# Service difficulty reports: N805UA

A list on [N805UA](https://openairdocs.org/aircraft/N805UA.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 · 117 reports

- [SDR CALA2025073107122](https://openairdocs.org/sdr/CALA2025073107122.md): Sensor · unsecure · Jul 25, 2025 · N805UA · Airbus A319131 · Door Warning System
  > CARGO DOOR OPEN ECAM ON TAXI OUT. FOUND FWD CARGO DOOR CLOSED INDICATION SWITCH ASSY LOOSE, UNABLE TO TIGHTEN DUE TO DAMAGED HARDWARE, CLOSED DOOR AND VERIFIED FWD CARGO DOOR CLOSED AND LATCHED IAW AMM 52-70-00-040-001-A, R & R THE FWD CARGO DOOR PROXIMITY
- [SDR CALA2025011601934](https://openairdocs.org/sdr/CALA2025011601934.md): Unknown · smoke · Jan 13, 2025 · N805UA · Airbus A319131 · Standard Practices/Structures
  > TOWER REPORTED THATTHEY OBSERVED WHITE SMOKE FROM THE TIRE AREA ON TAKEOFF. PERFORMED A GVI OF THE BRAKING SYSTEM AND TIRE REF AMM 32-40-00-210-801-A & 32-41-00-210-002-A NO DEFECTS NOTED. PERFORMED A WALK AROUND THE AIRCRAFT FOR HYDRAULIC LEAKS NO DEFECT
- [SDR CALA2025011401898](https://openairdocs.org/sdr/CALA2025011401898.md): Battery Pack · no test · Jan 12, 2025 · N805UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - AFT LEFT EPSU BATTERY BAD REPLACED BATTERY WITH SERVICEABLE ONE FROM STOCK. OPS CHECK GOOD.PARTS USED:18-3351-3-0001,QTY:1
- [SDR CALA2024092700697](https://openairdocs.org/sdr/CALA2024092700697.md): Pressure Switch · faulty · Sep 25, 2024 · N805UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > HYD G RSV LO LVL DEBREIFED CREW. #1 EDP WAS SHUT DOWN IMMEDIATLY WHEN LOW PRESSURE INDICATION APPEARED. FLUID LEVEL UPDATE REPLACED LOW LEVEL SWITCH REF TASK 29-11-41-000-003-A. TASK 29-11-41-400-003-A. OPS CHECK GOOD. QTY INDICATOR NORMAL.
- [SDR CALA2024053101650](https://openairdocs.org/sdr/CALA2024053101650.md): Battery Pack · discharged · May 30, 2024 · N805UA · Airbus A319131 · Lighting System
  > EMERGENCY EPSU BATTERY AFT L FAILS OPERATIONAL CHECK. REF TO PEMCO NR 15402.0026 REMOVED AND REPLACED EPSU BATTERY AT 13WL IAW A319 AMM 33-51-38- 000-002-A AND A319 AMM 33-51-38-400-002-A. OPERATIONAL TEST GOOD IAW A319 AMM 33-51-00-710-001-A
- [SDR CALA2024050601327](https://openairdocs.org/sdr/CALA2024050601327.md): Window · leaking · May 2, 2024 · N805UA · Airbus A319131 · Flight Compartment Windows
  > WATER LEAKING IN COCKPIT MEAR AFT BASE OF FO SIDE WINDOW FAIRHURST, FOUND EXTERIOR SEAL SPLIT IN FWD UPPER CORNER-ALLOWING RAIN TO SEEP IN. ACCOMPLISHED REPAIR PER MT56-003 REV A WITH SILICONE. REPAIR COVERED WITH TAPE. TAPE TO BE RECHECKED EACH FLIGHT AND R
- [SDR CALA2024032900905](https://openairdocs.org/sdr/CALA2024032900905.md): Fuel Cap · missing · Mar 27, 2024 · N805UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUELER REPORTED FUEL CAP MISSING DEFERRING MISSING CAP PER CDL, MX ACTION CW DEFERRED DEFERRED DISPATCH DESK: 28 NAME: JG DATE: 27-MAR-24- OK TO APPLY CDL 28A FOR MISSING FUEL CAP-CAP WAS MISSING ON ARRIVAL. STLOO CONFIRM FUEL CAP WAS LEFT ON TRUCK-NO
- [SDR CALA2023090402676](https://openairdocs.org/sdr/CALA2023090402676.md): Cap · missing · Aug 26, 2023 · N805UA · Airbus A319131 · Aircraft Fuel Distribution System
  > PDA2 - EXTERIOR WALK AROUND {A3NB-06-3-6001} - FUEL CAP MISSING AT RIGHT WING CAP, COUPLING R OFF 31-2825-9-0001 7042 ON 0000 CAP, COUPLING R OFF 31-2825-9-0001 7042 ON 31-2825-9-0001 0598 INSTALLED REFUEL DEFUEL COUPLING CAP REF AMM 28-25-41. NO DEFECTS NOTED
- [SDR CALA2023082802652](https://openairdocs.org/sdr/CALA2023082802652.md): Fuel Cap · missing · Aug 26, 2023 · N805UA · Airbus A319131 · Aircraft Fuel System
  > EXTERIOR WALK AROUND {A3NB-06-3-6001} - FUEL CAP MISSING AT RIGHT WING. CAP, COUPLING R OFF 31-2825-9-0001 7042 ON 0000 CAP, COUPLING R OFF 31-2825-9-0001 7042 ON 31-2825-9-0001 0598 INSTALLED REFUEL DEFUEL COUPLING CAP REF AMM 28-25-41. NO DEFECTS NOTED.
- [SDR CALA2023080402420](https://openairdocs.org/sdr/CALA2023080402420.md): Skin · damaged · Aug 3, 2023 · N805UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > REFERENCE LP# 5057236 DAMAGE SITES #2-4, AC SUSTAINED GROUND DAMAGE TO FUSELAGE APPROXIMATELY FWD OF FR65 TO AFT OF FR66 & S32L - S35L. AVO10948 ISSUED FOR REPAIR. PARAGRAPH. ENSURE THAT THERE IS NO DAMAGE TO THE ADJACENT WATER ADJACENT STRINGER, FRAME, CLEATS
- [SDR CALA2022071501759](https://openairdocs.org/sdr/CALA2022071501759.md): Skin · damaged · Jul 14, 2022 · N805UA · Airbus A300* · Fuselage Floor Panel
  > DURING A MAINTENANCE HMV-4 CHECK PRODUCTION REPORTED A MILLED DOUBLER ON THE FUSELAGE SKIN AT FR34/STR43 WHILE PERFORMING THE REQUIRED INSPECTION PER UAL EA 5300-02120 REV C OP 001. BETWEEN STGR44 AND STGR42HR PER PART-2 OF THE LATEST REVISION OF ECRA 5321-020
- [SDR CALA2022071501757](https://openairdocs.org/sdr/CALA2022071501757.md): Fitting · damaged · Jul 14, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > WHILE WORKING FLEET CAMPAIGN DIRECTIVE # 5330-05575 FIG 14 HOLE DIAMETER REPORTING RH, HOLES R1,R2,R3,R7,R8,R9,R10,R11,R12,R13,R 14,R15,R16,R17,R18,R19,R20,R21,R72,R73,R75, & R76 WITH DAMAGE AS MARKED ON FIG SHEET R11, R12, R13, R14, R15, R16, R17, R18, R19, R
- [SDR CALA2022070801672](https://openairdocs.org/sdr/CALA2022070801672.md): Door Sill · corroded · Jul 8, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > CABIN FLOOR STRUCTURE FR66 Y-1162 HAS CORROSION REMOVED CORROSION ON R2 DOOR SILL IAW SRM 51-74-00. FOUND TO BE OUT LIMITS IAW SRM 53-41-24-283 ORIGINAL THICKNESS 0.315" D=0.09 5". DOOR SILL REMOVED AND REPLACED IAW SRM 51-72-11-911-001. EMP: V933866 WC: 3208
- [SDR CALA2022062701593](https://openairdocs.org/sdr/CALA2022062701593.md): None · corroded · Jun 27, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > CABIN FLOOR SUPPORT STRUCTURE BTW FR66-FR68, Y-1292, FLOOR BEAM WITH CORROSION,REMOVED CORROSION ON CABIN FLOOR BEAM FR68 Y-1292, MEASURED ORIGINAL THICKNESS.160 D=0.110" L=1.920" W=2.200" FOUND OUT OF LIMITS. FLOOR BEAM REMOVED AND REPLACED STA: ST ENG BFM.
- [SDR CALA2022062401571](https://openairdocs.org/sdr/CALA2022062401571.md): None · corroded · Jun 24, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > AFT CABIN L2 DOORWAY, SHAPE SILL HAS CORROSION ON AFT END (NR 32 255). ON REMOVAL OF THE SHAPE SILL, CORROSION WAS FOUND. ON THE TOP FACE OF THE DOOR SILL. CORROSION WAS REMOVED AND FOUND OUT OF LIMITS AND REPLACED SHAPE SILL, DOOR SILL AND CORNER FITTINGS
- [SDR CALA2022062401576](https://openairdocs.org/sdr/CALA2022062401576.md): None · corroded · Jun 24, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > CABIN FLOOR SUPPORT STRUCTURE, FR65-FR66, Y-1732, BEAM WITH CORROSION (NR 32193) FLOOR BEAM REMOVED IAW SRM 51-72-11-911-001 AND INSTALLED NEW BE AM IAW SRM 51-42-11/001. EMP: V936191 WC: 32193 STA: ST ENG BFM SFR# 1028881
- [SDR CALA2022062401566](https://openairdocs.org/sdr/CALA2022062401566.md): Skin · dented · Jun 23, 2022 · N805UA · Airbus A319131 · Wing Structure
  > DENT RIGHT WING #1 SLAT, INBOARD OF THE ENGINE. BY A PERMANENT STRUCTURAL REPAIR WITHIN 5,000 FC OR 10,000 FH OR 24 MONTHS,WHICHEVER OCCURS FIRST.WORKED PERFORMED BY U163564. SLAT DENT DIMENSIONS L6.75 W3.75 D.190 IN SKIN AREA 3. PERFORMED REPAIR PER SRM 51-73
- [SDR CALA2022062401574](https://openairdocs.org/sdr/CALA2022062401574.md): Seat Track · corroded · Jun 22, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > CABIN FLOOR SUPPORT STRUCTURE BTW FR66-FR68, Y-1292, FLOOR BEAM WITH CORROSION
- [SDR CALA2022062201551](https://openairdocs.org/sdr/CALA2022062201551.md): Channel · corroded · Jun 21, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > AFT CABIN L2 DOORWAY, SHAPE SILL HAS CORROSION ON AFT END (NR 32 255)
- [SDR CALA2022062201550](https://openairdocs.org/sdr/CALA2022062201550.md): Floor Support · corroded · Jun 21, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > CABIN FLOOR SUPPORT STRUCTURE, FR65-FR66, Y-1732, BEAM WITH CORR OSION (NR 32193)
- [SDR CALA2022061501516](https://openairdocs.org/sdr/CALA2022061501516.md): None · corroded · Jun 15, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > AFT CARGO DOOR CUTOUT LOWER SILL TORQUE BOX UPPER SURFACE CORROD ED AROUND 3EA TIE DOWN FITTINGS BETWEEN FR56-FR58 REMOVED LOWER SILL IAW SRM 51-42-11/001 AND FABRICATED NEW LOWER SILL IAW SRM 57-72-11-911 (2024-T3) 0,125" AND INSTALLED NEW LO WER SILL IAW SRM
- [SDR CALA2022061501502](https://openairdocs.org/sdr/CALA2022061501502.md): Plate · corroded · Jun 14, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > AFT CARGO DOOR CUTOUT LOWER SILL TORQUE BOX UPPER SURFACE CORROD ED AROUND 3EA TIE DOWN FITTINGS BETWEEN FR56-FR58 REMOVED LOWER SILL IAW SRM 51-42-11/001 AND FABRICATED NEW LOWER SILL IAW SRM 57-72-11-911 (2024-T3) 0,125" AND INSTALLED NEW LO WER SILL IAW SRM
- [SDR CALA2022061301495](https://openairdocs.org/sdr/CALA2022061301495.md): Structure · cracked · Jun 13, 2022 · N805UA · Airbus A319131 · Cargo Compartments
  > FWD CARGO COMPARTMENT, FR30-FR34, AFT BULKHEAD, LH SIDE, LOWER S UPPORT STRUCTURE CRACKED. REMOVED PROFILE (PLATE) FWD CARGO FR34 IAW SRM 51-42-11. RECEIVE D NEW PLATE. LOCATED AND DRILLED NEW PLATE IAW SRM 51-44-11/001. INSTALLED NEW PLATE IAW SRM 51-42-11/00
- [SDR CALA2022061301494](https://openairdocs.org/sdr/CALA2022061301494.md): None · corroded · Jun 13, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > MAIN CABIN FLOOR STRUCTURE FR68, Y-765 HAS CORROSION REMOVED CORROSION AT MAIN CABIN FLOOR STRUCTURE FR68, Y-765 IAW P/N D5347219320000, BATCH 0002756757. EMP: V936054 WC: 32082 STA SMR 51-74-00. FOUND TOBE OUT OF LIMIT AT HARD POINT AREA IAW SRM: ST ENG BFM
- [SDR CALA2022061301488](https://openairdocs.org/sdr/CALA2022061301488.md): Beam · corroded · Jun 12, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > CABIN FLOOR STRUCTURE FR66 Y-1162 HAS CORROSION. DETAILS AWAITED
- [SDR CALA2022061301485](https://openairdocs.org/sdr/CALA2022061301485.md): Plate · damaged · Jun 10, 2022 · N805UA · Airbus A319131 · Fuselage Structure (General)
  > RH FR68 AND FR66 INNER CAP JOINT TO THE GUSSET PLATES FROM STRIN GER 10 TO STRINGER 16 HAS DAMAGE INDICATION IN ALL HOLES NOTED. DAMAGE CLASSIFIED AS OUTROUND HOLES AND GOUGES. REAMED TO 0.1865" ALL HOLES AT RH FR66 AND FR68 FROM STR10 TO ST STA: ST ENG BFM R1
- [SDR CALA2022060801471](https://openairdocs.org/sdr/CALA2022060801471.md): Floor Support · corroded · Jun 8, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > CABIN FLOOR SUPPORT STRUCTURE BTW FR64-FR70, Y160.5, BEAM WITH C ORROSION REMOVED CORROSION ON CABIN FLOORBEAM AND FOUND WITHIN LIMITS IA W A320 SRM 53-00-14-283-002 L=2" W=1", D=.014" (MAX DEPTH ALLOWE D=.016") AND COUPLINGS REMOVED AND REPLACED IAW A320 SRM
- [SDR CALA2022060801457](https://openairdocs.org/sdr/CALA2022060801457.md): Support · cracked · Jun 7, 2022 · N805UA · Airbus A319131 · Fuselage Structure (General)
  > FWD CARGO COMPARTMENT, FR30-FR34, AFT BULKHEAD, LH SIDE, LOWER SUPPORT STRUCTURE CRACKED.
- [SDR CALA2022060801456](https://openairdocs.org/sdr/CALA2022060801456.md): Beam · corroded · Jun 7, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > MAIN CABIN FLOOR STRUCTURE FR68, Y-765 HAS CORROSION
- [SDR CALA2022060201429](https://openairdocs.org/sdr/CALA2022060201429.md): Floorbeam · corroded · Jun 2, 2022 · N805UA · Airbus A319131 · Fuselage Main, Floor Beam
  > CABIN FLOOR STRUCTURE BEAM BETWEEN FR68/FR69 AND Y160.5 HAS CORR OSION. REMOVED AND INSTALLED FLOORBEAM MAIN CABIN FR68 TO FR70 LH Y160.5 IAW SRM A319 51-42-11. P/N: D5347219620000 - BATCH NOL 000392 206. EMP: V935976 WC: 32167 STA: ST ENG BFM SFR# 1028737
- [SDR CALA2022060201424](https://openairdocs.org/sdr/CALA2022060201424.md): Beam · corroded · Jun 2, 2022 · N805UA · Airbus A319131 · Fuselage Main, Structure
  > CABIN FLOOR SUPPORT STRUCTURE BTW FR64-FR70, Y160.5, BEAM WITH C ORROSION
- [SDR CALA2022060101408](https://openairdocs.org/sdr/CALA2022060101408.md): Beam · corroded · May 31, 2022 · N805UA · Airbus A319131 · Fuselage Main, Floor Beam
  > CABIN FLOOR STRUCTURE BEAM BETWEEN FR68/FR69 AND Y160.5 HAS CORROSION.
- [SDR CALA201812112544](https://openairdocs.org/sdr/CALA201812112544.md): Seal · missing · Dec 8, 2018 · N805UA · Airbus A319131 · Engine Thrust Reverser
  > ENG 2 HAS VISIBLE GAP BETWEEN TOP OF NACELLE & PYLON ABEAM COM P RESSOR SECTION TOP LEFT FOUND THE #2 ENG UPPER AFT C DUCT SEAL MISSING P/N 740-0104-29. REMOVED THE DAMAGED SEAL AND REPLACED WITH NEW. REF AMM 78-32-00
- [SDR CALA2017112404203](https://openairdocs.org/sdr/CALA2017112404203.md): Battery · faulty · Nov 24, 2017 · N805UA · Airbus A319131 · Emergency Lighting
  > CIDS EMERGENCY SYSTEM FAILED THE 2 SERVICE CHECK, BATTERY FAILED FWD LT AND EPSU EMERGENCY L AND EPSU EMER R. REPLACED EPSU BATTERIES AT (10WL), (11WL), AND (12WL) PER MM33- 51-38-400-002, OPS CHECKS GOOD.
- [SDR CALA2017060501683](https://openairdocs.org/sdr/CALA2017060501683.md): Altimeter · sticking · Jun 5, 2017 · N805UA · Airbus A319131 · Altimeter, Barometric/Encoder
  > STANDBY ALTIMETER INDICATION ERRONEOUS STBY ALTIMETER NEEDLE STICKS WHILE CLIMBING AND DESCENDING. REPLACED STANDBY ALTIMETER IAW AMM34-21-22-400-001-B. LIGHTING OPERATIONAL TEST PASSED.
- [SDR CALA2017021300364](https://openairdocs.org/sdr/CALA2017021300364.md): Proximity Switch · out of adjust · Feb 13, 2017 · N805UA · Airbus A319131 · Door Warning System
  > DOOR 2R SLIDE ARMING PROX SWITCH 7NW2 WAS FOUND OUT OF TOLERANCE. ADJUSTED THE DOOR 2R SLIDE ARMING PROXIMITY SWITCH 7NW2 WITH REF TO AMM 52-71-00-820-002-A01.
- [SDR CALA2017021300354](https://openairdocs.org/sdr/CALA2017021300354.md): Oven · faulty · Feb 13, 2017 · N805UA · Airbus A319131 · Buffet/Galleys
  > AFT GALLEY OVEN R42 POPPED ITS CB AS IT WAS PUT UNDER LOAD FOR REPORTED BURNING SMELL IN CABIN. INSTALLED SERVICEABLE OVEN OPS CHECK GOOD.
- [SDR CALA2017021200331](https://openairdocs.org/sdr/CALA2017021200331.md): Oven · defective · Feb 12, 2017 · N805UA · Airbus A319131 · Buffet/Galleys
  > ELECTRICAL BURNING SMELL THROUGHOUT CABIN. NO SMOKE PULLED FWD AND AFT GALLEY BREAKERS, APPLY POWER TO GALLEYS. TURNED ONE GALLEY DEVICE AT A TIME. FOUND NO FAULTS OR ODORS IN FORWARD GALLEY. AFT GALLEY DID PRESENT SOME HEAT/OVERHEAT ODORS AT TIMES, NOT ELE
- [SDR CALA2017021000310](https://openairdocs.org/sdr/CALA2017021000310.md): Skin · damaged · Feb 10, 2017 · N805UA · Airbus A319131 · Rudder, Plate/Skin
  > DURING RUDDER INSTALL FOUND SMALL PUNCTURE ON RT SIDE OF RUDDER ABOUT 18 INCHES AFT OF LOWER FWD HOST POINT AND 20 INCHES UP FROM BOTTOM OF RUDDER ALSO A SCRATCH ON UPPER HALF. PERMANENT REPAIR ACCOMPLISHED PER ECRA 5540-01477 AND REO L205285.
- [SDR CALA2017012300170](https://openairdocs.org/sdr/CALA2017012300170.md): Battery Pack · faulted · Jan 23, 2017 · N805UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT SYS TEST FAULTED FOR THE EPSU UNIT AND AFT EPSU BATTERY. REPLACED BATTERY PACK, TEST PASSED. IAW MM 33 51 38 000 002A,
- [SDR CALA2016083095699](https://openairdocs.org/sdr/CALA2016083095699.md): Connector · damaged · Aug 27, 2016 · N805UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS AT SEATS 11C, 29C DO NOT ILLUMINATE WHEN POWER OFF 11C OK, REPINNED SEAT 29C CONNECTOR, OPS CHECKED GOOD
- [SDR CALA2016082695687](https://openairdocs.org/sdr/CALA2016082695687.md): Lamp · inoperative · Aug 24, 2016 · N805UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS AT SEATS 11C, 29C DO NOT ILLUMINATE WHEN POWER IS OFF. REPLACED THE LAMPS, TESTED OK.
- [SDR CALA2016080995610](https://openairdocs.org/sdr/CALA2016080995610.md): Wire Harness · not reported · Aug 8, 2016 · N805UA · Airbus A319131 · Landing Gear System Wiring
  > NOSE WHEEL STEERING FAULT ECAM MESSAGE. EMERGENCY DECLARED AND LANDED OK. REPLACED NOSE GEAR HARNESS 2M, OPS CHECKED OK IAW MM 32-21-43-400-003-A
- [SDR CALA2016060895439](https://openairdocs.org/sdr/CALA2016060895439.md): Connector · dirty · Jun 7, 2016 · N805UA · Airbus A319131 · Landing Gear System Wiring
  > TWO ECAMS UPON AUTO BRAKE ARM WHEEL, NOSE WHEEL STEERING FAULT & BRAKES SYS 1 FAULT. EMER DECLARED TO ENSURE LONG RNWY. PFR FAULTED BSCU STEERING FDBK SENSORS, 3GC - 4GC. CLEANED CONNECTOR ON SERVO CTL NOSE WHEEL STEERING, 6GC, & ALL FAULTS WENT AWAY IAW TS
- [SDR CALA2015111794820](https://openairdocs.org/sdr/CALA2015111794820.md): Flap · malfunctioned · Nov 10, 2015 · N805UA · Airbus A319131 · Trailing Edge Flap Control System
  > FLAPS LOCKED AT POSITION 2, WING TIP BRAKES ENGAGED AT 190 KTS, RESET WTB FLAPS IAW AMM 27-50-00-869-006. PREFORMED OPERATIONS FLAP TEST IAW AMM 27-54-00-710-001, TESTED OK. ALSO CFDS SFCC 1 & 2 BITE TESTED OK IAW AMM 27-51-00. FLAPS WTB FAULT MSG CLEARED.
- [SDR CALA2015021293136](https://openairdocs.org/sdr/CALA2015021293136.md): Connector · not seated · Feb 8, 2015 · N805UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHT TEST FAILED WITH MSG EPSU INTERNAL LOAD EMER RT IAW TSM 33-51-00-810-807A. RESEAT CONNECTOR 12WL. GND OPERATIONS TESTED AMM 33-51-58 & NO DEFECTS NOTED.
- [SDR CALA2014062091305](https://openairdocs.org/sdr/CALA2014062091305.md): Warning System · false activation · Jun 17, 2014 · N805UA · Airbus A319131 · Bleed Air Indicating System
  > COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN, ENG PARAMETERS NORMAL. OCCURRED DURING CLIMB OUT WAS JUST MOMENTARY. THEN REOCCURRED DURING TAXI-IN & REMAINED DISPLAYED. WORKED WITH LOCAL MAINTENANCE & FOUND FAULT ACRONYM B25TK IN FADEC. TROUBLESHOOTING ON
- [SDR CALA2014010790066](https://openairdocs.org/sdr/CALA2014010790066.md): Light · inoperative · Jan 6, 2014 · N805UA · Airbus A319131 · Emergency Lighting
  > DOOR 1L SLIDE LIGHTS INOPERATIVE IAW TSM 33-51-00 -810-808-A.
- [SDR CALA2014010290019](https://openairdocs.org/sdr/CALA2014010290019.md): Starter · malfunctioned · Dec 31, 2013 · N805UA · Airbus A319131 · Engine Starter
  > START FAULT DISPLAYED ON UPPER ECAM SCREEN ENG 2. ENG 2 START FAULT LO START AIR PRESS, CHECK BLD AIR SUPPLY NR 2, ITEM ROLLED FWD. NORMAL AIR PRESS BUT NO ROTATION. MX ATTEMPTED STICK START, REPORTED AIR BLEED LEAK UNDER COWL. REPLACED THE ENG NR 2 START
- [SDR CALA2013111292851](https://openairdocs.org/sdr/CALA2013111292851.md): Actuator · faulty · Nov 10, 2013 · N805UA · Airbus A319131 · Stabilizer Actuator
  > ELAC 2 INOPERATIVE. ECAM F CTL ELAC 2 PITCH FAULT RESET TWICE CAME BACK AFTER 1 MIN EACH TIME. IAW TSM 27-93-00-810-836-A REPLACED PITCH TRIM ACTUATOR IAW AMM 27-44-57-000-001-A & GROUND CHECKED NORMAL.

Next page: https://openairdocs.org/aircraft/N805UA/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 = 'N805UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N805UA/reports

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