# Service difficulty reports: N832UA

A list on [N832UA](https://openairdocs.org/aircraft/N832UA.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 · 81 reports

- [SDR CALA2026031014477](https://openairdocs.org/sdr/CALA2026031014477.md): Fuel Cap · missing · Mar 9, 2026 · N832UA · Airbus A319131 · Fuel Storage
  > ON ARRIVAL FOUND REFUEL/DEFUEL COUPLING CAP MISSING FROM THE AIRCRAFT. INSTALLED NEW FUEL CAP.
- [SDR CALA2026022514057](https://openairdocs.org/sdr/CALA2026022514057.md): Power Supply · no test · Feb 23, 2026 · N832UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY MESSAGE DURING EMERGENCY LIGHT TEST. R & R RT EPSU IAW AMM 33-51-38-000-001-A AND 33-51-38-400-001-A. PASSED EMERGENCY LIGHT TEST.
- [SDR CALA2026021113699](https://openairdocs.org/sdr/CALA2026021113699.md): Battery · shorted · Feb 10, 2026 · N832UA · Airbus A319131 · Emergency Lighting
  > FWD LEFT EPSU UNIT INOPERATIVE. REPLACED EPSU BATTERY AT DOOR 1L PER AMM 33-51-38-000-002-A, BATTERY FAULT & UNIT FAULT CLEARED. FOUND BATTERY SHORTED & FAULTED UNIT.
- [SDR CALA2025102110335](https://openairdocs.org/sdr/CALA2025102110335.md): Skin · corroded · Oct 17, 2025 · N832UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN FR34 STR 43 IS CHAFFED. PERFORMED INTERNAL & EXTERNAL DOUBLER REPAIR PER HAECO REO L2558 5 / ECRA 5321-02170. GENERATE DIP ACCOMPLISH A PERMANENT REPAIR AT FR34 STGR 41LH - 41RH FUSELAGE SKIN PANEL PER PART 3 OF THE L ATEST REVISION OF E
- [SDR CALA2025101510118](https://openairdocs.org/sdr/CALA2025101510118.md): Stringer · corroded · Oct 6, 2025 · N832UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO STR 33R HAS CORROSION, FRS 59-61. REMOVED AND REPLACED STRINGER 33R BETWEEN FRS 59-61 IAW SRM 51-72-11 -911-001.
- [SDR CALA2025100309584](https://openairdocs.org/sdr/CALA2025100309584.md): Brace · gouged · Sep 30, 2025 · N832UA · Airbus A319131 · Fuselage Main, Bulkhead
  > FR 1 BULKHEAD CENTER SUPPORT STRUT HAS A GOUGE. REMOVED AND REPLACED RH CENTER POST AT FR 1 BULKHEAD IAW A319 S RM 51-42-11/001 AND SRM 51-72-11-911-002.
- [SDR CALA2025103010760](https://openairdocs.org/sdr/CALA2025103010760.md): Window Frame · cracked · Sep 26, 2025 · N832UA · Airbus A319131 · Fuselage Main, Structure
  > FLIGHT DECK, WINDSHIELD FRAME LT SIDE HAS A CRACK INDICATION I N LOWER HORIZONTAL FLANGE AT CONTINUITY FITTING INBD HOLE. ACCOMPLISHED INTERIM REPAIR PER HAECO REO-L25587 REV IR WITH NO DEVIATIONS IAW ECRA 5311-03394 PART 1 INTERIM REPAIR STEP 1.
- [SDR CALA2025092609292](https://openairdocs.org/sdr/CALA2025092609292.md): Fitting · cracked · Sep 23, 2025 · N832UA · Airbus A319131 · Fuselage Main, Structure
  > FLIGHT DECK RT CONTINUITY FITTING HAS CRACK INDICATION APPROX.400 INCH FROM CTR POST. REPLACED CONTINUITY FITTING IAW EA 5310-07675 004.
- [SDR CALA2025101510111](https://openairdocs.org/sdr/CALA2025101510111.md): Skin · corroded · Sep 22, 2025 · N832UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FR 34 AREA I STRG 42L HAS CORROSION. REPAIRED STR 42L BETWEEN FR34-29 IAW SRM 53-21-13-300-018.
- [SDR CALA2025101410055](https://openairdocs.org/sdr/CALA2025101410055.md): Stringer · corroded · Sep 22, 2025 · N832UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT PIT S37R HAS CORROSION FROM FR 59-61. REMOVED AND REPLACED STRINGER SECTION 37RH FROM FR 59-FR61 IAW SRM 51-72-11. SEE CONTINUATION SHEET ATTACHED FOR ADDITIONAL WORK ACCOMPLISHED. REF LP 6206878. REMOVED AND REPLACED STRINGER SECTION STR 37RH FROM FR59-
- [SDR CALA2025103010761](https://openairdocs.org/sdr/CALA2025103010761.md): Door Frame · corroded · Sep 15, 2025 · N832UA · Airbus A319131 · Fuselage Main, Structure
  > CABIN R-2 DOOR CORROSION AT FR 68 BETWEEN STR 22 AND STR 23. EVALUATED CORROSION AT R2 DOOR FR68 RT BETWEEN STR 22 AND 23 IAW SRM 53-41-12-283-001, CORROSION FOUND TO BE OUT OF LIMITS, MAXI MUM REWORK ALLOWED.02 IN, FOUND DAMAGE TO BE.025 IN. IAW SRM 5 3-41
- [SDR CALA2025092409209](https://openairdocs.org/sdr/CALA2025092409209.md): Rib · cracked · Sep 15, 2025 · N832UA · Airbus A319131 · Emergency Exits
  > POSSIBLE CRACK AT TWO PLACES ON INNER FWD RIB ON RT EMERGENCY EXIT HATCH. REMOVED AND REPLACED INNER FWD RIB ON R/H EMERGENCY EXIT IAW A31 9 SRM 51-72-11-911-001
- [SDR CALA2025092409207](https://openairdocs.org/sdr/CALA2025092409207.md): Skin · corroded · Sep 8, 2025 · N832UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > UPPER FUSELAGE, VERT STABILIZER FUSE CORRODED FWD OF VERT STAB AT FR 69 BETWEEN STR AD STR 2R. PERFORMED DOUBLER REPAIR IAW SRM 53-41-11-300-037.
- [SDR CALA2025092409206](https://openairdocs.org/sdr/CALA2025092409206.md): Support Beam · corroded · Sep 3, 2025 · N832UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA R/H AFT LATERAL SHEAR PLATE SUPPORT BEAM BETWEEN FR69-70 HAS CORROSION ON LOWER SURFACE. REMOVED AND REPLACED R/H FR 69-70 SHEAR PLATE SUPPORT BEAM AND REINSTALLED SHEAR PLATE RE APPLIED SURFACE PROTECTION IAW SRM 51-42-11 AND 51-75-12.
- [SDR CALA2025090208359](https://openairdocs.org/sdr/CALA2025090208359.md): Seat Track · corroded · Aug 28, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK -Y1292 FR 41-47 IS OUT OF LIMITS. REPLACED SEAT TRACK REMOVED AND REPLACED SEAT TRACK -Y1292 ON FR41-47 IAW A319 SRM 5 1-72-11.
- [SDR CALA2025090208358](https://openairdocs.org/sdr/CALA2025090208358.md): Seat Track · corroded · Aug 28, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN FLOOR BEAM Y765 CORRODED AT FR 16. REMOVED AND REPLACED SEAT TRACK Y765 FROM FR12 TO FR24 MAIN CAB IN IAW A319 SRM 51-42-11 AND SRM 51-72-11-911-001.
- [SDR CALA2025090208357](https://openairdocs.org/sdr/CALA2025090208357.md): Seat Track · corroded · Aug 28, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN SEAT TRACK -Y765 CORRODED AT FR 20. REMOVED AND REPLACED SEAT TRACK Y-765 AT BETWEEN FR12-FR24 IAW A 320 SRM 51-72-11-911-001.
- [SDR CALA2025090208356](https://openairdocs.org/sdr/CALA2025090208356.md): Floor Support · corroded · Aug 28, 2025 · N832UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOOR SUPPORT Y -765 HAS SPOTS OF CORROSION & SCRIBE MARKS AT FR67 AND 68. REMOVED AND REPLACED AFT CABIN WET AREA FLOOR SUPPORT -Y765 FR67 AN D 68 IAW SRM 53-41-14-03-A AND SRM 51-42-11/001.
- [SDR CALA2025082908262](https://openairdocs.org/sdr/CALA2025082908262.md): Dummy Rail · corroded · Aug 27, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN CTR DUMMY BEAM CORRODED AT FR21. REMOVED AND REPLACED NEW CTR DUMMY BEAM FROM FR 20 TO FR 24 IAW A319 SRM 51-42-11-001.
- [SDR CALA2025082908261](https://openairdocs.org/sdr/CALA2025082908261.md): Seat Track · corroded · Aug 27, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > FWD CABIN SEAT TRACK -Y1292 CORRODED AT FR20. REMOVED AND REPLACED SEAT TRACK Y-1292 FROM FR 12 TO FR 24 AT MA IN CABIN IAW SRM 51-42-11 AND SRM 51-72-11-911-001.
- [SDR CALA2025082908260](https://openairdocs.org/sdr/CALA2025082908260.md): Seat Track · corroded · Aug 27, 2025 · N832UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > -Y1292 FR 35-36 IS OUT OF LIMITS. REPLACED SEAT TRACK -Y1292 BTW FR 35 TO 36 IAW A319 SRM 51-72-11 AND SRM 51-42-11. SFR #1698.
- [SDR CALA2025082108015](https://openairdocs.org/sdr/CALA2025082108015.md): Floor Support · damaged · Aug 20, 2025 · N832UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN WET AREA FLOOR SUPPORT Y 765 HAD SCRIBE MARKS AT FR66. R & R THE FLOOR SUPPORT IAW SRM 51-72-1 1.
- [SDR CALA2025030702628](https://openairdocs.org/sdr/CALA2025030702628.md): Indication Sys · faulted · Mar 4, 2025 · N832UA · Airbus A319131 · Door Warning System
  > RIGHT OVERWING EXIT "SLIDE" DOES NOT INDICATE ARMED. INSTALL THE LOCK PIN ASSY ON THE INFLATION RESERVOIR IN THE AFT CARGO COMPARTMENT AS PER AMM 52-21-11-000-001-A STEP 3 A. ECAM PAGE INDICATION SHOWS RT HAND OVERWING DOOR CLOSED AND LATCHED BUT DOES NOT SHOW
- [SDR CALA2024112901348](https://openairdocs.org/sdr/CALA2024112901348.md): Chiller · malfunctioned · Nov 27, 2024 · N832UA · Airbus A319131 · Buffet/Galleys
  > AFT CHILLER OR CHILLERS MOTORS PULSATE ON/OFF. FA SMELLED ELECTR ICAL FA SMELL ELECTRIC BURN. OPERATED BOTH AFT GALLEY CHILLERS AND OPERATED NORMALLY. FOUND NO EVIDENCE OF ANY ELECTRICAL BURNING OR ODORS. ONLY SOURCE OF SMELL WAS A SMALL AMOUNT OF COFFEE ON A
- [SDR CALA2024092700698](https://openairdocs.org/sdr/CALA2024092700698.md): Fan · faulty · Sep 27, 2024 · N832UA · Airbus A319131 · Air Distribution Fan
  > WHILE PERFORMING SMOKE AND ODOR INSPECTION FOUND RT HAND RECERCULATION FAN C/B POPPED. UNABLE TO RESET. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE APPLY MEL # 2121B, CONTACT TOMC ONCE AT AIRCRAFT FOR DDP PROCEDURE.. UPDATED MAA CODE FIX USING VENDOR M
- [SDR CALA2023111703412](https://openairdocs.org/sdr/CALA2023111703412.md): Lens · wrong part · Nov 16, 2023 · N832UA · Airbus A319131 · Emergency Lighting
  > LEFT OVERWING EXIT DOOR LIGHTED SIGN LENS POINTING THE WRONG WAY REQ DEFER NEF 2522MP REJECTED MEL 2522MP-..LEGIBILTY OF SIGN IS CONSIDERED IMPAIRED DUE TO EXIT ARROW FACING THE WRONG DIRECTION. SINCE ITS EMERGENCY EXIT LIGHTING IT MUST BE FIXED. RPL LENS WITH
- [SDR CALA2023090402691](https://openairdocs.org/sdr/CALA2023090402691.md): Stringer · damaged · Sep 2, 2023 · N832UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > LH FR35 STGR28-31 HAS REJECTABLE DAMAGE INDICATIONS AT BULKHEAD HOLES AND AT LH STR31 AT FR35. "FR35 STGR 28LH-31LH BULKHEAD HOLES & LH STGR 31 AT FR35 WERE SOLUTION WITH INSP REQUIREMENTS. ACCOMPLISH A PERMANENT OR BEFORE 22-FEB-2024." REPAIRED AT BFM. REPAIR
- [SDR CALA2019083001458](https://openairdocs.org/sdr/CALA2019083001458.md): Cylinder · leaking · Aug 29, 2019 · N832UA · Airbus A319131 · Emergency Equipment
  > R2 PASSENGER CREW DOOR DAMPER EMERGENCY OPERATION CYCLINDER FOUND LEAKING. REMOVED AND REPLACED R2 DOOR EMERGENCY OPERATION CYLINDER DIAPHR AM IAW AMM 52-10-00-610-001-A.
- [SDR CALA2019083001447](https://openairdocs.org/sdr/CALA2019083001447.md): Skin · cracked · Aug 26, 2019 · N832UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DURING HMV-3/C-4 CHECK AT AAR DLH "REF NON-ROUTINE 9026654" ROTO PROBE INSP SHOWS CRACK INDICATION @ FR35 (HOLE#2) STRINGER 30RH SIDE @ 8 O''CLOCK. ACCOMPLISHED ITERIM REPAIR PER PART 1 OF ECRA 5331-02439.
- [SDR CALA2019082301410](https://openairdocs.org/sdr/CALA2019082301410.md): Door Frame · cracked · Aug 21, 2019 · N832UA · Airbus A319131 · Fuselage Main, Structure
  > AD 2018-03-12 EA 5340-01724 REV A OP 002 A-20 NO DOT ROTO PROBE INSP SHOWS CRACK INDICATION @ FR68 RH SIDE DOOR STOP #1 (BOTTOM DOOR STOP) LOWER I/B HOLE REPAIR BEFORE NEXT FLIGHT. ACCOMPLISHED FREEZE PLUG REPAIR TO FR68 RH SIDE DOOR STOP #1 LOWER I/B HOLE IAW
- [SDR CALA2019082301409](https://openairdocs.org/sdr/CALA2019082301409.md): Skin · dented · Aug 21, 2019 · N832UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DENT IN SKIN BETWEEN FR25-FR26 STR L/H 39-40 DENT IN FUSELAGE SKIN BETWEEN FR 25 AND FR 26 STR 39L AND 40L WA S OUT OF LIMITS. PERFROMED DUOBLER REPAIR IAW A319 SRM 53-00-11- 300-029. SIR INSPECTION THERSHOLD FROM THE TIME OF ADD EMP:V918695 ADL/REPAIR EMBODIM
- [SDR CALA2019082301408](https://openairdocs.org/sdr/CALA2019082301408.md): Bulkhead · cracked · Aug 21, 2019 · N832UA · Airbus A319131 · Fuselage Main, Bulkhead
  > L/H SIDE PRESSURE PANEL BTW FR 35-36 FASTNER HOLES OUTSIDE THE C UTOUT AREA #18, #19, #20, #24 AND #26 HAVE CRACK INDICATIONS. REPAIRED HOLES 18,19,20,24 AND 26 L/H SIDE PRESSURE PANEL BETW EEN FR35-36 IAW ECRA 5331-02433.
- [SDR CALA2019080401305](https://openairdocs.org/sdr/CALA2019080401305.md): Door Sill · corroded · Aug 2, 2019 · N832UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AAR NR 9027023, SPEC NO. A3NB-53-3-6222 DOTNO. A3-009 CORROSION ON L2 DOOR SILL BETWEEN AFT GIRTBAR FITTING LOWER PLATE AND FRA ME 68 REPLACED L2 DOOR SILL IAW A319 SRM 51-72-11 TREATED, PRIMED AND PAINTED IAW SRM 51-75-12.
- [SDR CALA2019080401304](https://openairdocs.org/sdr/CALA2019080401304.md): Door Sill · corroded · Aug 2, 2019 · N832UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > SPEC NO.A3NB-53-3-6222 DOTNO.A3-012 CORROSION ON R2 DOOR SILL TWO MOST INBOARD FASTENER HOLES NEXT AFT GIRT BAR LOWER ATTACH FIT TING AAR NR 9027032 REPLACED R2 DOOR SILL IAW SRM A319 51-72-11. TREATED, PRIMED AND PAINT IAW A319 SRM 51-75-12.
- [SDR CALA2017100903570](https://openairdocs.org/sdr/CALA2017100903570.md): Switch · stuck · Oct 9, 2017 · N832UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHTS STUCK IN THE ON POSITION. CYCLED NSFSB SWITCH. EMERGENCY LIGHTS OPS NORMAL.
- [SDR CALA2017091103151](https://openairdocs.org/sdr/CALA2017091103151.md): Power Supply · inoperative · Sep 11, 2017 · N832UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS TEST TO FAILED. REPLACED THE EPSU AND BATTERY 12WL IAW AMM 33-51-38, PB401.OK FOR SERVICE
- [SDR CALA2017071002179](https://openairdocs.org/sdr/CALA2017071002179.md): Switch · malfunctioned · Jul 10, 2017 · N832UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN ARMED OR OFF POSITION. RESET NSFSB SWITCH - OPS CHECKS GOOD.
- [SDR CALA2017061101791](https://openairdocs.org/sdr/CALA2017061101791.md): Socket · loose · Jun 11, 2017 · N832UA · Airbus A319131 · Electrical Power System
  > FA REPORTED ELECTRICAL BURNING ODOR AT ROWS 8-10. ODOR DISIPATED MINUTES LATER. ISOLATED TO ROWS 8-10. F/O WENT TO THE AREA OF ODOR & DID NOT DETECT ANYTHING. ODOR SEEMED TO BE ELECTRICAL IN NATURE. INSPECTED THE AREA FOR OBVIOUS ELECTRICAL PROBLEMS, FOUN
- [SDR CALA2016121901124](https://openairdocs.org/sdr/CALA2016121901124.md): Pcu · faulted · Dec 19, 2016 · N832UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHT TEST FAILS. MESSAGE IS AFT L PSCU IS AT FAULT. REPLACED EMERGENCY POWER CONTROL UNIT IAW 33-51-39.
- [SDR CALA2016081295639](https://openairdocs.org/sdr/CALA2016081295639.md): Connector · unsecure · Aug 9, 2016 · N832UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHT POWER SUPPLY WARNING LIGHT APPEARED DURING CIDS TEST. SECURED CONNECTOR AT THE POWER SUPPLY, OPS CHECKED GOOD.
- [SDR CALA2013122793995](https://openairdocs.org/sdr/CALA2013122793995.md): Battery · faulted · Dec 27, 2013 · N832UA · Airbus A319131 · Emergency Lighting
  > IAW NR 2 SVC ITEM R EMERGENCY LIGHT TEST FAULTS BATTERY EMERGENCY LIGHT 33-51-38. RESET LT EMERGENCY BATTERY AMM 24-50-00.
- [SDR CALA2013121693714](https://openairdocs.org/sdr/CALA2013121693714.md): Nut · damaged · Dec 13, 2013 · N832UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FASTENER ABOVE LT WING ESCAPE SLIDE PANEL ONE OUT. REPLACED CAPTION NUT & FASTENER.
- [SDR CALA2013111492937](https://openairdocs.org/sdr/CALA2013111492937.md): Liner · damaged · Nov 13, 2013 · N832UA · Airbus A319131 · Turbine Engine Air Inlet Section
  > ENG 1 INLET LINER HAS APPROXIMATELY 1-2 IN HANGING DOWN LOOSE AT 12 O'CLOCK POSITION.
- [SDR CALA2013081990543](https://openairdocs.org/sdr/CALA2013081990543.md): Sdac · unknown · Aug 18, 2013 · N832UA · Airbus A319131 · Hydraulic Indicating System
  > GREEN & YELLOW SYS LOW PRESSURE DISPLAYED ON UPPER ECAM SCREEN. REPLACED SDAC 1 IAW AMM, ALL INDICATIONS NORMAL.
- [SDR UALA2013052303580](https://openairdocs.org/sdr/UALA2013052303580.md): Switch · loose · May 22, 2013 · N832UA · Airbus A319131 · Audio Integrating System
  > CAPTAIN`S MICROPHONE TRIGGER ON SIDE STICK IS LOOSE. REPLACED IAW AMM AND ACCOMPLISHED OP TEST OF SIDE STICK ASSY, OPS NORMAL.
- [SDR UALA2013050203081](https://openairdocs.org/sdr/UALA2013050203081.md): Floor Panel · delaminated · May 1, 2013 · N832UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO PIT FLOOR PANEL 151ZG IS DELAMINATED 24 INCH BY 22 INCH, 7.5 INCH FROM FWD EDGE AND 4 INCH FROM DOOR EDGE. IPC REF 53-42-04-22X ITEM 90, P/N BF530014-103. SRM REF 53-02-00 PG 120. REMOVED AFT CARGO PIT FLOOR PANEL IAW IPC 53-42-04-22X FLOOR PNL 110
- [SDR UALA2013042602935](https://openairdocs.org/sdr/UALA2013042602935.md): Oxygen Mask · broken · Apr 26, 2013 · N832UA · Airbus A319131 · Crew Oxygen System
  > FIRST OFFICER`S OXYGEN MASK BROKEN. REPLACED OXYGEN MASK PER MM, OPS CHECKED OKAY.
- [SDR UALA2013042202773](https://openairdocs.org/sdr/UALA2013042202773.md): Position Sensor · out of adjust · Apr 21, 2013 · N832UA · Airbus A319131 · Rudder Control System
  > REF LOG 3 AUTO PILOT TRIMS A-C 2 UNITS LEFT RUDDER AND RIGHT 3 DEGREES BANK. -PER TSM 27-20-00-810-804- A ITEM 4A(1) ACP ADJ OF RUDDER POSITION INDICATING TO ITEM 4A 2 (A). CONTINUE WITH ITEM 4A2(C). ACP'D AFS TEST, AMM TASK 22-96-00 -710-001-A & EFCS-1, E
- [SDR UALA2013042202774](https://openairdocs.org/sdr/UALA2013042202774.md): Servo · faulted · Apr 19, 2013 · N832UA · Airbus A319131 · Aileron Control System
  > DURING FLIGHT CONTROL CHECK, RIGHT AILERON DOES NOT SHOW FULL DOWN TRAVEL INICATOR DOES NOT ENTER. REPLACED SERVO 33CE2 RIGHT GREEN SERVO ACTUATOR PER AMM. RIGGED AND OPS & LEAK CHECKED GOOD.
- [SDR UALA2013041502580](https://openairdocs.org/sdr/UALA2013041502580.md): Panel · damaged · Apr 14, 2013 · N832UA · Airbus A319131 · Nacelle/Pylon, Plate/Skin
  > NR 2 ENGINE OUTBOARD PYLON PANEL 482AR HAS WRINKLING DISTORTION ON THE LOWER EDGE BETWEEN THE FIRST TWO FASTENERS AND 1.5 INCHES AFT OF THE LEADING EDGE. REPLACED NR 2 OTBD PYLON PANEL UNDER WING LEADING EDGE.

Next page: https://openairdocs.org/aircraft/N832UA/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 = 'N832UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N832UA/reports

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