# Service difficulty reports: N659FE

A list on [N659FE](https://openairdocs.org/aircraft/N659FE.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 · 213 reports

- [SDR FDEA202606150816](https://openairdocs.org/sdr/FDEA202606150816.md): Pressure Deck · corroded · Jun 15, 2026 · N659FE · Airbus A300F4605R · Fuselage Main, Structure
  > FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR 39 - FR 40, BETWEEN Y0 AND Y450 CORRODED. COMPLIED WITH EA 6-5310-T0387809 P1. REPAIRED THE CORRODED AREA AT FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR39 - FR40, BETWEEN Y0 AND Y450. THIS I
- [SDR FDEA202606150815](https://openairdocs.org/sdr/FDEA202606150815.md): Pressure Deck · corroded · Jun 15, 2026 · N659FE · Airbus A300F4605R · Fuselage Main, Structure
  > FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR39 - FR40, BETWEEN -Y1959 AND -Y2462 CORRODED. COMPLIED WITH EA 6-5310-T0387809 P1. REPAIRED THE CORRODED AREA AT FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR39 - FR40, BETWEEN -Y1959 AND -Y246
- [SDR FDEA202606150814](https://openairdocs.org/sdr/FDEA202606150814.md): Pressure Deck · cracked · Jun 15, 2026 · N659FE · Airbus A300F4605R · Fuselage Main, Structure
  > FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR39 - FR40, BETWEEN Y1456 AND Y1959 CORRODED. COMPLIED WITH EA 6-5310-T0387809 P1. REPAIRED THE CORRODED AREA AT FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR39 - FR40, BETWEEN Y1456 AND Y1959.
- [SDR FDEA202606150813](https://openairdocs.org/sdr/FDEA202606150813.md): Pressure Deck · cracked · Jun 15, 2026 · N659FE · Airbus A300F4605R · Fuselage Main, Structure
  > FWD CARGO HORIZONTAL PRESSURE DECK UPPER SURFACE AT FR39 - FR40, Y450 - Y953 CRACKED AND CORRODED. COMPLIED WITH EA 6-5310-T0387809 P1. EA TITLE: FUSELAGE - MAINFRAME - EXFOLIATED CORROSION ON BULKHEAD PRESSURE FLOOR PANEL AT FR40 BETWEEN Y1959 AND Y-2354 - R
- [SDR FDEA202606120807](https://openairdocs.org/sdr/FDEA202606120807.md): Bearing Fitting · faulted · Jun 12, 2026 · N659FE · Airbus A300F4605R · Cargo/Baggage 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 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN
- [SDR FDEA202606110779](https://openairdocs.org/sdr/FDEA202606110779.md): Profile · corroded · Jun 11, 2026 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > BULK CARGO FLOOR SUPPORT AT FR66-FR68, LBL5 CORRODED. FABRICATED THE REPAIR PART PER DWG: A53974262(ISSUE.D) AND PART MARKED AS FXA5397426220400 PER GMM7-0-1001，REPLACED THE CORRODED FLOOR SUPPORT AT BULK CARGO FR66-FR68, Y0-Y140 PER A300-600F SRM5
- [SDR FDEA202606080769](https://openairdocs.org/sdr/FDEA202606080769.md): Web · cracked · Jun 8, 2026 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MDCC UNDERFLOOR WEB AT FR47, BETWEEN -Y953 AND -Y1456 CRACKED. REPAIRED THE MDCC UNDER FLOOR CRACKED WEB AT FR47, BETWEEN -Y953 AND -Y1456 IAW SRM53-15-15-201-C2 FIG.201. THIS REPAIR IS CATEGORY B IAW SRM53-15-15- 201-C2, IT MUST BE INSPECTED AT DEFINED INTE
- [SDR FDEA202606080768](https://openairdocs.org/sdr/FDEA202606080768.md): Web · cracked · Jun 8, 2026 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MDCC UNDERFLOOR WEB AT FR47, BETWEEN Y953 AND Y1456 CRACKED. REPAIRED THE MDCC UNDERFLOOR CRACKED WEB AT FR47, BETWEEN Y953 AND Y1456 IAW SRM 53-15-15-201-C2, FIG.201. THIS REPAIR IS CATEGORY B IAW SRM 53-15-15-201-C2, IT MUST BE INSPECTED AT DEFINED INTERVAL
- [SDR FDEA202605030535](https://openairdocs.org/sdr/FDEA202605030535.md): Door · no discrepancy · May 3, 2026 · N659FE · Airbus A300F4605R · Passenger/Crew Doors
  > WHEN ARRIVED AT A/C TO MOVE JET POST B-CHECK FOUND R1 OUTER DOOR HANDLE INOPERATIVE. OPERATED DOOR SEVERAL TIMES THROUGH FULL RANGE OF LATCHING MOTION USING OUTER HANDLE. DOOR HANDLE CYLED, LATCHED AND FUNCTIONED AS REQUIRED EACH TIME. COULD NOT DUPLICAT
- [SDR FDEA202512112234](https://openairdocs.org/sdr/FDEA202512112234.md): Warning Horn · faulted · Dec 11, 2025 · N659FE · Airbus A300F4605R · Emergency Equipment
  > R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING BUZZER INOPERATIVE. WARNING LIGHT FUNCTIONS NORMAL. GAVE R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING HORN A TAP & IT STARTED WORKING AGAIN. HORN OPS TESTED GOOD IAW AMM 52-73-12-04-02 ABOVE. NO 30 DAY HISTORY. OK FOR SE
- [SDR FDEA202510132006](https://openairdocs.org/sdr/FDEA202510132006.md): Power Supply · inoperative · Oct 13, 2025 · N659FE · Airbus A300F4605R · Emergency Lighting
  > DURING MX PREFLIGHT: COURIOR AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY BATTERY IAW AMM 33-51-14-04. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202510131996](https://openairdocs.org/sdr/FDEA202510131996.md): Power Supply · inoperative · Oct 13, 2025 · N659FE · Airbus A300F4605R · Emergency Lighting
  > DURING MX PREFLIGHT: COURIOR AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY BATTERY IAW AMM 33-51-14-04. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202509301856](https://openairdocs.org/sdr/FDEA202509301856.md): Slide · no discrepancy · Sep 30, 2025 · N659FE · Airbus A300F4605R · Escape Slide
  > R1 CREW ENTRY DOOR ESCAPE SLIDE WILL NOT ARM. CREW ENTRY DOOR ESCAPE SLIDE R1- INOP. SLIDE REMAINS INSTALLED ON DOOR. AMM: 52-10-30-05-02, DOOR FUNCTION TEST AND ECAM INDICATION GOOD IAW AMM. NO ADJUSTMENTS REQUIRED. OPS CHECK GOOD AT THIS TIME, ACFT OK
- [SDR FDEA202407030925](https://openairdocs.org/sdr/FDEA202407030925.md): Door · out of adjust · Jul 3, 2024 · N659FE · Airbus A300F4605R · Passenger/Crew Doors
  > PER CREW WRI 52-10/7294 & 52-10/7295, DOOR L1 DISARM ALARM AT DOOR ALSO ALERTED IN PASSENGER AREA DURING CRUISE. RELEASED FOR SERVICE PER MEL: 52-XX-XX-XX CAT: C EXP: 13JUL24 CREW ENTRY DOOR ESCAPE SLIDE L1 - INOP. SLIDE REMAINS INSTALLED ON DOOR." PERFOR
- [SDR FDEA202407030924](https://openairdocs.org/sdr/FDEA202407030924.md): Warning Message · illuminated · Jul 3, 2024 · N659FE · Airbus A300F4605R · Door Warning System
  > PER CREW WIR 52-XX-XXXX, DOOR L1 DISARM ALARM AT DOOR ALSO ALERTED IN PASSENGER AREA DURING CRUISE.. RELEASED FOR SERVICE PER MEL: 52-XX-XXX CAT: C EXP: 13JUL24 ECAM SLIDE INDICATION SYSTEM FOR L1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE
- [SDR FDEA202407030923](https://openairdocs.org/sdr/FDEA202407030923.md): Warning Message · false activation · Jul 3, 2024 · N659FE · Airbus A300F4605R · Door Warning System
  > LEFT CABIN DOOR OPEN INDICATION AT CRUISE. PRESSURIZATION GOOD. INDICATION WENT OUT DURING DECENT AT APPROX 10K FEET. DOOR DISARM ALARM AT DOOR ALSO ALERTED IN PASSENGER AREA.. RELEASED FOR SERVICE PER MEL: 52-XX-XX CAT: C EXP: 13JUL24 L1 DOOR CLOSED
- [SDR FDEA202401070043](https://openairdocs.org/sdr/FDEA202401070043.md): Frame · cracked · Jan 7, 2024 · N659FE · Airbus A300F4605R · Fuselage Main, Frame
  > AFT CARGO DOOR FWD CUTOUT FRAME 59A DEFORMED BETWEEN STGR40R AND STGR41R COMPLIED WITH EA 6-5310-T0377654 P1 REPAIRED THE GOUGED AND DEFORMED FRAME AT FR59A BETWEEN STGR40R AND STGR41R, THIS IS CAT B REPAIR. THE RDAF 81333802/003/2024#A REPRESENTS A STAGE
- [SDR FDEA202401040036](https://openairdocs.org/sdr/FDEA202401040036.md): Crossbeam · cracked · Jan 4, 2024 · N659FE · Airbus A300* · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT - CRACK FOUND ON CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959 JUST BELOW THE EXISTING REPAIR COMPLIED WITH EA 6-5310-T0377782 P1 REPAIRED THE MAIN DECK CARGO CRACKED CROSSBEAM AT FR64 BETWEEN -Y1456 AND -Y1959. THIS IS CAT B REP
- [SDR FDEA202401040035](https://openairdocs.org/sdr/FDEA202401040035.md): Crossbeam · cracked · Jan 4, 2024 · N659FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR30, BETWEEN Y1456 AND Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR30 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 PARA.15 FIG.212 & EA:
- [SDR FDEA202401030012](https://openairdocs.org/sdr/FDEA202401030012.md): Unknown · unknown · Jan 3, 2024 · N659FE · Airbus A300* · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPR FLANGE FOUND CRACKS AT RIB17 BETWEEN STGR2.8 AND REAR SPAR
- [SDR FDEA202401030011](https://openairdocs.org/sdr/FDEA202401030011.md): Rib · cracked · Jan 3, 2024 · N659FE · Airbus A300F4605R · Trailing Edge Flaps
  > LH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0377620 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB11 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LH
- [SDR FDEA202401030010](https://openairdocs.org/sdr/FDEA202401030010.md): Flap · cracked · Jan 3, 2024 · N659FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPR FLANGE FOUND 3EA CRACKS AT RIB12 STGR2.5-STGR2.7 AND RIB11 STGR2.7-STGR2.8 REPAIRED THE RH WING CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB12 STGR2.5-STGR2.7 AND RIB11 STGR2.7-STGR2.8 PER A300-600F SRM57-50-00-201 PARA.4.A FIG.2
- [SDR FDEA202401030009](https://openairdocs.org/sdr/FDEA202401030009.md): Flap · cracked · Jan 3, 2024 · N659FE · Airbus A300F4605R · Trailing Edge Flaps
  > RH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB15 BETWEEN STGR2.5 AND STGR2.6 REPAIRED THE RH WING CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB15 BETWEEN STGR2.5 AND STGR2.6 PER A300-600F SRM57-50-00-201 PARA.4.A FIG.201 AND REPAIRED THE RH WI
- [SDR FDEA202401020006](https://openairdocs.org/sdr/FDEA202401020006.md): Elevator · none · Jan 2, 2024 · N659FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON LH ELEVATOR T/E LOWER SKIN ER2-ER5 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON LH ELEVATOR T/E LOWER SKIN ER2-ER5 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM55-21-12-201 FIGURE 201. RSC TRACKING EA: 6-5520- T0
- [SDR FDEA202401020005](https://openairdocs.org/sdr/FDEA202401020005.md): Flap · unknown · Jan 2, 2024 · N659FE · Airbus A300F4605R · Leading Edge Devices
  > EXISTING REPAIR ON LH WING KRUEGER FLAP INNER SKIN, FROM I/B EDGE 5", FROM LOWER EDGE 10" REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON LH WING KRUEGER FLAP INNER SKIN, FROM I/B EDGE 5", FROM LOWER EDGE 10" WAS EVALUATED AND FOUND IN CONFORMITY
- [SDR FDEA202401020004](https://openairdocs.org/sdr/FDEA202401020004.md): Flap · unknown · Jan 2, 2024 · N659FE · Airbus A300F4605R · Leading Edge Devices
  > EXISTING REPAIR ON LH WING KRUEGER FLAP I/B UPPER SKIN, FROM LOWER EDGE 16.3" REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON LH WING KRUEGER FLAP I/B UPPER SKIN, FROM LOWER EDGE 16.3" WAS EVALUATED AND FOUND IN CONFORMITY WITH TAG: 8875B2 AND A3
- [SDR FDEA202312261957](https://openairdocs.org/sdr/FDEA202312261957.md): Stringer · corroded · Dec 26, 2023 · N659FE · Airbus A300F4605R · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER AT STGR44RH BETWEEN FR38.2 AND FR39 FOUND CORROSION REPAIRED THE FUSELAGE CORRODED STRINGER AT STGR44RH BETWEEN FR38.2 AND FR39 PER A300-600F SRM53-10-14-201 FIG.208. THIS IS CAT B REPAIR. THE FIRST INSPECTION WAS 51000FC / 89000FH AFTER
- [SDR FDEA202311281918](https://openairdocs.org/sdr/FDEA202311281918.md): Rib · damaged · Nov 28, 2023 · N659FE · Airbus A300* · Fuselage Structure (General)
  > L/H MLG RIB 5 FWD LUG HAS MINOR IMPACT DAMAGE ON FWD AND AFT SIDES. REPAIRED PER E.A. 6-5710-T0377239 PT 1.
- [SDR FDEA202311281910](https://openairdocs.org/sdr/FDEA202311281910.md): Fitting · corroded · Nov 28, 2023 · N659FE · Airbus A300F4605R · Main Landing Gear Attach Section
  > L/H MLG RIB 5 HAS CORROSION UNDER SPLIT BUSHINGS FWD LUG. APPROX 10 O'CLOCK LOOKING AFT. REPAIRED PER AIRBUS REPAIR INSTRUCTIONS R57240425.
- [SDR FDEA202106041449](https://openairdocs.org/sdr/FDEA202106041449.md): Fitting · cracked · Jun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > 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 EA: 6-5710-T0345244 B P6. TITLE: WINGS - BASIC WING STRUCTURE - CRACKED CRACKED HOLES AT FR47 REAR SPAR ARE
- [SDR FDEA202106041448](https://openairdocs.org/sdr/FDEA202106041448.md): Fitting · cracked · Jun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "H" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 B P1 STEP 4.D-4.E, TITLE: WINGS - CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM
- [SDR FDEA202106041447](https://openairdocs.org/sdr/FDEA202106041447.md): Floor Support · corroded · Jun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FR11-FR13A Y730 FLOOR SUPPORT FOUND HEAVY CORROSION REPLACED THE MAIN DECK FR11-FR13A Y730 CORRODED FLOOR SUPPORT WITH A FABRICATION PART PER A300-600F SRM 51-40-21 AND DWG A53612214 ISSUE V00. THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100
- [SDR FDEA202106041446](https://openairdocs.org/sdr/FDEA202106041446.md): Web · cracked · Jun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FR47 Y0 ~ -Y450 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB OF MAIN DECK UNDERFLOOR AT FR47 Y0~ -Y450 PER A300- 600F SRM53-15-15 FIG201. THIS IS CAT B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-15-15-2-002-00. IN
- [SDR FDEA202106041445](https://openairdocs.org/sdr/FDEA202106041445.md): Web · cracked · Jun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN DECK FR47 Y0 ~ Y450 UNDERFLOOR WEB CRACKED REPAIRED THE CRACKED WEB OF MAIN DECK UNDERFLOOR AT FR47 Y0~Y450 PER A300-600F SRM53-15-15 FIG201. THIS IS CAT B REPAIR AND IT MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-15-15-2-002-00. INSP
- [SDR FDEA202106041444](https://openairdocs.org/sdr/FDEA202106041444.md): Crossbeam · cracked · Jun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Main, Structure
  > MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR32, BETWEEN Y1456 AND Y1959 REPAIRED THE MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CRACKED CROSSBEAM AT FR32 BETWEEN Y1456 AND Y1959 PER A300-600F SRM53-10-15-201 FIG.212. THIS IS C
- [SDR FDEA202103140641](https://openairdocs.org/sdr/FDEA202103140641.md): Cylinder · failed · Mar 14, 2021 · N659FE · Airbus A300F4605R · Emergency Equipment
  > MDIS 659 25-60 3699 14MAR21 MEM OPEN U WHILE PER FORMING WIC 2561200-00-21 MOD TYPE W MOD NO. 6-2561200-00-21 REV NO. PS R1 CTA 6-0505-1-4805 REV BF: OPERATIONALLY TEST & REPLACE ESCAPE SLIDE - OPC DOOR ASSIST BOTTLE FAILED OPERATIONAL CHE
- [SDR FDEA2020052981074](https://openairdocs.org/sdr/FDEA2020052981074.md): Computer · failed · May 28, 2020 · N659FE · Airbus A300F4605R · Trailing Edge Flap Control System
  > 28MAY20, ON FINAL INTO KRIC FLYING ILS16 AFTER FLAPS WERE EXTENDED TO 20, RECEIVED ECAM AND FLAP WARNING. RECYCLED NO SUCCESS. FLEW BOX PATTERN COMPLETED QRH LANDED 30/20 FLAPS REMAINED 20 AFTER LANDING. TROUBLESHOOTING PROBLEM DOWN TO NR 2 SFCC UNIT PART O
- [SDR FDEA201909242333](https://openairdocs.org/sdr/FDEA201909242333.md): Unknown · odor · Sep 24, 2019 · N659FE · Airbus A300F4605R · Air Distribution System
  > PDIS 659 36-10 2144 24SEP19 ATL FACT U LOGPAGES:3140271 NOTICED STRONG BURNING ODOR ON TAXI OUT IN ATL. AFTER GEAR UP CALL FLAPS 2 SYS FAULT BEFORE WE EVEN CALLED FOR SLATS RETRACT. STRONG BURNING SMELL CONTINUED ALL THE WAY TO GATE. SHGN 24SE
- [SDR FDEA201903190676](https://openairdocs.org/sdr/FDEA201903190676.md): Fitting · cracked · Mar 19, 2019 · N659FE · Airbus A300F4605R · Wing, Center Box
  > FUSELAGE CTR WING BOX REAR SPAR HOLE C NDT INSPECTION FOUND CRACK (LT) COMPLIED WITH EA: 6-5710-T0345244 P1, TITLE: WINGS - BASIC WING STRUCTURE - EO 6-5710-7-3305E3 P3 & P4 - CRACK HOLES AT FR47 REAR SPAR AREA. REPAIRED FUSELAGE CTR WING BOX REAR SPAR LH HO
- [SDR FDEA201903190674](https://openairdocs.org/sdr/FDEA201903190674.md): Fitting · cracked · Mar 19, 2019 · N659FE · Airbus A300F4605R · Wing, Center Box
  > FUSELAGE CTR WING BOX REAR SPAR RH HOLE F NDT INSPECTION FOUND CRACK COMPLIED WITH EA: 6-5710-T0345244 P1, TITLE: WINGS - BASIC WING STRUCTURE - EO 6- 5710-7-3305E3 P3 & P4 - CRACK HOLES AT FR47 REAR SPAR AREA. REPAIRED FUSELAGE CTR WING BOX REAR SPAR RT HOLE
- [SDR FDEA201903170665](https://openairdocs.org/sdr/FDEA201903170665.md): Fitting · cracked · Mar 17, 2019 · N659FE · Airbus A300F4605R · Fuselage Main, Frame
  > EO 6-5310-E0330747 A P1 INSPECTION FOUND THE LOWER FRAME BASE FITTING HAS CRACK AT RT FR46 AREA 1 COMPLIED WITH EO #:6-5310-E0330747 B P14, TITLE:FUSELAGE-MAINFRAME- INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 AND 46, SB A300-53-6177. REPAIRED THE
- [SDR FDEA201903170664](https://openairdocs.org/sdr/FDEA201903170664.md): Fitting · cracked · Mar 17, 2019 · N659FE · Airbus A300F4605R · Fuselage Main, Frame
  > EO 6-5310-E0330747 A P1 INSPECTION FOUND THE LOWER FRAME BASE FITTING HAS CRACK AT RT FR45 AREA 1 COMPLIED WITH EO #:6-5310-E0330747 B P12, TITLE:FUSELAGE-MAINFRAME- INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 AND 46, SB A300-53-6177. REPAIRED THE
- [SDR FDEA201903170663](https://openairdocs.org/sdr/FDEA201903170663.md): Fitting · cracked · Mar 17, 2019 · N659FE · Airbus A300F4605R · Fuselage Main, Frame
  > EO 6-5310-E0330747 A P1 INSPECTION FOUND THE LOWER FRAME BASE FITTING HAS CRACK AT RT FR44 AREA 1 COMPLIED WITH EO #:6-5310-E0330747 B P10, TITLE:FUSELAGE-MAINFRAME- INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 AND 46, SB A300-53-6177. REPAIRED THE
- [SDR FDEA201903170661](https://openairdocs.org/sdr/FDEA201903170661.md): Fitting · cracked · Mar 17, 2019 · N659FE · Airbus A300F4605R · Fuselage Main, Frame
  > EO 6-5310-E0330747 A P1 INSPECTION FOUND THE LOWER FRAME BASE FITTING HAS CRACK AT LT FR46 AREA 1 COMPLIED WITH EO #:6-5310-E0330747 B P13, TITLE:FUSELAGE-MAINFRAME- INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 AND 46, SB A300-53-6177. REPAIRED THE
- [SDR FDEA201903170660](https://openairdocs.org/sdr/FDEA201903170660.md): Fitting · cracked · Mar 17, 2019 · N659FE · Airbus A300F4605R · Fuselage Main, Frame
  > EO 6-5310-E0330747 A P1 INSPECTION FOUND THE LOWER FRAME BASE FITTING HAS CRACK AT LT FR44 AREA 1 COMPLIED WITH FEDEX EO #:6-5310-E0330747 B P9, TITLE:FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 AND 46, SB A300-53-6177. REPAIRED
- [SDR FDEA201802230474](https://openairdocs.org/sdr/FDEA201802230474.md): Hose · leaking · Feb 23, 2018 · N659FE · Airbus A300F4605R · Hydraulic System, Main
  > ECAM ALERT FOR HYD RSVR LO LEVEL, PASSING THROUGH FL 320 FOR FL 350. ACCOMPLISHED ECAM PROCEDURES, ACCOMPLISHED QRH PROCEDURE. GRAVITY EXTENDED LANDING GEAR. EMERGENCY DECLARED AND LANDED. REPLACED THE NR 2 ENGINE GREEN SYS HYD PUMP PRESSURE HOSE ASSY IAW
- [SDR FDEA201712133380](https://openairdocs.org/sdr/FDEA201712133380.md): Switch · failed · Dec 13, 2017 · N659FE · Airbus A300B4605R · Fuel Pressure Sensor
  > ON CLIMB OUT FROM KFAR GOT FUEL CLOG LIGHT NR 2 ENG PASSING 10,000 FT. COMPLIED WITH ECAM AND REDUCED POWER. FUEL CLOG LIGHT WENT OUT AT A LOW POWER SETTING. ADVANCED POWER AND CLOG LIGHT CAME BACK ON. R&R NR 2 ENG FUEL FILTER IAW MM 73-12-02-04, FILETR R
- [SDR FDEA201708232329](https://openairdocs.org/sdr/FDEA201708232329.md): Buss · inoperative · Aug 23, 2017 · N659FE · Airbus A300F4605R · Emergency Lighting
  > COURIER EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED AC SERVICE BUSS IAW AMM 24-42-11-04. OPS CHECKED GOOD.
- [SDR FDEA201708192284](https://openairdocs.org/sdr/FDEA201708192284.md): Power Supply · malfunctioned · Aug 19, 2017 · N659FE · Airbus A300F4605R · Emergency Equipment
  > RIGHT CABIN DOOR DOES NOT SHOW ARMED ON ECAM WITH HANDLE IN ARMED POSITION. RESET AUTONOMOUS STANDBY POWER SUPPLY UNIT PER MM 52-73-18-04 AND ACCOMPLISHED OPS CHECK OF R1 DOORWARNING SYSTEM IAW AMM 52-73-13-05-02. SYSTEM OPS CHECKS GOOD AT THIS TIME. NO
- [SDR FDEA201707222021](https://openairdocs.org/sdr/FDEA201707222021.md): Pump · failed · Jul 22, 2017 · N659FE · Airbus A300F4605R · Hydraulic Pump (Electric/Engine), Main
  > AFTER TAKE OFF, AMBER LEFT ECAM FOR YELLOW HYD SYS LOW PRESSURE WITH ACCOMPANYING OVERHEAD YELLOW ENGINE HYD LOW PRESSURE LIGHT. TROUBLESHOT TO EGP, REMOVED AND REPLACED THE PUMP IAW AMM 29-11-32-04-02 AND REPLACED CASE DRAIN FILTER IAW MM 29-11-36-04-02. L

Next page: https://openairdocs.org/aircraft/N659FE/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 = 'N659FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N659FE/reports

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