N659FE

Service difficulty reports · 213

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 = 'N659FE' 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 FDEA202606150816Pressure Deck · corrodedFWD 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 IJun 15, 2026 · N659FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202606150815Pressure Deck · corrodedFWD 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 -Y246Jun 15, 2026 · N659FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202606150814Pressure Deck · crackedFWD 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. Jun 15, 2026 · N659FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202606150813Pressure Deck · crackedFWD 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 - RJun 15, 2026 · N659FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202606120807Bearing Fitting · faultedCARGO 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 MAINJun 12, 2026 · N659FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202606110779Profile · corrodedBULK 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 SRM5Jun 11, 2026 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202606080769Web · crackedMDCC 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 INTEJun 8, 2026 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202606080768Web · crackedMDCC 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 INTERVALJun 8, 2026 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202605030535Door · no discrepancyWHEN 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 DUPLICATMay 3, 2026 · N659FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202512112234Warning Horn · faultedR1 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 SEDec 11, 2025 · N659FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202510132006Power Supply · inoperativeDURING 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.Oct 13, 2025 · N659FE · Airbus A300F4605R · Emergency LightingSDR FDEA202510131996Power Supply · inoperativeDURING 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.Oct 13, 2025 · N659FE · Airbus A300F4605R · Emergency LightingSDR FDEA202509301856Slide · no discrepancyR1 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 OKSep 30, 2025 · N659FE · Airbus A300F4605R · Escape SlideSDR FDEA202407030925Door · out of adjustPER 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." PERFORJul 3, 2024 · N659FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202407030924Warning Message · illuminatedPER 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 Jul 3, 2024 · N659FE · Airbus A300F4605R · Door Warning SystemSDR FDEA202407030923Warning Message · false activationLEFT 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 CLOSEDJul 3, 2024 · N659FE · Airbus A300F4605R · Door Warning SystemSDR FDEA202401070043Frame · crackedAFT 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 STAGEJan 7, 2024 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202401040036Crossbeam · crackedMAIN 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 REPJan 4, 2024 · N659FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202401040035Crossbeam · crackedMAIN 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:Jan 4, 2024 · N659FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202401030012Unknown · unknownLH WING CENTER FLAP RIB UPR FLANGE FOUND CRACKS AT RIB17 BETWEEN STGR2.8 AND REAR SPARJan 3, 2024 · N659FE · Airbus A300* · Trailing Edge FlapsSDR FDEA202401030011Rib · crackedLH 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 - LHJan 3, 2024 · N659FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202401030010Flap · crackedRH 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.2Jan 3, 2024 · N659FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202401030009Flap · crackedRH 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 WIJan 3, 2024 · N659FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202401020006Elevator · noneEXISTING 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- T0Jan 2, 2024 · N659FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202401020005Flap · unknownEXISTING 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 CONFORMITYJan 2, 2024 · N659FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA202401020004Flap · unknownEXISTING 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 A3Jan 2, 2024 · N659FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA202312261957Stringer · corrodedFUSELAGE 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 Dec 26, 2023 · N659FE · Airbus A300F4605R · Fuselage Main, Longeron/StringerSDR FDEA202311281918Rib · damagedL/H MLG RIB 5 FWD LUG HAS MINOR IMPACT DAMAGE ON FWD AND AFT SIDES. REPAIRED PER E.A. 6-5710-T0377239 PT 1.Nov 28, 2023 · N659FE · Airbus A300* · Fuselage Structure (General)SDR FDEA202311281910Fitting · corrodedL/H MLG RIB 5 HAS CORROSION UNDER SPLIT BUSHINGS FWD LUG. APPROX 10 O'CLOCK LOOKING AFT. REPAIRED PER AIRBUS REPAIR INSTRUCTIONS R57240425.Nov 28, 2023 · N659FE · Airbus A300F4605R · Main Landing Gear Attach SectionSDR FDEA202106041449Fitting · crackedCENTER 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 AREJun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202106041448Fitting · crackedCENTER 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 Jun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202106041447Floor Support · corrodedMAIN 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 GMM6-2-100Jun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202106041446Web · crackedMAIN 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. INJun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202106041445Web · crackedMAIN 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. INSPJun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202106041444Crossbeam · crackedMAIN 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 CJun 4, 2021 · N659FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202103140641Cylinder · failedMDIS 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 CHEMar 14, 2021 · N659FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA2020052981074Computer · failed28MAY20, 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 OMay 28, 2020 · N659FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201909242333Unknown · odorPDIS 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 24SESep 24, 2019 · N659FE · Airbus A300F4605R · Air Distribution SystemSDR FDEA201903190676Fitting · crackedFUSELAGE 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 HOMar 19, 2019 · N659FE · Airbus A300F4605R · Wing, Center BoxSDR FDEA201903190674Fitting · crackedFUSELAGE 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 HOLEMar 19, 2019 · N659FE · Airbus A300F4605R · Wing, Center BoxSDR FDEA201903170665Fitting · crackedEO 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 THEMar 17, 2019 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201903170664Fitting · crackedEO 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 THEMar 17, 2019 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201903170663Fitting · crackedEO 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 THEMar 17, 2019 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201903170661Fitting · crackedEO 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 THEMar 17, 2019 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201903170660Fitting · crackedEO 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. REPAIREDMar 17, 2019 · N659FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201802230474Hose · leakingECAM 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 Feb 23, 2018 · N659FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201712133380Switch · failedON 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 RDec 13, 2017 · N659FE · Airbus A300B4605R · Fuel Pressure SensorSDR FDEA201708232329Buss · inoperativeCOURIER EMERGENCY LIGHT WILL NOT TEST. REMOVED AND REPLACED AC SERVICE BUSS IAW AMM 24-42-11-04. OPS CHECKED GOOD.Aug 23, 2017 · N659FE · Airbus A300F4605R · Emergency LightingSDR FDEA201708192284Power Supply · malfunctionedRIGHT 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 Aug 19, 2017 · N659FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA201707222021Pump · failedAFTER 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. LJul 22, 2017 · N659FE · Airbus A300F4605R · Hydraulic Pump (Electric/Engine), Main
Back to N659FE