N429UA

Service difficulty reports · 118

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N429UA' AND registry_match = 'registration'
  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 CALA2025082007943Bottle · low pressureSLIDE PRESSURE 2L AND2R ARE LOW BOTH PRESSURES IN THE TOP OF GREEN BAND OK FOR SERVICE.Aug 16, 2025 · N429UA · Airbus A320232 · Escape SlideSDR CALA2025081307675Slat Valve · no discrepancy2L DOOR SLIDE IN THE RED, PRESSURE INSPECTED AFT L2 DOOR SLIDE NEEDLE IS WITHIN THE GREEN BAND, IT WAS JUST A LITTLE HARD TO AT A ANGLE BUT OK TO CONTAug 11, 2025 · N429UA · Airbus A320232 · Escape SlideSDR CALA2025070906387Hydraulic Line · leakingAFTER GEAR EXTENSION, COMPLETE LOSS OF GREEN HYD SYS RESIVOR. FOUND HYDRAULIC HOSE AT THE RIGHT MLG DOOR ACTUATOR LEAKING. FOUND LANDING GEAR DOOR EXTENSION FLEX LINE FAILED REPLACED LINE REF AMM 29-23-11. ALL OPERATIONAL AND LEAK CHECKS OKAY .Jul 7, 2025 · N429UA · Airbus A320232 · Hydraulic System, MainSDR CALA2025062705978Slide · no discrepancyDOOR L2 SLIDE PRESSURE BELOW GREEN RANGE IAW AMM 25-62-00-210-001-A. MODEL A GAUGE NEEDLE AT TOP OF GREEN BAND, 2L WAS OPEN IN HEATED ENVIRONMENT FOR CATERING.Jun 24, 2025 · N429UA · Airbus A320232 · Escape SlideSDR CALA2025061205479None · none2L SLIDE PRESSURE IN THE RED ZONE INSPECTED SLIDE GAUGE AND FOUND IT TO BE WITHIN NORMAL LIMITS. OKAY FOR CONTINUED SERVICEJun 7, 2025 · N429UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2025050704519Bottle · no discrepancySLIDE 2L SERVICE PRESSURE IN RED ZONE EVALUATE GAUGE AND CONTACT TOMC WITH FINDINGS NEEDLE IS ON THE SPLIT BETWEEN GREEN AND RED, REF AMM25-62-00-810-803-A -GAUGE MODEL A IS INSTALLED AND PRESSURE IS WITHIN LIMITS (ACCEPTABLE UP TO A NEEDLE WIDTH INTO THE RMay 5, 2025 · N429UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2025032103062Warning Light · false activationFWD CARGO DOOR OPENINDICATION X 3 ECAM.REPEATEDLY HAPPENING. LOG PAGE 4161341 HAS BEEN REOPENED. VISUALLY CHECKED FORWARD CARGO DOOR IS CLOSED AND LOCKED (REF. AMM 52-70-00-040-001-A) AND INSTALLED INOPERATIVE STICKER ADJACENT TO LOWER ECAM DISPLAY.Mar 19, 2025 · N429UA · Airbus A320232 · Door Warning SystemSDR CALA2025031802912Bottle · no discrepancySLIDE PRESSURE ON DOOR2L IS IN THE RED. REF AMM 25-62-00-210-001-A. INSPECTED SLIDE PRESSURE AND NEEDLE IS RIGHT BETWEEN GREEN AND RED BAND. ACCEPTABLE PER AMM INSPECTION REQUIREMENTS FOR MODEL A GUAGE.Mar 14, 2025 · N429UA · Airbus A320232 · Escape SlideSDR CALA2025011301874Door · openFWD CARGO DOOR UNLOCKED INDICATION ECAM UPON CLIMB THRU APPROX 20 00MSL. FOUND FWD CARGO DOOR NOT FULLY STOWED POSITION. OPS CHK FWD CARGO DOOR. VERIFIED THE FWD CARGO GREEN INDICATIONS APPEAR IN THE INSPECTION WINDOW. FLIGHT DECK INDICATION OF FWD CARGOJan 11, 2025 · N429UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2024122001590Slat System · stuckFLAP INDICATOR SHOWINGXXFLAP AND SLATS STUCK AT.5 AND 2.5 FLIGHT CREW ADVISED, SET FLAP LEVER TO POSITION 1, FLAPS AND SLATS WENT HALF WAY. SET FLAP LEVER TO POSITION 2 AND FLAP AND SLATS WENT TO POSITION 2, THEN SET FLAP LEVER TO POSITION 3, FLAPS AND SLATS WDec 18, 2024 · N429UA · Airbus A320232 · Leading Edge Slat Control SystemSDR CALA2025091008753Aoa · faultyEG HAS BEEN NOTIFIED BY THE FAA THAT THIS AIRCAFT IS REPORTING HIGHER THAN EXPECTED RVSM ALTITUDES EG IS REQUESTING TO ACCOMPLIS H (ASE) ALTIMETRY SYSTEM ERROR CHK. 1. PERFORM AIRBUS SRM 51-11 -00 SECTION 4,A AND SRM 53-00-11 SECTION 4.B SKIN WAVINESS. 2. PERFAug 23, 2024 · N429UA · Airbus A320232 · Stall Warning SystemSDR CALA2023120603574Unknown · unknownDOOR L1 SLIDE WILL NOT ARM MAIN CABIN DOOR SHOWING NOT ARMED ON ECAM WITH DOOR CLOSED AND COMPLIED WITH THE REQUIREMENTS OF MEL 2560B. DOOR VERIFIED SMOOTHLY AS 1RH DOOR ARM LEVER. ARMED. CLOSED AND ARMED. ADD FAULT: 2500 ADD FAULT: 2560 DISPATCH DESK: S32 NANov 30, 2023 · N429UA · Airbus A320232 · DoorsSDR CALA2023112203449Fitting · crackedLH MLG DOOR FWD HINGE FITTINGS, FWD HALF HAS CRACK INDICATION AT CONNECTING PLATE LOWER FASTENER. GEN BY V892444 ON NR# 9292461/ 40461 REMOVED AND REPLACED LH MLG DOOR FWD HINGE FITTING IAW AIRBUS RE PAIR INSTRUCTION R53370500F. ACMP BY V061619 INSP BY V892285Nov 19, 2023 · N429UA · Airbus A320232 · Fuselage, Door HingeSDR CALA2023112003435Hinge Fitting · crackedRH MLG DOOR FWD HINGE FITTING, BOTH FWD AND AFT HINGE HALF HAVE CRACK INDICATIONS AT CONNECTING PLATE LOWER FASTENER. REMOVED AND REPLACED RH MLG DOOR FWD HINGE FITTING IAW AIRBUS RE PAIR INSTRUCTION R53370500F.Nov 18, 2023 · N429UA · Airbus A320232 · Fuselage, Door HingeSDR CALA2023081102489Pressure Switch · faultyHYD G RSVR LO LVL.ACCOMPLISHED ECAM/QRH.MANUALLY LOWERED GEAR. DEBRIEFED CREW - ALONG WITH HYD RES LOW LEVEL LOST HYD PRESSURE ON GREEN SYSTEM. NO VISIBLE LEAKS AND HYD QTY IN GREEN SYSTEM IS HIGH. REMOVED GREEN HYDRAULIC POWER ACCUMULATOR PER AMM 29-11-42 PERAug 8, 2023 · N429UA · Airbus A320232 · Hydraulic System, MainSDR CALA2023040601059Reservoir · lowG RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN. - HYD SERVICED GREEN HYD FLUID AND HEAD PRESSURE TO SERVICABLE LIMIT REF AMM 12-12-00. NO FAULTS NOTEDApr 6, 2023 · N429UA · Airbus A320232 · Hydraulic System, MainSDR CALA2022100702742Eiu · inoperativeENG 1 FUEL VALVE FAULT ON CLIMBOUT UPDATED PICTURES UNABLE TO POWER UP FADEC 1 ON CHANNEL A OR B ALSO LOWER ECAM SWAPPED ENGINE EIU AND #1 ENGINE PARAMETERS WENT TO NORMAL AND ENGINE PAGE SHOWING BOTH A AND B IGNITION ON WITH ENGINE MASTER ABLE TO ACCESS #1 EOct 7, 2022 · N429UA · Airbus A320232 · Fuel Control/Reciprocating EnginesSDR CALA2022061001479None · leakingECAM CAUTION MESSAGE - Y ENG PUMP LO PR MESSAGE INOP - HYD REPLACED PTU MANIFOLD QUICK DISCONNECT FITTING O-RING M&E SERVICED YELLOW STSTEM HYD. 40-0595-3-1983 , LEAK CHECK OK, MOTOR ENGINE PUMP PRESSURE NORMAL , CHECK ALL DPI AT FILTERS OK REF AMM 29-00-00-28Jun 10, 2022 · N429UA · Airbus A320232 · Hydraulic Pressure IndicatorSDR CALA2021060200783Lock · inoperativeFWD CARGODOOR SHOWING OPEN LOCKED FOR POSITIVE FIX DO THE FUNCTIONAL CHECK OF FWD CARGO DOOR REF AMM 52-31-00-720-001A. UNLOCKING FOR FIX FORWARD CARGO DOOR INDICATION OPERATION CHECKED OK AFTER REPLACING DOOR LOCK PIN AND ADJUSTING LOCK PER WRITE UP 6391178(RJun 2, 2021 · N429UA · Airbus A320232 · Cargo/Baggage DoorsSDR CALA2019070801171Transceiver · malfunctionedWR R/T ERROR WHEN RADAR ON. TILT OFF 0.5 DEGBETWEEN CA AND FO REPLACED WX RADAR R/T IAW AMM 34-41-37, OP CKS GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1118613 SN OFF 3495 TRANSCEIVER, WX OFF 31-2311-9-0001 3495 ON 31-2311-9-0001 1225.Jul 8, 2019 · N429UA · Airbus A320232 · Weather Radar SystemSDR CALA2019062401054Light · inoperativeR1 DOOR ESCAPE SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE IAW A320 AMM 25-62-44- 000-802 AND 25-62-44-400-802.Jun 23, 2019 · N429UA · Airbus A320232 · Escape SlideSDR CALA2019062210988Skin · corrodedCORROSION ON STRUCTURE BETWEEN FR12-FR13, STR41L-39L AFTER REMOVAL OF SURFACE CORRISION ON SKIN THE REMAINING THICKNESS FOUND TO BE NOMINAL .079" IAW A320 SRM 53-11-11-283-001, REMOVED FABRICATED AND REPLACED STR 39L BETWEEN FR12-13 AND THE FWD GUSSET AT FR13 Jun 17, 2019 · N429UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2019062210987Pressure Panel · crackedLH AND RH SIDE PRESSURE PANELS BETWEEN FR 35 AND 36 HAVE MULTIPL E CRACKS IN FASTENER HOLES. INTERIM REPAIR ACCOMPLISHED TO LH AND RH FR 35-36 PRESSURE PANEL S PER ECRA 5331-02397 PART 1.Jun 17, 2019 · N429UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2019061400955Wire · brokenEEPL HARNES, CONNECTOR 7260VC8, CONNECTING 31, 32 , 34ABC, HAS BROKEN WIRES 6 IN. FROM SEAT CONNECTOR. REFER TO AA R N/R: 9819958. REMOVED AND REPLACED EEPL HARNESS CONNECTOR 7260VC8 IAW A-320 AM M 33-51-22-400-802-C. THRU STEP 4.(4)(E). PERFORMED OPS CHECK IAJun 14, 2019 · N429UA · Airbus A320232 · Light System WiringSDR CALA2019060700904Flap · wornL1 DOOR OUTER DOOR HANDLE FLAP WORN. REFER TO AAR N/R: 9819940. REMOVED AND REPLACED L1 DOOR OUTER HANDLE FLAP I/A/W A320 CMM 52 -11-15-400-805, AND AMM''S 52-11-21-000-001, 52-11-21-400-001. HA NDLE ADJUSTMENTS ARE GOOD. DATA TRANSCRIBED FROM PAPER DOCUMENT AJun 6, 2019 · N429UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2019060700898Door Frame · crackedEMER EXIT HATCHES R AFT INTERIOR CRACKS ON R VE RT FRAME OTBD WINDOW. REMOVED AND REPLACED R/H BEAM AND SEGMENT ON R/H AFT EMERGENCY E XIT DOOR, AND RESTORED SURFACE PROTECTION IAW A320 SRM 51-72-11- 911-001 AND ER 5100R01017 REV E.Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2019060700897Door Frame · crackedEMER EXIT HATCHES L AFT INTERI OR CRACK ON R VERT FRAME OTBD WINDOW. REMOVED AND REPLACED R/H BEAM AND SEGMENT ON L/H AFT EMERGENCY E XIT DOOR, AND RESTORED SURFACE PROTECTION IAW A320 SRM 51-72-11- 911-001 AND ER 5100R01017 REV E.Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2019060700895Door Frame · crackedEMERGENCY EXIT DOORS, L/H AFT INTERIOR CRACKS ON L/H VERT FRAMES OTBD WINDOWS. REMOVED AND REPLACED L/H BEAM AND SEGMENT ON L/H AFT EMERGENCY E XIT DOOR, RESTORED SURFACE PROTECTION IAW A320 SRM 51-72-11-911- 001 AND ER 5100R01017 REV E.Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2019060700894Door Frame · crackedEMERGENCY EXIT DOORS L/H FWD INTERIOR CRACKS ON L/H VERT FRAMES OTBD WINDOW. REMOVED AND REPLACED L/H BEAM AND SEGMENT ON L/H FWD EMERGENCY E XIT DOOR IAW A320 SRM 51-72-11-911-001. RESTORED SURFACE PROTECT ION IAW ER 5100R01017 REV E.Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2019060700893Door Frame · crackedEMER EXIT HATCHES L FWD INTERIOR CRACKS ON R VE RT FRAME OTBD WINDOW. REMOVED AND REPLACED R/H BEAM AND SEGMENT L/H FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION IAW ER 5100R01017 REV E. ADD EMP:V923083Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2019060700892Door Frame · crackedEMER EXIT HATCHES, R FWD INTERI OR CRACKS ON R VERT FRAME OTBD WINDOW. REMOVED AND REPLACED R/H BEAM AND SEGMENT R/H FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION IAW ER 5100R01017 REV E. ADD EMP:V903758Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2019060700891Door Frame · crackedEMERGENCY EXIT DOORS R/H FWD I NTERIOR CRACK ON L/H VERT. FRAMES OTBD WINDOWS. REMOVED AND REPLACED L/H BEAM AND SEGMENT R/H FWD EMERGENCY EXIT DOOR IAW A320 SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION IAW ER 5100R01017 REV E. ADD EMP:V903758Jun 5, 2019 · N429UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2019060400880Skin · corrodedCORROSION FOUND I NSIDE SKIN AT FR 20 STR 28,29 RIGHT. REPAIRED CORROSION ON SKIN AT FR20 STR 28-29 RIGHT IAW ECRA 5331 -02395. THIS A PERMANINENT REPAIR NO FURTHER ACTION REQUIRED.Jun 2, 2019 · N429UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2019053100856Actuator · failed(A3NB-52-3-6091) L-50 NO DOT--R1 DOOR DAMPER ACTUATOR FAILS DAMPING TEST REMOVED AND REPLACED R1 DOOR DAMPER CYLINDER ACTUATOR IAW MM''S 52-11-14-000-001, AND 52-11-14-400-001. CLEARANCE AND ADJUSTMENT OF PERCUSSION BELL CRANK FINGER ARE GOOD. PART TRANSACTIONMay 28, 2019 · N429UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2019053100855Actuator · failed(A3NB-52-3-6091) L-28 NO DOT- R2 DOOR DAMPER ACTUATOR FAILED DAMPING CHECK REMOVED AND REPLACED R2 DOOR DAMPER ACTUATOR CYLINDER IAW A MM''S 52-13-14-000-001, AND 52-13-14-400-001. CLEARANCES AND ADJUSTMENT OF BELL CRANK FINGER ARE GOOD. PART TRANSACTION WAS AMay 28, 2019 · N429UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2019053100854Actuator · failed(A3NB-52-3-6091) L-28 NO DOT- L2 DOOR DAMPER ACTUATOR FAILS DAMPING CHECK REMOVED AND REPLACED L2 DOOR DAMPER ACTUATOR OR CYLINDER IAW AMM 52-13-14-000-001, AND 52-13-14-400-001. CLEARANCE AND BELL CRANK FINGER ADJUSTMENT ARE GOOD. THE PART TRANSACTION WAS ACCMay 28, 2019 · N429UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2019051300768Wire Harness · damaged(SUPPORT TASK) THE EEPL HARNESS FOR SEAT ROWS 12 TO 22 IS DAMAGED. REFER TO N/R: 9819035. REMOVED AND REPLACED HARNESS FROM RACEWAY ON ROWS 12 TO 22 IAW AMM 33-51-22-000-801C1. OPS CHECK TO BE ACCOMPLISHED ON CUSTOMER CARD NR 18-3351-1-4705 SEQ 545. WORK ACCOMMay 13, 2019 · N429UA · Airbus A320232 · Light System WiringSDR CALA2019051300765Connector · damaged(SUPPORT TASK) THE EEPL HARNESS THAT CONNECTS TO 7260VC9 IS DAMAGED. REFER TO N/R: 9819037. REMOVED AND REPLACED CONNECTORS ON EEPL HARNESS 7260VC9 IAW ESPM 20-53-51 PB0201 CONFIG 01. OPS TEST TO BE ACCOMPLISHED ON CUSTOMER WORK CARD NR 18-3351-1-4705 SEQ 545.May 13, 2019 · N429UA · Airbus A320232 · Light System WiringSDR CALA2019051300763Wire Harness · damaged(SUPPORT TASK) THE EEPL HARNESS THAT CONNECTS TO 7260VC7 IS DAMAGED. REFER TO N/R: 9819036. REMOVED AND REPLACED HARNESS FROM RACEWAY THAT GOES TO 7260VC7 IAW AMM 33-51-22-000-801C1. OPS CHECK TO BE ACCOMPLISHED ON CUSTOMER CARD NR 18-3351-1-4705 SEQ 545. DATAMay 13, 2019 · N429UA · Airbus A320232 · Light System WiringSDR CALA2018120702503Oven · contaminatedACRID ELECTRICAL SMELLTHROUGHOUT CABIN AFTERTAKEOFF. RAN CHEKLI STRETURND TOAIRPORT PERFORMED SMOKE/ODOR IN CABIN INSPECTION REF AMM 05-51-10-200-801C. CREW COMPLETED SMOKE/ODOR FORM AND INFORMED M/X THAT SMELL BEGAN DURING TAKEOFF. PERFORMED IDENTIFICATION CDec 3, 2018 · N429UA · Airbus A320232 · Buffet/GalleysSDR CALA2018012600347Connector · not seatedWHILE PERFORMING EMERGENCY SYSTEM TEST, RECEIVED AN EPSU BATTERY MESSAGE. RESEATED BATTERY CONNECTOR. TESTED GOOD.Jan 26, 2018 · N429UA · Airbus A320232 · Light System WiringSDR CALA2017111004019Wire · unsecureAISLE EMERGENCY LIGHT AT SEAT 30C HAS A WIRE EXTENDING INTO THE AILSEWAY. SECURED THE WIRING. OK FOR SERVICE.Nov 10, 2017 · N429UA · Airbus A320232 · Light System WiringSDR CALA2017110303926Connector · loose30C EMERGENCY LITE CONNECTOR LOOSE REPAIRED LOOSE CONNECTOR AT SEAT 30C EMERGENCY LIGHT OPS CK NORMAL REF SWPM 20-42-01. VERIFIED REPAIR AT CONNECTOR AT SEAT 30C EMERGENCY LIGHT REF SWP M 20-42-01 AND GMM-09-10-05.Nov 3, 2017 · N429UA · Airbus A320232 · Light System WiringSDR CALA2017102303768Battery · failedLEFT AND AFT EMERGENCY LIGHT BATTERYS FAIL CAPACITY CHECK. REMOVED AND REPLACED LEFT AND AFT EMERGENCY LIGHT BATTERYS REF AMM 33-51-38 PB401 OPS CHECK OK.Oct 23, 2017 · N429UA · Airbus A320232 · Emergency LightingSDR CALA2017071402244Power Supply · faultyEEPL ON SEATS, CENTER CABIN, ARE FLICKERING,. TROUBLESHOT, FOUND EPSU 11WL & OVERWING EMER LIGHT ASSY 60WL REMOVED AND REPLACED BOTH IAW MM 33-51-15-000-001A, 33-51-15-4 00-001A, 33-51-38-000-001A, 33-51-38-400-001A SYSTEM OPS CHECK GOOD IAW MM 33-51-00-710-00Jul 14, 2017 · N429UA · Airbus A320232 · Emergency LightingSDR CALA2017081402663Skin · corrodedRIGHT FUSELAGE EXT SKIN AROUND LAVATORY E, EXHAUST HAS CORROSION. BLENDED CORROSION AROUND LAVATORY EXHAUST VENT, FOUND TO BE OUT OF LIMITS ORIGINAL .063 REMAINING .052 LOSS OF .011. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-41-11-300-004, PG 1-6, Jul 10, 2017 · N429UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2017071002123Door Sill · corrodedCABIN UNDER FLOOR STRUCTURE WITH LIGHT CORROSION AT R2 DOOR SILL BEAM UPPER FACE FRAME 69-2 INCHES AND STRINGER 23. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001, AND 51-42-11-001, REV 118.Jul 9, 2017 · N429UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2017051201381Wire Harness · looseFOUND EMERGENCY LIGHT HARNESS HANGING DOWN SEAT 38 ABC. REPLACED SEAT ROW HARNESS, SECURED HARNESS. OPS CHK GOOD FOR LIGHT ASSY.May 12, 2017 · N429UA · Airbus A320232 · Light System WiringSDR CALA2017020600292Battery · dischargedEMERGENCY LIGHTS TEST FAILED AT PTP PANEL. REPLACED BATTERY AT EPSU 10WL REF AMM 33-51-38 PB401, NOW OK FOR SERVICE.Feb 6, 2017 · N429UA · Airbus A320232 · Emergency LightingSDR CALA2015111794839Pump · leakingENGINE 2 SHUTDOWN DUE TO OIL LOSS. BEGAN AT FL340, PUT TO IDLE. AT 3 QTS ECAM, ENG SHUTDOWN. FOUND AREA AROUND OIL PUMP VERY WET. R & R ENG 2 OIL PRESS PUMP. OPERATIONS & LEAK CHECKED GOOD.Nov 13, 2015 · N429UA · Airbus A320232 · Turbine Engine Oil System
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