# Airbus A310-300 - Type: Aircraft model (FAA registry) - Registry code: 3940007 - Manufacturer (registry): AIRBUS - Model: A310-300 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 284 - Weight class: 20,000 lb and over - Certification: Type certificated - Data sheet: [TCDS A35EU](https://openairdocs.org/tcds/A35EU) (OpenAirDocs) - Holder: Airbus SAS - Registered aircraft: 0 - Page: https://openairdocs.org/model/airbus-a310-300 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (89, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR FDEA202410231576](https://openairdocs.org/sdr/FDEA202410231576), Oct 23, 2024: SWITCH. FAILED. 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 D - [SDR FDEA202409191329](https://openairdocs.org/sdr/FDEA202409191329), Sep 19, 2024: FITTING. CORRODED. 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- T031649 - [SDR FDEA202409121332](https://openairdocs.org/sdr/FDEA202409121332), Sep 12, 2024: SEAT TRACK. CORRODED. 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 - [SDR FDEA202408111331](https://openairdocs.org/sdr/FDEA202408111331), Aug 11, 2024: SHEAR TIE. DAMAGED. 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 A - [SDR CA190327021](https://openairdocs.org/sdr/CA190327021), Mar 26, 2019: SWITCH. FAULTED. (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 TH - [SDR CA160223002](https://openairdocs.org/sdr/CA160223002), Feb 22, 2016: STRUT. FAULTY. (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 NO - [SDR CA160108004](https://openairdocs.org/sdr/CA160108004), Jan 6, 2016: WIRE. DAMAGED. (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), Dec 22, 2015: WATER HEATER. SPARKS. (CAN) WATER HEATER WAS PRODUCING SPARKS WHEN F/A DID RESET THE UNIT IN FLIGHT. - [SDR CA151203006](https://openairdocs.org/sdr/CA151203006), Nov 20, 2015: VALVE. FAILED. (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 - [SDR CA150930003](https://openairdocs.org/sdr/CA150930003), Sep 25, 2015: CDU. CRACKED. (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), May 19, 2015: DUCT. RUPTURED. (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 COW - [SDR CA150426001](https://openairdocs.org/sdr/CA150426001), Apr 25, 2015: INDICATOR. OVERHEATED. (CAN) APPROXIMATELY 5 MINUTES AFTER FULL ACFT ELECTRICAL POWER WAS APPLIED, THE RUDDER TRIM INDICATOR BEGAN EMMITING SMOKE AND PRODUCED A HEAVY ELECTRICAL BURNI - [SDR CA150318005](https://openairdocs.org/sdr/CA150318005), Mar 18, 2015: WIRE HARNESS. BURNED. (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 PAN - [SDR CA140812009](https://openairdocs.org/sdr/CA140812009), Aug 10, 2014: BOLT. MISSING. (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 R - [SDR CA140124007](https://openairdocs.org/sdr/CA140124007), Jan 23, 2014: FAIRING. RUPTURED. (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 INSPECTIO - [SDR CA140124006](https://openairdocs.org/sdr/CA140124006), Jan 22, 2014: WIRE. SHORTED. (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 - [SDR CA131219016](https://openairdocs.org/sdr/CA131219016), Dec 14, 2013: PIN. CRACKED. (CAN) PIN IS CRACKED. REPORTED TO MFG AND WAITING FOR MFG INSTRUCTIONS. - [SDR CA131213008](https://openairdocs.org/sdr/CA131213008), Dec 12, 2013: HINGE PIN. CRACKED. (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 - [SDR CA130826003](https://openairdocs.org/sdr/CA130826003), Aug 24, 2013: LINE. CRACKED. (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 B - [SDR CA130822012](https://openairdocs.org/sdr/CA130822012), Aug 22, 2013: MANIFOLD. LEAKING. (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 24-24-0 - [SDR CA130610006](https://openairdocs.org/sdr/CA130610006), Jun 4, 2013: EEC. MALFUNCTIONED. (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 AROU - [SDR CA130417001](https://openairdocs.org/sdr/CA130417001), Apr 12, 2013: CDU. DAMAGED. (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 - [SDR CA130318014](https://openairdocs.org/sdr/CA130318014), Mar 11, 2013: BEARING. CORRODED. (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 SL - [SDR CA130318011](https://openairdocs.org/sdr/CA130318011), Mar 11, 2013: SKIN. CRACKED. (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), Feb 2, 2013: ACTUATOR. FAILED. (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 - [SDR CA121203005](https://openairdocs.org/sdr/CA121203005), Nov 30, 2012: CONTROL PANEL. OVERHEATED. (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 - [SDR CA121127002](https://openairdocs.org/sdr/CA121127002), Nov 23, 2012: BOLT. WORN. (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 POSITI - [SDR CA120914010](https://openairdocs.org/sdr/CA120914010), Sep 10, 2012: DUCT. FRACTURED. (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. - [SDR CA120224005](https://openairdocs.org/sdr/CA120224005), Feb 7, 2012: CONTROL PANEL. SMOKE. (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), Oct 25, 2011: OVEN. BURNED. (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 CHECKE - [SDR 2011F00121](https://openairdocs.org/sdr/2011F00121), Mar 6, 2010: BLADE. BROKEN. HPT STAGE 1 BLADE FOUND BROKEN AND MISSING DURING ROUTINE BSI, ON FOLLOWING CF6-80C2A8 ENGINES SN 659611, 659399, 659526, 659392, 659408, 659612, 659414. SECOND - [SDR CA091203003](https://openairdocs.org/sdr/CA091203003), Dec 2, 2009: DUCT. CRACKED. (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 49-32-1 - [SDR CA090522001](https://openairdocs.org/sdr/CA090522001), May 16, 2009: HOSE. LEAKING. (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 H - [SDR CA090514004](https://openairdocs.org/sdr/CA090514004), May 7, 2009: DISPLAY. SMOKE. (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 PUL - [SDR CA080801004](https://openairdocs.org/sdr/CA080801004), Jul 23, 2008: ACCESS PANEL. MISSING. (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 PA - [SDR CA080728005](https://openairdocs.org/sdr/CA080728005), Jul 21, 2008: CIRCUIT BREAKER. BURNED. (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 - [SDR CA080617004](https://openairdocs.org/sdr/CA080617004), Jun 16, 2008: SHAFT. SHEARED. (CAN) ACFT ARRIVED AT GATE WITH CAPTAINS’ WINDSHIELD WIPER ASSEMBLY MISSING. FURTHER INVESTIGATION FOUND THAT CONVERTER SPLINED SHAFT HAD SHEARED OFF CAUSING TH - [SDR CA080409003](https://openairdocs.org/sdr/CA080409003), Apr 7, 2008: OUTFLOW VALVE. MALFUNCTIONED. 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 - [SDR CA080314016](https://openairdocs.org/sdr/CA080314016), Mar 9, 2008: SWITCH. CONTAMINATED. (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 RET - [SDR CA071127002](https://openairdocs.org/sdr/CA071127002), Nov 21, 2007: COFFEEMAKER. SPARKS. (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 U - [SDR CA070731001](https://openairdocs.org/sdr/CA070731001), Jul 27, 2007: SEAL. LEAKING. (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 - [SDR CA070313003](https://openairdocs.org/sdr/CA070313003), Mar 12, 2007: POWER SUPPLY. OVERHEATED. (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 - [SDR CA061227001](https://openairdocs.org/sdr/CA061227001), Dec 19, 2006: WIRE. BURNED. (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 DIS - [SDR CA061011005](https://openairdocs.org/sdr/CA061011005), Sep 29, 2006: ACCESS PANEL. MISSING. (CAN) UPON AIRCRAFT ARRIVAL, DURING WALK AROUND INSPECTION, FOUND THE FWD CARGO DOOR LOWER FWD ACCESS PANEL, FIN811AR, MISSING. MOUNTING HARDWARE, FASTENERS AND - [SDR CA060728005](https://openairdocs.org/sdr/CA060728005), Jul 21, 2006: CONTROL PANEL. SMOKE. (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 - [SDR CA060314001](https://openairdocs.org/sdr/CA060314001), Mar 9, 2006: COVER. MISSING. 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 - [SDR CA060228003](https://openairdocs.org/sdr/CA060228003), Feb 26, 2006: PICKUP. CONTAMINATED. 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. DU - [SDR CA050809001](https://openairdocs.org/sdr/CA050809001), Aug 4, 2005: SWITCH. SHORTED. (CAN) DURING STATION TURN AROUND, MAINTENANCE NOTICED SMALL SPARK COMING OUT OF THE ANTI-COLLISION CONTROL SWITCH (2LV). CIRCUIT BREAKER (5LV) OF THE LOWER BEAC - [SDR CA050722003](https://openairdocs.org/sdr/CA050722003), Jul 16, 2005: CIRCUIT BREAKER. BURNED. 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. - [SDR CA050707001](https://openairdocs.org/sdr/CA050707001), Jun 8, 2005: WHEEL. CRACKED. 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. DURI All 89: https://openairdocs.org/model/airbus-a310-300/reports.md ## STCs that may be installed (OpenAirDocs) (64, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC ST00374AT](https://openairdocs.org/stc/ST00374AT): Installation of Collins SAT-906 SATCOM system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC - [STC SA3400NM](https://openairdocs.org/stc/SA3400NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc - [STC SA3168SO](https://openairdocs.org/stc/SA3168SO): Installation of dual TRA-67A Mode 'S' transponder system. Honeywell International Inc - [STC ST00140AT](https://openairdocs.org/stc/ST00140AT): Installation of a MUA-45 Data Link System. Honeywell International Inc - [STC ST00825AT](https://openairdocs.org/stc/ST00825AT): Installation of a CAS-81 TCAS II. Honeywell International Inc - [STC ST00826AT](https://openairdocs.org/stc/ST00826AT): Installation of dual TRA-67 Mode S transponders. Honeywell International Inc - [STC SA8814SW](https://openairdocs.org/stc/SA8814SW): Replace core assembly of AiResearch APU oil cooler, part number 160192-1. Honeywell International Inc - [STC SA8947SW](https://openairdocs.org/stc/SA8947SW): Replace core assembly of AiResearch Bleed Air Precooler, part number 189120-1 and -3. Honeywell International Inc - [STC ST00087LA](https://openairdocs.org/stc/ST00087LA): Installation of Sony Trans Com Video Entertainment System Part Number 985-0173-006 Revision D. Burrana Inc - [STC ST01685AT](https://openairdocs.org/stc/ST01685AT): Installation of the RTA-44D VHG Data Radio System and/or the RTA-83B VHF Communications System. Honeywell International Inc - [STC SA7060NM](https://openairdocs.org/stc/SA7060NM): Installation of Honeywell/Racal Aeronautical satellite communications system. Honeywell International Inc - [STC ST00341WI](https://openairdocs.org/stc/ST00341WI): Installation of cabin air filter assembly 21FA102. Purolator Facet, Inc - [STC ST504CH](https://openairdocs.org/stc/ST504CH): Install Main Deck Cargo Loading System. Telair US LLC - [STC SA5835NM](https://openairdocs.org/stc/SA5835NM): Installation of Teledyne Controls Digital Flight Data Acquisition Unit. Teledyne Controls - [STC ST01111AT](https://openairdocs.org/stc/ST01111AT): Manufacture and installation of A300 Lerner Service Cart. Driessen Aircraft Interior Systems USA Inc - [STC ST00100NY](https://openairdocs.org/stc/ST00100NY): Conversion of Passenger to Freighter configuration by installing a large Main Deck Cargo door, upper deck class E cargo compartment, floor reinforcement, and other associated modifications. For some models, only specific serial numbered aircraft apply. Airbus Deutschland GmbH - [STC ST02227AT](https://openairdocs.org/stc/ST02227AT): Manufacture of service carts for galley stowage. JK Aerospace Inc - [STC ST02229AT](https://openairdocs.org/stc/ST02229AT): Manufacture of service carts for galley stowage. JK Aerospace Inc - [STC ST02247AT](https://openairdocs.org/stc/ST02247AT): Manufacture of standard galley insert units. JK Aerospace Inc - [STC ST01609CH](https://openairdocs.org/stc/ST01609CH): Installation of a Smiths Industries combined voice and flight data recorder, model 3257, and optional Smiths Industries Recorder Control Unit, model 3874. Smiths Aerospace LLC - [STC SA2983SO](https://openairdocs.org/stc/SA2983SO): Installation of coffee maker/water boiler, P/N 3510-0044-(), and rail assembly, P/N 416-0201-(). B/E Aerospace Inc. Lists A310 Series - [STC ST01004NY](https://openairdocs.org/stc/ST01004NY): Installation of cargo restraint straps. Airline Container Manufacturing Co Inc. Lists A310 Series - [STC SA9039NM-D](https://openairdocs.org/stc/SA9039NM-D): Installation of vacuum flush toilets. Rogerson ATS - [STC ST02508AT](https://openairdocs.org/stc/ST02508AT): Manufacture of a service cart for galley stowage, P/N CAF014-101-( ). JK Aerospace, Inc - [STC SA5814NM](https://openairdocs.org/stc/SA5814NM): Installation of Honeywell traffic alert and collision avoidance system. ACSS (Aviation Communication and Surveillance Syst - [STC ST00142LA](https://openairdocs.org/stc/ST00142LA): Installation of Honeywell Mode S transponder. ACSS (Aviation Communication and Surveillance Syst - [STC SA5817NM](https://openairdocs.org/stc/SA5817NM): Installation of vacuum toilet retrofit kit P/N 5718. Monogram Sanitation. Lists A310 Series - [STC ST02224AT](https://openairdocs.org/stc/ST02224AT): Manufacture of a Sterling Beverage System (SBS) portable beverage dispensing system, P/N 12-0001, in accordancd with SBS, Inc., Master Drawing List Report No. 20001, dtd 6/30/00, or later FAA approved revision. Aircraft installation in accordance with SBS Drawing No. 12012, "Galley Interface Criteria," dtd 11/14/00, or later FAA approved revision. Model applicability listed on AML No. ST02224AT is a required part of this STC. Sterling Beverage Systems, Inc. Lists A310 Series - [STC ST01874AT](https://openairdocs.org/stc/ST01874AT): Installation of beverage cart with portable beverage system. Sterling Beverage Systems, Inc - [STC ST02130AT](https://openairdocs.org/stc/ST02130AT): Manufacture of Beverage Carrier, P/N 1608-502. BFE Services. Lists A310 Series - [STC SA02100AT](https://openairdocs.org/stc/SA02100AT): Manufacture of a three tier folding cart BFE P/N 2934. BFE Services. Lists A310 Series - [STC ST148CH](https://openairdocs.org/stc/ST148CH): Installation of Radome. Norton Company - [STC SA3167SO](https://openairdocs.org/stc/SA3167SO): Installation of dual CAS-81A TCAS II system. Honeywell International Inc - [STC ST02078AT](https://openairdocs.org/stc/ST02078AT): Installation of a Triple rockwell Collins VHF 900B Transceiver and the replacement of control heads with Gables G7400-13 and G7400-16 to meet the 8.33 KHz channel space frequencies. Federal Express Corp. Lists A310 Series - [STC ST01099NY](https://openairdocs.org/stc/ST01099NY): Installation of Scott Aviation chemical oxygen generators P/N's S11701902 (two person) and S11701903 (three person). Scott Aviation - [STC SA7611SW](https://openairdocs.org/stc/SA7611SW): Recore of APU oil cooler P/N 160186 or 160192. Limco-Airepair, Inc. Lists A310 Series - [STC SA7883SW](https://openairdocs.org/stc/SA7883SW): Recore of Englehard PN D19772 ozone converters. Limco-Airepair, Inc. Lists A310 Series - [STC ST01391AT](https://openairdocs.org/stc/ST01391AT): Installation of Three Tier Folding Cart. BFE Services. Lists A310 Series - [STC ST00890AT](https://openairdocs.org/stc/ST00890AT): Installation of 218-passenger interior configuration. Delta Airlines Inc - [STC ST00558NY](https://openairdocs.org/stc/ST00558NY): Installation of 242Y, 248Y/12J Passenger Configuration. (A310 SERIES -324). UT Finance Corporation. Lists A310 Series - [STC ST625CH](https://openairdocs.org/stc/ST625CH): Installation of replacement coffee maker over-temperature switch. Aircraft Food Service Equipment Repair - [STC ST00033LB](https://openairdocs.org/stc/ST00033LB): Installation of a piston and shoe assembly. California Precision Hydraulics, Inc - [STC ST492CH](https://openairdocs.org/stc/ST492CH): Installation of replacement coffee maker gaskets. Aircraft Food Service Equipment Repair - [STC ST00303AT](https://openairdocs.org/stc/ST00303AT): Installation of a Collins data link system. Delta Airlines Inc. Lists A310 Series - [STC SA3490NM](https://openairdocs.org/stc/SA3490NM): Installation of stretcher carrier, P/N AM 2003. Air Medic, Inc. Lists A310 Series - [STC ST338CH](https://openairdocs.org/stc/ST338CH): Installation of replacement lavatory cartridge heater. Aircraft Food Service Equipment Repair - [STC ST313CH](https://openairdocs.org/stc/ST313CH): Installation of replacement oven fan guard (grid). Aircraft Food Service Equipment Repair - [STC ST00034LB](https://openairdocs.org/stc/ST00034LB): Installation of piston and shoe assembly. California Precision Hydraulics, Inc - [STC ST00612AT](https://openairdocs.org/stc/ST00612AT): Installation of window shade cartridge assemblies. Magee Plastics Company. Lists A310 Series - [STC ST00546AT](https://openairdocs.org/stc/ST00546AT): Installation of 3-tier folding cart. BFE Services. Lists A310 Series All 64: https://openairdocs.org/model/airbus-a310-300/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Airbus Industrie A310-300](https://openairdocs.org/model/airbus-industrie-a310-300): 0 registered aircraft, registry code 3930305 --- 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.