# Service difficulty reports: N809UA

A list on [N809UA](https://openairdocs.org/aircraft/N809UA.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 · 91 reports

- [SDR CALA2026030214140](https://openairdocs.org/sdr/CALA2026030214140.md): Unknown · odor · Feb 28, 2026 · N809UA · Airbus A319131 · Air Distribution System
  > STRONG SMELL OF DIRTY GYM SOCKS, WET DOG ON APPROACH IN FLIGHT DECK NO ODOR WHEN AIRCRAFT ARRIVED. OPERATED APU AND PACKS FOR 30 MINUTES. NO SMELL NOTED. INSPECTED PACK INTAKES, ENGINE INLETS AND EXHAUST AND DRAINS. NOTHING FOUND, UNABLE TO DUPLICATE. NO ODOR
- [SDR CALA2025041503838](https://openairdocs.org/sdr/CALA2025041503838.md): Slide · no discrepancy · Apr 12, 2025 · N809UA · Airbus A319131 · Escape Slide
  > AFT DOOR ESCAPE SLIDE REMOVE {A3NB-25-3-0021} - INSTALLED SLIDE ARM/DISARM SAFETY PIN IN DOOR L2 EMERGENCY CONTROL HANDLE. REMOVED DOOR L2 SIDE ARM/DISARM SAFETY PIN ON EMERGENCY CONTROL HANDLE REF. J/C 31-2562-1-3804. C/W RII FOR THE REACTIVATION OF THE L2 ES
- [SDR CALA2025041503837](https://openairdocs.org/sdr/CALA2025041503837.md): Slide · no discrepancy · Apr 12, 2025 · N809UA · Airbus A319131 · Escape Slide
  > AFT DOOR ESCAPE SLIDE REMOVE {A3NB-25-3-0021} - INSTALLED PAX DOOR DAMPER SAFETY PIN. DOOR LOCATION L2. REMOVED DOOR L2 DAMPER SAFETY PIN REF. J/C 31-2562-1-3804. C/W RII FOR THE REACTIVATION OF THE L2 ESCAPE SLIDE SYSTEM PER THE GMM
- [SDR CALA2025031102710](https://openairdocs.org/sdr/CALA2025031102710.md): Display · faulted · Mar 9, 2025 · N809UA · Airbus A319131 · Central Display
  > MCDU 2 BLANK SCREEN REQUESTING DEFERRAL. APPROVED. PLACARD #2 MCDU. PARTS BFS IAH. OK TO CONTINUE. REMOVED AND REPLACED RIGHT SIDE MCDU OPS CHECK GOOD REF AMM 22-82-12
- [SDR CALA2025021002254](https://openairdocs.org/sdr/CALA2025021002254.md): Accumulator · faulted · Feb 8, 2025 · N809UA · Airbus A319131 · Hydraulic Power Accumulator, Main
  > HYD G RSVR LO LVL INFLIGHT DEBRIEFED WITH THE PILOTS. THERE WAS A HYD G RSVR LO LVL ECAM MSG. THEY STATED THE RESERVOIR WAS LOW AND THINKING THERE IS A POSSIBLE LEAK ON THE GREEN SYSTEM. THE PILOTS FOLLOWED THEIR PROCEDURES AND HAD THE LANDING GEAR DOORS MANUA
- [SDR CALA2025012802087](https://openairdocs.org/sdr/CALA2025012802087.md): Servo Valve · faulted · Jan 26, 2025 · N809UA · Airbus A319131 · Landing Gear Brake System
  > BRAKES AUTOBRAKE FAULT ECAM MESSAGE WITH CORELATED CFDS MESSAGE BRK NORM SERVOVLV1(15GG)MUST REPLACE NORMAL BRAKE SERVO VALVE 15GG PLEASE FOLLOW TSM 32-42-00-810-805-A UNLOCKING TO FLAG SDR FLAGGING FOR SDR FOUND 15GG CLASS 1 AND FAULT 41 ON T/S DATA FOLLOWING
- [SDR CALA2024112901349](https://openairdocs.org/sdr/CALA2024112901349.md): Smoke Detector · malfunctioned · Nov 28, 2024 · N809UA · Airbus A319131 · Smoke Detection
  > AFT LAV SMOKE DETECTORALARMED W/O SMOKE PRESENT. RESET OK. BOTTL E NOT DISCHARDED CREW REPORTED ALARM WAS SOUNDING FROM LAV F. PERFORM AN OPS TEST OF THE LAV SMOKE DETECTION PER AMM 26-17-00-710-001-A. DE-ENERGIZED &ENERGIZED CIDS. REF AMM 23-73-00. PERFO
- [SDR CALA2024070101931](https://openairdocs.org/sdr/CALA2024070101931.md): Fuel Cap · missing · Jun 26, 2024 · N809UA · Airbus A319131 · Fuel Storage
  > PDA 2 REFERENCE LP 8421939 FOR MISSING FUEL CAP. CONTACTED TOM C NEWMAN REFERENCE LP 8421939.
- [SDR CALA2023121503653](https://openairdocs.org/sdr/CALA2023121503653.md): Sliding Window · overheated · Dec 13, 2023 · N809UA · Airbus A319131 · Flight Compartment Windows
  > FO/SIDE WINDOW LOWERSECTION RIGHT OF SENSORBUBBLING YELLOW COLOR OOZING FLUID. HOT. FLAGGED SDR FOR MTC DIVERSION WITH MELTED PLASTIC SMELL-VAPOR IN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN FLIGHT DECK. NO VISIB
- [SDR CALA2023071202234](https://openairdocs.org/sdr/CALA2023071202234.md): Door · faulted · Jul 9, 2023 · N809UA · Airbus A319131 · Landing Gear Door Actuator
  > L/G DOORS NOT CLOSED ECAM WITH CORRELATED R LG DOOR UPLOCK 2520GM (2522GM) ON LGCIU 1 AND 2. AIRCRAFT TO FERRY TO IAH FOR CONTINUATION OF TSM 32-31-00-810-861-A STEP 4..SUB STEP 6..GEAR SWING. NO PREVIOUS HISTORY IN THE LAST 30 DAYS..WHILE OPERATING RT MLG DO
- [SDR CALA2023070302135](https://openairdocs.org/sdr/CALA2023070302135.md): Battery Pack · no test · Jun 30, 2023 · N809UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (13WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR#5001245027-0010. EPSU BATTERY (13WL) FAILED ON EMERGENCY LIGHTING BATTERY S/N OFF:285851 QTY:1EA P/N ON:AD 3214-31 S/N:274411 QTY:1EA. CAPACITY TEST AND REQUIRE REPLACEMENT. B
- [SDR CALA2023070302134](https://openairdocs.org/sdr/CALA2023070302134.md): Battery · no test · Jun 30, 2023 · N809UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (10WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR#5001244981.0010. EPSU BATTERY (10WL) FAILED ON EMERGENCY LIGHTING BATTERY S/N OFF:285852 QTY: 1EA P/N ON:AD-3214-31 S/N ON: 283297 QTY:1 CAPACITY TEST AND REQUIRE REPLACEMENT.
- [SDR CALA2023070302133](https://openairdocs.org/sdr/CALA2023070302133.md): Battery Pack · no test · Jun 30, 2023 · N809UA · Airbus A319131 · Emergency Lighting
  > EPSU BATERY (11WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR#5001244997-0010. EPSU BATTERY (11WL) FAILED ON EMERGENCY LIGHTING BATTERY S/N OFF: 181186 QTY:1EA P/N ON:AD3214-31 S/N ON: 273854 CAPACITY TEST AND REQUIRE REPLACEMENT. BATTERY
- [SDR CALA2023070302132](https://openairdocs.org/sdr/CALA2023070302132.md): Battery Pack · no test · Jun 30, 2023 · N809UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (12WL) TEST FAILED; BATTERY NEEDS TO BE REPLACE. AS NOTED ON LTPR NR# 5001245021-0010. EPSU BATTERY (12WL) FAILED ON EMERGENCY LIGHTING BATTERY S/N OFF: 285853 QTY:1EA P/N ON: AD3214-31 S/N ON: 242320 CAPACITY TEST AND REQUIRE REPLACEMENT. BATT
- [SDR CALA2023063002089](https://openairdocs.org/sdr/CALA2023063002089.md): Skin · gouged · Jun 29, 2023 · N809UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > GOUGE ON FUSELAGE SKIN BTW FR27-28 STGR21-22 L/H. AS NOTED ON LTPR NR #5001243275-0010. ON LH FUSELAGE SKIN BTW FR27-28 STGR 21-22 IS PERMANENT CAT "B" FIED AS MAJOR PER UAL GMM 03-20-20. CUTOUT DEM:X=41MM, Y=28MM. D MBODIMENT 60000FC/120000FH. SUB INSP TBD, M
- [SDR CALA2023013000265](https://openairdocs.org/sdr/CALA2023013000265.md): Fastener · damaged · Jan 29, 2023 · N809UA · Airbus A319131 · Fuselage, Landing Gear Attach Fittings
  > R/H MLG DOOR ACTUATOR FITTING FWD OTBD FASTENER COMMON TO THE LO WER SKIN AND R/H FWD MLG DOOR HINGE FITTING HAS BROKEN AND IS MI SSING IT''S FASTENER HEAD PER HAECO LCQ NON ROUTINE 9296008/28008 GENERATED BY V061690 "AT RH KEEL BEAM MLG DOOR ACTUATOR & HINGE
- [SDR CALA2023013000264](https://openairdocs.org/sdr/CALA2023013000264.md): Fastener · missing · Jan 29, 2023 · N809UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > L/H FWD AND AFT OTBD FASTENERS ATTACHING ACTUATOR FITTING TO HIN GE FITTINGS ARE MISSING THEIR TENSION HEADS. L/H OTBD AFT IS MAR KED DOT LH1 AND L/H OTBD FWD IS MARKED LH2 PER HAECO LCQ NON ROU TINE 9296007/28007 REV IR PART 1, PERFORMED INTERIM REPAIR OF
- [SDR CALA2023011800145](https://openairdocs.org/sdr/CALA2023011800145.md): Electrical Box · missing · Jan 17, 2023 · N809UA · Airbus A319131 · Landing Gear System Wiring
  > PDA 3 NLG TOWING BOX LEVER MISSING BOTH SPRING CLIPS.. SEE PHOTO.. PHOTO ADDED THREADS WORN FOR BOLT -- NEED NEW ELEC BOX PARTS USED: 31-3252-9-9001,QTY:1 REPLACED AND TESTED NLG ELECT BOX REF 32-51-12.
- [SDR CALA2023010900050](https://openairdocs.org/sdr/CALA2023010900050.md): Proximity Sensor · faulted · Jan 7, 2023 · N809UA · Airbus A319131 · Emergency Exits
  > DOOR R EMER EXITECAM DISPLAYED SHORTLEY AFTER TAKE OFF REQUESTING MEL 5270BK. INSPECTED AREA, DOOR CONFIRMED LOCKED, PLACED ON MEL 5270BK SECURED AND FOOR ARMED SUSPECT COVER PLATE MAY NEED ADJUSTMENT. INSPECTED AREA, DOOR CONFIRMED LOCKED. ADJUSTED COVER P
- [SDR CALA2022080801978](https://openairdocs.org/sdr/CALA2022080801978.md): None · none · Aug 5, 2022 · N809UA · Airbus A300* · Engine Pressure Ratio (EPR)
  > CREW WRITE UP,"AT CRUISE THE FO SCREENBLANKED OUT. ENG2 N1DEGRADED MODE. RAN EC AMADIRUS ON BAT." BUS 2 SPLY BREAKER WAS NOTED "OUT" AFTER LANDING INTO DEN.
- [SDR CALA2021120102229](https://openairdocs.org/sdr/CALA2021120102229.md): None · failed · Dec 1, 2021 · N809UA · Airbus A319131 · Air Conditioning System
  > AIR PACK 1+2 FAULT REPORTED BY CREW. LOCKED FOR FIX OK TO UNLOCK TO FOR TECHNICIAN LOG UPDATE...BSS ADDED PFR REPORT TESTED BOTH RAM AIR OUT ACTUATORS, BOTH ARE FAILED. NEW ACTUATORS ON AOG, HARDWARE INSTALLED IN HINGES AND OLD ACTUATORS ON CART NEAR LH. A/
- [SDR CALA2021071601108](https://openairdocs.org/sdr/CALA2021071601108.md): Stiffener · cracked · Jul 15, 2021 · N809UA · Airbus A319131 · Fuselage Structure (General)
  > LH WINDSHIELD FRAME UPPER JUNCTION FASTENER HOLE IS CRACKED IN T HE FRAME LAYER AT 11:00 CONTACT ENGINEERING FOR REPAIR INSTRUCTI ONS PER NR 9290550 / 30550 AD 2020-19-03 GEN BY V061633 ACP REPAIR AT LH LATERAL WINDSHIELD FR4 UPPER STIFFENER FASTENER HOLE PER
- [SDR CALA2021070101015](https://openairdocs.org/sdr/CALA2021070101015.md): Door Sill · corroded · Jul 1, 2021 · N809UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD WET AREA RH SIDE R-1 DOOR SILL HAS CORROSION AT FR20 GIRT BA R FITTING FASTENER HOLES A3NB-3-6298 PER NR 9290559 / 30559 GEN BY V077960 REMOVED AND REPLACED FWD WET AREA RH SIDE R1 DOOR SILL FROM FR16 TO FR20 STR 23RH IAW DWG B2D53110334 AND A319 SRM 51-42
- [SDR CALA2021062300925](https://openairdocs.org/sdr/CALA2021062300925.md): Shear Web · cracked · Jun 21, 2021 · N809UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > PER NR 9290486/30486 AFT WET AREA RH SIDE SHEAR WEB JUST AFT OF FR68 CRACKED. AFT WET AREA RH SIDE SHEAR WEB JUST AFT FR68 REMOVED AND REPLACE D IAW UAL A319 SRM 51-42-11-001.
- [SDR CALA2021062000912](https://openairdocs.org/sdr/CALA2021062000912.md): Door Sill · corroded · Jun 20, 2021 · N809UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT WET AREA R/H SIDE DOOR SILL HAS CORROSION AT FR66 AROUND FAT ENER HOLE MOVING UNDER FWD GIRT BAR FITTING PER HAECO LCQ NR 929 0488/30488 GENERATED BY V077960
- [SDR CALA2021061800889](https://openairdocs.org/sdr/CALA2021061800889.md): Door Sill · corroded · Jun 17, 2021 · N809UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT WET AREA L/H SIDE L-2 DOOR SILL HAS CORROSION AT FR68 AROUND FASTENER HOLE JUST AFT GIRT BAR FITTING. PER HAECO LCQ NR 92904 92/30492. RMVD AND RPLD AFT WET AREA LH SIDE L2 DOOR SILL FROM FR66 TO FR6 8 IAW DWG 53480009002 AND A319-100 SRM 51-42-11/01.
- [SDR CALA2019061000925](https://openairdocs.org/sdr/CALA2019061000925.md): Intercostal · cracked · Jun 10, 2019 · N809UA · Airbus A319131 · Passenger/Crew Doors
  > R-1 DOOR STOP FITTING, FR20, STOP #1 I/B LOWER HOLE HAS A CRACK INDICATION IN INTERCOSTAL. A3NB-53-4-6304, AD RELATED TASK (AD 2 017-2-03) PER HAECO LCQ NR 9294247 GEN BY V061632 REPAIRED RH FR 20 DOOR STOP #1 IAW ECRA 5311-02165, REPLACED INTERCOSTAL. ACCOMPL
- [SDR CALA2019061000916](https://openairdocs.org/sdr/CALA2019061000916.md): Stop Fitting · cracked · Jun 8, 2019 · N809UA · Airbus A319131 · Service Doors
  > AD RELATED TASK (AD-2017-522-03) R-1 DOOR STOP FITTING, FR-16, S TOP #7 I/B UPPER & LOWER HOLES HAVE CRACK INDICATIONS IN INTERCO STAL (A3NB-53-4-6304) GEN BY V061632 PER HAECO LCQ NR 9294241 REPAIRED R1 FR16 DOOR STOP NO.7 IAW REO L22060 AND ECRA 5311-021 65
- [SDR CALA2017091803228](https://openairdocs.org/sdr/CALA2017091803228.md): Unknown · odor · Sep 18, 2017 · N809UA · Airbus A319131 · Air Distribution System
  > F/A REPORTS A FAINT SMOKE ODOR IN AFT AFT LAVATORY. NOT GETTING STRONGER, NO ODOR DETECTED IN AFT LAVATORY ON ARRIVAL. PERFORMED AN OPS TEST OF THE LAVATORY D SMOKE DETECTOR IAW AMM 26-17-00-710-001-A, CHECKED GOOD.
- [SDR CALA2016101795810](https://openairdocs.org/sdr/CALA2016101795810.md): Skin · dented · Oct 14, 2016 · N809UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > SKIN DENT AT FRAME 23 BELOW STR 22L. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-11-11 FIG 210.
- [SDR CALA2015102094605](https://openairdocs.org/sdr/CALA2015102094605.md): Skin · dented · Oct 17, 2015 · N809UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > SKIN DENT AT FRAME 23, BELOW STRINGER 22L, CARRIED FROM 1/16/13. REMOVED DAMAGE & INSTALLED DOUBLER REPAIR IAW SRM 53- 11-11 FIG 210.
- [SDR CALA2014121692830](https://openairdocs.org/sdr/CALA2014121692830.md): Oxygen Bottle · unserviceable · Oct 12, 2014 · N809UA · Airbus A319131 · Portable Oxygen System
  > AFT CABIN LT SIDE BEHIND LAST ROW OF SEATS HAVE BOTH PORTABLE O2 BOTTLE CANNULA TIGHTLY TIE WRAPPED TO BOTTLES RENDERING BOTTLES USELESS. REMOVED TIE WRAPS FROM BOTH BOTTLES & REPLACED UPPER BOTTLE.
- [SDR CALA2014022790490](https://openairdocs.org/sdr/CALA2014022790490.md): Flap · malfunctioned · Feb 25, 2014 · N809UA · Airbus A319131 · Trailing Edge Flap Control System
  > AIR RETURN DUE TO FLAP SYS FAULT MESSAGE ON ECAM. FLAPS STUCK IN POSITION NR 2.
- [SDR CALA2014011590162](https://openairdocs.org/sdr/CALA2014011590162.md): Computer · inoperative · Jan 14, 2014 · N809UA · Airbus A319131 · Autopilot Computer
  > FMGC NR 2 INOPERATIVE, FAILED IN FLIGHT.
- [SDR CALA2013122693942](https://openairdocs.org/sdr/CALA2013122693942.md): Acoustic Liner · damaged · Dec 25, 2013 · N809UA · Airbus A319131 · Turbine Engine Air Inlet Section
  > ACOUSTIC LINER ON ENG 1 AT 8 O'CLOCK REPAIR CAME UNDONE LEAVING HOLE IN LINER. GRAPHITE MATERIAL MISSING & HONEYCOMB EXPOSED APPROXIMATELY 1.250 X.500 JUST AFT OF PREVIOUS REPAIR AT 8 O'CLOCK POSITION. MUST FIX IAW MT 71-006 ITEM 8. REPAIRED NR 1 ENG INLET
- [SDR CALA2013121393687](https://openairdocs.org/sdr/CALA2013121393687.md): Shoulder Belt · frayed · Dec 13, 2013 · N809UA · Airbus A319131 · Flight Compartment Equipment
  > FLIGHT ATTENDANT`S SHOULDER STRAP AT FWD JUMP SEAT IS FRAYED. REMOVED & INSTALLED FLIGHT ATTENDANT`S SHOULDER STRAP FWD INBD JUMP SEAT, OPERATIONS NORMAL.
- [SDR CALA2013083090885](https://openairdocs.org/sdr/CALA2013083090885.md): Panel · damaged · Aug 29, 2013 · N809UA · Airbus A319131 · Passenger Compartment Equipment
  > SEAT 10A HAS SHARP METAL PIECE ON FLOOR THAT NEEDS TO BE TAPED OVER. REMOVED SHARP PIECE OF METAL FROM KICK PANEL AT 10A.
- [SDR UALA2013050703213](https://openairdocs.org/sdr/UALA2013050703213.md): Radome · damaged · May 6, 2013 · N809UA · Airbus A319131 · Aerodynamic Fairings
  > DURING BIRD STRIKE INSPECTION FOUND 14 IN DIA. BY 4 IN DEPTH. DENT ON CENTER OF RADOME. REPLACED RADOME IAW AMM 53-15-11-000-001A.
- [SDR UALA2013042502888](https://openairdocs.org/sdr/UALA2013042502888.md): Liner · delaminated · Apr 22, 2013 · N809UA · Airbus A319131 · Engine (Turbine/Turboprop)
  > ATTRITION LINER SEAM HAS 1 BY 1/2 INCH DELAMINATION AT 9 O'CLOCK POSITION. NR 1 ENGINE HAS TRANSITION SEAM REPAIRED IAW MM 71-11-11-300-014-B13.
- [SDR UALA2013040402231](https://openairdocs.org/sdr/UALA2013040402231.md): Light · broken · Apr 1, 2013 · N809UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT PATH BROKEN AT SEAT 10LT. REPLACED EMERGENCY LIGHT PATH AT SEAT 10LT, ALL OK.
- [SDR UALA2013022501117](https://openairdocs.org/sdr/UALA2013022501117.md): Cowling · damaged · Feb 22, 2013 · N809UA · Airbus A319131 · Engine Cowling System
  > CREW REPORT: SCRAPE ON NR 2 ENGINE COWLING DISCOVERED DURING WALK-AROUND.
- [SDR UALA2013013100582](https://openairdocs.org/sdr/UALA2013013100582.md): Hose · missing · Jan 31, 2013 · N809UA · Airbus A319131 · Hydraulic System, Main
  > HYD Y RSVR LO LVL ECAM SHORTLY AFTER POWER ADVANCED FOR TAKEOFF. TAKEOFF REJECTED. REPLACED MISSING HYD SERVICE HOSE. REPLACED FCDC 1 AND TESTED IAW AMM.
- [SDR UALA2013012500475](https://openairdocs.org/sdr/UALA2013012500475.md): Skin · dented · Jan 25, 2013 · N809UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > SKIN DENT AT FRAME 23 BELOW STR 22L. REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53- 11-11 FIG 210.
- [SDR UALA2012102906165](https://openairdocs.org/sdr/UALA2012102906165.md): Pump · vibration · Oct 25, 2012 · N809UA · Airbus A319131 · Hydraulic Pump (Electric/Engine), Main
  > VERY LOUD GRINDING NOISE AND VIBRATION COMING FROM FLOOR NEAR ROW 20. POSSIBLE PUMP MAINT TEXT: RAN HYD PUMPS AND ISOLATED FOUND WITH BLUE OVRD. PUMP ON-SEVERE VIBRATION AND NOISE BY ACCESS PANEL 195BB. (SUSPECT NEEDS BLUE HYD PUMP.) REPLACED BLUE SYSTEM H
- [SDR UALA2012062203375](https://openairdocs.org/sdr/UALA2012062203375.md): Video Monitor · malfunctioned · Jun 21, 2012 · N809UA · Airbus A319131 · Entertainment System
  > SEAT ROW 7A VIDEO MONITOR WILL NOT STOW. CABIN VIDEO MONITOR WILL NOT STOW, MONITOR REPLACED, OPS CHECK OK PER 221651.
- [SDR UALA2012051002680](https://openairdocs.org/sdr/UALA2012051002680.md): Battery Pack · inoperative · May 8, 2012 · N809UA · Airbus A319131 · Emergency Lighting
  > PER 3SVC ACFT FAILS EMERGENCY LIGHT TEST FOR LT EMERGENCY BATTERY AND AFT EMERGENCY BATTERY. REPLACED BOTH BATTERIES PER MM 33-51-38, EMERGENCY LIGHT TEST. OP CHECKED OK.
- [SDR UALA2012050302613](https://openairdocs.org/sdr/UALA2012050302613.md): Fmu · faulted · May 2, 2012 · N809UA · Airbus A319131 · Fuel Control/Turbine Engines
  > NR 1 ENGINE HAD AN OVERSPEED FAULT. MAINTENANCE INTERROGATED CFDS LAST LEG AND LAST LEG ECAM REPORTS SHOW 7 3-22-52, FADEC 1A AND 1B CELLS 07 AND 08 HAVE MULTIPLE HITS OF FAULT CODE, OSFFMU, ALSO ACCOMPLISHED ENG 1 FADEC BOTH CHANNELS GROUND SCAN AND SELF TES
- [SDR UALA2012031401670](https://openairdocs.org/sdr/UALA2012031401670.md): Unknown · malfunctioned · Mar 13, 2012 · N809UA · Airbus A319131 · Compressor Bleed Control
  > NR 1 ENGINE STATOR VANE ECAM. ECAM DIRECTED US TO SHUT DOWN ENGINE. GROUND FAULTS ON FADEC 1A AND 1B. REF TSM 75-30-00 PG 295 (TASK 810-843) AND TSM 75-30-00 PG A224 (TASK 810-845). CFDS SHOWED SVATK & MAINT MSG 75-32-41 CHA & CHB VSV ACT-HC-EEC1. PER TSM
- [SDR UALA2012010300050](https://openairdocs.org/sdr/UALA2012010300050.md): Actuator · faulty · Jan 2, 2012 · N809UA · Airbus A319131 · Rudder Control System
  > F/O RUDDER PEDALS WILL NOT RETRACT. INSTALLED PEDAL POSITION ADJUSTER ASSY, OPS CHECKED GOOD.
- [SDR UALA2011102105688](https://openairdocs.org/sdr/UALA2011102105688.md): Radome · dented · Oct 21, 2011 · N809UA · Airbus A319131 · Aerodynamic Fairings
  > DENT ON RADOME MEASURES APPROX 18 IN W BY 20 IN HIGH WITH SOFT-SPONGY AREAS. BEYOND LIMITS.

Next page: https://openairdocs.org/aircraft/N809UA/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 = 'N809UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N809UA/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.