N851UA

Service difficulty reports · 88

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 = 'N851UA' 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 CALA2026090319226Fan · faultedVENT BLOWER FAULT ECAM ON GROUND. SWITCHING BLOWER TO OVERIDE C AUSES CHEMICAL ODOR REMOVED BLOWER FAN REF AMM 21-26-51-000-001-A. REMOVED BLOWER FAN REF AMM 21-26-51-000-001-A. REMOVED AND REPLACED FAN AVIONICS FAN GROUND COOLING AMM 21-26-51/40.Sep 2, 2026 · N851UA · Airbus A319131 · Air Distribution FanSDR CALA2026090119178Deu · faultedODOR SIMILAR TO PLASTIC, CHEMICAL LEAVING FL300. NEVER STRONG. OVEN WAS OFF. ONLY IN FD SUSPECT DEU A WPB U103160, DEU WARMER THAN ADJACENT DEU M&E 31-2300-3-0029. R & R DEU-A(200RH1) ON 2010VU1, REF AMM 23-73-46-000-001-A/ AMM 23-73-46-400-001-A. PERFORMED Sep 1, 2026 · N851UA · Airbus A319131 · Communications SystemSDR CALA2026051116108Coupling · leakingAFTER NR 1 ENGINE RUN. FOUND WET SPOT UNDER THE FMU. SMELLS LIKE FUEL SUSPECT LEAK FROM ENG 1 HYD SUCTION TUBE QUICK DISCONNECT COUPLING, REPLACED LEAKING HYDRAULIC HALF COUPLER GREEN SUCTION LINE IAW AMM 29-11-39-400-802-A. NEEDS YELLOW HYDRAULICS SERVICED AMay 7, 2026 · N851UA · Airbus A319131 · Hydraulic System, MainSDR CALA2026043015855Switch · faultedEMERGENCY EXIT LIGHTS ILLUMINATED ON GROUND FA REPORTS RESET UN SUCCESSFUL SPOKE WITH FLIGHT CREW. OVERHEAD SWITCH IN FLIGHT DECK WAS IN ON POSITION AND OVERRIDING FLIGHT ATTENDANTS PANEL BUTTON POSITION. VERIFIED NO MESSAGES FOR DISCHAGRED EMERGENCY LIGHT BAApr 29, 2026 · N851UA · Airbus A319131 · Emergency LightingSDR CALA2026042015533Fuel Cap · missingMISSING CAP ON ARRIVAL. THE FUEL CAP MISSING FROM RT WING IAW AMM 28-25-41-010-801-A.Apr 16, 2026 · N851UA · Airbus A319131 · Fuel StorageSDR CALA2026032014714Seal · wornAIR BLEED MSG - DUE TO HISTORY OF AIR BLEED MSG, AVIATAR IS SHOWING L WING LOOP A 36-22-16 DURING CRUISE FLT DO THE FAULT ISOLATION PER TSM 36-22-00-810-825-A TO CHK L-WING LOOP A FOR DISCREPANCIES. VERIFY NO BLEED LEAKS ARE PRESENT. CHK LOOP RESISTANCE AND IMMar 18, 2026 · N851UA · Airbus A319131 · Pneumatic SystemSDR CALA2026031714618Window Frame · crackedFLIGHT DECK, WINDSHIELD CTR POST, LOWER NODE, INBD HOLE BOTH LT & RT SIDE HAS CRACK INDICATION AT LOWER SURFACE. LT SIDE: 40% S.H. 6 OCLOCK POS. AT .050 LONG. RT SIDE: 80% S.H. 6 OCLOCK POS. AT 100 LONG. ACCOMPLISHED INTERIM REPAIR AT LT & RT WINDSHIELD FRAMEMar 8, 2026 · N851UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026030914421Fitting · crackedWINDSHIELD LOWER NODE CONTINUITY FITTING LT & RT, CONTINUITY FITTINGS HAS CRACK INDICATIONS .4 FROM CENTER POST. REMOVED AND REPLACED CONTINUITY FITTING IAW EA5310-07675 REV B OPS 004.Mar 6, 2026 · N851UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026030314222Stringer · corrodedSTRINGER BELOW OUTFLOW VALVE CORRODED AT FR 65. REMOVED AND REPLACED STRINGER 31R, FR 64-67 IAW SRM 51-75-12-911-001.Feb 21, 2026 · N851UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2026021913907Shear Web · damagedSHEAR WEB LOWER FASTENER HOLE HAS A CRACK INDICATION, FRAME 61, S37L. REMOVED, FABRICATED, & INSTALLED THE SHEAR WEB IAW SRM 51-72-11-911-001, CAT A.Feb 17, 2026 · N851UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2025040203452Fuel Cap · missingPDA 2 FUEL CAP MISSING COMPLIED WITH CDL REQUESTING CDL 28A.Mar 29, 2025 · N851UA · Airbus A319131 · Fuel StorageSDR CALA2024012300181Fuel Cap · missingPDA 2 RAMP REPORTS FUEL CAP MISSING RAMP REPORTS AIRCRAFT ARRIVED FUEL CAP MISSING. REQUEST TO PLACE PLACED FUEL CAP ON CDL 28A. FUEL CAP ON CDL 28A. PDA2 CRATED AND SDR COMPLIED WITH. DISPATCH DESK: 03 NAME: JPD DATE: 19-JAN-24- OK TO CDLJan 20, 2024 · N851UA · Airbus A319131 · Fuel StorageSDR CALA2023101303038Brake · overtempREJECTED TAKEOFFHOT BRAKES UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. ACP INSP PER AMM 05-51-16-200-001. PERFORMED INSPECTION REF AMM 05-51-16 TIRES AND BRAKES OK NO DAMAGES NOTED AT THIS TIME. PERFORMED INSPOct 11, 2023 · N851UA · Airbus A319131 · BrakeSDR CALA2022062001545Servo Valve · faultyBRAKES AUTO BRK FAULT, REPORTING BRK NORM SERVOVLV1(15GG) DISPLAYS CODE FAULT CODE 85. TOMC ORDERED 15GG AOG UNLOCKING FOR UPDATE REF TSM 32-42-00-810-805-A, COMPLETED TSM UP TO STEP 4.B. NEED TO ACP RESISTANCE CHECK. CLEANED CONNECTOR ON SERVO VALVE 15GG, RESJun 20, 2022 · N851UA · Airbus A319131 · BrakeSDR CALA2021121402369Rivet · missingPDA 3 #1 ENG AIR INTAKE COWL INNER LIP SKIN HAS ONE RIVET HEAD BROKEN OFF/MISSING AT 6 O-CLOCK POSITION -- SEE PHOTO,S PHOTO,S ADDED REMOVED AND REPLACED REF ECRA7111-01387 NO FURTHER ACTION REQDDec 14, 2021 · N851UA · Airbus A319131 · Engine Cowl FlapsSDR CALA2021072101153Rivet · missingPDA 3 #1 ENG AIR INTAKE COWL INNER LIP SKIN AT 6 O-CLOCK POS HAS ONE RIVET HEAD BROKEN OFF & MISSING -- SEE PHOTO . REMOVED AND REPLACED FASTENER REF SRM 51-42-00 AND 71-11-11-300-015-AJul 20, 2021 · N851UA · Airbus A319131 · Nacelle/Pylon, Main FrameSDR CALA2021060200782Structure · corrodedA3NB-57-3-6007. CORROSION ON CENTER WING BOX, UPPER SKIN UPPER S URFACE BETWEEN FR41-FR42 APPRX Y1550.(UNDER APU FUEL FEEDLINE). RECEIVED FINAL EC/RA #5310-07880 VERIFIED ALL STEPS COMPLIED WIT H AND DEVIATIONS NOTED LP CREATED FOR ACCOMPLISHMENT OF ESFR ENTRYJun 2, 2021 · N851UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021053100762Skin · corrodedA3NB-57-3-6007. CORROSION ON CENTER WING BOX, UPPER SKIN UPPER S URFACE BETWEEN FR41-FR42 APPRX Y1550.(UNDER APU FUEL FEEDLINE). RECEIVED FINAL EC/RA #5310-07880 VERIFIED ALL STEPS COMPLIED WIT H AND DEVIATIONS NOTED LP CREATED FOR ACCOMPLISHMENT OF ESFR ENTRYMay 31, 2021 · N851UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2021053100749Floorbeam · corrodedA3NB-53-3-6222 DOT 42-039 MAIN AFT CABIN FLOOR SUPPORT BEAM HAVE CORROSION Y254 FR66 BLENDED MAIN AFT CABIN FLOOR SUPPORT BEAM Y254 AT FR66 IAW SRM 5 1-74-00 L=2.6" W=1.4" D=0.048" ORIGINAL THICKNESS 0.071", REMAIN ING 0.023" FOUND TO BE OUT OF LIMIT IAW SRM 5May 28, 2021 · N851UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2021052800746Crossbeam · crackedDURING ROTO PROBE OF LH FR16 CROSSBEAM, A CRACK INDICATIN WAS NO TED IN THE 3RD HOLE I/B TOP ROW (H3) AT 12 O''CLOCK, INDICATION I S IN THE FRAME RECIEVED FINAL EA # 319-5310-13-A2591 REV "NEW". VERIFIED ALL WO RK STEPS ACCOMPLISHED PER EA AND NO DEVIATIONS NOMay 27, 2021 · N851UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021052800744Crossbeam · crackedDURING ROTO PROBE OF LH FR16 CROSSBEAM, A CRACK INDICATIN WAS NO TED IN THE 3RD HOLE I/B TOP ROW (H3) AT 12 O''CLOCK, INDICATION I S IN THE FRAME RECIEVED FINAL EA # 319-5310-13-A2591 REV "NEW". VERIFIED ALL WO RK STEPS ACCOMPLISHED PER EA AND NO DEVIATIONS NOMay 26, 2021 · N851UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021051400657Door Frame · corrodedA3NB-53-3-6033: R/H FWD PASSENGER/CREW DOOR LOWER CUTOUT HAS COR ROSION AROUND THE SCUFF PLATE ATTACHING ANGLE FASTENER. NEW FITTING INSTALLED AT RH FWD PASSENGER CREW DOOR LOWER CUTOUT I.A.W SRM 51-72-11-911-001. ORIG. THICKNESS .130" REMOVED .057" MATERIAL RMay 14, 2021 · N851UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021051400650Floor Support · corroded(A3NB-53-3-6187) DOT 42-043 MAIN AFTCABIN R2 DOOR FLOOR STILL HA VE CORROSION BETWEEN FR66 TO FR68 REMOVED AND REPLACED DOOR SILL P/N D5348004320701 IAW SRM 51-42- 11 SFR#: 1025444. MAINTENANCE ACCOMPLISHED BY V933867 AT ST AERO SPACE BFM ON W/C # 6001650335May 12, 2021 · N851UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2021051400649Floor Support · corrodedA3NB-53-3-6222 DOT 42-078 MAIN AFT CABIN FLOOR SUPPORT BEAM Y765 FR66 HAVE CORROSION. REMOVED AND REPLACED FLOOR SUPPORT BEAM Y675 FR-64-66 P/N: D5342 09000200 BATCH #: 0003778331 I.A.W. 51-42-11. MAINTENANCE ACCOMP LISHED BY V934035 AT ST AEROSPACE BFM ON W/CMay 12, 2021 · N851UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2021051400648Floorbeam · corroded(A3NB-53-3-6222) DOT 42-042 MAIN CABIN FLOOR SUPPORT BEAM HAVE C ORROSION Y1292 FR68 REMOVED CORROSION ON FLOOR SEAM Y1292 FR 68 I.A.W SRM 51-74- 0,FOUND OUT OF LIMIT. DEEP=0.050"'' L=2.3"; W=2.0". TR 91552, IAW SRM 53-00-14-283-002, FIG 001, SHEET 01. REMOVEDMay 12, 2021 · N851UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2021051400647Shear Plate · damagedA3NB-53-3-6222 DOT 42-037 MAIN AFT CABIN FLOOR RH LATERAL SHEAR PLATE AT STGR23R BETWEEN FR69 AND FR70. REMOVED AND REPLACED MAIN AFT CABIN FLOOR R/H LATERAL SHEAR PLAT E AT STR 23(R) BETWEEN FR69-FR70 I.A.W SRM 51-44-11. MAINTENANCE ACCOMPLISHED AT ST AEROSPAMay 12, 2021 · N851UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2021051200640Fitting · corrodedA3NB-53-3-6033: R/H FWD PASSENGER/CREW DOOR LOWER CUTOUT HAS CORROSION AROUND THE SCUFF PLATE ATTACHING ANGLE FASTENER. FURTHER DETAILS AWAITEDMay 11, 2021 · N851UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021051200637Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED -Y1292. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11.May 10, 2021 · N851UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2021051200635Floorbeam · corroded(A3NB-53-3-6187) DOT 42-044 MAIN AFT CABIN FLOOR SUPPORT BEAM HA VE CORRISION -Y1292 FR66 REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW SRM 51-42-11. ACCOMP LISHED ON NR 6001650336 EMP# V933866 QCBB138.May 10, 2021 · N851UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2021051000628Floorbeam · not reportedMAIN AFT CABIN FLOOR SUPPORT BEAM AT 10"LT OF Y254 FR70. PER VT BFM NRC 0001407. REMOVED AND REPLACED MAIN AFT CABIN FLOOR SUPPORT BEAM AT 10" LT OF Y254 FR 70 IAW A319 SRM 51-42-11. PER VT BFM NRC 0001407. MA INTENANCE ACCOMPLISHED BY V934090. SFR 1025421May 7, 2021 · N851UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2021051000627Fitting · crackedDURING ROTO-PROBE OF RH FR16 NO 1 DOOR STOP FITTING, A CRACK INDIC ATION WAS NOTED IN THE UPPER I/B HOLE AT 2 O''CLOCK. CRACK INDICA TION IS IN THE INTERCOSTAL. PER VT NRC 0001666. GENERATED BY V93 4208 REMOVED AND REPLACED INTERCOSTAL FITTING P/N D53114236201May 7, 2021 · N851UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2021051000626Floorbeam · corrodedMAIN AFT CABIN FLOOR SUPPORT BEAM HAVE CORROSION Y1292 FR 66. REMOVED CORROSION ON FLOOR BEAM Y1292 FR 66 IAW SRM 51-74-00 FOU ND OUT OF LIMIT; DEEP=0.055" L=2.0"; W=2.5" TR 91552 IAW SRM 53- 00-44-203-002FIG 001 SHEET 01. REMOVED AND REPLACED FLOOR BEAM Y 12May 7, 2021 · N851UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2021050600614Floorbeam · corrodedMAIN FWD CABIN FLOOR SUPPORT BEAM 10" RT OF Y765 FR 16 CORRODED REMOVED AND REPLACED MAIN CABIN SUPPORT BEAM AT +Y503 FR 12 TO F R 16 I.A.W. SRM 51-42-11 INSPECTION NOT NEEDED. LP GENERATED FOR SDR TRACKING ONLY.May 5, 2021 · N851UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2021050600613Floor Support · corrodedMAIN AFT ACBIN FLOOR SUPPORT BEAM HAVE CORROSION Y765 FR 68 TO F R70 REMOVED AND REPLACED FLOOR SUPPORT BEAM Y765 FR 68-70 P/N: D5347 209200000 BATCH #: 0002717736 I.A.W. 51-42-11, REMOVED AND REPLA CED NEW COUPLING ANGLE P/N: D5347210420000 BATCH #: 000171888May 5, 2021 · N851UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2021050600612Seat Track · corrodedCORROSION ON FWD END OF OUTBD SEAT TRACK BETWEEN FR 20-21 REMOVED AND REPLACED SEAT TRACK AT FR12-FR24 R/H IAW A319 SRM 51 -42-11. MAINTENANCE ACCOMPLISHED BY V934090 AT ST AEROSPACE ON W /C 6001650367 INSPECTION NOT REQUIRED. LP GENERATED FOR SDR REPORTING OMay 5, 2021 · N851UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2021050600611Seat Track · corrodedCORROSION ON CABIN FLOOR SUPPORT, LH OUTBD LONGERON FR 18-20 REPAIRED FLOOR SUPPORT IAW SRM 53-21-14-300-002 INSPECTION NOT REQUIRED. LP GENERATED FOR SDR REPORTING ONLY.May 5, 2021 · N851UA · Airbus A319131 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2021050500600Floorbeam · corrodedMAIN AFT CABIN FLOOR SUPPORT BEAM HAVE CORROSION Y254 FR68 REMOVED AND INSTALLED NEW HARDPOINT ON LONGERON Y254 BETWEEN FR6 8 AND FR69 I.A.W. A319 SRM 51-42-11/001, 57-44-11/001, 53-41-14- 19-3 FIG. 023.May 4, 2021 · N851UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2021043000583Floorbeam · corrodedMAIN AFT CABIN FLOOR SUPPORT BEAM HAVE CORROSION Y254 FR68 REMOVED AND INSTALLED NEW HARDPOINT ON LONGERON Y254 BETWEEN FR6 8 AND FR69 I.A.W. A319 SRM 51-42-11/001, 57-44-11/001, 53-41-14- 19-3 FIG. 023. MAINTENANCE PERFORMED BY V934035Apr 30, 2021 · N851UA · Airbus A319131 · Fuselage Main, Floor BeamSDR CALA2021043000571Shear Plate · damagedREMOVED AND REPLACED SHEAR PLATE AT FR69-FR70 STR 23 L/H P/N 534 7112420200 IAW SRM 51-42-11Apr 28, 2021 · N851UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2019121902240Fitting · damagedRH MLG DOOR ACTUATOR FITTING REQUIRES REPLACEMENT CURRENT FITTIN G HAS OVERSIZE BUSHING UNREPAIRABLE, SUPPORT TASK, GENERATED BY MECH V061673 REMOVED, REPLACED AND INSTALLED NEW R/H ACT FITTING FOR BEARING SLEEVE WORN OUT IAW A319 SRM 51-42-11-801 PARAGRAPH (FDec 18, 2019 · N851UA · Airbus A319131 · Fuselage, Landing Gear Attach FittingsSDR CALA2019121902239Fitting · wornMLG ACTUATOR L/H & R/H UPPER ATTACH FITTINGS HAVE BEARING SLEEVE WORN REQUIRES MANUFACTURE OF 2EA & REQUIRES CAD PLATING TO BE I NSTALLED R/C EA 5330-04821-001/14221, SUPPORT TASK, RMVD, RPLCD & INSTALLED NEW L/H ACT FITTING FOR BEARING SLEEVE W ORN OUT IAW ADec 18, 2019 · N851UA · Airbus A319131 · Fuselage, Landing Gear Attach FittingsSDR CALA2019121302181Stringer · corrodedCORROSION ON STRINGER 41 RIGHT AFT OF FRAME 63 (A3NB-25-3-6242) PER HAECO LCQ REF. NO. 9292179 GENERATED BY V052030. REMOVED AND REPLACED STR 41R, FR61 TO FR64 IAW A319 SRM 51-72-11 -911-001 STEP 2D(1-5). PERFORMED BY SUPER V052030, MECH V927540, INSP BY V9016Dec 10, 2019 · N851UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2019121302176Stringer Splice · corrodedEVIDENCE OF SURFACE CORROSION IN B ILGE AREA, ON STRINGER 44, AFT OF FR65. REMOVED AND REPLACED SPLICE PLATE REPAIR IAW A319 SRM 51-42-11-8 01 PG 19-20.Dec 9, 2019 · N851UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2019120902165Stringer Splice · corrodedCORROSION ON EXISTING STRINGER SPLICE ON STRINGER 44RT FWD - A3N B-25-3-6242 - GENERATED BY TECH V052030 ON N/R 9292180 AT HAECO LCQ REMOVED AND REPLACED STRINGER SPLICE IAW A319 SRM 53-00-13-300-0 01 P9 FIGURE AT STRINGER 44 RT.Dec 6, 2019 · N851UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2018021000581Unknown · odorPACK ODOR DURING DESCENT BELOW 10000FT. INSPECTED THE APU AREA AND PACK INLETS FOR FLUID LEAKS, NONE FOUND. RAN PACKS, NO ODORS DETECTED. COULD NOT DUPLICATE THE PROBLEM. BOTH PACKS OPERATING NORMALLY. OK TO CONTINUE.Feb 10, 2018 · N851UA · Airbus A319131 · Air Distribution SystemSDR CALA2017063002061Battery · no testCABIN EMERGENCY LIGHT OPS CHECK HAS A MESSAGE FOR EPSU BATTERY. R & R THE EPSU BATTERY L11WL IAW AMM 33-51-38-000-001-A, AND OP CHECKED OK. ACCOMPLISHED IDT INSPECTION AND VERIFIED OPS CHECKED GOOD.Jun 30, 2017 · N851UA · Airbus A319131 · Emergency LightingSDR CALA2017050501256Altimeter · faultySTBY ALTIMETER STICKS AND THEN JUMPS 500-600 FEET DURING DESCENT. INSTALLED ALTIMETER PER AMM 34-21-22.May 5, 2017 · N851UA · Airbus A319131 · Altimeter, Barometric/EncoderSDR CALA2017020300245Fan · faultyTHERE WAS A SLIGHT ELETRICAL OR PAPER BURING ODOR IN CABIN AND COCKP IT. NOTICED FAN AMBER ON REMOVED AND REPLACED LEFT CABIN RECIRCULATION FAN IAW AMM 21-21-51. REPLACED RECIRCULATION FILTER IAW AMM 21-21-41. OPERATIONAL CHECKED GOOD IAW AMM 21-21-00-710-001-Feb 3, 2017 · N851UA · Airbus A319131 · Air Distribution FanSDR CALA2016081595648Battery Pack · no testEMERGENCY EXIT LIGHTS FLICKERING AT ROW 20. FOUND ESPU 10WL AND 12WL BATTERIES FAILING OP CHECK, REPLACED BATTERY PACK IAW MM 33-51-38-401. OPS CHECKED OK.Aug 14, 2016 · N851UA · Airbus A319131 · Emergency LightingSDR CALA2014041490814Fan · seizedCAPTAIN DIVERTED DENVER DUE TO SMOKE IN CABIN. LOUD NOISE & VIBRATION HEARD THEN STOPPED AS THEY WERE DIVERTING TO DENVER. PERFORM AMM TASK 05-51-10-200-801C1 DUE TO REPORT OF SMOKE SMELL. PFR SHOWS VENT EXTRACT FAULT 3 TIMES ON TAXI OUT. EXTRACT VENT FAULApr 13, 2014 · N851UA · Airbus A319131 · Air Distribution Fan
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