207282043](https://openairdocs.org/sdr/FDEA202207282043.md): Rib · cracked · Jul 28, 2022 · N686FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > 1EA 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
- [SDR FDEA202207282042](https://openairdocs.org/sdr/FDEA202207282042.md): Rib · cracked · Jul 28, 2022 · N686FE · Airbus A300B4605R · Wing, Rib/Bulkhead
  > 3EA 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 FLAP
- [SDR FDEA202207281842](https://openairdocs.org/sdr/FDEA202207281842.md): Floor Panel · damaged · Jul 28, 2022 · N686FE · Airbus A300* · Fuselage Floor Panel
  > FWD CARGO COMPT #131MG FLOOR PANEL WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005
- [SDR FDEA202207281841](https://openairdocs.org/sdr/FDEA202207281841.md): Floor Panel · damaged · Jul 28, 2022 · N686FE · Airbus A300* · Fuselage Floor Panel
  > FWD CARGO COMPT #131RG FLOOR PANEL WAS FOUND INSERT DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005
- [SDR FDEA202207272023](https://openairdocs.org/sdr/FDEA202207272023.md): Rib · cracked · Jul 27, 2022 · N686FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > 1EA 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 B
- [SDR FDEA202207272022](https://openairdocs.org/sdr/FDEA202207272022.md): Rib · cracked · Jul 27, 2022 · N686FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > 2EA 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 27
- [SDR FDEA202207272021](https://openairdocs.org/sdr/FDEA202207272021.md): Rib · cracked · Jul 27, 2022 · N686FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > 1EA 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 B
- [SDR FDEA202207272020](https://openairdocs.org/sdr/FDEA202207272020.md): Seat Track · corroded · Jul 27, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.2
- [SDR FDEA202207272019](https://openairdocs.org/sdr/FDEA202207272019.md): Seat Track · corroded · Jul 27, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.2
- [SDR FDEA202207271960](https://openairdocs.org/sdr/FDEA202207271960.md): Floor Support · corroded · Jul 27, 2022 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR FDEA202207262050](https://openairdocs.org/sdr/FDEA202207262050.md): Seat Track · none · Jul 26, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FOUND 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.
- [SDR FDEA202207262041](https://openairdocs.org/sdr/FDEA202207262041.md): Seat Track · none · Jul 26, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FOUND 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 AN
- [SDR FDEA202207262010](https://openairdocs.org/sdr/FDEA202207262010.md): Seat Track · none · Jul 26, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FOUND 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.203
- [SDR FDEA202207262009](https://openairdocs.org/sdr/FDEA202207262009.md): Seat Track · none · Jul 26, 2022 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > FOUND 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 CL
- [SDR FDEA202207261923](https://openairdocs.org/sdr/FDEA202207261923.md): Skin · unknown · Jul 26, 2022 · N686FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > AIRCRAFT 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 DETERMI
- [SDR FDEA202207212085](https://openairdocs.org/sdr/FDEA202207212085.md): None · none · Jul 21, 2022 · N686FE · Airbus A300F4605R · Standard Practices/Structures
  > THIS 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).
- [SDR FDEA202201140520](https://openairdocs.org/sdr/FDEA202201140520.md): Epsu · inoperative · Jan 14, 2022 · N686FE · Airbus A300F4605R · Emergency Lighting
  > MDIS 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
- [SDR FDEA202012033019](https://openairdocs.org/sdr/FDEA202012033019.md): Slide · detached · Dec 3, 2020 · N686FE · Airbus A300F4605R · Escape Slide
  > FOUND 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.
- [SDR FDEA202012023016](https://openairdocs.org/sdr/FDEA202012023016.md): Slide · detached · Dec 2, 2020 · N686FE · Airbus A300F4605R · Escape Slide
  > FOUND 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.
- [SDR FDEA2020071091483](https://openairdocs.org/sdr/FDEA2020071091483.md): Module · inoperative · Jul 9, 2020 · N686FE · Airbus A300F4605R · Fire Detection
  > NR 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.
- [SDR FDEA2020072311185](https://openairdocs.org/sdr/FDEA2020072311185.md): Wire Harness · malfunctioned · Jun 11, 2020 · N686FE · Airbus A300F4605R · Fire Detection
  > ON 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
- [SDR FDEA2020061211185](https://openairdocs.org/sdr/FDEA2020061211185.md): Fire Loop · faulted · Jun 11, 2020 · N686FE · Airbus A300F4605R · Fire Detection
  > ON 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
- [SDR FDEA202006111184](https://openairdocs.org/sdr/FDEA202006111184.md): Wire Harness · faulted · Jun 11, 2020 · N686FE · Airbus A300F4605R · Fire Protection System Wiring
  > DURING 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
- [SDR FDEA2020060531128](https://openairdocs.org/sdr/FDEA2020060531128.md): Pitot Line · obstructed · Jun 3, 2020 · N686FE · Airbus A300F4605R · Pitot/Static System
  > ABORTED 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 TES
- [SDR FDEA202001230211](https://openairdocs.org/sdr/FDEA202001230211.md): Spar · cracked · Jan 23, 2020 · N686FE · Airbus A300F4605R · Fuselage Main, Structure
  > INSPECTION 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 P
- [SDR FDEA202001230210](https://openairdocs.org/sdr/FDEA202001230210.md): Angle · cracked · Jan 23, 2020 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > INSPECTION 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 P
- [SDR FDEA202001160142](https://openairdocs.org/sdr/FDEA202001160142.md): Web · cracked · Jan 16, 2020 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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-
- [SDR FDEA202001160141](https://openairdocs.org/sdr/FDEA202001160141.md): Web · cracked · Jan 16, 2020 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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 A300-60
- [SDR FDEA202001160140](https://openairdocs.org/sdr/FDEA202001160140.md): Web · cracked · Jan 16, 2020 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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 A
- [SDR FDEA202001090081](https://openairdocs.org/sdr/FDEA202001090081.md): Floorbeam · cracked · Jan 9, 2020 · N686FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN 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 REPAIR
- [SDR FDEA202001090080](https://openairdocs.org/sdr/FDEA202001090080.md): Floorbeam · cracked · Jan 9, 2020 · N686FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN 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 RE
- [SDR FDEA202001090079](https://openairdocs.org/sdr/FDEA202001090079.md): Floorbeam · cracked · Jan 9, 2020 · N686FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN 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: 6-531
- [SDR FDEA202001090078](https://openairdocs.org/sdr/FDEA202001090078.md): Floorbeam · cracked · Jan 9, 2020 · N686FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN 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: 6-531
- [SDR FDEA201909142243](https://openairdocs.org/sdr/FDEA201909142243.md): Filter · odor · Sep 14, 2019 · N686FE · Airbus A300F4605R · Air Distribution System
  > PDIS 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 COMP
- [SDR FDEA2019032760734](https://openairdocs.org/sdr/FDEA2019032760734.md): Support · damaged · Mar 26, 2019 · N686FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > GEAR 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. LAN
- [SDR FDEA201807121693](https://openairdocs.org/sdr/FDEA201807121693.md): None · none · Dec 7, 2018 · N686FE · Airbus A300* · Fuselage Main, Longeron/Stringer
  > MAIN 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 AIRCRA

Next page: https://openairdocs.org/aircraft/N686FE/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 = 'N686FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N686FE/reports

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