# Service difficulty reports: N430UA

A list on [N430UA](https://openairdocs.org/aircraft/N430UA.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 · 116 reports

- [SDR CALA2026101220279](https://openairdocs.org/sdr/CALA2026101220279.md): Display · faulted · Oct 10, 2026 · N430UA · Airbus A320232 · Central Display
  > CAPTAINS PFD FAILED AT ROTATION SCREEN CAME ALIVE UPONLANDING. REMOVED AND REPLACED CAPT PFD AND RELAY 20WT1. OPS CHECK NORMAL IAW AMM 31-63-22-400-001-A.
- [SDR CALA2026060516847](https://openairdocs.org/sdr/CALA2026060516847.md): Fuel Cap · missing · Jun 2, 2026 · N430UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING. NO LEAKS AT COUPLING AND INSTALLED PLACARD 911288
- [SDR CALA2025082708178](https://openairdocs.org/sdr/CALA2025082708178.md): Warning Light · false activation · Aug 23, 2025 · N430UA · Airbus A320232 · Door Warning System
  > FWD CARGO DOOR ECAM ON LANDING ROLLOUT PLACING BACK ON MEL BECAUSE OF EXTENSIVE HISTORY. REQUESTING MEL 5270J NOC MEL 5270J APPROVED PLA APPLIED. DDP C/W. *DM* AWM 31-54-46 INSPECT WIRES TO PROX SWITCH FOR CONDITION. CHECK WIRES WITHIN HARNESS 4613VB. ALSO SEE
- [SDR CALA2025081507828](https://openairdocs.org/sdr/CALA2025081507828.md): Sensor · out of adjust · Aug 15, 2025 · N430UA · Airbus A320232 · Door Warning System
  > REPEAT LEVEL 2 CHRONIC FWD CARGO DOOR ECAM, WIRE HARNESS, 28WV, AND 30WV SENSORS HAVE BEEN REPLACED, SENSOR GAPS HAVE BEEN CHECKED SEVERAL TIMES, PROBLEM SEEMS TO HAPPEN A LOT ON TAXI WHEN A/C IS SHAKING, REF TSM 52-31-00-810-801-A. CLOSE AND LATCH THE DOOR AN
- [SDR CALA2025080607366](https://openairdocs.org/sdr/CALA2025080607366.md): Wire Harness · faulted · Aug 1, 2025 · N430UA · Airbus A320232 · Door System Wiring
  > LEVEL 2 CHRONIC FWD CARGO DOOR DISPLAYED ON UPPER ECAM. AVIATAR IS NOT REPORTING ANY CORRELATED CMS FAILURE MESSAGES. SENSORS 28 WV AND 30WV HAVE BEEN REPLACED & ADJUSTED MULTIPLE TIMES. INSPECTED FWD CARGO DOOR HANDLE LATCH ASSY & HOOK, NO DEFECTS FOUND,
- [SDR CALA2025071806709](https://openairdocs.org/sdr/CALA2025071806709.md): Seal · broken · Jul 17, 2025 · N430UA · Airbus A320232 · Nacelle/Pylon, Main Frame
  > FOUND ENGINE NR 1 FWD PYLON TO NACELLE PROFILES PANEL BROKEN. INSTALLED E#1 FWD PYLON TO NACELLE PROFILES PANEL REFERENCE AMM TASK 54-57-22-400-003-A.
- [SDR CALA2025071606633](https://openairdocs.org/sdr/CALA2025071606633.md): Proximity Switch · faulted · Jul 4, 2025 · N430UA · Airbus A320232 · Door Warning System
  > DOOR FWD CARGO ECAM 2 TIMES ON GND DURING BRAKING. PRESS NORMAL IN FLT. PLACED FWD CARGO INDICATION ON MEL 5270U. DOOR WAS VISUALLY CHECKED & CONFIRMED CLOSED & LATCHED FOR DEPARTURE. PROXIMITY SWITCH WAS REPLACED. INSPECT WIRES TO PROXIMITY SWITCH FOR CO
- [SDR CALA2025062605880](https://openairdocs.org/sdr/CALA2025062605880.md): Proximity Sensor · faulted · Jun 23, 2025 · N430UA · Airbus A320232 · Door Warning System
  > DOOR FWD CARGO ECAM ON LANDING ROLLOUT - WENT AWAY AT 80 KTS R/R FWD CARGO DOOR PROXIMITY SENSOR IAW IPC 52-71-02. ALL INDICATION OP CHECK NORMAL ON ECAM WHEN OPENING AND CLOSING DOOR
- [SDR CALA2024061700010](https://openairdocs.org/sdr/CALA2024061700010.md): Module · faulted · Jun 17, 2024 · N430UA · Airbus A320232 · Flight Control System
  > ERRONEOUS OVERSPEEDWARNING DURING FLAPRETRACTIONVMO WARNING AFTE R THAT PER CREW VERBAL WAS BELOW OVERSPEED BY 6 KNOTS ON CLIMB AND DECENT, GROUND TEST RESULTS, FOUND ADM 19FP3 DISCONNECTED FROM PITOT LINE.,
- [SDR CALA2024061701821](https://openairdocs.org/sdr/CALA2024061701821.md): Connector · disconnected · Jun 13, 2024 · N430UA · Airbus A320232 · Navigation System Wiring
  > ERRONEOUS OVERSPEED WARNING DURING FLAP RETRACTION VMO WARNING AFTE R THAT PER CREW VERBAL WAS BELOW OVERSPEED BY 6 KNOTS ON CLIMB AND FOUND ADM 19FP3 DISCONNECTED FROM PITOT LINE.
- [SDR CALA2024061301789](https://openairdocs.org/sdr/CALA2024061301789.md): Bracket · sheared · Jun 11, 2024 · N430UA · Airbus A320232 · Landing Gear Doors
  > LT MLG FWD DOOR FITTING HAS 2EA SHEARED FASTNER. REMOVED AND REPLACED LH MLG FWD DOOR HINGE FITTING IAW REPAIR IN STRUCTION R 533 70500 F.
- [SDR CALA2024031800771](https://openairdocs.org/sdr/CALA2024031800771.md): Proximity Sensor · intermittent · Mar 14, 2024 · N430UA · Airbus A320232 · Landing Gear Position and Warning
  > L/G/SHOCK ABSORBERFAULT ECAM. LOSS OFAUTO PILOT/THRUST. POST FLIGHT REPORT FAULTS N LG EXT PROX SENSOR 25GA AND N LG SHOCK ABSORBER 2526GM. VISUAL INSPECTION OF 25GA CHECKS NORMAL. REF TSM 32-31-00-810-815-A AND TSM 32-31-00-810-868-A. PIC INCLUDED OF POST FLT
- [SDR CALA2023102703205](https://openairdocs.org/sdr/CALA2023102703205.md): Door · warning message · Oct 24, 2023 · N430UA · Airbus A320232 · Cargo/Baggage Doors
  > AFT CARGO DISPLAYED ON UPPER ECAM SCREEN. - DOOR AFT CARGO DOOR SHOWED OPEN DURING FLIGHT. PERFORMED OPERATIONAL TEST OF AFT CARGO DOOR REF AMM 52-32-00-710-001-A. FOUND 2 SCREWS WHERE THE DOOR HANDLE ATTACHES TO THE LEVER ASSY VERY LOOSE CAUSING THE DOOR HAND
- [SDR CALA2023080202413](https://openairdocs.org/sdr/CALA2023080202413.md): Slide · unwanted deploy · Jul 30, 2023 · N430UA · Airbus A320232 · Escape Slide
  > DOOR 1L SLIDE DEPLOYED AT GATE. ITEM LOCKED FOR MAINT FERRY TO ORD, UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. UNLOCKING TO CLEAR ACCOMPLISHED INSTALLATION INSPECTION OF 1L ESCAPE SLIDE IAW AMM 25-62-44 OPS CHE
- [SDR CALA2023071702271](https://openairdocs.org/sdr/CALA2023071702271.md): Window · cracked · Jul 13, 2023 · N430UA · Airbus A320232 · Flight Compartment Windows
  > CRACKED/FAILED CAPTSLIDING COCKPIT WINDOW UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE EFS USING VENDOR MAA SCREEN UPDATED MAA CODE EFS USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING
- [SDR CALA2023022700562](https://openairdocs.org/sdr/CALA2023022700562.md): None · none · Feb 27, 2023 · N430UA · Airbus A320232 · Electrical Power System
  > EXTERNAL PWR RECPTACLE NOT ACCEPTING GND PWR DISCONNECTED EXTERNAL POWER RECEPTACLE AND INSPECTED FOR DAMAGE. RECONNECTED POWER RECEPTACLE TO ACFT, ACFT SHOWS POWER AVAILABLE AND OPERATES NORMAL AT THIS TIME. REF. AMM 24-41-00
- [SDR CALA2023020100304](https://openairdocs.org/sdr/CALA2023020100304.md): Power Supply · none · Feb 1, 2023 · N430UA · Airbus A320232 · Emergency Lighting
  > RIGHT EMERGENCY OVERWING LIGHT POWER SUPPLY IS FAULTING. REPLACED RIGHT EMERGENCY POWER SUPPLY BOX PER AMM33-51-38, OPS CHECKED GOOD PARTS USED: 1103737,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1103737 SN OFF 9557 POWER SUPPLY, C OFF 31-3350-9-9001
- [SDR CALA2022122103452](https://openairdocs.org/sdr/CALA2022122103452.md): Controller · faulted · Dec 20, 2022 · N430UA · Airbus A320232 · Drag Control System
  > FCTL SPLR FAULT AT CRZ SPLRS APPEAR FLUSH, INOP SYS SPLR 5 INSPECTED WIRING AT NR 5 SPOILER ACTUATORS, NO DAMAGE FOUND. VERIFIED INSTALLATION OF #5 SPOILER, SAFETY AND SECURITY OF COMPONENT UP TO 4 C 9 IAW GMM 09-25-05. ACCOMPLISHED CONTINUITY CHECKS AND MEGG
- [SDR CALA2022071301718](https://openairdocs.org/sdr/CALA2022071301718.md): Fitting · none · Jul 12, 2022 · N430UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > REF LP:8983603 R/MLG KEEL BEAM AFT REINFORCEMENT FITTING WEB HOLES R75 ELONGATE D AND R76 DOUBLE DRILLED. BEAM HOLES. PLANNING TO CONTACT ENGINEERING AFTER 22MAY2023 BUT INSTRUCTIONS" BEFORE 01JUN2023 FOR THE ECRA 5330-06960 PART 3 PERMANENT REPAIR INTERIM REP
- [SDR CALA2022071101705](https://openairdocs.org/sdr/CALA2022071101705.md): Frame · cracked · Jul 10, 2022 · N430UA · Airbus A320232 · Fuselage Main, Frame
  > L/H FR35 STGR 28-31 HOLE #2 HAS A CRACK INDICATION IN FRAME LAYE R AT THE 1 O''CLOCK POSITION ON HAECO LCQ REF 9294155/20155 AD RE LATED TASK AD 2016-14-03. NR GENERATED BY V061632 FOLLOWS "ACCOMPLISH A PERMANENT REPAIR ON THE HOLES AT FR35 OR BEFORE 06-JAN-23
- [SDR CALA2022071101704](https://openairdocs.org/sdr/CALA2022071101704.md): None · cracked · Jul 10, 2022 · N430UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FR36 PRESSURE DECK BETWEEN LH765 & 1523, HOLES 2,4,5,6,9,10,11,1 2,13,14,15,16 HAVE CRACK INDICATIONS IN PRESSURE DECK LAYER ON H AECO LCQ REF 9294636/30636 AD RELATED SUPPORT TASK. NR GENERATED BY V892444 WORK RECORDED & DIPS CARRIED ON LOG PAGES 9026593 AND
- [SDR CALA2022071101703](https://openairdocs.org/sdr/CALA2022071101703.md): Frame · cracked · Jul 9, 2022 · N430UA · Airbus A320232 · Fuselage Structure (General)
  > RH FR35 STR30 HOLE #2 HAS A CRACK INDICATION IN FRAME LAYER AT THE 4 O''CLOCK POSITION. AS FOLLOWS "ACCOMPLISH PERMANENT REPAIR AT RH FR35 STR30 HOLE #2 OR BEFORE 06JAN2023." INSP:LC19 PER PART 3 OF THE LATEST OF THE REVISION OF ECRA 5331-02922 ON PERFORMED IN
- [SDR CALA2022071101702](https://openairdocs.org/sdr/CALA2022071101702.md): Panel · cracked · Jul 9, 2022 · N430UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FR36 PRESSURE DECK BETWEEN LH 765 AND RH, HOLES 2,4,10,11,13,15, 16,19,20,21,24,29,31,32,40 HAVE CRACK IN PRESSURE DECK LAYER GEN ERATED BY V892444 AT HAECO LCQ PER NR 9294638 (30638) AD RELATED SUPPORT TASK INTERIM REPAIR PERFORMED ON FR36 PRESSURE DECK BETWE
- [SDR CALA2022071101701](https://openairdocs.org/sdr/CALA2022071101701.md): Pressure Deck · cracked · Jul 9, 2022 · N430UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FR36 PRESSURE DECK BETWEEN RH 765 AND RH 1523, HOLES 5,10,12,13, 14,15,16,17,18 HAVE CRACK INDICATIONS IN PRESSURE DECK LAYER AD RELATED SUPPORT TASK, GENERATED BY V892444 AT HAECO LCQ PER NR 9 294640 (30640) 1-7 FOR AFFECTED HOLE LOCATIONS. PER PART 1 STEP.2
- [SDR CALA2022070801687](https://openairdocs.org/sdr/CALA2022070801687.md): Frame · cracked · Jul 7, 2022 · N430UA · Airbus A320232 · Fuselage Main, Frame
  > LH FR 68, STGR 22 WEB, HORIZONTAL FLANGE RADIUS AFT SIDE OF FRAM E, HAS A CRACK INDICATION AT LOWER SURFACE 1.25" LONG, FROM BELO W RADIUS INTO INBD CAP, TO OTBD DIRECTION. GENERATED BY V061671 ON HAECO LCQ NR 9294408/30408 CCOMPLISH INITIAL INSPECTIONS ON FRA
- [SDR CALA2022070801686](https://openairdocs.org/sdr/CALA2022070801686.md): Fitting · damaged · Jul 7, 2022 · N430UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LH KEEL BEAM & MLG DOOR FITTING HAS DISCREPANT HOLES. LOCATIONS & DETAILS. PER PART 1.2 OF ECRA "ACCOMPLISH A PART 3 OF LATEST REVISION OF ECRA 5330-06961 ON OR BEFORE PERMANENT REPAIR OF THE LH MLG DOOR FITTING KEEL BEAM HOLES PER 24-JUN-2023." PERFORMED INT
- [SDR CALA2022070801685](https://openairdocs.org/sdr/CALA2022070801685.md): Frame · cracked · Jul 7, 2022 · N430UA · Airbus A320232 · Fuselage Main, Frame
  > RH FR 68, STGR 22 WEB, HORIZONTAL FLANGE RADIUS AFT SIDE OF FRAME, HAS A CRACK INDICATION AT LOWER SURFACE.535" LONG, STATING FROM INBD CAP, TO OTBD DIRECTION. GENERATED BY V061671 ON HAECO L CQ NR 9294409/30409 TION ON FRAME REPAIR PART FILLET RADII AND FAST
- [SDR CALA2022062901601](https://openairdocs.org/sdr/CALA2022062901601.md): Intercostal · cracked · Jun 28, 2022 · N430UA · Airbus A320232 · Fuselage Main, Frame
  > L/H Y+1292 FR 11-8" HAS CRACKED WEB. GENERATED AT HAECO LCQ PER NR 9294798 (30798) BY V061673. {SUPPORT TASK} REPAIRED CRACKED WEB AT L/H Y+1292 FR 11-8 IAW A320 SRM 53-11-14 -300-005. PERFORMED BY V929087 INSP BY V919150.
- [SDR CALA2022062801598](https://openairdocs.org/sdr/CALA2022062801598.md): Angle · cracked · Jun 27, 2022 · N430UA · Airbus A320232 · Emergency Exits
  > R/H AFT EMERGENCY EXIT DOOR FORWARD SUPPORT ANGLE HAS CRACK. AT HAECO LCQ NON-ROUTINE CARD 9294699/30699 GENERATED BY V061771. D OT: RR131 REMOVED AND REPLACED SUPPORT ANGLE ON RIGHT HAND AFT EXIT DOOR I AW A320 SRM 51-42-11 & SRM 51-72-11 PER MECH V052030 IN
- [SDR CALA2022061701520](https://openairdocs.org/sdr/CALA2022061701520.md): Angle · cracked · Jun 16, 2022 · N430UA · Airbus A320232 · Emergency Exits
  > SUPPORT TASK: L/H FORWARD EMERGENCY EXIT DOOR FORWARD SUPPORT AN GLE HAS CRACK. DOT: RR128. AT HAECO LCQ NON-ROUTINE 9294696/3069 6 GENERATED BY V061771. REMOVED AND REPLACED SUPPORT ANGLE ON LH EMERGENCY EXIT DOOR IAW A320 SRM 51-42-11 & 51-72-11. REMOVED DOT
- [SDR CALA2022060801459](https://openairdocs.org/sdr/CALA2022060801459.md): Stringer Splice · corroded · Jun 7, 2022 · N430UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FWD CARGO STRINGER SPLICE AT FR33/34 STR39L HAS CORROSION. DOT: 20 GENERATED BY N078570 AT HAECO LCQ PER NR 9294617 (30617) SUPP ORT TASK REMOVED AND REPLACED FWD CARGO STRINGER SPLICE-COUPLING AT STRG 39L BETWEEN FR33 AND FR34 IAW A320 SRM 51-72-11-911-001. N
- [SDR CALA2022060101410](https://openairdocs.org/sdr/CALA2022060101410.md): Intercostal · cracked · May 31, 2022 · N430UA · Airbus A320232 · Emergency Exits
  > RH AFT EMERGENCY EXIT DOOR AFT SUPPORT ANGLE HAS CRACK SUPPORT GENERATED BY V061771 AT HAECO LCQ PER NR 9294700 REMOVED AND REPLACED SUPPORT ANGLE ON AFT EXIT DOOR IAW A320 SRM 51-42-11 & 51-72-11. PERFORMED BY V052030 INSP BY V892285
- [SDR CALA2022060101409](https://openairdocs.org/sdr/CALA2022060101409.md): Support Angle · cracked · May 31, 2022 · N430UA · Airbus A320232 · Emergency Exits
  > LH FWD EMERGENCY EXIT DOOR AFT SUPPORT ANGLE HAS CRACK SUPPORT T ASK GENERATED BY V061771 AT HAECO LCQ PER NR 9294697/30697 REMOVED AND REPLACED SUPPORT ANGLE ON EXIT DOOR LH AFT IAW A320 SRM 51-42-11 & SRM 51-72-11 PERFORMED BY V052030 INSP BY V892285
- [SDR CALA2022053001379](https://openairdocs.org/sdr/CALA2022053001379.md): Fitting · corroded · May 28, 2022 · N430UA · Airbus A320232 · Fuselage Main, Floor Beam
  > R2 DOOR SILL FWD CORNER FITTING HAS CORROSION SPOTS DOT:M072 (A3 NB-05-3-6059) GENERATED BY V919150 AT HAECO LCQ PER NR 9294532 ( 30532) REMOVED AND REPLACED FWD CORNER 19HING ON R2 DOOR SILL IAW A320 SRM 51-42-11 AND SRM 51-72-11 PERFORMED BY V052030 INSP BY
- [SDR CALA2022052501330](https://openairdocs.org/sdr/CALA2022052501330.md): Stringer · corroded · May 23, 2022 · N430UA · Airbus A320232 · Fuselage Structure (General)
  > EVIDENCE OF CORROSION AFT CARGO STR 43L FR64-65 AT HAECO LCQ NON ROUTINE 9294478/30478 GENERATED BY V052040 SPEC (A3NB-05-3-6026) REMOVED AND REPLACED AFT CARGO STR 43L FR64-65 IAW A320 SRM 53-4 BY V892285 1-13-283-002. INSTALLED 25 EA FASTENERS AND INSTALLED
- [SDR CALA2017041400992](https://openairdocs.org/sdr/CALA2017041400992.md): Battery · inoperative · Apr 14, 2017 · N430UA · Airbus A320232 · Emergency Equipment
  > FLT DECK EMER FLASHLIGHT NOT BLINKING. REPLACED BATTERY IN EMER FLASHLIGHT @ FLT DECK AND APPLIED NEW SEAL. OPS GOOD.
- [SDR CALA2017041400991](https://openairdocs.org/sdr/CALA2017041400991.md): Flashlight · unsecure · Apr 14, 2017 · N430UA · Airbus A320232 · Emergency Equipment
  > AFT CABIN FLASHLIGHT AFT CABIN WAS PULLED OUT OF HOLDER. INDICATOR LIGHT NOT FLASHING REPLACED BATTERY AT AFT OTBD EMER FLASHLIGHT AND RESEALED. OPS GOOD.
- [SDR CALA2015080794181](https://openairdocs.org/sdr/CALA2015080794181.md): Battery · failed · Aug 2, 2015 · N430UA · Airbus A320232 · Emergency Lighting
  > IAW A CHECK J C 4-2025 ITEM 27, CABIN EMER LIGHTING CHECK FAILS BATTERY AFT LT. REPLACED BATTERY, TEST RESPONSE PASSED.
- [SDR CALA2014060291189](https://openairdocs.org/sdr/CALA2014060291189.md): Proximity Switch · dirty · May 28, 2014 · N430UA · Airbus A320232 · Door Warning System
  > DOOR 1L NOT SHOWING ARMED. VERIFIED DOOR CLOSED & ARMED PRIOR TO DEPARTURE. CLEANED PROXIMITY SWITCH 4WN1 SYS CHECK NORMAL.
- [SDR CALA2013123094002](https://openairdocs.org/sdr/CALA2013123094002.md): Warning System · activated · Dec 29, 2013 · N430UA · Airbus A320232 · Hydraulic Indicating System
  > HYD RAT FAULT INDICATED ON UPPER ECAM SCREEN. RAT OUT MESSAGE INDICATED ALSO. DISCONNECTED ELECTRICAL CONNECTOR 2454GE-C.
- [SDR CALA2013121293639](https://openairdocs.org/sdr/CALA2013121293639.md): Control Unit · inoperative · Dec 11, 2013 · N430UA · Airbus A320232 · Smoke Detection
  > SMOKE DETECTOR CONTROL SYSTEM INOPERATIVE. REPLACED SDCU IAW AMM 26-17-34. OPERATIONS TESTED OKAY.
- [SDR CALA2013092791507](https://openairdocs.org/sdr/CALA2013092791507.md): Oxygen Mask · unsecure · Sep 27, 2013 · N430UA · Airbus A320232 · Passenger Oxygen System
  > 20 ABC OXY MASKS HANGING. RESTOWED MASKS ROW 20ABC IAW MX TIP 35-003. REQUIRES MAN MASK RELEASE OPERATIONS CHECKED IAW AMM 35-2 3-00-710-001 WITHIN 3 DAYS. ACCOMPLISHED ACPD OPERATIONAL TEST OXY GEN MASK IAW AMM 35-23-00 OK.
- [SDR CALA2013092391372](https://openairdocs.org/sdr/CALA2013092391372.md): Oxygen Mask · unsecure · Sep 22, 2013 · N430UA · Airbus A320232 · Passenger Oxygen System
  > O2 MASK DROPPED AT 29 DEF. SECURED O2 MASK AT 29 DEF. REPACKED & ENSURE LATCH FULL ENGAGED IAW MT35-003.
- [SDR CALA2013081990525](https://openairdocs.org/sdr/CALA2013081990525.md): Engine · making metal · Aug 17, 2013 · N430UA · Airbus A320232 · APU Core Engine
  > APU AUTO SHUTDOWN WITH SMOKE REPORTED AND VIBRATION FELT IN COCKPIT. REMOVED APU MAG CHIP DECTECTORS AND FOUND A LARGE DEPOSIT OF METAL FLAKES. SUGGEST APU CHANGE. METAL FLAKES BEYOND LIMITS IAW 49-91-42. APU PN MR49206.
- [SDR UALA2013053003767](https://openairdocs.org/sdr/UALA2013053003767.md): Cap · missing · May 29, 2013 · N430UA · Airbus A320232 · Smoke Detection
  > PUSH BUTTON CAP FOR CARGO SMOKE TEST IS MISSING. JUST POST FOR CAP USEABLE. REPLACED CARGO SMOKE TEST BUTTON CAP.
- [SDR UALA2013052303566](https://openairdocs.org/sdr/UALA2013052303566.md): Control Panel · failed · May 22, 2013 · N430UA · Airbus A320232 · Weather Radar System
  > NO CAPTAIN`S SIDE RADAR DISPLAY, FIRST OFFICER`S SIDE OK. REPLACED WEATHER TRANSCIEVER IAW MM. ALSO REPLACED WEATHER CONTROL PANEL. FOUND LOOSE PARTS INSIDE CONTROL PANEL. NEW CONTROL PANEL CHECKED NORMAL AT GATE. WEATHER PAINTS ON BOTH DISPLAYS.
- [SDR UALA2013040802301](https://openairdocs.org/sdr/UALA2013040802301.md): Valve · failed · Apr 6, 2013 · N430UA · Airbus A320232 · Cabin Temperature Control System
  > CABIN TEMP, ALL ZONES EXTREMELY ERRATIC AND IMPOSSIBLE TO CONTROL. ROAMS TO EXTREME. REPLACED HOT AIR PRESSURE REGULATING VALVE. OPS CHECKED GOOD.
- [SDR UALA2013032802000](https://openairdocs.org/sdr/UALA2013032802000.md): Liner · damaged · Mar 28, 2013 · N430UA · Airbus A320232 · Turbine Engine Compressor Section
  > PIECE OF HONEYCOMB RUB STRIP MISSING ON NR 2 ENGINE AT 6:00 AND 6:30 POSITIONS. REPAIRED FAN CASE ATTRITION LINER AT 6:00 AND 6:30 POSITIONS PER MT 72-017 REV E.
- [SDR UALA2013031901662](https://openairdocs.org/sdr/UALA2013031901662.md): Liner · damaged · Mar 17, 2013 · N430UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE A QUARTER SIZE PIECE OF ATTRITION LINER MATERIAL MISSING. REPAIRED ATTRITION LINER REPAIR.
- [SDR UALA2013030501308](https://openairdocs.org/sdr/UALA2013030501308.md): Controller · faulty · Mar 4, 2013 · N430UA · Airbus A320232 · Waste Disposal System
  > CREW REFUSAL. MUST FIX DF0451 PRIOR TO DEPARTURE. TOILET VACUUM MOTOR STARTED RUNNING CONTINUOUSLY AFTER TAKEOFF. REMOVED AND REPLACED LAV BLOWER MOTOR CONTROLLER.

Next page: https://openairdocs.org/aircraft/N430UA/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 = 'N430UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N430UA/reports

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