N803UA

Service difficulty reports · 97

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 = 'N803UA' 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 CALA2026072017894Ils System · faultedNAV LS TUNING DISAGREE SYSTEM RESET DIDNT WORK INFLIGHT FAULT WAS NOT PRESENT ON ARRIVAL. VERIFIED FREQUENCIES ON LS WERE TUNED TO SAME FREQ PREFORMED BITE TEST OF MMR 1 & 2 IAW AMM 34-36-00-740-006-A NO FAULTS. PREFORMED AFS TEST & LAND TEST IAW AMM 22-97-00-Jul 17, 2026 · N803UA · Airbus A319131 · Localizer/VOR SystemSDR CALA2026071417751Battery Pack · no testEPSU BATTERY FWD L FAULT ON CIDS EMERGENCY LIGHT TEST. ATA 33-51-38. PERFORMED FAULT ISOLATION IAW TSM 33-51-00-810-802-A. STEP 4. A. (1) REQUIRES BATTERY REPLACEMENT WHEN RED BATTERY FAULT LED IS DISPLAYED ON EPSU BATTERY. PERFORMED SYSTEM RESET, EPSU BATTERJul 12, 2026 · N803UA · Airbus A319131 · Emergency LightingSDR CALA2026041515378Seat · faultedCAPTAIN'S SEAT DOES NOT STOP WHEN MOVING VERTICAL WHEN OPERATING THE ELECTRIC VERTICAL IN UP POSITION IT WILL HOLD IN PLACE MOMENTARILY. THEN SEAT BASE COLUMN WILL SLOWLY DROOP DOWN CAUSING THE WHOLE CAPT SEAT TO FALL OVER. REMOVED EXISTING SEAT PER MM 25-11-Apr 14, 2026 · N803UA · Airbus A319131 · Flight Compartment EquipmentSDR CALA2025111811303Slide · no discrepancyR2 DOOR SLIDE PRESSURE NOT IN GREEN. VERIFIED SLIED PRESSURE AT DOOR 2R. SLIDE PRESSURE INDICATED IN GREEN BAND. IAW AMM 25-62-00.Nov 16, 2025 · N803UA · Airbus A319131 · Escape SlideSDR CALA2025071406511Fuel Cap · missingPDA 2 UPON ARRIVAL TO DENVER, FLIGHT 1925, FUELER REPORTED REFUEL/DEFUEL COUPLING CAP MISSING. SDR AND SFR FLAGGED FOR REFUEL DEFUEL COUPLING CAP MISSING ON ARRIVAL, PART DEPARTING AIRCRAFT. CAP WAS REPLACED.Jul 12, 2025 · N803UA · Airbus A319131 · Fuel StorageSDR CALA2025052604939Unknown · odorELEC SMELL FROM AIRCONDITIONING TROUBLESHOT PER TSM 24-00-00-810-823-A AND ALSO 49-00-00-200-814-A. DURING INSPECTION FOUND NO ODOR IN THE COCKPIT OR CABIN. RAN THE APU AND THE PACKS WITH NO STRANGE ODOR. CHECKED ALL CIRCUIT BREAKERS AND ACCOMPLISHED EXTERNAL May 23, 2025 · N803UA · Airbus A319131 · Air Distribution SystemSDR CALA2025040703565Wire · brokenEMERGENCY EXIT ISLE LIGHT IS INOP AT SEAT 23C UPON INSPECTION FOUND 1 WIRE BROKEN FROM PLUG COMING FROM SEAT HARNESS REQUESTING MEL 3350C FOR ISLE LIGHT AT SEAT 23C SECURED BROKEN WIRE WITH TAPE NO HAZZARD TO PASSENGERS OR FLIGHT CREW APPROVED DEFERRAL FOR 23CMar 31, 2025 · N803UA · Airbus A319131 · Light System WiringSDR CALA2025031802911Switch · faultedAFT CARGO DOOR OPEN /CLOSE SWITCH INOP, ONLY WORKS WHEN FWD CARGO DOOR OPERATED. PLACING AFT CARGO DOOR OPEN/CLOSE SWITCH ON MEL 5230AB. OK TO APPLY MEL 5230AB FOR AFT CARGO DOOR ELECTRICAL CONTROL INOP PLACED AFT CARGO DOOR OPEN/CLOSE SWITCH ON MEL 5230AB. COMar 14, 2025 · N803UA · Airbus A319131 · Cargo/Baggage DoorsSDR CALA2025030702619Battery · no testACP. CABIN EMERGENCY LIGHT CHECK GOT MESSAGE EMER SYSTEM EPSU BATTERY AFT L ATA 33-51-38. R/R EPSU 13WL BATTERY REF AMM 33-51-38, OPS CHECKS OK.Mar 7, 2025 · N803UA · Airbus A319131 · Emergency LightingSDR CALA2025022402418Slide · no testDURING EMERGENCY LIGHT TEST RECEIVED "EPSU EXT LOAD FWD L" MESSAGE. SEE PIC. PERFORMED EPSU BITE TEST ON FWD LEFT REF AMM 33-51-00-710-001. EPSU SHOWS EXTERIOR LIGHTS FAULT. NEEDS TO T/S REF TSM 33-51-00-810-808-A STEP 4.B.(2). REQUEST MEL 3350P FOR ESCAPE SLIFeb 24, 2025 · N803UA · Airbus A319131 · Escape SlideSDR CALA2025020602219Warning Message · false activationL/G SYS DISAGREE AFTERLANDING. GEAR SHOWSDOWN AND LOCKED. LGCIU 1 AND 2 BITE TEST. TEST PASSED , PERFORMED GROUND SCAN, NO FAULTS , CHECKED PROX SENSORS, NO DEFECTS NOTED, FOUND NO HISTORY, REF. AMM 32-69-00Feb 4, 2025 · N803UA · Airbus A319131 · Landing Gear Position and WarningSDR CALA2024112901352Battery · no testCABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - FWD L/H CABIN EMERGENCY LIGHTING CAPACITY BATTERY, FAILED TEST. REPLACED FWD L/H EMERGENCY BATTERY REF. AMM-33-51-38. OPS CHECK GOOD.Nov 28, 2024 · N803UA · Airbus A319131 · Emergency LightingSDR CALA2024072602110Door Frame · crackedL/H O/W EMERGENCY EXIT HAS CRACK IN SUPPORT FRAME. GEN BY ON HAECO LCQ NR 9294305/26305Jul 25, 2024 · N803UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024072602109Door Frame · crackedR/H O/W EMERGENCY EXIT HAS CRACKS IN SUPPORT FRAME. GEN BY ON HAECO LCQ NR 9294304/26304Jul 25, 2024 · N803UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2024061101774Fuel Cap · missingPDA 2 FUEL CAP MISSING ON ARRIVAL YYC AFTER FLT 1760-08 IAH-YYC REF LOGPAGE #8233867 FOR CDL OF FUEL CAP. WILL FOLLOW UP WITH IAH TO DETERMINE IOF FUELER FAILED TO INSTALL OR NOT AND WILL UPDATE THIS LOGPAGEJun 9, 2024 · N803UA · Airbus A319131 · Fuel StorageSDR CALA2024052401576Fuel Cap · missingPDA 2 FUEL CAP MISSING. PLACED ON CDL LOG PAGE 8027174.May 21, 2024 · N803UA · Airbus A319131 · Fuel StorageSDR CALA2024052001516Seal · wornON CLIMBOUT FROMORD FL290 SEVEREAIRFRAME VIBRATION ADDED VIBRATION REPORT CHECK LIST. PERFORMED DECISION TABLE IAW AMM TASK 05-50-00-810-801-A, AS PER INFO PUT INTO DECISION TABLE FROM VIBRATION REPORTING SHEET DONE BY FLIGHT CREW, CORRECTIVE ACTION TYPE 1 ELMay 16, 2024 · N803UA · Airbus A319131 · Landing Gear DoorsSDR CALA2024022900596Fuel Cap · missingPDA 1 AIRCRAFT ARRIVED WITHOUT FUEL CAP, SEE LP 7181851. SDR SELECTED BY TOMC PER PDA PROCEDURES. REQUEST CDL 28A, PLACARD APPLIED CDL APPLIED DISPATCH DESK: 001 NAME: R.R. DATE: 25-FEB-24- CDL APPROVED BY TOMC PER CDL 28A. REPLACED MISSING FUEL CAP AS PER AMMFeb 26, 2024 · N803UA · Airbus A319131 · Fuel StorageSDR CALA2023051001452Probe · failedON INITIAL T/O ATTMPTTHRUST LAGGED ON ENG2. 2ND ATTMPT THRUST NO RM BUT NO FLX/TOGA P2T2 PROBE IS OFF 10 DEGREES ON THE HIGH SIDE AND WITH THIS HI TIME ENGINE VS THE LOW TIME ON THE LEFT, THAT THAT WOULD CAUSE THE ISSUE ON T.O. USING FLEX. P2T2 PROBE HAS BEEN May 10, 2023 · N803UA · Airbus A319131 · Engine Bleed Air SystemSDR CALA2023030600641Actuator · noneENGINE COMPRESSORVALVE FAULT. ENG 1.ON T/O ROLL. REJECTEDT/O TS AND FOUND #1 ENGINE VSV ACTUATOR TO BE BAD. REMOVED #1 ENG VSV ACTUATOR REF MM 75-32-41-000-010-A. INSTALLED VARIABLE STATOR VANE (VSV ) ACTUATOR PER TASK 75-32-41-400-010-A , IDLE LEAK CHECKED NOMar 6, 2023 · N803UA · Airbus A319131 · Compressor Bleed ValveSDR CALA2023021600464Engine · stalledCREW REPORTS #1 ENGINE STALL ECAM FOLLOWED BY EGT IN RED, ENGINE WAS SHUTDOWN. PER CREW ENGINE WINDMILLED APPROX 80 MINUTES AND THEY DID NOT RECALL IF POSITIVE OIL PRESSURE WAS MAINTAINED. LANDING WAS UNDER WEIGHT AND NORMAL. TOMC-MEREDITH ADDED ESN V11464 81Feb 16, 2023 · N803UA · Airbus A319131 · Turbine Engine Compressor SectionSDR CALA2022060101417Fuel Cap · missingTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL REPORT SUBMITTED ON 6/01/22.REFUEL-DEFUEL COUPLING CAP REPORTED MISSING WITH NO FUEL LEAK NOTED.REPLACED FUEL CAP AND LANYARD.May 30, 2022 · N803UA · Airbus A300* · Aircraft Fuel SystemSDR CALA2022010500034Reservoir · inoperativeECAM CAUTION MESSAGE - G RSVR LO LVL MESSAGE INOP - HYD LOST G HYD FLUID 2 HRSINTO FLT AFTER IT HADBEEN SERVIDED BEFOREF LIGHT. REPLACED GREEN PRIORITY VALVE REF AMM 29-11-33-400-001-A. OPS CHKS NORMAL. NO LEAKS NOTED. ADD EMP:060698 ROTABLE PARTS CHANGE WAS IJan 5, 2022 · N803UA · Airbus A300* · Hydraulic System, MainSDR CALA2021123002486Frame · crackedL/H FR35 STR30 HOLE #1 PRODUCED CRACK INDICATIONS AT THE 2:00 PO SITION. HO,LE #3, #4. LH FORWARD PIT AFT OF FRAME 35 HOLES COMMO N TO ANGLE FITTING REMOVAL UPPER ROW 7TH AFT OF FRAME 35 INTERIO R SURFACE IS GOUGED JUST ABOVE THE HOLE AT 12:00. PER HAECO LCQ NDec 30, 2021 · N803UA · Airbus A300* · Fuselage Main, StructureSDR CALA2021123002483Frame · crackedR1 DOOR FRAME 16 DOUBLE JOGGLE HOLE #6 IS CRACKED IN THE FRAME L AYER AR 11:00 POSITION. PER HAECO LCQ NR 9292446/20446 GENERATED BY V061680 CRA 5311-02722 AND HAECO REO-L23506 WITH NO DEVIATIONS. DIP READ GLE AREA PER PART 2 OF THE LATEST REVISION OF ECRA 531Dec 30, 2021 · N803UA · Airbus A300* · Fuselage Main, FrameSDR CALA2021123002482Structure · crackedR/H FR35 STR30 HOLE #1,#4, #3, #2,PRODUCED CRACK INDICATIONS AT THE 6:00 POSITION 2ND LAYER. PER HAECO LCQ NR''S 9292019/20019, 9 292016/20016, 9292017/20017, 9292018/20018. GENERATED BY V061690 PERMANENT REPAIR ON THE FR 35 STR30RH HOLES #1-#4 PER PART 3 OF WDec 29, 2021 · N803UA · Airbus A300* · Fuselage Main, StructureSDR CALA2021122902481Angle · crackedL/H FR35 STR30 HOLE #1 PRODUCED CRACK INDICATIONS AT THE 2:00 PO SITION. HO,LE #3, #4. LH FORWARD PIT AFT OF FRAME 35 HOLES COMMO N TO ANGLE FITTING REMOVAL UPPER ROW 7TH AFT OF FRAME 35 INTERIO R SURFACE IS GOUGED JUST ABOVE THE HOLE AT 12:00. PER HAECO LCQ NDec 29, 2021 · N803UA · Airbus A300* · Fuselage Main, StructureSDR CALA2021122702443Stringer · elongatedSTRINGER 30R BETWEEN FR34 AND F35 HAVE ELONGATED HOLES.PER HAECO LCQ NR 9292881/20881 GENERATED BY V061742 REPAIR AND REQUIRES INSP AT 60,000 FC/120,000 FH FROM AIRCRAFT F ON HAECO NR 9292881. IRST FLIGHT IAW SRI 53-21-13-205-018 TABLE 1. WORK ACCOMPLISHED ACCDec 26, 2021 · N803UA · Airbus A300* · Fuselage Structure (General)SDR CALA2021120602242Joint · corrodedAFT PIT UNDER FLOOR BAY FRAME 64 LOWER STRINGER CLEAT AHS CORR A FT SIDE.A3NB-05-3-6022 GENERATED BY:V061334 AT HAECO LCQ PER NON ROUTINE 9292412. (20412) REMOVED AND REPLACED BOLT STRAP AND SPLICES BRACKETS AND ASSOCIA REPLACED SHEAR USED WITH NEW P/N D534708Dec 2, 2021 · N803UA · Airbus A319131 · Cargo CompartmentsSDR CALA2021120202238Fitting · noneLEFT ELEVATOR NEEDS HINGE FITTING INNER BUSHING 5 EACH REMOVED A ND REPLACED PER NR 9292272/20272 SPEC# A3NB-55-3-0001 GEN BY V06 1070 RMVD AND RPLD 4 EACH ELEVATOR INNER BUSHINGS AT HINGES #2 I/B, # 3 I/B, #5 I/B AND #6 I/B IAW CMM 55-21-15-401-801-A01. RMVD Dec 1, 2021 · N803UA · Airbus A319131 · Flight Control SystemSDR CALA2021112902182Door Sill · corrodedR2 DOOR SILL HAS CORROSION AR FR66. PER HAECO LCQ NR 9292548/205 48 GENERATED BY V061742. REMOVED AND REPLACED R2 DOOR SILL FR 66-68 IAW A319 SRM 51-72-11 -911-001. ACMP BY MECH V061742 INSP BY V077960Nov 28, 2021 · N803UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021112902175Door Sill · corrodedR2 DOOR SILL SHAPE SILL IS CORRODED PER NR 9292359 / 20359 GEN B Y V892442 SPEC # A3NB-53-3-6187 RMVD AND RPLD R2 DOOR SHAPE SILL IAW SRM 51-72-11-911-002 REPAIR ED TOPCOAT IAW SRM 51-85-12-911-002 BY MECH V061742 INSP BY V077 960Nov 26, 2021 · N803UA · Airbus A319131 · Fuselage Structure (General)SDR CALA2021112202148Door Sill · noneL2 DOOR SILL HAS LIGHT SURFACE. PER HAECO LCQ NR 9292357/20357 G ENERATED BY V892442. CUT OUT CORRODED NUT PLATE HOLE AT FR66 DOOR SILL FLANGE, CUT A FILLER FOR REPAIR PRINCIPLE 6 AND ISNTALLED IAW A319 SRM 53-41-1 4-283-002, SRM 53-41-300-001. PERFORMED BY V9Nov 20, 2021 · N803UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021112202146Fitting · corrodedFR 68 RH LOWEST HOLE JUST ABOVE DOOR SILL PLATE IS CORRODED. PER HAECO LCQ NR 9292399/20399 GENERATED BY V892442 -1.1"SHIM AND FILLER INSTALLED. SRI 53-41-12-205-003 TABLE 1 REQ UIRES A DETAILED INSPECTION FROM FIRST FLIGHT 24,000FC (FH NOT R ELEVANT. SUBSEQUENov 20, 2021 · N803UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2019042200639Fastener · missingPDA 3 BELLY FAIRING PANEL 192AB HAS 1 EA MISSING FASTENER.RPL FASTENER. RPL FASTENER SEE LOG PAGE 3043667.Apr 22, 2019 · N803UA · Airbus A319131 · Aerodynamic FairingsSDR CALA2017091103148Battery · dischargedDURING EMERGENCY LIGHT TEST WITH THE PTP, EPSU AFT LEFT 13WL FAILED BATTERY TEST. REMOVED AND REPLACED THE EPSU BATTERY IAW AMM 33-51-38-000-002- A. PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-001-A, NO DEFECTS NOTED.Sep 11, 2017 · N803UA · Airbus A319131 · Emergency LightingSDR CALA2017091103135Battery · dischargedDURING EMERGENCY LIGHT TEST WITH THE PTP, EPSU RIGHT 12 WL FAILED BATTERY. REMOVED AND REPLACED THE BATTERY IAW AMM 33-51-38-000-002- A. PERFORMED OPERATIONAL TEST IAW AMM 33-51-00-710-001-A, NO DEFECTS NOTED.Sep 11, 2017 · N803UA · Airbus A319131 · Emergency LightingSDR CALA2016072595585Line · damagedHYD EDP 1 LO PR WITH HYD G RESERVOIR LOW LEVEL AND LOW PRESSURE ECAM MESSAGES DISPLAYED. CREW REPORT FLUID LEVEL AT ZERO, TURNED ENG 1 HYD PUMP IAW QRH AS SOON AS ECAM DISPLAYED. FOUND THE ENG 1 PRESSURE LINE IN THE PYLON DAMAGED. REMOVED AND REPLACED THEJul 24, 2016 · N803UA · Airbus A319131 · Hydraulic System, MainSDR CALA2015091194288Keelbeam · damagedINSPECTION OF LT & RT MLG DOOR, FWD ATTACH HINGE FITTING, LT & RT DOOR ACTUATOR FITTINGS, LT & RT KEEL BEAM BUTTERFLY DOUBLERS,& HORIZONTAL KEEL BEAM STRAP AT RIB W10 WAS PERFORMED. MULTIPLE HOLES WERE FOUND OUT OF ROUND & BEYOND REF REQUIREMENTS. REPAIR ACCOSep 9, 2015 · N803UA · Airbus A319131 · Fuselage Main, KeelSDR CALA2015050693660Control Lever · faultyON EXTENSION LGCIU 1 & 2 FAILED. GEAR HAD TO BE MANUALLY EXTENDED IAW ECAM. REPLACED LG CONTROL LEVER, OK NO FAULTS.May 4, 2015 · N803UA · Airbus A319131 · Landing Gear SelectorSDR CALA2015032093449Stringer · corrodedAFT CARGO HAS CORROSION ON STRINGER 38R BETWEEN FRAME 59 & 60. R & R STRINGER IAW SRM 51-42-11 PGS 7-10 & 30-31.Mar 19, 2015 · N803UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2015032093443Panel · damagedRIGHT WING FUEL PANEL 640MB LANDING HAS AN ELONGATED SCREW HOLE AFT SIDE 1ST HOLE OTBD OF CTR LINE. REPAIRED SCREW HOLE IAW REO-L18752 REV IR & UAL ECRA 5720 636. THIS REPAIR HAS BEEN APPROVED AS CAT B PERMANENT REPAIR & TO ACP INITIAL INSPECTION IAW PART 2 OMar 18, 2015 · N803UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2015022093149Skin · dentedFUSELAGE DENTED AT FRAME 5 BETWEEN STRINGER 35L & 36L. DENT MEASURES 1.4W X .025D & .5" FROM FRAME. REPAIRED AREA IAW SRM 53-00-41 FIG 232. SRI 53-00-11-2-017-00 REQUIRES FIRST INSP 60000C AFTER REPAIR EMBODIMENT. CURRENT CYCLES 23,653C.Feb 18, 2015 · N803UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2015021293140Skin · corrodedR2 DOOR CUT OUT HAS CORROSION UNDER SCUFF PLATE AT FRAME 67R - 68R ON EXTERNAL SKIN, STRINGER 22 - 23R. BLENDED IAW SRM 51-74-00 PAR 6, MAX THICKNESS .240", MAT LOSS =.013". MATERIAL REMAINS .227" & IS WITHIN LIMITS IAW SRM 53-41-11 FIG 106 SHEET 1. FLAT PEFeb 8, 2015 · N803UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2015021293130Door Sill · corrodedL1 DOOR SILL HAS CORROSION AROUND FWD GIRT BAR FITTING, FWD INBD HOLE & AFT OTBD HOLE. REMOVE CORROSION FROM BOTH HOLES IAW SRM 53-11-14 FIG 108. NDT INSPECTION IAW 51-10-01 & NO CRACKS FOUND. FABRICATED TWO EACH BUSHINGS IAW SRM 53-11-14 FIG 108. INSTALLEFeb 6, 2015 · N803UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015021093073Door Sill · corrodedR2 DOOR SILL AFT CORNER HAS LIGHT SURFACE CORROSION 2 INCHES FWD OF FRAME 68. REPLACED R2 DOOR SILL AFT CORNER & REPAIRED ANGLE IAW SRM 53-41-14 FIG 201 SHEET 3 REPAIR PRINCIPLE 5.Feb 5, 2015 · N803UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2015011392953Pressure Switch · faultyBLUE ELEC PUMP LOW PRESS & BLUE SYS LOW PRESS. NO CB`S TRIPPED. REPLACED PRESS SWITCH & WARNING CONTROL BOARD.Jan 11, 2015 · N803UA · Airbus A319131 · Hydraulic Pressure SensorSDR CALA2014122692867O-Ring · blownSYSTEM Y HYD QTY LOST IN FLIGHT. RESERVOIR QTY DROPPED WITH NO SYS PRESS. DIVERTED & FOUND PTU O RINGS BLOWN OUT. REPLACED CHECK VLV ASSEMBLY & O RINGS FOR PTU. OPERATIONS CHECKED & LEAK GOOD. SERVICED SYS TO NORMAL.Dec 20, 2014 · N803UA · Airbus A319131 · Hydraulic System, MainSDR CALA2014102992624Mount · corrodedRIGHT PYLON ENG MOUNT HAS SURFACE CORROSION. PERFORMED ECRA 5450-02273 NO DEFAULTS FOUND. OK TO CONTINUE.Oct 27, 2014 · N803UA · Airbus A319131 · Engine Mount SectionSDR CALA2014032490672Light · missingEMERGENCY EXIT LIGHTS AT SEATS 1B & 2B MISSING. REPAIRED EMERGENCY LIGHT AT 2B, 1B INOPERATIVE.Mar 24, 2014 · N803UA · Airbus A319131 · Emergency Lighting
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