# Service difficulty reports: N808UA

A list on [N808UA](https://openairdocs.org/aircraft/N808UA.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 · 78 reports

- [SDR CALA2025102110349](https://openairdocs.org/sdr/CALA2025102110349.md): Light · inoperative · Oct 20, 2025 · N808UA · Airbus A319131 · Emergency Lighting
  > 29C EMERGENCY EXIT PATHLIGHT INOP SEAT EXIT PATH LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY AT SEAT 29C REF CMM 25-26-13. OP CHECK GOOD.
- [SDR CALA2025052304929](https://openairdocs.org/sdr/CALA2025052304929.md): Display · faulty · May 21, 2025 · N808UA · Airbus A319131 · Communications System
  > HEARD PWR TRANSFR SCREENS MOMENTARILY BLACKED OUT LOST RADIOSDEBRIEF FLIGHT CREW: CAPT SAID 10,000 FT HEARD "CLUNK" SUCH AS A POWERTRANSFER, ALL SCREENS WENT BLACK AND CAME BACK, RADIOS WOULD NOT TRANSMIT AT THIS POINT. AFTER ENGINE SHUTDOWN AT THE GATE THEN R
- [SDR CALA2024122303151](https://openairdocs.org/sdr/CALA2024122303151.md): Attach Bracket · gouged · Dec 22, 2024 · N808UA · Airbus A319131 · Wing, Attach Fittings
  > NO.2 FLAP TRACK, FLAP ATTACH BRACKET GOUGED. REFERENCE L/P 3131726 (THIS WAS CLOSED PREMATURELY) ACCOMPLISH INTITIAL AND REPETITIVE INSPECTIONS PER PART 2 ON OR BEFORE 6 MONTHS FROM 22/22/2024. DIP 05-DIP SOURCE DOCUMENT NEEDS TO BE INCLUDED IN LOG. THIS L/P A
- [SDR CALA2024043001265](https://openairdocs.org/sdr/CALA2024043001265.md): Battery · faulty · Apr 29, 2024 · N808UA · Airbus A319131 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - SHOWS EPSU BATTERY AFT L UPON CIDS PTP CHECK IAW TSM TASK 33-51-00-810-802-A, ACP OPERATIONAL TEST OF THE 33-51-38-000-002-A AND TASK 33-51-38-400-002-A. EPSU BITE CHECKS EMERGENCY LIGHTS NOT WITH
- [SDR CALA2023091802815](https://openairdocs.org/sdr/CALA2023091802815.md): Servo Control · leaking · Sep 16, 2023 · N808UA · Airbus A319131 · Drag Control System
  > HYDRAULIC FLUID LEAKING FROM LEFT HAND NUMBER THREE FLAP TRACK FARING. OPERATED FLAPS TO FULL DOWN POSITION AND PRESSURIZED GREEN HYDRAULICS AND FOUND LEFT WING SPOILER #1 SERVO CONTROL SPOILER ACTUATOR LEAKING ADDED PICTURES. PERFORMED RII PER GMM 09-25-05.
- [SDR CALA2023082502637](https://openairdocs.org/sdr/CALA2023082502637.md): Check Valve · leaking · Aug 24, 2023 · N808UA · Airbus A319131 · Hydraulic System, Main
  > AT CRUISE LOST GREENSYS HYD...SHOWING 0 PSI RECOMMENDS ENGINE RUN FOR GREEN ENGINE 1 HYDRAULIC PUMP OPS CONFIRMATION. NOTICED HYD FLUID LEAKING FROM #2 ENGINE UPON ARRIVAL TO GATE. CORRECTION. LEAK WAS FROM #1 ENGINE NOT #2. FOUND #1 ENGINE GREEN HYDRAULIC PUM
- [SDR CALA2023070702194](https://openairdocs.org/sdr/CALA2023070702194.md): Sensor · faulty · Jul 5, 2023 · N808UA · Airbus A319131 · Landing Gear Position and Warning
  > AFTER LIFT OFF THE LANDING GEAR LEVER WOULD NOT GO UP FOLLOWED BY THE FOLLOWING ECAM MESSAGES L/G DOORS NOT CLOSED/ L/G GEAR NOT UPLOCKED AND L/G SHOCK ABSORBER FAULT. REPORTED BY CREW TOMC SMITH... INTERROGATED BOTH LGCIUS, FOUND NLG SHOCK ABSORBER (2526GM)
- [SDR CALA2023061601878](https://openairdocs.org/sdr/CALA2023061601878.md): Panel · dented · Jun 15, 2023 · N808UA · Airbus A319131 · Fuselage Main, Structure
  > DENT ON LEFT SIDE FUSELAGE 29 INCH AFT OF FWD BULK HEAD 8 INCH BELOW STATIC AREA.047. MOVING TO DIAGRAM FOR DENT TYPE 1, BACK INTO AIRBUS SRM REQUIREMENTS CAPITAL D IS.100 AND LITTLE D IS 19 INCHES.MOVING WITHIN R4 OR R5 AS THAT SHOWS A 45 DEGREE ANGLE FROM
- [SDR CALA2023033100926](https://openairdocs.org/sdr/CALA2023033100926.md): Pump · inoperative · Mar 30, 2023 · N808UA · Airbus A319131 · Hydraulic Power System
  > HYD G ENG 1 PUMP LO PR. REMOVED AND REPLACED E1 EDP REF AMM 29-11-51 UP TO STEP F OF INSTALL. STILL REQUIRES OPS CHECK AND LEAK CHECK. HEAD PRESSURE OF HYDRAULIC SYSTEM REMOVED. GREEN RESERVIOR STILL REQUIRES / SERVICE. PARTS USED: 31-2914-9-9003,QTY:1 ADD EM
- [SDR CALA2023011100091](https://openairdocs.org/sdr/CALA2023011100091.md): Pressure Switch · reads low · Jan 10, 2023 · N808UA · Airbus A319131 · Hydraulic Pressure Sensor
  > HYD B SYS LO PR REMOVED AND REPLACED THE BLUE SYSTEM PRESSURE SWITCH. PERFORMED OPERATIONAL CHECK AND LEAK CHECK OF BLUE HYD SYSTEM PRESSURE SWITCH.OPS CHECK GOOD.
- [SDR CALA2021092801723](https://openairdocs.org/sdr/CALA2021092801723.md): Lanyard · missing · Sep 28, 2021 · N808UA · Airbus A319131 · Aircraft Fuel System
  > PDA 1 OPS REPORTS FUEL CAP LANYARD IS MISSING MERRIMAN, DAVID (V929618)APPLIED CDL 28A. CAP LANYARD MISSING PER CDL DISPATCH DESK: 08 NAME: AN DATE: 28-SEP-21- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER
- [SDR CALA2021082501434](https://openairdocs.org/sdr/CALA2021082501434.md): Generator · no test · Aug 25, 2021 · N808UA · Airbus A319131 · AC Generator-Alternator
  > EMERGENCY GENERATOR SYSTEM OPS CHECK FAILED TO SHED. EMER GEN AND ESS TR VOLTAGE ANS FREQS DO NOT SHOW. REPLACED RELAY 12XE AND SWITCHING CONTACTOR 3XC NO HELP. AWAITING CONTROL UNIT 1XE FOR FURTHER TROUBLESHOOTING CONFIRMATION.. NO FIX. REPLACED EMERGENCY GE
- [SDR CALA2021080601264](https://openairdocs.org/sdr/CALA2021080601264.md): Frame · cracked · Aug 4, 2021 · N808UA · Airbus A319131 · Fuselage Main, Frame
  > RH FRAME 16 UPPER DOUBLE JOGGLE AREA, HOLE #5 HAS CRACK INDICATI ON IN DOOR FRAME LAYER IN 6 OCLOCK DIRECTION AND HOLE #6 HAS A C RACK INDICATION IN FRAME LAYER IN 9 OCLOCK DIRECTION AS SEEN FRO M IB REPAIR BEFORE FLIGHT PER NR 9292378 / 32378 GEN BY V892444 R
- [SDR CALA2021070501021](https://openairdocs.org/sdr/CALA2021070501021.md): Door Sill · corroded · Jul 3, 2021 · N808UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > CORROSION ON R2 SOOR SILL FWD INBD CORNER. PER HAECO LCQ NR 9292 459/32459 GENERATED BY V892443
- [SDR CALA2019052000801](https://openairdocs.org/sdr/CALA2019052000801.md): Pressure Panel · cracked · May 19, 2019 · N808UA · Airbus A319131 · Fuselage Main, Bulkhead
  > RT SIDE PRESSURE PANEL BETWEEN FR35-36 ADDITIONAL FASTENERS HOLES OUTSIDE THE CUTOUT AREA CRACKED AT HOLES 2,5,14,15,18,20,21,23,24,28 AND 29, CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS AND REPAIR BEFORE NEXT FLIGHT ACCOMPLISHED INTERIM REPAIR ON RT SIDE PRES
- [SDR CALA2019052000800](https://openairdocs.org/sdr/CALA2019052000800.md): Pressure Panel · cracked · May 19, 2019 · N808UA · Airbus A319131 · Fuselage Main, Bulkhead
  > LT SIDE PRESSURE PANEL BETWEEN FRAME 35-36 ADDITIONAL CRACKS FOUND OUTSIDE OF THE CUTOUT AREA AT HOLES 2,3,4,5,17 AND 29, CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS AND REPAIR BEFORE NEXT FLIGHT ACCOMPLISHED INTIREM REPAIR OF LT SIDE PRESSURE PANEL BETWEEN FR
- [SDR CALA2019051700785](https://openairdocs.org/sdr/CALA2019051700785.md): Pressure Panel · cracked · May 17, 2019 · N808UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > AD 2018-06-04 EA 5330-05216 DOT NO.A3- NO DOT RT SIDE PRESSURE PANEL BETWEEN FRAME 35 AND 36 ADDITIONAL FASTENERS OUTSIDE THE CUT OUT AREA CRACKED AT 2,5,15,18,20,21,23,24,28,29. CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS AND REPAIR BEFORE NEXT FLIGHT N/R S/
- [SDR CALA2019050700705](https://openairdocs.org/sdr/CALA2019050700705.md): Window Post · cracked · May 5, 2019 · N808UA · Airbus A319131 · Fuselage Main, Structure
  > CRACK INDICATION ON LT WINDSHIELD AT SIDE POST FR4 REPAIRED LT WINDSHIELD SIDE POST AT FR4 LOWER WEB IAW ECRA 5311-02139 REV A, ACCOMPLISH THE INITIAL INSP REQUIREMENTS AT LT WINDSHIELD SIDE POST PER PART 2 OF ECRA 5311-02139 REVA ON OR BEFORE THE A/C REACHES
- [SDR CALA2019050700695](https://openairdocs.org/sdr/CALA2019050700695.md): Door Frame · cracked · May 4, 2019 · N808UA · Airbus A319131 · Fuselage Main, Structure
  > RT FR68 DOOR STOP FITTING NR 1 BOTTOM FITTING I/B LOWER FASTENER HOLE HAS CRACK INDICATION ACCOMPLISHED REPAIR OF CRACKED LOWER I/B HOLE AT LOWEREST STOP FITTING ON FR68 RT IAW SRM 53-41-12 -300-010, INSP THRESHOLDS FROM TIME OF REPAIR EMBODIMENT FC41900/FH NO
- [SDR CALA2017051901484](https://openairdocs.org/sdr/CALA2017051901484.md): Slide · failed · May 19, 2017 · N808UA · Airbus A319131 · Escape Slide
  > CABIN EMERGENCY LIGHTS FAIL TEST PER 2 SVC. FAILURE MSG IS, EPSU EXT LOAD AFT L. REPLACED EMERGENCY SLIDE AT DOOR 2L REF AMM 25-62-44. ALL TESTS PASS
- [SDR CALA2017031700644](https://openairdocs.org/sdr/CALA2017031700644.md): Battery Pack · inoperative · Mar 17, 2017 · N808UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT POWER SUPPLY FOUND INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-5 1-38-000-002A, AND 33-51-38-400-002A, OPS CHECKED GOOD.
- [SDR CALA2014100792367](https://openairdocs.org/sdr/CALA2014100792367.md): Battery · not seated · Oct 2, 2014 · N808UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED ON 2 SVC. RESEATED EPSU BATTERY IN AFT CABIN IAW AMM 33-51-38. EMER LIGHT TEST PASSED.
- [SDR CALA2013121693713](https://openairdocs.org/sdr/CALA2013121693713.md): Computer · faulty · Dec 14, 2013 · N808UA · Airbus A319131 · Elevator Control System
  > ELAC 2 PITCH FAULT DISPLAYED ON ECAM WITH ENGS RUNNING & FLIGHT CONTROLS OPERATED. REPLACED ELAC 2 & COMPLETED ASSOCIATED GND TESTS, INDICATIONS NORMAL. LAND TEST ACCOMPLISHED ON CF324. REPLACED RT YELLOW ELEVATOR SERVO UNIT & RIGGED IAW 27-34-00-82 0-003-B
- [SDR CALA2013121193593](https://openairdocs.org/sdr/CALA2013121193593.md): Wire · broken · Dec 2, 2013 · N808UA · Airbus A319131 · Fire Protection System Wiring
  > NR 1 PYLON FIRE EXTINGUISHER BOTTLES BAY. FWD BOTTLE DISCHARGE CARTRIDGE CONNECTOR WIRING CONDUIT IS BROKEN & WORN AT CLAMP AT RT SIDE AFT OF FWD BOTTLE BELOW HYD TUBE GANG CLAMP ASSEMBLY.
- [SDR CALA2013090691081](https://openairdocs.org/sdr/CALA2013090691081.md): Battery · faulty · Sep 6, 2013 · N808UA · Airbus A319131 · Emergency Lighting
  > FOUND EPSU BATTERY AFT L FAULT. REPLACED BATTERY IAW AMM.
- [SDR CALA2013082090569](https://openairdocs.org/sdr/CALA2013082090569.md): Lamp · inoperative · Aug 17, 2013 · N808UA · Airbus A319131 · Emergency Lighting
  > COCKPIT OPEN LIGHT INOPERATIVE. REPLACED LAMPS.
- [SDR UALA2013062404373](https://openairdocs.org/sdr/UALA2013062404373.md): Floor Panel · delaminated · Jun 21, 2013 · N808UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151VG DELAMINATED ABOUT 36 BY 12 INCHES. REPLACED FLOOR PANEL IAW MM.
- [SDR UALA2013062404372](https://openairdocs.org/sdr/UALA2013062404372.md): Floor Panel · delaminated · Jun 21, 2013 · N808UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO FLOOR PANEL 151ZG DELAMINATED ABOUT 21 BY 27 INCHES. FLOOR PANEL REPLACED IAW MM.
- [SDR UALA2013053003750](https://openairdocs.org/sdr/UALA2013053003750.md): Oxygen Mask · damaged · May 25, 2013 · N808UA · Airbus A319131 · Crew Oxygen System
  > F/O OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). ANCHOR PIN ON HARNESS ON THE TOP LEFT IS SHEARED OFF. REPLACED F/O O2 MASK, OPS CHECKS GOOD NO LEAKS.
- [SDR UALA2013051403354](https://openairdocs.org/sdr/UALA2013051403354.md): Power Supply · faulty · May 10, 2013 · N808UA · Airbus A319131 · Emergency Lighting
  > EPSU EMERGENCY LIGHT FAULT DISPLAYED. REPLACED EPSU 11-WL PER AMM 33-51-28-000-001-A.
- [SDR UALA2013051003268](https://openairdocs.org/sdr/UALA2013051003268.md): Epsu · faulty · May 10, 2013 · N808UA · Airbus A319131 · Emergency Lighting
  > EPSU EMERGENCY LIGHT FAULT DISPLAYED. REPLACED EPSU #11-WL PER AMM.
- [SDR CALA2013082690764](https://openairdocs.org/sdr/CALA2013082690764.md): Power Supply · faulty · May 9, 2013 · N808UA · Airbus A319131 · Emergency Lighting
  > EPSU EMERGENCY LIGHT FAULT DISPLAYED. REPLACED EPSU NR 11-WL IAW AMM 33-51-28-000-001-A.
- [SDR UALA2013040802318](https://openairdocs.org/sdr/UALA2013040802318.md): Pump · faulty · Apr 7, 2013 · N808UA · Airbus A319131 · Engine Fuel Pump
  > REPLACE FUEL PUMP. REPLACED NR 1 ENGINE FUEL PUMP PER AMM, OPS AND LEAK CHECKED OKAY.
- [SDR UALA2013022401079](https://openairdocs.org/sdr/UALA2013022401079.md): Window · delaminated · Feb 23, 2013 · N808UA · Airbus A319131 · Flight Compartment Windows
  > CAPTS AFT SIDE WINDOW DELAMINATING AT TOP. REPLACED CAPTAIN'S AFT SIDE WINDOW, OPS CHECKS NORMAL.
- [SDR UALA2013022401078](https://openairdocs.org/sdr/UALA2013022401078.md): Sliding Window · delaminated · Feb 22, 2013 · N808UA · Airbus A319131 · Flight Compartment Windows
  > CAPTAINS SLIDING WINDOW PANE REMOVED, NEW WINDOW REQUIRES INSTALLATION PER AMM. REPLACED CAPTAIN'S SLIDING WINDOW, CHECKS OKAY.
- [SDR UALA2013022201069](https://openairdocs.org/sdr/UALA2013022201069.md): Windshield · delaminated · Feb 22, 2013 · N808UA · Airbus A319131 · Flight Compartment Windows
  > CAPT'S WINDSHIELD DELAMINATED AT TOP. REPLACED CAPTS WINDSHIELD PER MM.
- [SDR UALA2013011600254](https://openairdocs.org/sdr/UALA2013011600254.md): Wire · severed · Jan 14, 2013 · N808UA · Airbus A319131 · Flight Control System Wiring
  > WIRE REPAIR. WIRE #2795-0165 SEVERED AT 42CE3 RELAY POSITION X1 TO 1846VT POSITION 4 PIN D FROM 187VU TO 184 VU. INSTALLED NEW WIRE 2795- 0165 FROM 42CES POSITION X1 TO 1846VT POSITION 4 PIN D AND TERMINATED IAW ESPM 20-53-21. PERFORMED INTEGRITY TEST OF TH
- [SDR UALA2012091205133](https://openairdocs.org/sdr/UALA2012091205133.md): Unknown · malfunctioned · Sep 12, 2012 · N808UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS FAIL WITH FAULTS, EPSU INT LOAD AFT LEFT, EPSU BATTERY EMERGENCY RIGHT, EMERGENCY LEFT. REF MM, CYCLED EMERGENCY LIGHT SYSTEM, TESTED GOOD.
- [SDR UALA2012090705056](https://openairdocs.org/sdr/UALA2012090705056.md): Starter · sparks · Sep 6, 2012 · N808UA · Airbus A319131 · Engine Starter
  > NR 1 ENGINE NO START AT DEPARTURE TIME, SPARKS COMING OUT ON START UP. REPLACED STARTER ON NR 1 ENGINE. DRY MOTOR RUN AND LEAK CHECK GOOD.
- [SDR UALA2012072303969](https://openairdocs.org/sdr/UALA2012072303969.md): Power Supply · failed · Jul 23, 2012 · N808UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED TEST WITH 'EPSU INT LOAD AFT L'. REPLACED EPSU 13WL, OPS CHECKED OKAY.
- [SDR UALA2012070503588](https://openairdocs.org/sdr/UALA2012070503588.md): Life Vest · missing · Jul 4, 2012 · N808UA · Airbus A319131 · Life Jacket
  > CAPTAIN'S LIFE VEST MISSING. SUPPLEMENTAL DATA UPDATE, REPLACED LIFE VEST.
- [SDR UALA2012032901965](https://openairdocs.org/sdr/UALA2012032901965.md): Line · leaking · Mar 29, 2012 · N808UA · Airbus A319131 · Hydraulic System, Main
  > HYD FLUID LEAKING FROM RT HORIZONTAL STAB ATTACH AREA. HYD LEAK FROM RUDDER AREA. SOURCE OF LEAK IS FLARED LINE.
- [SDR UALA2012030601446](https://openairdocs.org/sdr/UALA2012030601446.md): Display · faulty · Mar 6, 2012 · N808UA · Airbus A319131 · Central Display
  > CREW COMMENTS: DISPLAY UNIT TOO DIM TO CLEARLY READ IN DAYLIGHT. FLIGHT DIVERTED DUE TO EXTENSIVE HOLD. PER TOMC ONLY LOWER CAN BE DEFERRED. RPLC'D LWR ECAM DISPLAY 4WT2 AND SELECTED PROPER SWITCH SETTINGS, CKS OK. (ALSO REPLACED P/N 3907130302 - DASH NUM
- [SDR UALA2011121606905](https://openairdocs.org/sdr/UALA2011121606905.md): Transceiver · malfunctioned · Dec 16, 2011 · N808UA · Airbus A319131 · Communications System
  > RED WR R-T MSG, FLIGHT DIVERTED. PER MEL 3441A. REQUIRES TRANSCEIVER.
- [SDR UALA2011111806329](https://openairdocs.org/sdr/UALA2011111806329.md): Window · delaminated · Nov 18, 2011 · N808UA · Airbus A319131 · Flight Compartment Windows
  > 1ST OFFICER FIXED SIDE WINDOW HAS DELAMINATION INTO AREA "A". \==REF: 56-11-12 P. 608== NOT ACCEPTABLE-FIGURE 605 BY- 7715:RT FIXED WINDOW REMOVED REF AMM 56-11-12, TASK 56-11-12-000-001. FINISHED INSTALLATION OF FIRST OFFICER FIX WINDOW PER AMM.
- [SDR UALA2011110706022](https://openairdocs.org/sdr/UALA2011110706022.md): Wire Harness · unsecure · Nov 6, 2011 · N808UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHT SEAT HARNESS LIGHT IS NOT SECURED AT SEATS 7B&C. NEEDS THE HARNESS FOR SEAT BR9638-65. INPUT INTO AMIS HISTORY. SECURED HARNESS AT SEAT 7B&C AND UPDATED WITH INFO IN DF806.
- [SDR UALA2011110706033](https://openairdocs.org/sdr/UALA2011110706033.md): Wire · broken · Nov 5, 2011 · N808UA · Airbus A319131 · Light System Wiring
  > EMERGENCY LIGHT AT SEAT 7C INOP. THERE IS A BROKEN WIRE AT THE CONNECTOR UNDER SEAT 7C. BY- 177127:BROKEN WIRE IS NOT BARE OR EXPOSED TO PAX UNDERNEATH SEAT. SECURED WIRE.^06NOV ORD INF-:PCN 565-2457 IS INCORRECT. PART # BR9638-65 IS ON AC.^06NOV SFO INF
- [SDR UALA2011060202684](https://openairdocs.org/sdr/UALA2011060202684.md): Battery · failed · May 31, 2011 · N808UA · Airbus A319131 · Emergency Lighting
  > DURING 3 SERVICE EMERGENCY EXIT LIGHT TEST, EPSU BATTERY FWD LEFT AND EPSU BATTERY AFT LEFT FAILED. REPLACED EPSU BATTERY AFT LEFT. PASSES BITE TEST ON EPSU. REPLACED EPSU BATTERY OVER DOOR 1L AS PER MM AND ACCOMPLISHED SYSTEM TEST PER MM. SYSTEM OPS NORMA
- [SDR UALA2011031601269](https://openairdocs.org/sdr/UALA2011031601269.md): Amu · faulty · Mar 15, 2011 · N808UA · Airbus A319131 · Communications System
  > F/O O2 MASK MIC DOESN'T WORK. REPLACED MASK, NO HELP. REPLACED AMU PER MM. CHECKED GOOD.
- [SDR UALA2010111504228](https://openairdocs.org/sdr/UALA2010111504228.md): Coffeemaker · failed · Nov 15, 2010 · N808UA · Airbus A319131 · Buffet/Galleys
  > C-B M41 POPPED. FLT ATTENDANT REPORTS SMOKE SPARK THEN C-B POP. CREW REPORTED THAT CB SMOKED, SPARKED THEN POPPED-NOT THE COFFEMAKER. PER INBD FLT ATTN THERE WAS A POP WHEN CB M41 TRIPPED. SHE DID NOT SEE SPARK OR ODOR SMOKE. MECH TRIED TO RESET CB M41, GOT P

Next page: https://openairdocs.org/aircraft/N808UA/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 = 'N808UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N808UA/reports

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