N488UA

Service difficulty reports · 105

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 = 'N488UA' 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 CALA2026081418631Battery · dischargedCOCKPIT EMERGENCY FLASHLIGHT HAS A DEAD BATTERY. REMOVED AND REPLACED COCKPIT EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-65-98.Aug 13, 2026 · N488UA · Airbus A320232 · Emergency EquipmentSDR CALA2026032714859Skin · contaminatedLH TOP SKIN PANEL, FOUND LIQUID ENGRESS INDICATION AT 12 INCHES FROM I/B EDGE AND 14 INCHES FROM T/E DEFECT IS 1 INCH DIA. IN SI ZE. REPAIRED L/H ELEVATOR TOP SKIN 12IN FROM I/B 14IN FROM T/E 1.38I N DIG ZONE A IAW SRM 55-21-11-300-004 CATEGORY A REPAIR.Mar 24, 2026 · N488UA · Airbus A320232 · Elevator StructureSDR CALA2026032314762Skin · damagedLEFT TOP SKIN PANEL, FOUND LIQUID ENGRESS INDICATION AT 154.5 INCH ES FROM INBD EDGE AND 9 INCHES FROM T/E. DEFECT IS 1 INCH DIA. IN SIZE. REPAIRED LT ELEVATOR TOP SKIN 154.5 IN FROM INBD 9IN FROM T/E 1. 25IN DIA ZONE A IAW SRM 55-21-11-300-004, CATEGORY A REMar 22, 2026 · N488UA · Airbus A320232 · Horizontal Stabilizer, Plate/SkinSDR CALA2026031914685Door Sill · corrodedAFT MAIN CABIN FLOOR STRUCTURE R-2 DOOR SILL CORROSION BETWEEN G IRT BAR FITTINGS. REMOVED AND REPLACED R2 DOOR SHAPE SILL (CENTER) IAW SRM 51 -42-11.Mar 16, 2026 · N488UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2026040114989Door Sill · corrodedR2 DOOR SILL AT FR68 HAS CORROSION AROUND NUTPLATE FASTENER HOLE . GENERATED BY V061680 ON AAR LCQ NR 9296398/24398 ESFR COMPLETED REPAIRED DOOR SILL AT FR68 R2 DOOR IAW A320 SRM 53-41-14-300-001 ACMP BY MECH V061742 INSP BY V077960 RII INSP C/W AAR QC LC-30Mar 12, 2026 · N488UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2026030514337Shear Panel · corrodedAFT CABIN LT SHEAR WEB AT FR 69 - FR 70 WAS CORRODED. REPLACED THE LT SHEAR WEB IAW SRM 51 -72-11, AND SRM 51-42-11.Mar 2, 2026 · N488UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2026030514335Floor Support · corrodedAFT MAIN CABIN FLOOR STRUCTURE CORRODED RT FLOOR SUPPORT, Y -1162.5 AT FR 66. REMOVED AND REPLACED RT FLOOR SUPPORT IAW SRM 51-72-11-911-001.Mar 2, 2026 · N488UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2026030314242Door Frame · crackedLEFT FWD EMERGENCY EXIT DOOR VERTICAL FRAME, FOUND SEVERAL CRACKS IAW AAR LCQ N/R 9296297/24297. REMOVED AND INSTALLED THE VERTICAL FRAME IAW SRM AND DWG 1I D522-79040.Feb 28, 2026 · N488UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025120511785Battery Pack · no testDURING THE EMERGENCY LIGHTING TEST USING PTP 110RH, RECIEVED FAULT EPSU UNIT FWD LT. REPLACED EPSU BATTERY AT L1 DOOR IAW AMM 33-51-38. OP CHECKED GOOD.Dec 3, 2025 · N488UA · Airbus A320232 · Emergency LightingSDR CALA2025091608963None · no discrepancyBIRDSTRIKE ON T/O LEFT WINDSCREEN HOT BRAKES FROM RTO 440 DEGREES. ACP BIRDSTRIKE PER AMM 05-51-14-200-803. ACP'D BIRDSTRIKE INSP OF AIRFRAME AND ENGS PER AMM 05-51-14. NO DAMAGE NOTED.Sep 12, 2025 · N488UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2025090908667Battery · no testCABIN EMER LIGHTING OPS CHK FAIL REPLACE LT EPSU BATTERY REPLACED LT EPSU IAW 33-51-38-400-002-A OPS CHK PASSED.Sep 8, 2025 · N488UA · Airbus A320232 · Emergency LightingSDR CALA2025043004341Bottle · noneDOOR 2L SLIDE PRESSURE INDICATOR SHOWING LOW PRESSURE. CHECK DOOR 2L SLIDE PRESSURE INDICATOR AT DOOR. NEEDLE IS ON THE LINE DIVIDING AREA A AND AREA B. THE NEEDLE IN AREA B, WHICH IS HALF THE RANGE OF AREA A, SHOWS A PRESSURE LEVEL THAT CAN BE ACCEPTED PERApr 28, 2025 · N488UA · Airbus A320232 · Escape SlideSDR CALA2025021902379Slide · faultyREPLACED DOOR 2 LEFT EVACUATION SLIDE ASSY PER JOB CARD 31-2561-9-0015 REPLACED DOOR L2 EVACUATION SLIDE ASSY. SER # OFF 7468. SER# ON 7104. REF AMM 25-62-44.PARTS USED: 31-2561-9-0015, QTY :1. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1565986 SN OFF 7468.SLIFeb 16, 2025 · N488UA · Airbus A320232 · Escape SlideSDR CALA2025012702057Bypass Valve · faultedLOST/CABIN TEMP CONTROL TALKED TO INBOUND FLIGHT CREW, THERE WAS NO ISSUES WITH BLEED AIR OR AIR FLOW FROM VENTS AND GASPERS. CREW UNABLE TO CONTROL TEMPERTURE WITH ZONE SELECT SWITCHES. ACCOMPLISHED TSM 21-61-00-810-905-A NO ISSUES, SEE LOG PAGE 3659407. FOUNJan 25, 2025 · N488UA · Airbus A320232 · Cabin Temperature Control SystemSDR CALA2025010301771Lanyard · out of positionDOOR 1L/INDICATOR ON FLO OR POSSIBLY NOT GETTING TO FULL ARM PO SITION. FOUND LANYARD MATERIAL OBSTRUCTING GIRT BART TRAVEL. STOWED LANYARD IN PLACE. CYCLED DOOR OPEN AND CLOSED SEVERAL TIMES. ARMED AND DISARMED DOOR SEVERAL TIMES ALSO. DOOR INDICATION NORMALJan 1, 2025 · N488UA · Airbus A320232 · Emergency EquipmentSDR CALA2023120103506Relay · faultySIDESTICK PRIORITY DISPLAYED ON UPPER ECAM SCREEN. - F-CTL RESETTING SECS AND GRD SCAN CHECKS OK. TSM CALLS OUT TO CHANGE RELAYS 47CE1 AND 47CE2. SECOND HIT AND DOES HAVE SEC HISTORY. SEE TSM 27-92-00-810-830AH FLT WAS RTO. FO FLYING AND HAD STICK NOSE DOWN ANNov 28, 2023 · N488UA · Airbus A320232 · Flight Control SystemSDR CALA2023090802738Slide · unwanted deployDEPLOYED OVERWING SLIDE ON AIRCRAFT LEFT. PICS OF DEPLOYED SLIDE. REMOVED LH OFFWING SLIDE INFLATION RESERVOIR REF AMM 25-62-46-000-001-A. INFLATION RESERVOIR REMOVED PLACED IN AFT CGO PIT LT O/W WING SLIDE REMOVED REF AMM 25-62-42-000-002-A. BOTTLE, ASSY, O OAug 25, 2023 · N488UA · Airbus A320232 · Escape SlideSDR CALA2023082102595Stringer · corrodedAFT CRG LH SIDE FR59- STRG-30 CORRODE, REQUIRES FURTHER EVALUATION. AS NOTED ON LTPR NR#5001249722-0010. HEET 2. WORK PERFORMED ON LTPR NR# 5001249722-0010. THIS REPAIR 205-001, TABLE 004. INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR SUBSEQUENT INSPECTION AT IAug 20, 2023 · N488UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2023081602516Battery · no testEPSU BATTERY (13WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMNT. LTPR NR#5001250321-0010. BATTERY REPLACEMENT OF (13WL) PERFORMED IAW AMM:33-51-38-000-002 REV 120 & AMM:33-51-3-400-002 REV 120. TEST SATIRFACTORY. REMOVE PART INFOAug 14, 2023 · N488UA · Airbus A320232 · Emergency LightingSDR CALA2023081602515Battery · no testEPSU BATTERY (12WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMNT. LTPR NR#5001250432-0010. BATTERY REPLACEMENT OF (12WL) PERFORMED IAW AMM:33-51-38-000-002 REV 120 & AMM:33-51-38-400-002 REV 120. TEST SATIRFACTORY. REMOVE PART INFAug 14, 2023 · N488UA · Airbus A320232 · Emergency LightingSDR CALA2023081602514Battery · no testEPSU BATTERY (10WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMNT. LTPR NR#5001250322-0010. BATTERY REPLACEMENT OF (10WL) PERFORMED IAW AMM:33-51-38-000-002 REV 120 & AMM:33-51-38-400-002 REV 120. TEST SATIRFACTORY. REMOVE PART INFAug 14, 2023 · N488UA · Airbus A320232 · Emergency LightingSDR CALA2023081602513Battery · no testEPSU BATTERY (11WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMNT. LTPR NR#5001250423-0010. BATTERY REPLACEMENT OF (11WL) PERFORMED IAW AMM:33-51-38-000-002 REV 120 & AMM:33-51-38-400-002 REV 120. TEST SATIRFACTORY. REMOVE PART INFAug 14, 2023 · N488UA · Airbus A320232 · Emergency LightingSDR CALA2023050801411Unknown · unknownC/B TRIPPED R ELEC BAY FOUND 16CE2 ELAC 2 STBY SPLY ON 105VU POPPED.RESET C.B. UPDATED LABOR HOURS TOMC REQUESTED TO HAVE CB REPLACED AS A PRECAUTION. BREAKER P/N REF AMM 27-93-00, PERFORMED OPERATIONAL CHECK OF ELAC 2. C.B. EN2995-004A7A5A M&E # 18-2424-3-00May 8, 2023 · N488UA · Airbus A320232 · Flight Control SystemSDR CALA2022060201422Tube · looseHYDRAULIC QUANTITY LOW LEFT OR GREEN SYSTEM GREEN LO LVL ON ARRIVAL FOUND B NUT AT BOTTOM OF GREEN ACCUMULATOR LEAKING AS INDICATED BY MISS ALLIGNED WITNESS STRIPE. TIGHTENED B NUT, SERVICED HYDRAULICS. OPERATED HYDRAULIC SYSTEM. NO LEAKS NOTED.Jun 2, 2022 · N488UA · Airbus A320232 · Hydraulic Power Accumulator, MainSDR CALA2021092801719Fuel Cap · missingPDA 1 LANYARD MISSING FROM FUEL CAP. OPBLM CHRISTIANSEN ITEM ENTEREDIN CCL 28A. OPBLM CHRISTIANSENSep 28, 2021 · N488UA · Airbus A320232 · Aircraft Fuel SystemSDR CALA2021092801718Lanyard · missingRIGHT SIDE FUEL CAPLANYARD MISSINGFUEL CAP SECURE CURTIS, ZACHERY (V927339)VERIFIED NO LEAKS AT SPR COUPLING PER CDL 28A PROCEDURES.OPBLM CHRISTIANSEN. DISPATCH DESK: 01 NAME: CR DATE: 26-SEP-21- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FSep 28, 2021 · N488UA · Airbus A320232 · Aircraft Fuel SystemSDR CALA2021081601344Handle · bindingFLAP HANDLE BINDING ON FLAP RETRACTION. REMOVED AND REPLACED FLAP AND SLAT CONTROL LEVER REF AMM 27-51-43. OPS CHECK GOOD REMOVED AND REPLACED FLAP/SLAT COMMAND SENSOR UNIT REF AMM 27-51-17. OPS CHECK GOOD ROTABLE PARTS CHANGE WAS INDICATED - TT # 1999483 SN Aug 15, 2021 · N488UA · Airbus A320232 · Trailing Edge Flap Control SystemSDR CALA2021080901304Cover · missingPDA 3 LEFT WING #4 FLAP FAIRING 533CB MISSING BOLT COVER ON I/B SIDE. SEE PHOTO. REQUEST CDL. DISPATCH DESK: 34 NAME: SB.DATE: 07-AUG-21- APPROVED CDL 27AD APPLIED CDL. SEE AMM 57-55-11-400-001-A. STEP 4. B. (7) (E). RETAINER 59 AND PUSH-FIT COVER 45. REQUIAug 9, 2021 · N488UA · Airbus A320232 · Trailing Edge FlapsSDR CALA2021080401256Valve · failedENG2 BEARING 4 OIL SYSHI PRESS ECAM ON CLIMBOUT OF ORD.ECAM WENT AWAYAFTER A FEW MINUTES. RELATED CLM ARE "CHECK HARNESS OR CHANGE VALVE 4006EN (ENG 2)" AND "CHECK N4 BRG SCAV PRESSXMTR2 CITCUIT 4005 EN. AS WELL AS A RELATED "ENG 2 EIU" FAULT. TROUBLESHOOT PERAug 4, 2021 · N488UA · Airbus A320232 · Turbine Engine Oil SystemSDR CALA2021070501020Skin · corrodedFUSELAGE CROWN IN AREA COVERED BY VERT LWR L/E FAIRING AT BASE O F VERT STAB (2 EA) COAX CABLES CORROSION AT SKIN ON HAECO LCQ RE F 9294543/24543 A3NB-53-3-6208. NR GENERATED BY N079592 REPAIR AT FUSELAGE CROWN BASE OF VERT STAB FR69-70 STR 2R-2L ACC OMPLISHEDJul 3, 2021 · N488UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2021070101014Frame · crackedLEFT FRAME 35 AT S30L NR 2 HOLE CRACK INDICATION A3NB-53-3-6315 PER HA ECO LCQ NR 9294502/24502. INTERIM REPAIR ACCOMPLISHED IAW PART 1 OF ECRA 5331-02733. REAMED THE LH FRAME 35 AT STR30 #2 HOLE TO .4687. ACCOMPLISH INITIAL INSPECTION AT LH FR35 STR30 HOLE #Jul 1, 2021 · N488UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2021070101009Skin · crackedAFT PIT LT FRAME 61 CRACK INDICATION NOTED IN THE VERTICAL WEB OF THE FRAME AT LT STRINGER 37. INTERIM REPAIR ACCOMPLISHED IAW PART 1 OF ECRA 5341-01251. REAMED THE EFFECTED HOLE IN THE AFT PIT LH FRAME 61 VERTICAL WEB OF THE FRAME AT LH STRINGER 37 TO .190. AJun 30, 2021 · N488UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2021062300940Stop Fitting · crackedR1 DOOR FRAME 16 STOP FITTING #7 UPPER AND LOWER INBOARD HOLES ARE CRACKED IN THE INTERCOSTAL FITTING AT 6:00. INTERIM REPAIR ACCOMPLISH IAW PART 1 OF ECRA 5311-02584. REPLACED THE R1 DOOR FRAME STOP #7 INTERCOASTAL FITTING IAW ECRA 5311-02584. ACCOMPLISH INITJun 22, 2021 · N488UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2021062000904Intercostal · crackedPER NR 9294472/24472 L1 DOOR FRAME 16 STOP FITTING #7 UPPER AND LOWER INBD HOLES ARE CRACKED IN THE INTERCOSTAL FITTING. "REPAIR BEFORE NEXT FLIGHT", CONTACT ENGINEERING FOR APPROVED REPAIR IN STRUCTIONS. GENERATED BY V061633. REPAIR ON LH FR16 DOOR STOP FITTIJun 18, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2021061800891Floor Support · corrodedPER NR 9294698/24698. AFT PUT BETWEN FR63-64 LEFT STR42L HAS CORROSION. REPLACED DAMAGED SECTION OF S42L BETWEEN FR 62-64 IAW SRM 53-00-13-300-001. SUPPLEMENTAL INSPECTIONS REQUIRED IAW SRI 53-00-13-205-001 BEGINNING AT 60000FC OR 120000FH FROM REPAIR EMBODIJun 17, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2021061500883Stringer · corrodedAFT PUT BETWEN FR63-64 LEFT STR42L HAS COR ROSION. REPLACED DAMAGED SECTION OF S42L BETWEEN FR 62-64 IAW SRM 53-00-13-300-001. SUPPLEMENTAL INSPECTIONS REQUIRED IAW SRI 53-00-13-205-001 BEGINNING AT 60000FC OR 120000FH FROM REPAIR.Jun 15, 2021 · N488UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2021060400788Shear Tie · corrodedPER NR 9294611/24611. AFT CABIN SHEAR TIE FR70 STGR 23R HAS CORR OSION. GENERATED BY N078570. UPON EVAL OF SHEAR TIE AT FR70 STR 23-25R FOUND TO BE OUT OF LIM ITS. REMOVED, FABRICATED AND ISNTALLED SHEAR TIE IAW A320 SRM 51 -72-11, 51-44-11, 51-42-11. MECH V06Jun 3, 2021 · N488UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2021060400787Shear Panel · corrodedLH SHEAR PLATE IS CORRODED. A3NB-53-3-6222 ON HAECO LCQ NR 92944 40/24440. REMOVED AND REPLACED LH SHEAR PLATE IAW A320 SRM 51-42-11 AND SR M 51-72-11. SDR.Jun 2, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2021060400785Door Sill · corrodedL2 DOOR SILL HAS CORROSION. A3NB-53-3-6222 GENERATED BY V892442 ON HAECO LCQ NR 9294450/24450 L-2 DOOR SILL FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DO OR SILL IAW A320 SRM 51-42-11 AND 53-41-14-283-002. ACCOMPLISHED BY MECH V061673 INSP BY N078570Jun 2, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2021060200777Door · corrodedR2 DOOR SILL HAS CORROSION (A3NB-53-3-6222). REMOVED AND REPLACED R2 DOOR SILL IAW A320 SRM 51-72-11-911-001.May 31, 2021 · N488UA · Airbus A320232 · Service DoorsSDR CALA2021053100748Shear Web · corrodedAFT CABIN RH SHEAR WEB AT FR 70 LOWER SURFACE HAS CORROSION AND UPPER SURFACE HAS TOOL MARK A3NB-53-3-6222. GENERATED BY N078570 ON NR 9294610/HAECO NR 24610 REMOVED AND REPLACED CORRODED SHEAR WEB AT FR 70-69 LOWER SURFAC E IAW A320 SRM 51-42-11-001 SDR. ACCOMay 28, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2021052800743Shear Panel · corrodedRH SHEAR PLATE IS CORRODED. REMOVED AND REPLACED SHEAR PLATE RH FR 69-70 IAW SRM 51-42-11-001 AND SRM 51-72-11-911-001.May 26, 2021 · N488UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2021032600379Battery · no testDURING CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPS. CHK. RIGHT BATTERY AT FLOOR LEVEL OVER WING SEAT ROW 21F FAILED TEST. REPLACED BATTERY PACK AT RIGHT OW SEAT ROW 21F, OPS. CHK''S. GOOD, IAW AMM 33-51-38-00-002-AO.Mar 26, 2021 · N488UA · Airbus A320232 · Emergency LightingSDR CALA2021032600378Battery · no testDURING CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPS. CHK. FWD LEFT BATTERY FAILED TEST. REPLACED FWD ELL BATTERY PACK ABOVE FWD ENTRY DOOR 1L, OPS. CHK''S GOOD, IAW AMM 33-51-38-00-002-AO.Mar 26, 2021 · N488UA · Airbus A320232 · Emergency LightingSDR CALA2021012500092Power Supply · failedEPSU UNIT EMERGENCY L MESSAGE PRESENT REPLACED EPSU, REF AMM 33-51-38-000-001-A & 33-51-38-400-001-A. ALSO REPLACED BATTERY PACK REF AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPERATIONS CHECKED OK. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1249021 SN OFFJan 25, 2021 · N488UA · Airbus A320232 · Emergency LightingSDR CALA2020012600226Shear Tie · gougedFWD CARGO FRAME 27, STRINGER 43R - 44R CLEAT GOUGED. REMOVED AND REPLACED THE CLEAT IAW SRM 51-72-1 1-911-001 PARA S, D 1.Jan 20, 2020 · N488UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2020012300197Skin · dentedREPAIR REQUIRED AT FR.27, BETWEEN STR. 43R AND STR. 44 AT CENTER FUSELAGE. PER TASK CARD: 5273678/4216 (CUSTOMER REQUEST) (SUPPOR T TASK) PER HAECO LCQ N/R 9290201 GENERATED BY V061737 REF TERMINATING ACTION FOR DENT LOCATED AT FR27 BETWEEN S43R AND S44 FROM Jan 17, 2020 · N488UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2020012000194Plate · corrodedAFT CARGO DOOR TORSION BOX SILL PLATE CORROSION AT FR54 (A3NB-05 -3-6012) PER N/R 9290354 GENERATED. RMVD & RPLCD W/NEW TORSION BOX COVER PLATE AT AFT CARGO DOOR ENTRY PER SRM 53-41-49-283-004 & SRM 51-42-11-801. PERFORMED BY MECH, INSP.Jan 17, 2020 · N488UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019081601367Servo · leakingPOSITION FERRY MADE AIR RETURN DUE TO LOSS OF YELLOW HYDS. SPOILER #4 LEAK. REMOVED #4 SPOILER REF M.M. 27-64-44-000-001-A. FOUND #4 RIGHT SPOILER ACT LEAKING. REMOVED AND REPLACED #4 SPL ACT. REF AMM 27-64-51-400-004-A, 27-64-00-820-001-C, 27-64-00-710-001-A.Aug 14, 2019 · N488UA · Airbus A320232 · Hydraulic System, MainSDR CALA2018110502299Contactor · warning messageDC ESS BUS SHED DISPLAYED ON UPPER ECAM SCREEN. - EL EC REF TSM 24-60-00-710-801. BERG TOMC. REPLACED DC SHED ESSENTIAL BUS CONTACTOR, CKS OK, REF AMM24-62-5 5.Nov 5, 2018 · N488UA · Airbus A320232 · Electrical Power System Wiring
Back to N488UA