# Service difficulty reports: N472UA A list on [N472UA](https://openairdocs.org/aircraft/N472UA.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 102 reports - [SDR CALA2026092419794](https://openairdocs.org/sdr/CALA2026092419794.md): Light · inoperative · Sep 23, 2026 · N472UA · Airbus A320232 · Emergency Lighting > EMERGENCY LIGHT ON SEAT 7C INOP. REMOVED AND INSTALLED NEW LIGHT ASSY REF AMM 33-51-11/401 CONFIG 00. OPS CHECK GOOD AT THIS TIME. - [SDR CALA2026061517104](https://openairdocs.org/sdr/CALA2026061517104.md): Door · damaged · Jun 12, 2026 · N472UA · Airbus A320232 · Passenger/Crew Doors > LOWER AFT CORNER OF L1 DOOR DAMAGED.REMOVED DAMAGE REF SRM 51-27-11. PERFORMED DOOR SKIN CUT OUT PER STEP 1 OF AVO 17658. REQUESTING INSPECTION OF TRIMMED EDGE PER STEP 2 OF AVO 17658. ACP DISPOSITION 2 ON AVO 17658 NO CRACKS INDICATED REF NTM PT6 51-10-08. - [SDR CALA2026052016420](https://openairdocs.org/sdr/CALA2026052016420.md): Pressure Switch · faulted · May 17, 2026 · N472UA · Airbus A320232 · Hydraulic System, Main > HYD G ENG 1 PUMP LO PR PREVIOUS HISTORY LOG PAGE 8914306, SEE TSM 29-11-00-810-804-A INSPECTED ENGINE AND WHEEL WELL AND FOUND NO LEAKS. GREEN SYSTEM WAS FOUND LOW. SERVICED GREEN SYSTEM REF. AMM 12-12-29-611-001-A. RAN ENGINE #1 FOLLOWING TSM 29-11-00-810-804 - [SDR CALA2025102810631](https://openairdocs.org/sdr/CALA2025102810631.md): Battery · no test · Oct 26, 2025 · N472UA · Airbus A320232 · Emergency Lighting > EPSU BATTERY FWD L INDICATION AFTER EMERGENCY LIGHT TEST PARTS NIS AT BNA PARTS UPDATED REMOVED AND REPLACED FWD LEFT EPSU BATTERY PER AMM 33-51-38. OPS CHECK GOOD. TEST OK. PARTS USED: 18-3351-3-0001, QTY:1 - [SDR CALA2025100309577](https://openairdocs.org/sdr/CALA2025100309577.md): Pin · installed · Oct 1, 2025 · N472UA · Airbus A320232 · Standard Practices/Structures > INSTALLED SAFETY LOCK PIN ON THE INFLATION RESERVOIR FOR LEFT OFFWING SLIDE. REF AMM 25-62-00-481-001-A. VERIFIED CORRECT INSTALLATION OF SAFETY LOCK PIN ON THE LH OFFWING SLIDE INFLATION RESERVOIR REMOVED SAFETY LOCK PIN ON THE INFLATION RESERVOIR FOR LEFT OF - [SDR CALA2025070906376](https://openairdocs.org/sdr/CALA2025070906376.md): Blanking Plate · missing · Jul 7, 2025 · N472UA · Airbus A320232 · Fuselage Main, Structure > PDA 2 CREW LOG PAGE# 5470969, LEFT MAIN LANDING GEAR PURPLE BLANKING PLUG MISSING. LEFT MLG MISSING BLANKING PLUG. PERFORMED INTERIM REPAIR PER PART 1 OF ECRA 3211-01346 TO LT MLG BLANKING PLUG. ISSUE DIP TO ACCOMPLISH DAILY INSP IAW PART 2 & PERMANENT REPAIR - [SDR CALA2025052604944](https://openairdocs.org/sdr/CALA2025052604944.md): Power Supply · faulted · May 23, 2025 · N472UA · Airbus A320232 · Emergency Lighting > EMERGENCY LIGHT SWITCH (4WL) ON FWD OVERHEAD PANEL MALFUCTIONING. REPLACED EMERGENCY LIGHT SWITCH (4WL) REF AWM 33-51-01 PG 01. OPS CHECKED GOOD.PARTS USED: EMERGENCY LIGHT TEST FAILED EPSU INT LOAD EMER L SEE PIC. R/R POWER SUPPLY UNIT(11WL) REF AMM 33-51-38 - [SDR CALA2024110601047](https://openairdocs.org/sdr/CALA2024110601047.md): Warning Light · false activation · Nov 4, 2024 · N472UA · Airbus A320232 · Doors > DOOR 2L ECAM UPON LANDING. DOOR SHOWED OPEN ON DOORS SYNOPTIC PAGE. DOOR WAS VERIFIIED DOOR 2R INDICATED PER PFR AND LAST LEG RPT. PLACED DOOR 2R ECAM INDICATION ON MEL 5270AV. REQUIRES TO BE CHECKED BEFORE EA. DEPARTURE..APPROVED PLACED DOOR 2R ECAM INDICATI - [SDR CALA2024051301456](https://openairdocs.org/sdr/CALA2024051301456.md): Floor Support · corroded · May 10, 2024 · N472UA · Airbus A320232 · Fuselage Miscellaneous Structure > RH AFT MAIN CABIN BETWEEN FR68 & FR69 AND ABOUT 12 INCHES FROM S IDEWALL, FLOOR SUPPORT STRUCTURE CORRODED. PERFORMED DVI IAW NTM 51-90-00 OUT OF LIMITS IAW SRM 53-41-14-28 51-42-11, REINSTALLED FLOOR SUPPORT BTW FR66 TO FR68, RESTORED SURF 3-009, REMOVED RH F - [SDR CALA2024051301468](https://openairdocs.org/sdr/CALA2024051301468.md): Frame · corroded · May 9, 2024 · N472UA · Airbus A320232 · Fuselage Main, Frame > FR 68 AT STR23 RH, PREVIOUS CORROSION REPAIR WAS REEVALUATED AND SUBSEQUENTLY REPAIRED IAW ECRA5341-01452. WEB AT STR23RH WAS REPAIRED AT BFM. REPAIR IS EXPECTED TO BECOME PART 3 OF LATEST REV OF ECRA5341-01452 ON/BEFORE MAY 3, 2025. PERMANENT SOLUTION W/ INSP - [SDR CALA2024051301454](https://openairdocs.org/sdr/CALA2024051301454.md): Window Frame · cracked · May 4, 2024 · N472UA · Airbus A320232 · Fuselage Main, Structure > PER ECRA 5311-03212 PART 1.2: LH FRONT WINDSHIELD FRAME, LOWER NODE, CRACKED HOLE D WAS REPAIRED AT BFM. REPAIR IS A PERMANENT REPAIR WITH INSPECTION REQUIREMENTS. - [SDR CALA2024051301455](https://openairdocs.org/sdr/CALA2024051301455.md): Skin · corroded · Apr 1, 2024 · N472UA · Airbus A320232 · Fuselage Main, Plate/Skin > AFT. UPPER FUSELAGE, ELT ANT. HAS CORRODED/ SMOKING RIVETS PART I. ELT ANTENNA UPPER FUSELAGE SKIN, BETWEEN FR64 - FR65 AND BETWEEN STGR 1LH AND STGR 1 RH, PERMANENT REPAIR IAW EC/RA # 5341-01453. - [SDR CALA2024051301453](https://openairdocs.org/sdr/CALA2024051301453.md): Door Sill · corroded · Mar 29, 2024 · N472UA · Airbus A320232 · Fuselage Miscellaneous Structure > R2 DOOR LOWER CUT-OUT DOOR SILL ASSY CORRODED. CORROSION ON AREA OUT OF LIMITS IAW SRM 53-41-14-283-002, REMOVE D AND REINSTALLED SCUFF PLATES IAW AMM 53-45-15-400-001-A, REMOVED AND REPLACED DOOR SILL IAW D53480505 AND SRM 51-42-11/001. - [SDR CALA2024041701116](https://openairdocs.org/sdr/CALA2024041701116.md): Floor Support · corroded · Mar 29, 2024 · N472UA · Airbus A320232 · Fuselage Miscellaneous Structure > AFT MAIN CABIN BETWEEN FR65 AND FR66 ABOUT 20 INCHES TO THE LEFT OF CENTER FUSELAG,E FLOOR SUPPORT STRUCTURE HAS CORROSION. - [SDR CALA2024041501078](https://openairdocs.org/sdr/CALA2024041501078.md): Shear Plate · corroded · Mar 29, 2024 · N472UA · Airbus A320232 · Fuselage Miscellaneous Structure > LH AFT MAIN CABIN BETWEEN FR69 AND FR70 LATERAL SHEAR PLATE BOTTOM SURFACE HAS CORROSION AND CRACKED. SDR REMOVED SHEAR PLATE AND FRAME SUPPORT IN L/H AFT MAIN CABIN RESTORED TREAM PRIMER, TOP COAT AND CIC IAW SRM 51-75-11 SRM 51- IN BTW FR69-FR70 IAW SRM 51-4 - [SDR CALA2024040800994](https://openairdocs.org/sdr/CALA2024040800994.md): Floor Support · corroded · Mar 29, 2024 · N472UA · Airbus A320232 · Fuselage Miscellaneous Structure > RH AFT MAIN CABIN BETWEEN FR69 AND FR70 LATERAL SHEAR PLATE BOTT OM FACE CORRODED. - [SDR CALA2024040800993](https://openairdocs.org/sdr/CALA2024040800993.md): Floor Support · corroded · Mar 29, 2024 · N472UA · Airbus A320232 · Fuselage Miscellaneous Structure > RH AFT MAIN CABIN AT FR68 ABOUT 28 INCHES FROM R2 DOOR CUT-OUT, FLOOR SUPPORT STRUCTURE HAS CORROSION. - [SDR CALA2024041601099](https://openairdocs.org/sdr/CALA2024041601099.md): Beam · corroded · Mar 27, 2024 · N472UA · Airbus A320232 · Fuselage Miscellaneous Structure > RH AFT MAIN CABIN AT FR66 ABOUT 24 INCHES FROM R2 DOOR CUT-OUT, FLOOR SUPPORT STRUCTURE CORRODED. REMOVED AND REMPLACED BEAM SUPPORT IN MAIN CABIN BETWEEN FRAME 64 TO FRAME 66 R/H IAW SRM 51-42-11. EMP: V942985 WC: 96354 STA: ST ENG BFM - [SDR CALA2024042201152](https://openairdocs.org/sdr/CALA2024042201152.md): Shear Tie · cracked · Mar 20, 2024 · N472UA · Airbus A320232 · Fuselage Internal Mounting Structure > DURING ROTO OF LH FR43 FOOT CRACKS NOTED AT THE 3:00 AND 9:00 PO SITION OF FRAME "REPAIR BEFORE NEXT FLIGHT RII, SDR REMOVED AND REAPLACED FOOT LH FR43 AND RESTORED SURFACE PROTECTION IAW SRM 51-75-12 AND REPAIR DRAWING 15R53370232 ISSUE D, EA# 5330-06692 REV - [SDR CALA2023101703098](https://openairdocs.org/sdr/CALA2023101703098.md): Fuel Cap · missing · Oct 15, 2023 · N472UA · Airbus A320232 · Fuel Storage > PDA 2 FUEL CAP MISSING ENGINEERING ADVISED. COMPLIED WITH DEFERRAL AS REQUIRED COMPLIED WITH DEFERRAL AS REQUIRED DISPATCH DESK: 24 NAME: ZR DATE: 15-OCT-23- FUEL CAP MISSING REPLACED FUEL CAP AS PER AMM 28-25-00-440-003-A. NO DEFECTS OK TO CONTINUE. - [SDR CALA2022090502285](https://openairdocs.org/sdr/CALA2022090502285.md): Flap · locked · Aug 31, 2022 · N472UA · Airbus A300* · Flight Control System > FLT DECLARING A MECHANICAL EMERGENCY INTO SFO DUE FLAP LOCK PRIOR TO LANDING FLAP CONFIGURATION. FURTHER DETAILS AWAITED. - [SDR CALA2022061501512](https://openairdocs.org/sdr/CALA2022061501512.md): None · failed · Jun 15, 2022 · N472UA · Airbus A300* · Engine Controls > ONE TLA FAULT DISPLAYED ON UPPER ECAM SCREEN. - ENG 2 CAME ON AND EXTINGUISHED. REPEAT GRIPE. 1 UPDATE. STARTED TS TASK 76-00-00-810-802-B, FOUND FADECA AND 2 UPDATE, ENG #2 WIRING CHECK ALL OK FROM EEC 4000KS TO TCU FADECB FAULT CODE TRAXCF, NEXT STEP CHE - [SDR CALA2022053001402](https://openairdocs.org/sdr/CALA2022053001402.md): Fuel Cap · missing · May 26, 2022 · N472UA · Airbus A300* · Aircraft Fuel System > FUEL CAP MISSING REQUESTING DEFERRAL, FUEL CAP MISSING. DDP C/W. PLACED ON DEFERRAL, DDP C/W. ARRIVED DEN WITH NO CAP DISPATCH DESK: 39 NAME: PL,DATE: 26-MAY-22- OK TO DEFER FUEL CAP MISSING THIS ITEM IS A PDA CATEGORY 2. DFW RESEARCHED WITH FUELER AND THEY S - [SDR CALA2022042701088](https://openairdocs.org/sdr/CALA2022042701088.md): Intercostal · cracked · Apr 27, 2022 · N472UA · Airbus A320232 · Doors > A3NB-52-4 "DOT 143-017" R/H FWD EMERGENCY ESCAPE DOOR INTERCOAST ALS FWD OF WINDOW HAS VISUAL INDICATION OF CRACK EMANATING FROM RIVETS. REQUEST NDT VERIFY.() RH FWD EMERGENCYDOOR (EXIT) ANGEL SEGMENT REQUIRED AND COMPLIED WITH ECRA #5221-01061 REV_ NO DIVIATI - [SDR CALA2022042501057](https://openairdocs.org/sdr/CALA2022042501057.md): Intercostal · cracked · Apr 22, 2022 · N472UA · Airbus A320232 · Doors > A3NB-52-4 "DOT 143-016'' R/H AFT EMERGENCY ESCAPE DOOR INTERCOSTA LS INBD AND OTBD OF WINDOW HAVE VISUAL INDICATION OF CRACKS EMAN ATING FROM RIVETS. REQUEST NTD VERIFY.() REMOVED R/H AFT EMERGENCY ESCAPE DOOR INTERCOSTALS INBD AND OTBD AND REPLACED NEW INTERC - [SDR CALA2022042501056](https://openairdocs.org/sdr/CALA2022042501056.md): Intercostal · cracked · Apr 22, 2022 · N472UA · Airbus A320232 · Doors > (A3NB-52-4-6031) LH AFT EMERGENCY ESCAPE DOOR INTERCOSTAL I/B AN D O/B OF WINDOW HAVE SIGNS OF CRACKS AT RIVETS. REQUEST VERFICAT IONS DOT 31-060() REMOVED AND REPLACED LH AFT EMERGENCY ESCAPE DOOR INTERCOSTAL I/ MOBILE. NR#0030547 B AND O/B OF WINDOW IAW 51-4 - [SDR CALA2022042501055](https://openairdocs.org/sdr/CALA2022042501055.md): Intercostal · cracked · Apr 22, 2022 · N472UA · Airbus A320232 · Doors > (A3NB-52-4-6031) LH FWD EMERGENCY ESCAPE DOOR INTERCOSTAL I/B AN D O/B OF WINDOW HAVE SIGNS OF CRACKS AT RIVETS. REQUEST VERFICAT ION DOT 31-061() REMOVED L/H FWD EMERGENCY ESCAPE DOOR INTERCOSTALS I/B AND O/B A ND REPLACED WITH NEW INTERCOSTALS IAW SRM 51-42- - [SDR CALA2021080901303](https://openairdocs.org/sdr/CALA2021080901303.md): Control Valve · malfunctioned · Aug 9, 2021 · N472UA · Airbus A320232 · Cabin Temperature Control System > CABIN TEMPS UNCONTROLLABLE ON CLIMBOUTCOCKPIT 136 TOMC UPDATE: CREW ADVISED VIA ACARS PACK 1 OUTLET TEMP MUCH HIGHER THAN PACK 2 OVER 10 DEG, TOMC ADVISED CREW TO TURN OFF PACK WITH HIGHEST OUTLET TEMP (PACK 1) CREW REPLIED THE TEMPS STARTED TO DROP. TOMC SUSP - [SDR CALA2020040300760](https://openairdocs.org/sdr/CALA2020040300760.md): Door Frame · corroded · Apr 1, 2020 · N472UA · Airbus A320232 · Fuselage Main, Structure > WHILE AT AAR DLH DURING HMV-3 CHECK FOUND CORROSION ON FR68 AT STR23 AND A CRACK AT THE DOOR STOP #1, REPAIR BEFORE NEXT FLIGHT. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5341-01220. ACCOMPLISH A PERMANENT REPAIR AT RH FR68, STR23 PER PART 3 OF ECRA 5341- - [SDR CALA2020040300759](https://openairdocs.org/sdr/CALA2020040300759.md): Frame · corroded · Apr 1, 2020 · N472UA · Airbus A320232 · Fuselage Main, Frame > WHILE AT AAR DLH DURING HMV-3 CHECK FOUND FR68 AT STR23 R/H CORRODED ON FWD SIDE OF FRAME. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5341-01220. ACCOMPLISH A PERMANENT REPAIR AT RH FR68, STR23 PER PART 3 OF ECRA 5341-01220 ON OR BEFORE 17SEP2020. PLANNING - [SDR CALA2018012100270](https://openairdocs.org/sdr/CALA2018012100270.md): Wire Harness · damaged · Jan 21, 2018 · N472UA · Airbus A320232 · Light System Wiring > SEAT 34C EMERGENCY LIGHT IS INOPERATIVE. REPLACED THE SEAT WIRE HARNESS AND OPS CHECKED GOOD. - [SDR CALA2017100603505](https://openairdocs.org/sdr/CALA2017100603505.md): Slide · malfunctioned · Oct 6, 2017 · N472UA · Airbus A320232 · Escape Slide > L1 DOOR WILL NOT ARM. REMOVED AND REPLACED THE DOOR SLIDE PACK IAW AMM 25-62-44. OPS CHECKED GOOD. - [SDR CALA2017100603504](https://openairdocs.org/sdr/CALA2017100603504.md): Harness · no test · Oct 6, 2017 · N472UA · Airbus A320232 · Equipment/Furnishings Wiring > EMERGENCY EXIT LIGHTS MESSAGE OF ESPU EXT LOAD EMER L. FOUND THE R1 DOOR SLIDE PACK HARNESS FAULTED. REMOVED AND REPLACED THE R1 DOOR SLIDE PACK ASSY IAW 25-62-44-400- 803-A. EMERGENCY LIGHT SYSTEM TESTED NORMAL, NO FAULTS NOTED - [SDR CALA2017100203419](https://openairdocs.org/sdr/CALA2017100203419.md): Power Supply · inoperative · Oct 2, 2017 · N472UA · Airbus A320232 · Emergency Lighting > EMERGENCY LIGHT HAD A FAILURE MESSAGE OF THE ESPU BATTERY. REPLACED ESPU IAW AMM 33-51-38-000-001, 33-51-38-400-001. REPLAC ED BATTERY IAW AMM 33-51-38-000-002, 33-51-38-400-002. OPS CHECKED OK. - [SDR CALA2017092203301](https://openairdocs.org/sdr/CALA2017092203301.md): Flashlight · broken · Sep 22, 2017 · N472UA · Airbus A320232 · Emergency Equipment > DOOR 2L LT JUMPSEAT AFT EMER FLASHLIGHT FELLOUT OF ITS BRACKET. RED LIGHT IS NOT FLASHING. REMOVED & INSTALLED SERVICEABLE EMERGENCY FLASHLIGHT AT DOOR 2L. NO FAULTS NOTED. - [SDR CALA2017042101081](https://openairdocs.org/sdr/CALA2017042101081.md): Battery Pack · faulted · Apr 21, 2017 · N472UA · Airbus A320232 · Emergency Lighting > FOUND ON RON CHECK. FWD AND AFT LEFT EEL BATTERY PACK FAULTS. REPLACED FWD AND AFT EEL BATTERY PACKS. OPS CHECKED NORMAL. - [SDR CALA2017011600127](https://openairdocs.org/sdr/CALA2017011600127.md): Battery · discharged · Jan 16, 2017 · N472UA · Airbus A320232 · Emergency Lighting > DURING EMERG LIGHT TEST FAULTED LT & RT AFT EPSU. REPLACED LT & RT AFT EPSU BATTERY PACKS, TEST OK. - [SDR CALA2017011600126](https://openairdocs.org/sdr/CALA2017011600126.md): Battery · not seated · Jan 16, 2017 · N472UA · Airbus A320232 · Emergency Lighting > WHILE TESTING EMERGENGY LIGHT SYSTEM, LEFT FWD EPSU BATTERY FAULTED AND WILL NOT TEST. HAD FWD LEFT EPSU FAULT, RESEATED EPSU BATTERY, TEST OK. - [SDR CALA2016051895373](https://openairdocs.org/sdr/CALA2016051895373.md): Warning System · false activation · May 15, 2016 · N472UA · Airbus A320232 · Smoke Detection > SMOKE FOR AFT CARGO COMPARTMENT WARNING WITH FIRE BOTTLE DISCHARGE. ACFT DIVERTED DUE TO WEATHER. PERFORMED OPERATIONS TEST OF CARGO FIRE EXTINGUISHER SYS, CHECKED ALL NORMAL IAW AMM 26-23-00. R & R FIRE BOTTLE. - [SDR CALA2015060893871](https://openairdocs.org/sdr/CALA2015060893871.md): Latch · out of adjust · Jun 5, 2015 · N472UA · Airbus A320232 · Passenger Oxygen System > ROWS 10ABC & 12ABC O2MASKS DROPPED, WILL NOT STOW DUE TO LATCH BROKEN. ADJUSTED O2 PANELS 10ABC, 12ABC LATCHES. OPENED SAME O2 MASK COMPARTMENTS & REPACKED MASKS IAW MT35-002. OPERATIONS CHECK MAN MASK RLS IAW AMM 35-23-00-710-001. OPERATIONS CHECKED GOOD. - [SDR CALA2015011392940](https://openairdocs.org/sdr/CALA2015011392940.md): Door Sill · corroded · Jan 10, 2015 · N472UA · Airbus A320232 · Fuselage Miscellaneous Structure > CORROSION ON R2 DOOR SILL BEAM AROUND AFT FLOORBOARD NUTPLATE HOLES. BLENDED CORROSION ON AFT FLOORBOARD NUT PLATE HOLES & INSTALLED REPAIR IAW SRM 53 -41-14 FIG 201PARA 5A PRINCIPLE 5. - [SDR CALA2015010992915](https://openairdocs.org/sdr/CALA2015010992915.md): Door Sill · corroded · Jan 7, 2015 · N472UA · Airbus A320232 · Fuselage Miscellaneous Structure > CORROSION ON L2 DOOR SILL BEAM AROUND AFT FLOORBOARD NUTPLATE HOLE. REMOVED CORROSION ON AFT NU PLATE HOLE. FABRICATED & INSTALLED TOPCOAT REPAIR & FASTENERS IAW SRM 53-41-14 REPAIR 5 FIG 201 SH3 PRINCIPLE F 40. - [SDR CALA2014102192543](https://openairdocs.org/sdr/CALA2014102192543.md): Light · malfunctioned · Oct 19, 2014 · N472UA · Airbus A320232 · Emergency Lighting > EMERGENCY LIGHT TEST FAILED, EPSU BATTERY AFT. CYCLED EMER LIGHT CB`S CHECKED OK IAW AMM 33-51-00-710-001-A. - [SDR CALA2014041490816](https://openairdocs.org/sdr/CALA2014041490816.md): Igniter · faulty · Apr 12, 2014 · N472UA · Airbus A320232 · APU Start/Ignition System > ECAM MSG APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN, APU. APU AUTO SHUTDOWN ON TWO ATTEMPTED STARTS. PLACED ON MEL 49-10B. SHOWS IGNITION & FUEL CONTROL FAULT. TROUBLE SHOT APU TO PLUGS IAW THE MX MSG. R & R APU IGNITER PLUGS IAW AMM 49-41-41. - [SDR CALA2014032490678](https://openairdocs.org/sdr/CALA2014032490678.md): Unknown · leaking · Mar 24, 2014 · N472UA · Airbus A320232 · Turbine Engine Oil System > GROUND UNDER ENG 2 IS WET WITH WHAT APPEARS TO BE OIL, DROPS HANGING OFF ENG. - [SDR CALA2014030390506](https://openairdocs.org/sdr/CALA2014030390506.md): Seal · unsecure · Mar 2, 2014 · N472UA · Airbus A320232 · Engine Thrust Reverser > SEAL HANGING OUT OF NR 1 ENG REVERSER SHROUD. OPENED FAN COWL, ABLE TO MANUALLY EXTEND THE REVERSER ENOUGH TO RE SEAT THE BULB SEAL IN ITS TRACK. RETRACED REVERSER TO PROPER OPERATING POSITION, HCU IN NORMAL FUNCTION MODE. FAN COWLING CLOSED & SECURED, OK T - [SDR CALA2013111993052](https://openairdocs.org/sdr/CALA2013111993052.md): Cone · cracked · Nov 17, 2013 · N472UA · Airbus A320232 · Engine Collector/Tailpipe/Nozzle > NR 1 ENG EXHAUST CONE CRACKED. IAW MM 78-11-12-200-011-B FOR ALLOWABLE LIMITS. HAS MULTIPLE EXTENDING PASSED PREVIOUS STOP DRILLS HAVE CRACK EXCEEDING 6IN ZONE 1 REJECTING TAIL CONE. REPLACED TAIL CONE IAW MM. - [SDR CALA2013111592960](https://openairdocs.org/sdr/CALA2013111592960.md): Light · defective · Nov 14, 2013 · N472UA · Airbus A320232 · Exterior Lighting > RT WING NAV 2 POSITION LIGHT BLINKING BLUE INDICATOR NEOL. REPLACED LAMP ASSEMBLY 565-1601 NR 2 POSITION RT. - [SDR CALA2013103092511](https://openairdocs.org/sdr/CALA2013103092511.md): Light · inoperative · Oct 29, 2013 · N472UA · Airbus A320232 · Exterior Lighting > NOSE GEAR TAXI LIGHT SYSTEMS INOPERATIVE. - [SDR CALA2013090591004](https://openairdocs.org/sdr/CALA2013090591004.md): Trim Panel · unsecure · Sep 3, 2013 · N472UA · Airbus A320232 · Passenger Compartment Equipment > FWD GALLEY FLOOR MOLDING TORN UP. ATTACHED FLOOR MOLDING. Next page: https://openairdocs.org/aircraft/N472UA/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N472UA' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N472UA/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.