N679FE

Service difficulty reports · 176

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 = 'N679FE' 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 FDEA202607301074Restraint · brokenMAIN 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 Jul 30, 2026 · N679FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202606200788Cvr · malfunctionedCVR 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.Jun 20, 2026 · N679FE · Airbus A300F4605R · Audio/Video MonitoringSDR FDEA202602190245Safety Wire · wrong partTHE 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 CORREFeb 19, 2026 · N679FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202602190243Safety Wire · wrong partTHE 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 SAFETYFeb 19, 2026 · N679FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202509221760Fitting · not reportedDOORS - 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 Sep 22, 2025 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202509061737Repair · noneEXISTING 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 Sep 6, 2025 · N679FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202509051621Door · crackedMAIN 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 CARGOSep 5, 2025 · N679FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202508291580Seat Track · noneEXISTING 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: FUSELAAug 29, 2025 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508291566Skin · delaminatedRH 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 SPOILAug 29, 2025 · N679FE · Airbus A300F4605R · SpoilersSDR FDEA202508291565Flap · misrepairedEXISTING 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 57-50-0Aug 29, 2025 · N679FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202508271583Floor Support · noneEXISTING 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: Aug 27, 2025 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202508261556Seat Track · damagedEXISTING 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. BUTAug 26, 2025 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508261539Seat Track · wornMAIN 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.Aug 26, 2025 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508261538Web · crackedMAIN 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 A300-60Aug 26, 2025 · N679FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202508231555Repair · misrepairedEXISTING 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 Aug 23, 2025 · N679FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202508211582Seat Track · noneEXISTING 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.Aug 21, 2025 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508211581Seat Track · noneEXISTING 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.20Aug 21, 2025 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202508191503Floorbeam · crackedMAIN 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" REPAAug 19, 2025 · N679FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202508191502Door Frame · crackedRH 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:Aug 19, 2025 · N679FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202407311077Fitting · crackedDURING 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 21R53810798Jul 31, 2024 · N679FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202407311076Fitting · crackedDURING 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 REPAJul 31, 2024 · N679FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202305110849Crossbeam · crackedMDCC 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 - MAIMay 11, 2023 · N679FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202305110848Crossbeam · crackedMDCC 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 - MAIMay 11, 2023 · N679FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202305110847Crossbeam · crackedMDCC 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 - MAINMay 11, 2023 · N679FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202302160278Jackscrew · failedPDIS 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 SFeb 16, 2023 · N679FE · Airbus A300F4605R · Leading Edge Slat Control SystemSDR FDEA202106171561Engine · failedAT 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 3Jun 17, 2021 · N679FE · Airbus A300F4605R · Turbine Engine Oil SystemSDR FDEA202101140098Actuator · failed(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. AFTEJan 14, 2021 · N679FE · Airbus A300F4605R · Landing Gear ActuatorSDR FDEA202012243206Seat Track · crackedMAIN 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.Dec 24, 2020 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202012183187Web · damagedDURING 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 MARKEDec 18, 2020 · N679FE · Airbus A300F4605R · Horizontal Stabilizer StructureSDR FDEA202012153168Skin · crackedRT 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. SUPDec 15, 2020 · N679FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA202012103118Floorboard · crackedFWD 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.Dec 10, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012103117Floorboard · crackedFWD 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.Dec 10, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012103116Floorboard · damagedFLOORBOARD 151TF DAMAGED. FABRICATED FLOOR PANEL 151TF ON VTMAE TRAVELER T20/1525286, IAW DWG SRZ-25-005R. CLASSIFIED AS CAT A AND MAJOR REPAIR.Dec 10, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012103115Floorboard · crackedFWD 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.Dec 10, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012093093Floorboard · damagedZONE 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.Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012093092Floorboard · damagedZONE 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.Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012093091Floorboard · damagedZONE 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.Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012093090Floorboard · damagedZONE 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.Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012093087Floorboard · damagedZONE 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.Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012093085Floorboard · damagedZONE 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.Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012093084Floorboard · damagedZONE 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.Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012093083Floorboard · damagedZONE 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.Dec 9, 2020 · N679FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202012093081Floorboard · damagedZONE 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.Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012093080Floorboard · damagedZONE 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.Dec 9, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012073060Floorboard · damagedZONE 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.Dec 7, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012073059Floorboard · brokenZONE 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.Dec 7, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012073058Floorboard · damagedZONE 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.Dec 7, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012073057Floorboard · damagedZONE 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.Dec 7, 2020 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202012023012Seat Track · gougedSEAT 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. Dec 2, 2020 · N679FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202011242954Shear Plate · crackedFLOOR 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.Nov 24, 2020 · N679FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
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