# Service difficulty reports: N844UA

A list on [N844UA](https://openairdocs.org/aircraft/N844UA.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 · 98 reports

- [SDR CALA2026080618336](https://openairdocs.org/sdr/CALA2026080618336.md): Unknown · odor · Aug 4, 2026 · N844UA · Airbus A319131 · Air Distribution System
  > BURNING ELECTRICAL ODOR BY ROWS 21 AND 27 NO ELECTRICAL BURNING ODOR NOTED AT THIS TIME IN THE CABIN OR FLIGHT DECK WITH BOTH ENGINES RUNNING AND BOTH PACKS ON IAW AMM 05-51-10-200-801-C1. OK FOR SERVICE.
- [SDR CALA2026012613292](https://openairdocs.org/sdr/CALA2026012613292.md): Pressure Gauge · unknown · Jan 26, 2026 · N844UA · Airbus A319131 · Emergency Equipment
  > L1 DOOR PRESSURE GAUGE IS VERY DIFFICULT TO READ. L-1 DOOR ESCAPE SLIDE PRESSURE IS VISIBLE, IAW AMM 25-62-44. ACFT OK FOR SERVICE.
- [SDR CALA2026012613282](https://openairdocs.org/sdr/CALA2026012613282.md): Pressure Gauge · dirty · Jan 26, 2026 · N844UA · Airbus A319131 · Emergency Equipment
  > DOOR PRESSURE GAUGE VERY VERY DIFFICULT TO READ AT 1L CHECK DOOR 1L SLIDE INFLATION RESERVOIR PRESSURE WAS PERFORMED IAW TASK 25-62-00-210-001-A AND CLEANING OF THE PEEPHOLE
- [SDR CALA2025102410478](https://openairdocs.org/sdr/CALA2025102410478.md): Battery · no test · Oct 22, 2025 · N844UA · Airbus A319131 · Emergency Lighting
  > ON PERFORMING EMERGENCY LIGHTING TEST FOUND FAULTED (EPSU UNIT EMERG LEFT). ATA 33-51-38. REMOVED AND REPLACED EPSU BATTERY LEFT REF AMM 33-51-38/401, OPS CHECK GOOD.
- [SDR CALA2025101610187](https://openairdocs.org/sdr/CALA2025101610187.md): Adr · faulted · Oct 13, 2025 · N844UA · Airbus A319131 · Air Data Computer
  > NAV ADR 1 FAULT LAND VERIFY REQUIRED CYCLED RELATED BREAKERS, RERACKED ADIRU 1 AND PERFORMED BITE TEST OF ADIRU AND IRU TWICE REF AMM 34-13-00-740 AND AMM 34-14-00-740-004 TEST PASSED ON BOTH ATTEMPTS AND TESTED ADIRU 2 AND 3 ALL TESTS PASSED VIEW PICTURES TAK
- [SDR CALA2025100209536](https://openairdocs.org/sdr/CALA2025100209536.md): Cover · chipped · Oct 2, 2025 · N844UA · Airbus A319131 · Escape Slide
  > SLIDE COVER 2R PAINT CHIPPING
- [SDR CALA2025092909346](https://openairdocs.org/sdr/CALA2025092909346.md): Power Supply · faulted · Sep 29, 2025 · N844UA · Airbus A319131 · Emergency Lighting
  > EPSU UNIT EMERGENCY RIGHT FAULT. REMOVED & REPLACED RT EPSU (12WL) IAW AMM 33-51-38, OPS CHECK GOOD.
- [SDR CALA2025092609304](https://openairdocs.org/sdr/CALA2025092609304.md): Power Supply · faulted · Sep 25, 2025 · N844UA · Airbus A319131 · Emergency Lighting
  > EPSU UNIT EMER LEFT FAULTED, REMOVED AND REPLACED LT OVERWING EPSU POWER SUPPLY IAW AMM 33-51-38-000-001-A. OPS CHECK OK, OK FOR SERVICE.
- [SDR CALA2025092609302](https://openairdocs.org/sdr/CALA2025092609302.md): Battery · faulted · Sep 25, 2025 · N844UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY FWD L FAULTED. REMOVED AND REPLACED FWD L EPSU BATTERY AMM REF 33-51-38-000-002-A. OPS CHECK OK, OK FOR SERVICE.
- [SDR CALA2025090208382](https://openairdocs.org/sdr/CALA2025090208382.md): Control Panel · faulted · Aug 31, 2025 · N844UA · Airbus A319131 · Communications System
  > LOST INTERCOM IN COCKPIT AND ALL COMMUNICATIONS NOTHING OUTGOING OVER 100KNOTS AN AUDIBLE AUTOTHRUST CAUTION THROUGH V1 TAKE OFF. REESTABLISHED AUTOTHRUST AFTER LEVEL OFF AT 5000 FT. THEN WAS ABLE TO ESTABLISH COMMS WITH ACP3. FAULTS CLEARED ON POWER TRANSFE
- [SDR CALA2025052905058](https://openairdocs.org/sdr/CALA2025052905058.md): Power Supply · no test · May 28, 2025 · N844UA · Airbus A319131 · Emergency Lighting
  > FOUND SEVERAL EMERG AISLE LIGHTS OUT T/S EMERGENCY LIGHT SYSTEM FOUND POWER SUPPLY (11WL) BAD ON LEFT SIDE UNDER EMERGENCY EXIT DOOR ROW 21ABC. REMOVED AND REPLACED POWER SUPPLY LEFT CENTER REF AMM 33-51-38. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.
- [SDR CALA2025021302311](https://openairdocs.org/sdr/CALA2025021302311.md): Filter · faulted · Feb 12, 2025 · N844UA · Airbus A319131 · Cabin Temperature Control System
  > HOT AIR FAULT TURNED OFF HOT AIR PER ECAM POST FLIGHT REPORT FAULTED TRIM AIR PRESS VALVE FAILURE, PER TSM TASK 21-63-00-810-805-A STEP 4A (1) REPLACED TRIM AIR PRESSURE-REGULATING VALVE FILTER (REF. AMM 21-63-00-920-001). PERFORMED OPS CHECK TEST OF CAB TEMP
- [SDR CALA2024112701327](https://openairdocs.org/sdr/CALA2024112701327.md): Audio Control · unknown · Nov 25, 2024 · N844UA · Airbus A319131 · Communications System
  > AT 120KTS HAD COMPLETE RADIO AND INTERCOMM TRANSMISSION FAILURE ON VHF1 VHF2 AND VHF3 FOUND VHF 1 2 AND 3 OPERATING NORMALLY. ESTABLISHED COMMUNICATION WITH GROUND OPS USING ALL THREE VHF. ACCMP RMP BITE REF AMM 23-13-00-740-001-A FOR RMP 1 2 AND 3. ACCMP VHF
- [SDR CALA2024080600378](https://openairdocs.org/sdr/CALA2024080600378.md): Actuator · failed · Aug 6, 2024 · N844UA · Airbus A319131 · Compressor Bleed Control
  > COMPRESSOR VANE DISPLAYED ON UPPER ECAM SCREEN. ENGI NE PARAMETE RS NORMAL. - ENG 2 65KTS ENG2 COMP VANEON ECAM. INITIATEDABORT 70KTS. MAX SPD85KTS. SHUT ENG2 DOWN FOUND #2 ENGINE VARIABLE STATOR VANE ACTUATOR FAILED REF TSM 75-30-00-810-846-A. REMOVED #2 ENGI
- [SDR CALA2024080500365](https://openairdocs.org/sdr/CALA2024080500365.md): Cap · missing · Aug 5, 2024 · N844UA · Airbus A319131 · Aircraft Fuel System
  > PDA 2 REF L/P 8803799 FUEL CAP MISSING SPOKE TO TOMC AND ADVISED FUEL CAP MISSING.FUEL CAP MISSING, NO LEAKS ON NOZZLE NOTED. FUEL CAP NIS. M&E 31-2825-9-0001. COMPLIED WITH CDL. DISPATCH DESK: 00 NAME: BB DATE: 02-AUG-24- APPROVED CDL FOR FUEL CAP. CAP, COUPL
- [SDR CALA2024041601111](https://openairdocs.org/sdr/CALA2024041601111.md): Power Supply · inoperative · Apr 13, 2024 · N844UA · Airbus A319131 · Emergency Lighting
  > AT THE END OF THE EMERGENCY SYSTEM LIGHT TEST THE SYSTEM READ EPSU INT LOAD EMER L ATA 33-51-38 OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - FOLLOWED A319 TSM 33-51-00-810-807-A PERFORMED A VISUAL CHECK OF THE CABIN EMERGENCY LIGHTING IN REFE
- [SDR CALA2024032100806](https://openairdocs.org/sdr/CALA2024032100806.md): Fitting · cracked · Mar 20, 2024 · N844UA · Airbus A319131 · Fuselage Main, Structure
  > WINDSHIELD CONTINUITY FITTING HAS CRACK INDICATION ON LEFT AND RIGHT SIDE. PER HAECO LCQ NR 9290207 / 40207 REMOVED AND REPLACED WINDSHIELD CONTINUITY FITTINGS LEFT AND RIGHT HAND AT FR4 IAW UAL ECRA# 5310-08284. GENERATED & RECEIVED FI NAL RFTS #1 OPS GOOD
- [SDR CALA2024032100805](https://openairdocs.org/sdr/CALA2024032100805.md): Door · cracked · Mar 20, 2024 · N844UA · Airbus A319131 · Passenger/Crew Doors
  > LH AFT CREW DOOR UPPER AFT CORNER HAS CRACK INDICATION IN RADIUS AT FR 68 STR 8 PER HAECO LCQ NR 9290260/40260
- [SDR CALA2024032700884](https://openairdocs.org/sdr/CALA2024032700884.md): Skin · dented · Mar 13, 2024 · N844UA · Airbus A319131 · Wing, Plate/Skin
  > BIRD STRIKE DAMAGE AT L/H WING, LEADING EDGE #2.
- [SDR CALA2024031100680](https://openairdocs.org/sdr/CALA2024031100680.md): Skin · contaminated · Mar 9, 2024 · N844UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 92 IN FROM IB EDGE 8 IN FROM T RAILING EDGE AND 2 1/2 IN DIAMETER PER HAECO LCQ NR 9290326/4032 6. REPAIRED LH ELEVATOR UPPER SKIN 92 IN FROM IB 8 IN FROM TE 2.5 I N DIA ZONE A IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAIR
- [SDR CALA2024031100679](https://openairdocs.org/sdr/CALA2024031100679.md): Skin · contaminated · Mar 9, 2024 · N844UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 75 IN FROM IB EDGE 14 1/2 IN F ROM TRAILING EDGE AND 2 IN DIAMETER PER HAECO LCQ NR 9290324/403 24. REPAIRED LH ELEVATOR UPPER SKIN 75 IN FROM IB 14.5 IN FROM TE 2 IN DIA ZONE A IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAIR
- [SDR CALA2024031100678](https://openairdocs.org/sdr/CALA2024031100678.md): Skin · contaminated · Mar 9, 2024 · N844UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 79 1/2 IN FROM I/B EDGE 15 IN FROM TRAILING EDGE AND 1 IN DIAMETER PER HAECO LCQ NR 9290325/40 325. DRILLED WITNES HOLES IN LH ELEVATOR 79.5 IN FROM IB 15 IN FROM T E ZONE A 1.5 IN DIA IAW A319 AMM 55-20-00-200-006 PAR 4 A (
- [SDR CALA2024031100677](https://openairdocs.org/sdr/CALA2024031100677.md): Skin · contaminated · Mar 9, 2024 · N844UA · Airbus A319131 · Elevator, Plate/Skin
  > RH ELEVATOR HAS LIQUID INGRESS FROM IB 54 1/2 IN FROM TRAILING EDGE 8 IN AND 2 INCHES IN DIAMETER PER HAECO LCQ NR 9290319/40319. DRILLED WITNES HOLES ON RH ELEVATOR UPPER SKIN 54.5 IN FROM IB 8 IN FROM TE ZONE A 1.5 IN DIA FOUND NO LIQUID REPAIRED HOLES IA
- [SDR CALA2024031100676](https://openairdocs.org/sdr/CALA2024031100676.md): Skin · contaminated · Mar 9, 2024 · N844UA · Airbus A319131 · Elevator, Plate/Skin
  > RH ELEVATOR HAS LIQUID INGRESS FROM IB 28 IN FROM TRAILING EDGE 23 IN AND 2 1/2 INCHES IN DIAMETER PER HAECO LCQ NR 9290320/4032 0. REPAIRED RH ELEVATOR 28 IN FROM IB 23 IN FROM TE 2.5 IN DIA ZONE A IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAIR.
- [SDR CALA2024031100675](https://openairdocs.org/sdr/CALA2024031100675.md): Skin · contaminated · Mar 9, 2024 · N844UA · Airbus A319131 · Elevator, Plate/Skin
  > RH ELEVATOR HAS LIQUID INGRESS FROM I/B 123 1/2 IN FROM TRAILING EDGE 18 1/2 IN AND 2 INCHES IN DIAMETER PER HAECO LCQ NR 929031 8/40318. REPAIRED RH ELEVATOR 123.5 IN FROM I/B 18.5 IN FROM T/E 2 IN DIA ZONE A IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAIR.
- [SDR CALA2024031100674](https://openairdocs.org/sdr/CALA2024031100674.md): Skin · contaminated · Mar 9, 2024 · N844UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 21 1/2 IN FROM IB EDGE 22 1/2 IN FROM TRAILING EDGE AND 2 IN DIAMETER PER HAECO LCQ NR 9290327 /40327. REPAIRED LH ELEVATOR 21.5 IN FROM IB 22.5 IN FROM TE 2 IN DIA ZO NE A IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAIR.
- [SDR CALA2024030500635](https://openairdocs.org/sdr/CALA2024030500635.md): Skin · cracked · Feb 29, 2024 · N844UA · Airbus A319131 · Emergency Exits
  > LEFT OVERWING HATCH INTERNAL SKIN CRACKED. REMOVED AND REPLACED LT O/W HATCH AFT VERTICAL SEGMENT IAW A319 SRM 51-42-11/001.
- [SDR CALA2023030900666](https://openairdocs.org/sdr/CALA2023030900666.md): Shock Absorber · none · Mar 9, 2023 · N844UA · Airbus A319131 · Landing Gear System
  > L/G SHOCK ABSORBER FAULT ECAM MESSAGE CAME ON IN CRZ AT FL370. NO ABNORMAL L/G INDICATIONS POST FILGHT REPORT INDICATES FAULT AT (24GA), JACKED NOSE OF REMOVED 24GA PROX SENSOR. REMOVED NOSE GEAR TARGET LEVER PN D67880 FOUND BUSHINGS WORN OUT AIRCRAFT, FOUND Z
- [SDR CALA2023021400436](https://openairdocs.org/sdr/CALA2023021400436.md): Skin · dented · Feb 14, 2023 · N844UA · Airbus A319131 · Fuselage Floor Panel
  > FUSELAGE OUTWARD DENT BETWEEN FR26&27 AND STR37L&38L. CURRENT AIRCRAFT TIME 29120FC/66097FH. INITIATE DIP FOR INSP THRESHOLD FROM TIME OF EMBODIMENT 60000FC/ 120000FH WHICHEVER COMES FIRST. INSP INTERVALS N/A & METHOD N/A. DENT IS OUT OF LIMITS REF SRM 53-00-1
- [SDR CALA2022123003526](https://openairdocs.org/sdr/CALA2022123003526.md): Door · missing · Dec 29, 2022 · N844UA · Airbus A319131 · Fluid Service Doors
  > PDA 1 POTABLE WATER SERVICE DOOR FOUND MISSING FROM ACFT UPON ARRIVAL IN DFW POTABLE WATER SERVICE DOOR WAS PREVIOUSLY ON PLACARD (CDL 52C) FOR A BROKEN HINGE. REFERENCE LOGPAGE 3406076. REFER TO LOGPAGE 3406076 FOR UPDATES AND MAINTENANCE ACTION(S). THIS LOGP
- [SDR CALA2021061500882](https://openairdocs.org/sdr/CALA2021061500882.md): Packing · leaking · Jun 15, 2021 · N844UA · Airbus A319131 · Hydraulic System, Main
  > HYD Y ENG2 RSVR LOW LVL FOUND PTU MANIFOLD LEAKING AT QUICK DISCONNECT FITTING 3701 GM, UPON REMOVAL FOUND FAILED PACKING REMOVED AND REPLACED PACKING REF AMM 29-13-15-400-001-A OPS CHECK NORMAL IAW AMM 29-23-00-710-002-A.
- [SDR CALA2019110301894](https://openairdocs.org/sdr/CALA2019110301894.md): Skin · damaged · Oct 31, 2019 · N844UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > EXISTING FASTENER HOLES AT FR20-21 S41R-42R ARE VISUALLY OUT OF ROUND. REF HAECO NR 9292317. DTA REQUIRED. INTERIM REPAIR ACP PER ECRA 5331-02494 PART 1 STEP 1 INTERIM REPAIR INSTRUCTIONS. REF PART 1 STEP 2, ACCOMPLISH A PERMANENT REPAIR AT THE CENTER FUSELAGE
- [SDR CALA2019110101880](https://openairdocs.org/sdr/CALA2019110101880.md): Fitting · worn · Oct 30, 2019 · N844UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > LH MLG DOOR AFT ACTUATOR FITTING TO KEEL BEAM. LUG AFT FACE AROU ND BUSHING HOLE HAS SCORING AND WEAR SUPPORT TASK AD 2015-02-14 PER HAECO LCQ NR 9292308 REMOVED AND REPLACED L/H MLG DOOR ACTUATOR FITTING IAW A320 SRM 51-72-11, 51-42-11 AND REO L22380 AND 53-3
- [SDR CALA2019102901854](https://openairdocs.org/sdr/CALA2019102901854.md): Skin · dented · Oct 28, 2019 · N844UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DENT AT BOTTOM OF FUSELAGE JUST AFT BEHIND NLG - LP 3133264 NEED S RE-EVALUATION SUPPORT TASK PER HAECO LCQ NR 9292021 GENERATED BY V061588 DENT LOCATED BOTTOM OF FUSELAGE JUST AFT BEHIND NLG AT FR20-21, STR 41R-42R. DENT FOUND TO BE OUT OF LIMITS PER SRM 53-1
- [SDR CALA2019091301531](https://openairdocs.org/sdr/CALA2019091301531.md): Fitting · worn · Sep 10, 2019 · N844UA · Airbus A319131 · Landing Gear Position and Warning
  > LANDING GEAR WOULD NOT RETRACT PFR SHOWS "WARNING L/G SHOCK ABSORBER FAULT" WITH FAILURE MESSAGE "32-21-13 NLG SHOCK ABSORBER (2526GM). SOURCE LCCIU 1&2. TSM 32-31-00-710-003-A INDICATES AIRCRAFT LIFTING REQUIRED CORRECTION TSM 32-31-00-720-003-A FOUND FLT GR
- [SDR CALA2018121402565](https://openairdocs.org/sdr/CALA2018121402565.md): Wire · broken · Dec 11, 2018 · N844UA · Airbus A319131 · Landing Gear System Wiring
  > L/G/SYS/DISAGREE ECAM T/S AND FOUND 21GA AT FAULT. PROBLEMS WITH BACKSIDE CORROSION AN D SOCKET A WIRE BROKEN. REPLACED CONNECTOR AND WIRE IAW AWM 32-1 1-01 PG 4 LEFT LEG. TEST NORMAL AT THIS TIME. REF LP-8442477
- [SDR CALA2018121102554](https://openairdocs.org/sdr/CALA2018121102554.md): Sensor · faulted · Dec 10, 2018 · N844UA · Airbus A319131 · Landing Gear Position and Warning
  > L/G LGCIU 1 FAULT ECAMWHEN GEAR SELECTED DOWN REF L/P 8442364 -BROKEN WIRE REPAIRED AND 21GA SENSOR REPL''D. PERFORMED L/G BITE PER M/M 32-69-00-740-001-A WITH NO FAULTS ON EITHER LGCIU. ACFT OK FOR SERVICE. T/S AND FOUND 21GA SENSOR AT FAULT. PROBLEMS WITH BA
- [SDR CALA2017120804364](https://openairdocs.org/sdr/CALA2017120804364.md): Cover · loose · Dec 8, 2017 · N844UA · Airbus A319131 · Escape Slide
  > DOOR L EMER EXIT DISPLAYED ON UPPER ECAM SCREEN L OVRWNG EXIT DO OR INDICATING OPEN ON LWR ECAM FOUND DOOR SLIDE COVER OFF,INSTALLED COVER
- [SDR CALA2017120804365](https://openairdocs.org/sdr/CALA2017120804365.md): Cover · loose · Dec 8, 2017 · N844UA · Airbus A319131 · Emergency Exits
  > LEFT OVER WING EMERG EXIT COVER CAME OFF SHOWED DOOR OPEN ONE ECAM ON LNDG INSTALLED COVER
- [SDR CALA2017120104281](https://openairdocs.org/sdr/CALA2017120104281.md): Cover · loose · Dec 1, 2017 · N844UA · Airbus A319131 · Emergency Exits
  > DOOR L EMER EXIT ECAM ON TOUCHDOWN RESECURED COVER FLAP AS REQUIRED IAW TSM 52-21-00. EXTINGUSHED ECAM MESSAGE.
- [SDR CALA2017110603960](https://openairdocs.org/sdr/CALA2017110603960.md): Power Supply · faulty · Nov 6, 2017 · N844UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTING SYSTEM CHECK, LT OVERWING HATCH EEL EPSU FAILED PUSH TO TEST FUNCTION. REPLACE THE POWER SUPPLY CABIN EMERGENCY LIGHT.
- [SDR CALA2017110603959](https://openairdocs.org/sdr/CALA2017110603959.md): Slide · delaminated · Nov 6, 2017 · N844UA · Airbus A319131 · Escape Slide
  > LT FUSELAGE, OVERWING SLIDE HAS AFT, LOWER SURFACE CORNER, HEAVILY DELAMINATED DAMAGED. REPLACED LT OVERWING SLIDE REF AMM 25-62-42-400-001-A.
- [SDR CALA2017101303615](https://openairdocs.org/sdr/CALA2017101303615.md): Circuit Breaker · malfunctioned · Oct 13, 2017 · N844UA · Airbus A319131 · Emergency Lighting
  > WHEN PERFORMING A EMERGENCY LIGHT TEST, 'EPSU INT LOAD FWD L, AND EPSU BATTERY EMER R FAULTS GENERATED. RESET EMERGENCY LIGHTING TEST CIRCUIT BREAKERS AT 49 AND 121 VU PANEL, OPS TESTED OK.
- [SDR CALA2017060501728](https://openairdocs.org/sdr/CALA2017060501728.md): Battery Pack · no test · Jun 5, 2017 · N844UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED A SYSTEM BITE TEST. RESET FWD LT AND MID LT BATTERIES, SYSTEM TESTED OK, IAW AMM 33-00-00
- [SDR CALA2017042801163](https://openairdocs.org/sdr/CALA2017042801163.md): Battery · not seated · Apr 28, 2017 · N844UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY EMER L CIDS MESSAGE DISPLAYED AFTER TEST ATA 33-51-38. RESET THE EPSU BATTERY, SYSTEM CHECKED OK PER MM 33-51-00.
- [SDR CALA2017030600554](https://openairdocs.org/sdr/CALA2017030600554.md): Connector · loose · Mar 6, 2017 · N844UA · Airbus A319131 · Light System Wiring
  > SEAT ROW 2AB EMERGENCY EXIT PATH LIGHTS FAILS TO ILLUMINATE WHEN TESTED. SECURED CONNECTOR UNDER SEAT,OPS CKD OK
- [SDR CALA2017021700387](https://openairdocs.org/sdr/CALA2017021700387.md): Battery Pack · no test · Feb 17, 2017 · N844UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED AT PTP PANEL. REPLACED BATTERY PACK AT EPSU 13WL. OK FOR SERVICE IAW AMM 33-51-3 8 PB401
- [SDR CALA2016020395070](https://openairdocs.org/sdr/CALA2016020395070.md): Priority Valve · faulty · Jan 31, 2016 · N844UA · Airbus A319131 · Hydraulic System, Main
  > GEAR NOT DOWN LOCKED DISPLAYED ON UPPER ECAM SCREEN. MANUAL EXT GOOD REPLACED PRIORITY VLV OF GREEN HYD SYS IAW AMM 29-11-33-400-001-A. CYCLED GEAR SWING 3 TIMES IAW AMM 32-31-00-720-002A 14 SEC TO CLOSE 18 SEC TO OPEN. OPERATIONS NORMAL.
- [SDR CALA2016020395078](https://openairdocs.org/sdr/CALA2016020395078.md): Unknown · odor · Jan 30, 2016 · N844UA · Airbus A319131 · Air Distribution System
  > SULFUR SMELL, SMOKE ODOR SMELL IN FLIGHT DECK. FOUND LT RECIRC FAN NOT RUNNING. ISOLATED & RE-RAN BOTH PACKS WITH NO ODOR DETECTED. CB`S COLLARED & DEFERRED.
- [SDR CALA2014060991230](https://openairdocs.org/sdr/CALA2014060991230.md): Stringer · corroded · Jun 5, 2014 · N844UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > STRINGER 33R BETWEEN FRAME 59 & 60 HAS LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-73-11. THICKNESS OF THE FLANGE IS 0.063. LOW READING AFTER BLENDING IS 0.037. MAX LOSS ALLOWED IS 0.0315, 0.5 X TC. WITHIN LIMITS IAW SRM 53-00- 13 FIG 202 SH 4 PG 231.

Next page: https://openairdocs.org/aircraft/N844UA/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 = 'N844UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N844UA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.