N836AW

Service difficulty reports · 155

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 = 'N836AW' 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 AALA201707079009Panel · displacedDURING LANDING, EMERGENCY EXIT WARNING CAME ON FOR LEFT OVERWING EXIT. REINSTALLED PANEL AS REQUIRED AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.Jul 6, 2017 · N836AW · Airbus A319132 · Emergency ExitsSDR AALA201705269004Tachometer · failedWITH AUTO BRAKES ARMED FOR LANDING, JUST AFTER TOUCH DOWN AND SPOILERS DEPLOYED, RECEIVED AN AUTO BRAKE FAULT. REPLACED THE NR 1 WHEEL TACHOMETER, OPS CHECKED GOOD IAW MM 32-42-57-400.May 25, 2017 · N836AW · Airbus A319132 · BrakeSDR AALA201611259011Lens · brokenL1 DOOR EMERGENCY LIGHT COVER BROKEN. REPLACED BROKEN L1 DOOR EMERGENCY LIGHT LENS COVER IAW AMM 33-51-13. THE AIRCRAFT WAS NOT GROUNDED.Nov 23, 2016 · N836AW · Airbus A319132 · Emergency LightingSDR AALA201611089003Adiru · faultedAIRCRAFT WAS GROUNDED. LOW SPEED REJECT. ECAM RUDDER TRAVEL LIMITER FAULT. MASTER CAUTION ILLUMINATED. REPLACED ADIRU 3 PER MM 34-12-34.Nov 7, 2016 · N836AW · Airbus A319132 · Inertial Guidance SystemSDR AALA201608059001Lens · brokenEMERGENCY EXIT LIGHT LENS L1 DOOR BROKEN. REPLACED LIGHT LENS AND ACCOMPLISHED A SATISFACTORY OPS CHECK.Aug 4, 2016 · N836AW · Airbus A319132 · Emergency LightingSDR AALA201602229006Apu · leakingAIRCRAFT WAS GNDED. VERY STRONG ODOR DIRTY SOCK SMELL IRRITATES NASAL PASSAGES BADLY. FOUND APU LEAKING OIL FROM TURBINE ACCESS PLATE AFT OF INLET & REPLACED THE APU IAW TASK CARD 26L31049003. A SATISFACTORY OPERATIONAL & LEAK CHECK WAS ACCOMPLISHED & NO ODFeb 21, 2016 · N836AW · Airbus A319132 · APU Core EngineSDR AALA201512269003Cover · missingAIRCRAFT WAS NOT GNDED. EMER SIGN COVER AT DOOR 2L MISSING. INSTALLED NEW EMER SIGN COVER AT DOOR 2L.Dec 25, 2015 · N836AW · Airbus A319132 · Emergency LightingSDR AALA201509099005Battery · dischargedFLIGHT ATTENDANT REPORTS, REAR GALLEY EMER FLASHLIGHT BATTERY LOW. REPLACED AFT LT GALLEY EMER FLASHLIGHT BATTERY.Sep 8, 2015 · N836AW · Airbus A319132 · Emergency EquipmentSDR AALA201507279018Computer · malfunctionedFLIGHT 1947 EN-ROUTE, ELAC 2 FAULTED WITH ELAC 1 ON MEL, FOLLOWED BY BRAKE SYS 1 FAULT. DECLARED AN EMER & THE FLIGHT DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. R & R ELAC 2 IAW AMM 27-93-34-000 400-001-A. REPLACED ELAC 1 TO CLEAR MEL. PERFORMEJul 24, 2015 · N836AW · Airbus A319132 · Elevator Control SystemSDR AALA201506029003Reservoir · low pressureCIDS CAUTION MSG. FOUND LT SLIDE INFLATION RESERVOIR PRESS LOW. SERVICED THE LT SLIDE INFLATION RESERVOIR.Jun 1, 2015 · N836AW · Airbus A319132 · Escape SlideSDR AALA201505269003Fitting · corrodedC11 CHECK, CORROSION ON THE RT MLG RETRACTION JACK FITTING ON THE AFT SPAR UPPER FACE. REPAIRED IAW SRM 57-26-13-PB201 FIGURE 207.May 24, 2015 · N836AW · Airbus A319132 · Wing, Attach FittingsSDR USAA2014123000004Control Unit · inoperativeAUTO BRAKES FAILED ON LANDING, BRAKE NR 1 APPEARED TO NEVER HAVE OPERATED, BRAKE PRESS INDICATOR TRIPLE INDICATOR DID NOT SHOW ANY BRAKE PRESS. ACCOMPLISHED TROUBLESHOOTING IAW TSM 32-42-00-810-823A, TSM 32-42-00-720-003A & TSM 32-42-00-810-817A. REPLACED BRDec 28, 2014 · N836AW · Airbus A319132 · Landing Gear Brake SystemSDR USAA2014110500009Hydraulic Line · leakingGREEN HYD QTY LOSS AFTER TAKEOFF. DECLARED AN EMER & RETURNED TO FIELD. AFTER AN UNEVENTFUL LANDING, THE ACFT WAS TOWED FROM THE RUNWAY TO THE GATE DUE TO LOSS OF NOSE WHEEL STEERING. RT MLG DOOR ACTUATOR FWD FLEX LINE LEAKING, R & R DUE TO DPI'S ACTIVATED.Nov 4, 2014 · N836AW · Airbus A319132 · Hydraulic System, MainSDR USAA2014092500006Windshield · crackedLEFT WINDSHIELD CRACKED. REPLACED LT WINDSHIELD IAW JOB CARD 26L21056001.Sep 24, 2014 · N836AW · Airbus A319132 · Flight Compartment WindowsSDR USAA2014090200003Computer · unserviceableDURING CLIMB OUT CREW REPORTED ECAM DISPLAYED VENT SKIN VLV FAULT. SELECTED BOTH BLOWER & EXTRACT VLV TO OVERRIDE, BUT EXTRACT DOOR REMAINED HALF OPEN THROUGHOUT FLIGHT & LANDING. FLIGHT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. R & R AEVC IAW AMM 21-26-Sep 1, 2014 · N836AW · Airbus A319132 · Air Distribution SystemSDR USAA2014060900007Gust Lock · lack of lubeTHE GUST LOCK AT L1 DOOR DOESN'T RELEASE PROPERLY, GRABS. LUBRICATED L1 GUST LOCK RELEASE. OPERATIONAL CHECK OK.Jun 8, 2014 · N836AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2014011500004Battery · dischargedCREW REPORTED THE EMERGENCY FLASHLIGHT AT DOOR 1L INOPERATIVE. REPLACED THE BATTERY.Jan 14, 2014 · N836AW · Airbus A319132 · Emergency EquipmentSDR USAA2013111100011Bottle · dischargedR2 DOOR SLIDE PRESSURE IS IN THE RED BAND AREA. R & R DOOR ESCAPE SLIDE IAW JC 26L00025010.Nov 9, 2013 · N836AW · Airbus A319132 · Escape SlideSDR USAA2013102800018Unknown · odorINTERMITTENT ODOR IN COCKPIT WITH APU, ENGINES OFF & GROUND AIR CONNECTED. MAINTENANCE TROUBLESHOT CABIN AIR QUALITY, NO FAULTS FOUND, AC RELEASED FOR SERVICE.Oct 27, 2013 · N836AW · Airbus A319132 · Air Distribution SystemSDR USAA2013100700015Fitting · out of adjustCREW REPORTED L1 DOOR WILL NOT CLOSE. MX ADJUSTED L1 DOOR UPPER AND LOWER, FWD AND AFT, DOOR LATCH FITTINGS IAW AMM 52-11-11-400-001-A, FIG SHEET 1. OPS CHECK GOOD.Oct 4, 2013 · N836AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2013092000002Floor Panel · debondedFWD CARGO BAY FLOOR PANEL 131EG DISBONDED. REPLACED FLOOR PANEL IAW SRM 53-22-14-400.Sep 19, 2013 · N836AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2013061700029Cover · missingF/A REPORT EMERGENCY EXIT COVER PLATE ON DOOR 2L MISSING.Jun 15, 2013 · N836AW · Airbus A319132 · Emergency LightingSDR USAA2013061200003Control Panel · faultyAFTER ACTIVATION OF GROUND POWER, A STRONG ELECTRICAL ODOR WAS NOTED. WITH AN OPENED COCKPIT WINDOW TO VENTILATE, THE ODOR PERSISTED. MX COMPLETED T/S JOB CARD 26L00021001 AND FOUND FUSE K ON TRANFORMER 35LP BLOWN AND CAPTAIN'S ACP INOP. REPLACED FUSE IAW SCJun 11, 2013 · N836AW · Airbus A319132 · Audio Integrating SystemSDR USAA2013053100008Track · lack of lubeDOOR L1 HARD TO OPEN AND CLOSE. LUBED L1 DOOR TRACKS.May 30, 2013 · N836AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2013041900008Fan · failedFLIGHT ATTENDANTS REPORTED A DIRTY SOCK SMELL WHEN DESCENDING INTO DSM. WHEN ARRIVING AT GATE, TURNED ON APU BLEED AND GOT ACID SMELL IN THE FLIGHT DECK FOLLOWED BY A DIRTY SOCK SMELL IN ENTIRE CABIN. TURNED OFF APU BLEED AND ODOR SUBSIDED. REPLACED APU COApr 18, 2013 · N836AW · Airbus A319132 · Air Distribution FanSDR USAA2013031200005Pad · obstructedCREW REPORTED DOOR 2L ARMING MECHANISM STIFF. MAINTENANCE REMOVED DEBRIS FROM 2L GIRT BAR PAD. OPS CHECK NORMAL.Mar 11, 2013 · N836AW · Airbus A319132 · Emergency EquipmentSDR USAA2012122400010Lever · lack of lubeCREW REPORTED DOOR 2L IS VERY HARD TO ARM. MAINTENANCE LUBED THE 2L DOOR ARMING LEVER AND GIRT BAR. OPS CHECK GOOD. ARMED EASY WITH LEVER.Dec 22, 2012 · N836AW · Airbus A319132 · Passenger/Crew DoorsSDR USAA2012091000048Power Supply · inoperativeFOUND LEFT AFT ABOVE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) LEFT AFT ABOVE DOOR LIGHT. OPS CHECKED GOOD.Sep 8, 2012 · N836AW · Airbus A319132 · Emergency LightingSDR USAA2012070200015Power Supply · inoperativeEMERGENCY LIGHT TEST FAILED. REMOVED AND REPLACED POWER SUPPLY AND LIGHT ASSEMBLY AT RIGHT OVERWING PER AMM 33-51-38. OPS CHECKED GOOD.Jun 30, 2012 · N836AW · Airbus A319132 · Emergency LightingSDR USAA2012061500018Power Supply · inoperativeOPERATIONAL TEST OF EMERGENCY LIGHT FAULT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT RIGHT AT ROW 9. OPS CHECKED GOOD.Jun 12, 2012 · N836AW · Airbus A319132 · Emergency LightingSDR USAA2012050900009Power Supply · inoperativeFOUND OVER THE WING CABIN EMERGENCY EXIT ROW LIGHTS ON BOTH SIDES INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY PER AMM 33-51-39-401. OPS CHECKED GOOD.May 7, 2012 · N836AW · Airbus A319132 · Emergency LightingSDR USAA2012040600008Fmu · cokedON TAKEOFF, AS THRUST WAS INCREASED, NR 1 ENGINE EPR STAGNATED AT APPROXIMATELY HALFWAY POINT AND THEN ENGINE FAILED ECAM APPEARED. TAKEOFF ABORTED, NR 1 ENGINE WAS SHUTDOWN. ENGINE CONTINUED TO SMOKE. REMOVED AND REPLACED ENGINE 1. VENDOR (IAE) TEARDOWN RApr 1, 2012 · N836AW · Airbus A319132 · Fuel Control/Turbine EnginesSDR USAA2012032600020Lens · broken1S CHECK - BROKEN LENS EMERGENCY EXIT ON DOOR FRAME UPPER (BIG) AND LOWER (SMALL) AT R2 DOOR WAY. REPLACED LENS EMERGENCY EXIT ON DOOR FRAME UPPER (BIG) AND LOWER (SMALL) AT R2 DOOR WAY IAW A319 AMM 33-51-16.Mar 23, 2012 · N836AW · Airbus A319132 · Emergency LightingSDR USAA2012032700015Sill · corroded1S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT FR66, S23L. REPAIRED LOWER SILL AT FR66, S23L IAW A319 SRM 53-41-14 REPAIR PRINCIPLE 6.Mar 14, 2012 · N836AW · Airbus A319132 · Fuselage Miscellaneous StructureSDR USAA2012032700010Hinge Fitting · excess play1S CHECK - RUDDER HINGE POINT NR 5 HAS EXCESSIVE PLAY OF 0.565 INCH AT VERTICAL STABILIZER STA 2985, RIB 7. REPLACED RUDDER HINGE FITTING NR 5 IAW A319 SRM 51-72-11 & AMM 55-36-41-400-001.Mar 13, 2012 · N836AW · Airbus A319132 · Rudder StructureSDR USAA2012032700009Hinge Fitting · excess play1S CHECK - RUDDER HINGE POINT NR 3 HAS EXCESSIVE PLAY OF 0.570 INCH AT VERTICAL STABILIZER STA.2279, RIB 5. REPLACED RUDDER HINGE FITTING NR 3 IAW A319 SRM 51-72-11 & AMM 55-36-41-400-001.Mar 13, 2012 · N836AW · Airbus A319132 · Rudder StructureSDR USAA2012032700008Hinge Fitting · excess play1S CHECK - RUDDER HINGE POINT NR 2 HAS EXCESSIVE PLAY OF 0.565 INCH AT VERTICAL STABILIZER STA 1926, RIB 4. REPLACED RUDDER HINGE FITTING NR 2 IAW A319 SRM 51-72-11 & AMM 55-36-41-400-001.Mar 13, 2012 · N836AW · Airbus A319132 · Rudder StructureSDR USAA2012032700007Hinge Fitting · excess play1S CHECK - RUDDER HINGE POINT NR 1 HAS EXCESSIVE PLAY OF 0.566 INCH AT VERTICAL STABILIZER STA 780, RIB 2. REPLACED RUDDER HINGE FITTING NR 1 IAW A319 SRM 51-72-11 & AMM 55-36-41-400-001.Mar 13, 2012 · N836AW · Airbus A319132 · Rudder StructureSDR USAA2012032800001Floor Panel · delaminated1S CHECK - DELAMINATION ON FLOOR PANEL 161BF BETWEEN FR59 TO FR63 & Y765 TO -Y970.8. REPLACED FLOOR PANEL 161BF IAW A319 SRM 53-02-00 & IRM 9701 REV G.Mar 12, 2012 · N836AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012032700014Floor Panel · delaminated1S CHECK - DELAMINATION ON FLOOR PANEL 162BF BETWEEN FR59 TO FR63 & BETWEEN -Y765 & -Y970.8. REPLACED FLOOR PANEL 162BF IAW A319 SRM 53-02-00 & IRM 9701 REV G.Mar 12, 2012 · N836AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012032000024Floor Panel · delaminated1S CHECK - DELAMINATION ON FLOOR PANEL 131BF BETWEEN FR24 TO FR28 & BETWEEN Y765 TO Y970.8. REPLACED FLOOR PANEL 131BF IAW A319 SRM 53-02-00 AND IRM 9701 REV G.Mar 12, 2012 · N836AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012032000023Floor Panel · delaminated1S CHECK - DELAMINATION ON FLOOR PANEL 131EG BETWEEN FR28 TO FR34 & BETWEEN Y1328 TO Y1042.1. REPLACED FLOOR PANEL 131EG IAW A319 SRM 53-02-00 AND IRM 9701 REV G.Mar 12, 2012 · N836AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012032000022Floor Panel · delaminated1S CHECK - DELAMINATION ON FLOOR PANEL 131AF BETWEEN FR24 TO FR28 & BETWEEN Y765 TO -Y765. REPLACED FLOOR PANEL 131AF IAW A319 SRM 53-02-00 AND IRM 9701 REV G.Mar 12, 2012 · N836AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012032000021Floor Panel · delaminated1S CHECK - DELAMINATION ON FLOOR PANEL 131CG BETWEEN FR28 TO FR34 & BETWEEN Y1912.8 TO -Y1912.8. REPLACED FLOOR PANEL 131CG IAW A319 SRM 53-02-00 AND IRM 9701 REV G.Mar 12, 2012 · N836AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2012030200007Battery · dischargedEMERGENCY EXIT LIGHT TEST FAILED. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY FWD PER AMM 33-51-38-401.Mar 1, 2012 · N836AW · Airbus A319132 · Emergency LightingSDR USAA2011090800020Line · out of positionR1 DOOR SLIDE MOORING LINE REQUIRED INSPECTION. REPOSITIONED R1 DOOR SLIDE MOORING LINE PER AMM25-62-44-401.Sep 4, 2011 · N836AW · Airbus A319132 · Escape SlideSDR USAA2011062700005Floorbeam · corrodedMCN - C11 - LEVEL 2 EXFOLIATION CORROSION FLOORBEAM BETWEEN FR68 TO FR69, -Z240, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Z240, -Y1292 IAW A319 SRM 51-72-11.Jun 15, 2011 · N836AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2011062300026Floorbeam · corrodedMCN - C11 - LEVEL 2 EXFOLIATION CORROSION FLOORBEAM AT FR66, -Z240, Y1292. REPLACED FLOORBEAM AT FR66, -Z240, Y1292 IAW A319 SRM 51-42-11.Jun 15, 2011 · N836AW · Airbus A319132 · Fuselage Main, Floor BeamSDR USAA2011062300025Plate · corrodedMCN - C11 - LEVEL 2 EXFOLIATION CORROSION FLOOR PANEL CONNECTING PLATE AT FR68, -Z240 BETWEEN -Y1292 TO -Y1732. REPLACED FLOOR PANEL CONNECTING PLATE AT FR68, -Z240 BETWEEN -Y1292 TO -Y1732IAW A319 SRM 51-40-02.Jun 5, 2011 · N836AW · Airbus A319132 · Fuselage Floor PanelSDR USAA2010111292594Sign · missingFLT 471 - SFO-LAS - EMERGENCY LIGHTS - L1 DOOR LOWER EMERGENCY EXIT SIGN MISSING. INSTALLED L1 DOOR LOWER EMERGENCY EXIT SIGN.Nov 11, 2010 · N836AW · Airbus A319132 · Emergency Lighting
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