Airbus A310-324

Service difficulty reports · 1,439

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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 = 'A310324'
  ORDER BY difficulty_date DESC"

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SDR FDEA201601040020Stringer · corrodedAFT CARGO BAY, STRINGER 55R, FOUND CORRODED BETWEEN FRAMES 64 - 65. REPAIRED THE STRINGER IAW SRM 53-10-14-201 FIG 201 VIEW F & G. MAJOR REPAIR IAW GMM 6-2-100.Jan 4, 2016 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201512304106Beam · corrodedCENTER WING FUEL TANK, BOTTOM SKIN LONGITUDINAL BEAM 4RT OTBD ATTACHED SPLICE FITTING, CORRODED AT FRAME 40. BLENDED OUT & SMOOTHED THE CORRODED AREA IAW SRM 51-74-10. THE DAMAGE WAS OUT OF THE DESIGN THICKNESS TOLERANCE IAW DWG A57112070. REPLACED IAW SRM Dec 30, 2015 · N809FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA201512304105Stringer · corrodedFORWARD CARGO COMPARTMENT STRINGER 44R CORRODED BETWEEN FRAMES 38 - 38.1. REPAIRED THE STRINGER IAW SRM 53-10-14-201 FIG 201. MAJOR REPAIR IAW GMM 6-2-100.Dec 30, 2015 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201512304104Stringer Splice · corrodedAFT CARGO BAY STRINGER 54L, STRINGER SPLICE FITTING FOUND CORRODED AT FRAME 65. REPLACED THE SPLICE FITTING IAW SRM 51-40-21. THIS IS A MAJOR REPAIR IAW GMM 6-2-100.Dec 30, 2015 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201512284090Engine · power lossDURING DESCENT BELOW PROFILE THRUST WAS APPROX 75 - 77% N1. AT PROFILE THROTTLES REDUCED TO IDLE & APPROX 60% N1, A THUMPING SOUND WAS HEARD & FELT. SUSPECT COMPRESSOR STALL. ALTITUDE 30000 FT SPEED 0.8. NO ABNORMAL ENG INDICATIONS. SUSPECT ENG NR 2. Dec 28, 2015 · N808FD · Airbus A310324 · Engine (Turbine/Turboprop)SDR FDEA201512264080Stringer · corrodedEXISTING REPAIR ON FUSELAGE STRINGER 55 LT SIDE, BETWEEN FRAME 59 & 61 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & CORROSION WAS FOUND AT THE REPAIR AREA. THE EXISTING SPLICE REPAIR WAS REMOVED & PERFORMED AGAIN IAW SRM 53-10-14 FDec 26, 2015 · N809FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201512013845Door · departedON DEPARTURE, MAIN WW FWD LEFT & CENTER DOORS DEPARTED ACFT.Dec 1, 2015 · N809FD · Airbus A310324 · Service DoorsSDR FDEA201511213745Flap · stuckFLAP SYS 1 & 2 FAULT, FLAPS STUCK. REMOVED TWO BOLTS FROM RT TORQUE LIMITED COUPLER TO FOM. DRAINED FLUID FROM RT WING NR 1 FLAP DRIVE GEAR BOX FOR INSPECTION PURPOSE. GPS OVERRIDE SWITCH IN COCKPIT, CAPTAINS RIGHT KNEE, REQUIRES SAFETY. FOUND JAM FAULTS ONov 21, 2015 · N803FD · Airbus A310324 · Trailing Edge Flap Control SystemSDR FDEA201511193714Bracket · damagedON POST FLIGHT FOUND FUELING DOOR 144DR MISSING WITH DAMAGE TO RT PACK INLET FAIRING. REPLACED BROKEN COOLING DUCT SUPPORT BRACKET IAW SRM 51-72-10. REMOVED AND REPLACED R/H AIR INLET FAIRINGS DUCT AND REFUELING PANEL DOOR ASSY IAW MM 53-15-73-04 AND 52-42-Nov 19, 2015 · N804FD · Airbus A310324 · Fluid Service DoorsSDR FDEA201510313432Actuator · leakingBLUE RESERVOIR LO LEVEL ECAM WITH ASSOCIATED SPOILERS FAULTS. FOLLOWED ECAM & QRH, RETURNED FOR UNEVENTFUL LANDING. FOUND NR 3 RT SPOILER ACTUATOR, SIDE CAP BLOWN OUT, REQUIRES ACTUATOR PART. R & R NR 3 RT SPOILER ACTUATOR IAW AMM 27-64-14-04. OPERATIONAL Oct 31, 2015 · N804FD · Airbus A310324 · Drag Control ActuatorSDR FDEA201510303445Computer · failedDURING LANDING, GEAR EXTENSIONS WITH POSITION DETECTOR, SYS NR 2 SELECTED, GOT ECAM, LG DOOR SYS INOPERATIVE UNTIL ALL GEARS WERE DOWN & LOCKED. SYS NR 1 MEL'D, INOPERATIVE. R & R NR 2 FLIGHT WARNING COMPUTER IAW AMM 31-53-34-04. PERFORMED ECAM & LG WARNINGOct 30, 2015 · N804FD · Airbus A310324 · Central WarningSDR FDEA201509172894Switch · failedDURING TAKEOFF ROLL, RECEIVED A MOMENTARY NR 2 THRUST REVERSER UNLOCKED ALERT & INSTRUMENT CLUSTER TOP LIGHT. LIGHT EXTINGUISHED & TAKEOFF WAS CONTINUED. AFTER TAKEOFF & WHEELS UP, THE ALERT CAME BACK ON. NO ADVERSE CONTROL WAS NOTICED. COMPLIED WITH ECAM.Sep 17, 2015 · N810FD · Airbus A310324 · Engine Thrust ReverserSDR FDEA201508252695Stringer · damagedREMOVED STRINGER 44 AT FRAME 19 - 20 TO FOM. REMOVED SHEAR TIE & COUPLING. COUPLING & STRINGER FOUND TO BE DAMAGED. FABRICATED NEW STRINGER ON T15 1157203. RECEIVED NEW COUPLING, INSTALLED SHEAR TIE, COUPLING & STRINGER 44 AT FRAME 19 - 20 IAW SRM 51-40-21Aug 25, 2015 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201507072165Hydraulic Line · leakingEN-ROUTE, GREEN HYD LEVEL DECREASING SLOWLY. DESCENDING THRU FL 150, ECAM WARNING, HYD LEVEL LO, RAN QRH. LEAK FOUND AT LT MAIN GEAR FLEX HOSE PN 00624AE711082-4 FOR STRUT BRACE ACTUATOR. REPLACED WITH ALTN FROM HYD SPARE KIT PN 24060610-0240. PERFORMED PRJul 7, 2015 · N811FD · Airbus A310324 · Hydraulic System, MainSDR FDEA201506231983Proximity Sensor · failedLANDING GEAR WOULD NOT RETRACT USING SYSTEM 1. REMOVED AND REPLACED THE LEFT MAIN GEAR TORQUE LINK PROXIMITY DETECTOR IAW AMM 32-00-00-04.Jun 23, 2015 · N809FD · Airbus A310324 · Landing Gear Position and WarningSDR FDEA201506181846Crossbeam · corrodedBULK CARGO FRAME 67 -Y-940, CROSSBEAM WITH INNER GRANULAR CORROSION. REPLACED THE CORRODED CROSSBEAM OF BULK CARGO IAW SRM 51-40-21. THIS REPAIR CATEGORY A, MAJOR REPAIR IAW GMM6-2-100.Jun 18, 2015 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201506171831Windshield · crackedAT FL 370 CAPTAIN`S OUTER WINDSCREEN SHATTERED. PRESSURIZATION HELD OK, DIVERTED. R & R CAPTAIN`S WINDSHIELD PANEL IAW AMM 56-11-11-04. WINDSHIELD PANEL ANTI-ICING & DE- FOGGING OPERATIONAL TESTED SATISFACTORY.Jun 17, 2015 · N808FD · Airbus A310324 · Flight Compartment WindowsSDR FDEA201506151817Repair · delaminatedAGEING INSPECTION, EXISTING REPAIR ON RT OUTER FLAP, UPPER SKIN OUT OF RIB 10 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH APPROVED DATA. BUT INSPECTION FOUND DELAMINATION ON OLD REPAIR. REPAIRED THE DAMAGJun 15, 2015 · N803FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201506151816Repair · delaminatedAGEING INSPECTION, EXISTING REPAIR ON RT OUTER FLAP, UPPER SKIN OUT OF RIB 10 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH APPROVED DATA. BUT INSPECTION FOUND DELAMINATION ON OLD REPAIR. REPAIRED THE DAMAGJun 15, 2015 · N803FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201506151815Skin · delaminatedAGEING INSPECTION, EXISTING REPAIR ON RT OUTER FLAP UPPER SKIN OUT OF RIB 10 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH APPROVED DATA. BUT INSPECTION FOUND DELAMINATION ON OLD REPAIR. REPAIRED THE DAMAGEJun 15, 2015 · N803FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201506151812Skin · crackedRIGHT WING FIXED TE LOWER SKIN AT RIBS 11 - 12 CRACKED 1 INCH. REPAIRED IAW EA 6-5730-T0318078 & R57249152. MAJOR REPAIR IAW GMM 6-2-100.Jun 15, 2015 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201505061396Skin · crackedRIGHT WING ROOT REAR SPAR BOTTOM SKIN FOUND ONE EACH FASTENER HEAD POPPED OUT. REMOVED THE HEAD POPPED OUT FASTENER IAW SRM 51-40-21. CARRIED OUT ROTOTEST INSPECTION TO FASTENER HOLE IAW NTM 51-10-18, FOUND CRACK. REAMED THE HOLE TO REMOVE CRACK IAW SRM 51-May 6, 2015 · N811FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201505031377Sensor · failedMLG WOULD NOT COME UP DURING DEPARTURE IN SYS 1 & SWITCHED TO SYS 2 & STILL WOULD NOT COME UP. ALSO HAD ADC 1 FAULT, PITCH TRIM NR 1 FAULT, CAPTAIN PROBABLY HEAT, MULTIPLE TIMES. THE JET THOUGHT IT WAS STILL ON THE GND. ALSO CABIN PRESSURE NR 1 FAULT. ALSOMay 3, 2015 · N809FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201504301331Window · failedAFTER TAKEOFF GOT RT WINDOW HEAT FAULT. FOLLOWED QRH & RESET RT WINDOW HEAT. LATER CLIMBING THROUGH FL 280, THE LT WINDSHIELD COMPLETELY SHATTERED ON THE OUTSIDE PANE WITH NO WARNING. THERE WAS SOME ELEC ARCING AFTERWARD. LATER ON DESCENT GOT RT WINDOW HEAApr 30, 2015 · N808FD · Airbus A310324 · Flight Compartment WindowsSDR FDEA201504291321Fairing · crackedRIGHT WING TIP FENCE FAIRING RIB CRACKED, WY495. REPLACED THE CRACKED RIB OF RT WING TIP FENCE FAIRING AT WY 501 IAW SRM 51-40-21.Apr 29, 2015 · N811FD · Airbus A310324 · Wing Main, Frame StructureSDR FDEA201504291320Rib · crackedRIGHT WING TIP FENCE FAIRING AROUND FASTENER HOLES CRACKED AT WY501. REPLACED IAW SRM 51-40-21.Apr 29, 2015 · N811FD · Airbus A310324 · Wing, Rib/BulkheadSDR FDEA201504291319Frame · corrodedAV COMPARTMENT FOUND FRAME 17 CORRODED BETWEEN STRINGER 42 & 43L. BLENDED OUT THE CORROSION IAW SRM 51-74-10 & EA 6-5310-T0317322 P1.Apr 29, 2015 · N811FD · Airbus A310324 · Fuselage Main, FrameSDR FDEA201504291318Frame · nickedMDCC LT FRAME 34 SURFACE FOUND NICK BETWEEN STRINGER 12LT & 22LT. BLEND OUT & SMOOTHED THE NICK AREA IAW SRM51-73-10. APPLIED ALODINE IAW SRM 51-21-10. NO CRACK FOUND IAW NTM 51-10-08. COMPLIED WITH EA6-5310-T0317082.Apr 29, 2015 · N811FD · Airbus A310324 · Fuselage Main, FrameSDR FDEA201504161242Door Frame · crackedFORWARD CARGO DOOR ACTUATOR ATTACH FITTING. SDI FOUND CRACK WITH A HFEC INSPECTION. REMOVED THE FWD CARGO DOOR IAW AMM 52-31-11-04. REPLACED THE CRACKED FRAME OF FWD CARGO DOOR IAW SRM 51-40-21. INSTALLED THE FWD CARGO DOOR IAW AMM 52-31-11-04 & TESTED OK.Apr 16, 2015 · N811FD · Airbus A310324 · Cargo/Baggage DoorsSDR FDEA201504161241Fitting · crackedAFT CARGO COMPARTMENT DOOR ACTUATOR FITTINGS. FOUND CRACK WITH A HFEC INSPECTION. REPLACED THE CRACKED FRAME OF AFT CARGO DOOR AT FRAME 61A IAW SRM 51-40-21. INSTALLED THE AFT CARGO DOOR IAW AMM 52-31-11-04 & TESTED OK. MAJOR REPAIR IAW GMM 6-2-100.Apr 16, 2015 · N811FD · Airbus A310324 · Cargo/Baggage DoorsSDR FDEA201504081201Altimeter · malfunctionedREPEAT WRITE UP, STBY ALTIMETER WITHIN 30' OF PRIMARY ALTIMETERS ON THE GND. AT FL 300 STBY ALTIMETER WAS 160 FT HIGHER, AT FL 148 STBY ALTIMETER WAS 250 FT HIGHER. R & R THE STBY ALTIMETER IAW AMM 34-12-22-04. INTEGRAL LIGHTING OPERATIONAL TEST NORMAL IAW Apr 8, 2015 · N810FD · Airbus A310324 · Altimeter, Barometric/EncoderSDR FDEA201504071200Altimeter · malfunctionedAT CRUISE ALTITUDE 35,000, STBY ALTIMETER INDICATES 250 HIGHER THAN BOTH CAPTAINS & COPILOTS ALTIMETERS. R & R THE STBY ALTIMETER IAW AMM 34-12-22-04. INTEGRAL LIGHTING OPERATIONAL TEST NORMAL IAW AMM 33-13-00-05. ACFT OK FOR SERVICE.Apr 7, 2015 · N810FD · Airbus A310324 · Altimeter, Barometric/EncoderSDR FDEA201503060700Slide · unwanted deployDOOR R1 SLIDE DEPLOYED ACCIDENTALLY AT BLOCK. REMOVED AND REPLACED THE R1 SLIDE IAW MM 25-61-22-04-02, ARMED THE R1 SLIDE OPS TEST IAW MM 52-73-00-05. REMOVED AND REPLACED THE DIAPHRAGM AND SERVICED THE EMERGENCY OPERATION CYLINDER OF R1 DOOR IAW AMM 52-1Mar 6, 2015 · N804FD · Airbus A310324 · Escape SlideSDR FDEA201503020625Seat Track · damagedCOMPLY WITH WRI 25-50/0216 & 0217, REPAIR THE SEAT TRACK ASSEMBLY OF MDC FRAME 54.2 - 58 RESTRAINT ID N1199. REPAIRED THE SEAT TRACK IAW SRM 53-10-16 FIGURE 202. THIS REPAIR CATEGORY A. MAJOR REPAIR IAW GMM 6-2-100.Mar 2, 2015 · N810FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201502220573Skin · damagedFOUND ONE LIGHTNING STRIKE AT THE TRAILING EDGE OF THE LT WING TIP UPPER INBD SURFACE. REPLACED THE SKIN IAW SRM 57-30-11.Feb 22, 2015 · N808FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201502160536Fitting · crackedAFT CARGO COMPARTMENT DOOR ACTUATOR FITTING CRACKED. REMOVED THE AFT CARGO DOOR ASSEMBLY IAW AMM 52-32-11-04. REPLACED THE FRAME HEAD IAW SRM 51-40-21. INSTALLED THE AFT CARGO DOOR ASSEMBLY IAW AMM 52-32-11-04. TESTED OK.Feb 16, 2015 · N808FD · Airbus A310324 · Cargo/Baggage DoorsSDR FDEA201502130527Crossbeam · corrodedAFT CARGO FLOOR FRAME 63 CROSSBEAM CORRODED BETWEEN Y140 & Y805. REPAIRED THE CROSSBEAM PER SRM 53-10-15 FIG.209.SHT.1Feb 13, 2015 · N808FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA201502130526Crossbeam · corrodedAFT CARGO FLOOR FRAME 61 CROSSBEAM CORRODED BETWEEN -Y805 & Y805. REPAIR THE CROSSBEAM PER SRM 53-10-15 FIG.209 SHT.1Feb 13, 2015 · N808FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA201501070049Bleed Valve · malfunctionedFLIGHT DEPARTED WITH MEL 36-11-06-1A, NR 1 BLEED AIR VLV INOPERATIVE. DURING CLIMB OUT, WE DEVELOPED A NR 2 HP BLEED FAULT. FOLLOWED ECAM & QRH PROCEDURES. PROCEDURES LED US TO DUAL BLEED FAILURE CHECKLIST & WE COMPLIED. R & R NR 2 ENG HP BLEED VLV IAW MM Jan 7, 2015 · N808FD · Airbus A310324 · Compressor Bleed ValveSDR FDEA201410123118Skin · corrodedLEFT WING UPPER SURFACE SKIN FOUND CORROSION AT THE FRONT OF NR 2 SPOILER. REPAIRED LT WING UPPER SURFACE SKIN IAW EA 6-5730-T0311884 P1. TITLE WING PLATES & SKINS LHS WING TOP SKIN PANEL 2 TE OVERHANG CORROSION REPAIR BETWEEN RIBS 5 - 7. MAJOR REPAIR IAW GOct 12, 2014 · N807FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201410113111Tee Fitting · crackedCENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING RT NR 10 FASTENER HOLE WITH CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0312253 TITLE WINGS BASIC WING STRUCTURE SB A310-57-2047 FRAME 47 HOLES CRACKED. MAJOR REPAIR IAW GMM 6-2-100.Oct 11, 2014 · N807FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201410062974Bracket · crackedLEFT AILERON OTBD HINGE PANEL BRACKET CRACKED REPAIRED LT AILERON OTBD HINGE PANEL BRACKET IAW EA 6-5750-T0312135. WINGS FLIGHT SURFACES FRONT SPAR LOWER DOUBLER BROKEN AT LT AILERON LOWER SURFACE LE MAJOR REPAIR IAW GMM 6-2-100.Oct 6, 2014 · N807FD · Airbus A310324 · AileronsSDR FDEA201410032930Fitting · crackedANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.Oct 3, 2014 · N807FD · Airbus A310324 · Fuselage Main, Attach FittingsSDR FDEA201410032929Angle · crackedANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.Oct 3, 2014 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201410032928Angle · crackedANGLE & TEE FITTING CRACKED FRAME 47. REPAIRED IAW IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.Oct 3, 2014 · N807FD · Airbus A310324 · Wing Main, Frame StructureSDR FDEA201410032927Angle · crackedREAR SPAR INTERNAL ANGLE & TEE FITTING RT NR 1 FASTENER HOLE WITH A CRACK SIGNAL. REPAIREDSPAR ANGLE & TEE FITTING IAW EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100.Oct 3, 2014 · N807FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201409302860Floorbeam · corrodedFORWARD CARGO COMPARTMENT FLOORBEAM TEE CORRODED AT FRAME 37, Y140 - Y805. REPAIRED THE FLOORBEAM IAW EA 6-5310-T0311889. MAJOR REPAIR IAW GMM 6-2-100.Sep 30, 2014 · N807FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA201409272822Floorbeam · delaminatedAFT CARGO BAY FLOORBEAM TEE FOUND DELAMINATION AT FRAME 60 Y-805 - Y-1470. CUT THE DELAMINATED BEAM IAW SRM 53-10-15 FIG 207 CHECKED THE CRACKS TO CUTOUT PER NTM 51-10-08 MADE THE REPAIR PARTS IAW SRM 53-10-15 FIG 207 WET INSTALLED THE REPAIR IAW SRM 51-4Sep 27, 2014 · N807FD · Airbus A310324 · Fuselage Main, Floor BeamSDR FDEA201409242751Fitting · crackedCENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING LT NR 10 FASTENER HOLE WITH CRACK SIGNAL. REPAIRED CENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING LT NR 10 FASTENER HOLE PER EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100Sep 24, 2014 · N807FD · Airbus A310324 · Wing Miscellaneous StructureSDR FDEA201409112578Skin · corrodedAV COMPARTMENT FUSELAGE SKIN FRAME 16A - 17 STRINGER 44 - 45 RT INNER SURFACE FOUND CORROSION. COMPLIED WITH EA 6-5310-T0310792 P1 EA TITLE FUSELAGE MAIN FRAME CORROSION INTERNAL DOUBLER AT FRAME 16A - 17. MAJOR REPAIR IAW GMM 6-2-100.Sep 11, 2014 · N804FD · Airbus A310324 · Fuselage Main, Plate/Skin
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