Airbus A310-304

Service difficulty reports · 238

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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 aircraft_model_key = 'A310304'
  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 06FDEA03042Door · misrepairedFOUND REPAIR RT APU DOOR BETWEEN STA 4969/5001 FS 97/98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR . NEW REPAIR ACAug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) DoorsSDR 06FDEA03041Door · misrepairedFOUND REPAIR RT APU DOOR BETWEEN STA 4937/4969 FR 96/97 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLAug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) DoorsSDR 06FDEA03040Door · misrepairedFOUND REPAIR LOCATED LT APU DOOR BETWEEN STA 5033/5045 FS 99/99. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR. ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIRAug 22, 2006 · N817FD · Airbus A310304 · Auxiliary Power Unit (APU) DoorsSDR 06FDEA03039Skin · damagedPREVIOUS REPAIR FOUND AT BULK COMP´T DOOR SKIN LOCATED AT BEAM 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR ACCOMPLISHED USING FAA DATA EXISTING REPAIR COVERED BY RAS REF:RAS/DAHAM/4014519/2001. REPAIR EVALUATED PER GMM 6-2-100Aug 22, 2006 · N817FD · Airbus A310304 · Cargo/Baggage DoorsSDR 06FDEA3036None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT FUSELAGE SKIN LOCATED BETWEEN FS 64/67 AND BETWEEN STRG 33/40 RT . REPAIR REQUIRES EVALUATION FORAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3037None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT FUSELAGE SKIN LOCATED BETWEEN FS 66/68 AND BETWEEN STRG 48/54 RT . REPAIR REQUIRES EVALUATION FORAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3038None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED LT FS4715/4760, FS 89/90, STRG 33/38 NEXT TO APU INLET. REPAIR REQUIRED EVALUATION FOR MAJOR/ MINOR DAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3039None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. PREVIOUS REPAIR FOUND AT BULK COMP´T DOOR SKIN LOCATED AT BEAM 5. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATIONAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3040None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED LT APU DOOR BETWEEN STA 5033/5045 FS 99/99. REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATIONAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3041None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT. FOUND REPAIR RT APU DOOR BETWEEN STA 4937/4969 FS 96/97 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THEAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3042None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR RT APU DOOR BETWEEN STA 4969/5001 FS 97/98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND REPAAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3043None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 4986/5003 FR 98. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3044None · noneNR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT APU DOOR BETWEEN STA 5055/5065 FS 100/100. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATIOAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3054None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AND UPPER SKIN SURFACE OF T/E RIB 11/RIB 12. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVEAug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3053None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED MLG RT W/W DOOR AT INNER LOWER SKIN SURFACE AT OUTB LOWER PART. REPAIR REQUIRE EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3052None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED AT RT ELEVATOR AT INNER LOWER SKIN SURFACE STA 833/ ER 38 AND STA 791/ ER36. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3051None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED RT ELEVATOR AT INNER LOWER SKIN STA 604/ER26 AND STA 566/ER 24. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3050None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED ON LT NR 2 SLAT SKIN SURFACE OF L/E BETWEEN RIB 44/45 (NEXT JACK RIB 4). REPAIR REQUIRES EVALUATION FOR MAJOR/ MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3049None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1. FOUND REPAIR LOCATED INBD FLAP LT AT LOWER SURFACE AT RIB 8/ RIB 10. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA.Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3048None · noneFOUND REPAIR LOCATED LT INBD FLAP AT T/E UPPER AND LOWER SKIN SURFACE BETWEEN RIB 5 AND RIB 8. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3047None · noneFOUND REPAIR LOCATED RT OUTB FLAP AT INNER LOWER SKIN SURFACE AT T/E OF INBD OF RIB 3. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR 06FDEA3046None · noneCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, FOUND REPAIR LOCATED RT INB FLAP AT INNER LOWER AND UPPER SKIN SURFACE AT T/E OF FLAP RIB 19. REPAIR REQUIRE EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR ACCOMPLISHED USING FAA APPROVED DATA.Aug 22, 2006 · N817FD · Airbus A310304 · Standard Practices/StructuresSDR CA060502002Wire · burned(CAN) DURING ROUTINE INSPECTION, FOUND THE ELECTRICAL OUTLET WIRE FIN 8ME CHAFED ON FRAME 17 BETWEEN STR 28 AND 29 RT SIDE. THE GROMMET PROTECTION HAD FALLEN OFF FROM THE FRAME AND WIRE WAS HANGING ON THE FRAME WITH THE RESULT OF ARCING AND FRAME DAMAGE. THE WApr 27, 2006 · Airbus A310304 · Electrical Power System WiringSDR CA060502003Wire · burned(CAN) DURING AIRCRAFT TOWING, THE NAV 2 POSITION LIGHT CB POPPED. UNABLE TO RESET. DURING INVESTIGATION, FOUND THE 4 WIRES FROM THE LIGHT UNIT ASSY (7LA) BURNED ABOUT 8 INCHES LONG. WIRING WAS REPLACED AND LIGHT ASSEMBLY AND RELAY WERE REPLACED AS PRECAUTIONARApr 22, 2006 · Airbus A310304 · Light System WiringSDR CA051130001Flap System · malfunctionedDURING APPROACH, ECAM MESSAGE CAME ON FLAP SYSTEM 1 AND 2 FAULT AT POSITION 15/20. RETURNED FLAP TO 0 THE SAME THING HAPPENED ON SECOND ATTEMPT. DURING INSPECTION, FOUND THE RIGHT TORQUE LIMITER FLAP GEAR BOX NR 1 INDICATOR TRIPPED. INDICATOR RESET AND OIL Nov 28, 2005 · Airbus A310304 · Trailing Edge Flap Control SystemSDR CA050808001Circuit Breaker · burned(CAN) DURING ENGINES GROUND RUN AFTER A ROUTINE INSPECTION VISIT, THE FOLLOWING CIRCUIT BREAKERS WERE FOUND POPPED, FUEL LT INNER TANK PUMP NR 1, FUEL RT INNER TANK PUMP NR 2, FUEL CENTER TANK RT PUMP, FUEL LT OUTER TANKPUMP NR 1 AND AFT CABIN FAN. DURING INVAug 4, 2005 · Airbus A310304 · Electrical Power SystemSDR CA050726001Bolt · broken(CAN) DURING TRANSIT CHECK INSPECTION, FOUND NR 2 MAIN WHEEL WITH 2 EA BROKEN TIE BOLTS. THE MAIN WHEEL ASSEMBLY WAS REPLACED. DURING REPLACEMENT OF THE WHEEL ASSEMBLY, FOUND THE BRAKE DAMAGE BY THE BROKEN TIEBOLTS. THE BRAKE ASSEMBLY WAS ALSO REPLACED.Jul 23, 2005 · Airbus A310304 · Wheel/Ski/FloatSDR CA050516008Inverter · failed(CAN) DURING FLIGHT DECK PREPARATION WITH EXTERNAL POWER OFF AND BATTERIES POWER ON, SMOKE ODOR WAS NOTICED IN FLIGHT DECK. DURING INVESTIGATION FOUND STATIC INVERTER AT FAULT WITH THE SUPPLIED FUSE BLOWN. BOTH UNITS WERE REPLACED. ALSO THIS POWER PROBLEM DISApr 26, 2005 · Airbus A310304 · AC InverterSDR CA050301001Tube · odor(CAN) DURING PRE-DEPARTURE CHECK, ON THE GROUND, BURN SMELL WAS NOTICED FROM RT ECAM SYSTEM. DISPLAY UNIT WAS REMOVED AND INSPECTED. NO FAULT WAS FOUND AND SYSTEM WAS DEACTIVATED UNDER MEL. UNIT WAS REPLACED AT THE NEXT STATION. UNIT WAS SENT TO THE OEM FOR Feb 25, 2005 · Airbus A310304 · Central WarningSDR CA041020003Strut · lack of lube(CAN) ON APPROACH TO AIRPORT, FLIGHT CREW WAS UNABLE TO OBTAIN POSITIVE NOSE LANDING GEAR DOWN LOCK INDICATION EVEN AFTER SEVERAL CYCLES. A LANDING GEAR GRAVITY EXTENSION WAS CARRIED OUT SUCCESSFULLY.TROUBLE SHOOTING OF THE ELECTRICAL INDICATION SYSTEM DID NOTOct 16, 2004 · Airbus A310304 · Main Landing Gear Strut/Axle/TruckSDR CA040924001Vapor Barrier · damaged(CAN) DURING INVEST OF A PNEUMATIC LEAK AT LT A/C PACK DISCHARGE DUCT HEAT EXCHANGER CONNECTOR, FUEL VAPOR BARRIERS FOUND DAMAGED ABOVE THIS AREA. METAL FUEL VAPOR BARRIER HAD DAMAGE OF APPROX 2 SQ FT. FIBER FUEL VAPOR BARRIER PUNCTURED 2 SQ. IN. FUEL VAPORSep 18, 2004 · Airbus A310304 · Air Distribution SystemSDR CA040909004Control Unit · malfunctioned(CAN) IN CRUISE, NR 5 SPOILER EXTENDED MOMENTARY FOLLOWED BY SPOILER 5FAULT ON ECAM. SPOILER PANEL RETRACTED ON IT S OWN. SPOILER RESET AFTER LANDING AND CHECKED OK.TROUBLING SHOOTING INDICATED NR 2 EFCU AT FAULT. NR 2 EFCU REPLACED AND DFDR REMOVED AND SENTSep 6, 2004 · Airbus A310304 · Auto Flight SystemSDR CA040916003Reservoir · discharged(CAN) FL320, AROUND 2 HRS PRIOR TO ARRIVAL IN YYZ, LT OVERWING EMERGENCY EVACUATION SLIDE HAD STARTED TO PARTIALLY INFLATE IN FLIGHT. CREW DECIDED TO LAND AT CLOSEST SUITABLE AIRPORT WITH MX. AFTER ALL PAX DEPLANNED, DISARMED LT OVERWING DOOR & OPENED IT NORMAAug 1, 2004 · Airbus A310304 · Escape SlideSDR CA040630005Fitting · loose(CAN) ON FINAL APPROACH, WHEN FLAP/SLAT WERE EXTENDED, THE HYDRAULIC RESERVOIR LOW LEVEL ECAM WARNING CAME ON. AIRCRAFT OVERSHOT AND CHECKLIST PROCEDURE INDICATE A FAILURE OF GREEN HYDRAULIC SYSTEM. ALTERNATE GEAR EXTENSION PERFORMED. DURING INVESTIGATION,Jun 29, 2004 · Airbus A310304 · Hydraulic System, MainSDR CA040603005Wire · chafed(CAN) AIRCRAFT ARRIVED WITH THE RT OUTER TANK FUEL PUMP NR 1 LOW PRESSURE LIGHT ON. FOLLOWING TROUBLE SHOOTING, THE WIRE FOR NR 1 RT OUTER PUMP WAS FOUND SHORTED IN THE CONDUIT AT REAR SPAR WS 915.0. WIRE WAS REPLACED. MFG WAS ADVISED OF THIS PROBLEM. A CAJun 2, 2004 · Airbus A310304 · Engine Fuel System WiringSDR CA040427007Wire · damaged(CAN) FLIGHT CREW REPORTED LT SIDE WINDSHIELD HEAT C/B POPPING. WINDSHIELD HEAT REGULATOR REPLACED. FURTHER INVESTIGATION REVEALED AN OPEN WIRE BETWEEN PIN J AND GROUND. FOUND THE ELECTRICAL RETRACTABLE CORD DAMAGE BELOW THE SLIDING WINDOW. CORD ASSEMBLY WAApr 15, 2004 · Airbus A310304 · Ice/Rain Protection System WiringSDR CA040203015Adapter · mismanufactured(CAN) THIS PROBLEM AFFECTS AIRCRAFT MODIFIED BY INSTALLATION OF AN EMS MODIFICATION IAW STC SA97-50 ONLY. SEAT TRACK ADAPTERS, PN 6372 HAVE BEEN DETERMINED TO BE UNDER STRENGTH BY DESIGN. DESIGN DOES NOT MEET THE CERTIFICATION BASIS OF THE AIRCRAFT.Jan 29, 2004 · Airbus A310304 · Fuselage, Seat/Cargo Attach FittingsSDR CA030421001Hose · ruptured(CAN) ON FINAL APPROACH WHEN GEAR SELECTEDDOWNGREEN HYDRAULIC SYSTEM QUANTITY DROPPED TO NEARLY ZERO .DURING INVESTIGATION FOUND THE HYDRAULIC DOWN LINE RUPTURED AT THE UPPER RIGHT HAND MAIN LANDING GEAR SWIVEL AREA. LINE WAS REPLACED AND SYSTEM TESTED SERVICEApr 16, 2003 · Airbus A310304 · Landing Gear Retraction/Extension SystemSDR CA030214011Wire · burned(CAN) ENGINE NR 2, HYDRAULIC FIRE SHUTOFF VALVE, CIRCUIT BREAKER 558 POPPING AND WILL NOT RESET. INSPECTION FOUND WIRING DAMAGED (P/N'S: 2912-5006, 2912-5007 AND 29-5003)(BURNT OVER 12INCHES)FROMCONNECTOR OF THE NR 2 ENGINE FIRE SHUTOFF VALVE (YELLOW SYSTEM),Jan 30, 2003 · Airbus A310304 · Hydraulic Power System WiringSDR CA021108021Bolt · sheared(CAN) DURING AIRCRAFT WALK AROUND, FOUND NR 4 MLG WHEEL ASSY BOLT SHEARED AND MISSING.Oct 12, 2002 · Airbus A310304 · Wheel/Ski/FloatSDR CA011101021Circuit Breaker · failed(CAN) 1. ON TAKEOFF, FLIGHT CREW HEARD CB'S POP WITH SMELL OF BURNING PLASTIC.2. EMERGENCY DECLARED & AIRCRAFT RETURNED TO YYZ. AIRCRAFT LANDED WITHOUT INCIDENT. 3. UPON INSPECTION CB'S J71J74 & K73 WERE FOUND POPPED WITH VISIBLE SIGNS OF ARCING. ALL CB'S REPLOct 9, 2001 · Airbus A310304 · AC Power Distribution SystemSDR CA010815004Warning System · false activation(CAN) 1. DURING TAKEOFF, ECAM WARNING FOR BULK CARGO DOOR INDICATION. AIRCRAFT RETURNED TO GATE. SYSTEM CHECKED AND MEL 52-7-0 APPLIED. AIRCRAFT RELEASED FOR FLIGHT. 2. NO PROBLEM DURING SUBSEQUENT FLIGHT. 3. UPON ARRIVAL TO HOME BASE, BULK CARGO DOOR INDICATIJul 20, 2001 · Airbus A310304 · Door Warning SystemSDR AUS20010785Computer · faulty(AUS) FLIGHT AUGMENTATION COMPUTER FAULTY.Jul 15, 2001 · Airbus A310304 · Flight Management Computing Hardware SystemSDR CA010815003Door · missing(CAN) 1. DURING THE TURNAROUND IT WAS OBSERVED THAT THE MID LAV SERVICING PANEL DOOR WAS MISSING. 2. DMI 35881 WAS RAISED UNDER CDL 52-4. AIRCRAFRT RELEASED FOR FLIGHT.3. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT.Jul 13, 2001 · Airbus A310304 · Service DoorsSDR CA010815005Controller · failed(CAN) 1. AT CRUISE, ECAM CONTROLLER SHOWED SIGNS OF BEING ERRATIC, FLASHING THEN TURNED BLACK. SMOKE STARTED FOR 10 SECONDS WITH ELECTRICAL SMELL. CB POPPED AND SMOKE STOPPED. NOT ENOUGH SMOKE TO DON O2 MASKS. 2. PHONE PATCH MADE TO DISPATCH REGARDING PROBLEM.Jun 20, 2001 · Airbus A310304 · Central WarningSDR CA010511028Heater · failed(CAN) DURING FLIGHT, SMOKE WAS OBSERVED COMING FROM FORWARD GALLEY NR 2 BOILER. ALL CB PULLED & GALLEY POWER SHEDDED. NO MORE SMOKE OBSERVED & FLIGHT CONTINUED WITHOUT INCIDENT. NR 2 WATER BOILER CHANGED IAW MM 25-30 & CHECKED SERVICEABLE. NO FURTHER INCIDENTApr 9, 2001 · Airbus A310304 · Buffet/GalleysSDR CA010320021Line · loose(CAN) PILOT OBSERVED GREEN SYSTEM HYDRAULICS WAS LOOSING FLUID. AIRCRAFT DIVERTED TO YYT. HYDRAULIC LINE IN NR 1 ENGINE PYLONFOUND LOOSE. LINE TIGHTENED AND LEAK CHECK CARRIED OUT SERVICEABLE.Feb 14, 2001 · Airbus A310304 · Hydraulic System, MainSDR CA010301027Bushing · rotated(CAN) AIRCRAFT RETURNED TO YTR AS GEAR WOULD NOT RETRACT. AIRCRAFT PUT ON JACKS AND FOUND THAT LT BOGIE WOULD NOT TILT. IT WAS DETERMINED THAT ONE BUSHING ON THE SHOCK ABSORBER HAD ROTATED CAUSING THE HINGE PIN TO SEIZE, THEREFORE BOGIE WOULD NOT TILT AND GEARFeb 11, 2001 · Airbus A310304 · Main Landing Gear Strut/Axle/TruckSDR CA010226013Duct · damaged(CAN) DURING CLIMB, NR 2 ENGINE FIRE INDICATION OBSERVED. ENGINE RETARDED TO IDLE. FIRE WARNING DISAPPEARED. AIRCRAFT LANDED WITHOUT INCIDENT. 14TH STAGE DUCT FOUND DAMAGED. REPLACED I.A.W. MM 36-00-00. SUSPECT CLAMP CAUSED PROBLEM. RELATED PARTS REPLACED INCLJan 27, 2001 · Airbus A310304 · Engine Bleed Air SystemSDR CA010105009Probe · reads high(CAN) ON CLIMB, AIRCRAFT BEGAN TO GIVE ERRONEOUS COMMANDS TO PILOTS FLIGHT DIRECTOR, FLIGHT DIRECTOR THEN FAILED, AUTO THROTTLE MOVED TO IDLE WITHOUT COMMAND. AIRCRAFT RETURNED TO BASE. ON LANDING ALL INDICATIONS RETURNED TO NORMAL. FAULT CODE INDICATED NR 1 FJan 5, 2001 · Airbus A310304 · Autopilot System
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