Airbus A318-111

Service difficulty reports · 353

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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 = 'A318111'
  ORDER BY difficulty_date DESC"

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SDR ANCF2012080300127Valve · damagedAFTER TAKEOFF PROCEDURE TO PEI - VENT SKIN VALVE ECAM APPEARS AND THE CAB ALT STAYS AT 5000FT AND DOES NOT PRESSURIZE. -- IN ACCORDANCE WITH TASK 21-31-00-710- 002-A OPERATIONAL TEST OF THE PRESSURIZATION CONTROL MONITORING WAS ACCOMPLISHED IN BOTH PCP. IT WAug 3, 2012 · N597EL · Airbus A318111 · Pressure Regulator/Outflow ValveSDR F3LA2012053000764Girt Bar · out of adjustL2 DOOR SLIDE DOES NOT SHOW ARMED IN FLIGHT SHOWS ARMED ON GROUND. FOUND L2 DOOR GIRT BAR FITTINGS OUT OF ADJUSTMENT. ADJUSTED GIRT BAR FITTINGS IAW AMM 52-13-22-820-056-A.May 29, 2012 · N801FR · Airbus A318111 · Emergency EquipmentSDR F3LA2012053000762Actuator · failedSTRONG ELECTRICAL/OIL ODOR FUMES IN COCKPIT AND CABIN ON CLIMB. RETURNED TO DEPARTURE. NR 1 PACK OVERHEAT FAULT. SHUTDOWN PACK, BLOWING VERY HOT AIR. REMOVE AND REPLACE NR 1 ACM IAW AMM 21-52-21 PB 401. OPS CHECKED GOOD.May 25, 2012 · N801FR · Airbus A318111 · Cabin Cooling SystemSDR ANCF2012050400122Unknown · smokeON GROUND WITHOUT PASSENGERS ON BOARD, AFTER OPENING PAX DOOR 1L AND COMING INTO THE AIRCRAFT A STRONG ELECTRICAL SMOKE. DOOR WAS LEFT ON FORWARD GALLEY CLOSE C/B PANEL. IN ACCORDANCE WITH 05-21-20 AND 05-22-10 THE FORWARD CABIN UTILITY AREA OVERHEAD COMPARTMMay 1, 2012 · N597EL · Airbus A318111 · Air Distribution SystemSDR ANCF2012040800119Warning Light · false activationDURING FLIGHT, NR 1 ENGINE COMPRESSOR VANE FAULT ECAM ILLUMINATED. IAW AMM 73-29-00-710-040B OPS TEST OF THE FADEC ON GROUND PERFORMED WITH ENGINE MOTORING & MCDU SHOW NO FAULT RECORDED. IAW AMM 75-31-20-820-001, VBV SYSTEM WAS CLOSED DIMENSION A AND B WERE Apr 8, 2012 · N592EL · Airbus A318111 · Engine Indicating SystemSDR F3LA2012041000740Plate · corrodedLATERAL SHEAR PLATE FRAME 69 TO FRAME 70, STRINGER 23 RT TO STRINGER 24 RT HAS CORROSION. R & R SHEAR PLATE IAW SRM 51 -42-11, PARA 6 B-18, D 1-5 AND EO AO-53EO-31 434.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2012041000739Plate · corrodedLATERAL SHEAR PLATE FRAME 69 TO FRAME 70, STRINGER 23 LT TO STRINGER 24 LT HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11 PARAGRAPH 6 B-1 B, 0 1-5 AND EO AO-53EO-31434.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2012041000738Floorbeam · corrodedAFT CABIN FLOORBEAM FRAME 66 Y765 CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012041000737Floor Support · corrodedAFT CABIN FRAME 66 TO FRAME 68, Y1292 FLOOR SUPPORT HAS CORROSION IN 3 AREAS. R & R FLOOR SUPPORT IAW SRM 51-42-11, PARA 5.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2012041000734Floorbeam · corrodedAFT CABIN FRAME 66 TO FRAME 68, Y1292 FLOORBEAM HAS CORROSION IN 3 AREAS. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012041000736Floorbeam · corrodedAFT CABIN FRAME 68, Y-1292 FLOORBEAM HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012041000735Tray · crackedSHEAR PLATE TRAY AT FRAME 68 TO FRAME 69. STRINGER 23 RT TO STRINGER 24, RT IS CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51 -42-11, PARAGRAPH 5, 6, 7 AND 13.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA201204100734Plate · crackedC-CHECK, SHEAR PLATE TRAY AT FRAME 68 TO FRAME 69, S23-24L CRACKED. R & R SHEAR PLATE TRAY IAW SRM 51-42-11 PARAGRAPH 5, 6, 7 AND 13.Apr 6, 2012 · N803FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR ANCF2012031300115Sdac · damagedDURING TAKEOFF ROLL CONFIG PARK ON WAS PRESENTED ON ECAM WITH PARK BRAKE IN OFF POSITION. TAKEOFF WAS ABORTED A SECOND ATTEMPT WAS PERFORMED AND CONTINOUS REPETITIVE CHIME WAS HEARD WITHOUT ANY ECAM ANNUNCIATION, TAKEOFF WAS ABORTED ONCE AGAIN. IN ACCORDANCEMar 22, 2012 · N591EL · Airbus A318111 · Central WarningSDR F3LA2012003200723Battery Pack · failedEMERGENCY LIGHTS CAPACITY TEST, FAILED TEST FOR EPSU (1 OWL) FWD LEFT. R & R EPSU BATTERY 1 OWL AMM 33-5 1-38-000-002-A, AMM 33-5 1-38-400-002-A, OPS CHECK GOOD REF AMM 33-51-38-71 0-052.Mar 20, 2012 · N802FR · Airbus A318111 · Emergency LightingSDR F3LA2012003200722Shear Plate · corrodedFUSELAGE FRAME 68 TO FRAME 70 LT SIDE LATERAL SHEAR PLATE HAS CORROSION. R & R SHEAR PLATE REF EO AO-53EO-3 1434.Mar 9, 2012 · N802FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2012003200727Sill · corrodedFLOORBEAM FRAME 68, LT SIDE DOOR SILL BEAM HAS CORROSION AROUND FASTENER HOLES. REPAIRED DOOR SILL BEAM IAW SRM 53-41-14 AND SRM 53-41 -42, FIG 201, SHEET 1.Mar 9, 2012 · N802FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2012003200726Floorbeam · corrodedFLOORBEAM FRAME 68, Y1292 HAS CORROSION AROUND FASTENER HOLES. R & R FLOORBEAM IAW SRM SL-42-11, PAR 5.Mar 9, 2012 · N802FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012003200725Floorbeam · corrodedFLOORBEAM FRAME 68, V-765 HAS CORROSION IN 2 AREAS. R & R FLOORBEAM IAW SRM 51 -42-11, PAR 5.Mar 9, 2012 · N802FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012003200724Floorbeam · corrodedFLOORBEAM AT FRAME 68, Y-1292 HAS CORROSION AROUND FASTENER HOLES IN 2 AREAS. R & R FLOORBEAM IAW SRM 51-42-11, PAR 5.Mar 9, 2012 · N802FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012003080720Shear Plate · crackedC-CHECK: FUSELAGE LT SIDE AT FRAME 68, STRINGER 23, LEFT LATERAL SHEAR PLATE CRACKED. R & R PLATE IAW SRM 51-42-11, PAR 6.B.Mar 5, 2012 · N801FR · Airbus A318111 · Fuselage Miscellaneous StructureSDR F3LA2012003070719Floorbeam · corrodedC-CHECK: MAIN CABIN FRAME 68 FLOOR PANEL FASTENER HOLES BETWEEN V1292, FLOORBEAM HAS CORROSION. BLENDED OUT CORROSION IAW SRM 51-73-00 PARAGRAPH 5. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-14, FIGURE 101, SHEET 1.Mar 5, 2012 · N801FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012003060717Floorbeam · corrodedC-CHECK: MAIN CABIN FLOORBEAM HAS CORROSION AROUND FASTENER HOLES FRAME 66 TO FRAME 68, -Y765. R & R FLOORBEAM IAW SRM 51-42-11, PARAGRAPH 5.Mar 5, 2012 · N801FR · Airbus A318111 · Fuselage Main, Floor BeamSDR F3LA2012003060716Frame Splice · corrodedC-CHECK: AFT GALLEY AREA FRAME 70, -Y1292 SPLICE PLATE (SHEAR PLATE) HAS CORROSION. R & R AFT GALLEY SHEAR PLATE IAW SRM 51-42-11, PARAGRAPH 17-18 AND EO AO-53EO-31 434, KIT PIN F9-531207DOL R02.Mar 5, 2012 · N801FR · Airbus A318111 · Fuselage Main, FrameSDR F3LA2012022800712Battery · failedBATTIERY 10 WL FAILED CAPACITY TEST IAW CARD A332204-02. REPLACED EPSU BATTERY 10 WL IAW AMM33-51-38-400-002-A.Feb 23, 2012 · N801FR · Airbus A318111 · Emergency LightingSDR F3LA2012021400709Control Cable · frozenDISCREPANCY DURING PRE FLIGHT INSPECTION, R2 CABIN DOOR WILL NOT ARM. FOUND EXCESSIVE WATER AND ICE IN GIRT BAR FLEX CABLE. CLEANED AND LUBED R2 DOOR GIRT BAR CABLE. OP'S AND RIG CHECKED NORMAL.Feb 11, 2012 · N802FR · Airbus A318111 · Passenger/Crew DoorsSDR F3LA2012021400706Girt Bar · dirtyR2 DOOR ESCAPE SLIDE WILL NOT ARM. CLEANED AND LUBED GIRT BAR FITTINGS. PERFORMED TEST OF EMERGENCY ESCAPE SLIDE RELEASE MECHANISM IAW AMM SUPPLEMENT 52-73-00-710-050-A. OPS CHECKED GOOD.Feb 10, 2012 · N802FR · Airbus A318111 · Emergency EquipmentSDR F3LA2012020700705Engine · making metalABORTED TAKEOFF. UNUSUAL VIBRATION NOTED ON START OF NR 2 ENGINE DURING TAXI. NO ECAMS NOTED. ON APPLICATION OF TAKE OFF THRUST, A LOUD COMPRESSOR STALL, FLAMES NOTED BY TOWER FROM ENGINE REAR. ECAM FOR NR 2 OIL FILTER CLOGGED. IMMEDIATELY SECURED NR 2 ENFeb 2, 2012 · N801FR · Airbus A318111 · Engine (Turbine/Turboprop)SDR ANCF2012013000111Computer · faultyREJECTED TAKE OFF DUE TO AILERON SERVO FAULT, IAW AMM 27-93-24-000/400-001A THE ELAC 2 WAS REPLACED TEST ON GROUND SATISFACTORY IAW AMM 27-93-00-710-001-A AND 22-97-710-001-A.Jan 30, 2012 · N591EL · Airbus A318111 · Flight Control SystemSDR ANCF2012012600110Apu · failedDURING TRANSIT CHECK STRONG ODOR DETECTED IN CABIN, VENTILATED IAW AMM 21-00-00-615-001 DECONTAMINATION OF THE ECS WAS PERFORMED. APU TOTALLY INOPERATIVE, PNEUMATIC AND ELECTRIC SYS. APU REPLACED IAW AMM 49-00-00-710-010A. OPS TEST OF THE APU SUCCESSFUL.Jan 26, 2012 · N598EL · Airbus A318111 · APU Bleed Air SystemSDR ANCF2012012300108Warning System · false activationGEN 1 FAULT DURING TAKEOFF ROLL, TAKEOFF THRUST WAS APPLIED AND THE FAULT CAME ON AT ABOUT 60-70 KTS, REJECTED TAKEOFF WAS DONE. IN ACCORDANCE WITH AMM 24-21-00 PB 601 INTEGRATED DRIVE GENERATOR SYSTEM CHECK WAS PERFORMED OK. IN ACCORDANCE WITH AMM 32-40-00 Jan 23, 2012 · N591EL · Airbus A318111 · AC Generator-AlternatorSDR ANCF2012011800107Apu · damagedBLEED AIR ON MAINTENANCE STATUS PAGE BUN OIL SMELL IN COCKPIT DURING FLIGHT,CHECK APU OIL LEAKS IAW 49-90-00 P830 APU TROUBLESHOOTING WAS PERFORMED FOUND OIL LEAK ITEM DEFERRED TO N°17 MEL 49-10-01 CAT C. DURING CHECK APU FOR LEAKS WERE FOUND EVIDENCE OF LEAKJan 18, 2012 · N598EL · Airbus A318111 · APU Core EngineSDR ANCF2012010800105Slide · deployedTHE ESCAPE SLIDE PACK-ASSEMBLY WAS DEPLOYMENT.Jan 8, 2012 · N590EL · Airbus A318111 · Escape SlideSDR ANCF2011123000101Warning System · activatedDURING FLY WHEEL N/W STEERING FAULT.Dec 30, 2011 · N597EL · Airbus A318111 · Landing Gear Steering SystemSDR MU1Z2011020200007Radome · damagedDURING DESCENT STRONG HIT WAS FELT IN THE RADOME ZONE, WITH VISUAL CONFIRMATION OF BIRD STRIKE AFTER PARKING (RADOME BROKEN) THE MEASURES OF THE DAMAGE ARE THE FOLLOWING: LENGTH: 190 MM, WIDE: 130 MM, DEPTH: 5 MM. DENT DAMAGE (BIRD STRIKE) IN THE BULKHEAD ARDec 10, 2011 · N591EL · Airbus A318111 · Aerodynamic FairingsSDR ANCF2011112900106Slide · partial deployDOOR 1L SLIDE FELL OUT (OR PARTIALLY DEPLOYED) AFTER DOOR WAS OPENED. IN ACCORDANCE WITH AIRBUS TASKS 25-62-44-000-002 & 25-62-44-400-006 THE ESCAPE SLIDE PACK-ASSY WAS REMOVED AND REPLACED. IN ACCORDANCE WITH AIRBUS TASK N° 52-10-00-610-001 THE REPLACEMENT Nov 29, 2011 · N589AV · Airbus A318111 · Escape SlideSDR ANCF2011112900096Oven · defectiveAFT GALLEY OVEN 511 PRODUCE BLACK SMOKE WITH SMELLS LIKE BURNT ELECTRICAL INSULATION.Nov 29, 2011 · N589AV · Airbus A318111 · Buffet/GalleysSDR F3LA2011110400687Megaphone · inoperativeDURING A-CHECK MX, THE AFT MEGAPHONE BATTERY NEEDED TO BE REPLACED IAW A-CHECK CARD (TIME) AFTER BATTERY REPLACEMENT MEGAPHONE FAILED THE REQUIRED OPERATION TEST. REPLACED THE AFT MEGAPHONE OP'S CHECKED GOOD REF AMM 25-65-51, PB 201.Nov 4, 2011 · N805FR · Airbus A318111 · Emergency EquipmentSDR ANCF2011052900092Cabin Pressure · malfunctionedAFTER T/O, VENT AVIONICS SYS FAULT WAS PRESET, ECAM ACTIONS WERE ACCOMPLISHED AND RESULTS WERE UNSUCCESSFUL, ACFT DID NOT PRESSURIZE. IAW AMM-21-26-00-040-004. DEACTIVATION OF THE SKIN AIR INLET VALVE WAS VERIFIED AND WAS FOUND CORRECT.Nov 1, 2011 · N598EL · Airbus A318111 · Air Distribution SystemSDR ANCF2011108900097Flap · malfunctionedDURING APPROACH WHEN SETTING FLAPS AT POSITION 2 F/CTL: FLAPS LOCKED - AUGMENT FAULT ON ECAM.Oct 8, 2011 · N595EL · Airbus A318111 · Trailing Edge Flap Control SystemSDR ANCF2011052900086Wheel · vibrationDURING TAKEOFF LIGHT VIBRATION WAS FELT AFTER AIRBORNE ECAM WARNING OF NAV ADR DISAGREE PLUS FLT CONTROLS ALTN LAW, ECAM ACTION WERE PERFORMED. IN ACCORDANCE WITH AMM 32-41-12-401 THE NOSE WHEEL RT AND LT WERE REPLACED TIRE PRESS 196 PSI. IN ACCORDANCE WITH Aug 27, 2011 · N589AV · Airbus A318111 · Wheel/Ski/FloatSDR F3LA2011080900665Battery Pack · failedESPU LLWL (13WL) FAILED SYS TEST IAW A-CHECK CARD A332201-03. REPLACED BATTERY PACK ON ESPU LLWL(13WL) IAW AMM 33-51-38, PB 401.Aug 5, 2011 · N803FR · Airbus A318111 · Emergency LightingSDR ANCF2011052900083Thermostat · damagedAT CRUISE AIR ENG 2 BLEED FAULT. RIGHT FAN AIR VALVE CONTROL THERMOSTAT WAS REPLACED IAW AMM 36-11-43-000-001/ 400-001.Jul 26, 2011 · N589AV · Airbus A318111 · Pneumatic Distribution SystemSDR EE4Y20110427Skin · dentedLEFT AFT DOOR SKIN WITH DENT, OUT OF THE A318 SRM ALLOWABLE LIMITS.Jun 20, 2011 · N598EL · Airbus A318111 · Passenger/Crew DoorsSDR ANCF2011052900079A/C Pack · failedPILOT REPORTED AFTER SELECTING BLEED ON THERE WAS SMOKE IN THE COCKPIT WITH APU BLEED AND EXTERNAL BLEED ALSO. PACK NR 1 HAVE A FAILURE THIS ITEM IS TRANSFERED TO DMI MEL 15, MEL 21-52-01, CAT C, PACK 1 INOPERATIVE.May 29, 2011 · N595EL · Airbus A318111 · Cabin Cooling SystemSDR F3LA2011051800641Battery · failedACFT LP 598021 I2M: EPSU TEST FAILED 11WL BATTERY. R & R EPSU BATTERY FOR 11WL IAW A318 AMM 33-51-38-000-002 AND 33-51-38-400-002. TEST OK.May 13, 2011 · N803FR · Airbus A318111 · Emergency LightingSDR F3LA2011032100618Windshield · crackedF/O FRONT WINDSHIELD CRACKED, ANTI-ICE RT WINDSHIELD ECAM. R & R THE F/O FRONT WINDSHIELD IAW AMM 56-11-11-400-000-001.Mar 17, 2011 · N803FR · Airbus A318111 · Flight Compartment WindowsSDR F3LA2011022100605Engine · overtempAIR TURN BACK DUE TO BIRDSTRIKE ON NR 1 ENGINE. ENGINE SHUTDOWN, INVESTIGATION FOR ENGINE SHUTDOWN SHOWS THE EGT WAS EXCEEDED AT 1015 DEGREES CELCIUS FOR 21 SECONDS. PERFORMED AN AIRFRAME AND ENG NR 1 BIRDSTRIKE INSP. REF TASK CARDS MP05510-02 AND MP72400-0Feb 16, 2011 · N803FR · Airbus A318111 · Engine (Turbine/Turboprop)SDR EE4Y20110099Skin · dentedLOWER FUSELAGE FR24-FR25, STR 11LT DENT ON STRINGER EVALUATION.Feb 9, 2011 · N592EL · Airbus A318111 · Fuselage Main, Plate/SkinSDR EE4Y20110088Skin · dentedHORIZONTAL STABILIZER LT AND RT LOWER SKIN WITH DENTS.Feb 4, 2011 · N592EL · Airbus A318111 · Horizontal Stabilizer, Plate/Skin
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