# Service difficulty reports: N460UA

A list on [N460UA](https://openairdocs.org/aircraft/N460UA.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 · 101 reports

- [SDR CALA2025091008740](https://openairdocs.org/sdr/CALA2025091008740.md): Battery · no test · Sep 9, 2025 · N460UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGTH TEST SHOWING EPSU BATTERY EMER R, EPSU BATTERY EMER L, AND AFT L DURING SERVICE CHECK 2. RESET CB ON 49VU H5, H6 AND 122VU V7, PERFORMED CIDS EMERGENCY LIGHT TEST AND JUST HAVE EPSU BATTERY EMER R ON CIDS DISPLAY. ALL WORK PERFORMED IN REFER T
- [SDR CALA2025081807878](https://openairdocs.org/sdr/CALA2025081807878.md): Warning System · false indication · Aug 16, 2025 · N460UA · Airbus A320232 · Door Warning System
  > FA REPORTS EMERGENCY EXIT DOOR 2L INDICATES ARMED BUT LOCK INDICATION MISALIGNED ARMED, DISARMED AND REARMED DOOR 2L INSPECTED DOOR NO MISALIGNMENT SHOWN IN LOCK INDICATION. ECAM SHOWS DOOR CLOSED IAW AMM 05-28-30-200-007-A
- [SDR CALA2025081307690](https://openairdocs.org/sdr/CALA2025081307690.md): Limiter · failed · Aug 11, 2025 · N460UA · Airbus A320232 · Auto Flight System
  > OPERATIONAL TEST OF THE RUDDER-TRAVEL LIMITING FUNCTION IAW AMM 22-61-00-710-001-A. PERFORMED OPS CHECK OF RUDDER TRAVEL LIMITING FUNCTION IAW AMM 22-61-00-710-001-A, OPS CHECK FAILED. CONTINUED TROUBLESHOOTING REF TSM LOSS OF THE RUDDER TRAVEL LIMITATION-FUN
- [SDR CALA2025050804560](https://openairdocs.org/sdr/CALA2025050804560.md): Cover · unsecure · May 6, 2025 · N460UA · Airbus A320232 · Escape Slide
  > TEST FLIGHT DISCREPANCY. R1 DOOR RATTLING NOISE DURING FLIGHT. RESECURE R-1 DOOR SLIDE COVER AND VERIFIED DOOR COVER INSULATION AND VISUAL INDICATOR AND ARMED INDICATOR IAW A320 MM 25-62-44-4 00-802-A STEPS 10,11, AND 12.
- [SDR CALA2025050504457](https://openairdocs.org/sdr/CALA2025050504457.md): Stringer · damaged · May 4, 2025 · N460UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 25L FR 21-24 HAS A PREVIOUS MISDRILLED HOLE. ACCOMPLISH REPAIR INSTRUCTIONS PER HAECO REO L25446 REV IR WITH NO DEVIATIONS/ECRA 5311-03356.
- [SDR CALA2025050504461](https://openairdocs.org/sdr/CALA2025050504461.md): Window Frame · cracked · May 3, 2025 · N460UA · Airbus A320232 · Fuselage Main, Structure
  > RH COCKPIT, SLIDING WINDOW, FWD LATCH AREA, MILLED RISER, UNDE R LATCH CRACKED. ACCOMPLISHED REPAIR PER HAECO REO-L25450 REV 1R WITH NO DEVIATIONS. INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-03359 TO RH FR4 VERTICAL STIFFENER.
- [SDR CALA2025050504452](https://openairdocs.org/sdr/CALA2025050504452.md): Cover · corroded · May 3, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > FWD PIT TORSION BOX COVER REQUIRES REPLACEMENT. REPLACED FWD PIT TORSION BOX COVER. REMOVED AND REPLACED FWD IT TORSION BOX COVER IAW A320 SRM 51-42 -11.
- [SDR CALA2025050504450](https://openairdocs.org/sdr/CALA2025050504450.md): Scuff Plate · gouged · May 2, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR CUTOUT THRESHOLD UNDER SCUFF PLATE HAS GOUGES/T OOLING MARKS 2 EA LOCATIONS. REMOVED AND REPLACED TORSION BOX COVER ON AFT CARGO DOOR CUTOUT IAW A320 SR, 51-72-11-911-001.
- [SDR CALA2025050204416](https://openairdocs.org/sdr/CALA2025050204416.md): Skin · cracked · May 1, 2025 · N460UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > L/H HOLE #2 AT FR 35 HAS BEEN PREVIOUSLY WORKED. ACCOMPLISHED REPAIR PER HAECO RCO-L25396 WITH NO DEVIATIONS. ACCOMPLISHED A PERMANENT REPAIR AT LH FR35 STA R30LH HOLE #2 PER PART 3 OF THE LATEST REVISION OF ECRA 5320-07500 ON OR BEFORE 22OCT2025. INTERIM RE
- [SDR CALA2025050204414](https://openairdocs.org/sdr/CALA2025050204414.md): Rib · corroded · May 1, 2025 · N460UA · Airbus A320232 · Wing, Rib/Bulkhead
  > LH WING T/E LOWER SURFACE PANEL LANDS AT RIB 23-27 HAVE EVIDENCE OF CORROSION. ACCOMPLISHED REPAIR INSTRUCTIONS PER HAECO REO-L25457 REV IR WIT H NO DEVIATIONS IAW A320 ECRA 5751-01560.
- [SDR CALA2025050204412](https://openairdocs.org/sdr/CALA2025050204412.md): Frame · cracked · May 1, 2025 · N460UA · Airbus A320232 · Fuselage Main, Frame
  > FRAME 68 RH AT STR 8 HAS CRACK INDICATION ON AFT FACE AT RADIUS OF FLANGE JUST ABOVE UPPERMOST FASTENER IN WEB, APPROX.50 INCH LONG. PREFORMED FRAME FITTING REPAIR AT FR68 RH STR8R IAW A320SRN53-41-12. W/P/B PERFORMED FRAME FITTING REPAIR AT FR68 RH STR8R
- [SDR CALA2025042404196](https://openairdocs.org/sdr/CALA2025042404196.md): Floor Support · damaged · Apr 23, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT THRESHOLD PLATE SUPPORT HAS ELONGATED HOLES. REMOVED & REPLACED AFT CARGO PIT THRESHOLD PLATE SUPPORT IAW A320 SRM 51-42-11/001.
- [SDR CALA2025041803987](https://openairdocs.org/sdr/CALA2025041803987.md): Flap Track · corroded · Apr 17, 2025 · N460UA · Airbus A320232 · Trailing Edge Flap Control System
  > LH WING O/B FLAP TRACK 4, RIB 15-16 INTERNAL DOUBLER HAS CORROSI ON AROUND FASTENERS AND EVIDENCE OF DEBOND ON MAIN STRUCTURE. REMOVE ONLY LH O/B FLAP FOR OVERHAUL. REMOVED AND REPLACED LH WING O/B FLAP IAW AMM TASK 27-54-62 -000-001-A AND AMM TASK 27-54-62
- [SDR CALA2025041803998](https://openairdocs.org/sdr/CALA2025041803998.md): Plate · corroded · Apr 16, 2025 · N460UA · Airbus A320232 · Rudder Structure
  > RUDDER TIP ATTACH POINT HOLES HAVE CORROSION DAMAGE ON BOTH SIDES. REMOVED AND REPLACED L/H AND R/H LIGHTNING PROTECTION PLATE IAW A320 35-41-14-300-008.
- [SDR CALA2025041503854](https://openairdocs.org/sdr/CALA2025041503854.md): Fitting · cracked · Apr 11, 2025 · N460UA · Airbus A320232 · Fuselage Main, Structure
  > LH AND RH CONTINUITY FITTINGS HAVE CRACK INDICATION. REMOVED AND REPLACED CONT FITTINGS IAW A320 R53112919/ SRM 51-42 -11.
- [SDR CALA2025041503853](https://openairdocs.org/sdr/CALA2025041503853.md): Door Sill · corroded · Apr 11, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > R2 SHAPE SILL FOUND TO BE OUT OF LIMITS REQUIRES REPLACEMENT. REMOVED AND REPLACED R2 SHAPE SILL IAW SRM A320 51-42-11/001
- [SDR CALA2025041503851](https://openairdocs.org/sdr/CALA2025041503851.md): Door Sill · corroded · Apr 11, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT WET AREA FLOOR R2 DOOR SILL AT FR 66 HAS CORROSION. EVALUATED CORROSION FOUND TO BE OUT OF LIMITS MORE THAN 50% IAW A320 SRM 53-41-14-283-002. REMOVED AND REPLACED R2 DOOR SILL AT F R 66 IAW A320 SRM 53-41-14-283-002 AND A320 SRM 51-42-11/001.
- [SDR CALA2025041503849](https://openairdocs.org/sdr/CALA2025041503849.md): Door Frame · cracked · Apr 9, 2025 · N460UA · Airbus A320232 · Fuselage Main, Structure
  > L/H AFT O/W ESCAPE HATCH,AFT VERT.FRAME APPEARS TO BE CRACKED. REMOVED AND REPLACED L/H AFT O/W ESCAPE HATCH AFT VERTICAL FRAME IAW A320 SRM 51-72-11-911-001 REMOVED AND REPLACED LH AFT O/W ESCAPE HATCH AFT VERTICAL FRAME IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2025041503848](https://openairdocs.org/sdr/CALA2025041503848.md): Door Frame · cracked · Apr 9, 2025 · N460UA · Airbus A320232 · Fuselage Main, Structure
  > L/H AFT O/W ESCAPE HATCH,FWD. VERT.FRAME APPEARS TO BE CRACKED. REMOVED AND REPLACED L/H AFT O/W ESCAPE HATCH FWD VERTICAL FRAME IAW A320 SRM 51-72-11-911-001. REMOVED AND REPLACED LH AFT O/W ESCAPE HATCH FWD VERTICAL FRAME IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2025040103383](https://openairdocs.org/sdr/CALA2025040103383.md): Door Sill · corroded · Mar 28, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SHAPE SILL HAS CORROSION. REMOVED AND REPLACED L2 DOOR SHAPE SILL IAW SRM A320-51-72-11-911-001. REMOVED AND REPLACED L2 DOOR SHAPE SILL IAW SRM A320 51-72-11-91 1-001.
- [SDR CALA2025040103380](https://openairdocs.org/sdr/CALA2025040103380.md): Floor Support · corroded · Mar 27, 2025 · N460UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR FWD AND AFT GIRT BAR FITTING MAIN STRUCTURE HAS CORROSION. REMOVED AND REPLACED L2 DOOR SILL IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2025040103379](https://openairdocs.org/sdr/CALA2025040103379.md): Bracket · cracked · Mar 26, 2025 · N460UA · Airbus A320232 · Fuselage Main, Structure
  > OB CROSSBEAM TO FRAME CONNECTING BRACKET AT FR 68 LEFT HAND IS C RACKED AT FASTENER HOLE. REMOVED AND REPLACED O/B CROSSBEAM TO FRAME CONNECTING BRACKET A T FR 68 IAW SRM A320 51-72-11-911-001.
- [SDR CALA2025032003013](https://openairdocs.org/sdr/CALA2025032003013.md): Skin · contaminated · Mar 19, 2025 · N460UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS TOP SIDE AT 131.5 IN FROM I/B EN D, 6.5 IN FROM TRAILING EDGE 3IN IN DIAMETER. REPAIRED LH ELEVATOR 131.5 IN FROM IB AND 6.5 IN FROM TE IAW SRM 55-21-11-300-005.
- [SDR CALA2025032003012](https://openairdocs.org/sdr/CALA2025032003012.md): Skin · contaminated · Mar 19, 2025 · N460UA · Airbus A320232 · Elevator, Plate/Skin
  > L/H ELEVATOR HAS LIQUID INGRESS TOP SIDE AT 159 IN FROM I/B END, 12IN FROM TRAILING EDGE, 1 IN IN DIAMETER. REPAIRED L/H ELEVATOR TOP SIDE OF 159IN FROM INBOARD END, 12IN FROM TRAILING EDGE. 1INCH IN DIAMETER AS REQUIRED IN ZONE A IAW A320 SRM 55-21-11-300-
- [SDR CALA2024011200099](https://openairdocs.org/sdr/CALA2024011200099.md): Lgciu · failed · Jan 8, 2024 · N460UA · Airbus A320232 · Landing Gear Retraction/Extension System
  > LG DOORS FAILED TO RETRACT AFTER T/O. DISAGREE LIGHTS ON WHEEL P G. CYCLED GEAR HANDLE.NO HELP CREW NOTED NORMAL GEAR DOOR OPS NORMAL ON GROUND. PLEASE FOLLOW TSM 32-31-00-810-898-A. SFOLM TRINH. 08-JAN-2024. PLACED AIRCRAFT ON JACKS,ACCOMPLISHED GEAR SWING,GE
- [SDR CALA2023041001091](https://openairdocs.org/sdr/CALA2023041001091.md): Fuel Cap · missing · Apr 10, 2023 · N460UA · Airbus A320232 · Aircraft Fuel System
  > PDA 2, TOW TEAM REPORTED FUEL CAP MISSING FROM AIRCRAFT UPON ARRIVAL. TOMC SMITH INSTALLED SERVICEABLE FUEL CAP. PARTS USED: 1844397,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1844397 SN OFF 7014 CAP, COUPLING R OFF 31-2825-9-0001 7014 ON 31-2825-9-0
- [SDR CALA2023022200501](https://openairdocs.org/sdr/CALA2023022200501.md): Skin · dented · Feb 20, 2023 · N460UA · Airbus A320232 · Fuselage Floor Panel
  > DENT BETWEEEN FR32-33 AND STR41-42. CONTACTED BY STAND AND IS OUT OF LIMITS. 53-21-11-205-068 TABLE 1 ZONE J. CURRENT AIRCRAFT TIME 29710FC/69556FH. INITIATE DIP TO PERFORM EDDY CURRENT AND DVI INSPECTION AT INTERVALS OF 1200FC/2400FH, WHICHEVER COMES FIRST.
- [SDR CALA2023020600349](https://openairdocs.org/sdr/CALA2023020600349.md): Panel · stuck · Feb 6, 2023 · N460UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHTS WILL NOT TURN OFF AFTER SELECTING ON FROM AFT ATT PANEL. FOUND EMER LIGHT SWITCH AT AFT ATTENDANT PANEL STUCK IN ON POSITION AND SWITCH WOULD NOT RELEASE. REMOVED AND REPLACED THE AFT ATTENDANT PANEL. OPS CHECK IS GOOD.
- [SDR CALA2021091501580](https://openairdocs.org/sdr/CALA2021091501580.md): Fuel Cap · missing · Sep 15, 2021 · N460UA · Airbus A320232 · Fuel Storage
  > PDA 2 REF LP 7032358, FUEL CAP REPORTED MISSING BY FUELER. ITEM ENTERED INTO HISTORY E-SFR ENTRY MADE. SDR #1026386 SUBMITTED. MISSING FUEL CAP, AS REPORTED BY FUELER.PLACED ON CDL, CDL CARD 280010, PAGE 28-2 / COMPLIED WITH CDL.R&R FUEL CAP AND RETAINER. OPS
- [SDR CALA2021091301559](https://openairdocs.org/sdr/CALA2021091301559.md): Fuel Cap · missing · Sep 11, 2021 · N460UA · Airbus A320232 · Fuel Storage
  > MISSING FUEL CAP, AS REPORTED BY FUELER. PLACED ON CDL, CDL CARD 280010, PAGE 28-2 DISPATCH DESK: 01 NAME: C H DATE: 10-SEP-21- OK TO DEFER FUEL CAP REF CDL 28A COMPLIED WITH CDL.
- [SDR CALA2021031200301](https://openairdocs.org/sdr/CALA2021031200301.md): Doubler · corroded · Mar 10, 2021 · N460UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > FUSELAGE REIENFORCEMENT DOUBLER AT AVIONICS COMPARTMENT INLET VA LVE HAS CORROSION AT 6 O''CLOCK POSITION ON HAECO LCQ REF 9290312 GENERATED BY MECH V899045 REMOVED AND REPLACED AVIONICS COMPARTMENT REINFORCEMENT DOUBLER IAW A320 SRM 51-72-11 MECH BY V914162 I
- [SDR CALA2019040800548](https://openairdocs.org/sdr/CALA2019040800548.md): Beam · corroded · Apr 6, 2019 · N460UA · Airbus A320232 · Fuselage Main, Structure
  > AFT WET AREA Y-1589 FR 66 SEAL BEAM CORROSION. CUT OUT DAMAGE AREA AT AFT WET AREA FR68 Y-1589 SEAL BEAM,FABRIC ATED & INSTALLED REPAIR PARTS,ANGLE 1(EA) AND FILLER 1(EA)
- [SDR CALA2019032200446](https://openairdocs.org/sdr/CALA2019032200446.md): Beam · worn · Mar 21, 2019 · N460UA · Airbus A320232 · Fuselage Main, Structure
  > COMPLETE REPAIR PER SRM 53-11-14-283-005 FIG 1 AT R1 SILL BEAM WHERE FWD GIRT FITTING MOUNTS INCLUDING MATERIAL REMAINING BY BOLT HOLES, SPOT FACE AT BOLT HOLES, BUSHINGS IF NEEDED, NDT ROTO CHECK OF HOLES. REF N/R 99830719 REF. N/R:99830831 CLEANED AREA FOR N
- [SDR CALA2019032200445](https://openairdocs.org/sdr/CALA2019032200445.md): Beam · worn · Mar 21, 2019 · N460UA · Airbus A320232 · Fuselage Main, Structure
  > COMPLETE REPAIR PER SRM 53-11-14-283-005 FIG 1 AT L1 SILL BEAM WHERE AFT GIRT FITTING MOUNTS INCLUDING MATERIAL REMAINING BY BOLT HOLES, SPOT FACE AT BOLT HOLES BUSHINGS IF NEEDED, NDT ROTO CHECK OF HOLES, REF N/R 99830717 REF N/R:99830829 CLEANED AREA FOR NDT
- [SDR CALA2019032200444](https://openairdocs.org/sdr/CALA2019032200444.md): Beam · worn · Mar 21, 2019 · N460UA · Airbus A320232 · Fuselage Main, Structure
  > COMPLETE REPAIR PER SRM 53-11-14-283-005 FIG 1 AT L1 SILL BEAM WHERE FWD GIRT FITTING MOUNTS INCLUDING MATERIAL REMAINING BY BOLT HOLES, SPOT FACE AT BOLT HOLES, BUSHINGS IF NEEDED, NDT ROTO CHECK OF HOLES. REF N/R 99830716 REF. N/R:99830831 CLEANED ARE FOR N
- [SDR CALA2019032200443](https://openairdocs.org/sdr/CALA2019032200443.md): Beam · worn · Mar 21, 2019 · N460UA · Airbus A320232 · Fuselage Main, Structure
  > COMPLETE REPAIR PER SRM 53-11-14-283-005 FIG 1 AT R1 SILL BEAM WHERE AFT GIRT FITTING MOUNTS INCLUDING MATERIAL REMAINING BY BOLT HOLES, SPOT FACE AT BOLT HOLES, BUSHINGS IF NEEDED, NDT ROTO CHECK OF HOLES. REF N/R 99830721 REF. N/R:99830832 CLEANED AREA FOR N
- [SDR CALA2017051201380](https://openairdocs.org/sdr/CALA2017051201380.md): Battery · faulty · May 12, 2017 · N460UA · Airbus A320232 · Emergency Lighting
  > AFTER EPSU BITE TEST, THERE IS A EPSU BATTERY FWD L FAULT (10WL) AND EPSU BATTERY EMER L FAULT (11WL). REMOVE AND REPLACED EPSU BATTERY FWD L (10WL) AND EPSU BATTERY EMERGENCY (11WL) IAW- AMM-33-51-38-000 -002-A /33-51-38-400-002-A. PERFORMED OPS TEST REF AMM-
- [SDR CALA2013112293190](https://openairdocs.org/sdr/CALA2013112293190.md): Unknown · malfunctioned · Nov 21, 2013 · N460UA · Airbus A320232 · Heating System
  > AFT CARGO PIT HOT AIR VALVE WILL NOT OPEN, EVEN WHEN TEMP SELECTED FULL HOT.
- [SDR CALA2013112093122](https://openairdocs.org/sdr/CALA2013112093122.md): Seal · torn · Nov 20, 2013 · N460UA · Airbus A320232 · Landing Gear Doors
  > SMALL DOOR ON LT NLG HAS SEAL TORN & DISTORTED. MADE INTERIM REPAIR IAW ECRA.
- [SDR CALA2013110792722](https://openairdocs.org/sdr/CALA2013110792722.md): Solenoid · faulty · Nov 6, 2013 · N460UA · Airbus A320232 · Leading Edge Slat Control System
  > SLAT SYS 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL REPLACED THE EXTEND SOLENOID ON 25CV POWER CONTROL UNIT REF AMM. PERFORMED OPS CHECKS PER AMM 27-84-00-710. NO DEFECTS OR LEAKS NOTED. SYSTEM CHECKS OK
- [SDR CALA2013103192535](https://openairdocs.org/sdr/CALA2013103192535.md): Rivet · sheared · Oct 30, 2013 · N460UA · Airbus A320232 · Nacelle/Pylon Miscellaneous Structure
  > RT SIDE OF NR 2 ENG PYLON HAS DOOR OPEN. FOUND SHEAR RIVETS SHEARED AT AUTOMATIC OPENING MECHANISM. INSTALLED NEW RIVETS IAW MM, ALSO PERFORMED A VISUAL INSPECTION OF BLEED DUCTS. NO DEFECTS NOTED.
- [SDR CALA2013090991099](https://openairdocs.org/sdr/CALA2013090991099.md): Tire · faulty · Sep 6, 2013 · N460UA · Airbus A320232 · Tire
  > NLG CONTINUES TO SPIN AFTER RETRACTION. REPLACED NLG TIRES IAW MM.
- [SDR CALA2013090591005](https://openairdocs.org/sdr/CALA2013090591005.md): Cover · detached · Sep 5, 2013 · N460UA · Airbus A320232 · Service Doors
  > PRESSURE GAUGE COVER AT DOOR 2R IS NOT CONNECTED. OK TO CONTINUE WITHOUT IAW MT-008. TO BE REPLACED IN 10 DAYS, OLD WINDOW IN FLIGHT DECK IN THE MRD POUCH SECTION. REATTACHED GAUGE COVER ON 2R DOOR WITH ADHESIVE.
- [SDR CALA2013083090886](https://openairdocs.org/sdr/CALA2013083090886.md): Battery · discharged · Aug 30, 2013 · N460UA · Airbus A320232 · Emergency Lighting
  > DURING NR 2 SERVICE CHECK STEP 3 HAD EPSU EMERGENCY L MESSAGE. REPLACED LT EPSU BATTERY FOR 11WL OVERWING, BEHIND LOWER SIDEWALL PANEL. CHECKED NORMAL.
- [SDR CALA2013083090858](https://openairdocs.org/sdr/CALA2013083090858.md): Power Supply · faulty · Aug 30, 2013 · N460UA · Airbus A320232 · Emergency Lighting
  > DURING NR 2 SERVICE CHECK STEP 3, EMERGENCY EPSU R FAULT. REPLACED EPSU AT 12WL LOWER RIGHT SIDEWALL OVERWING, CHECKED GOOD.
- [SDR CALA2013080990290](https://openairdocs.org/sdr/CALA2013080990290.md): Fire Loop · faulted · Aug 8, 2013 · N460UA · Airbus A320232 · Fire Detection
  > FIRE LOOP B FAULT DISPLAYED ON UPPER ECAM SCREEN, NR 1 ENGINE. NR 1 ENGINE ECAM FIRE LOOP B FAULT.
- [SDR UALA2013072505240](https://openairdocs.org/sdr/UALA2013072505240.md): Switch · malfunctioned · Jul 23, 2013 · N460UA · Airbus A320232 · Passenger Oxygen System
  > OXYTEN MASKS DROPPED AT SEATS 32ABC. REPLACED EMERGENCY OXYGEN CONTAINER SWITCH TO DOOR. PACKED OXYGEN MASKS. OPS TESTED MANUAL RELEASE OK IAW AMM.
- [SDR UALA2013061704188](https://openairdocs.org/sdr/UALA2013061704188.md): Acoustic Liner · damaged · Jun 16, 2013 · N460UA · Airbus A320232 · Turbine Engine Air Inlet Section
  > HOLE IN ACCOUSTIC LINING ON NR 2 ENGINE.
- [SDR UALA2013050203074](https://openairdocs.org/sdr/UALA2013050203074.md): Pump · failed · Apr 30, 2013 · N460UA · Airbus A320232 · Hydraulic Pump (Electric/Engine), Main
  > ECAM CAUTION MESSAGE, ENGINE PUMP LOW PRESSURE. HYD SYSTEM QTY WENT TO ZERO INFLIGHT, GROUND CREW REPORTED MAJOR LEAK. REPLACED NR 2 ENGINE HYDRAULIC PUMP FOR YELLOW SYSTEM IAW MM, LEAK AND OPS CHECKED NORMAL.
- [SDR UALA2013040402216](https://openairdocs.org/sdr/UALA2013040402216.md): Sensor · malfunctioned · Apr 3, 2013 · N460UA · Airbus A320232 · Cabin Temperature Control System
  > TEMP CONTROL ABNORMAL. COCKPIT AND FWD CABIN REQ TEMP KNOBS TURNED FULL CTR CLOCKWISE TO COOL. REPLACED OUTLET TEMP SENSOR AND WATER SENSOR IAW MM. OPERATED PACK, PACK OPS NORMAL.

Next page: https://openairdocs.org/aircraft/N460UA/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 = 'N460UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N460UA/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.