Airbus A310-203

Service difficulty reports · 2,392

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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 = 'A310203'
  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 FDEA201302190369Shear Tie · misinstalledDURING ACCOMPLISHMENT OF EO 6-5310-7-5020 APT2. FOUND EDGE DISTANCE FOR HOLES H1 AND H2 AT FR 43 RT TO BE BELOW MINUM OF .472. R & R FRAME FOOT AT FR43 RT IAW SRM 51-72-10.Feb 19, 2013 · N410FE · Airbus A310203 · Fuselage Internal Mounting StructureSDR FDEA201302170357Skin · dentedDENT ON TAILCONE JUST AFT OF RIB 92 AND 93 BETWEEN STR 2L AND 3L APPROX. 1" X 1". REPAIRED DENT ON TAILCONE AFT OF FR 92 (RIB) BETWEEN STR 2 AND 3L IAW EA 6-5310-T0300131 REF WRI 53103597.Feb 17, 2013 · N410FE · Airbus A310203 · Aerodynamic FairingsSDR FDEA201302090314Web · corrodedAVIONICS COMPARTMENT LT SIDE WALL CORRODED AT WEB BETWEEN FR 14 AND 15 UNDER AIR CONDITION DUCT IN 3 PLACES. AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND TO BE OUT LIMITS IAW SRM 51-74-10. FABRICATED 2 EA WEBS IAW DWG A21214044 AND 2 EA ANGLES IAW DWG A2121404Feb 9, 2013 · N410FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201302090313Frame · corrodedFOUND 1" SQ OF CORROSION ON FRAME 14A LT AT STR 30L AREA FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL IAW SRM 51-74-10. REPAIRED FRAME 14A LT AT STR 30-32L IAW SRM 53-12-13.Feb 9, 2013 · N410FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201302090311Skin · crackedLT WING UPPER FIXED T/E AT AILERON ACTUATOR CUTOUT PANEL LANDING FOR PANEL 575 BT IS CRACKED .4 IN LENGTH. REMOVED LANDING AT LT WING UPPER FIXED T/E AT AILERON ACTUATOR CUT-OUT IAW SRM 51-40-21, PARA 5, 7, AND 16. LOCATED AND DRILLED NEW LANDING IAW SRM 5Feb 9, 2013 · N410FE · Airbus A310203 · Wing, Plate/SkinSDR FDEA201302040265Floor Panel · damagedFLOOR PANEL 231NH CRUSHED IN TWO LOCATIONS AT CLEVIS ADAPTER CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Feb 4, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201302040264Floorboard · damagedFLOOR PANEL 231AH CRUSHED, TWO LOCATIONS, AT CLEVIS ADAPTER CUTOUTS.Feb 4, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201302010252Skin · damagedRT ELEVATOR HAS TWO SMALL HOLES APPROX .2500" LONG X .1250" WIDE ON LOWER SIDE OF COMPOSITE. REPAIRED RT ELEVATOR LOWER SIDE BY CUTTING OUT DAMAGED SKIN, FILLING AND APPLYING REPAIR DOUBLER AND REPROTECTED COATING IAW SRM 55-21-11, PARA 5, I AND EA 6-5520-TFeb 1, 2013 · N410FE · Airbus A310203 · Elevator, Plate/SkinSDR FDEA201301310237Buffer · bindingDURING CLIMBOUT, FLAP VANE JAMMED. HANDLE WAS AT SLATS/FLAPS POS 15/0 . SLATS/FLAPS INDICATED 15/5. FLAPS SYS 1 AND SYS 2 FAULT LIGHTS ON. SLATS/FLAPS EXTENDED NORMALLY FOR LANDING. SFCC NR 1 AND SFCC NR 2 BOTH FAULTED " LT VANE OUT ". EFCU NR 1 FAULTS MJan 31, 2013 · N426FE · Airbus A310203 · Trailing Edge Flap Control SystemSDR FDEA201301300227Web · corrodedFLOOR LT SHEAR WEB UPPER SURFACE CORRODED AT 2 PLACES AND AT FOUR BOLTS AROUND PLUGGED DUCT BETWEEN FR 11 AND FR 12. AFTER LEVEL 1 CORROSION REMOVAL ON WEB FOUND TO BE OUT OF MFG DWG TOLERANCE. MFG NEW WEB AND REPLACED IAW SRM 51-40-20, PAR 6, PAR 7 AND SRM Jan 30, 2013 · N410FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201301290217Switch · malfunctionedDEPARTING & DURING FLAP RETRACTION, RECEIVED AN ECAM ALERT "FLAPS VANE JAM". COMPLIED WITH QRH, CYCLED THE FLAPS, AND UNABLE TO FIX PROBLEM. RETURNED TO DEPARTURE. FOUND BOTH NR 1 & NR 2 SFCC'S FAULTED "LT VANE IN 2" ON ARRIVAL. RESET BOTH SFCC'S & RETRAJan 29, 2013 · N426FE · Airbus A310203 · Trailing Edge Flap Control SystemSDR FDEA201301220160Skin · dentedFUSELAGE FRAMES 77-78, STRINGERS 27-28L, THREE DENTS MEASURED. DENTS NR 1 AND 3 OUT OF LIMITS IAW SRM 53-10-12, DIA 109, DENT NR 2 WITHIN LIMITS IAW SRM 53-10-12, DIA 109, FIG 110. NDT CONFIRMS NO CRACK CONDITION EXISTS INTERNAL AND EXTERNAL IAW NTM 51-10-07Jan 22, 2013 · N410FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201301220158Floor Support · corrodedAFT CARGO BAY LONGITUDINAL BEAM BETWEEN FR 63-64 HAS A 1" SQ AREA OF CORROSION AT LWR SURFACE LT SIDE. AFTER REMOVAL OF LEVEL 1 CORROSION FOUND AFT CARGO COMPT LONGITUDINAL BEAM BETWEEN FR 63-64, LT SIDE TO BE OUT OF LIMITS IAW DWG 17, A255-71979. R & R LONGJan 22, 2013 · N410FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201301210154Tee Fitting · corrodedAVIONICS COMPARTMENT CEILING TEE FITTING AT SEAT TRACK 5L CORRODED AT FR 14 AROUND CLIPNUT. R & R TEE FITTING DUE TO BEYOND REPAIR IAW SRM 51-72-10, PAGE 2, PARA. 5. REPROTECTED FASTENERS IAW SRM 51-75-10.Jan 21, 2013 · N410FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201301210152Controller · inoperativeCLIMBING OUT OF 12,000 RECEIVED A "CABIN ALT EXCEEDS 10,000" RED ECAM. DONNED O2 MASK. CABIN WAS VERIFIED ABOVE 10,000. BOTH FWD & AFT FLOW VALVE ON NR 2 SYSTEM WERE FULLY OPENED AND AMBER. BOTH FWD & AFT OUTFLOW VALVE ON NR 1 SYS WERE FULLY CLOSED. WJan 21, 2013 · N427FE · Airbus A310203 · Cabin Pressure ControllerSDR FDEA201301190149Seat Track · corrodedSEAT TRACK 5R CORRODED AT THE FLANGES AT FR 15A, CORROSION OUT OF LIMITS. MATERIAL LOSS IS .063". R & R SEAT TRACK 5R AT FR 15A.Jan 19, 2013 · N410FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201301190147Structure · damagedON REMOVAL OF SEAT TRACK 5R FR 15A, FOUND THREE ELONGATED HOLES ON EXISTING MATING STRUCTURE (EXTRUSION) EXTRUSION BEYOND ECONOMICAL REPAIR. R & R EXTRUSION IAW SRM 51-72-10. REPROTECTED IAW SRM 51-75-10.Jan 19, 2013 · N410FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201301190143Floor Panel · crackedFLOOR PANEL 262MF CRACKED ACROSS MID SECTION AT CLEVIS ADAPTER CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jan 19, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301160108Cargo Track · damagedMAIN DECK CARGO TRACK 3R HAS 2 INCH LONG DAMAGED AREA AT FR 74. FABRICATED, LOCATED, DRILLED, AND INSTALLED NEW SEAT TRACK SECTION 3R WITH SPLICES FROM FR73.5 TO 74.5 IN MDCC IAW SRM 51-72-10 PARA 6, SRM 51-40-21 PARA 6 & 8, AND SRM 53-10-16 PG 247-248. PJan 16, 2013 · N410FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201301160110Seat Track · corrodedFR 79-80 SEAT TRACK 4L HAS 2EA AREAS OF CORROSION AT UPPER SURFACE. REMOVED CORROSION & FOUND OUT OF LIIMITS IAW SRM 53-10-16, FIG 101. FABRICATED, DRILLED, LOCATED, AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-16.Jan 16, 2013 · N410FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201301110078Floor Panel · damagedFLOOR PANEL BETWEEN TRACKS 2L AND 3L AND FR 51 AND FR 59 HAS TWO AREAS OF IMPACT DAMAGE. REMOVED AND REINSTALLED NEW FLOOR PANEL IAW AMM 53-10-25-04 FABRICATED NEW FLOOR PANEL IAW DWG 5RZ-25-005Jan 11, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301110077Floor Panel · damagedFLOOR PANEL BETWEEN TRACKS 2R & 3R AND FR 59 AND FR61 HAS THREE AREAS OF IMPACT DAMAGE. REMOVED AND REINSTALLED NEW FLOOR PANEL IAW 310 53-10-25-04 FABRICATED NEW FLOOR PANEL IAW DWG 5RZ -25-005Jan 11, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301110082Floor Panel · crackedFLOOR PANEL BETWEEN SEAT TRACKS 2R & 3R, FR33 & FR37 TOP SKIN CRACKED IN TWO PLACES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jan 11, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301110079Floorboard · crackedFLOORBOARD BETWEEN SEATS TRACKS 2R & 3R FR34 THRU FR 36 TOP SKIN CRACKED IN TWO PLACES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jan 11, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301110075Floorboard · damagedMAIN DECK CARGO FLOORBOARD 242EK BETWEEN SEAT TRACK 2R AND 3R, FR 50 AND FR 54, HAS TWO INSERTS PULLED OUT AND TWO AREAS OF IMPACT DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jan 11, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301110074Floorboard · crackedFLOORBOARD 231YH HAS AN 11 INCH CRACK AT CLEVIS CUT OUT. FABRICATED FLOORBOARD IAW DWG, SRZ 25-005, REV J.Jan 11, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301110073Floorboard · damagedFLOORBOARD 252WH UPPER SURFACE HAS 10 SQUARE INCHES CRUSHED & DAMAGED AT MID CLEVIS AND THREE WORN INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jan 11, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301110072Floorboard · damagedFLOORBOARD 252RT UPPER SURFACE HAS THREE 1 SQUARE INCH PUNCTURE AND THREE WORN INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jan 11, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301090057Floorboard · crackedFLOORBOARD 252GF CRACKED AROUND CLEVIS ADAPTER, FABRICATED FLOORBOARD IAW DWG, SRZ 25-005, REV J.Jan 9, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301080055Floorboard · damagedFLOORBOARD 143DF HAS BROKEN OUT EDGE FILLER, 60". FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jan 8, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301080054Unknown · unknownATS LEVER TRIPPED OFF AT TOGA ON TAKEOFF. RESET ATS LEVER AND SELECTED TOGA AGAIN, SAME RESULT. ABORTED TAKEOFF. AT BLOCK IN CREW REPORTED THAT AFTER RESETTING YAW DAMP AND TRIM SWITCHES, AUTOTHROTTLE OPERATED NORMALLY THE WHOLE FLT. PERFORMED MTP TEST ANJan 8, 2013 · N431FE · Airbus A310203 · Auto Throttle SystemSDR FDEA201301070031Floor Panel · crackedFLOOR PANEL 251NG TOP SKIN CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jan 7, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301070034Floorboard · crackedFLOORBOARD 221CF CRACKED AT TWO PLACES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jan 7, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301070033Floorboard · damagedFLOORBOARD 242BF CRUSHED AT UPPER SIDE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jan 7, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301060030Adapter · damagedMAIN DECK CARGO CLEVIS ADAPTER AT FR 36 BETWEEN SEAT TRACKS 4L AND 5L HAS IMPACT DAMAGE AT SCALLOP ONE SQUARE INCH. AFTER BLEND OUT OF DAMAGED AREA IAW SRM 51-73-10, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, FIG 101. R & R CLEVIS ADAPTER IAW SRM 51-75-10Jan 6, 2013 · N410FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201301060029Floor Panel · crackedFLOOR PANEL 242QJ HAS THREE PLACES WITH CRACKS IN TOP SKIN AND ONE MISSING INSERT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jan 6, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301060028Floor Panel · crackedFLOOR PANEL 241MK TOP SKIN CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jan 6, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301040014Floorboard · damagedFLOORBOARD 242ZJ, CRUSHED AT UPPER SIDE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ -25-005, REV J.Jan 4, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201301040013Floorboard · damagedFLOORBOARD 242UJ CRUSHED AT UPPER SIDE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ-25-005, REV J.Jan 4, 2013 · N410FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201212134295Warning Light · false activationAPPROX 10 MINUTES INTO FLIGHT, ECAM "HYD GREEN RSVR LO LEVEL" QUANTITY INDICATED. TURNED PUMPS OFF IAW ECAM. FOLLOWED QRH PROCEDURES TO EXTEND LANDING GEAR. LANDING UNEVENTFUL. CLEANED WHEEL WELL AND SERVICED GREEN SYS. HYD TO MIDDLE OF THE HAT AMM 12-12-Dec 13, 2012 · N429FE · Airbus A310203 · Hydraulic System, MainSDR FDEA201210313788Jackscrew · failedDURING DESCENT AT MEM TO 36R, SLATS WOULD NOT EXTEND AT 210 KTS. EXECUTED QRH PROCEDURES, DECLARED EMERGENCY AND REMAINDER OF APPROACH AND LANDING NORMAL. CREW LEFT SLAT/FLAP HANDLE IN 30/40 POSITION TO ASSIST MX PROCEDURES. REMOVED REPLACED RIGHT WING NR Oct 31, 2012 · N435FE · Airbus A310203 · Leading Edge Slat Control SystemSDR FDEA201210303780Hinge Fitting · crackedLEFT MLG UNSAFE DOOR INDICATION ON T/O. THEN UNSAFE MLG INDICATION ON APPROACH. FOUND LT MLG CENTER HINGE FITTINGS FRACTURED AT ACTUATOR ATTACHEMENT LUG, AND CROSSOVER BEAM FITTING CRACKED. REMOVED AND REPLACED LT MLG CENTER HINGE FITTINGS AND CROSSOVER BEAOct 30, 2012 · N403FE · Airbus A310203 · Landing Gear DoorsSDR FDEA201210103586Actuator · leakingDURING RETRACTION OF THE LANDING GEAR, LEFT ECAM ANNUNCIATED GREEN HYD SYS QUANTITY/PRESSURE LOSS. COMPLIED WITH ECAM AND QRH MANUALLY EXTENDING THE LANDING GEAR FOR UNEVENTFUL LANDING AT DEPARTURE AIRPORT. FOUND LT KRUGER FLAP ACTUATOR SWIVEL BLOWN OUT. Oct 10, 2012 · N431FE · Airbus A310203 · Leading Edge Slat ActuatorSDR FDEA201209013204Outflow Valve · inoperativeRT NR 1 PRESSURE REGULATOR FAULT DURING CLIMB, FWD NR 1 OUTFLOW VALVE STUCK FULL OPEN. QRH NO HELP. CABIN WOULD NOT PRESSURIZE. TROUBLESHOT TO NR 1 FWD OUTFLOW VALVE STUCK OPEN. REPLACED OUTFLOW VALVE IAW AMM CH 21-31-12-04-01. OPS CKS GOOD. ACFT OK FOR Sep 1, 2012 · N410FE · Airbus A310203 · Pressure Regulator/Outflow ValveSDR FDEA201208243148Structure · damagedLT WING NR 6 SPOILER HAS HOLE APPROX .25W X .56L X .25D. LOCATED 12.125" FROM OTBD EDGE AND 21" FROM T/E OF SPOILER REPAIRED ONE HOLE MEASURING .25W X .56L X .25D ON NR 6 SPOILER USING RESIN & CARBON FIBER IAW SRM 57-76-11, PAR 12C. COMPLIED WITH EA 6-5750-1Aug 24, 2012 · N428FE · Airbus A310203 · SpoilersSDR FDEA201208233144Filter · cloggedREJECTED TAKEOFF AT 70 KTS FOR NR 2 ENGINE FUEL FILTER CLOG ALERT ON ECAM. REPLACED NR 2 ENGINE MAIN FUEL FILTER IAW MM 73-12-03-02 IDLE LEAK CHECKED GOOD. RAN NR 2 ENGINE AT TAKE OFF POWER IAW JRH. NO ECAM MESSAGES NOTED OK TO CONTINUE.Aug 23, 2012 · N403FE · Airbus A310203 · Engine Fuel DistributionSDR FDEA201208233141Controller · failedSLATS FAILED TO EXTEND ON APPROACH. CHECKED NR 1 AND NR 2 SFCCS. NR 1 SFCC FAULTS JAM, NR 2 SFCC FAULTS LT RETRACT SWITCH. ADDED MPN 49-079-05 QTY 2 EA CG, SFCC1 - SLATS JAM - SEE TSM 27-80-02 (FIRST TIME OCCURANCE) THIS CHECKS DRIVE LINE AND COMPONENTAug 23, 2012 · N443FE · Airbus A310203 · Leading Edge Slat Control SystemSDR FDEA201208032826Controller · faultedPASSING THROUGH 10,000 FT, RECEIVED CABIN ALT ALERT. DESCENDED TO 10,000. ACFT WOULD NOT PRESSURIZE IN AUTO WITH REGULATORS NR 1, NR 2 OR IN MANUAL POSITION. ALL DOORS & OUTFLOW VALVES INDICATED, SHOWED CLOSED. FOUND NR 2 CABIN PRESSURE CONTROLLER FAULTINGAug 3, 2012 · N410FE · Airbus A310203 · Cabin Pressure ControllerSDR FDEA201207152580Skin · damagedDURING INSPECTION OF CIRCUMFERENTIAL SKIN JOINT AT FR 54 BETWEEN STGR 45 LT AND STGR 44 LT FASTENER HOLE 1EA WITH PRIOR BUSHING REPAIR IS ELONGATED. WORK IN CONJUNCTION WITH WORK CARD T 6-5330-29226 C P3. COMPLIED WITH EA 6-5330-160142 - FUSELAGE - MAIN Jul 15, 2012 · N403FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201207152579Skin · crackedLT WING FIXED L/E INBD CUT OUT FOR SHUTTER DOOR NR 1 TOP EXTERNAL SKIN CRACKED 1.25" APPROXIMATELY. REPAIRED SKIN IAW SRM 51-40-21 DWGS A57246236, A57246240 AND EA 6-5740.Jul 15, 2012 · N429FE · Airbus A310203 · Wing, Plate/Skin
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