# Service difficulty reports: N680FE

A list on [N680FE](https://openairdocs.org/aircraft/N680FE.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 5 · 219 reports

- [SDR FDEA202606280938](https://openairdocs.org/sdr/FDEA202606280938.md): Spoiler · delaminated · Jun 28, 2026 · N680FE · Airbus A300F4605R · Wing, Control Surfaces
  > LH 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 DELAMINATI
- [SDR FDEA202606280930](https://openairdocs.org/sdr/FDEA202606280930.md): Spoiler · delaminated · Jun 28, 2026 · N680FE · Airbus A300F4605R · Spoilers
  > RH 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 DELAMINATION
- [SDR FDEA202606240829](https://openairdocs.org/sdr/FDEA202606240829.md): Seat Track · damaged · Jun 24, 2026 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING 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
- [SDR FDEA202606240799](https://openairdocs.org/sdr/FDEA202606240799.md): Frame · damaged · Jun 24, 2026 · N680FE · Airbus A300F4605R · Fuselage Main, Frame
  > EXISTING 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-
- [SDR FDEA202606240798](https://openairdocs.org/sdr/FDEA202606240798.md): Pressure Deck · not reported · Jun 24, 2026 · N680FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING 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 R
- [SDR FDEA202606230797](https://openairdocs.org/sdr/FDEA202606230797.md): Seat Track · none · Jun 23, 2026 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING 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-
- [SDR FDEA202606230796](https://openairdocs.org/sdr/FDEA202606230796.md): Crossbeam · not reported · Jun 23, 2026 · N680FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING REPAIR ON MAIN DECK CROSSBEAM FR20,Y1959~Y2462 REQUIRES EVALUATION FOR CONFORMITY.
- [SDR FDEA202606190795](https://openairdocs.org/sdr/FDEA202606190795.md): Seat Track · no discrepancy · Jun 19, 2026 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING 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.
- [SDR FDEA202606190794](https://openairdocs.org/sdr/FDEA202606190794.md): Seat Track · no discrepancy · Jun 19, 2026 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK FR36-FR38.1,Y450 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK FR36-FR38.1,Y450 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH SRM 53-10-16, FIG 203.
- [SDR FDEA202606190793](https://openairdocs.org/sdr/FDEA202606190793.md): Crossbeam · no discrepancy · Jun 19, 2026 · N680FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING REPAIR ON MAIN DECK CROSSBEAM FR38,Y0~Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CROSSBEAM FR38, Y0~Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5314-69630
- [SDR FDEA202606180929](https://openairdocs.org/sdr/FDEA202606180929.md): Flap · cracked · Jun 18, 2026 · N680FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP FOUND 1EA CRACK AT RIB26 FIRST FASTENER BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA 6-5750-T0362465 A P2, EA TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP, CRACK IN UPPER FLANGE OF RIB 26 & 27. REMOVED THE EXISTING DOUBLER ON BOTTOM S
- [SDR FDEA202606160867](https://openairdocs.org/sdr/FDEA202606160867.md): Stiffener · cracked · Jun 16, 2026 · N680FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE, CROSSBEAM ATTACHED, STIFFENER CRACKED, AT FR54.3, BETWEEN -Y450 AND -Y953 REPAIRED THE CRACK AT MAIN DECK CARGO FLOOR SUPPORT STRUCTURE CROSSBEAM ATTACHED STIFFENER AT FR54.3, BETWEEN -Y450 AND -Y953 PER
- [SDR FDEA202606140921](https://openairdocs.org/sdr/FDEA202606140921.md): Door · none · Jun 14, 2026 · N680FE · Airbus A300F4605R · Standard Practices/Structures
  > 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 DOOR/HYD SYS - DETAILED VISUAL INSPECTION O
- [SDR FDEA202602180227](https://openairdocs.org/sdr/FDEA202602180227.md): Safety Wire · wrong part · Feb 18, 2026 · N680FE · Airbus A300F4605R · Escape Slide
  > L1 DOOR EJECTOR BAG RELEASE CABLE/INFLATOR ACTUATING ARM CLIP HAD IMPROPER BREAKAWAY COPPER WIRE INSTALLED. INSTALLED CORRECT CAD PLATED BREAK AWAY WIRE MS20995CY AS PER CMM AND E.A. LISTED ABOVE FOR THE L1 DOOR SLIDE SERIAL NUMBER 0443TH EJECTOR BAG RE
- [SDR FDEA202510292105](https://openairdocs.org/sdr/FDEA202510292105.md): Battery · inoperative · Sep 10, 2025 · N680FE · Airbus A300F4605R · Emergency Lighting
  > ON POSTFLIGHT INSPECTION FOUND EMERGENCY LIGHTING TEST INOP. REMOVED AND INSTALLED NEW POWER SUPPLY UNIT AS REQUIRED. OPS CHECKED GOOD.
- [SDR FDEA202409191329](https://openairdocs.org/sdr/FDEA202409191329.md): Fitting · corroded · Sep 19, 2024 · N680FE · Airbus A310300 · Wing Main, Frame Structure
  > CORROSION FOUND BETWEEN BUSHES 'D" AND "E" DURING RH RIB 5 INSPECTION COMPLIED WITH FED EX EA 6-571-T0316490 PT2 AND R57240425. MAJOR REPAIR. EA 6-5710- T0316490 WINGS - BASIC WING STRUCTURE - CORROSION REPAIR OF RIB 5 FWD LUG RH. MPN A57240810214.
- [SDR FDEA202406130805](https://openairdocs.org/sdr/FDEA202406130805.md): Pitot Tube · fod · Jun 13, 2024 · N680FE · Airbus A300F4605R · Pitot/Static System
  > DISCREPANCY BETWEEN AIRSPEED ON CAPT & FO. AT CRUISE.02 MACH & ABOUT 8-10 KNOT DISCREPANCY AT FL 340. ALSO RECEIVED A MOMENTARY OVERSPEED WARNING AT FL 340 IN SMOOTH AIR, CAPT SHOWED.80 MACH & FO SHOWED.82. FO AIRSPEED SEEMS CLOSER TO STDBY AIRSPEED ON BO
- [SDR FDEA202403140333](https://openairdocs.org/sdr/FDEA202403140333.md): Electronic Unit · faulted · Mar 14, 2024 · N680FE · Airbus A300F4605R · Pitot/Static Anti-Ice System
  > DURING CLIMB RECEIVED FO PITOT HEAT FAULT. COMPLIED WITH ECAM. ENTERED ICING CONDITIONS. RECEIVED NI MODE 1 AND MODE 2 FAULT. UNRELIABLE AIRSPEED. DETERMINED DURING LEVEL FLIGHT THAT IT WAS ON THE FO S SIDE. DESCENDED TO GET OUT OF THE ICING CONDITIONS. LOST
- [SDR FDEA202401120071](https://openairdocs.org/sdr/FDEA202401120071.md): Web · cracked · Jan 12, 2024 · N680FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FR47 -Y953 ~ -Y1456 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB AT MAIN DECK FR47 -Y953 ~ -Y1456 UNDERFLOOR AREA PER A300- 600F SRM53-15-15-201-C2 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI5
- [SDR FDEA202401120070](https://openairdocs.org/sdr/FDEA202401120070.md): Web · cracked · Jan 12, 2024 · N680FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FR47 Y953-Y1456 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB AT MAIN DECK FR47 Y953-Y1456 UNDERFLOOR AREA PER A300- 600F SRM53-15-15-201-C2 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-
- [SDR FDEA202401120069](https://openairdocs.org/sdr/FDEA202401120069.md): Web · cracked · Jan 12, 2024 · N680FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK FR47 Y0-Y450 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB AT MAIN DECK FR47 Y0-Y450 UNDERFLOOR AREA PER A300-600F SRM53-15-15-201-C2 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002-
- [SDR FDEA202302270346](https://openairdocs.org/sdr/FDEA202302270346.md): Landing Gear · failed · Feb 27, 2023 · N680FE · Airbus A300F4605R · Trailing Edge Flap Control System
  > MDIS 680 27-50 1704 27FEB23 DEN OPEN U THE #7 TIRE THROWN TREAD AND DAMAGED THE R/H INBOARD FLAP. SEE ATTACHMENTS TIRE R&R ON WRI 34-42/1703 TIRE R&R'D DAMAGE WRI'S 53-30/1710, 1714 53-40/1708, 1709,1711 53-50/1706 1707,1712,
- [SDR FDEA202205091166](https://openairdocs.org/sdr/FDEA202205091166.md): Light · failed insp · May 9, 2022 · N680FE · Airbus A300F4605R · Emergency Lighting
  > MDIS 680 33-50 0976 07MAY22 PIT OPEN U PER A-CHECK, EMERGENCY LIGHT OPS TEST FAILED BITE-CHECK. DUPLICATE SDR SEE 22-1140
- [SDR FDEA202205071140](https://openairdocs.org/sdr/FDEA202205071140.md): None · none · May 7, 2022 · N680FE · Airbus A300* · Emergency Lighting
  > MDIS 680 33-50 0976 07MAY22 PIT OPEN U PER A-CHECK, EMERGENCY LIGHT OPS TEST FAILED BITE-CHECK. FACT 10MAY22 23:37 TUL REPLACED BURNED OUT BULBS IN DOOR EXIT SIGNS, (3 IN
- [SDR FDEA202108272171](https://openairdocs.org/sdr/FDEA202108272171.md): Seat Track · damaged · Aug 27, 2021 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > REMOVE LOBE DAMAGED SEAT TRACK (AT LS Y1995 TRACK) FROM SPLICE CENTER BETWEEN FR26/FR27 TO FR33/FR34 0000392279: ORTEN, JONATHAN C - 30-AUG-2021 18:25 REPLACED SEAT TRACK SECTION REFERENCE A300-310 SRM 51-14-16---------- 0000638304: LONEY, RANDOLPH C - 3
- [SDR FDEA202107171837](https://openairdocs.org/sdr/FDEA202107171837.md): Frame · corroded · Jul 17, 2021 · N680FE · Airbus A300F4605R · Fuselage Main, Frame
  > 1 EA CORROSION INDICATION WAS FOUND ON THE HOLE "N" OF RH FRAME 47. ACCOMPLISHED THE TASK I.A.W A300-600F EA WORK CARD NO:T6-5710-T0362495 P1, SEQ NO:001066
- [SDR FDEA202107171836](https://openairdocs.org/sdr/FDEA202107171836.md): Angle · gouged · Jul 17, 2021 · N680FE · Airbus A300F4605R · Leading Edge Devices
  > RH WING L/E KRUEGER BOX O/B SIDE RIB NEAR PNEUMATIC DUCT AREA GOT A GOUGE REINFORCED WITH A REPAIR ANGLE I.A.W A300-600F EA WORK CARD NO: T6-5710-T0362830 P1, SEQ NO:001065
- [SDR FDEA202107161835](https://openairdocs.org/sdr/FDEA202107161835.md): Frame · cracked · Jul 16, 2021 · N680FE · Airbus A300F4605R · Fuselage Main, Frame
  > 1EA CRACK INDICATION WAS FOUND ON THE HOLE "J" OF FR47,STR24L-STR25L. THE CRACK INDICATION IS OVER 100%FSH. ACCOMPLISHED THE WORK:FR47,STR24L-STR25L HOLE ''J'' GOUGE REPAIR - THIS EA DEVIATES FROM EO 6-5310-7-5017 (AIRBUS SERVICE BULLETIN) I.A.W. A300-600F
- [SDR FDEA202107121841](https://openairdocs.org/sdr/FDEA202107121841.md): Fitting · cracked · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Main, Attach Fittings
  > 1EA CRACK INDICATION WAS FOUND ON THE HOLE "N" OF FR47 SPLICE FITTING BETWEEN STR24&26,LH. THE CRACK INDICATION IS OVER 100%FSH. ACCOMPLISHED THE WORK CARD:INSPECTION HOLES IN FUSELAGE FRAME47 SPLICE FITTING BETWEEN STR24&26,LH/RH, AIRBUS SB A300-53-6123
- [SDR FDEA202107121734](https://openairdocs.org/sdr/FDEA202107121734.md): Floor Panel · damaged · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #241WH FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
- [SDR FDEA202107121733](https://openairdocs.org/sdr/FDEA202107121733.md): Floor Panel · damaged · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #242GJ FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
- [SDR FDEA202107121732](https://openairdocs.org/sdr/FDEA202107121732.md): Floor Panel · damaged · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #242EF FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
- [SDR FDEA202107121731](https://openairdocs.org/sdr/FDEA202107121731.md): Floor Panel · damaged · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #242NH FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
- [SDR FDEA202107121730](https://openairdocs.org/sdr/FDEA202107121730.md): Floor Panel · damaged · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #241AK FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
- [SDR FDEA202107121729](https://openairdocs.org/sdr/FDEA202107121729.md): Floor Panel · damaged · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #151VF LOOR PANEL OF LOWER AFT CARGO COMPARTMENT WAS FOUND EDGE DAMAGED WITH MARK 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 FDEA202107121728](https://openairdocs.org/sdr/FDEA202107121728.md): Floor Panel · damaged · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #151XF LOOR PANEL OF LOWER AFT CARGO COMPARTMENT WAS FOUND EDGE DAMAGED WITH MARK 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 FDEA202107121727](https://openairdocs.org/sdr/FDEA202107121727.md): Floor Panel · damaged · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #132NG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND EDGE DAMAGED WITH MARK 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 FDEA202107121726](https://openairdocs.org/sdr/FDEA202107121726.md): Floor Panel · damaged · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #132MG FLOOR PANEL OF LOWER FWD CARGO COMPARTMENT WAS FOUND EDGE DAMAGED WITH MARK 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 FDEA202107121725](https://openairdocs.org/sdr/FDEA202107121725.md): Floor Panel · damaged · Jul 12, 2021 · N680FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #231CF FLOOR PANEL OF MDC COMPARTMENT WAS FOUND EDGE BROKEN ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600F SRM 53-10-20-201, PARA. 8A, P. 201- 205, FIG. 201.
- [SDR FDEA202107101716](https://openairdocs.org/sdr/FDEA202107101716.md): Structure · worn · Jul 10, 2021 · N680FE · Airbus A300F4605R · Spoilers
  > RH WING #2 SPOILER O/B EDGE FWD SECTION WORN ACCOMPLISHED THE TASK I.A.W A300-600F EA WORK CARD NO: T6-5750-T0362676 P1,SEQ NO:001059.
- [SDR FDEA202107101719](https://openairdocs.org/sdr/FDEA202107101719.md): Rib · cracked · Jul 10, 2021 · N680FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA CRACK (12MM) WAS FOUND AT R/H WING CENTER FLAP RIB 27 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE WORK: RH CENTER FLAP CRACK IN UPPER FLANGE OF RIB 27 AT STRINGERS 2.8 - ALI 575306-01(FAA AD 2019-21-01) I.A.W. A300-600 EA NO: 6-5750-T0362465
- [SDR FDEA202107101718](https://openairdocs.org/sdr/FDEA202107101718.md): Support · chafed · Jul 10, 2021 · N680FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > NO 1 PYLON AFT FAIRING SUPPORT WEB GOT CHAFING AT RIB 19 O/B ACCOMPLISHED LH PYLON AFT FAIRING SPAR AT RIB 19 OUTBOARD FLANGE WEAR DAMAGE REPAIR INSTRUCTION I.A.W EA: #6-5450-T0362605 P1, SEQ NO: 001050
- [SDR FDEA202107101717](https://openairdocs.org/sdr/FDEA202107101717.md): Skin · delaminated · Jul 10, 2021 · N680FE · Airbus A300F4605R · Spoilers
  > 2EA DELAMINATIONS WERE FOUND. AREA 1 (20CM2) IS NEAR I/B HINGE ARM OF RH SPOILER 4 LOWER SKIN. AREA 2 (17.5CM2) IS NEAR O/B HINGE ARM OF RH SPOILER 4 LOWER SKIN. ACCOMPLISHED RH #4 SPOILER LOWER SKIN DELAMINATION REPLACEMENT OF REINFORCEMENT PLIES NEAR C
- [SDR FDEA202107091708](https://openairdocs.org/sdr/FDEA202107091708.md): Channel · cracked · Jul 9, 2021 · N680FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous Structure
  > #1 ENG LH CORE COWL INNER LAST FRAME WAS FOUND CRACK ACCOMPLISHED THE HAT FRAME REPAIR I.A.W. GOODRICH GE CF6-80C2 A5F CMM 71-13-31 REPAIR NO.1, P. 6001-6003.
- [SDR FDEA2020061681154](https://openairdocs.org/sdr/FDEA2020061681154.md): Adapter · cracked · Jun 8, 2020 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ADAPTER AT 3L ID C840 HAS LOBE DAMAGE, RESTRAINT REMOVED, SEE WRI 25-50/8938. NO OTHER DAMAGE NOTED. INSTALLED SEAT TRACK ADAPTER REF DWG A53781936.
- [SDR FDEA2020061081154](https://openairdocs.org/sdr/FDEA2020061081154.md): Adapter · damaged · Jun 8, 2020 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK ADAPTER AT 3L ID C840 HAS LOBE DAMAGE, RESTRAINT REMOVED, SEE WRI 25-50/8938. NO OTHER DAMAGE NOTED.
- [SDR FDEA201901290224](https://openairdocs.org/sdr/FDEA201901290224.md): Accumulator · failed · Jan 29, 2019 · N680FE · Airbus A300F4605R · Landing Gear Brake System
  > ON APPROACH, LT SIDE BRAKE PRESURE GAGE READS 500 LBS. RIGHT SIDE 0 LBS. DECLARED EMERGENCY IN CASE LT BRAKE WAS STICKING. LT YELLOW SYSTEM BRAKE PRESURE INDICATOR. PARKING BRAKE ACCUM LOW, WHILE ATEMPTING TO SERVICE FLUID WAS COMING OUT OF SERVICE PORT. FOUND
- [SDR FDEA201901220190](https://openairdocs.org/sdr/FDEA201901220190.md): Adapter · damaged · Jan 22, 2019 · N680FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MCD ADAPTER FR58 L/H DAMAGED. REMOVED AND INSTALLED NEW ADAPTER IAW SRM 51-40-21, CAT A AND MAJOR REPAIR.
- [SDR FDEA201901220191](https://openairdocs.org/sdr/FDEA201901220191.md): Adapter · damaged · Jan 22, 2019 · N680FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MCD FLOOR ADAPTER FR59 LT DAMAGED. REMOVED AND INSTALLED NEW ADAPTER FR59 IAW SRM 51-40-21, CAT A AND MAJOR REPAIR.
- [SDR FDEA201901190183](https://openairdocs.org/sdr/FDEA201901190183.md): Seat Track · corroded · Jan 19, 2019 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MDCC BET FR59 ANF FR60 AT Y "0" SEAT TRACK HAS NICKS, GOUGES AND SCRATCHES. 91-053 REMOVED DAMAGE SECTION FROM SEAT TRACK Y 0 AT FRAME 58-50 LT SIDE ON MDCC AND FABRICATED REPAIR SEAT TRACK SPLICES PER SRM SRM 51-10-16, INSTALLED REPAIR SEAT TRACK SPLICES FROM

Next page: https://openairdocs.org/aircraft/N680FE/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 = 'N680FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N680FE/reports

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