# Service difficulty reports: N679FE

A list on [N679FE](https://openairdocs.org/aircraft/N679FE.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 · 176 reports

- [SDR FDEA202607301074](https://openairdocs.org/sdr/FDEA202607301074.md): Restraint · broken · Jul 30, 2026 · N679FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN CARGO DECK RESTRAINT MC1487 IN 8L HAS A BROKEN TIP. REMOVED DAMAGED RESTRAINT FROM AIRCRAFT COAT CLOSET AND SHIPPED FOR REPAIR. AIRCRAFT HAS SEAT TRACK DAMAGE AND FLOOR PANEL DAMAGE AT RESTRAINT ATTACH POINTS AND WILL REQUIRE SHEETMETAL REPAIR PRIOR
- [SDR FDEA202606200788](https://openairdocs.org/sdr/FDEA202606200788.md): Cvr · malfunctioned · Jun 20, 2026 · N679FE · Airbus A300F4605R · Audio/Video Monitoring
  > CVR WOULD NOT TEST PROPERLY DURING PREFLIGHT. RELEASED FOR SERVICE PER MEL: 23-71-01 CATEGORY: A EXPIRATION: 23JUN26 MEL 23-71-01: CVR - INOP.AMM: 23-71-00-05 PERFORMED ADJ/TEST OF CVR IAW AMM 23-71-00-5 AND OPS CHECK WAS GOOD. NO FAULT FOUND.
- [SDR FDEA202602190245](https://openairdocs.org/sdr/FDEA202602190245.md): Safety Wire · wrong part · Feb 19, 2026 · N679FE · Airbus A300F4605R · Emergency Equipment
  > THE R1 DOOR SLIDE EJECTOR BAG INFLATOR VALVE ACTUATING ARM HAS THE INCORRECT BREAKAWAY SAFETY WIRE INSTALLED. FOUND WHILE ACCOMPLISHING F.E.A. 6-2560-F0386375 REV A. FACT 19FEB26 22:10 MEM AMM: 25-61-21-04 FEA: FEA 6-2560-F0386375 INSTALLED THE CORRE
- [SDR FDEA202602190243](https://openairdocs.org/sdr/FDEA202602190243.md): Safety Wire · wrong part · Feb 19, 2026 · N679FE · Airbus A300F4605R · Emergency Equipment
  > THE L1 DOOR SLIDE EJECTOR BAG INFLATOR VALVE ACTUATING ARM HAS THE INCORRECT BREAKAWAY SAFETY WIRE INSTALLED. FOUND WHILE ACCOMPLISHING F.E.A. 6-2560-F0386375 REV A. AMM: 25-61-20-05-01 EA: 6-2560-F0386375 REV A PART 1 INSTALLED CAD- PLATED COPPER SAFETY
- [SDR FDEA202509221760](https://openairdocs.org/sdr/FDEA202509221760.md): Fitting · not reported · Sep 22, 2025 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > 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 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION
- [SDR FDEA202509061737](https://openairdocs.org/sdr/FDEA202509061737.md): Repair · none · Sep 6, 2025 · N679FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > EXISTING DOUBLER REPAIR ON EXTERIOR SKIN BETWEEN FR 83 & FR84, STRINGER 39R & 42R REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF THE REPAIR CONFORMS TO FAA APPROVED DATA. REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH SRM 53-10-12 FIG.208. EO
- [SDR FDEA202509051621](https://openairdocs.org/sdr/FDEA202509051621.md): Door · cracked · Sep 5, 2025 · N679FE · Airbus A300F4605R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR23 AND FR24 FOUND CRACK SIGNAL ON 3EA FASTENER HOLES COMPLIED WITH EA: 6-5230-T0384815 P1. TITLE: DOORS - CARGO DOOR/HYD SYS - CRACKED HOLES ON MAIN DECK CARGO DOOR UPPER LONGERON. REPAIRED THE MAIN DECK CARGO
- [SDR FDEA202508291580](https://openairdocs.org/sdr/FDEA202508291580.md): Seat Track · none · Aug 29, 2025 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y953 BETWEEN FR47 AND FR49 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y953 BETWEEN FR47 AND FR49 WAS EVALUATED AND FOUND IN CONFORMITY WITH EA 6-5310-69677 A. TITLE: FUSELA
- [SDR FDEA202508291566](https://openairdocs.org/sdr/FDEA202508291566.md): Skin · delaminated · Aug 29, 2025 · N679FE · Airbus A300F4605R · Spoilers
  > RH WING #3 SPOILER CENTER I/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 43 MM*25MM, DEPTH: 1.2MM COMPLIED WITH EA: 6-5750-T0384693 P1. TITLE: WING - FLIGHT SURFACES - RT NR 3 SPOILER CENTER HINGE ARM AREA DELAMINATION. REPAIRED THE RT WING NR 3 SPOIL
- [SDR FDEA202508291565](https://openairdocs.org/sdr/FDEA202508291565.md): Flap · misrepaired · Aug 29, 2025 · N679FE · Airbus A300F4605R · Trailing Edge Flaps
  > EXISTING REPAIR ON RH WING OUTER FLAP LEADING EDGE SKIN BETWEEN RIB14 AND RIB17 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH WING OUTER FLAP LEADING EDGE SKIN BETWEEN RIB14 AND RIB17 WAS EVALUATED & FOUND NOT IN CONFORMITY WITH SRM 57-50-0
- [SDR FDEA202508271583](https://openairdocs.org/sdr/FDEA202508271583.md): Floor Support · none · Aug 27, 2025 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > EXISTING REPAIR ON MAIN DECK FLOOR SUPPORT AT -Y1959 BETWEEN FR12A AND FR18 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK FLOOR SUPPORT AT -Y1959 BETWEEN FR12A AND FR18 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53612213(ISSUE:
- [SDR FDEA202508261556](https://openairdocs.org/sdr/FDEA202508261556.md): Seat Track · damaged · Aug 26, 2025 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y0 BETWEEN FR58 AND FR62 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y0 BETWEEN FR58 AND FR62 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-16-201 FIG.201. BUT
- [SDR FDEA202508261539](https://openairdocs.org/sdr/FDEA202508261539.md): Seat Track · worn · Aug 26, 2025 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK AT FR63 -Y2462 WORN REPAIRED THE MAIN DECK WORN SEAT TRACK AT FR63 -Y2462 PER A300-600F SRM53-10-16-201 FIG.201. THIS IS CATEGORY Ï¿½AÏ¿½ REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100.
- [SDR FDEA202508261538](https://openairdocs.org/sdr/FDEA202508261538.md): Web · cracked · Aug 26, 2025 · N679FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK UNDERFLOOR WEB CRACKED AT FR47 BETWEEN Y0 AND -Y450 REPAIRED THE CRACKED WEB IN MAIN DECK UNDERFLOOR AT FR47 BETWEEN Y0 AND -Y450 PER A300-600F SRM53-15-15-201-C2. THIS IS CATEGORY "B" REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-60
- [SDR FDEA202508231555](https://openairdocs.org/sdr/FDEA202508231555.md): Repair · misrepaired · Aug 23, 2025 · N679FE · Airbus A300F4605R · Cargo/Baggage Doors
  > EXISTING REPAIR ON FWD CARGO DOOR INNER SKIN LOWER EDGE BETWEEN FR21A AND FR22A REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FWD CARGO DOOR INNER SKIN LOWER EDGE BETWEEN FR21A AND FR22A WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600F
- [SDR FDEA202508211582](https://openairdocs.org/sdr/FDEA202508211582.md): Seat Track · none · Aug 21, 2025 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y953 BETWEEN FR57 AND FR57.3 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y953 BETWEEN FR57 AND FR57.3 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-16-201 FIG.
- [SDR FDEA202508211581](https://openairdocs.org/sdr/FDEA202508211581.md): Seat Track · none · Aug 21, 2025 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y953 BETWEEN FR26 AND FR30 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT -Y953 BETWEEN FR26 AND FR30 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-16-201 FIG.20
- [SDR FDEA202508191503](https://openairdocs.org/sdr/FDEA202508191503.md): Floorbeam · cracked · Aug 19, 2025 · N679FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN Y1456 AND Y1959 REPAIRED THE CRACKED CROSSBEAM AT MAIN DECK CARGO COMPARTMENT AT FR64 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 PARA.14. THIS IS CATEGORY "A" REPA
- [SDR FDEA202508191502](https://openairdocs.org/sdr/FDEA202508191502.md): Door Frame · cracked · Aug 19, 2025 · N679FE · Airbus A300F4605R · Fuselage Main, Structure
  > RH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 1EA CRACK REPLACED THE RH FWD PAX DOOR CRACKED FRAME SEGMENT AT FR14C WITH FABRICATED PART PER A300-600F SRM51-40-21 AND DWG: F52181299(ISSUE: G). RSC TRACKING EA: 6-5210- T0384786 RAISED AND ACCOMPLISHED. TITLE:
- [SDR FDEA202407311077](https://openairdocs.org/sdr/FDEA202407311077.md): Fitting · cracked · Jul 31, 2024 · N679FE · Airbus A300F4605R · Fuselage Main, Structure
  > DURING UT INSPECTION OF LH FR40 FWD, LOWER OUTBOARD RADUIS BETWEEN STGR 32L AND STGR 33L. CRACK INDICATION NOTED ON FASTENER HOLE AT 6:O'CLOCK POSITION. REPAIRED LH FR40 FWD LOWER OUTBOARD RADIUS BETWEEN STGR 32L AND STGR 33L PER REPAIR DRAWING 21R53810798
- [SDR FDEA202407311076](https://openairdocs.org/sdr/FDEA202407311076.md): Fitting · cracked · Jul 31, 2024 · N679FE · Airbus A300F4605R · Fuselage Main, Structure
  > DURING HFEC AND UT INSPECTION OF RH FR40 FWD, LOWER OUTBOARD RADIUS BETWEEN STGR 32R AND STGR 33R. CRACK INDICATION NOTED ON AREA "A" (FASTENER HOLE) AT 6 O'CLOCK POSITION. REPAIRED RH FR40 FWD LOWER OUTBOARD RADIUS BETWEEN STGR 32R AND STGR 33R PER REPA
- [SDR FDEA202305110849](https://openairdocs.org/sdr/FDEA202305110849.md): Crossbeam · cracked · May 11, 2023 · N679FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC FLOOR CROSSBEAM FWD STIFFENER CRACKED AT FR31,BTW -Y450 - -Y953. PERFORMED THE REPAIR ON MDCC FLOOR CROSSBEAM AT FR30,BTW -Y450 - -Y953 AS PER A300- 600F SRM 53-10-15-201 FIGURE 212 SHEET 1, SHEET 2 AND FEDEX EA:6-5310-T0374310 P1,TITLE:FUSELAGE - MAI
- [SDR FDEA202305110848](https://openairdocs.org/sdr/FDEA202305110848.md): Crossbeam · cracked · May 11, 2023 · N679FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC FLOOR CROSSBEAM FWD STIFFENER CRACKED AT FR30,BTW -Y450 - -Y953. PERFORMED THE REPAIR ON MDCC FLOOR CROSSBEAM AT FR30,BTW -Y450 - -Y953 AS PER A300- 600F SRM 53-10-15-201 FIGURE 212 SHEET 1, SHEET 2 AND FEDEX EA:6-5310-T0374310 P1,TITLE:FUSELAGE - MAI
- [SDR FDEA202305110847](https://openairdocs.org/sdr/FDEA202305110847.md): Crossbeam · cracked · May 11, 2023 · N679FE · Airbus A300F4605R · Fuselage Main, Structure
  > MDCC FLOOR CROSSBEAM FWD STIFFENER CRACKED AT FR32,BTW -Y450 - -Y953. PERFORMED THE REPAIR ON MDCC FLOOR CROSSBEAM AT FR32,BTW -Y450 - -Y953 AS PER A300- 600F SRM 53-10-15-201 FIGURE 212 SHEET 1, SHEET 2 AND FEDEX EA:6-5310-T0374312 P1,TITLE:FUSELAGE - MAIN
- [SDR FDEA202302160278](https://openairdocs.org/sdr/FDEA202302160278.md): Jackscrew · failed · Feb 16, 2023 · N679FE · Airbus A300F4605R · Leading Edge Slat Control System
  > PDIS 679 27-80 1336 16FEB23 LAX OPEN U SLATS SYS 1 AND 2 FAULT ON CONFIGURING APPROX 4000 FT, 220 KNOTS, WITH NO ASSOCIATED SFPI LIGHT. PER ECAM CYCLED SLAT LEVER, THEY REMAINED IN THE UP POSITION. FOLLOWED THE QRH PERFORMED UNEVENTFUL NO S
- [SDR FDEA202106171561](https://openairdocs.org/sdr/FDEA202106171561.md): Engine · failed · Jun 17, 2021 · N679FE · Airbus A300F4605R · Turbine Engine Oil System
  > AT CRUISE ECAM INDICATION OF OIL FILTER CLOG FOR NR 1 ENGINE. PROCEEDED IAW ECAM AND SHUT THE MOTOR DOWN AFTER THREE MINUTES UNSUCCESSFULLY TO GET THE WARNING TO EXTINGUISH. RETURN TO KAFW FOR UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING. APPROXIMATELY 3
- [SDR FDEA202101140098](https://openairdocs.org/sdr/FDEA202101140098.md): Actuator · failed · Jan 14, 2021 · N679FE · Airbus A300F4605R · Landing Gear Actuator
  > (WRI 32-30/9393) MAINT TEST FLIGHT: DURING REFLY FOR MANUAL GEAR EXT AIRSPEED 180 KTS FL 20 (L) MLG DID NOT EXTEND FOR 76 SECONDS. RIGHT MLG EXTENDED AFTER 16 SEC AND 15 SEC FOR NLG. TOWER CONFIRMED ALL GEAR DOWN. ALSO SYSTEM 2 3 CONFIRMING GEAR DOWN. AFTE
- [SDR FDEA202012243206](https://openairdocs.org/sdr/FDEA202012243206.md): Seat Track · cracked · Dec 24, 2020 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK FLOOR STRUCTURE SEAT TRACK CRACKED AND RIVETS SHEARED STA Y1959, FR 20 TO FR 21. COMPLIED WITH EA 6-5310-T0358314 PT1 FUSELAGE-MAINFRAME-MCD Y1959 SEAT TRACK CRACK BETWEEN FR 19 AND FR 20 REPAIR. MAJOR REPAIR.
- [SDR FDEA202012183187](https://openairdocs.org/sdr/FDEA202012183187.md): Web · damaged · Dec 18, 2020 · N679FE · Airbus A300F4605R · Horizontal Stabilizer Structure
  > DURING AGING ASSESSMENT EMPENNAGE ACCESS TANK 312AR BETWEEN FR 85 TO FR 86, STRINGER 33R, WEB FLANGE WAS FOUND TO BE UNSERVICEABLE. REMOVED AND REPLACED WEB FLANGE, IAW SRM 51-40-21. PART FABBED ON TRAVELER T20/1525932. PART NR FX-A53986750-206 PART MARKE
- [SDR FDEA202012153168](https://openairdocs.org/sdr/FDEA202012153168.md): Skin · cracked · Dec 15, 2020 · N679FE · Airbus A300F4605R · Wing, Plate/Skin
  > RT WING CENTER TOP SKIN AND RIB FLANGE-SDI TWO CRACKS FOUND ON RIB 21 AND 26, AS MARKED ALSO FR 27. FOUND NO CRACK NOTED ON RIB 21, PER NTM 51-10-08. REPAIRED 2 EA CRACKS ON RIB 27 AND RIB 26 OF RT WING CENTER FLAP, IAW SRM 57-50-00 FIG 205 AND FIG 206. SUP
- [SDR FDEA202012103118](https://openairdocs.org/sdr/FDEA202012103118.md): Floorboard · cracked · Dec 10, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131MG HAS CRACK. FABRICATED FLOOR PANEL 131MG ON VTMAE TRAVELER NR T20/1525251, IAW DWG SRZ-25-005R. CLASSIFIED AS CAT A AND MAJOR REPAIR.
- [SDR FDEA202012103117](https://openairdocs.org/sdr/FDEA202012103117.md): Floorboard · cracked · Dec 10, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131NG HAS CRACK. FABRICATED FLOOR PANEL 131NG ON VTMAE TRAVELER T20/1524954, IAW DWG SRZ-25-005R. CLASSIFIED AS CAT A AND MAJOR REPAIR.
- [SDR FDEA202012103116](https://openairdocs.org/sdr/FDEA202012103116.md): Floorboard · damaged · Dec 10, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > FLOORBOARD 151TF DAMAGED. FABRICATED FLOOR PANEL 151TF ON VTMAE TRAVELER T20/1525286, IAW DWG SRZ-25-005R. CLASSIFIED AS CAT A AND MAJOR REPAIR.
- [SDR FDEA202012103115](https://openairdocs.org/sdr/FDEA202012103115.md): Floorboard · cracked · Dec 10, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL 131SG HAS CRACK. FABRICATED FLOOR PANEL ON VTMAE TRAVELER T20/1525253, IAW DWG SRZ-25-005R. CLASSIFIED AS CAT A AND MAJOR REPAIR.
- [SDR FDEA202012093093](https://openairdocs.org/sdr/FDEA202012093093.md): Floorboard · damaged · Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 240 MAIN CABIN FLOOR BOARD 241EJ IS BROKEN. FABRICATED ZONE 240 FLOOR BOARD 241EJ ON VTMAE TRAVELER NR T20/1525269, IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202012093092](https://openairdocs.org/sdr/FDEA202012093092.md): Floorboard · damaged · Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 240 MAIN CABIN FLOOR BOARD 242QF IS BROKEN. FABRICATED ZONE 240 FLOOR BOARD 242QF ON VTMAE TRAVELER NR T20/1525259, IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202012093091](https://openairdocs.org/sdr/FDEA202012093091.md): Floorboard · damaged · Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 240 MAIN CABIN FLOOR BOARD 241WH IS BROKEN. FABRICATED ZONE 240 FLOOR BOARD 241WH ON VTMAE TRAVELER NR T20/1525255, IAW DWG SRZ-25-005, REVISION R, MAJOR REPAIR.
- [SDR FDEA202012093090](https://openairdocs.org/sdr/FDEA202012093090.md): Floorboard · damaged · Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 250 MAIN CABIN FLOOR BOARD 252YG IS BROKEN. FABRICATED FLOOR BOARD 252YG ON VTMAE TRAVELER NR T20/1524940, IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.
- [SDR FDEA202012093087](https://openairdocs.org/sdr/FDEA202012093087.md): Floorboard · damaged · Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 240 MAIN CABIN FLOOR BOARD 241HK IS BROKEN. FABRICATED ZONE 240 FLOOR BOARD 241HK ON VTMAE TRAVELER NR T20/1524938, IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.
- [SDR FDEA202012093085](https://openairdocs.org/sdr/FDEA202012093085.md): Floorboard · damaged · Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 230 FLOOR BOARD 232VH IS BROKEN. FABRICATED ZONE 230 FLOOR BOARD 232VH ON VTMAE TRAVELER NR T20/1524935, IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.
- [SDR FDEA202012093084](https://openairdocs.org/sdr/FDEA202012093084.md): Floorboard · damaged · Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 260 MAIN CABIN FLOOR BOARD 262MF IS BROKEN. FABRICATED ZONE 260 FLOOR BOARD 262MF ON VTMAE TRAVELER NR T20/1524713, IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.
- [SDR FDEA202012093083](https://openairdocs.org/sdr/FDEA202012093083.md): Floorboard · damaged · Dec 9, 2020 · N679FE · Airbus A300F4605R · Standard Practices/Structures
  > ZONE 230 FLOOR BOARD 232KG IS BROKEN. FABRICATED ZONE 230 FLOOR BOARD 232KG ON VTMAE TRAVELER NR T20/1524715, IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.
- [SDR FDEA202012093081](https://openairdocs.org/sdr/FDEA202012093081.md): Floorboard · damaged · Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 260 MAIN CABIN FLOOR BOARD 262KF IS BROKEN. FABRICATED ZONE 260 FLOOR BOARD 262KF ON VTMAE TRAVELER NR T20/1524714, IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202012093080](https://openairdocs.org/sdr/FDEA202012093080.md): Floorboard · damaged · Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 240 MAIN CABIN FLOOR BOARD 241TH IS BROKEN. FABRICATED ZONE 240 FLOOR BOARD 241TH ON VTMAE TRAVELER NR T20/1525260, IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202012073060](https://openairdocs.org/sdr/FDEA202012073060.md): Floorboard · damaged · Dec 7, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 240 MAIN CABIN FLOOR BOARD 241JF IS BROKEN. FABRICATED ZONE 240 FLOOR BOARD 241JF ON VTMAE TRAVELER NR T20/1525277, IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202012073059](https://openairdocs.org/sdr/FDEA202012073059.md): Floorboard · broken · Dec 7, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 230 FLOOR BOARD 231CF IS BROKEN. FABRICATED ZONE 230 FLOOR BOARD 231CF ON VTMAE TRAVELER NR T20/1524716, IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202012073058](https://openairdocs.org/sdr/FDEA202012073058.md): Floorboard · damaged · Dec 7, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 260 MAIN CABIN FLOOR BOARD 262ZF IS BROKEN. FABRICATED ZONE 260 FLOOR BOARD 262ZF ON VTMAE TRAVELER NR T20/1524720, IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202012073057](https://openairdocs.org/sdr/FDEA202012073057.md): Floorboard · damaged · Dec 7, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
  > ZONE 240 MAIN CABIN FLOOR BOARD 241GJ IS BROKEN. FABRICATED ZONE 240 FLOOR BOARD 241GJ ON VTMAE TRAVELER NR T20/1525261, IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202012023012](https://openairdocs.org/sdr/FDEA202012023012.md): Seat Track · gouged · Dec 2, 2020 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK GOUGED AT FR 75, SECOND ROW FROM OUTBOARD SIDE, -Y1221, 19-02. REMOVED GOUGED, IAW SRM 51-73-10 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 101. REMOVED AND INSTALLED SEAT TRACK REPAIR SECTION BETWEEN FR 74-76 -Y1221, IAW SRM 53-10-16 FIG 201.
- [SDR FDEA202011242954](https://openairdocs.org/sdr/FDEA202011242954.md): Shear Plate · cracked · Nov 24, 2020 · N679FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > FLOOR STRUCTURE TO FUSELAGE SKIN SHEAR WEB CRACKED FR 80, RT SIDE. REMOVED AND REPLACED SHEAR WEB AT FR 80 RT SIDE, IAW SRM 51-40-21. P/N A5398111320151 BATCH NR 0003485578. CAT "A" MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N679FE/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 = 'N679FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N679FE/reports

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