N808UA

Service difficulty reports · 78

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2025102110349Light · inoperative29C 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.Oct 20, 2025 · N808UA · Airbus A319131 · Emergency LightingSDR CALA2025052304929Display · faultyHEARD 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 RMay 21, 2025 · N808UA · Airbus A319131 · Communications SystemSDR CALA2024122303151Attach Bracket · gougedNO.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 ADec 22, 2024 · N808UA · Airbus A319131 · Wing, Attach FittingsSDR CALA2024043001265Battery · faultyOPERATIONAL 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 Apr 29, 2024 · N808UA · Airbus A319131 · Emergency LightingSDR CALA2023091802815Servo Control · leakingHYDRAULIC 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.Sep 16, 2023 · N808UA · Airbus A319131 · Drag Control SystemSDR CALA2023082502637Check Valve · leakingAT 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 PUMAug 24, 2023 · N808UA · Airbus A319131 · Hydraulic System, MainSDR CALA2023070702194Sensor · faultyAFTER 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) Jul 5, 2023 · N808UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2023061601878Panel · dentedDENT 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 FROMJun 15, 2023 · N808UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2023033100926Pump · inoperativeHYD 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 EMMar 30, 2023 · N808UA · Airbus A319131 · Hydraulic Power SystemSDR CALA2023011100091Pressure Switch · reads lowHYD 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.Jan 10, 2023 · N808UA · Airbus A319131 · Hydraulic Pressure SensorSDR CALA2021092801723Lanyard · missingPDA 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 METERSep 28, 2021 · N808UA · Airbus A319131 · Aircraft Fuel SystemSDR CALA2021082501434Generator · no testEMERGENCY 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 GEAug 25, 2021 · N808UA · Airbus A319131 · AC Generator-AlternatorSDR CALA2021080601264Frame · crackedRH 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 RAug 4, 2021 · N808UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2021070501021Door Sill · corrodedCORROSION ON R2 SOOR SILL FWD INBD CORNER. PER HAECO LCQ NR 9292 459/32459 GENERATED BY V892443Jul 3, 2021 · N808UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2019052000801Pressure Panel · crackedRT 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 PRESMay 19, 2019 · N808UA · Airbus A319131 · Fuselage Main, BulkheadSDR CALA2019052000800Pressure Panel · crackedLT 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 FRMay 19, 2019 · N808UA · Airbus A319131 · Fuselage Main, BulkheadSDR CALA2019051700785Pressure Panel · crackedAD 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/May 17, 2019 · N808UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2019050700705Window Post · crackedCRACK 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 May 5, 2019 · N808UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2019050700695Door Frame · crackedRT 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 NOMay 4, 2019 · N808UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2017051901484Slide · failedCABIN 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 PASSMay 19, 2017 · N808UA · Airbus A319131 · Escape SlideSDR CALA2017031700644Battery Pack · inoperativeEMERGENCY 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.Mar 17, 2017 · N808UA · Airbus A319131 · Emergency LightingSDR CALA2014100792367Battery · not seatedEMERGENCY LIGHT TEST FAILED ON 2 SVC. RESEATED EPSU BATTERY IN AFT CABIN IAW AMM 33-51-38. EMER LIGHT TEST PASSED.Oct 2, 2014 · N808UA · Airbus A319131 · Emergency LightingSDR CALA2013121693713Computer · faultyELAC 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-BDec 14, 2013 · N808UA · Airbus A319131 · Elevator Control SystemSDR CALA2013121193593Wire · brokenNR 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.Dec 2, 2013 · N808UA · Airbus A319131 · Fire Protection System WiringSDR CALA2013090691081Battery · faultyFOUND EPSU BATTERY AFT L FAULT. REPLACED BATTERY IAW AMM.Sep 6, 2013 · N808UA · Airbus A319131 · Emergency LightingSDR CALA2013082090569Lamp · inoperativeCOCKPIT OPEN LIGHT INOPERATIVE. REPLACED LAMPS.Aug 17, 2013 · N808UA · Airbus A319131 · Emergency LightingSDR UALA2013062404373Floor Panel · delaminatedAFT CARGO FLOOR PANEL 151VG DELAMINATED ABOUT 36 BY 12 INCHES. REPLACED FLOOR PANEL IAW MM.Jun 21, 2013 · N808UA · Airbus A319131 · Fuselage Floor PanelSDR UALA2013062404372Floor Panel · delaminatedAFT CARGO FLOOR PANEL 151ZG DELAMINATED ABOUT 21 BY 27 INCHES. FLOOR PANEL REPLACED IAW MM.Jun 21, 2013 · N808UA · Airbus A319131 · Fuselage Floor PanelSDR UALA2013053003750Oxygen Mask · damagedF/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.May 25, 2013 · N808UA · Airbus A319131 · Crew Oxygen SystemSDR UALA2013051403354Power Supply · faultyEPSU EMERGENCY LIGHT FAULT DISPLAYED. REPLACED EPSU 11-WL PER AMM 33-51-28-000-001-A.May 10, 2013 · N808UA · Airbus A319131 · Emergency LightingSDR UALA2013051003268Epsu · faultyEPSU EMERGENCY LIGHT FAULT DISPLAYED. REPLACED EPSU #11-WL PER AMM.May 10, 2013 · N808UA · Airbus A319131 · Emergency LightingSDR CALA2013082690764Power Supply · faultyEPSU EMERGENCY LIGHT FAULT DISPLAYED. REPLACED EPSU NR 11-WL IAW AMM 33-51-28-000-001-A.May 9, 2013 · N808UA · Airbus A319131 · Emergency LightingSDR UALA2013040802318Pump · faultyREPLACE FUEL PUMP. REPLACED NR 1 ENGINE FUEL PUMP PER AMM, OPS AND LEAK CHECKED OKAY.Apr 7, 2013 · N808UA · Airbus A319131 · Engine Fuel PumpSDR UALA2013022401079Window · delaminatedCAPTS AFT SIDE WINDOW DELAMINATING AT TOP. REPLACED CAPTAIN'S AFT SIDE WINDOW, OPS CHECKS NORMAL.Feb 23, 2013 · N808UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2013022401078Sliding Window · delaminatedCAPTAINS SLIDING WINDOW PANE REMOVED, NEW WINDOW REQUIRES INSTALLATION PER AMM. REPLACED CAPTAIN'S SLIDING WINDOW, CHECKS OKAY.Feb 22, 2013 · N808UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2013022201069Windshield · delaminatedCAPT'S WINDSHIELD DELAMINATED AT TOP. REPLACED CAPTS WINDSHIELD PER MM.Feb 22, 2013 · N808UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2013011600254Wire · severedWIRE 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 THJan 14, 2013 · N808UA · Airbus A319131 · Flight Control System WiringSDR UALA2012091205133Unknown · malfunctionedEMERGENCY LIGHTS FAIL WITH FAULTS, EPSU INT LOAD AFT LEFT, EPSU BATTERY EMERGENCY RIGHT, EMERGENCY LEFT. REF MM, CYCLED EMERGENCY LIGHT SYSTEM, TESTED GOOD.Sep 12, 2012 · N808UA · Airbus A319131 · Emergency LightingSDR UALA2012090705056Starter · sparksNR 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.Sep 6, 2012 · N808UA · Airbus A319131 · Engine StarterSDR UALA2012072303969Power Supply · failedEMERGENCY LIGHT TEST FAILED TEST WITH 'EPSU INT LOAD AFT L'. REPLACED EPSU 13WL, OPS CHECKED OKAY.Jul 23, 2012 · N808UA · Airbus A319131 · Emergency LightingSDR UALA2012070503588Life Vest · missingCAPTAIN'S LIFE VEST MISSING. SUPPLEMENTAL DATA UPDATE, REPLACED LIFE VEST.Jul 4, 2012 · N808UA · Airbus A319131 · Life JacketSDR UALA2012032901965Line · leakingHYD FLUID LEAKING FROM RT HORIZONTAL STAB ATTACH AREA. HYD LEAK FROM RUDDER AREA. SOURCE OF LEAK IS FLARED LINE.Mar 29, 2012 · N808UA · Airbus A319131 · Hydraulic System, MainSDR UALA2012030601446Display · faultyCREW 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 NUMMar 6, 2012 · N808UA · Airbus A319131 · Central DisplaySDR UALA2011121606905Transceiver · malfunctionedRED WR R-T MSG, FLIGHT DIVERTED. PER MEL 3441A. REQUIRES TRANSCEIVER.Dec 16, 2011 · N808UA · Airbus A319131 · Communications SystemSDR UALA2011111806329Window · delaminated1ST 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.Nov 18, 2011 · N808UA · Airbus A319131 · Flight Compartment WindowsSDR UALA2011110706022Wire Harness · unsecureEMERGENCY 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.Nov 6, 2011 · N808UA · Airbus A319131 · Light System WiringSDR UALA2011110706033Wire · brokenEMERGENCY 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 INFNov 5, 2011 · N808UA · Airbus A319131 · Light System WiringSDR UALA2011060202684Battery · failedDURING 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 NORMAMay 31, 2011 · N808UA · Airbus A319131 · Emergency LightingSDR UALA2011031601269Amu · faultyF/O O2 MASK MIC DOESN'T WORK. REPLACED MASK, NO HELP. REPLACED AMU PER MM. CHECKED GOOD.Mar 15, 2011 · N808UA · Airbus A319131 · Communications SystemSDR UALA2010111504228Coffeemaker · failedC-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 PNov 15, 2010 · N808UA · Airbus A319131 · Buffet/Galleys
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