# Service difficulty reports: N825UA

A list on [N825UA](https://openairdocs.org/aircraft/N825UA.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 2 · 70 reports

- [SDR CALA2026080918392](https://openairdocs.org/sdr/CALA2026080918392.md): Fuel Cap · missing · Aug 7, 2026 · N825UA · Airbus A319131 · Fuel Storage
  > FUELER REPORTED AIRCRAFT ARRIVED WITH FUEL COUPLING CAP MISSING. INSTALLED A NEW FUEL COUPLING CAP IAW AMM 28-25-41-400-005-A. NO OTHER DEFECTS NOTED
- [SDR CALA2025112511444](https://openairdocs.org/sdr/CALA2025112511444.md): Skin · dented · Nov 22, 2025 · N825UA · Airbus A319131 · Passenger/Crew Doors
  > DENT ON LOWER AFT CORNER OF DOOR 1L. DENT MEASURES 3" X 1.5" AND IS.015" DEEP. LOCATED AT BOTTOM RT CORNER OF DOOR. 1" UP FROM BOTTOM AND 6" IN FROM AFT EDGE. APPLIED DENT DOT WITH LOG PAGE #. REF. SRM 52-00-00-283-002 FIG 2. REPAIR AT OR BEFORE 200 FC (
- [SDR CALA2025102710583](https://openairdocs.org/sdr/CALA2025102710583.md): Battery Pack · no test · Oct 26, 2025 · N825UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY BATTERY L DISPLAYED DURING EMERGENCY LIGHTING BITE TEST. REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-38. OPS CHECK GOOD.
- [SDR CALA2025091608962](https://openairdocs.org/sdr/CALA2025091608962.md): Bezel · not seated · Sep 12, 2025 · N825UA · Airbus A319131 · Emergency Equipment
  > 2R DOOR SLIDE ARMINDICATOR BLOCKED BYPACK COVER ON LOWER LOF DOO R AND FLOOR DOOR 2R SLIDE BEZEL FWD LOWER CORNER NOT SEATED PROPERLY OBSRUCTING VIEW OF ARMED INDICATOR DOT ON GIRT BAR. RESEATED SLIDE BEZEL. REF AMM 25-62-44
- [SDR CALA2025052004842](https://openairdocs.org/sdr/CALA2025052004842.md): Fitting · worn · May 16, 2025 · N825UA · Airbus A319131 · Fuselage, Door Hinge
  > L/H MLG DOOR ACTUATOR TOP ATTACHMENT FITTING ON KEEL BEAM, HAT B USHING MIGRATED COMPLETELY OUT OF FITTING. COMPLETE ESFR COMPLETE ESFR COMPLETE REMOVED & REPLACED L/H MLG DOOR ACTUATOR UPPER AFT FITTING PER A 319 UAL REPAIR DRAWING R53370501. ISSUE F.
- [SDR CALA2025032503158](https://openairdocs.org/sdr/CALA2025032503158.md): Light Sys · malfunctioned · Mar 24, 2025 · N825UA · Airbus A319131 · Emergency Lighting
  > EMER EXIT LIGHT REMAIN ILLUMINATED UNTILGEAR IS RETRACTED NORMAL OPERATION INDICATES THE EMERGENCY LIGHTS COME ON AUTOMATICALLY WHEN NO SMOKING SWITCH 190RH IS IN THE ON POSITION. THEY ALSO COME ON, WHEN NO SMOKING SWITCH 190RH IS IN THE AUTO POSITION AND WHEN
- [SDR CALA2025012300177](https://openairdocs.org/sdr/CALA2025012300177.md): Fuel Cap · missing · Jan 21, 2025 · N825UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP MISSING REPORTED BY FUELER REF L/P 3598742 INSTALLED NEW FUEL CAP REF AMM 28-25-41-400-007-A. NOTE: PDA L/P 3601214.
- [SDR CALA2025011301882](https://openairdocs.org/sdr/CALA2025011301882.md): Battery · no test · Jan 9, 2025 · N825UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - FWD LH EPSU FOUND BATT FAULT. REPLACED BATTERY PACK OF THE EPSU IAW AMM 33-51-38-400-002-A0. OPS TEST GOOD.
- [SDR CALA2023122103699](https://openairdocs.org/sdr/CALA2023122103699.md): Wheel · damaged · Dec 17, 2023 · N825UA · Airbus A319131 · Wheel/Ski/Float
  > LEFT MAIN OUTBOARD WHEEL MISSING A LUG NUT ADDED PICTURE. WHEEL, TIRE, AS OFF 31-3245-9-9001 1996 ON 31-3245-9-9001 2843 WHEEL, TIRE, AS OFF 31-3245-9-9001 1996 ON 0000 #1 MLG WHEEL ASSY CHANGED DUE TO BROKEN TIE BOLT, REF AMM 32-41-11-400-006-A.
- [SDR CALA2023070702183](https://openairdocs.org/sdr/CALA2023070702183.md): Fitting · cracked · Jul 5, 2023 · N825UA · Airbus A319131 · Fuselage Structure (General)
  > WINDSHIELD LH CONTINUITY FITTING HAS A CRACK INDICATION AT UPPER FLANGE BEGINNING OF RADIUS PER HAECO LCQ N/R 9298605/44605 GEN BY V892444 REVISION. ON OR BEFORE 58900 TOTAL FLT CYCLES. PERFORM REPEAT THEREAFTER. INSPECTIONS AT INTERVALS NOT TO EXCEED 8800 FLT
- [SDR CALA2023063002096](https://openairdocs.org/sdr/CALA2023063002096.md): Shear Plate · corroded · Jun 29, 2023 · N825UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO PIT FR59 AT STGR 38R PROFILE PANEL SUPPORTING SHEAR PLATE HAS CORROSION ON FWD END PER HAECO LCQ N/R 9298945/44945 GEN BY V925324
- [SDR CALA2023062602026](https://openairdocs.org/sdr/CALA2023062602026.md): Stringer · corroded · Jun 25, 2023 · N825UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > FWD CARGO PIT R/H FR30 BETWEEN STRINGERS 41R-42R HAS CORROSION ON CLEAT PER HAECO LCQ NON ROUTINE 9298726/44726 GENERATED BY V91 9150 RMV AND RPL AND INSTALLED NEW CLEAT PO#1134829.4 D5323072020002 AT FWD CARGO R/H FR30 BETWEER STRG 5.41R-42R IAW A319 SRM 51-4
- [SDR CALA2023062602014](https://openairdocs.org/sdr/CALA2023062602014.md): Doubler · corroded · Jun 24, 2023 · N825UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FWD CARGO PIT R/H BETWEEN FR30-34 AND BETWEEN STRINGERS 43R-44 HAS CORROSION ON SKIN DOUBLER PER HAECO LCQ N/R 9298727/44727 GEN BY V919150 RMVD AND FABRICATED AND INSTALLED DOUBLER AT FWD CARGO FR30-FR34 BETWEEN STRINGER 43R-44 IAW A319 SRM 53-21-11-08-A DWG
- [SDR CALA2023061601876](https://openairdocs.org/sdr/CALA2023061601876.md): Unknown · corroded · Jun 15, 2023 · N825UA · Airbus A319131 · Fuselage Structure (General)
  > UPON REMOVAL OF GIRT BAR FITTING BASE PLATE TO APPLY REPAIR TO L 2 DOOR SILL FOUND CORROSION AT FR66 PER NR9298903/44903 GEN BY V 080280 RMVD AND RPLD L2 DOOR SILL IAW SRM 51-72-11-911-001 APPLIED TOPC OAT IAW SRM 51-75-12-911-002 BY MECH V928628 INSP BY V0779
- [SDR CALA2023061601875](https://openairdocs.org/sdr/CALA2023061601875.md): Unknown · corroded · Jun 15, 2023 · N825UA · Airbus A319131 · Fuselage Structure (General)
  > UPON REMOVAL OF GIRT BAR FITTING BASE PLATE TO APPLY REPAIR TO R 2 DOOR SILL FOUND CORROSION AT FR66 PER NR9298904/44904 GEN BY V 080280 REMOVED AND REPLACED R2 DOOR SILL IAW SRM 51-72-11 BY MECH V0397 46 INSP BY N078625
- [SDR CALA2023061201814](https://openairdocs.org/sdr/CALA2023061201814.md): Door · corroded · Jun 9, 2023 · N825UA · Airbus A319131 · Cargo/Baggage Doors
  > AFT CARGO PIT DOOR THRESHOLD HAS SEVERAL AREAS OF SURFACE CORROS ION PER HAECO LCQ N/R 9298567/44567 GEN BY V925324 RMVD AND RPLD AFT CARGO PIT DOOR THRESHOLD IAW SRM 51-74-00 AND 53-41-49-283-003 MECH V925324 INSP BY V061704
- [SDR CALA2023042401237](https://openairdocs.org/sdr/CALA2023042401237.md): Bypass Valve · failed · Apr 24, 2023 · N825UA · Airbus A319131 · Cabin Temperature Control System
  > AIR PACK 2 REG FAULT...FLIGHT DECK TEMP UNCONTROLLABLE...AT 84 DEGREES AND CLIMBING. POST FLIGHT REPORT INFO REMOVED RIGHT PACK PANEL 192FB FOR TROUBLESHOOTING ACCESS. REPLACED PACK 2 TURBINE BYPASS VALVE (30HH) REF AMM 21-63-00-720-001-A. VERIFIED ALL ZONE TE
- [SDR CALA2021101401877](https://openairdocs.org/sdr/CALA2021101401877.md): Fuel Cap · missing · Oct 14, 2021 · N825UA · Airbus A319131 · Aircraft Fuel System
  > PDA 3 UNDERWING FUEL CAP MISSING C/W DDP PER MEL PLACED ON C/W DDP PER MEL DISPATCH DESK: 37 NAME: JO DATE: 10-OCT-21- OK TO CDL NEED FUEL CAP M/E 31-2825-9-0001 INSTALLED FUEL CAP REF. IPC 28-11-43
- [SDR CALA2020020800371](https://openairdocs.org/sdr/CALA2020020800371.md): Window Frame · cracked · Feb 4, 2020 · N825UA · Airbus A319131 · Fuselage Main, Structure
  > DURING C-2 CHECK AT AAR DLH "REFNON-ROUTINE 9622631" FOUND WINDS HIELD CENTER POST LOWER ATTACHMENT INTERNAL R/H WINDSHIELD FRAME HAS CRACK INDICATION IN UPPER RADIUS OF CUTOUT EMINATING OUT OF UPPER BOLT HOLE. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 53
- [SDR CALA2020020800370](https://openairdocs.org/sdr/CALA2020020800370.md): Window Frame · cracked · Feb 4, 2020 · N825UA · Airbus A319131 · Fuselage Main, Structure
  > DURING C-2 CHECK AT AAR DLH "REF NON-ROUTINE 9622630" FOUND WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL LH WINDSHIELD FRAME HAS CRACK INDICATION IN UPPER RADIUS OF CUTOUT EMINATING OUT OF UPPER BOLT HOLE. ACCOMPLISHED PART 1 OF ECRA 5311-02243. NEED TO AC
- [SDR CALA2019041200567](https://openairdocs.org/sdr/CALA2019041200567.md): Control Unit · inoperative · Apr 11, 2019 · N825UA · Airbus A319131 · Weather Radar System
  > WR ANT. WEATHER RADAR INOP. PFR HIT ON ANTENNA R&R RADAR ANTENNA UNIT IAW AMM 34-41-11, OPS TEST WOULD NOT TILT +10 DEGREES PER OPS TEST. R&R RADAR CONTROL UNIT IAW AMM 34-41-12, OPS TEST AND BITE TEST OF RADAR SYSTEMS PASSED. OK FOR SERVICE. ROTABLE PARTS CHA
- [SDR CALA2016112500970](https://openairdocs.org/sdr/CALA2016112500970.md): Battery Pack · faulted · Nov 25, 2016 · N825UA · Airbus A319131 · Lighting System
  > FWD EPSU FAULT LIGHT DURING TEST REPLACED EMERGENCY BATTERY PER AMM 33-51-38. NOW OK
- [SDR CALA2015111794834](https://openairdocs.org/sdr/CALA2015111794834.md): Skin · unknown · Nov 12, 2015 · N825UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR, UPPER SKIN HAS 19 TRAPPED WATER INDICATIONS. ALL REPAIRS ACCOMPLISHED IAW SRM 55-21-11 & ECRA 5520-01470 ECRA PART 2. REQUIRES 1ST INSPECTION AT 60000C OR 120000T WHICHEVER COMES 1ST.
- [SDR CALA2015111794833](https://openairdocs.org/sdr/CALA2015111794833.md): Skin · unknown · Nov 12, 2015 · N825UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT ELEVATOR, UPPER SKIN HAS 10 TRAPPED WATER INDICATIONS. ALL REPAIRS ACCOMPLISHED IAW SRM 55-21-11 & ECRA 5520-01470 ECRA PART 2. REQUIRES 1ST INSPECTION AT 60000C OR 120000T WHICHEVER COMES 1ST.
- [SDR CALA2015111794818](https://openairdocs.org/sdr/CALA2015111794818.md): Stringer · corroded · Nov 10, 2015 · N825UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > STRINGER 31R, BETWEEN FRAMES 65 & 66, JUST BELOW OUTFLOW VLV HAS EXFOLIATED CORROSION. R & R STRINGER 31R, BETWEEN FRAMES 65 & 66 IAW SRM 51-42-11.
- [SDR CALA2015111794812](https://openairdocs.org/sdr/CALA2015111794812.md): Door Sill · corroded · Nov 9, 2015 · N825UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL CORRODED UNDER FWD & AFT GIRT BAR FITTINGS. R & R R2 DOOR SILL IAW SRM 51-42-11 PG 25 & 51-72-11 PG 1.
- [SDR CALA2015101294584](https://openairdocs.org/sdr/CALA2015101294584.md): Unknown · malfunctioned · Oct 12, 2015 · N825UA · Airbus A319131 · Cabin Pressure Control System
  > CABIN ALTITUDE ROSE TO 11000 FEET AT FL 330. CPC 1 & 2 SHOWS NO FAULTS. REPLACED CPC 1 & 2 PRECAUTIONARY & DISCUSSED ACTION WITH TOMC, IAW AMM 21-31-34-000 & 21-31-34-401. BITE TESTED GOOD, NO FAULTS PRESENT.
- [SDR CALA2015101494587](https://openairdocs.org/sdr/CALA2015101494587.md): Unknown · malfunctioned · Oct 11, 2015 · N825UA · Airbus A319131 · Cabin Pressure Control System
  > CABIN PRESS STARTED TO CLIMB ON INITIAL DESCENT. CABIN ALT ROSE TO 11000 FEET AT FL 330. DECLARED EMER, DONNED O2 MASKS CPC 1 & 2 SHOWED NO FAULTS. REPLACED CPC 1 & 2 PRECAUTIONARY. BITE TESTED GOOD, NO FAULTS PRESENT.
- [SDR CALA2014123092870](https://openairdocs.org/sdr/CALA2014123092870.md): Oxygen Mask · unwanted deploy · Dec 21, 2014 · N825UA · Airbus A319131 · Passenger Oxygen System
  > O2 MASKS DROPPED ROW 32ABC. INSPECTED PAX O2 PANEL IAW MT 35-003, NO DAMAGE NOTED. REPACKED O2 COMPARTMENT & SECURED PANEL DOOR. MANUAL MASK RELEASE OPERATIONAL CHECK IAW AMM 35-23-00- 710-001 WITHIN 3 DAYS.
- [SDR CALA2014122392863](https://openairdocs.org/sdr/CALA2014122392863.md): Oxygen Mask · unwanted deploy · Dec 21, 2014 · N825UA · Airbus A319131 · Passenger Oxygen System
  > O2 MASKS DROPPED ROW 32ABC. INSPECTED PAX O2 PANEL IAW MT 35-003, NO DAMAGE NOTED. REPACKED O2 COMPARTMENT & SECURED PANEL DOOR. MANUAL MASK RELEASE OPERATIONAL CHECK IAW AMM 35-23-00- 710-001 WITHIN 3 DAYS.
- [SDR CALA2013082690734](https://openairdocs.org/sdr/CALA2013082690734.md): Grill · cracked · Aug 23, 2013 · N825UA · Airbus A319131 · Engine Cowling System
  > NR 1 ENGINE NOSE COWL EXHAUST GRILL IS CRACKED, MARKED. REMOVED NR 1 ENGINE NOSE COWL EXHAUST GRILL & SENT TO SHOP. WELD REPAIRED ACCOMPLISHED IAW 71-11-11-200-011-A 13. INSTALLED PANEL AFTER WELD REPAIR.
- [SDR CALA2013082390702](https://openairdocs.org/sdr/CALA2013082390702.md): Power Supply · inoperative · Aug 23, 2013 · N825UA · Airbus A319131 · Emergency Lighting
  > DURING EMERGENCY LIGHT SYS CHECK, THE " EPSU INT LOAD FWD L" MESSAGE SHOWS. REPLACED FWD LT EPSU, 10WL IAW AMM 33-51-38-000-001-A, 33-51-38-400-001-A. ACCOMPLISHED CIDS RESET. TESTED OK.
- [SDR UALA2013061404107](https://openairdocs.org/sdr/UALA2013061404107.md): Fitting · gouged · Jun 13, 2013 · N825UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > NR 1 FEC, SMALL GOUGES IN THE FWD MOUNTING SPIGOT FITTING. ACCOMPLISHED BLENDING IAW 54-51-18, PG.103
- [SDR UALA2013061704165](https://openairdocs.org/sdr/UALA2013061704165.md): Gearbox · leaking · Jun 11, 2013 · N825UA · Airbus A319131 · Turbine Engine Accessory Drive
  > HAND SIZED PUDDLE OF OIL UNDER ENG 1 AFT OF DRAIN MAST. OIL ON BOTTOM OF ENGINE. OPERATED ENGINE FOUND OIL LEAKING OUT OF LIMITS FROM TOP OF ANGLE GEARBOX IAW TSM 79-00-00-810-838-A, IF UNABLE TO CORRECT SOURCE OF EXTERNAL OIL LEAK, REPLACE ENGINE. REPLACED N
- [SDR UALA2013060303849](https://openairdocs.org/sdr/UALA2013060303849.md): Windshield · faulty · Jun 3, 2013 · N825UA · Airbus A319131 · Flight Compartment Windows
  > ANTI-ICE RT WINDSHIELD EICAS. (REPEAT GRIPE) DEFERED IAW MEL 30-42 PTS IAW MM 30-42-00-710-001A AND WSM 30-42-02 SENSOR TEST OK SUSPECT WINDSHIELD AT FAULT IN FLT NEEDS NEW WINDSHIELD, PCN (110- 3206). REPLACED WINDSHIELD IAW MM.
- [SDR UALA2013060303848](https://openairdocs.org/sdr/UALA2013060303848.md): Controller · faulty · May 31, 2013 · N825UA · Airbus A319131 · Windshield/Door Rain/Ice Removal
  > R WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. ANTI ICE. REPLACED WHC IAW AMM, OPS CHECK OK.
- [SDR UALA2013053103811](https://openairdocs.org/sdr/UALA2013053103811.md): Wire Harness · failed · May 30, 2013 · N825UA · Airbus A319131 · Ice/Rain Protection System Wiring
  > RIGHT WINDSHIELD DISPLAYED ON UPPER ECAM SCREEN. ANTI-ICE INSTALLED HARNESS 9F21895-501 TO SWAP TO SPARE SENSOR FOR RT WINDSHIELD.
- [SDR UALA2013012100346](https://openairdocs.org/sdr/UALA2013012100346.md): Shunt · corroded · Jan 20, 2013 · N825UA · Airbus A319131 · DC Indicating System
  > FOUND SHUNT 3PB2 CORRODED BETWEEN CONTACTS. REPLACED SHUNT 3PB2. BCL TEST OKAY.
- [SDR UALA2013011700300](https://openairdocs.org/sdr/UALA2013011700300.md): Sdac · failed · Jan 15, 2013 · N825UA · Airbus A319131 · Electrical Power System
  > ELEC BCL2 FAULT ECAM. TROUBLESHOT PER TSM 24-38-00-810- 833 WITH NO DEFECTS. REMOVED AND REPLACED SDAC2 IAW AMM 31-55-34, OPS CHECKED NORMAL.
- [SDR UALA2013010200006](https://openairdocs.org/sdr/UALA2013010200006.md): Interface Unit · faulty · Jan 2, 2013 · N825UA · Airbus A319131 · Landing Gear Retraction/Extension System
  > WHILE ENROUTE GOT LGCIU 1 FAULT. NO AIRBORNE RESET AVAIL. GPWS AND REVERSER INOP. RETURNED TO DENVER. REPLACED LGCIU 1, OP CKS GOOD.
- [SDR UALA2011111406198](https://openairdocs.org/sdr/UALA2011111406198.md): Computer · faulty · Nov 12, 2011 · N825UA · Airbus A319131 · Aileron Control System
  > FLIGHT CONTROL BUMPING. AFTER 90 MINUTES AT CRUISE FL360 HAD LOW AMPLITUDE BUMPS FELT IN COCKPIT, OBSERVED BOTH AILERONS PULSE UP ONE INCH SIMULTANEOUSLY. WITH ELAC1 OR ELAC2 OFF, THE BUMPING STOPPED. SIMILAR BUMP NOTED WHEN SWITCHING ELAC1 OFF. NOTED BY M
- [SDR UALA2011111006143](https://openairdocs.org/sdr/UALA2011111006143.md): Computer · faulty · Nov 10, 2011 · N825UA · Airbus A319131 · Elevator Control System
  > ELAC-2 ISSUES, FLIGHT DIVERTED. NR 2 ELAC REF MM. PERFORMED OPERATIONAL TEST OF ELAC. PERFORMED EFCS 1&2, NO FAULTS FOUND. PERFORMED AFS TEST REF MM, TEST PASSED ON GND. KNOWN GOOD ELAC1 AND 2 DUE TO CONTINUING ELAC 1 AND 2 FAULTS WITH MULTIPLE SEPARATE REPLAC
- [SDR UALA2011110305951](https://openairdocs.org/sdr/UALA2011110305951.md): Computer · faulty · Nov 3, 2011 · N825UA · Airbus A319131 · Elevator Control System
  > ELAC 1 FAULT. REPLACED ELAC 2 PER MM. OPERATIONAL CHKS OKAY.
- [SDR UALA2011101105526](https://openairdocs.org/sdr/UALA2011101105526.md): Seat · binding · Oct 10, 2011 · N825UA · Airbus A319131 · Flight Compartment Equipment
  > F/O SEAT FORWARD AFT IS BINDING USING MANUAL CONTROLS. REPLACED F/O'S SEAT PER MM.
- [SDR UALA2011081504309](https://openairdocs.org/sdr/UALA2011081504309.md): Outflow Valve · faulty · Aug 14, 2011 · N825UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > AVIONICS PROBLEM, FLIGHT DIVERTED. AVIONICS VENT SKIN VLV FAULT AFTER T/O. FOLLOWED FLT MAN BOTH BLOWER AND EXTRACT VLV TO OVERRIDE, NOW INLET VLV SHOWS CLOSED BUT EXTRACT SHOWS FULL OPEN. SAMC TEXT: EXTRACT VLV SHOULD SHOW CLOSED IN THIS CONFIGURATION SUS
- [SDR UALA2011071403570](https://openairdocs.org/sdr/UALA2011071403570.md): Wedge · damaged · Jul 14, 2011 · N825UA · Airbus A319131 · Trailing Edge Flaps
  > LEFT OUTBD TRAILING EDGE FLAP, TRAILING EDGE WEDGE HAS NUMEROUS HAIL-DAMAGE DENTS APPROXIMATELY ONE-SIXTEENTH OF AN INCH DEEP.
- [SDR UALA2011060802806](https://openairdocs.org/sdr/UALA2011060802806.md): Thrust Reverser · delaminated · Jun 7, 2011 · N825UA · Airbus A319131 · Engine Thrust Reverser
  > FOUND DELAMINATION ON ENG CORE SIDE OF THE NR 1 LEFT SIDE THRUST REV HALF OUTER METAL PLY IS PEELING UP. AREA OF DAMAGE IS 128 SQ INCHES AND IS WITHIN CF LIMITS, TO BE RE-CHECKED ONCE DAILY. DL8304 CREATED TO MONITOR. REPAIRED DAMAGE AREA PER MT.
- [SDR UALA2011060602755](https://openairdocs.org/sdr/UALA2011060602755.md): Light · disconnected · Jun 6, 2011 · N825UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT ROWS 6C AND 10C DO NOT TURN ON. RECONNECTED EMERGENCY LIGHTS ROWS 6C AND 10C, TESTED ALL NORMAL.
- [SDR UALA2010122004617](https://openairdocs.org/sdr/UALA2010122004617.md): Control Unit · faulty · Dec 20, 2010 · N825UA · Airbus A319131 · Fuel Indicating System
  > LT CTR TANK PUMP LOW PRESS MSG, FLT DIVERTED. R & R FUEL LEVEL SENSING CONTROL UNIT. CYC RIGHT CTR FUEL PUMP CB INSP CONNECTOR AT FUEL PUMP AND CONTACTOR 36QA. MOVED 5000LBS OF FUEL WITH THE RIGHT CTR PUMP. REPLACED RELAY 45QA, LEFT CTR PUMP OPERATES NORM
- [SDR UALA2010071302499](https://openairdocs.org/sdr/UALA2010071302499.md): Power Supply · failed · Jul 13, 2010 · N825UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ARE LIT IN BACK GALLEY IN FLIGHT. EMERGENCY LIGHT TEST FAILED OVERWING POWER SUPPLY UNIT 12WL. REPLACED UNIT, OPS CHECKS OKAY.

Next page: https://openairdocs.org/aircraft/N825UA/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 = 'N825UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N825UA/reports

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