Airbus A319-111

Service difficulty reports · 2,475

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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 = 'A319111'
  ORDER BY difficulty_date DESC"

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SDR F3LA2016090600052Slide Raft · failedREF LOG PAGE 1001551: DURING ROUTINE HEAVY SERVICE CHECK, R-1 DOOR FAILED EMERGENCY LIGHTING TEST. R & R R-1 DOOR SLIDE REF TC25831-02. TESTED EMERGENCY LIGHT TEST IAW WORK CARD, OPS CHECK GOOD, END.Sep 4, 2016 · N919FR · Airbus A319111 · Escape SlideSDR F3LA2016062100051Engine · shutdownDURING CRUISE FLIGHT THE CREW NOTED, ECAM ENGINE 2 STALL WHICH WAS SOON FOLLOWED BY ENGINE 2 SHUTDOWN. THE CREW DECLARED EMERGENCY LANDING. MAINTENANCE R & R NR 2 ENGINE. REF WC MP71042-01 AND MP71042-02, REMOVAL AND INSTALLATION CARDS. OPS CHECK GOOD.Jun 19, 2016 · N935FR · Airbus A319111 · Engine (Turbine/Turboprop)SDR F3LA2016052000047Apu · contaminatedREFERENCE LOG PAGE 1043522, DURING CLIMB OUT, THE CREW NOTICED AN OIL FUME SMELL IN COCKPIT & CABIN. THE ACFT RETURNED. MX DISCOVERED OIL SPILL AROUND APU AIR INLET & DUCT ASSEMBLY. CLEANED AREA OF OIL & PERFORMED LEAK CHECK. RAN NR ONE & TWO PACK WITH BLEMay 19, 2016 · N920FR · Airbus A319111 · APU Core EngineSDR WX0A2016042973145Engine · failedNUMBER 2 ENG FAILED DURING GO AROUND. DISCHARGED NR 1 FIRE BOTTLE. R&R NR 2 ENGINE PER T/C 71-400-001. ALL OPS AND LEAK CHECKS GOOD.Apr 28, 2016 · N311NV · Airbus A319111 · Engine (Turbine/Turboprop)SDR WX0A2016042973141Acoustic Panel · crackedDURING DAILY CHECK WALK AROUND, DISCOVERED CRACKED ACOUSTIC PANEL AT 12 - 2 O'CLOCK POSITION ON NR 2 ENG. R & R ACOUSTIC PANEL AT 12 - 2 O'CLOCK POSITION IAW AMM 72-23-00. ALL IS GOOD.Apr 27, 2016 · N327NV · Airbus A319111 · Turbine Engine Air Inlet SectionSDR F3LA2016041900034Proximity Sensor · out of adjustREFERENCE LOG PAGE 991830. AFTER TAKEOFF THE FLIGHT CREW RECEIVED A WARNING INDICATION THE LG FAILED TO RETRACT. PERFORMED AN AIR TURN BACK & THE ACFT RETURNED TO THE FIELD. PERFORMED AN INSPECTION OF THE NLG PROXIMITY SENSORS 24GA & 25GA & FOUND THE PROXIMApr 19, 2016 · N922FR · Airbus A319111 · Landing Gear Position and WarningSDR F3LA2016040800032Floorbeam · corrodedDURING C CHECK, NOTED CORROSION AT FRAME 66 & FLOORBEAM Y1292. R & R FLOORBEAM IAW SRM 51-42-11.Apr 8, 2016 · N928FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2016040800031Plate · corrodedDURING C CHECK, NOTED CORROSION AT FRAME 66 & Y1732. PERFORMED REPAIR IAW SRM 53-41-14.Apr 8, 2016 · N928FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2016040800030Door Sill · corrodedDURING C CHECK, NOTED CORROSION ON NUTPLATE HOLE ON L2 AFT GIRT BAR FITTING. R & R L2 DOOR SILL IAW SRM 51-72-11.Apr 8, 2016 · N928FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2016040800029Fitting · corrodedDURING C CHECK, NOTED R1 DOOR AFT GIRT BAR FITTING HAS CORROSION. REPAIRED R1 DOOR GIRT BAR FITTING IAW SRM 51-73-00, SRM 51-74-00, NTM 51-10-08 & SRM 51-21-11.Apr 8, 2016 · N928FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2016040800028Floorbeam · corrodedDURING C CHECK, NOTED CORROSION, BETWEEN FRAME 64 & 67, Y254. R & R FLOORBEAM IAW SRM 51-42-11 & SRM 51-72-1.Apr 4, 2016 · N928FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2016040800027Shear Plate · corrodedDURING C CHECK, NOTED RT SHEAR PLATE, BETWEEN STRINGER 23 & 24, AT FRAME 68 - 70 HAS CORROSION. R & R SHEAR WEB & WEB SUPPORT IAW SRM 51-42-11.Apr 4, 2016 · N928FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2016040800026Fitting · corrodedDURING C CHECK, NOTED R1 DOOR AFT GIRT BAR FITTING HAS CORROSION. REPAIRED R1 DOOR AFT GIRT BAR FITTING IAW SRM 51-73-00, 51-74-00, 53-11-11, NTM 51-10-08 & SRM 51-21-11.Apr 4, 2016 · N928FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2016040800025Shear Plate · corrodedDURING C CHECK, NOTED LT AFT SHEAR PLATE, BETWEEN STRINGER 23 & 24 AT FRAME 68 & 70 HAS CORROSION. R & R LT AFT SHEAR PLATE IAW SRM 51-42-11 & SRM 51-44-11.Apr 4, 2016 · N928FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2016040800024Floorbeam · corrodedDURING C CHECK, NOTED CORROSION AT FRAME 66 & Y1292. R & R THE FLOORBEAM AT FRAME 66 & Y1292 IAW SRM 51-42-11.Mar 31, 2016 · N928FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2016032600014Engine · leakingAFTER TAKEOFF THE FLIGHT CREW RECEIVED A CARGO & LAVATORY SMOKE MSG. THE ACFT RETURNED TO THE FIELD & MX DISCOVERED OIL WETTING IN THE NR 2 ENG COMPRESSOR. MX REMOVED ENG SN 575632 & INSTALLED SERVICEABLE ENG 575640 IAW MPD TASK CARDS MP 71042-01, MP 71042-0Mar 24, 2016 · N922FR · Airbus A319111 · Engine (Turbine/Turboprop)SDR WX0A2016030173097Fan · faultyDURING CRUISE FLIGHT AT FL 340, CREW FELT A VIBRATION FOLLOWED BY A STRONG FUME SMELL IN THE FLIGHT DECK THAT DRIFTED ALL THE WAY DOWN THE CABIN. DECLARED AN EMER WITH ATC & DIVERTED. ALL QRH CHECKLISTS WERE COMPLIED WITH. CREW HAD DONNED THEIR OXYGEN MASKSFeb 29, 2016 · N327NV · Airbus A319111 · Air Distribution FanSDR WX0A2016010473060Warning System · activatedAFTER TAKEOFF FROM NLG INDICATOR DISPLAYED, UNLK, ACCOMPANIED WITH ECAM MSG, LG DOORS NOT CLOSED, & LG NOT LOCKED. THE CONDITION WAS OBVIOUS, CONFIRMED, DUE TO EXCESSIVE GEAR NOISE. PERFORMED ECAM PROCEDURE WHICH CORRECTED THE ISSUE. PERFORMED INSPECTION OFJan 1, 2016 · N326NV · Airbus A319111 · Landing Gear Position and WarningSDR F3LA2015121801155Floorbeam · corrodedAIRCRAFT DUE C 9 CHECK. MAIN CABIN FLOORBEAM HAS CORROSION 5" AFT OF FRAME 66, & 10" INBD OF Y765. CORRODED AREA FOUND TO HAVE OVER 50% MATERIAL LOSS. R & R FLOORBEAM IAW SRM 52-42-11 PARA 2 D. ACFT DUE OUT OF C CHECK 12 16 2015. REFERENCE NR 35394.Dec 16, 2015 · N908FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2015103001151Controller · defectiveFIRST OFFICERS WINDOW HEAT & WINDSHIELD HEAT ECAM. R & R WINDOW HEAT CONTROLLER 2DG2. OPERATIONAL CHECK & BITE TESTED GOOD IAW AMM 30-42-34 PB401. REFERENCE LP 949698.Oct 27, 2015 · N908FR · Airbus A319111 · Windshield/Door Rain/Ice RemovalSDR F3LA2015090401144Bottle · leakingR2 DOOR ASSIST BOTTLE EMPTY. SERVICED R2 DOOR ASSIST BOTTLE IAW AMM 52-10-00-614-001-A. REFERENCE NR 25069.Aug 23, 2015 · N933FR · Airbus A319111 · Passenger/Crew DoorsSDR F3LA2015080701143Light · inoperativeLIGHT INOPERATIVE AT LT EMER ESCAPE HATCH HANDLE. R & R EMER LIGHT 70WL1. OPERATIONS CHECKED GOOD IAW AMM 33-51-11-400-001-A. REF LOG PAGE 895364 ITEM 2.Aug 6, 2015 · N924FR · Airbus A319111 · Emergency LightingSDR F3LA2015062201137Web · crackedAIRCRAFT DUE C8 CHECK, DISCREPANCY. MAIN CABIN RT TRAY WEB IS CRACKED 4'' AFT OF FRAME 68 RT. R & R CRACKED TRAY WEB IAW SRM 51-42-11 PAR 6 7 13. ACFT DUE OUT OF C CHECK 06 23 2015.Jun 17, 2015 · N922FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2015062201139Shear Plate · crackedAIRCRAFT DUE C8 CHECK, DISCREPANCY. MAIN CABIN LT SHEAR PLATE IS CRACKED AFT OF FRAME 69. R & R CRACKED SHEAR PLATE IAW SRM 51-42-11 PAR 6 13 & EO A0-53EO-31434. ACFT DUE OUT OF C CHECK 6 23 2015.Jun 16, 2015 · N922FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2015062201138Shear Plate · crackedAIRCRAFT DUE C8 CHECK, DISCREPANCY. MAIN CABIN LT SHEAR PLATE IS CRACKED AFT OF FRAME 69. R & R CRACKED SHEAR PLATE IAW SRM 51-42-11 PAR 6 1 & EO A0-53EO-31434. ACFT DUE OUT OF C CHECK 6 23 2015.Jun 16, 2015 · N922FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2015052001135Shear Plate · crackedAIRCRAFT DUE C6 CHECK, AFT CABIN RT LATERAL SHEAR PLATE CRACKED AT FRAME 69 - 70. R & R SHEAR PLATE IAW SRM 51-42-1. ACFT DUE OUT OF C6 CHECK ON 5 25 2015.May 20, 2015 · N947FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2015052001134Shear Plate · crackedAIRCRAFT DUE C6 CHECK, AFT CABIN LT LATERAL SHEAR PLATE CRACKED FRAME 69 - 70. R & R SHEAR PLATE IAW SRM 51-42-11. ACFT DUE OUT OF C6 CHECK ON 5 25 2015.May 20, 2015 · N947FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2015051101132Fuel Line · leakingNUMBER 2 ENG FUEL LEAK FROM MAIN FUEL SUPPLY LINE. R & R MAIN FUEL SUPPLY LINE IAW AMM 73-11-11 PAGE BLOCK 401. LEAK CHECKED GOOD. TORQUE WRENCH F9TAB3949C CALIBRATION DATE 10 15, LOG PAGE 896973.May 11, 2015 · N905FR · Airbus A319111 · Engine Fuel DistributionSDR F3LA2015041501130Duct · failedDISCREPANCY, ENG 2 FIRE, AIR TURN BACK 1839 Z. ENG 2 FIRE INDICATION ON TAKEOFF AFTER THRUST REDUCTION ON ENG 2 IAW ECAM. FIRE INDICATION CHANGED TO AMBER, ENG 2 SHUTDOWN. ENG 2 SHUTDOWN COMPLETED. FOUND HIGH PRESS BLEED DUCT BROKEN CAUSING ENG 2 FIRE INDIApr 12, 2015 · N920FR · Airbus A319111 · Pneumatic Distribution SystemSDR F3LA2015041501129Hydraulic Line · chafedREFERENCE LOG PAGE 802478 ITEM NR 1. AIR TURN BACK AT 14:55 Z HYD RESERVOIR LOW LEVEL. YELLOW HYD QTY WENT TO ZERO JUST AFTER TAKEOFF. R & R HYD PRESS LINE, PN D2901005100740 & AFT CLAMP BLOCK PN D2901013500000.Apr 12, 2015 · N934FR · Airbus A319111 · Hydraulic System, MainSDR F3LA2015040601127Unknown · malfunctionedFLAP JAM AT SLAT ONLY, FLAPS LOCKED. PERFORMED BITE TEST OF SFCC IAW AMM 27-51-00-740-002-A. PERFORMED 2 FULL FLAPS & SLATS CYCLES, NO DEFECTS NOTED. PERFORMED VISUAL INSPECTION OF THE FLAPS & SLATS, NO DEFECTS NOTED LP 893710.Apr 2, 2015 · N935FR · Airbus A319111 · Trailing Edge Flap Control SystemSDR F3LA2015031601122Battery · dischargedEPSU BATTERY AFT LT 13 WL, FAILED BATTERY TEST AT SCHEDULED HEAVY SERVICE CHECK. R & R THE EPSU BATTERY AT 13WL IAW AMM 33-51-38-000-002A & 33-51-38-400-002A.Mar 16, 2015 · N919FR · Airbus A319111 · Emergency LightingSDR F3LA2015031701124Skin · debondedAIRCRAFT DUE C8 & S2 CHECK. DISCREPANCY, RT ELEVATOR THERMO GRAPHIC INSPECTION SHOWS INDICATIONS THAT ARE IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR WITH HOT BONDER IAW SRM 55-20-00, PB201, PAR 2 A & SRM 55-21-11, PB201, C1, PAR 5 D, FIG 204. Mar 13, 2015 · N921FR · Airbus A319111 · Elevator, Plate/SkinSDR F3LA2015031701123Skin · debondedAIRCRAFT DUE C8 & S2 CHECK. DISCREPANCY, LT ELEVATOR THERMO GRAPHIC INSPECTION SHOWS INDICATIONS THAT ARE IRREGULAR IN SHAPE & BLACK IN COLOR. REPAIRED LT ELEVATOR WITH HOT BONDER IAW SRM 55-20-00, PB201, PAR 2 A & SRM 55-21-11, PB201, PAR 5 E. SEE NDT REPOMar 11, 2015 · N921FR · Airbus A319111 · Elevator, Plate/SkinSDR F3LA2015031101118Battery Pack · failedEPSU EMER LIGHT BATTERY 12WL, MIDDLE RT FAILED CAPACITY TEST ON A6 CHECK. R & R EPSU BATTERY 12WL IAW AMM 33-51-38-000-002A & 33-51-38-400-002A. OPERATIONS CHECKED GOOD. OK FOR SERVICE.Mar 9, 2015 · N912FR · Airbus A319111 · Emergency LightingSDR F3LA2015030501116Light · damagedDURING A SCHEDULED HEAVY SERVICE CHECK, THE EMER PATH SEAT MOUNTED LIGHT AT SEAT ROW 22 WAS FOUND DAMAGED. R & R LIGHT ASSEMBLY IAW AMM 33-51-18 PB 401.Mar 5, 2015 · N932FR · Airbus A319111 · Emergency LightingSDR F3LA2015030501115Plate · corrodedACFT DUE C8 & S2 CHECK. DISCREPANCY, LT AFT LATERAL SHEAR PLATE HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11. ACFT DUE OUT OF C CHECK ON 3/22/2015.Mar 4, 2015 · N921FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2015030501114Plate · corrodedACFT DUE C8 & S2 CHECK. DISCREPANCY, RT AFT LATERAL SHEAR PLATE HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11. ACFT DUE OUT OF C CHECK ON 3/22/2015.Mar 4, 2015 · N921FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2015030501113Beam · corrodedACFT DUE C8 & S2 CHECK. DISCREPANCY, MAIN CABIN FLOOR & TRACK BEAM HAS CORROSION AT FRAME 19 - 20, Y1292, OUT OF LIMITS. R & R BEAM IAW SRM 51-42-11. ACFT DUE OUT OF C CHECK ON 3/22/2015.Mar 4, 2015 · N921FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2015021701106Warning System · false activationREFERENCE LOG PAGE 910707 ITEM NR 1. SMOKE LAVATORY SMOKE ECAM ON DESCENT. PERFORMED SDCU BITE TEST AS REQUIRED IAW AMM 26-15-00-410-003. PERFORMED LAVATORY SMOKE DETECTOR TEST AS REQUIRED IAW AMM 26-16-00-710-001. NO DEFECTS NOTED. FIRE DEPARTMENT PERFORFeb 14, 2015 · N933FR · Airbus A319111 · Smoke DetectionSDR F3LA2015021201105Hydraulic Line · chafedOIL LEAKING FROM NR 2 ENG PYLON AFT OF BREATHER TUBE. R & R PRESS HYD LINE IN NR 2 PYLON. LOG PAGE 913804.Feb 12, 2015 · N918FR · Airbus A319111 · Hydraulic System, MainSDR F3LA2015020401104Battery Pack · dischargedLEFT EPSU BATTERY FAILS TEST. REPLACED LT EPSU IAW AMM 33-51-38 PB 401. OPERATIONS CHECKED NORMAL. LOG PAGE 843284.Feb 3, 2015 · N935FR · Airbus A319111 · Emergency LightingSDR F3LA2014123001096Battery Pack · dischargedEPSU EMER LIGHT BATTERY 10WL, FWD LT, FAILED CAPACITY TEST AT A CHECK. R & R BATTERY ASSEMBLY IAW AMM 33-51-36-000-002A & 33-51-36-400-002A.Dec 23, 2014 · N908FR · Airbus A319111 · Emergency LightingSDR F3LA2014120301092Battery · dischargedEPSU BATTERY 13WL AFT LT FAILED CAPACITY TEST. R & R EPSU BATTERY 13WL IAW AMM 33-51-38 PB401. OPERATIONS CHECKED GOOD.Dec 3, 2014 · N906FR · Airbus A319111 · Emergency LightingSDR F3LA2014112401088Engine · malfunctionedAIRCRAFT DEPARTED & ENG 1 LOST OIL PRESS, OIL QTY WAS AT 0. CREW PERFORMED IN FLIGHT SHUTDOWN. EMER WAS DECLARED. ACFT ARRIVED WITHOUT FURTHER INCIDENT. ACFT ARRIVED WITH OIL TANK EMPTY. OIL WAS FOUND IN HOT STREAM OF EXHAUST PIPE, NO EVIDENCE OF OIL IN CNov 22, 2014 · N925FR · Airbus A319111 · Engine (Turbine/Turboprop)SDR F3LA2014111701087Shear Plate · corrodedAIRCRAFT C 9 CHECK. LT SHEAR PLATE IS CRACKED AT FRAME 69. R & R LT SHEAR PLATE SRM 57-42-11 EA A0-53T-30654.Nov 14, 2014 · N905FR · Airbus A319111 · Fuselage Miscellaneous StructureSDR F3LA2014111101086Floorbeam · corrodedAIRCRAFT DUE C 9 CHECK. MAIN CABIN FLOORBEAM HAS CORROSION AT FRAME 68, -Y1292. BLENDED DAMAGED AREA & REMOVED CORROSION. ORIGINAL THICKNESS .150 INCHES & .116 INCHES REMAINS. MAX ALLOWABLE DAMAGE DEPTH IS .016 INCHES SO BLEND OUT WAS OUT OF LIMITS. R & RNov 7, 2014 · N905FR · Airbus A319111 · Fuselage Main, Floor BeamSDR F3LA2014111001084Slide · defectiveAIRCRAFT DUE C 7 CHECK. DURING SCHEDULED OPERATIONAL CHECK OF R 2 DOOR SLIDE, LIGHTS DID NOT ILLUMINATE WHEN SLIDE DEPLOYED. R & R R2 DOOR SLIDE WITH SERVICEABLE UNIT IAW TASK CARD TC25831-03. ACFT DUE OUT OF C CHECK 11/11/2014.Nov 7, 2014 · N929FR · Airbus A319111 · Escape SlideSDR F3LA2014111001083Pipe · brokenREFERENCE LOG PAGE 868242 ITEM 1. HYD GREEN RESERVOIR LOW LEVEL. FOUND GREEN HCU PIPE BROKEN. REMOVED HCU PIPE AMM 29-11-49-000-049. INSTALLED HCU PIPE AMM 29-11-49-400-049.Nov 7, 2014 · N926FR · Airbus A319111 · Hydraulic Reservoir, MainSDR F3LA2014111101085Shear Plate · corrodedAIRCRAFT DUE C 9 CHECK. MAIN CABIN RT SHEAR PLATE IS CRACKED 3 INCHES AFT OF FRAME 69. R & R CRACKED SHEAR PLATE IAW SRM 51-42-11 PAR 6 & 13 & EO A0-53EO-31434. ACFT DUE OUT OF C CHECK 11-15-2014.Nov 6, 2014 · N905FR · Airbus A319111 · Fuselage Miscellaneous Structure
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