N428UA

Service difficulty reports · 197

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 = 'N428UA' 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 CALA2025051604726Beam · corrodedR2 DOOR SILL BEAM HAS CORROSION AT FR68 AREA. REPAIRED R2 DOOR SILL BEAM @ FR 68 IAW A320 SRM 53-41-14-300-001 FIGURE 1 REPAIR PRINCIPLE 7.May 13, 2025 · N428UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2025051604725Skin · dentedDENT ON FUSELAGE AT FR66L STR26-27. REPAIRED DENT ON LH FUSELAGE SKIN @ FR66 STR26-27 IAW A320 SRM 5 3-41-11-300-093.May 11, 2025 · N428UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2025051604724Shear Plate · corrodedMAIN CABIN AFT WET AREA FR69-70 LH SHEAR PLATE HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED LH FR 69-70 SHEAR PLATE IAW A320 SRM 51-42- 11/001.May 10, 2025 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2024123001692Autobrake Sys · no testBRAKES AUTO BRK FAULT AFTER GEAR EXTENTION TEST RESULTS PERFORMED BITE CHECK-BITE TEST OF BSCU NORMAL BRAKING TEST PER AMM TASK 32-46-00-740-005-A. NO FAULTS FOUND ON BSCU CHANNELS 1 OR 2. NO FAULT HISTORY IN THE PAST 90 DAYS IN SCEPTRE. NO CURRENT FAULTS ON EDec 26, 2024 · N428UA · Airbus A320232 · Landing Gear Brake SystemSDR CALA2024101500837Engine · vibrationENG 2 N1 VIB INDICATION ON MEL TOMC APPROVES MEL 7700G FOR ENG 2 N1 VIB TURNS YELLOW X OCCASIONALY. REPLACED EVMU IAW MM77-32-34/401 , IPC REF 77-32-34-01A NO HELP STATUS MESSAGE NEED FURTHER T/S. ADJUST AND TEST IAW MM UNIT, ENGINE VI OFF 31-7731-9-0001 0564 Oct 14, 2024 · N428UA · Airbus A320232 · Engine (Turbine/Turboprop)SDR CALA2024030500643Fuel Cap · missingPDA 2 FUEL CAP WAS FOUND MISSING PRIOR TO REFUELING FUEL CAP WAS CONFIRMED LEFT ON TRUCK IN IAD PRIOR TO FLIGHT 1262-02 COMPLIED WITH GMM. REPLACED FUEL/DEFUEL COUPLING CAP IAW AMM 28-25-41-400-005-A, OK FOR SVC.Mar 2, 2024 · N428UA · Airbus A320232 · Fuel StorageSDR CALA2023110303276Proximity Sensor · faultyL/G NOT UPLOCKEDWITH SHOCK ABSORBERFAULT DURING DEBREIF PILOT STATED IT WAS THE NLG SHOCK ABSORBER FAULT. ADDING POST FLIGHT REPORT REMOVED UNSERVICEABLE PROX SENSOR 24GA AND INSTALLED SERVICEABLE RECOMMEND FOLLOWING TSM 32-31-00-810-868-A SUSPECT SENSOR 24GA Nov 1, 2023 · N428UA · Airbus A320232 · Landing Gear Position and WarningSDR CALA2023092202859Window Frame · crackedFLIGHT DECK LOWER NODE R/H AND L/H I/B HOLES HAVE CRACK INDICATIONS. ACCOMPLISHED INTERIM REPAIR OF THE FRONT WINDSHIELD FRAME AND CONTINUITY FITTINGS PER ECRA 5311-03068 REV- PT1, QC INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-03068. PER PART 1 STEP 3-Sep 21, 2023 · N428UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2023092002822Window Frame · damagedFRONT WINDSHIELD FRAME AND CONTINUITY FITTING HAVE REJECTABLE INDICATIONS "ACCOMPLISH INITIAL INSPS OF THE FRONT WINDSHIELD FRAMES OF ECRA 5311-03068 ON OR BEFORE THE AC REACHES 65681 TOTAL AND CONTINUITY FITTINGS PER PART 2 OFTHE LATEST REVISION AIRCRAFT FLIGSep 18, 2023 · N428UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2023091802813Panel · crackedLOG PAGE FOR NEW DTA DIP REQUIREMENTS PER ECRA 5311-02197 REV D PT 1B REFERANCE LOG PAGE #3786677 "FOR RH FR35-36 PRESSURE PANEL, HOLES #A1- #A28, PLANNING AC FH''S (WHICHEVER COMES FIRST), BUT BEFORE 61707 TOTAL AC TO CONTACT ENG''ING AFTER 60707 TOTAL AC FH'Sep 17, 2023 · N428UA · Airbus A320232 · Fuselage Structure (General)SDR 2023FA0000274Unknown · cracked5 CRACKS NOT CONTAINED WITHIN AREA A1. OUT OF SUBTASK 72-50-00-230-071 ACCEPTANCE LIMITS. LIFE LIMITED PART (LLP) TO BE RETIRED WITH 12565 CYCLES SINCE NEW (LLP LIMIT IS 20000 CYCLES)May 19, 2023 · N428UA · Airbus A320232 · Turbine SectionSDR CALA2023051201467Fuel Cap · missingFUELER REPORTS FUEL CAP MISSING. INSTALLED FUEL CAP.May 9, 2023 · N428UA · Airbus A320232 · Fuel StorageSDR CALA2023050901439Coupling · unknownPDA 2 REF LP 4548150 - ON ARRIVAL, FUELER REPORTS FUEL CAP MISSING. REFER LP# 4548160 UPDATE INFO...ACCOMPLISHED ACFT WINGS AND FUSELAGE VISUAL INSPECTION. NO DAMEGE FOUND. OK TO CONTINUE.May 9, 2023 · N428UA · Airbus A320232 · Aircraft Fuel SystemSDR CALA2022081702115Light · inoperativeCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - AFT EMERGENCY BATTERY FAILED CAP TEST REMOVED AND REPLACED AFT EMERGENCY BATTERY. OPS CHECK GOODAug 17, 2022 · N428UA · Airbus A320232 · Emergency LightingSDR CALA2022081202059Relay · inoperativeAUTO FLT ''A-THR OFF''DISPLAYED ON UPPER ECAM SCREEN. AUTO THRUST FAIL TROUBLESHOT PER TSM 22-31-00-810-812-A. PERFORMED GROUND SCAN OF THE AFS AND REPLACED RELAYS 17CA1, 17CA2, 18CA1, 18CA2, 5CA1, AND 5CA2. ENG 2 EEC WAS ALSO REPLACED FOR ANOTHER PROBLEM, SEEAug 12, 2022 · N428UA · Airbus A320232 · Auto Throttle SystemSDR CALA2022021400366Light · failedEPSU EXT LOAD FWD L ON FORWARD PANEL DURING EMERGENCY LIGHT TEST. REF 33-51-38.Feb 11, 2022 · N428UA · Airbus A320232 · Lighting SystemSDR CALA2021081801374Packing · leakingHYD Y QTY LOW...SYSTEM NORM B4 T/O LOST FLUID AT ALTITUDE PER CAPTAIN YELLOW HYDRAULIC SYSTEM RAN WITH 0 QTY. INSPECTED MLG WHEEL WELL AND FOUND YELLOW SYSTEM PRIORITY MANIFOLD ASSY (3015GM) MISTING HYD FLUID. REF IPC 29-13-15-02A SUSPECT ITEM 40 AND 10. IPC PAug 18, 2021 · N428UA · Airbus A320232 · Hydraulic System, MainSDR CALA2019110501919Hydraulic Line · leakingHYDRAULIC QUANTITY LOW LEFT OR GREEN SYSTEM SHOWING 4.5 LITRESIN FLIGHT FL350 FOUND EVIDENCE OF HYD LEAK ON LOWER FUSELAGE JUST BEHIND THE GEARWHEEL PREVIOUS UPDATE NO HELP WILL NEED TO START TROUBLESHOOTING FOUND LEFT MLG HOSE LEAKING. R/R HOSE LEAK AND OPS CNov 2, 2019 · N428UA · Airbus A320232 · Hydraulic System, MainSDR CALA2019072801264Roller · lack of lubeFLAPS LOCKED - ALIGNMENT FAULT DISPLAYED ON UPPER EC AM SCREEN. - F-CTL PLEASE WORK FAULTS IAW TSM 27-51-00-810-818-A. TOMC SMITH 847-700-9980 CONTACT TOMC 847-700-9980 UNLOCKED FOR AVIONICS UPDATE, TOMC SMITH SFCC BITE , NO CURRENT FAULT FOUND. ON LAST LEG RJul 28, 2019 · N428UA · Airbus A320232 · Trailing Edge Flap Control SystemSDR CALA2019072401252Skin · dentedFUSELAGE EXTERIOR SKIN LOWER LOBE FR25-26 STR 41-43 RT SKIN DENTED A3NB-53-3-6105 PER NON ROUTINE 9293391 DISCREPANT LOCATION SHOULD READ FR25-26, STR 42R-43R. ACCOMPLISHED INTERIM REPAIR PER ECRA 5331-02415 PART 1. ACCOMPLISH THE INITIAL INSPECTION REQUIREMENJul 18, 2019 · N428UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2019071901222Intercostal · corrodedAFT PIT FR56-57 STR 38R INTERCOSTAL TOP SURFACE CORROSION A3NB-5 3-4-5179 PER NON ROUTNE 9293340 REMOVED AND REPLACED CORRODED INTERCOSTAL AT FR56-57 STR38R IAW CRA 5341-01175.Jul 18, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019071801216Pressure Panel · crackedDURING INSPECTION AND MODIFICATION PER EA 5330-05216 OP2 AT LT PRESSURE PANEL AT FR35-36 HOLES SHOWN FIGURE 1 WERE FOUND WITH CRACK INDICATIONS DAMAGE IS BEYOND EA LIMITS PER NON ROUTINE 9293540 ACCOMPLISHED INTERIM REPAIR AT LH PRESSURE PANEL FR 35-36 HOLES IJul 17, 2019 · N428UA · Airbus A320232 · Fuselage Main, BulkheadSDR CALA2019071901223Pressure Panel · crackedDURING INSPECTION AND MODIFICATION PER EA 5330-05216 OP3 AT RT PRESSURE PANEL AT FR35-36 HOLES SHOWN IN FIGURE 1 WERE FOUND WITH CRACK INDICATIONS DAMAGE IS BEYOND EA LIMITS PER NON ROUTINE 9293541 ACCOMPLISHED REPAIR AT RT PRESSURE PANEL AT FR 35-36 HOLES IAWJul 17, 2019 · N428UA · Airbus A320232 · Fuselage Main, BulkheadSDR CALA2019071801210Plate · corrodedAFT CARGO PIT SKIN PLATE BETWEEN STRG 38R-39R IS CORRDED APPRX. 2" AFT FRAME 65 A3NB-53-3-6185 PER NON ROUTINE 9293158 ACCOMPLISHED REPAIR IAW ECRA 5331-02416 PART 1. ACCOMPLISH THE IN ITIAL INSPECTION REQUIREMENTS PER PART 2 OF ECRA 5331-02416 ON OR BEFORE THJul 16, 2019 · N428UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2019071801212Skin · dentedREF LOG PAGE 3639919 DENT FOUND CREASE OUT OF LIMITS RE-EVALUATE DENT AND POSSIBLE CREASE BELOW LH PAX WINDOW 2 STA897+ FR23-24 STR21-22L PER NON ROUTINE 9293275 DENT FOUND TO BE OUT OF LIMITS PER SRM 53-11-11-283-001 AND SRM 53-11-11-283-012 DIA 02. ACCOMPLISJul 16, 2019 · N428UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2019071801211Keelbeam · damagedDURING ACCOMPLISHMENT OF FCD 5330-05575 REV D KEEL BEAM HOLES LABELED L2, L8, L21, L74, 10, R18 AND R19 WERE FOUND OUT OF ROUND ECRA 5311-02186 APPENDIX A DEFINES LOCATION AND DETAILS OF THE DISCREPANT HOLES PER NON ROUTINE 9293501 ACCOMPLISHED INTERIM REPAIR Jul 16, 2019 · N428UA · Airbus A320232 · Fuselage Main, KeelSDR CALA2019070801168Stringer · corrodedAFT CARGO FLOOR FR59 STR40R HAS CORROSION A3NB-53-4-6179 PER NON ROUTINE 9293045 REMOVED AND REPLACED STR 40R B/W FR58-63 IAW SRM 51-72-11-9 11-001 AND 51-42-11-001.Jul 7, 2019 · N428UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019070801167Strap · corrodedFWD CARGO STRAP BELOW CLEAT AT FR29 ST41R-40R HAS CORROSION ON REF 9293149 SPEC A3NB-05-3-6013. REMOVED & REPLACED LOWER STRAP BELOW CLEAT AT FR29 ST 41R-40R IAW SRM 51-42-11 PARA E & SRM 51-72-11 PARA 3 & 4 AT ON HANGAR NR 9293149.Jul 7, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019070801166Skin · dentedLWR FUSELAGE EXTERIOR SKIN BETWEEN FR28-29 STR43R HAS DENT A3NB- 05-3-6003 PER NON ROUTINE 9292198 REPAIRED LWR FUSELAGE EXTERIOR SKIN B/W FR28-29R AT STR43R IAW SRM 53-00-11-300-042.Jul 7, 2019 · N428UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2019070801162Cleat · corrodedCLEAT AT FR 65 STR 39R HAS CORROSION PER NR LP 9293324 REMOVED AND REPLACED CLEAT AT FR63 STR 39R IAW SRM 51-72-11 -911-001.Jul 7, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019070801161Cleat · corrodedFWD CARGO CLEAT FR30 STR 42R-41R HAS CORROSION ON REF 9293153 SPEC A3NB-05-3-6013. REMOVED & REPLACED FWD CARGO CLEAT AT FR30 STR 42R TO 41R IAW SRM 51-72-11-911-001 AT ON HANGAR NR 9293153.Jul 7, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019070801160Cleat · corrodedFWD CARGO FR32 CLEAT STR 40R-39R HAS CORROSION PER NR LP 9293169 REMOVED AND REPLACED FWD CARGO CLEAT AT FR32 STR 40R TO 39R IAW SRM 51-72-11-911-001.Jul 7, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019070801157Stringer · corrodedFWD PIT STR 39 FRAME 28-29 HAS SPOTS OF CORROSION. A3NB-53-3-61 05. NR 9293222 REPAIRED STR 39L BTW FRAMES 28 & 29 AT FWD PIT IAW SRM 53-00-13-300-001 FIG 1 SHEET 3 THIS REPAIR REQUIRES REINSPECT AT 60000FC OR 12000FH FROM REPAIR EMBODIMENT. SUBSEQUENT INSPECTJul 6, 2019 · N428UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019070801153Skin · damagedFWD PIT BILGE AREA FR 29 STR 42-43R SKIN HAS DAMAGE HOLT AT CLEAT AREA PER NR 9293008 AND REPAIRED FWD PIT BILGE AREA AT FR29 STR 42-43R IAW SRM 53-0 0-11-300-043.Jul 5, 2019 · N428UA · Airbus A320232 · Fuselage Main, Plate/SkinSDR CALA2019070801152Cleat · corrodedFWD PIT HAS CORROSION CLEAT AT FR33 STR42L-43L A3NB-53-3-6112 PER HAECO LCQ NON ROUTINE 9293190 REMOVED AND REPLACED CLEAT IN FWD CARGO AT FR33 BETWEEN STR 42L- 43L IAW SRM 51-72-11-911-002 PARA 2.Jul 5, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019070501139Stringer · corrodedAFT CARGO FLOOR FR 56-57 STR 40 RT CORROSION. A3NB-53-4-6179, NR 9293053 REMOVED AND REPLACED AFT CARGO STR 40R FRAME 56-57 IAW SRM 51-72-11-911-001 & SRM 51-42-11-001.Jul 4, 2019 · N428UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019070501138Skin · dented2EA DENTS ON TOP OF TAIL CONE APPROX. 1FT LEFT OF RUDDER TRAILING EDGE TRIANGLE. A3NB-05-3-6072. NR 9292361 REPAIRED DENTED AREA BTEWEEN FR51 AND FR82 STR 2L AND 3L IAW SRM 53-51-11-300-002 FIG 01.Jul 4, 2019 · N428UA · Airbus A320232 · Aerodynamic FairingsSDR CALA2019070301125Cleat · corrodedFWD PIT FR31 STR42-43LT CLEAT CORRODED A3NB-05-3-6013 PER NON ROUTINE 9293394 REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAM 31 BETWEEN STR 42L TO 43L IAW SRM 51-72-11-911-002 PARA 2.Jul 1, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019070301124Cleat · corrodedFWD CARGO FR29 STR43L-42L CLEAT HAS CORROSION A3NB-05-3-6013 PER NON ROUTINE 9292919 REMOVED AND REPLACED CLEAT IN FWD CARGO AT FR 29 BETWEEN STR 42L TO 43L IAW SRM 51-72-11-911-002 PARA 2.Jul 1, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019070301123Cleat · corrodedFWD CARGO CLEAT FR30 ST43L-42L HAS CORROSION A3NB-05-3-6013 PER NON ROUTINE 9293157 REMOVED AND REPLACED CLEAT IN FWD CARGO AT FRAME 30 BETWEEN STRINGER 42L AND STRINGER 43L IAW SRM 51-72-11-911-002.Jul 1, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019070301122Cleat · corrodedFWD CARGO FR29 ST43R-42R CLEAT HAS CORROSION A3NB-05-3-6013 PER NON ROUTINE 9292916 REMOVED AND REPLACED CLEAT AT FWD CARGO FR29 B/W STR43R-42R IAW SRM 51-72-11-911-001 AND SRM 51-42-11-001.Jul 1, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019070301121Cleat · corrodedFWD PIT CLEAT FRAME 31 STR 42R-43R IS CORRODED A3NB-53-3-6105 PER NON ROUTINE 9293216 REMOVED AND REPLACED CLEAT IN FWD CARGO AT FR 31 BETWEEN ST 42R AND 43R IAW SRM 51-72-11-911-002 PARA 2.Jul 1, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2019070201112Stringer · corrodedFWD CARGO STR 40R HAS CORROSION BETWEEN FR31-32 ON REF 9293168 SPEC A3NB-05-3-6013. REMOVED & REPLACED STR 40R AT FWD CARGO FR29-35 IAW SRM 51- 7-11-001 & SRM 51-42-11-001 AT ON HANGAR NR 9293168. MAINT PERFORMED RII INSP PERFORMED.Jun 30, 2019 · N428UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2019063001099Stringer · corrodedAFT CARGO PIT STRINGER 39R JUST AFT OF FRAME 65 IS CORRODED. REMOVED AND REPLACED AFT CARGO PIT STRINGER 39R IAW A320 51-72-1 1-911-001.Jun 27, 2019 · N428UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA201906301085Floor Support · bentAFT CARGO FLOOR FR54 STR43RT AND 43LT FLOOR SUPPORTS BENT A3NB-5 3-4-6179 . REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT AT FR54 STR43R-STR4 3L IAW A320 SRM 51-42-11.Jun 26, 2019 · N428UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA201906301084Shear Tie · corrodedFWD CARGO FR32 CLEAT ST41R-40R HAS CORROSION A3NB-05-3-6013 PER HAECO LCQ NON ROUTINE 9293167 GENERATED BY N078625 REMOVED AND REPLACED CLEAT AT FRAME 32 BETWEEN STRINGER 40R TO S TRINGER 41R IAW A320 SRM 51-72-11-911-002.Jun 26, 2019 · N428UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA201906301082Cargo Track · corrodedAFT CARGO CLEAT HAS CORROSION AT FR 65 STR43LT. REMOVED AND REPLACED AFT CARGO CLEAT IAW SRM 51-42-11-001.Jun 26, 2019 · N428UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2019062901086Not Reported · corrodedAFT CARGO FLOOR FR59 STR43 RT CORRODED. REMOVED AND REPLACED STR43RT FR57-60 IAW SRM 51-42-11 AND S RM 51-72-11-911-001.Jun 26, 2019 · N428UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2019062901070Shear Tie · corrodedFWD CARGO FR26 STR43L-42L CLEAT HAS CORROSION A3NB-05-3-6013 PER HAECO LCQ NON ROUTINE 9292913 GENERATED BY N078625 REMOVED AND REPLACED CLEAT AT FRAME 26 BETWEEN STRINGER 43L AND 42L IAW A320 SRM 51-72-11-911-002 PERFORMED BY MECH V892568 MECH V080285 INSP BYJun 24, 2019 · N428UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2019062901069Shear Tie · corrodedFWD CARGO CLEAT FR30 ST40R-41R HAS CORROSION A3NB-05-3-6013 PER HAECO LCQ NON ROUTINE 9293152 GENERATED BY N078625 REMOVED AND REPLACED CLEAT AT FRAME 30 BETWEEN STRINGER 40R TO S TRINGER 41R IAW A320 SRM 51-72-11-911-002 PERFORMED BY MECH V892 568 MECH V08028Jun 24, 2019 · N428UA · Airbus A320232 · Fuselage Internal Mounting Structure
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