N684FE

Service difficulty reports · 190

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 = 'N684FE' 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 FDEA202408161140Support · failedAFTER TAKEOFF WHEN WE BROUGHT THE GEAR UP (SYS 1) GEAR WOULD NOT RETRACT. WE TRIED USING SYS 2 AS WELL BUT THE GEAR DID NOT RETRACT. AMM: 32-00-00-04, TSM: 32-61-00, FOUND RH MLG BOGIE BEAM PROX SENSOR ASSY TO BE BROKEN AT TANGS ALLOWING SHIFT OF PROX DETEAug 16, 2024 · N684FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA202402260214Web · crackedMAIN DECK FR47 -Y953 ~ -Y1456 UNDERFLOOR WEB CRACKED. REPAIRED THE CRACKED WEB AT MAIN DECK FR47 -Y953 ~ -Y1456 UNDERFLOOR 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 SRI 53-Feb 26, 2024 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202112012956None · damagedUPON POST FLIGHT INSPECTION, FOUND #6 MLG TIRE BLOWN AND BEAD UNSEATED. STILL IN TACT AND ON WHEEL. NO DAMAGE. REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: Z32-002-03 POS: 6 SRL: 25001 TAG NBR: 6485F1 ON MPN: Z32-002-03 CPN: 3211843 SRL: F3664 TDec 1, 2021 · N684FE · Airbus A300* · BrakeSDR FDEA202110202599None · noneMAIN DECK FLOOR SEAT TRACK FOUND GOUGE AT FR60 9" Y953 ACCOMPLISHED THE SEAT TRACK REPAIR I.A.W A300-600F SRM 53-10-16-201, PARA4, P203-208, FIG201Oct 20, 2021 · N684FE · Airbus A300* · Fuselage Structure (General)SDR FDEA202110162711Floor Panel · damagedMAIN CARGO COMPT FLOOR PANEL #242ZH WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201-205 ,FIG201.Oct 16, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110162704Floor Panel · damagedMAIN CARGO COMPT FLOOR PANEL #232VH WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201- 205, FIG201.Oct 16, 2021 · N684FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202110152713Floor Panel · damagedAFT CARGO COMPT FLOOR PANEL #151QF WAS FOUND EDGE DAMAGED ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.Oct 15, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110152708Floor Panel · damagedFWD CARGO COMPT FLOOR PANEL #131RG WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.Oct 15, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110152706Floor Panel · damagedMAIN CARGO COMPT FLOOR PANEL #232YG WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201-205 ,FIG201.Oct 15, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110142563Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 27AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGERS 2.Oct 14, 2021 · N684FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202110142562Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 27FWD AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGERS 2.Oct 14, 2021 · N684FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202110142561Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 26AFT AREA(REAR) OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGOct 14, 2021 · N684FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202110142560Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB 26AFT AREA(FWD) OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO: 6-5750-T0364644 P1, TITLE: WING-FLIGHT SURFACES-RH CENTER FLAP, CRACKS IN UPPER FLANGES OF RIB26 AND 27 BETWEEN STRINGEOct 14, 2021 · N684FE · Airbus A300F4605R · Wing, Control SurfacesSDR FDEA202110142559Rib · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP 27AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE REPAIR I.A.W FEDEX EA NO:6-5750-T0364642, TITLE:WING-FLIGHT SURFACES- LHCENTER FLAP, CRACK IN UPPER FLANGE OF RIB27 AT STRINGERS2.8 -ALI575306-01 & A300- 600Oct 14, 2021 · N684FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202110132653None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON FUSELAGE SKIN BTW FR49 TO FR50 AND STR37L TO STR39L. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SROct 13, 2021 · N684FE · Airbus A300* · Fuselage Main, Plate/SkinSDR FDEA202110132652None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON RUDDER TRAILING EDGE APEX AREA LOCATED BTW T/E SCREW LINE NO.19 AND NO.20 FASTENER COUNT FROM LOWER SIDE. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINOct 13, 2021 · N684FE · Airbus A300* · Rudder StructureSDR FDEA202110132606None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON L/H WING O/B FLAP UPR SURFACE SKIN LOCATED AT RIB15 AND FRONT SPAR DATUM. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROct 13, 2021 · N684FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202110132605None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR L/E PANEL 613AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 5Oct 13, 2021 · N684FE · Airbus A300* · Wing, Plate/SkinSDR FDEA202110132604None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON L/H WING LWR L/E PANEL 513AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-600F SRM 5Oct 13, 2021 · N684FE · Airbus A300* · Wing, Plate/SkinSDR FDEA202110122709Floor Panel · damagedAFT CARGO COMPT FLOOR PANEL #152QF WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.Oct 12, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110122707Floor Panel · damagedFWD CARGO COMPT FLOOR PANEL #132LG WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.Oct 12, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110122705Floor Panel · damagedFWD CARGO COMPT FLOOR PANEL #132RG WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8B , FIG203 SHEET1 , P209-211.Oct 12, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110122712Floor Panel · damagedMAIN CARGO COMPT FLOOR PANEL #241GJ WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201-205 ,FIG201.Oct 12, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110122710Floor Panel · damagedMAIN CARGO COMPT FLOOR PANEL #231EF WAS FOUND EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F S.R.M 53-10-20-201 PARA.8A , P201-205 ,FIG201.Oct 12, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110102716None · wornN00301 FR38.2/FR40 RH NO.4 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P.201~210 FIG.201 PFM REPAIR ACCOMPLISHED.Oct 10, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110102715None · wornN00302 FR54/FR54.2 LH NO.5 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P.201~210 FIG.201 PFM REPAIR ACCOMPLISHED.Oct 10, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110102714None · wornN00303 FR54/FR54.2 RH NO.5 DUMMY SEAT TRACK GAP OVER 1.0MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P.201~210 FIG.201 PFM REPAIR ACCOMPLISHED.Oct 10, 2021 · N684FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202110052592Web · cracked#2 PYLON I/B SIDE WAS FOUND A WEB UPPER CORNER CRACK AT RIB 8A. REPLACED THE DAMAGE PART WITH NEW I.A.W A300-600F SRM 51-72-10-001,PAGE2Oct 5, 2021 · N684FE · Airbus A300* · Nacelle/Pylon StructureSDR FDEA202110052590Web · cracked#2 PYLON O/B SIDE WAS FOUND A WEB UPPER CORNER CRACK AT RIB 8A. REPLACED THE DAMAGE PART WITH NEW I.A.W A300-600F SRM 51-72-10-001,PAGE2Oct 5, 2021 · N684FE · Airbus A300* · Nacelle/Pylon StructureSDR FDEA202109172321Idg · faultedREJECTED TAKEOFF AT APPROXIMATELY 50 KNOTS FOR GEN 2 FAULT. IDG2 FAULT LIGHT WAS FLICKERING PRIOR TO GEN2 FAULT. AFTER TAXIING CLEAR, GEN FAULT RESET PER ECAM/QRH, BUT IDG2 FAULT CONTINUED TO FLICKER FOR 10 MINUTES. MEL 17SEP21 00:38 MEM U RELEASED Sep 17, 2021 · N684FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA202012043031Valve · leakingPDIS 684 29-02 9691 04DEC20 DEN OPEN U LOGPAGES:3359248. AT FL350 1.25 HRS AFTER T/O, GREEN SYS HYD QTY WAS OBSERVED 2 NEEDLE WIDTHS ABOVE THE YELLOW ARC. AT 1.5 HRS NEEDLE WAS 1 NEEDLE WIDTH INTO YELLOW ARC. DIVERT TO KDEN. BLEED GRN SYS AND FOUND GRN SYSDec 4, 2020 · N684FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201904050762Skin · delaminatedRH AILERON UPPER SURFACE FROM O/B TO I/B 10 IN , FROM T/E TO L/E 11 IN FOUND BULGE REPAIRED THE RH AILERON UPPER SURFACE FROM O/B TO I/B 10 IN , FROM T/E TO L/E 11 IN BULGE PER A300-600F SRM57-61-11-101 FIG103 AND SRM51-77-12 PARA.4.D.(3) . EA # 6-5750- T03Apr 5, 2019 · N684FE · Airbus A300F4605R · AileronsSDR FDEA201903280742Skin · corrodedLEFT WING O/B FLAP O/B TRAILING EDGE UPPER SKIN JUST UNDER THE STATIC DISCHARGER FITTING FOUND CORRODED. COMPLIED WITH EA 6-5750-T0345881 P1. MAJOR REPAIR IAW GMM 6-2-100.Mar 28, 2019 · N684FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201903250705Rib · crackedLEFT WING I/B FLAP RIB 3 UPPER FLANGE FOUND CRACK BETWEEN STRINGER 2.5 AND REAR SPAR. COMPLIED WITH EA 6-5750-T0345820 PT1. REPAIRED THE LT WING I/B FLAP RIB. MAJOR REPAIR IAW GMM 6-2-100.Mar 25, 2019 · N684FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201903250704Frame · chafedMAIN DECK FR57.3 STR 12-13R FRAME CHAFED REPAIRED THE MAIN DECK FR57.3 STR 12-13R FRAME PER SRM 53-10-13 FIG 202. THIS REPAIR IS CATEGORY B AND MUST BE INSPECTED AT DEFINED INTERVALS PER SRI 53-10-13-2-002-00. THE FIRST INSPECTION IS 42500FC AFTER REPAIR ENBODMar 25, 2019 · N684FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201903220701Web · crackedMAIN DECK FR47 Y0 ~ -Y450 UNDERFLOOR 1EA WEB CRACKED REPAIRED THE MAIN DECK FR47 Y0~-Y450 UNDERFLOOR WEB PER SRM 53-15-15 FIG 201. THE REPAIR IS CATEGORY B AND MUST BE INSPECTED AT DEFINED INTERVALS PER SRI 53-15-15-2-002-00. INSPECTION THRESHOLD IS 24000FC FRMar 22, 2019 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201901160156Rib · crackedMDIS 684 57-40 7425 08JAN19 MEM FACT U NR 2 LT L/E SLAT FOUND NR 1 RIB CRACKED SHGN 08JAN19 11:15 MEM U REMOVED RIB IN REF TO SRM 51-40-20 REF. WRI 27-80/7424 FOR PICTURE AND PART ORDERED FOR REPAIR. MSN: 1951225 PART 09JAN19 11:14 MEM U IDENTIFIED PARTS MPN: Jan 16, 2019 · N684FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA2018112103316Bolt · sheared#4 MLG WHEEL IS HAS 3 EA WHEEL HALF BOLTS BROKEN. REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: Z32-002-03 POS: 4 SRL: U2911 TAG NBR:ON MPN: Z32-002-03 CPN: 3211843 SRL: 19894 Nov 20, 2018 · N684FE · Airbus A300F4605R · Wheel/Ski/FloatSDR FDEA201707272057Line · leakingLEVEL CRUISE AT 340, RECEIVED A HYD QTY LOW FOLLOWED BY A LOW PRESSURE GREEN SYSTEM. LOW PRESSURE LIGHT GREEN SYSTEM REMAINED ILLUMINATED. COMPLIED WITH ECAM AND QRH. DECLARED AN EMERGENCY AND CONTINUED FLIGHT TO DESTINATION. GREEN QTY IN RED ZONE, INCREAJul 27, 2017 · N684FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201702090487Gcu · malfunctionedEXPERIENCED MULTIPLE AC BUSS 2 FAULTS DURING ARRIVAL. DECLARED EMERGENCY AND LANDED. CHANGED NR 2 AC BUSS GCU. OPS CHECKED NORMAL ON ENGINE RUN. OPS CEHCKED GPCU ALL TESTS OK. ACFT OK FOR SERVICEFeb 9, 2017 · N684FE · Airbus A300F4605R · AC Generation SystemSDR FDEA201702020314Idg · failedWHILE DESCENDING AT APPROX 17000 FT, ECAM SHOWED NR 2 IDG LOW OIL PRESSURE . DISCONECTED THE NR 2 IDG IAW ECAM AND REFERRED TO QRH PROCEDURE. FOUND IDG SIGHT GAGE TO INDICATE FULL OIL, ELECTRICAL CONNECTIONS SECURE AND DPI INDICATOR SET. REMOVED CONNECTORSFeb 2, 2017 · N684FE · Airbus A300F4605R · Alternator-Generator DriveSDR FDEA201612244537Gcu · failedDURING TAXI OUT, NR 1 GENERATOR FAULTED. PERFORMED PDM PROCEDURE. STARTED THE APU ALL ELECTRICAL POWER WAS LOST REMOVED AND REPLACED LT AND RT GCU IAW AMM 24-23-12. REMOVED AND REPLACED THE APU GCU IAW AMM 24-22-12. RAN ENGINES AND APU, OPS CHECKED GOODDec 24, 2016 · N684FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA201611154026Frame · damagedE & E BAY RT SIDE UPPER CORNER MAIN DECK FLOORBEAM AT FRAME 13 IS LOOSE REMOVED DAMAGED FRAME BETWEEM STRINGERS 24R & SPLICE IAW SRM 51-40-21 & DAMAGED FITTING. INSTALLED & REPAIRED IAW SRM 53-12-13 FIG 201. MAJOR REPAIR.Nov 15, 2016 · N684FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201611154023Spar · crackedLOWER SPAR OF CANTILEVER STRUCTURE IS CRACKED BETWEEN RIB A11 & RIB J08 REPAIRED AREA ON NR 1 PYLON LOWER SPAR BETWEEN RIBS A11 & J08 IAW SRM 54- 52-11 FIG 201. MAJOR REPAIRNov 15, 2016 · N684FE · Airbus A300F4605R · Nacelle/Pylon, Main FrameSDR FDEA201611154014Frame · crackedAFT CARGO DOOR ACTUATOR BRACKET CRACKED. REMOVED AND REINSTALLED AFT CARGO DOOR IAW A300-600 AMM 52-32-11-04-01. PERFORMED OPS TEST IAW A300-600 AMM 52-32-11-05-01, 52-71-11-05-02, AND 52-73-00-05-02.OPS TEST GOOD. REMOVED AND REPLACED AFT CARGO DOOR ACTUANov 15, 2016 · N684FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201611124006Mount · corrodedNR 2 PYLON FWD MOUNT CORRODED. REPAIRED IAW SRM 54-51-81. MAJOR REPAIR.Nov 12, 2016 · N684FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR FDEA201611124005Mount · corrodedCORROSION ON NR 1 PYLON FWD MOUNT. REPAIRED BY INSTALLATION OF BUSHINGS IAW SRM 54-51-81 MAJOR REPAIR .Nov 12, 2016 · N684FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR FDEA201611124004Floor Panel · crackedMAIN CARGO FLOOR PANEL 231EF CRACKED. A NEW FLOOR PANEL FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Nov 12, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201611123988Floor Panel · delaminatedMAIN CARGO FLOOR PANEL 241BF DELAMINATED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Nov 12, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201611123987Floor Panel · crackedMAIN CABIN FLOOR PANEL 252PH CRACKED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.Nov 12, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor Panel
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