# Service difficulty reports: Airbus A310-300

A list on [Airbus A310-300](https://openairdocs.org/model/airbus-a310-300.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 89 reports

- [SDR FDEA202410231576](https://openairdocs.org/sdr/FDEA202410231576.md): Switch · failed · Oct 23, 2024 · N733FD · Airbus A310300 · Door Warning System
  > PDIS 733 52-70 8386 23OCT24 05:16 MEM OPEN PASSING FL230, RECEIVED A FLASHING RED LIGHT AND ALARM FOR THE R ENTRY DOOR. ALARM AND LIGHT STOPPED BELOW FL190 ON DESCENT. NO ECAM INDICATION OR PRESSURIZATION ISSUES NOTED. FACT 31OCT24 20:47 ME
- [SDR FDEA202409191329](https://openairdocs.org/sdr/FDEA202409191329.md): Fitting · corroded · Sep 19, 2024 · N680FE · Airbus A310300 · Wing Main, Frame Structure
  > CORROSION FOUND BETWEEN BUSHES 'D" AND "E" DURING RH RIB 5 INSPECTION COMPLIED WITH FED EX EA 6-571-T0316490 PT2 AND R57240425. MAJOR REPAIR. EA 6-5710- T0316490 WINGS - BASIC WING STRUCTURE - CORROSION REPAIR OF RIB 5 FWD LUG RH. MPN A57240810214.
- [SDR FDEA202409121332](https://openairdocs.org/sdr/FDEA202409121332.md): Seat Track · corroded · Sep 12, 2024 · N655FE · Airbus A310300 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN DECK SEAT TRACK A POINT GOT CORROSION AT FR15B Y953 REPLACED THE SEAT TRACK WITH NEW PART. I.A.W A300-600F SRM 51-72-10-001, P2. THIS REPAIR CLASSIFIED AS MINOR, PER GMM 06-2-100. AT FR15A~19, Y953 NOTE: 5.(C), P/N TYPE ERROR, CREATED A NEW SDR NO:24-
- [SDR FDEA202408111331](https://openairdocs.org/sdr/FDEA202408111331.md): Shear Tie · damaged · Aug 11, 2024 · N730FD · Airbus A310300 · Fuselage Internal Mounting Structure
  > COMPLY WITH EO 6-5310-E0330747 D P12 REPAIRED THE FRAME FOOT CRACK AT FR45 RH SIDE AREA 2 COMPLIED WITH EO 6-5310-E0330747 D P12 REPAIRED THE FRAME FOOT CRACK AT FR45 RH SIDE AREA 2, TITLE: FUSELAGE - MAINFRAME - INSPECTION OF LOWER FRAME BASE FITTING BET
- [SDR CA190327021](https://openairdocs.org/sdr/CA190327021.md): Switch · faulted · Mar 26, 2019 · Airbus A310300 · Elevator Control System
  > (CAN) EN ROUTE ECAM YELLOW SERVO JAM. ECAM ACTIONS HAD ALREADY BEEN PERFORMED. YELLOW SERVO CTL SWITCHED OFF. SUSPECT AN INDICATION PROBLEM. CREW IS CHECKING THEIR ETOPS AND FUEL REQUIREMENTS. DUE TO FAULT AND RELATED INOP HYD SYSTEM FLIGHT UNABLE TO CONTINUE
- [SDR CA160223002](https://openairdocs.org/sdr/CA160223002.md): Strut · faulty · Feb 22, 2016 · Airbus A310300 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) ESTABLISHED ON FINAL FOR LANDING THE CREW SELECTED GEAR DOWN, THEY DID NOT GET A GREEN LIGHT FOR THE NOSE GEAR FROM EITHER SYS, RED LIGHTS ONLY FOR THE NOSE GEAR INDICATING AN UNSAFE GEAR SITUATION. THE CREW COMPLETED THEIR CHECKS IAW THE QRH. AN EMERG
- [SDR CA160108004](https://openairdocs.org/sdr/CA160108004.md): Wire · damaged · Jan 6, 2016 · Airbus A310300 · Electrical Power System Wiring
  > (CAN) WIRES LOCATED IN THE WHEEL WELL NEAR A CANISTER. THE WIRE ROUTING WAS TOO SLACK AND WITH TIME THE LOOSE PROTECTED WIRES GOT WORN OUT.
- [SDR CA151223004](https://openairdocs.org/sdr/CA151223004.md): Water Heater · sparks · Dec 22, 2015 · Airbus A310300 · Wash Water System
  > (CAN) WATER HEATER WAS PRODUCING SPARKS WHEN F/A DID RESET THE UNIT IN FLIGHT.
- [SDR CA151203006](https://openairdocs.org/sdr/CA151203006.md): Valve · failed · Nov 20, 2015 · Airbus A310300 · Landing Gear Brake System
  > (CAN) ECAM YELLOW SYS LOW PRESSURE IN FLIGHT. 10 SECONDS AFTER, LOSS OF MOST OF THE YELLOW SYSTEM HYDRAULIC FLUID AND ASSOCIATED PITCH FEEL, SPOILER, YAW DAMPER 2 AFS.
- [SDR CA150930003](https://openairdocs.org/sdr/CA150930003.md): Cdu · cracked · Sep 25, 2015 · Airbus A310300 · Engine Thrust Reverser
  > (CAN) CDU HOUSING CRACKED DURING TESTING OF THRUST REVERSER. OPERATED OK FOR 1 CYCLE AND THEN CRACKED AND SEPARATED ON CYCLE 2.
- [SDR CA150520002](https://openairdocs.org/sdr/CA150520002.md): Duct · ruptured · May 19, 2015 · Airbus A310300 · Engine Bleed Air System
  > (CAN) DURING WALK AROUND, MAINTENANCE HEARD AN UNUSUAL NOISE COMING FROM NR NR 1 ENGINE. SOUND OF BLEED LEAK, RUSHING AIR. AFTER OPENING THE THRUST REVERSER COWLS, THE TECH FOUND A RUPTURED DUCT ON THE THRUST REVERSER PRESSURE REGULATING AND SHUTOFF VALVE, P
- [SDR CA150426001](https://openairdocs.org/sdr/CA150426001.md): Indicator · overheated · Apr 25, 2015 · Airbus A310300 · Independent Instruments
  > (CAN) APPROXIMATELY 5 MINUTES AFTER FULL ACFT ELECTRICAL POWER WAS APPLIED, THE RUDDER TRIM INDICATOR BEGAN EMMITING SMOKE AND PRODUCED A HEAVY ELECTRICAL BURNING ODOR.
- [SDR CA150318005](https://openairdocs.org/sdr/CA150318005.md): Wire Harness · burned · Mar 18, 2015 · Airbus A310300 · Electrical Power System Wiring
  > (CAN) DURING POWER ON OF ACFT, MULTIPLE WIRES BURN ON THE LT FWD AREA OF PANEL 800VU. PRELIMINARY OBSERVATION OF ROOT CAUSE IS WIRE CHAFING ON SHARP EDGE OF PANEL 800VU LH HINGE. IT IS OF INTEREST TO NOTE THAT THESE WIRES ARE STANDARD WIRES FOUND IN THE ESPM,
- [SDR CA140812009](https://openairdocs.org/sdr/CA140812009.md): Bolt · missing · Aug 10, 2014 · Airbus A310300 · Landing Gear Door Retract Section
  > (CAN) A/C HAD INFLIGHT TURNBACK LT MLG DOOR NOT CLOSING. MAINTENANCE FOUND LH MLG UPLOCK (FIN 321212) ROD ASSY (REF A310 IPC 32-36-44-02 ITEM 100) ADRIFT FROM RETAINER BRACKET (REF A310 IPC 32-16-16-05 ITEM 100). THE RETAINER BOLT WAS MISSING. INSPECTION SHOW
- [SDR CA140124007](https://openairdocs.org/sdr/CA140124007.md): Fairing · ruptured · Jan 23, 2014 · Airbus A310300 · Aerodynamic Fairings
  > (CAN) DURING WALK AROUND INSPECTION, IT WAS FOUND THAT THE RT VERTICAL STABILIZER TO FUSELAGE FAIRING WAS DAMAGED, REFER IPC 53-19-69, ITEM 250. AFTER INSPECTION IT WAS NOTED THAT THE DAMAGE WAS DUE TO DELAMINATION OF THE PANEL. PANEL REPLACED AND INFORMED.
- [SDR CA140124006](https://openairdocs.org/sdr/CA140124006.md): Wire · shorted · Jan 22, 2014 · Airbus A310300 · Hydraulic Power System Wiring
  > (CAN) DURING FLIGHT LT INNER FUEL PUMP FAULT MESSAGE TRIGGERED. TROUBLESHOOTONG CARRIED OUT AND THE FOLLOWING FINDING WERE OBSERVED, GREEN HYD PUMP NR 2 WIRING AT SPECIFIED RAMP SUPPORT SHORTED TO GROUND, RESULTING IN 2 OF THE 3 PHASES TO SEVERE AND CAUSING O
- [SDR CA131219016](https://openairdocs.org/sdr/CA131219016.md): Pin · cracked · Dec 14, 2013 · Airbus A310300 · Main Landing Gear Attach Section
  > (CAN) PIN IS CRACKED. REPORTED TO MFG AND WAITING FOR MFG INSTRUCTIONS.
- [SDR CA131213008](https://openairdocs.org/sdr/CA131213008.md): Hinge Pin · cracked · Dec 12, 2013 · Airbus A310300 · Main Landing Gear Strut/Axle/Truck
  > (CAN) DURING THE A-CHECK, WHILE PERFORMING LUBRICATION OF THE LT MLG, THE FWD ATTACHMENT PIN WAS FOUND WITH CRACKS AND A PORTION BROKEN OFF. THIS PIN IS PART OF THE GEAR AND IS REPLACED WITH THE GEAR ON OVERHAUL. THE GEAR WAS OVERHAULED IN OCT 2007 AND HAS A
- [SDR CA130826003](https://openairdocs.org/sdr/CA130826003.md): Line · cracked · Aug 24, 2013 · Airbus A310300 · Hydraulic System, Main
  > (CAN) DURING FLIGHT THE GREEN HYDRAULIC FLUID NOTICED TO BE DECREASING, FOLLOWED BY ECAM LOW LEVEL WARNING. LANDING MANUALLY EXTENDED FOR LANDING. ACFT HAD TO BE TOWED OFF RUNWAY DUE TO LOSS OF STEERING FROM GREEN HYDRAULIC SYSTEM FLUID LOSS. FOUND NR 2 ENGI
- [SDR CA130822012](https://openairdocs.org/sdr/CA130822012.md): Manifold · leaking · Aug 22, 2013 · Airbus A310300 · Hydraulic System, Main
  > (CAN) O-RING FAILURE BETWEEN MANIFOLD ASSY FIN 291112, PN A2901150800000 AND BOSS FITTING MS21902-10. CAUSING ACFT TURN BACK DUE HYDRAULIC LOSS. IPC REF 24-24-03-04 050, O-RING REPLACED ON MANIFOLD ASSY FIN 291112. DEFECT ITEM NR 1100188.
- [SDR CA130610006](https://openairdocs.org/sdr/CA130610006.md): Eec · malfunctioned · Jun 4, 2013 · Airbus A310300 · Fuel Controlling System
  > (CAN) AT THE TOP OF DESCENT, UPON THRUST REDUCTION TO FLIGHT IDLE, BOTH THRUST LEVERS WENT TO IDLE BUT THE NR 2 ENGINE N1 STAYED AT 70 PERCENT N1. STARTING AROUND 12,000 FT, TAT ABOVE FREEZING, THE N1 STARTED REDUCING TOWARDS IDLE. IT REACHED IDLE AT AROUND 8,
- [SDR CA130417001](https://openairdocs.org/sdr/CA130417001.md): Cdu · damaged · Apr 12, 2013 · Airbus A310300 · Engine Controls
  > (CAN) NR 1 ENGINE THRUST REVERSER FAULT ON LANDING. FOUND OTBD REVERSER SLEEVE NOT FULLY STOWED. THRUST REVERSER WAS DEACTIVATED IAW MEL. ON DEPARTURE, THE NR 1 POWER LEVER WOULD NOT MOVE OUT OF IDLE POSITION. CENTER DRIVE UNIT (CDU) FEEDBACK MECHANISM FOUN
- [SDR CA130318014](https://openairdocs.org/sdr/CA130318014.md): Bearing · corroded · Mar 11, 2013 · Airbus A310300 · Emergency Exits
  > (CAN) DURING INSPECTION UNABLE TO OPEN RT OVERWING EMERGENCY EXIT DOOR, FROM THE INSIDE NOR FROM THE OUTSIDE. DOOR HAD TO BE PRYED UP IN ORDER TO OPEN. FOUND SLIDING BEARING/BUSHING CORRODED ON LIFTING MECHANISM SHAFT, ITEM 220 OF IPC 52-23-11, FIG 14.
- [SDR CA130318011](https://openairdocs.org/sdr/CA130318011.md): Skin · cracked · Mar 11, 2013 · Airbus A310300 · Cargo/Baggage Doors
  > (CAN) DURING VISUAL INSPECTION, FOUND AFT CARGO DOOR ACTUATOR FITTING AT FRAME 61A AND INNER SKIN CRACKED BETWEEN LONGERON 1 AND 1A.
- [SDR CA130204003](https://openairdocs.org/sdr/CA130204003.md): Actuator · failed · Feb 2, 2013 · Airbus A310300 · Landing Gear Door Actuator
  > (CAN) ON APPROACH THE CREW OBSERVED AN UNSAFE INDICATION OF THE NOSE GEAR UPON SELECTING GEAR DOWN FOR LANDING. THE CREW DECLARED AN EMERGENCY AND FOLLOWED THE APPLICABLE ABNORMAL CHECKLIST AND PERFORMED A GRAVITY GEAR EXTENSION WHICH RESULTED IN A SAFE GEAR I
- [SDR CA121203005](https://openairdocs.org/sdr/CA121203005.md): Control Panel · overheated · Nov 30, 2012 · Airbus A310300 · VHF Communications System
  > (CAN) IN CRUISE AT FL 370, VHF 2 CONTROL PANEL GREEN LIGHT WAS INTERMITTENT, THEN BECAME EXTINGUISHED. CREW NOTICED AN ELECTRICAL SPARK FOLLOWED IMMEDIATELY BY A LIGHT WHITE SMOKE COMING FROM UNIT AT THE ACTIVE GREEN LIGHT. THE CREW PULLED THE ASSOCIATED CIR
- [SDR CA121127002](https://openairdocs.org/sdr/CA121127002.md): Bolt · worn · Nov 23, 2012 · Airbus A310300 · Trailing Edge Flap Control System
  > (CAN) ON APPROACH, THE SLATS EXTENDED NORMALLY BUT NO FURTHER MOVEMENT OF THE FLAP LEVER WAS POSSIBLE AFTERWARDS. THE SLAT/FLAP LEVER WAS STUCK IN THE UP POSITION PREVENTING THE MOVEMENT THROUGH THE POSITION DETENTS. THE CREW ADVISED ATC THAT A HIGHER APPROA
- [SDR CA120914010](https://openairdocs.org/sdr/CA120914010.md): Duct · fractured · Sep 10, 2012 · Airbus A310300 · Air Distribution System
  > (CAN) ACFT ARRIVED WITH 2 SNAGS RELATED TO AIR CONDITIONNING. CABIN TEMP HARD TO COOL DOWN AND LOW FLOW PLUS BOTH PACKS SURGING ON THE GROUND. REF W/O 1089584. DURING TROUBLESHOOTING, FOUND NR 1 PACK OUTLET DUCT RUPTURED. MISSING AREA APPROX 6" X 3". DUCT W
- [SDR CA120224005](https://openairdocs.org/sdr/CA120224005.md): Control Panel · smoke · Feb 7, 2012 · Airbus A310300 · Rudder Tab Control System
  > (CAN) FOUND SMOKE EMANATING FROM RUDDER AND AILERON TRIM CONTROL PANEL DURING COCKPIT PRE-DISPATCH CHECK. PART WAS REPLACED.
- [SDR CA111026013](https://openairdocs.org/sdr/CA111026013.md): Oven · burned · Oct 25, 2011 · Airbus A310300 · Buffet/Galleys
  > (CAN) FWD GALLEY NR 2 OVEN BURNING ODOR. MEL 25-20, CAT D RAISED BY KLM IN AMS. UPON INVESTIGATION, FOUND FAN SEIZED. REPLACED OVEN IAW AMM 25-34-00. OPS CHECKED SERVICEABLE.
- [SDR 2011F00121](https://openairdocs.org/sdr/2011F00121.md): Blade · broken · Mar 6, 2010 · Airbus A310300 · Turbine Section
  > HPT STAGE 1 BLADE FOUND BROKEN AND MISSING DURING ROUTINE BSI, ON FOLLOWING CF6-80C2A8 ENGINES SN 659611, 659399, 659526, 659392, 659408, 659612, 659414. SECONDARY DAMAGE WAS ALSO OBSERVED ON NUMBER OF BLADES. ALL THE BLADES WAS NEW WHEN INSTALLED.
- [SDR CA091203003](https://openairdocs.org/sdr/CA091203003.md): Duct · cracked · Dec 2, 2009 · Airbus A310300 · APU Engine Fuel and Control
  > (CAN) PIREP DEFECT 1037394 - FUEL MIGRATING FROM LT INNER TANK TO CTR TANK. MX FOUND THE APU BOOST PUMP CANNISTER DELIVERY DUCT CRACKED. REPLACED PER MM 49-32-14 AND SERVICEABLE. (TC NR 20091203003)
- [SDR CA090522001](https://openairdocs.org/sdr/CA090522001.md): Hose · leaking · May 16, 2009 · Airbus A310300 · Hydraulic System, Main
  > (CAN) AFTER LANDING, DURING TAXI, THE GREEN HYD FLUID HAS BEEN LOST. THE ACFT HAS BEEN TOWED TO THE GATE. HOSE HAS BEEN REPLACED ON LT MLG DRAG BRACE. HYD SYS HAS BEEN BLED AND ACFT RETURNED TO SERVICE.
- [SDR CA090514004](https://openairdocs.org/sdr/CA090514004.md): Display · smoke · May 7, 2009 · Airbus A310300 · Central Warning
  > (CAN) CREW DETECTED SMOKE IN FLIGHT DECK. DETERMINED IT WAS COMING FROM THE TCAS DISPLAY UNIT. ODOR DISSIPATED WHEN THE CIRCUIT BREAKER FOR TCAS MONITOR WAS PULLED. MONITOR LEFT DE-ACTIVATED UNDER MEL 34-35 WHILE PART ON ORDER.
- [SDR CA080801004](https://openairdocs.org/sdr/CA080801004.md): Access Panel · missing · Jul 23, 2008 · Airbus A310300 · Leading Edge Devices
  > (CAN) ON ARRIVAL, LEADING EDGE SLAT TRACK ACCESS PANEL 512HB FOUND MISSING. ADJACENT PANEL 512JB ALSO FOUND DAMAGED. LOST IN FLIGHT. PANEL 512HB REPLACED AND PANEL 512JB REPAIRED IAW SRM.
- [SDR CA080728005](https://openairdocs.org/sdr/CA080728005.md): Circuit Breaker · burned · Jul 21, 2008 · Airbus A310300 · Fuel System Wiring
  > (CAN) DURING TROUBLESHOOTING OF THE INOPERATIVE LT OUTER TANK FUEL PUMP (DEACTIVATED IAW MEL) THE CIRCUIT BREAKER 3QA WAS FOUND BURNED, BODY CRACKED AND ONE LEG MISSING. CIRCUIT BREAKER WAS REPLACED AND SYS TESTED SERVICEABLE. A DETAILED VISUAL INSPECTION CAMP
- [SDR CA080617004](https://openairdocs.org/sdr/CA080617004.md): Shaft · sheared · Jun 16, 2008 · Airbus A310300 · Windshield/Door Rain/Ice Removal
  > (CAN) ACFT ARRIVED AT GATE WITH CAPTAINS’ WINDSHIELD WIPER ASSEMBLY MISSING. FURTHER INVESTIGATION FOUND THAT CONVERTER SPLINED SHAFT HAD SHEARED OFF CAUSING THE WIPER ASSY TO DEPART ACFT WHILE TAXIING IN FROM LANDING TO APRON. WIPER ASSY WAS FOUND IN TAXIWAY.
- [SDR CA080409003](https://openairdocs.org/sdr/CA080409003.md): Outflow Valve · malfunctioned · Apr 7, 2008 · Airbus A310300 · Pressure Regulator/Outflow Valve
  > AFTER 30 MIN IN CRUISE, CAB PRESSURE REG NR 2 FAULT, FOLLOWED BY CAB PRESSURE REG NR 1 FAULT. UNABLE TO CONTROL IN MANUAL. EMERGENCY DESCENT AND QAR PROCEDURES FOLLOWED. PAX MASK SYSTEM ACTIVATED IN AUTO. FLIGHT RETURNED TO STATION AT FL 10,000 FT. ACFT W
- [SDR CA080314016](https://openairdocs.org/sdr/CA080314016.md): Switch · contaminated · Mar 9, 2008 · Airbus A310300 · Trailing Flap Position Indicating System
  > (CAN) DURING CLIMB, ECAM WARNING "FLAP KRUEGER NOT RETRACTED LIGHT" CAME ON. FLIGHT RETURNED TO THE STATION. SFCC INDICATED FAULT COMING FROM THE LT KRUEGER RETRACT SWITCH. MAINT FOUND THE SWITCH BACK SHELL CONTAMINATED WITH WATER. CONNECTOR AND SWITCH CLEANE
- [SDR CA071127002](https://openairdocs.org/sdr/CA071127002.md): Coffeemaker · sparks · Nov 21, 2007 · Airbus A310300 · Buffet/Galleys
  > (CAN) DURING FLIGHT, THE F/A REPORTED THE FWD COFFEE MAKER/WATER BOILER OVERHEATING AND NOTICED SOME SPARK COMING FROM THE UNIT. THE UNIT WAS DEACTIVATED. THE UNIT WAS REPLACED BY MAINTENANCE AND ROUTED TO THE REPAIR SHOP FOR INVESTIGATION. (TC NR 20071127002)
- [SDR CA070731001](https://openairdocs.org/sdr/CA070731001.md): Seal · leaking · Jul 27, 2007 · Airbus A310300 · Fuel Controlling System
  > (CAN) DURING TAXI-IN AT THE GATE, A LARGE FUEL LEAKAGE WAS OBSERVED COMING FROM THE HMU FUEL DRAIN BELOW NR 2 ENGINE. ENGINE WAS SHUTDOWN, BUT LEAKAGE CONTINUED. NR 2 ENGINE FIRE HANDLE WAS PULLED AND LEAKAGE STOPPED. FOUND LEAKAGE WAS FOM THE MEC SHAFT SEA
- [SDR CA070313003](https://openairdocs.org/sdr/CA070313003.md): Power Supply · overheated · Mar 12, 2007 · Airbus A310300 · Passenger Compartment Lighting
  > (CAN) DURING CRUISE, FLIGHT CREW OBSERVED WHAT APPEARED TO BE WHITE SMOKE EMANATING FROM READING LIGHT (PSU) PANEL ASSEMBLY ABOVE SEAT 30 AB. CREW SWITCHED OFF READING LIGHTS AND SMOKE STOPPED. ON ARRIVAL TO THE STATION, MAINTENANCE FOUND ONE TRANSFORMER PRINT
- [SDR CA061227001](https://openairdocs.org/sdr/CA061227001.md): Wire · burned · Dec 19, 2006 · Airbus A310300 · Navigation System Wiring
  > (CAN) ON ARRIVAL, FLIGHT CREW REPORTED TCAS AND RA FAILURE FLAGS ON BOTH IVSI’S DURING FLIGHT. WHILE TROUBLESHOOTING TCAS FAILURE, SEVERAL BURNED WIRES WERE DISCOVERED IN A BUNDLE LOCATED BEHIND THE ATC1 AND TCA RACK (500VU). THE WIRE SUSPECTED OF CAUSING THE
- [SDR CA061011005](https://openairdocs.org/sdr/CA061011005.md): Access Panel · missing · Sep 29, 2006 · Airbus A310300 · Fuselage Structure (General)
  > (CAN) UPON AIRCRAFT ARRIVAL, DURING WALK AROUND INSPECTION, FOUND THE FWD CARGO DOOR LOWER FWD ACCESS PANEL, FIN811AR, MISSING. MOUNTING HARDWARE, FASTENERS AND LANYARDS WERE STILL ATTACHED TO THE CARGO DOOR. DOOR WAS INSPECTED AND NO FURTHER DAMAGE WAS NOTICE
- [SDR CA060728005](https://openairdocs.org/sdr/CA060728005.md): Control Panel · smoke · Jul 21, 2006 · Airbus A310300 · VHF Communications System
  > (CAN) DURING FLIGHT, LIGHT SMOKE CAME FROM THE NR 1 VHF CONTROL PANEL. THE CIRCUIT BREAKER WAS PULLED AND THE FLIGHT PROCEEDED WITHOUT ANY FURTHER PROBLEM. THE PANEL WAS REPLACED AT THE ARRIVAL STATION AND WAS SYSTEM CHECKED SERVICEABLE. PANEL WAS ROUTED TO TH
- [SDR CA060314001](https://openairdocs.org/sdr/CA060314001.md): Cover · missing · Mar 9, 2006 · Airbus A310300 · Cargo/Baggage Doors
  > THE AIRCRAFT ARRIVED FROM FLIGHT WITH ONE OF THE FORWARD CARGO DOOR ACCESS PANEL LATCH COVER MISSING. DURING INVESTIGATION FOUND THE PANEL ATTACHMENT AREAS HAD ELONGATED, WHICH ALLOWED THE ATTACHMENT SCREWS TO PASS THROUGH THE ACCESS PANEL. NEW PANEL ASSY WA
- [SDR CA060228003](https://openairdocs.org/sdr/CA060228003.md): Pickup · contaminated · Feb 26, 2006 · Airbus A310300 · Trailing Edge Flap Control System
  > AIRCRAFT LANDED WITH FULL SLATS AND NO FLAPS. UNABLE TO EXTEND FLAPS ON LANDING. SYSTEM TORQUE LIMITERS AND SCREW JACKS LIMITER INSPECTED AND NO FAULT FOUND. DURING TROUBLESHOOTING, THE LT AND RT POWER PICK UP UNITS WERE FOUND CONTAMINATED WITH SKYDROL AND
- [SDR CA050809001](https://openairdocs.org/sdr/CA050809001.md): Switch · shorted · Aug 4, 2005 · Airbus A310300 · Exterior Lighting
  > (CAN) DURING STATION TURN AROUND, MAINTENANCE NOTICED SMALL SPARK COMING OUT OF THE ANTI-COLLISION CONTROL SWITCH (2LV). CIRCUIT BREAKER (5LV) OF THE LOWER BEACON WAS POPPED. FOUND THE ANTI-COLLISION SWITCH CONTACTS 1B AND 2B SHORTED TOGETHER, REGARDLESS OF
- [SDR CA050722003](https://openairdocs.org/sdr/CA050722003.md): Circuit Breaker · burned · Jul 16, 2005 · Airbus A310300 · Engine Fuel System Wiring
  > FLIGHT CREW REPORTED, RT OUTER TANK FUEL PUMP NR 1, LOW PRESSURE FAULT. DURING TROUBLESHOOTING, FOUND CIRCUIT BREAKER FIN 4QA TRIPPED AND EMITTING BURNT SMELL. CIRCUIT BREAKER WAS REPLACED AND SYSTEM OPS CHECKED SERVICEABLE.
- [SDR CA050707001](https://openairdocs.org/sdr/CA050707001.md): Wheel · cracked · Jun 8, 2005 · Airbus A310300 · Wheel/Ski/Float
  > DURING TRANSIT CHECK ONE OF THE MAIN WHEEL TIRE WAS FOUND WITH LOW PRESSURE. MAIN WHEEL ASSEMBLY WAS REMOVED AND SENT TO THE REPAIR SHOP FOR INVESTIGATION. DURING INSPECTION, THE OUTBOARD WHEEL HALVE WAS FOUND CRACKED APPROX ONE INCH LONG ON LOWER WHEEL WEB

Next page: https://openairdocs.org/model/airbus-a310-300/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 aircraft_model_key = 'A310300'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a310-300/reports

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