# Service difficulty reports: N684FE

A list on [N684FE](https://openairdocs.org/aircraft/N684FE.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 · 190 reports

- [SDR FDEA202408161140](https://openairdocs.org/sdr/FDEA202408161140.md): Support · failed · Aug 16, 2024 · N684FE · Airbus A300F4605R · Landing Gear Retraction/Extension System
  > AFTER 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 DETE
- [SDR FDEA202402260214](https://openairdocs.org/sdr/FDEA202402260214.md): Web · cracked · Feb 26, 2024 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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-
- [SDR FDEA202112012956](https://openairdocs.org/sdr/FDEA202112012956.md): None · damaged · Dec 1, 2021 · N684FE · Airbus A300* · Brake
  > UPON 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 T
- [SDR FDEA202110202599](https://openairdocs.org/sdr/FDEA202110202599.md): None · none · Oct 20, 2021 · N684FE · Airbus A300* · Fuselage Structure (General)
  > MAIN 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, FIG201
- [SDR FDEA202110162711](https://openairdocs.org/sdr/FDEA202110162711.md): Floor Panel · damaged · Oct 16, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > MAIN 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.
- [SDR FDEA202110162704](https://openairdocs.org/sdr/FDEA202110162704.md): Floor Panel · damaged · Oct 16, 2021 · N684FE · Airbus A300* · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA202110152713](https://openairdocs.org/sdr/FDEA202110152713.md): Floor Panel · damaged · Oct 15, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > AFT 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.
- [SDR FDEA202110152708](https://openairdocs.org/sdr/FDEA202110152708.md): Floor Panel · damaged · Oct 15, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > FWD 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.
- [SDR FDEA202110152706](https://openairdocs.org/sdr/FDEA202110152706.md): Floor Panel · damaged · Oct 15, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > MAIN 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.
- [SDR FDEA202110142563](https://openairdocs.org/sdr/FDEA202110142563.md): Rib · cracked · Oct 14, 2021 · N684FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA 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.
- [SDR FDEA202110142562](https://openairdocs.org/sdr/FDEA202110142562.md): Rib · cracked · Oct 14, 2021 · N684FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA 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.
- [SDR FDEA202110142561](https://openairdocs.org/sdr/FDEA202110142561.md): Rib · cracked · Oct 14, 2021 · N684FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA 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 STRING
- [SDR FDEA202110142560](https://openairdocs.org/sdr/FDEA202110142560.md): Rib · cracked · Oct 14, 2021 · N684FE · Airbus A300F4605R · Wing, Control Surfaces
  > 1EA 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 STRINGE
- [SDR FDEA202110142559](https://openairdocs.org/sdr/FDEA202110142559.md): Rib · cracked · Oct 14, 2021 · N684FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA 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- 600
- [SDR FDEA202110132653](https://openairdocs.org/sdr/FDEA202110132653.md): None · unknown · Oct 13, 2021 · N684FE · Airbus A300* · Fuselage Main, Plate/Skin
  > AIRCRAFT 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 SR
- [SDR FDEA202110132652](https://openairdocs.org/sdr/FDEA202110132652.md): None · unknown · Oct 13, 2021 · N684FE · Airbus A300* · Rudder Structure
  > AIRCRAFT 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 DETERMIN
- [SDR FDEA202110132606](https://openairdocs.org/sdr/FDEA202110132606.md): None · unknown · Oct 13, 2021 · N684FE · Airbus A300* · Wing, Control Surfaces
  > AIRCRAFT 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 APPR
- [SDR FDEA202110132605](https://openairdocs.org/sdr/FDEA202110132605.md): None · unknown · Oct 13, 2021 · N684FE · Airbus A300* · Wing, Plate/Skin
  > AIRCRAFT 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 5
- [SDR FDEA202110132604](https://openairdocs.org/sdr/FDEA202110132604.md): None · unknown · Oct 13, 2021 · N684FE · Airbus A300* · Wing, Plate/Skin
  > AIRCRAFT 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 5
- [SDR FDEA202110122709](https://openairdocs.org/sdr/FDEA202110122709.md): Floor Panel · damaged · Oct 12, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > AFT 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.
- [SDR FDEA202110122707](https://openairdocs.org/sdr/FDEA202110122707.md): Floor Panel · damaged · Oct 12, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > FWD 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.
- [SDR FDEA202110122705](https://openairdocs.org/sdr/FDEA202110122705.md): Floor Panel · damaged · Oct 12, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > FWD 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.
- [SDR FDEA202110122712](https://openairdocs.org/sdr/FDEA202110122712.md): Floor Panel · damaged · Oct 12, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > MAIN 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.
- [SDR FDEA202110122710](https://openairdocs.org/sdr/FDEA202110122710.md): Floor Panel · damaged · Oct 12, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > MAIN 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.
- [SDR FDEA202110102716](https://openairdocs.org/sdr/FDEA202110102716.md): None · worn · Oct 10, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > N00301 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.
- [SDR FDEA202110102715](https://openairdocs.org/sdr/FDEA202110102715.md): None · worn · Oct 10, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > N00302 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.
- [SDR FDEA202110102714](https://openairdocs.org/sdr/FDEA202110102714.md): None · worn · Oct 10, 2021 · N684FE · Airbus A300* · Fuselage Main, Structure
  > N00303 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.
- [SDR FDEA202110052592](https://openairdocs.org/sdr/FDEA202110052592.md): Web · cracked · Oct 5, 2021 · N684FE · Airbus A300* · Nacelle/Pylon Structure
  > #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,PAGE2
- [SDR FDEA202110052590](https://openairdocs.org/sdr/FDEA202110052590.md): Web · cracked · Oct 5, 2021 · N684FE · Airbus A300* · Nacelle/Pylon Structure
  > #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,PAGE2
- [SDR FDEA202109172321](https://openairdocs.org/sdr/FDEA202109172321.md): Idg · faulted · Sep 17, 2021 · N684FE · Airbus A300F4605R · AC Generator-Alternator
  > REJECTED 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
- [SDR FDEA202012043031](https://openairdocs.org/sdr/FDEA202012043031.md): Valve · leaking · Dec 4, 2020 · N684FE · Airbus A300F4605R · Hydraulic System, Main
  > PDIS 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 SYS
- [SDR FDEA201904050762](https://openairdocs.org/sdr/FDEA201904050762.md): Skin · delaminated · Apr 5, 2019 · N684FE · Airbus A300F4605R · Ailerons
  > RH 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- T03
- [SDR FDEA201903280742](https://openairdocs.org/sdr/FDEA201903280742.md): Skin · corroded · Mar 28, 2019 · N684FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT 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.
- [SDR FDEA201903250705](https://openairdocs.org/sdr/FDEA201903250705.md): Rib · cracked · Mar 25, 2019 · N684FE · Airbus A300F4605R · Trailing Edge Flaps
  > LEFT 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.
- [SDR FDEA201903250704](https://openairdocs.org/sdr/FDEA201903250704.md): Frame · chafed · Mar 25, 2019 · N684FE · Airbus A300F4605R · Fuselage Main, Frame
  > MAIN 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 ENBOD
- [SDR FDEA201903220701](https://openairdocs.org/sdr/FDEA201903220701.md): Web · cracked · Mar 22, 2019 · N684FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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 FR
- [SDR FDEA201901160156](https://openairdocs.org/sdr/FDEA201901160156.md): Rib · cracked · Jan 16, 2019 · N684FE · Airbus A300F4605R · Leading Edge Devices
  > MDIS 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:
- [SDR FDEA2018112103316](https://openairdocs.org/sdr/FDEA2018112103316.md): Bolt · sheared · Nov 20, 2018 · N684FE · Airbus A300F4605R · Wheel/Ski/Float
  > #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
- [SDR FDEA201707272057](https://openairdocs.org/sdr/FDEA201707272057.md): Line · leaking · Jul 27, 2017 · N684FE · Airbus A300F4605R · Hydraulic System, Main
  > LEVEL 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, INCREA
- [SDR FDEA201702090487](https://openairdocs.org/sdr/FDEA201702090487.md): Gcu · malfunctioned · Feb 9, 2017 · N684FE · Airbus A300F4605R · AC Generation System
  > EXPERIENCED 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 SERVICE
- [SDR FDEA201702020314](https://openairdocs.org/sdr/FDEA201702020314.md): Idg · failed · Feb 2, 2017 · N684FE · Airbus A300F4605R · Alternator-Generator Drive
  > WHILE 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 CONNECTORS
- [SDR FDEA201612244537](https://openairdocs.org/sdr/FDEA201612244537.md): Gcu · failed · Dec 24, 2016 · N684FE · Airbus A300F4605R · AC Generator-Alternator
  > DURING 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 GOOD
- [SDR FDEA201611154026](https://openairdocs.org/sdr/FDEA201611154026.md): Frame · damaged · Nov 15, 2016 · N684FE · Airbus A300F4605R · Fuselage Main, Frame
  > E & 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.
- [SDR FDEA201611154023](https://openairdocs.org/sdr/FDEA201611154023.md): Spar · cracked · Nov 15, 2016 · N684FE · Airbus A300F4605R · Nacelle/Pylon, Main Frame
  > LOWER 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 REPAIR
- [SDR FDEA201611154014](https://openairdocs.org/sdr/FDEA201611154014.md): Frame · cracked · Nov 15, 2016 · N684FE · Airbus A300F4605R · Fuselage Main, Frame
  > AFT 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 ACTUA
- [SDR FDEA201611124006](https://openairdocs.org/sdr/FDEA201611124006.md): Mount · corroded · Nov 12, 2016 · N684FE · Airbus A300F4605R · Nacelle/Pylon, Attach Fittings
  > NR 2 PYLON FWD MOUNT CORRODED. REPAIRED IAW SRM 54-51-81. MAJOR REPAIR.
- [SDR FDEA201611124005](https://openairdocs.org/sdr/FDEA201611124005.md): Mount · corroded · Nov 12, 2016 · N684FE · Airbus A300F4605R · Nacelle/Pylon, Attach Fittings
  > CORROSION ON NR 1 PYLON FWD MOUNT. REPAIRED BY INSTALLATION OF BUSHINGS IAW SRM 54-51-81 MAJOR REPAIR.
- [SDR FDEA201611124004](https://openairdocs.org/sdr/FDEA201611124004.md): Floor Panel · cracked · Nov 12, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 231EF CRACKED. A NEW FLOOR PANEL FABRICATED IAW SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201611123988](https://openairdocs.org/sdr/FDEA201611123988.md): Floor Panel · delaminated · Nov 12, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CARGO FLOOR PANEL 241BF DELAMINATED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.
- [SDR FDEA201611123987](https://openairdocs.org/sdr/FDEA201611123987.md): Floor Panel · cracked · Nov 12, 2016 · N684FE · Airbus A300F4605R · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252PH CRACKED. THE FLOOR PANEL WAS FABRICATED IAW SRZ 25-005. MAJOR REPAIR.

Next page: https://openairdocs.org/aircraft/N684FE/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 = 'N684FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N684FE/reports

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