# Service difficulty reports: N665FE A list on [N665FE](https://openairdocs.org/aircraft/N665FE.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 · 201 reports - [SDR FDEA202610151590](https://openairdocs.org/sdr/FDEA202610151590.md): Hydraulic System · low quantity · Oct 15, 2026 · N665FE · Airbus A300F4605R · Hydraulic System, Main > DURING TAKEOFF ROLL AT 65 KNOTS, MASTER CAUTION WITH BLUE HYD SYS RSVR LO. REJECTED TAKEOFF AT 75 KIAS. COMPLIED WITH ECAM AND QRH. AMM 12-12-29-00, BLUE HYD QTY LOW. SERVICED BLUE HYD SYS IAW AMM 12-12-29-00. - [SDR FDEA202603030308](https://openairdocs.org/sdr/FDEA202603030308.md): Safety Wire · failed · Mar 3, 2026 · N665FE · Airbus A300F4605R · Emergency Equipment > FOUND R1 DOOR SLIDE EJECTOR BAG RELEASE CABLE WITH IMPROPER SAFETY WIRE INSTALLED. EA: 9-2560-T0386431 INSTALLED PROPER SAFETY WIRE MS20995CY16 ON THE R1 DOOR SLIDE SN# 0552 EJECTOR BAG RELEASE CABLE. REF E.A. ABOVE. - [SDR FDEA202603030307](https://openairdocs.org/sdr/FDEA202603030307.md): Safety Wire · failed · Mar 3, 2026 · N665FE · Airbus A300F4605R · Emergency Equipment > THE L1 SLIDE PACKBOARD/ACTIVATION SAFETY/BREAKAWAY WIRE REQUIRES REPLACEMENT, IT HAS THE INCORRECT SAFETY WIRE INSTALLED. AMM: 25-61-20-05-01 EA: 9-2560-T0386431 INSTALLED THE CORRECT SAFETY WIRE PER AMM 25-61-20-05-01 AND EA 9-2560-T0386431. AIRCRAFT - [SDR FDEA202410281594](https://openairdocs.org/sdr/FDEA202410281594.md): Cargo Track · damaged · Oct 28, 2024 · N665FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT - EXISTING SEAT TRACK REPAIR AT -Y450 BETWEEN FR40 AND FR45 REQUIRES EVALUATION FOT CONFORMITY TO APPROVED DATA THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT SEAT TRACK AT -Y450 BETWEEN FR40 AND FR45 WAS EVALUATED AND FOUND - [SDR FDEA202410181542](https://openairdocs.org/sdr/FDEA202410181542.md): Cargo Track · worn · Oct 18, 2024 · N665FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings > MAIN DECK CARGO COMPARTMENT - SEAT TRACK -Y1456 FR53-FR54 INNER SURFACE WORN REPAIRED THE WORN SEAT TRACK AT MAIN DECK CARGO COMPARTMENT -Y1456 BETWEEN FR53 AND FR54 PER A300-600F SRM 53-10-16-201 FIG.201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX - [SDR FDEA202410181541](https://openairdocs.org/sdr/FDEA202410181541.md): Crossbeam · corroded · Oct 18, 2024 · N665FE · Airbus A300F4605R · Fuselage Main, Structure > MAIN DECK CARGO - CROSSBEAM LOWER SURFACE FR59 Y953-Y1456 CORRODED. COMPLIED WITH EA: 6-5310-T0381123 P1. TITLE: FUSELAGE - MAINFRAME - CORROSION ON MDCC FR59 CROSSBEAM LOWER FLANGE. REPAIRED THE MAIN DECK CARGO CORRODED CROSSBEAM AT FR59 BETWEEN Y953 AND - [SDR FDEA202410181540](https://openairdocs.org/sdr/FDEA202410181540.md): Floor Support · no discrepancy · Oct 18, 2024 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > EXISTING REPAIR ON MAIN DECK FLOOR SUPPORT AT Y730 BETWEEN FR11 AND FR13A REQUIRES EVALUATION FOR CONFORMITY ENTRY IN ERROR DUPLICATE WITH SDR#: 24-1506 - [SDR FDEA202410151506](https://openairdocs.org/sdr/FDEA202410151506.md): Floor Support · corroded · Oct 15, 2024 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > EXISTING REPAIR ON MAIN DECK FLOOR SUPPORT AT Y730 BETWEEN FR11 AND FR13A REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK SUPPORT AT Y730 BETWEEN FR11 AND FR13A WAS EVALUATED AND FOUND CONFORMITY WITH DWG: A53612214(ISSUE.V00), BUT THE - [SDR FDEA202410111486](https://openairdocs.org/sdr/FDEA202410111486.md): Frame · cracked · Oct 11, 2024 · N665FE · Airbus A300F4605R · Fuselage Main, Frame > INSPECTION OF FR40 LOWER JUNCTION FASTENER HOLE #3 LH SIDE FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-T0381079 P1. TITLE: WINGS - BASIC WING STRUCTURE - FR40 LH LOWER JUNCTION LOWER HOLE - CRACK REPAIR. REPAIRED THE CRACKED #3 HOLE AT FR40 LH SIDE LOWER J - [SDR FDEA202410081441](https://openairdocs.org/sdr/FDEA202410081441.md): Seat Track · damaged · Oct 8, 2024 · N665FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK LOBES DAMAGED FOR LOCK AT POS MP0754 REPAIRED THE DAMAGED SEAT TRACK AT MAIN DECK -Y953 BETWEEN FR28 AND FR29 PER A300- 600F SRM 53-10-16-201 FIG.201. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100. - [SDR FDEA202410071439](https://openairdocs.org/sdr/FDEA202410071439.md): Frame · cracked · Oct 7, 2024 · N665FE · Airbus A300F4605R · Fuselage Main, Frame > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL COMPILED WITH EA: 6-5710-T0381007 P1. REPAIRED THE CENTER WING BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE - [SDR FDEA202410071438](https://openairdocs.org/sdr/FDEA202410071438.md): Frame · cracked · Oct 7, 2024 · N665FE · Airbus A300F4605R · Fuselage Main, Frame > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO: 6-5710-E0342809 D P1. REPAIRED THE CRACKED HOLE "I" OF CENTER WING BOX - REAR SPAR AND BOTTOM PANEL AT - [SDR FDEA202410071437](https://openairdocs.org/sdr/FDEA202410071437.md): Rib · cracked · Oct 7, 2024 · N665FE · Airbus A300F4605R · Trailing Edge Flaps > RH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB26 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0380847 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS AT UPPER FLANGES OF RIB 26 AT STR. 2.7 / 2.8 - ALI 575306-01-1A. REPAIRE - [SDR FDEA202410071436](https://openairdocs.org/sdr/FDEA202410071436.md): Rib · cracked · Oct 7, 2024 · N665FE · Airbus A300F4605R · Trailing Edge Flaps > LH WING CENTER FLAP RIB UPR FLANGE FOUND 6EA CRACKS AT RIB25 BETWEEN STGR2.8 AND REAR SPAR, RIB26 BETWEEN STGR2.6 AND REAR SPAR, AND RIB27 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0380959 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP - [SDR FDEA202410071435](https://openairdocs.org/sdr/FDEA202410071435.md): Rib · cracked · Oct 7, 2024 · N665FE · Airbus A300F4605R · Trailing Edge Flaps > LH WING CENTER FLAP RIB UPR FLANGE FOUND 4EA CRACKS AT RIB18 BETWEEN STGR2.8 AND REAR SPAR, RIB19 BETWEEN STGR2.7 AND REAR SPAR, AND RIB20 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0380959 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP - [SDR FDEA202410071434](https://openairdocs.org/sdr/FDEA202410071434.md): Rib · cracked · Oct 7, 2024 · N665FE · Airbus A300F4605R · Trailing Edge Flaps > LH WING CENTER FLAP RIB UPR FLANGE FOUND 7EA CRACKS AT RIB11 BETWEEN STGR2.6 AND REAR SPAR, RIB12 BETWEEN STGR2.7 AND REAR SPAR, AND RIB13 BETWEEN STGR2.6 AND STGR2.7 COMPLIED WITH EA: 6-5750-T0380959 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CR - [SDR FDEA202410071433](https://openairdocs.org/sdr/FDEA202410071433.md): Web · cracked · Oct 7, 2024 · N665FE · 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 SRI53-15-15-2-002 - [SDR FDEA202410071432](https://openairdocs.org/sdr/FDEA202410071432.md): Web · cracked · Oct 7, 2024 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MAIN DECK FR47 Y0-Y450 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB AT MAIN DECK FR47 Y0-Y450 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 SRI53-15-15-2-002-00. I - [SDR FDEA202404020432](https://openairdocs.org/sdr/FDEA202404020432.md): Power Supply · failed · Apr 2, 2024 · N665FE · Airbus A300F4605R · Emergency Lighting > IN THE ATTEMPT TO REMOVE FOR TIME, S/N BATT PACK(S/N 243728 PS3) - THE EMER PWR SUP UNIT(29WL1) P/N 3214-41 INTERNAL CIRCUIT CARD BROKE(FELL OUT OF UNIT). C/W PT1, STEP 1 OF ABOVE EA. ACFT OK FOR SVC ONCE THE MEL OF 33-51-05-01 IS APPLIED. COURIER CO - [SDR FDEA202210082520](https://openairdocs.org/sdr/FDEA202210082520.md): Retainer · failed · Oct 8, 2022 · N665FE · Airbus A300F4605R · Emergency Equipment > CREW REPORTED R1 DOOR DIFFICULT TO DISARM. ON ARRIVAL AT A/C, FOUND DOOR OPENED & GIRT BAR HANGING UNDER DOOR. DURING TROUBLESHOOTING OF DOOR ARM/DISARM SYSTEM, FOUND GIRT BAR RETAINING CLIPS MISSING FROM GIRT EXTENSION. ALLOWING GIRT BAR TO MIGRATE IN - [SDR FDEA202206011348](https://openairdocs.org/sdr/FDEA202206011348.md): None · none · Jun 1, 2022 · N665FE · Airbus A300* · Passenger/Crew Doors > RH FWD PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS - [SDR FDEA202206011351](https://openairdocs.org/sdr/FDEA202206011351.md): None · none · Jun 1, 2022 · N665FE · Airbus A300* · Wing, Control Surfaces > RH WING #5 SPOILER CENTER O/B HINGE ARM O/B SIDE FOUND 2EA DELAMINATIONS. SIZE: (1) 45MM*25MM, DEPTH: 1.57MM (2)45MM*25MM, DEPTH: 1.27MM - [SDR FDEA202206011350](https://openairdocs.org/sdr/FDEA202206011350.md): None · none · Jun 1, 2022 · N665FE · Airbus A300* · Wing, Control Surfaces > LH WING #5 SPOILER CENTER I/B HINGE ARM O/B SIDE FOUND DELAMINATION (SIZE: 20MM*33MM, DEPTH: 1.78MM) AND CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION (SIZE: (1)18MM*20MM, DEPTH: 2.06MM (2)50MM*40MM, DEPTH: 2.2MM) - [SDR FDEA202206011349](https://openairdocs.org/sdr/FDEA202206011349.md): None · none · Jun 1, 2022 · N665FE · Airbus A300* · Wing, Control Surfaces > LH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION (SIZE: 40MM*20MM, DEPTH: 1.9MM) AND CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION (SIZE: (1)30MM*40MM, DEPTH: 2.6MM (2)30MM*20MM, DEPTH: 2.3MM) - [SDR FDEA202206011347](https://openairdocs.org/sdr/FDEA202206011347.md): None · none · Jun 1, 2022 · N665FE · Airbus A300* · Fuselage Main, Structure > AFT CARGO COMPT. FLOOR STRUCTURE CROSSBEAM AT FR62 BETWEEN Y140 AND Y300 FOUND CORROSION - [SDR FDEA202008272048](https://openairdocs.org/sdr/FDEA202008272048.md): Valve · inoperative · Aug 27, 2020 · N665FE · Airbus A300F4605R · Landing Gear Retraction/Extension System > LANDING GEAR DID NOT EXTEND. ECAM PROCEDURE LDG GEAR MANUAL EXTENSION. LANDING GEAR DOWN AND LOCKED W/ MANUAL EXT. WHEN GEAR HANDLE WAS PUT DOWN NOTHING HAPPENEDAFTER GO AROUND PERFORMED QRH/ECAM LG GRAVITY EXTENSION. AFTER COMPLETING OF QRH OVERHEAD PANE - [SDR FDEA2019120103151](https://openairdocs.org/sdr/FDEA2019120103151.md): Skin · delaminated · Nov 30, 2019 · N665FE · Airbus A300F4605R · Spoilers > RT WING NR 4 SPOILER HINGE ARM AND UPR SURFACE FOUND DELAMINATION. REPAIRED THE RT WING NR 4 SPOILER HINGE ARM AND UPR SURFACE DELAMINATION PER SRM57-72-11/201 PARA 12 AND EA 6-5750-T0350630 P1. TITLE: WING - FLIGHT SURFACE - RT NR 4 SPOILER CENTER HINGE ARM - [SDR FDEA2019120103150](https://openairdocs.org/sdr/FDEA2019120103150.md): Skin · delaminated · Nov 30, 2019 · N665FE · Airbus A300F4605R · Spoilers > LT WING NR 5 SPOILER HINGE ARM AND UPR SURFACE FOUND DELAMINATION. REPAIRED THE LT WING NR 5 SPOILER HINGE ARM AND UPR SURFACE DELAMINATION PER SRM57-72-11/201 PARA 12 AND EA 6-5750-T0350601 P1. TITLE: WING - FLIGHT SURFACE - LT NR 5 SPOILER CENTER HINGE ARM - [SDR FDEA201911032850](https://openairdocs.org/sdr/FDEA201911032850.md): Floorbeam · damaged · Nov 3, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Floor Beam > EXISTING REPAIR ON MDCC CROSSBEAM AT FR64 BETWEEN Y953 AND Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR64 BETWEEN Y953 AND Y1456 WAS EVALUATED AND FOUND DID NOT IN CONFORMITY WITH EA: 6-5310-83491. THE REPAIR WAS - [SDR FDEA201911152806](https://openairdocs.org/sdr/FDEA201911152806.md): None · none · Nov 1, 2019 · N665FE · Airbus A300F4605R · Standard Practices/Structures > EXISTING REPAIR ON MDCC SEAT TRACK AT Y0 BETWEEN FR53 AND FR54 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC SEAT TRACK AT Y0 BETWEEN FR53 AND FR54 WAS EVALUATED. THE REPAIR WAS PERFORMED PER EA: 6-5310-T0322392 A. THE REPAIR BETWEEN FR5 - [SDR FDEA201910312791](https://openairdocs.org/sdr/FDEA201910312791.md): Web · cracked · Oct 31, 2019 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MAIN DECK FR47 -Y953 ~ -Y1456 UNDERFLOOR WEB CRACKED REPAIRED THE MAIN DECK FR47 -Y953 ~ -Y1456 UNDERFLOOR WEB CRACK PER A300-600F SRM53-15-15 FIG201. THIS REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002- - [SDR FDEA201910312790](https://openairdocs.org/sdr/FDEA201910312790.md): Web · cracked · Oct 31, 2019 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous Structure > MAIN DECK FR47 Y0 ~ -Y450 UNDERFLOOR WEB CRACKED REPAIRED THE MAIN DECK FR47 Y0 ~ -Y450 UNDERFLOOR WEB CRACK PER A300-600F SRM53- 15-15 FIG201. THIS REPAIR WAS CATEGORY B AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI53-15-15-2-002-00. INSP - [SDR FDEA201910252751](https://openairdocs.org/sdr/FDEA201910252751.md): Floorbeam · cracked · Oct 25, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Floor Beam > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR32, BETWEEN Y1456 AND Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACK AT FR32 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 FIGURE 212 & EA: 6-531 - [SDR FDEA201910252750](https://openairdocs.org/sdr/FDEA201910252750.md): Floorbeam · cracked · Oct 25, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Floor Beam > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR31, BETWEEN Y1456 AND Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACK AT FR31 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 FIGURE 212 & EA: 6-531 - [SDR FDEA201910252749](https://openairdocs.org/sdr/FDEA201910252749.md): Floorbeam · cracked · Oct 25, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Floor Beam > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR30, BETWEEN Y450 AND Y953 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACK AT FR30 BETWEEN Y450 AND Y953 PER A300-600F SRM53-10-15-201 FIGURE 212 & EA: 6-5310- - [SDR FDEA201910242741](https://openairdocs.org/sdr/FDEA201910242741.md): Crossbeam · none · Oct 24, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Structure > EXISTING REPAIR ON MDCC CROSSBEAM AT FR30 BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR30 BETWEEN -Y450 AND -Y953 WAS EVALUATED. NO REPAIR RECORD WAS FOUND AND THE REPAIR DID NOT SUPPORTED BY CURRE - [SDR FDEA201910242739](https://openairdocs.org/sdr/FDEA201910242739.md): Crossbeam · none · Oct 24, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Structure > EXISTING REPAIR ON MDCC CROSSBEAM AT FR29 BETWEEN -Y450 AND -Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR29 BETWEEN -Y450 AND -Y953 WAS EVALUATED. NO REPAIR RECORD WAS FOUND AND THE REPAIR DID NOT SUPPORTED BY CURRE - [SDR FDEA2019102432731](https://openairdocs.org/sdr/FDEA2019102432731.md): Crossbeam · cracked · Oct 23, 2019 · N665FE · Airbus A300F4605R · Fuselage Main, Structure > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BETWEEN -Y1456 AND -Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSSBEAM CRACK AT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F 53-10-15-201 FIGURE 211. MAJOR REPA - [SDR FDEA201811303408](https://openairdocs.org/sdr/FDEA201811303408.md): Bushing · defective · Nov 30, 2018 · N665FE · Airbus A300F4605R · Passenger/Crew Doors > R1 DOOR EXTERNAL HANDLE WILL NOT REMAIN LOCKED IN EXTENDED POSITION THAT ALLOWS DOOR TO BE CLOSED FROM OUTSIDE OF AIRCRAFT. INTERNAL OPERATION OF DOOR OR STOWING OF EXTERNAL HANDLE NOT AFFECTED. FACT 06DEC18 18:18 MEM REMOVED AND REPLACED BUSHINGS IN EXTERIOR - [SDR FDEA201712153397](https://openairdocs.org/sdr/FDEA201712153397.md): Warning Buzzer · inoperative · Dec 15, 2017 · N665FE · Airbus A300F4605R · Escape Slide > MDIS 665 52-70 9733 15DEC17 MEM FACT U RI CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM BUZZER INOP. WARNING LIGHT OPERATE NORMALLY. RELEASED FOR SERVICE PER MEL: 52-73-01-02 CATEGORY: C EXPIRATION: 25DEC17 "MEL 52-73-01-02: R1 CREW ENTRY D - [SDR FDEA201710283089](https://openairdocs.org/sdr/FDEA201710283089.md): Idg · failed · Oct 28, 2017 · N665FE · Airbus A300F4605R · AC Generator-Alternator > DURING CRUISE FLT, FL 320, NR 1 IDG FAULTED, NR 1 GENERATOR OFF AND AC BUSS 1 FAILED. DOUBLE FAILURE OF GENERATOR 1 AND AC BUSS 1. FOLLOWED ECAM AND QRH, UNABLE TO RECOVER EQUIPMENT ON AC BUSS NR 1. REMOVED AND REPLACED NR 1 ENGINE IDG IAW AMM 24-11-11-0 - [SDR FDEA201706201718](https://openairdocs.org/sdr/FDEA201706201718.md): Processor · inoperative · Jun 20, 2017 · N665FE · Airbus A300F4605R · Landing Gear Position and Warning > ON APPROACH AFTER EXTENDING LANDING GEAR, NOTICED THERE WERE NO "BRAKE RELEASE" BARS ON ANY OF THE WHEELS. CYCLED BRAKE & ANTI-SKID SWITCH, NO HELP. SELECTED BRAKE & ANTI-SKID SWITCH OFF AS A PRECAUTION. LANDING WAS GOOD. LOST NOSE WHEEL STEERING ON RO - [SDR FDEA201705131405](https://openairdocs.org/sdr/FDEA201705131405.md): Proximity Sensor · unknown · May 13, 2017 · N665FE · Airbus A300F4605R · Landing Gear Retraction/Extension System > DURING DEPARTURE, LANDING GEAR WOULD NOT RETRACT WITH SYS 1 POSITION DETECTION, SWITCHED TO SYSTEM 2 POSITION DETECTION, STILL WOULD NOT RETRACT, CYCLED SYS 1 AND SYS 2 SEVERAL TIMES, ON FINAL ATTEMPT WITH SYS 2 GEAR RETRACTED. BITE CHECKED PROXIMITY P - [SDR FDEA201704271280](https://openairdocs.org/sdr/FDEA201704271280.md): Stiffener · corroded · Apr 27, 2017 · N665FE · Airbus A300F4605R · Fuselage Main, Plate/Skin > FWD LAV PANEL LOWER O/B HAS CORROSION. REMOVED CORRODED STIFFENER PER SRM 51-40-21, LOCATED AND DRILLED HOLES IN NEW STIFFENER, INSTALLED NEW STIFFENER IAW SRM 51-40-21, PAINTED AREA EXTERNAL SKIN IAW SRM 51-75-10, CLASSIFIED AS MAJOR REPAIR. - [SDR FDEA201704141185](https://openairdocs.org/sdr/FDEA201704141185.md): Floor Panel · damaged · Apr 14, 2017 · N665FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN CARGO FLOOR PANEL 231SG HAS MULTIPLE HOLES. FABRICATED FLOOR PANEL 231SG ON T17/1268908 IAW SRZ-25-005. CLASSIFIED AS CAT "A" MAJOR REPAIR. - [SDR FDEA201704141199](https://openairdocs.org/sdr/FDEA201704141199.md): Floor Panel · cracked · Apr 14, 2017 · N665FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN CARGO FLOOR PANEL 242AJ HAS A CRACK AT THE FASTENER HOLE. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR - [SDR FDEA201704141194](https://openairdocs.org/sdr/FDEA201704141194.md): Frame · dented · Apr 14, 2017 · N665FE · Airbus A300F4605R · Fuselage Main, Frame > MAIN CABIN, FRAME 58 BETWEEN STRINGER 13L AND 14L DENTED AND GOUGED. REMOVED DAMAGE IAW SRM 53-10-13 FIG 202. FABRICATED A REPAIR ANGLE, TREATED AND PRIMED THE REPAIR ANGLE IAW SRM 51- 21-10. INSTALLED THE REPAIR ANGLE IAW SRM 53-10-13 FIG 202 MAJOR REPA - [SDR FDEA201704141186](https://openairdocs.org/sdr/FDEA201704141186.md): Floor Panel · cracked · Apr 14, 2017 · N665FE · Airbus A300F4605R · Fuselage Floor Panel > MAIN CABIN FLOOR PANEL 221PF CRACKED. FABRICATED A NEW FLOOR PANEL. MAJOR REPAIR - [SDR FDEA201704131179](https://openairdocs.org/sdr/FDEA201704131179.md): Floor Panel · delaminated · Apr 13, 2017 · N665FE · Airbus A300F4605R · Fuselage Floor Panel > AFT CARGO BAY FLOOR PANEL 152TF EDGE DELAMINATED. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ-25-005. MAJOR REPAIR. - [SDR FDEA201704131178](https://openairdocs.org/sdr/FDEA201704131178.md): Floor Panel · broken · Apr 13, 2017 · N665FE · Airbus A300F4605R · Fuselage Floor Panel > AFT CARGO BAY FLOOR PANEL 151SF BROKEN ON THE CORNER. A NEW FLOOR PANEL WAS FABRICATED IAW SRZ-25-005. MAJOR REPAIR. Next page: https://openairdocs.org/aircraft/N665FE/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 = 'N665FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N665FE/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.