# Service difficulty reports: N835UA

A list on [N835UA](https://openairdocs.org/aircraft/N835UA.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 · 94 reports

- [SDR CALA2026040315050](https://openairdocs.org/sdr/CALA2026040315050.md): Nacelle · no discrepancy · Apr 3, 2026 · N835UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > CREW AND RAMP REPORTED NR 2 ENGINE COWLING BIRD STRIKE. PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-51-14-200-803-A, RADOME AND WALK AROUND TO VERIFY NO FURTHER DAMAGE. SUBTASK 05-51-14-210-078-E, INSPECTION OF NR 1 ENGINE/NACELLES. ALL DEBRIS WAS FOUND IN
- [SDR CALA2026012213174](https://openairdocs.org/sdr/CALA2026012213174.md): Fuel Cap · missing · Jan 21, 2026 · N835UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING ON ARRIVAL. REPLACED THE FUEL CAP IAW AMM 28-25-41
- [SDR CALA2025120511814](https://openairdocs.org/sdr/CALA2025120511814.md): Eec · faulted · Dec 3, 2025 · N835UA · Airbus A319131 · Fuel Controlling System
  > SETTING TAKEOFF POWER. ENG 1 LAGGED IN POWER. ABORTED TO. WHILE RETURN ENG 1 EPR MODE FAULT PERFORMED TSM TASK 73-22-00-810-857-A LOSS OF THE P4.9 (P5) INPUT ON ENGINE 1, NO DAMAGED FOUND ON P5 PRESSURE TUBES, REMOVED AND REPLACED E1 EEC IAW AMM 73-22-34/401
- [SDR CALA2025112811582](https://openairdocs.org/sdr/CALA2025112811582.md): Anti-Ice Valve · warning message · Nov 24, 2025 · N835UA · Airbus A319131 · Engine Anti-Icing System
  > ANTI ICE ENG2 VALVE OPEN IN FLIGHT CREW REPORTS THEY CYCLED NR 2 ANTI ICE SWITCH SWITCH ON GROUND AND MESSAGE CLEARED. NO MESSAGE ON ARRIVAL AT GATE. REF AMM 30-21-00/001 CONFIG 13
- [SDR CALA2025111211161](https://openairdocs.org/sdr/CALA2025111211161.md): Panel · cracked · Nov 8, 2025 · N835UA · Airbus A319131 · Passenger/Crew Doors
  > L-1 DOOR EXTERNAL SKIN UPPER PLATE FWD CORNER HAS CRACK. R & R THE L1 DOOR EXTERNAL SKIN UPPER PLATE IAW SRM 51-72-11-941-001.
- [SDR CALA2025101410063](https://openairdocs.org/sdr/CALA2025101410063.md): Web · cracked · Oct 11, 2025 · N835UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LH SHEAR WEB FR68-FR69 IS CRACKED. REMOVED AND REPLACED SHEAR WEB AT LH FR 68-69 STRG 23L IAW A319 SRM 51-72-11-911-001.
- [SDR CALA2025101510120](https://openairdocs.org/sdr/CALA2025101510120.md): Angle · cracked · Oct 10, 2025 · N835UA · Airbus A319131 · Fuselage Main, Structure
  > LEFT EMERGENCY EXIT AFT VERTICAL FRAME CRACKED. REMOVED AND REPLACED WITH NEW ANGLE SEGMENT IAW SRM 51-72- 11-911-001.
- [SDR CALA2025100909835](https://openairdocs.org/sdr/CALA2025100909835.md): Skin · contaminated · Oct 3, 2025 · N835UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS A LIQUID INGRESS INDICATION 39" FROM INBD 12" FROM TRAILING EDGE 2"X 2". REPAIRED LEFT ELEVATOR 39" FROM INBD 12" FROM TRAILING EDGE ZONE A AS REQUIRED IAW SRM 55-21-11-300-005 CATEGORY A REPAIR A.
- [SDR CALA2025100909834](https://openairdocs.org/sdr/CALA2025100909834.md): Skin · contaminated · Oct 3, 2025 · N835UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS A LIQUID INGRESS INDICATION 45.5" FROM INBD 15" FROM TRAILING EDGE 4" X 2" IN SIZE. REPAIRED LEFT ELEVATOR 45.5" FROM INBD 15" FROM TRAILING EDGE Z ONE A AS REQUIRED IAW SRM 55-21-1-300-005 CATEGORY A REPAIR.
- [SDR CALA2025100609648](https://openairdocs.org/sdr/CALA2025100609648.md): Skin · contaminated · Oct 3, 2025 · N835UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT ELEVATOR HAS A LIQUID INGRESS INDICATION 139 IN FROM INBD 10.5"IN FROM TRAILING EDGE 2" X 2" IN SIZE. REPAIRED RH WLWVATOR UPPER SKIN 139IN FROM I/B 10.5IN FROM T/E 2.5IN DIA ZONE A IAW SRM 55-21-11-300-005 CATEGORY A
- [SDR CALA2025100609646](https://openairdocs.org/sdr/CALA2025100609646.md): Skin · contaminated · Oct 3, 2025 · N835UA · Airbus A319131 · Elevator, Plate/Skin
  > RIGHT ELEVATOR HAS A LIQUID INGRESS INDICATION 142.5" FROM INBD 15.5" TRAILING EDGE 4"X 2" SIZE. REPAIRED R/H ELEVATOR UPPER SKIN 142.5IN FROM I/B 15.5IN FROM T/ E ZONE A 3IN DIA IAW A319 SRM 55-21-11-300-005 CATEGORY A.
- [SDR CALA2025081107531](https://openairdocs.org/sdr/CALA2025081107531.md): Light · faulted · Aug 8, 2025 · N835UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING TEST RESULTS WITH FAULT EPSU EXT LOAD EMER R. REPLACED RT AFT EMERGENCY OVERWING LIGHT ASSY IAW AMM 33-51-15-400-001-A, OPS TESTED GOOD.
- [SDR CALA2025071406505](https://openairdocs.org/sdr/CALA2025071406505.md): Oxygen Box · no test · Jul 11, 2025 · N835UA · Airbus A319131 · Passenger Oxygen System
  > SEAT 21DEF OXYGEN MASK COMPARTMENT DID NOT OPEN DURING OPERATIONAL REST. REMOVED OXYGEN BOX AT SEAT 21DEF, REF AMM 35-21-41. READY FOR INSPECTION PART NUMBER VERIFICATION AND CLEARANCE TO INSTALL. PART VERIFICATION AND CLEARANCE NOT REQUIRED FOR INSTALLATIO
- [SDR CALA2025040703563](https://openairdocs.org/sdr/CALA2025040703563.md): Unknown · odor · Apr 6, 2025 · N835UA · Airbus A319131 · Air Distribution System
  > FAS RPT BURNING ODOR IN AFT GALLEY. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. INVESTIGATE AFT GALLEY FOR ODORS, RUN OVEN, COFFEE MAKERS, LIGHTS, ETC. ACCOMPLISHED INSPECTION REF AMM 05-51-10. OPERATED OVEN, C
- [SDR CALA2025031302800](https://openairdocs.org/sdr/CALA2025031302800.md): Reservoir · low · Mar 12, 2025 · N835UA · Airbus A319131 · Hydraulic Reservoir, Main
  > HYD Y RES OVHT YELLOW SYSTEM RESOVOIR QUANTITY WAS BELOW THE REQUIRED SERVICE LEVEL. SERVICED YELLOW SYSTEM PER AMM 12-12-29. REMOVED AND REPLACED THE YELLOW CHECK VALVE Y(3083) PER AMM29-24-21-000-001. ACCOMPLISHED TEST 3 IDLE LEAK CHECK PER 71-00-00-710-012
- [SDR CALA2025013002122](https://openairdocs.org/sdr/CALA2025013002122.md): Battery Pack · no test · Jan 28, 2025 · N835UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - LEFT BATTER FAILED THE CAPACITY TEST. REMOVED AND REPLACED CABINE EMERGENCY LIGHTING TC:17-3351-1-7100 AND 18-3351-1-7100, OPS CHECK GOOD
- [SDR CALA2024022100488](https://openairdocs.org/sdr/CALA2024022100488.md): Intercostal · dented · Feb 13, 2024 · N835UA · Airbus A319131 · Passenger/Crew Doors
  > L1 DOOR CUT OUT AFT LOWER CORNER INTERCOSTAL FITTING #1 HAS A DENT.
- [SDR CALA2024022700551](https://openairdocs.org/sdr/CALA2024022700551.md): Skin · damaged · Feb 9, 2024 · N835UA · Airbus A319131 · Nacelle/Pylon, Plate/Skin
  > LH PYLON IB SAIL TAIL PNL, HAS HEAT DAMAGE.
- [SDR CALA2024022100485](https://openairdocs.org/sdr/CALA2024022100485.md): Plate · dented · Feb 8, 2024 · N835UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > UNABLE TO DO ROTO-PROBE INSPECTION AT LH FR68 STGR16 HOLES 1-5 DUE TO NOT MEETING ROUND CONDITIONS. W/C:88534
- [SDR CALA2024022100487](https://openairdocs.org/sdr/CALA2024022100487.md): Gusset · dented · Feb 8, 2024 · N835UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > UNABLE TO DO ROTO-PROBE INSPECTION AT LH FR68 STGR12 HOLES 1-5 DUE TO NOT MEETING ROUND CONDITIONS. W/C:88532
- [SDR CALA2024022100486](https://openairdocs.org/sdr/CALA2024022100486.md): Gusset · dented · Feb 8, 2024 · N835UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > (A3NB-53-4-6355) RH FR66 INNER CAP FRAME TO THE GUSSET PLATE AT STGR 10 HOLES 1-5 NOT MEETING TRUE ROUND CONDITION. W/C:88517
- [SDR CALA2023062802040](https://openairdocs.org/sdr/CALA2023062802040.md): Connector · broken · Jun 27, 2023 · N835UA · Airbus A319131 · Light System Wiring
  > SEAT ROW 22LH EMERGENCY PATHWAY LIGHTING CONNECTOR BROKEN PER STS NR 0017. DURING T/S FOUND BROKEN TERMINAL OF THE EMERGENCY ESCAPE PATHWAY LIGHT. REPLACED TERMINAL PER EPSM 20-48-14-01 STEP B. PREFORMED OP CHECK PER A319 AMM 33-51-00-710-008-A. SYSTEM CHECK G
- [SDR CALA2023031500767](https://openairdocs.org/sdr/CALA2023031500767.md): Unknown · unknown · Mar 15, 2023 · N835UA · Airbus A319131 · Standard Practices/Structures
  > HIGH SPEED REJECTEDTAKEOFF AT 100KTS PERFORMED INSPECTION AFTER HIGH SPEED REJECTED TAKEOFF PER A319/320 A..M.M 05-51-16-200-001-A FOUND BRAKE TEMP WITHIN LIMITS FUSE PLUGS AND TIRES GOOD PER PHASE ONE INSPECTION
- [SDR 2023FA0000031](https://openairdocs.org/sdr/2023FA0000031.md): Seal · cracked · Jan 17, 2023 · N835UA · Airbus A319131 · Turbine Section
  > NR 2 ENGINE STAGE 6 TURBINE INNER AIR SEAL CRACKED, IAW VRS4018, HAS BEEN FOUND IN THE FPI PROCESS. LIFE LIMITED PART TO BE RETIRED WITH 8577 CYCLES REMAINING (LLP LIMIT IS 20000 CYCLES)
- [SDR CALA2022122603493](https://openairdocs.org/sdr/CALA2022122603493.md): Anti-Ice Valve · faulted · Dec 26, 2022 · N835UA · Airbus A319131 · Airfoil Anti/De-ice System
  > WING A.ICE SYS FAULT DISPLAYED ON ECAM. BOTH L&R WAI VALVES IN THE CLOSED POSITION L&R WAI VALVES IN THE CLOSED POSITION. ACCOMPLISHED WAI TEST USING ENGINE AIR TEST PASS. INDICATIONS NORMAL, CYCLED CBS C1/C2/F1/Q7 FAULT MESSAGES CLEAR.
- [SDR CALA2022020300301](https://openairdocs.org/sdr/CALA2022020300301.md): Shock Absorber · overserviced · Feb 2, 2022 · N835UA · Airbus A319131 · Landing Gear Door Retract Section
  > L/G GEAR NOT UPLOCKED ECAM AFTER T/O.SHOCK ABSORBER FAULT SEE L/P 7923622 FOR SERVICE ON NOSE LANDING GEAR SHOCK STRUT. PERFORMED FUNCTIONAL TEST OF THE NORMAL EXTENSION AND RETRACTION O F THE LANDING GEAR AS PER MM-32-31-00-720-002-A. ALL TEST PASSED SEE L/P
- [SDR CALA2022020100287](https://openairdocs.org/sdr/CALA2022020100287.md): Intercostal · cracked · Jan 31, 2022 · N835UA · Airbus A319131 · Fuselage Main, Frame
  > AD RELATED (AD 2019-20-10) L-1 DOOR STOP #7 I/B LOWER HOLE AND U PPER HOLE HAVE CRACK INDICATIONS IN INTERCOSTAL LAYER. GENERATED BY V061632 PER NR 9292224 (40224) AT HAECO LCQ. SUPPORT TASK. FR 16 ACCOMPLISH INITIAL INSPECTION AT LH FRAME 20 DOOR STOP #1 AND
- [SDR CALA2022020100286](https://openairdocs.org/sdr/CALA2022020100286.md): Intercostal · cracked · Jan 31, 2022 · N835UA · Airbus A319131 · Fuselage Structure (General)
  > AD RELATED (AD 2019-20-10) R-1 DOOR STOP #1 I/B UPPER AND LOWER HOLES HAVE CRACK IN INTERCOSTAL LAYER. FR16. SUPPORT TASK. GENER ATED BY V061632 AT HAECO LCQ PER NR 9292218 (40218) REPAIRED R-1 DOOR STOP #1 I/B UPPER AND LOWER HOLES PER ECRA 531 1-02751 AND HA
- [SDR CALA2022020100284](https://openairdocs.org/sdr/CALA2022020100284.md): Intercostal · cracked · Jan 31, 2022 · N835UA · Airbus A319131 · Fuselage Main, Frame
  > AD RELATED (AD 2019-20-10) R1 DOOR STOP #7 I/B UPPER AND LOWER H OLES HAVE CRACK INDICATIONS IN THE FRAME LAYER. SUPPORT TASK. GE NERATED AT HAECO LCQ PER NR 9292222 AT HAECO LCQ BY V061632. FR 16 ACCOMPLISH INITIAL INSPECTION AT L/H FRAME 20 DOOR STOP #1 HOLE
- [SDR CALA2022020100285](https://openairdocs.org/sdr/CALA2022020100285.md): Intercostal · cracked · Jan 31, 2022 · N835UA · Airbus A319131 · Fuselage Main, Frame
  > AD RELATED (AD 2019-20-10) L-1 DOOR STOP #7 I/B LOWER HOLES HAVE CRACK INDICATIONS IN FRAME LAYER. FR20. GENERATED BY V061632 AT HAECO LCQ PER NR 9292225 (40225) SUPPORT TASK..2640 FINAL DIA.3397 #3 HOLE.2888 AND FINAL.3397. ACCOMPLISH OF THE LASTEST REVIS
- [SDR CALA2022011400148](https://openairdocs.org/sdr/CALA2022011400148.md): Stringer Splice · corroded · Jan 13, 2022 · N835UA · Airbus A319131 · Fuselage Structure (General)
  > FWD CARGO STRINGER SPLICE STR 41L FR30-FR31 CORRODED. REMOVED AND REPLACED STRINGER SPLICE ON STR 41 LEFT BETWEEN FRAM ES 30-31 IAW A320 SRM 51-72-11
- [SDR CALA2022011400140](https://openairdocs.org/sdr/CALA2022011400140.md): Frame · corroded · Jan 13, 2022 · N835UA · Airbus A319131 · Fuselage Structure (General)
  > FWD CARGO BLIGE AREA 42R REPAIR CORRODED FR 22-27 REMOVED EXISTING REPAIR BUT & TRIMMED SECTION OF REPAIR AND INST ALLED IN FWD CARGO PIT BETWEEN FR 26-27RT ON STRINGER 42RT IAW A 320 SRM 51-72-11 AND SRM 53-21-13-300-003
- [SDR CALA2022010300015](https://openairdocs.org/sdr/CALA2022010300015.md): Anti-Ice System · fault message · Jan 3, 2022 · N835UA · Airbus A300* · Airfoil Anti/De-ice System
  > SYS FAULT DISPLAYED ON UPPER ECAM SCREEN. - WING ANTI-ICE. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V907081 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. T-S WING ANT
- [SDR CALA2020012600218](https://openairdocs.org/sdr/CALA2020012600218.md): Floor Support · corroded · Jan 17, 2020 · N835UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CABIN FLOOR STRUCTURE AT Y765, FRAME 70 WAS CORRODED. REMOVED AND REPLACED AFT CABIN FLOOR STRUCTURE AT Y765 BETWEEN FRAMES 66 - 70 IAW 51-42-11 PAR 2.D, AND 51-49-00 TABLE 11.
- [SDR CALA2020011000114](https://openairdocs.org/sdr/CALA2020011000114.md): Shear Web · corroded · Jan 8, 2020 · N835UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > N/R 6226504: A3NB-53-3-6185 AFT CABIN R/H SHEAR WEB BETWEEN FR 6 9 AND FR 70 HAS CORROSION. REMOVED AND REPLACED R/H SHEAR WEB IN AFT CABIN REF SRM 51-42-11. DATA WAS TRANSCRIBED FROM PAPER DOC UAL N/R 6226504, WORK ACP BY MECH INSP ON 07JAN20.
- [SDR CALA2020011000113](https://openairdocs.org/sdr/CALA2020011000113.md): Shear Web · corroded · Jan 8, 2020 · N835UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > N/R 6226502: A3NB-53-3-6185 AFT CABIN L/H SHEAR WEB BETWEEN FR 6 9 AND FR 70 HAS CORROSION. REMOVED AND REPLACED L/H AFT SHEAR WEB IN AFT CABIN IAWE SRM 51- 42-11. DATA WAS TRANSCRIBED FROM PAPER DOC UAL N/R 6226502, WORK ACP BY MECH INSP ON 07JAN20.
- [SDR CALA2020010600063](https://openairdocs.org/sdr/CALA2020010600063.md): Skin · dented · Dec 30, 2019 · N835UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DENT LH SIDE UNDER SECOND WINDOW BETWEEN FR23 & 24, JUST ABOVE GOLD STRIP. REPORTED BY MOVE TEAM EVALUATED DENT: D=.036" T=.079" A=2.0". DENT IS TYPE 1, ZONE 1. ACCOMPLISHED EXTERNAL DVI (TEMPORARY SOLUTION), NO DEFECTS NOTED IAW SRM 53-11-11-283-012. MUST AC
- [SDR CALA2019090601502](https://openairdocs.org/sdr/CALA2019090601502.md): Contactor · defective · Sep 6, 2019 · N835UA · Airbus A319131 · AC Power Distribution System
  > CAPT LOST A BOTH SREENS AND BOTH EWD AND SD WERE FLASHING OFF SUSPECT LOSS OF AC BUS1 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PERFORM TEST OF AC ESSENTIAL GEN SWITCHING PER AMM 24-25-00-710- 001. MAC METER INITIATED FOR WITH VENDOR MAC RELATED WORK ORDER
- [SDR CALA2018120202476](https://openairdocs.org/sdr/CALA2018120202476.md): Warning System · false activation · Nov 30, 2018 · N835UA · Airbus A319131 · Airfoil Anti/De-ice System
  > WING A. ICE SYS FAULT UPPER ECAM ON CLIMBOUT WHEN WING ANTI-ICE SELECTED. TROUBLESHOT PER TSM 30-11-00-810-805-A / 30-11-00-810-803-A / 32-31-00-810-842-A. UNABLE TO DUPLICATE FAULT ON GROUND. PER TSM 30-11-00-810-805-A CLEANED BOTH LEFT AND RIGHT WAI VALVE FI
- [SDR CALA2018082701847](https://openairdocs.org/sdr/CALA2018082701847.md): Battery · no test · Aug 23, 2018 · N835UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY LEFT FAILED AN EMERGENCY LIGHT TEST. REMOVED AND REPLACED THE BATTERY IAW AMM 33-51-38. OPS CHECKED GOOD.
- [SDR CALA2017120104248](https://openairdocs.org/sdr/CALA2017120104248.md): Door Sill · corroded · Dec 1, 2017 · N835UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > SUPPORT TASK - UPON REMOVAL OF FLOOR PANEL IN AFT CARGO PIT FOUND CORROSION ON DOOR SILL IB COVER SHEET R&R COVER SHEET IN AFT CARGO PIT FR56-59RT, P/N: D5347715400, PO:1039704.1 IAW A319 SRM 51-42-11.
- [SDR CALA2017051201374](https://openairdocs.org/sdr/CALA2017051201374.md): Battery · faulty · May 12, 2017 · N835UA · Airbus A319131 · Emergency Lighting
  > CABIN EEL LIGHTS SYSTEM CHECK - MAINTENANCE MESSAGE EPSU BATT FWD L, EPSU BATT EM RT. REPLACED EEL LIGHTS BATTS REF AMM 33-51-38. OPS CHECK GOOD
- [SDR CALA2017032100672](https://openairdocs.org/sdr/CALA2017032100672.md): Power Supply · inoperative · Mar 21, 2017 · N835UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED. REPLACED EMERGENCY POWER SUPPLY REF 33-51-38. OPS CHECK GOOD.
- [SDR CALA2015051593784](https://openairdocs.org/sdr/CALA2015051593784.md): Battery · discharged · May 14, 2015 · N835UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED FWD LT BATTERY. REPLACED EMER LT BATTERY AT DOOR 1L. OPERATIONS CHECKED NORMAL IAW MM 33-51-38.
- [SDR CALA2014102992625](https://openairdocs.org/sdr/CALA2014102992625.md): Chiller · malfunctioned · Oct 28, 2014 · N835UA · Airbus A319131 · Buffet/Galleys
  > REPORT OF EXHAUST SMELL NEAR FWD AFT LAVATORY, AFT GALLEY AREA. FOUND AFT GALLEY FWD CHILLER BLUE POWER LIGHT FLASHING, WITH LITTLE OR NO AIRFLOW FROM CHILLER. UNIT SHUTS OFF & RESTARTS. REPLACED AFT GALLEY FWD CHILLER, CLEANED FILTER. NO SMELL AFTER REPLA
- [SDR CALA2014101392394](https://openairdocs.org/sdr/CALA2014101392394.md): Slat · dented · Oct 8, 2014 · N835UA · Airbus A319131 · Leading Edge Devices
  > NUMBER 2 LT SLAT HAS DENT AT INBD END THAT IS OUT OF LIMITS. DAMAGE REMOVED & DOUBLER REPAIR INSTALLED IAW SRM 57-40-00. HFEC IAW NTM 51-10-08 PB6.
- [SDR CALA2014100792374](https://openairdocs.org/sdr/CALA2014100792374.md): Door Sill · corroded · Oct 5, 2014 · N835UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL HAS CORROSION AT NUTPLATE HOLES AT AFT INBD END. REMOVED CORROSION & FOUND BEYOND SRM ALLOWABLE LIMITS. REPAIR AT R2 DOOR SILL IAW SRM 53-41-14 FIG 201 SHEET 3, REPAIR PRINCIPLE 4.
- [SDR CALA2014060591212](https://openairdocs.org/sdr/CALA2014060591212.md): Sensor · faulty · Jun 3, 2014 · N835UA · Airbus A319131 · Landing Gear Position and Warning
  > UNABLE TO RETRACT LG AFTER TAKEOFF. INSTALLED RT MLG EXTEND SENSOR 20GA IAW MM 32-31-73-400-001-A. FIRST SENSOR FROM STOCK WAS NO HELP. TRIED SECOND SENSOR & ALL WAS GOOD. SHOOK OUT WIRING FROM 20GA TO THE JUNCTION BOX ON TOP OF THE GEAR. RAN ENGS FOR 5 M
- [SDR CALA2014010890091](https://openairdocs.org/sdr/CALA2014010890091.md): Epr System · faulted · Jan 8, 2014 · N835UA · Airbus A319131 · Engine Pressure Ratio (EPR)
  > DIVERTED TO IAD DUE TO AN EPR MODE FAULT ON THE NR 1 ENG.
- [SDR CALA2013123094054](https://openairdocs.org/sdr/CALA2013123094054.md): Battery · faulty · Dec 29, 2013 · N835UA · Airbus A319131 · Battery/Charger System
  > BCL 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ELEC REPLACED NR 2 BATTERY IAW AMM 24-38-51 PG 401, ALL TESTS PASSED.

Next page: https://openairdocs.org/aircraft/N835UA/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 = 'N835UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N835UA/reports

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