N438UA

Service difficulty reports · 127

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 = 'N438UA' 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 CALA2026102220530Plate · corrodedAFT CARGO BAY, AFT LAV EXHAUST VENT BETWEEN FR 69 & FR 70, STR 30R - 33R HAD CORROSION ON LOWER, INBD SIDE AT CONTACT POINT OF VENT OUTLET & AIRFRAME. R & R THE PLATE, FR 69-70 S30-33R IAW SRM 53-41-00-210 -030-C1, SRM 53-41-11-283-065, & SRM 51-72-11-911-001Oct 20, 2026 · N438UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2026102220520Sign · missingMAIN CABIN EMERGENCY EXIT IDENTIFIERS AT THE LT & RT OVERWING HATCH (4EA, FWD AND AFT) ARE NOT INSTALLED. INSTALLED MAIN CABIN EMERGENCY EXIT IDENTIFIERS AT THE LT & RT OVERWING HATCHES FWD AND AFT IAW AMM 33-51-13-400-001-A OPS CHECK GOOD IAW AMM 33-51-13-4Oct 20, 2026 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2026092119596Transceiver · faultedELECTRICAL BURNING ODOR AFTER LANDINGPICTURE UPDATE. BRIEFED FLIGHT CREW. CREW STATED A BURNING ODOR WAS PRESENT IN FLIGHT DECK, AND WAS NOTIEABLE UPON ENTERING THE COCKPIT. CAPT ALSO REPORTED HEARING A CRACKLING/POPPING NOISE NEAR THE LT INSTRUMENT PANEL. VSep 17, 2026 · N438UA · Airbus A320232 · Weather Radar SystemSDR CALA2026081918736Battery · faultedEPSU EMERGENCY LEFT BATTERY MESSAGE DISPLAYED ON EMERGENCY BATTERY TEST REPLACED EPSU BATTERY IAW AMM 33-51-38.Aug 18, 2026 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2026033014900Hydraulic Line · brokenIN FLIGHT ECAMG SYS LO PRESSUREG RSVR LO LVLG ENG1 PUMP LO PR LOCKING LOG CAPT STATED THEY FOLOWED PROCEDURES AFTER ECAM WARNING. PUMP RAN APROX 2MIN AFTER ECAM WARNING FOR G HYD LOW PRESS AS THEY FOLLOWED CHECKLIST. HYD FLUID COMING FROM ENG 1 PYLON. ZONE CMar 27, 2026 · N438UA · Airbus A320232 · Hydraulic System, MainSDR CALA2026012913428Seal · damagedSOUNDED LIKE ELECTRICAL ARCING & STATIC SIZZLING. SPOKE WITH FLT CREW. FLIGHT CREW CONFIRMED THE INITIAL POPPING SOUND FOLLOWED SIZZLING SOUND THROUGHOUT THE ENTIRE FLIGHT AS RECORDED BY CAPTAIN. UPON INSPECTION OF CAPTAINS SIDE, FIXED WINDOW, ON EXTERIOR, FOUJan 26, 2026 · N438UA · Airbus A320232 · Windshield/Door Rain/Ice RemovalSDR CALA2025102410479Battery Pack · failedCABIN EMERGENCY LIGHTING CARD 18-3351-1-0003 IS FAILING FOR EPSU BATTERY EMERGENCY LIGHT. IAW MM 33-51-38, REMOVED AND REPLACED BATTERY OF 11WL & 13WL EPSU'S OPS CK'D GOOD.Oct 22, 2025 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2025090208387Skin · dentedUPPER FUSELAGE DENT APROX .5" FWD OF FR 12 & 1" ABOVE STGR 1L. PERFORMED A DOUBLER REPAIR TO EXTERNAL SKIN AT LOCATION OF DAMAGE FR12 STRG 1L IAW SRM 53-11-11-300-054. THIS IS A CATEGORY B REPAIR.Aug 22, 2025 · N438UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2025081107522Lavatory · odorAFT LAV D GIVING VERYROUGH SMELL. NO WASTE VISIBLE. STARTED SMELLING AFTER TAKEOFF, NOTIFY LAV SERVICE TO DUMP AND RESERVICE LAV SYS, NO WATER OR WASTE LEAKS NOTED, NO FOUL ODORS NOTED AT AFT LAV D.Aug 7, 2025 · N438UA · Airbus A320232 · LavatoriesSDR CALA2025061205488Proximity Sensor · dirtyDOOR 2L SHOWS ARMED ONECAM. BUT F/A SAYS DOORSHOWING DISARMED. CLEANED ARM/UNARMED PROX SENSOR, NO HELP REMOVED AND REPLACED ARMED/UNARMED PROX SENSOR DOOR 2L REF AMM 52-71-11, AJUSTED AND OPS CHECK GOOD PER AMM 52-71-00 VERIFIED REPLACEMENT OF #2 L DOOR PROX Jun 8, 2025 · N438UA · Airbus A320232 · Door Warning SystemSDR CALA2025041603894Slide · no discrepancyRIGHT HAND OFF-WING ESCAPE SLIDE, REMOVE {A3NB-25-3-6280} - PERFORMED INSTALLATION OF THE LOCK PIN ASSEMBLY IN THE INFLATION RESERVOIR OF THE RH OFFWING/EMERGENCY-EXIT-DOOR ESCAPE-SLIDE SYSTEMS IAW AMM TASK 25-62-00-481-001-A PERFORMED REMOVAL OF THE LOCK PIN Apr 13, 2025 · N438UA · Airbus A320232 · Escape SlideSDR CALA2025021702348Lanyard · missingPURSER REPORTS R WINGEMERGENCY EXITS HAVEONE ESCAPE ROPE WHENIT SHOULD BE TWO. REPLACED MISSING RH OVERWING EMERGENCY EXIT LIFELINE ESCAPE ROPE AS REQUIRED.PARTS USED: 31-2565-3-0002,QTY :1Feb 14, 2025 · N438UA · Airbus A320232 · Emergency EquipmentSDR CALA2025013002127Battery · no testOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - FAULT 'EPSU BATTERY EMER R' SHOWING. REPLACED EMERGENCY POWER SUPPLY BATTERY REF. AMM 33-51-00. OPS CHECKS GOOD.Jan 28, 2025 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2025013002125Power Supply · no testOPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - FAULT 'EPSU INT LOAD AFT L' SHOWING. TEST AT LEFT AFT EPSU GETS NO RESPONSE. REPLACED POWER SUPPLY ASSEMBLY REF. AMM 33-51-00. OPS CHECKS GOOD.PARTS USED: 31-3350-9-9001,QTY :1 ROTABLE PARTS CHANGJan 28, 2025 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2024041201043Lamp · missingPDA 2 CREW REPORTED LEFT (RETRACTABLE) LANDING LIGHT WAS FOUND MISSING ON LOGPAGE 7620746, REF GMM 02-30-95,Apr 11, 2024 · N438UA · Airbus A320232 · Exterior LightingSDR CALA2023120103515Battery · no testEPSU BATTERY (13WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT EMP 5H0332 & INSP BY LHT EMP 5P0052 AS RECORDED ON LTPR NR#5001274773-0040. PERFORMED EPSU BATTERY REPLACEMENT (13WL) IAW AMM: Nov 29, 2023 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2023120103513Battery · no testEPSU BATTERY (12WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT AS RECORDED ON LTPR NR#5001274773-0030. PERFORMED EPSU BATTERY REPLACEMENT (12WL) IAW AMM: 33-51-38-000- 002 / 33-51-38-400-00Nov 29, 2023 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2023120103511Battery · no testEPSU BATTERY (11WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT EMP 5H0332 & INSP BY LHT EMP 5P0052 AS RECORDED ON LTPR NR#5001274773-0020. PERFORMED EPSU BATTERY REPLACEMENT (11WL) IAW AMM: Nov 29, 2023 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2023120103509Battery · no testEPSU BATTERY (10WL) FAILED EMERGENCY LIGHTNING CAPACITY TEST. REPLACEMENT REQUIRED IAW AMM: 33-51-38/401 REV 122. WORK ACCOMP BY LHT EMP 5H0332 & INSP BY LHT EMP 5P0052 AS RECORDED ON LTPR NR#5001274773-0010. PERFORMED EPSU BATTERY REPLACEMENT (10WL) IAW AMM: Nov 29, 2023 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2023061901944Manifold · unknownY SYS LO PR MANIFOLD. FOUND YELLOW SYS PTU MANIFOLD PTU SUPPLY CHECK VALVE NUT/SEAL PARTS ADDED FOUND EXTRUDED O-RING ON MANIFOLD CHECK VALVE. DISCONNECTED PTU REUPLOAD PICTURE LEAKING OR MANIFOLD CRACKED AT THE MATING SURFACE, SEE IMAGE QUICK-DISCONNECT LINE Jun 16, 2023 · N438UA · Airbus A320232 · Hydraulic System, MainSDR CALA2023052401606Battery · no testLH EPSU BATTERY FAILD OPS CHECK PER STS N0292 REMOVED AND REPLACED 13WL EPSU BATTERY PER A320 AMM 33-51-38-000 -002-A/33-51-38-400-002-A. PERFORMED OP CHECK PER A320 AMM SUBTA SK 33-51-00-710-050-A. TESK OK. PER STS N0292May 23, 2023 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2023051501502Battery · no testFWD LEFT EPSU BATTERY FAILED TEST REQUIRES REPLACEMENT UPDATE INFO TO INCLUDE STS NR281 REMOVED AND REPLACED FWD LEFT EPSU BATTERY PER A320 AMM 33-51-38 -000/400-002-A. OPS CHECK GOOD AT THIS TIMEMay 13, 2023 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2023051201476Wire · brokenCEILING CABIN EMERGENCY LIGHT INOP. FIN 205WL REFERENCE STS NR N0248 REPAIRED BROKEN WIRE IAW ESPM 20-48-11 PR EFORMED OPS IAW AMM 33-51-00-710-805 TEST OK STS QC 0047May 11, 2023 · N438UA · Airbus A320232 · Light System WiringSDR CALA2022081902128Fitting · crackedCRACK INDICATION ON CONTINUITY FITTING RH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX. SEE AEROMAN NON ROUTINE 2022-293704 01 CRACK INDICATION NOT FOUND DIP REPETITIVE INSPECTION REPAIR IS CATEGORY B. REQUIRED AFTER 57,000 TOTAL FLIGHT CICLES BUT BEFORE 58,000 TOTAug 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022081902127Fitting · crackedCRACK INDICATION ON CONTINUITY FITTING LH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX. SEE AEROMAN NON ROUTINE 2022-293703 01 CRACK INDICATION NOT FOUND DIP REPETITIVE INSPECTION REPAIR IS CATEGORY B. REQUIRED AFTER 57,000 TOTAL FLIGHT CICLES BUT BEFORE 58,000 TOTAug 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022081902126Frame · crackedCRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING LH SID E CRACK LENGTH 0.080 INCHES APPROX. CICLES FOR EC 5311-02858 PART 2 INSPECTION REQUIREMENTS I.A.W EC/RA #5311-02858 PART 1 STEP 7. THIS REPAIR IS CATEGORY "B". SEE AEROMAN NON ROUTINE 2022-293701Aug 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022081902125Frame · crackedCRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING RH SID E. CRACK LENGTH 0.100 INCHES APPROX.SEE AEROMAN NON ROUTINE 2022 -293702 CICLES FOR EC 5311-02858 PART 2 INSPECTION REQUIREMENTS I.A.W EC/RA #5311-02858 PART 1 STEP 7. THIS REPAIR IS CATEGORY "B"Aug 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022081602077Fitting · crackedCRACK INDICATION ON CONTINUITY FITTING RH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX.THIS PERFORMED PERMANET REPAIR (REPLACED)CONTINUITY FITTING RH SIDE. ROTO TEST INSPECTION OF THE CONTINUITY FITTINGS TO SPLICE FITTINGS 3 FASTENER HOLES.Aug 16, 2022 · N438UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022081602076Fitting · crackedCRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING RH SIDE. CRACK LENGTH 0.100 INCHES APPROX. PERFORMED PERMANENT REPAIR (REPLACED) WINDSHIELD CENTRAL RH SIDE.Aug 16, 2022 · N438UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022081602075Fitting · crackedCRACK INDICATION ON WINDSHIELD CENTRAL LOWER NODE FITTING LH SIDE CRACK LENGTH 0.080 INCHES APPROX. PERFORMED PERMANENT REPAIR (REPLACED) WINDSHIELD CENTRAL LH SIDE.Aug 16, 2022 · N438UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022081602074Fitting · crackedCRACK INDICATION ON CONTINUITY FITTING LH SIDE. CRACK LENGTH 0.2 00 INCHES APPROX.PERFORMED PERMANENT REPAIR (REPLACED)CONTINUITY FITTING LH SIDE.Aug 16, 2022 · N438UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022081202037Frame · corrodedCORROSION LOWER SILL FR 66 RH SIDE AT AFT GALLEY AREA, SEE AEROMAN NON ROUTINE 2022-293845 PERFORMED PERMANENT REPAIR ON LOWER SILL RH SIDE AT AFT GALLEY L=2.755IN, W=1.984IN, D=0.087IN, EDDY CURRENT DONE ON REWORKED ULTRASONIC THICKSNESS MEASURES ON REWORKED Aug 10, 2022 · N438UA · Airbus A320232 · Fuselage, Wing Attach FittingsSDR CALA2022071801799Floorbeam · corrodedCORROSION FLOORBEAM +Y1162 LOCATED BTW FR 68 AND FR 69 AT AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM +Y1162 LOCATED BTW FR.68 AND ADDITIONAL DAMAGE ON AREA IAW NTM 51-90-00 FR.69 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472000 TOOL USED CALIPJul 17, 2022 · N438UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022071801798Floorbeam · corrodedCORROSION FLOORBEAM +Y160 LOCATED BTW FRAME 68 TO FRAME 70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM +Y160 LOCATED BTW FRAME 68 TO INSPECTION AND FOUND ADDTIONAL DAMAGE IAW NTM 51-90-00 FRAME 70 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG 53472040Jul 17, 2022 · N438UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022071801797Floorbeam · corrodedCORROSION FLOORBEAM -Y765 LOCATED BTW FR 67 AND FR 70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOOR BEAM -Y765 LOC. BTW FR 67 AND FR S/N 604311, DUE DATE JUL-30-2022. 70 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472040 TOOL USED DIGITAL CALIPER: P/N Jul 17, 2022 · N438UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022071801796Floorbeam · corrodedCORROSION FLOORBEAM +Y765 LOCATED BTW FR 67 AND FR 70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM +Y765 LOC. BTW FR.67 AND FR.70 ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE IAW NTM 51-90-00 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472040, TOOJul 17, 2022 · N438UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022071801795Floorbeam · corrodedCORROSION FLOORBEAM +Y512 LOCATED BTW FRAME 64 TO FRAME 70 AT AFT GALLER AREA REMOVED AND REPLACED FLOORBEAM TY512 LOC BTW FR 64 TO FR 70 AREA AND NO FOUND ADDTIONAL DAMAGE IAW NTM 51-90-00 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG 53472094000 TOOL USEJul 17, 2022 · N438UA · Airbus A320232 · Fuselage Floor PanelSDR CALA2022071801794Floorbeam · corrodedCORROSION FLOORBEAM -Y765 LOCATED BTW FR 64 AND FR 66 AT AFT GALLEY AREA REMOVED AND REPLACED FLOOR BEAM -Y765 LOC BTW FR64 AND FR66 AT AFT GALLEY AREA IAW A320 SRM 51-42-11 AND DWG D92495124 AND D53472201 AND PERFORMED DETAIL VISUAL INSPECTION ON AREA AND NOTJul 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022071801793Floorbeam · elongatedELONGATED HOLE FLOORBEAM -Y1292 LOCATED BTW FRAME 64 AND FRAME 66 AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM -Y1292 LOCATED BTW FRAM 64 AND FRAME 66 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472201 PERFORMED DETAIL VISUAL INSPECTION ON ADJACENJul 17, 2022 · N438UA · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2022071301723None · gougedGOUGE EXTERNAL SKIN LOCATED FRAME25 AND 3 INCHES BTW STR42L TO STR 43L AT LOWER FUSELAGE 60000 FC, 120000 F/H IAW SRI 53-21-11-205-071 TABLE 001 PERFORMED SCEPTRE AND LOGPAGE NUMBER IS N.9030382 INSTALLED DOT IAW GMM 06-35-05 UPDATE LOG PAGE MAJOR REPAIR IS "YJul 13, 2022 · N438UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2020062001020Power Supply · no testEMERGENCY EXIT LIGHT TEST FAILED, EPSU AT LT AFT POSITION. TRIED TESTING AT ESPU NO REPONSE. REPLACED ESPU REF AMM 33-51-38-000-001-A & 33-51-38-400-001-A OPS CHECKED OK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1103732 SN OFF 8072 POWER SUPPLY, C OFF 31Jun 19, 2020 · N438UA · Airbus A320232 · Emergency LightingSDR CALA2020012300203Web · crackedLEFT AFT OVERWING HATCH FWD AND AFT INNER WEB WAS CRACKED AROUND VARIOUS FASTENER BUCKTAILS, REMOVED & REPLACED IAW SRM 51-72-11-911-002.Jan 18, 2020 · N438UA · Airbus A320232 · Emergency ExitsSDR CALA2020012300202Door Frame · crackedLEFT FWD EMERGENCY EXIT HATCH AFT VERTICAL FRAME WAS CRACKED AT FASTENER AREAS, REMOVED & REPLACED IAW SRM 51-72-11-911-002.Jan 18, 2020 · N438UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2020012300201Door Frame · crackedLEFT FWD EMERGENCY EXIT HATCH FWD VERTICAL FRAME WAS CRACKED AT FASTENE R AREAS, REMOVED & REPLACED THE VERTICAL SEGMENT IAW SRM 51-72-11-911-002.Jan 18, 2020 · N438UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2020012300200Web · crackedRH FWD OVERWING HATCH FWD AND AFT INNER WEB IS CRACKED AROUND VA RIOUS FASTENER BUCKTAILS. REMOVED & REPLACED IAW SRM 51-72-11-911-002.Jan 18, 2020 · N438UA · Airbus A320232 · Emergency ExitsSDR CALA2020012300199Door Frame · crackedRIGHT AFT EMERGENCY EXIT DOOR FWD WEB & AFT FRAME CRACKED, REMOVED & REPLACED IAW SRM 51-72-11-910-002.Jan 18, 2020 · N438UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2020012000196Angle · corrodedRT AFT EMERG EXIT DOOR INNER SURFACE LOWER FWD ANGLE HAS CORROSION - {A3NB-05-3-6159} - GENERATED BY TECH ON N/R 9298395 AT RMVD AND RPLCD ANGLE & RIB ON RT AFT EMERGENCY EXIT DOOR IAW SRM 51-72-11-811-002-2A. PERFORMED BY MECH, INSP.Jan 17, 2020 · N438UA · Airbus A320232 · Emergency ExitsSDR CALA2020012000195Plate · corrodedAFT PIT TORSION BOX COVER SHEET HAS CORROSION UNDER TIE DOWN FIT TINGS - A3NB-25-3-6241 - GENERATED. RMVD & RPLCD AFT CARGO PIT TORSION BOX COVER SHEET IAW SRM 51-72-11-911-002 & SRM 51-42-11-801. PERFORMED BY MECH, INSP.Jan 17, 2020 · N438UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019112542048Controller · faultedSYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. CAB PR ECAM OCCURRED AFTER TO ROTATION. T/S REF TSM 21-31-00-810-806A AND FOUND #2 CPC AT FAULT (12HL). R&R REF AMM 21-31-34-400-001-A. ALL OPS CHECKS GOOD. IPC REF 21-31-08-02A ITEM 130 EFF IS CORRECT. NOTE STEP 4.ANov 20, 2019 · N438UA · Airbus A320232 · Cabin Pressure ControllerSDR CALA201906301078Hydraulic System · low pressureHYD B SYS LOW PR ECAM, TRIPPED CB, PUMP MAY HAVE OVR-HEAT. ON ARRIVAL, B ELECTRIC 50 AMP HYD PUMP CB GRID AB ON 123VU POPPED. AT THE GATE PUSHED CB IN AND OPERATED THE PUMP AND ALL FLIGHT CONTROLS FOR 60 MINUTES. ALL INDICATION OK. PUMP ITSELF WAS NOT OVERHEATJun 26, 2019 · N438UA · Airbus A320232 · Hydraulic System, Main
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