# Service difficulty reports: N853UA

A list on [N853UA](https://openairdocs.org/aircraft/N853UA.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 · 80 reports

- [SDR CALA2026042315642](https://openairdocs.org/sdr/CALA2026042315642.md): Fuel Cap · missing · Apr 22, 2026 · N853UA · Airbus A319131 · Fuel Storage
  > RAMP REPORTED FUEL CAP MISSING. INSTALLED MISSING FUEL CAP
- [SDR CALA2026012713321](https://openairdocs.org/sdr/CALA2026012713321.md): Floor Support · corroded · Jan 22, 2026 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RIGHT FR 68 - 70, -Y1292 FLOOR SUPPORT CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11/001.
- [SDR CALA2026011613007](https://openairdocs.org/sdr/CALA2026011613007.md): Floor Support · corroded · Jan 15, 2026 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT FLOOR SUPPORT Y765 CORRODED AT FASTENER HOLES BETWEEN FR 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT AT Y765, FR 66 - 70 IAW SRM 51-42-11/001.
- [SDR CALA2026011613006](https://openairdocs.org/sdr/CALA2026011613006.md): Floor Support · corroded · Jan 15, 2026 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > SECONDARY FINDING UPON REMOVING FLOOR PANEL FOR FLOOR SUPPORT REPLACEMENT, FOUND CORROSION ON FLOOR SUPPORT Y+160 HARDPOINT. REMOVED AND REPLACED THE FLOOR SUPPORT AT Y160 FR 68 TO 70 IAW SRM 51-42-11/001.
- [SDR CALA2026011613004](https://openairdocs.org/sdr/CALA2026011613004.md): Skin · contaminated · Jan 15, 2026 · N853UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SKIN HAS LIQUID INGRESS INDICATION 126 INCHE S FROM INBD, AND 9.5 INCHES FROM TRAILING EDGE. DRILLED WITNESS HOLES IN LT ELEVATOR UPPER SKIN 126IN FROM I/B 9.5IN FROM T/E. FOUND NO LIQUID, REPAIRED IAW SRM 55-21-11-30 0-004. CATEGORY A R
- [SDR CALA2026011613003](https://openairdocs.org/sdr/CALA2026011613003.md): Skin · contaminated · Jan 15, 2026 · N853UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SKIN HAS LIQUID INGRESS INDICATION 29 INCHES FROM INBD, AND 21 INCHES FROM TRAILING EDGE. DRILLED WITNESS HOLES IN LT ELEVATOR UPPER SKIN 29IN FROM I/B 21 IN FROM T/E ZONE A, FOUND NO LIQUID. REPAIRED AREA IAW SRM 5 5-21-11-300-004, CATE
- [SDR CALA2026011613002](https://openairdocs.org/sdr/CALA2026011613002.md): Skin · contaminated · Jan 15, 2026 · N853UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SKIN HAS LIQUID INGRESS INDICATION 156 INCHE S FROM INBD, AND 7.0 INCHES FROM TRAILING EDGE. DRILLED WITNESS HOLES ON ELEVATOR UPPER SKIN LT 156IN FROM I/B 7 IN FROM T/E ZONE A-C, FOUND NO LIQUID REPAIRED IAW SRM 55-2 1-11-300-004, CATEGO
- [SDR CALA2026011613001](https://openairdocs.org/sdr/CALA2026011613001.md): Skin · contaminated · Jan 15, 2026 · N853UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR UPPER SKIN HAS LIQUID INGRESS INDICATION 30 INCHES FROM INBD AND 16.5 INCHES FROM TRAILING EDGE. DRILLED WITNESS HOLES IN LT ELEVATOR UPPER SKIN 30IN FROM I/B 16.5IN FROM T/E ZONE A, FOUND NO LIQUID, REPAIRED AREA IAW SRM 55-21-11-300-004 CATE
- [SDR CALA2026011913086](https://openairdocs.org/sdr/CALA2026011913086.md): Pin · corroded · Jan 14, 2026 · N853UA · Airbus A319131 · Engine Mount Section
  > NR 1 ENGINE AFT MOUNT LOWER INBD, CENTER,OTBD INNER PINS & OTBD UPPER INNER PIN ARE CORRODED [04 PINS]. REPLACED NR 1 ENG AFT LOWER & UPPER, INNER PINS (INBD, CENTER & OTBD (4 PINS) IAW AMM 71-22-400-010-A.
- [SDR CALA2025081507832](https://openairdocs.org/sdr/CALA2025081507832.md): Brace · loose · Aug 15, 2025 · N853UA · Airbus A319131 · Cargo Compartments
  > FA REPORTS METAL BRACE UNDER 34D IS LOOSE. REMOVED BAGGAGE BAR FROM ROW 34DEF AND DEFERRED PER MEL 2521Y OK TO MEL. REMOVED AND ROUTED TO TERMINAL A STORES M&E 31-2526-3-0025 (139-00-293-21).
- [SDR CALA2025051404675](https://openairdocs.org/sdr/CALA2025051404675.md): Slide · deployed · May 14, 2025 · N853UA · Airbus A319131 · Escape Slide
  > LEFT OVERWING SLIDE DEPLOYED. REMOVED LH OFFWING SLIDE REF AMM TASK 25-62-42-000-002-A UP TO AND INCLUDING STEP 4.A.(5)(H) VERIFIED LEFT HAND OVERWING SLIDE WAS INSTALLED REF. AMM 25-62-42-400-001-A AND INFLATION (RESERVOIR) WAS INSTALLED REF AMM 25-62-46-400
- [SDR CALA2025051504689](https://openairdocs.org/sdr/CALA2025051504689.md): Unknown · unknown · May 14, 2025 · N853UA · Airbus A319131 · Cabin Equipment/Furnishings
  > AFT LAV D PAPER TOWEL DI SPENSOR SHOWS BURN MARK AND PAPER TOWELS SHOW SIGNS OF COMBUSTION. VISUALLY INSPECTED LAV D. NO SIGNS OF BURNING BEHIND PAPER TOWEL HOLDER. NO SIGNS OF SMOKING IN LAV. LAV DIDNT SMELL LIKE SMOKE. NO SIGNS OF BURN MARKS IN PAPER TOWE
- [SDR CALA2025041603892](https://openairdocs.org/sdr/CALA2025041603892.md): Switch · faulted · Apr 13, 2025 · N853UA · Airbus A319131 · Flight Compartment Equipment
  > CAP SEAT ELECTRIC ADJUSTMENT SWITCH MOVES SEAT ON ITS OWN. DEFERRED CAPT SEAT ELECTRIC ADJUSTMENT INOP REF MEL 2511C, MANUAL WORKS OK, CB U11 COLLARED, STICKER APPLIED. PERFORMED RII INSP OF CAPT SEAT INSTALL. VERIFIED TEST AND OPS C HECK OK, SEAT LOCKS IN
- [SDR CALA2025040803635](https://openairdocs.org/sdr/CALA2025040803635.md): Door · no discrepancy · Apr 7, 2025 · N853UA · Airbus A319131 · Emergency Exits
  > REMOVED LEFT AND RIGHT OVERWING EMERGENCY EXIT HATCHES AS REQ BY EXCESSIVE FLIGHT TURBULENCE INSPECTION REF LP 4422981 REINSTALLED LEFT AND RIGHT OVERWING EMERGENCY ESCAPES HATCHES REF AMM 52-21-11-400-001-A. VERIFIED ALL SAFTEY PINS REMOVED AND STORED.
- [SDR CALA2025032403151](https://openairdocs.org/sdr/CALA2025032403151.md): Trash Bin · odor · Mar 23, 2025 · N853UA · Airbus A319131 · Buffet/Galleys
  > POSSIBLE BURNING SMELL IN AFT GALLEY UP ON ARRIVAL SPOKE WITH CREW AND FOUNF THE SOURCE OF THE SMELL COMING FROM THE AFT GALLEY TRASH INTERNAL BIN. REPLACED AFT GALLEY INTENAL TRASH BIN. REQUESTING A CARRY TO HAVE CABIN RE-CECULATION FILTERS REPLACED WITHIN TW
- [SDR CALA2024080900398](https://openairdocs.org/sdr/CALA2024080900398.md): Fuel Cap · missing · Aug 6, 2024 · N853UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP MISSING. SEAL INTEGRITY GOOD. REQUESTING CDL 28A DISPATCH DESK: 09 NAME: AB DATE: 06-AUG-24- CDL 28A APPROVED PLACARDS
- [SDR CALA2023053101699](https://openairdocs.org/sdr/CALA2023053101699.md): Battery · no test · May 29, 2023 · N853UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (13WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR#5001235878-0010 EPSU BETTERY (13WL) FAILED ON EMERGENCY LIGHTING BATTERY S/N OFF:279090 QTY:1EA P/N ON:AD3214-31 S/N ON:283003 QTY:1EA CAPACITY TEST AND REQUIRE REPLACEMENT. B
- [SDR CALA2023053101697](https://openairdocs.org/sdr/CALA2023053101697.md): Battery · no test · May 29, 2023 · N853UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (10WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR#5001235874-0010. EPSU BETTERY (10WL) FAILED ON EMERGENCY LIGHTING BATTERY S/N OFF:283015 QTY:1EA P/N ON:AD3214-31 S/N ON:287739 QTY:1EA CAPACITY TEST AND REQUIRE REPLACEMENT.
- [SDR CALA2023053101696](https://openairdocs.org/sdr/CALA2023053101696.md): Battery · no test · May 29, 2023 · N853UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (11WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR# 5001235875-0010. EPSU BETTERY (11WL) FAILED ON EMERGENCY LIGHTING BATTERY S/N OFF:282995 QTY:1EA P/N ON:AD3214-31 S/N ON:282297 QTY:1EA CAPACITY TEST AND REQUIRE REPLACEMENT.
- [SDR CALA2023053101698](https://openairdocs.org/sdr/CALA2023053101698.md): Battery · no test · May 26, 2023 · N853UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (12WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR#5001235876-0010. EPSU BATTERY (12WL) FAILED ON EMERGENCY LIGHTING BATTERY P/N ON: AD3214-31 S/N ON:284086 QTY:1EA. CAPACITY TEST AND REQUIRE REPLACEMENT. BATTERY REPLACEMENT OF
- [SDR CALA2021051200645](https://openairdocs.org/sdr/CALA2021051200645.md): Landing · damaged · May 12, 2021 · N853UA · Airbus A319131 · Wing, Plate/Skin
  > RIGHT WING FUEL TANK PANEL LANDING BETWEEN RIB 13-14 HAS 2EA ELO NGATED HOLES. PER HAECO LCQ NR 9292607/38607 GENERATED BY V07796 0. REPAIRED 2EA HOLES AT RIGHT WING FUEL TANK PANEL 640HB LANDING B ETWEEN RIB 13-14 IAW SRM 57-21-11-300-002.THIS IS A CAT B REPA
- [SDR CALA2021042200522](https://openairdocs.org/sdr/CALA2021042200522.md): Door Sill · corroded · Apr 21, 2021 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL FR66 FLANGE FOUND TO BE OUT OF LIMITS PER NR 929244 1 AND WILL REQUIRE REPAIR AREA C PER NR 9292634 / 38634 REPAIRED L2 DOOR SILL AT FR66 IAW SRM 53-41-14-700-001.
- [SDR CALA2021042200520](https://openairdocs.org/sdr/CALA2021042200520.md): Stringer · corroded · Apr 21, 2021 · N853UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STR30R HAS CORROSION EXTENDING BETWEEN FR6 4-65. RMVD, LOCATED,DRILLED,DEBURRED AND INSTALLED STR31R FOR AFT CARG O COMPARTMENT FROM FR64 TO FR67 ALL IAW SRM 51-42-11/001,SRM 51- 44-11/001. TOP COATED FASTENERS IAW SRM 51-75-12-911-006.
- [SDR CALA2021042200518](https://openairdocs.org/sdr/CALA2021042200518.md): Intercostal · cracked · Apr 20, 2021 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RH FR-16 STOP #7 UPPER AND INBD LOWER HOLE HAS A CRACK INDICATIO N AT 1 O''CLOCK IN THE INTERCOSTAL GEN BY V061632 PER NR9292398 / 38398. REMOVED AND REPLACED RH FR16 STOP 7 INTERCOSTAL FITTING IAW A319 SRM 51-42-11-00 AND ECRA 5311-02542 DWG R531113118 BY MEC
- [SDR CALA2021042200517](https://openairdocs.org/sdr/CALA2021042200517.md): Intercostal · cracked · Apr 20, 2021 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RH FR-16 STOP #7 UPPER AND INBD LOWER HOLE HAS A CRACK INDICATIO N AT 1 O''CLOCK IN THE INTERCOSTAL GEN BY V061632 PER NR9292398 / 38398. REMOVED AND REPLACED RH FR16 STOP 7 INTERCOSTAL FITTING IAW A319 SRM 51-42-11-00 AND ECRA 5311-02542 DWG R531113118 BY MEC
- [SDR CALA2021042200516](https://openairdocs.org/sdr/CALA2021042200516.md): Intercostal · cracked · Apr 20, 2021 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LH FR16 #7 DOOR STOP UPPER AND LOWER INBD HOLES HAVE CRACK INDICATIONS PER NR9292406 / 38406 REMOVED AND REPLACED LH FR16 STOP 7 INTERCOSTAL FITTING IAW A319 SRM 51-42-11-001, ECRA 5311-02542 AND DWG R531113118.
- [SDR CALA2021042200513](https://openairdocs.org/sdr/CALA2021042200513.md): Shear Tie · corroded · Apr 20, 2021 · N853UA · Airbus A319131 · Fuselage Internal Mounting Structure
  > SHEAR TIE HAS CORROSION AT FR28 BETWEEN STR42-43R PER NR 929256 2 / 38562 GEN BY V925324 RMVD AND RPLD CLEAT SHEAR TIE AT FR28 BETWEEN STRG 42R TO 43R IA W SRM 53-21-12-11-A AND SRM 51-42-11-001 PARA E AND F PG 6-16. T REATED, PRIMED AND TOP COAT AREAS IAW SFR
- [SDR CALA2021042200511](https://openairdocs.org/sdr/CALA2021042200511.md): Door Sill · corroded · Apr 19, 2021 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL IS CORROED AT FR68 PER HAECO LCQ NON ROUTINE 929244 2/38442 GENERATED BY V061680 REPAIRED R2 DOOR SILL FR68 IAW SRM 53-41-14-283-002 AND 53-41-14 -300-001 BY MECH V914232 INSP BY V061629
- [SDR CALA2021041900496](https://openairdocs.org/sdr/CALA2021041900496.md): Shear Tie · corroded · Apr 19, 2021 · N853UA · Airbus A319131 · Fuselage Internal Mounting Structure
  > SHEAR TIE HAS CORROSION AT FR28 BETWEEN STR-42-43R PER NR 929256 2 / 38562. RMVD AND RPLD CLEAT SHEAR TIE AT FR28 BETWEEN STRG 42R TO 43R IA W SRM 53-21-12-11-A AND SRM 51-42-11-001 PARA E AND F PG 6-16. TREATED, PRIMED AND TOP COAT AREAS IAW SFRM 51-23-11-00
- [SDR CALA2021041600477](https://openairdocs.org/sdr/CALA2021041600477.md): Door Sill · out of limits · Apr 15, 2021 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FR68 L2 DOOR SILL FLANGE FOUND TO BE OUT OF LIMITS ON NR 9292441 AND WILL REQUIRE TO BE REPAIRED AREA A PER NR 9292635 / 38635 REPAIRED FR68 L2 DOOR SILL FLANGE IAW SRM 53-41-14-300-001 FIG 0 01 PRINCIPAL 7 SHEET 4.
- [SDR CALA2019031100379](https://openairdocs.org/sdr/CALA2019031100379.md): Toilet · leaking · Mar 8, 2019 · N853UA · Airbus A319131 · Waste Disposal System
  > EVIDENCE OF WATER LEAK COMING FROM AFT LAV. REMOVED AND REPLACED AFT LAV TOILET ASSY IAW AMM 38-31-41. OPERATIONAL CHECK NO LEAK FOUND. REF ECRA 2011-01000 FOR AIRCRAFT CLEAN UP PROCEDURES.WITHIN 36 MONTHS, ACP ECRA 2011-01000, LAVATORY SPILL, SECTION2.C., SUP
- [SDR CALA2019020400207](https://openairdocs.org/sdr/CALA2019020400207.md): Idg · inoperative · Feb 4, 2019 · N853UA · Airbus A319131 · AC Generator-Alternator
  > ON T/O GEN 2 FAULT ALSO TR2 FAULT ABLE TO GET GEN 2 BACK ON LINE AFTER GEAR DOWN LOST GEN PER AMM 24-21-51-000-010-A, STARTED REMOVAL OF NR 2 ENGINE IDG UP TO STEP 4C. REMOVED AND REPLACED THE NR 2 ENGINE GENERATOR IAW AMM 24-21-51 OPS AND LEAK CHK GOOD ITEM R
- [SDR CALA2017111104029](https://openairdocs.org/sdr/CALA2017111104029.md): Container · damaged · Nov 11, 2017 · N853UA · Airbus A319131 · Escape Slide
  > LEFT OVERWING SLIDE CONTAINER DISBONDED AND CRACKED.
- [SDR CALA2017111004015](https://openairdocs.org/sdr/CALA2017111004015.md): Container · damaged · Nov 10, 2017 · N853UA · Airbus A319131 · Escape Slide
  > RIGHT OVERWING SLIDE CONTAINER DISBONDED AND SEAL RETAINER HAS SHEARED RIVETS. INSTALLED A NEW OVERWING SLIDE.
- [SDR CALA2017051201378](https://openairdocs.org/sdr/CALA2017051201378.md): Light · malfunctioned · May 12, 2017 · N853UA · Airbus A319131 · Emergency Lighting
  > WITH A/C POWER OFF AND EMERGENCY LIGHT SWITCH SET TO ON, MULTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE. PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTINGS, FAULT SHOWN FOR LT FWD EMERGENCY POWER SUPPLY UNIT. RESET BREAKER AND PERFORMED OPERATIONAL TEST OF EMERGENC
- [SDR CALA2017051201377](https://openairdocs.org/sdr/CALA2017051201377.md): Power Supply · inoperative · May 12, 2017 · N853UA · Airbus A319131 · Emergency Lighting
  > WITH EMER LIGHTS ARMED AND A/C PWR TURNED OFF, ONLY CENTER CABIN EMER LIGHTS TURN ON. EMER LIGHTS TEST FROM PTP TESTED OK. REPLACED POWER SUPPLY UNIT AT AFT POSITION DUE UNIT FAILED INDICATION, REF AMM 33-51-38-400-001-A. REPLACED BATTERIES AT AFT, MID RIGHT A
- [SDR CALA2016101795809](https://openairdocs.org/sdr/CALA2016101795809.md): Skin · dented · Oct 14, 2016 · N853UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN RT DENT FOUND OUT OF LIMITS AT FR1-FR2 28+WL. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-11-PH4S FIG 230.
- [SDR CALA2016081195620](https://openairdocs.org/sdr/CALA2016081195620.md): Battery Pack · broken · Jun 9, 2016 · N853UA · Airbus A319131 · Emergency Equipment
  > AFT CABIN RH EMERGENCY FLASHLIGHT BATTERY PACK BROKEN. REPLACED AFT CABIN FLASHLIGHT BATT PACK, OPS CHECK GOOD
- [SDR CALA2016060195422](https://openairdocs.org/sdr/CALA2016060195422.md): Slide · damaged · May 28, 2016 · N853UA · Airbus A319131 · Escape Slide
  > DEPLOYED DEFLATED SLIDE ON R1 DOOR. REPLACED SLIDE IAW MM 25-62-44.
- [SDR CALA2014080191586](https://openairdocs.org/sdr/CALA2014080191586.md): Skin · damaged · Jul 29, 2014 · N853UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > LEFT AIRFONE ANTENNA AREA NEEDS REPAIRED AT FRAME 63 - 64 STRINGER 41 - 42LT VARIANT 002. REPAIRED IAW SRM 53-00-11 PARAGRAPH 4S FIG 230.
- [SDR CALA2014072891547](https://openairdocs.org/sdr/CALA2014072891547.md): Skin · dented · Jul 27, 2014 · N853UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN RT DENT FOUND OUT OF LIMITS AT FRAME 1 - 28 + WL. INSTALLED A 7 X 7 REPAIR IAW SRM 53-00-11 4S-230 PRINCIPLE 2. FIRST INSPECTION REQUIRED AT 77452 PTC. R & R IAW SRM 53-00-11-PH4S FIG 230. REINSPECT IAW SRI53-00-11-2-017-00.
- [SDR CALA2014072891546](https://openairdocs.org/sdr/CALA2014072891546.md): Shear Web · corroded · Jul 25, 2014 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RIGHT FRAME SUPPORT FOR SHEAR WEB FOUND CORRODED FRAME 69 - 70R PN 5347112320300. R & R SHEAR WEB IAW SRM 51-42-11.
- [SDR CALA2014072591512](https://openairdocs.org/sdr/CALA2014072591512.md): Door Sill · corroded · Jul 22, 2014 · N853UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > MAJOR REPAIR. R2 DOOR SILL HAS CORROSION AT GIRT BAR ATTACHMENT BETWEEN FRAME 66 & 68 AT STRINGER 43. AFTER REMOVING CORROSION, MATERIAL LOSS WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. R & R RT 2 DOOR SILL.
- [SDR CALA2013112593223](https://openairdocs.org/sdr/CALA2013112593223.md): Converter · faulty · Nov 23, 2013 · N853UA · Airbus A319131 · Windshield/Door Rain/Ice Removal
  > LT WINDSHIELD WIPER INOPERATIVE ANTI ICE. CAPTAIN`S WIPER WOULD NOT TURN OFF, CB PULLED. REPLACED CAPTAIN`S WIPER MOTOR CONVERTER IAW MM, OPERATIONS CHECKED OKAY.
- [SDR CALA2013082690748](https://openairdocs.org/sdr/CALA2013082690748.md): Door · out of adjust · Aug 24, 2013 · N853UA · Airbus A319131 · Fixed Inner Doors
  > COCKPIT DOOR LOWER LATCH DOES NOT APPEAR TO BE LOCKING PROPERLY. ADJUSTED COCKPIT DOOR. OPERATIONS CHECKED NORMAL.
- [SDR UALA2013052303589](https://openairdocs.org/sdr/UALA2013052303589.md): Oxygen Mask · frayed · May 23, 2013 · N853UA · Airbus A319131 · Crew Oxygen System
  > FIRST OFFICER`S O2 MASK HOSE IS FRAYED. REPLACED O2 MASK IAW AMM, OPS CHECKED GOOD.
- [SDR UALA2013051603381](https://openairdocs.org/sdr/UALA2013051603381.md): Mount · broken · May 14, 2013 · N853UA · Airbus A319131 · Passenger Compartment Equipment
  > SEAT 12DEF INBD AFT SEAT MOUNT BROKEN FASTENER. REPLACED AFT MOUNT.
- [SDR UALA2013040402233](https://openairdocs.org/sdr/UALA2013040402233.md): Power Supply · inoperative · Mar 31, 2013 · N853UA · Airbus A319131 · Emergency Lighting
  > CIDS EMERGENCY TEST INDICATES DOOR 1L FAIL. REPLACED POWER SUPPLY AND BATTERY AS REQ, 1L MESSAGE EXTINGUISHED. OPS CHECK GOOD.
- [SDR UALA2013030401269](https://openairdocs.org/sdr/UALA2013030401269.md): Pump · damaged · Mar 2, 2013 · N853UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > GREEN SYSTEM HYD RESERVIOR OVERHEAT ON. CREW FOLLOWED FM. NOTED ECAM MSG GREEN RESERVOIR OVHT MESSAGE AT TOP OF DESCENT. HYD FLUID RESERVOIR CHECKS GOOD AT ARRIVAL. ACFT DECLARED AMBER TO SFO. FOUND DPI POPPED ON CASE DRAIN AND EDP SHAFT SHEARED. REPLACE
- [SDR UALA2013020700757](https://openairdocs.org/sdr/UALA2013020700757.md): Oil System · leaking · Feb 6, 2013 · N853UA · Airbus A319131 · Turbine Engine Oil System
  > DURING ENGIINE SHUTDOWN, EXCESSIVE SMOKE FROM EXHAUST. INSPECTION REVEALED PUDDLE OF OIL IN LOWER TURBINE CASE. NR 2 ENGINE RUN PER JRH 2-40-6 HPT DRY-OUT PROCEDURE. ACCOMPLISHED TWO, TEN MINUTE IDLE RUNS, NO OIL PUDDLING OR SMOKE PRESENT AFTER IDLE RUNS

Next page: https://openairdocs.org/aircraft/N853UA/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 = 'N853UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N853UA/reports

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