# Service difficulty reports: N839AW A list on [N839AW](https://openairdocs.org/aircraft/N839AW.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 4 · 165 reports - [SDR AALA202610101350](https://openairdocs.org/sdr/AALA202610101350.md): Master Cylinder · defective · Oct 5, 2026 · N839AW · Airbus A319132 · Master Cylinder/Brake Valve > AIRCRAFT WAS GROUNDED: RIGHT BRAKE UNABLE TO MODULATE BRAKING PRESSURE, RIGHT BRAKE PEDAL HAS LITTLE OR NO FEEDBACK - MAINTENANCE REPLACED THE RIGHT-HAND MASTER CYLINDER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-43-12 - [SDR AALA202610072532](https://openairdocs.org/sdr/AALA202610072532.md): Brake Sys · contaminated · Oct 4, 2026 · N839AW · Airbus A319132 · Landing Gear Brake System > AIRCRAFT WAS NOT GROUNDED: DURING TAXI IN RIGHT BRAKE PEDAL SOFT DURING APPROXIMATELY FIRST HALF OF TOTAL TRAVEL CAUSING RIGHT BRAKE TO GRAB BUT BRAKE FUNCTIONS NORMALLY - MAINTENANCE INSPECTED AND BLED THE RIGHT BRAKE SYSTEM PER AMM 32-43-00 - [SDR AALA202606153421](https://openairdocs.org/sdr/AALA202606153421.md): Bottle · low pressure · Jun 12, 2026 · N839AW · Airbus A319132 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: LEFT AFT PASSENGER / CREW DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00. - [SDR AALA202601018306](https://openairdocs.org/sdr/AALA202601018306.md): Hinge Fitting · damaged · Dec 21, 2025 · N839AW · Airbus A319132 · Fuselage, Door Hinge > AIRCRAFT IN BASE MAINTENANCE: LT MLG DOOR FWD ATTACH FITTING BEARING DAMAGED. MAINTENANCE REPLACED FITTING (HINGE ASSY) LT MLG DOOR IAW A321 SRM 51-72-11-911-001. - [SDR AALA202512190633](https://openairdocs.org/sdr/AALA202512190633.md): Control Unit · fault message · Dec 15, 2025 · N839AW · Airbus A319132 · Aircraft Fuel Distribution System > AIRCRAFT WAS GROUNDED: ACCOUNT MAINTENANCE CENTER TANK PUMP 2 ECAM SYSTEM FAULT. DECESSION MADE TO RETURN TO DFW NO EMERGENCY DECLARED, AND FLIGHT WAS NOT OVERWEIGHT FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO GATE UNDER ITS OWN POWER. MAINTEN - [SDR AALA202512194629](https://openairdocs.org/sdr/AALA202512194629.md): Control Unit · fault message · Dec 15, 2025 · N839AW · Airbus A319132 · Aircraft Fuel Distribution System > AIRCRAFT WAS GROUNDED, ACCOUNT MAINTENANCE CENTER TANK PUMP 2 ECAM SYSTEM FAULT. DECESSION MADE TO RETURN TO DFW NO EMERGENCY DECLARED, AND FLIGHT WAS NOT OVERWEIGHT FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO GATE UNDER ITS OWN POWER. MAINTE - [SDR AALA202512184629](https://openairdocs.org/sdr/AALA202512184629.md): Pump · warning message · Dec 15, 2025 · N839AW · Airbus A319132 · Fuel Boost Pump > AIRCRAFT WAS GROUNDED: ACCOUNT MAINTENANCE CENTER TANK PUMP 2 ECAM SYSTEM FAULT. DECESSION MADE TO RETURN TO DFW NO EMERGENCY DECLARED, AND FLIGHT WAS NOT OVERWEIGHT FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO GATE UNDER ITS OWN POWER. (OPEN) - [SDR AALA202511255657](https://openairdocs.org/sdr/AALA202511255657.md): Elec Connector · disconnected · Nov 20, 2025 · N839AW · Airbus A319132 · Light System Wiring > AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK, FOUND EMERGENCY CEILING LIGHT AT ROW 23 INOP. MAINTENANCE FOUND ROW 23 CEILING PANEL EMERGENCY LIGHT ELECTRICAL CONNECTOR NOT CONNECTED. RECONNECTED AND OPS CHECK GOOD IAW AMM 33-51-11. - [SDR AALA202507098993](https://openairdocs.org/sdr/AALA202507098993.md): Door Latch · binding · Jul 8, 2025 · N839AW · Airbus A319132 · Fixed Inner Doors > AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR TOOK TWO OFF US TO GET OPEN AND WILL NOT CLOSE NOW THAT THE DOOR IS OPEN. MAINTENANCE ADJUSTED COCKPIT DOOR LATCH MECHANISM REF. AMM 52-51-21. - [SDR AALA202501238733](https://openairdocs.org/sdr/AALA202501238733.md): Battery · no test · Jan 22, 2025 · N839AW · Airbus A319132 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT DURING THE PRE-FLIGHT CHECKS THEY WERE UNABLE TO SEE RED FLASHING LIGHT ON THE AFT GALLEY FLASHLIGHT. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY PER AMM 25-60-00. - [SDR AALA202411149345](https://openairdocs.org/sdr/AALA202411149345.md): Skin Panel · worn · Nov 13, 2024 · N839AW · Airbus A319132 · Wing, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTER BOTTOM SKIN PANEL LOWER SURFACE HAS ELONGATED FASTENER HOLE BETWEEN RIBS 17 AND 18. REPAIRED SKIN PANEL PER SRM 57-21-11-300-002. - [SDR AALA202409177988](https://openairdocs.org/sdr/AALA202409177988.md): Hinge Fitting · excess play · Sep 13, 2024 · N839AW · Airbus A319132 · Elevator Structure > AIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON RH HORIZONTAL STABILIZER. REPLACED HINGE ARM END FITTING # 1 ON RH HORIZONTAL STABILIZER IAW AMM55-16-42-000-001-A AND AMM 55-16-42-400-001-A REFER TO INDIVIDUAL SIGN-OFFENTRIES FOR WORK - [SDR AALA202411016951](https://openairdocs.org/sdr/AALA202411016951.md): Hinge Arm · excess play · Sep 11, 2024 · N839AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING 5 ON RH HORIZONTAL STABILIZER I.A.W AMM-55-16-42-000-001-A AND AMM-55-16-42-400-001-A. - [SDR AALA202410298739](https://openairdocs.org/sdr/AALA202410298739.md): Fitting · cracked · Sep 10, 2024 · N839AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT FR 16 RIGHT AND #7 DOOR STOP FITTING. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11. - [SDR AALA202411054876](https://openairdocs.org/sdr/AALA202411054876.md): Window Frame · cracked · Sep 9, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD RIGHT HAND LATERAL FRAME UPPER TENSION BOLT HOLE AT FR 4 RIGHT HAND. REPLACED FRAME PER EA 357887. - [SDR AALA202411059130](https://openairdocs.org/sdr/AALA202411059130.md): Window Frame · cracked · Sep 9, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD LEFT HAND LATERAL FRAME UPPER TENSION BOLT HOLE AT FR 4 LEFT HAND. REPLACED FRAME PER EA 357887. - [SDR AALA202409209108](https://openairdocs.org/sdr/AALA202409209108.md): Beam · corroded · Sep 8, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN LEFT HAND DOOR SILL BEAM BETWEEN FR 67 AND FR 68 AT S23L. REPAIRED DOOR SILL BEAM PER SRM 53-41-14-300-001. - [SDR AALA202411113496](https://openairdocs.org/sdr/AALA202411113496.md): Door Frame · cracked · Sep 7, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE ON THE DOUBLE JOGGLE AREA AT FR 16 LEFT AND #5 DOOR STOP FITTING. REPLACED FRAME PER EA 357865. - [SDR AALA202411084056](https://openairdocs.org/sdr/AALA202411084056.md): Frame · cracked · Sep 7, 2024 · N839AW · Airbus A319132 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME DOUBLE JOGGLE AREA FASTENER HOLE AT FR 16 RIGHT AND S5R. REPAIRED FRAME PER EA 357885. - [SDR AALA202409201145](https://openairdocs.org/sdr/AALA202409201145.md): Floor Support · corroded · Sep 7, 2024 · N839AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM BETWEEN FR 12 AND FR 20 AT +Y503.2. REPLACED FLOOR BEAM PER SRM 51-72-11. - [SDR AALA202411131499](https://openairdocs.org/sdr/AALA202411131499.md): Window Frame · cracked · Sep 5, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > **SUPPLEMENTAL REPORT TO ADD UPPER RADIUS CRACK** AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CENTER POST FRAME LOWER NODE ATTACHMENT AREA LOWER AND UPPER INBOARD RADIUS CRACKED BETWEEN FR 3 AND FR 5 AT Y0. REPLACED CENTER PO - [SDR AALA202411081499](https://openairdocs.org/sdr/AALA202411081499.md): Window Frame · cracked · Sep 5, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CENTER POST FRAME LOWER NODE ATTACHMENT AREA LOWER INBOARD RADIUS CRACKED BETWEEN FR 3 AND FR 5 AT Y0. REPLACED CENTER POST FRAME PER EA 357783. - [SDR AALA202411081765](https://openairdocs.org/sdr/AALA202411081765.md): Window Frame · cracked · Sep 5, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CENTER POST FRAME LOWER NODE ATTACHMENT AREA LOWER INBOARD RADIUS CRACKED BETWEEN FR 3 AND FR 5 AT Y0. REPLACED CENTER POST FRAME PER EA 357783. - [SDR AALA202411081823](https://openairdocs.org/sdr/AALA202411081823.md): Fitting · cracked · Sep 5, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 3 AND FR 5 AT Y0. REPLACED CONTINUITY FITTING PER EA 357783. - [SDR AALA202411085807](https://openairdocs.org/sdr/AALA202411085807.md): Fitting · cracked · Sep 5, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED BETWEEN FR 3 AND FR 5 AT Y0. REPLACED CONTINUITY FITTING PER EA 357783. - [SDR AALA202410231409](https://openairdocs.org/sdr/AALA202410231409.md): Fork · worn · Sep 2, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU RIGHT HAND LATERAL FORK END FITTING WORN BETWEEN FR 23 AND FR 24 AT S32L. REPLACED RIGHT HAND LATERAL FORK END FITTING PER EA 357678. - [SDR AALA202410235424](https://openairdocs.org/sdr/AALA202410235424.md): Fork · worn · Sep 2, 2024 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FORK END FITTING WORN BETWEEN FR 23 AND FR 24 AT S32L. REPLACED LEFT HAND LATERAL FORK END FITTING PER EA 357678. - [SDR AALA202308144249](https://openairdocs.org/sdr/AALA202308144249.md): Switch · warning message · Aug 10, 2023 · N839AW · Airbus A319132 · Hydraulic System, Main > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO COS DUE TO A YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL MESSAGE AFTER TAKEOFF. THE AIRCRAFT LANDED SAFELY AT COS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE YELLOW HYDRAULIC - [SDR AALA202303072489](https://openairdocs.org/sdr/AALA202303072489.md): Support · loose · Mar 4, 2023 · N839AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: 80VU RACK UPPER FITTING SUPPORT ROD LOOSE. MAINTENANACE REPLACED 80VU RACK UPPER FITTING SUPPORT ROD PER SRM 51-72-11. - [SDR AALA202302082126](https://openairdocs.org/sdr/AALA202302082126.md): Connector · defective · Feb 7, 2023 · N839AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: SEAT ROW 9 ABC AND 10ABC EMERGENCY LIGHTS ON SEAT INOPERATIVE. MAINTENANCE REPLACED SIDEWALL EMERGENCY LIGHT CONNECTOR 7260VC3 PER AWM 33-51-06 AND ESPM 20-48-21. A SATISFACTORY OPERATIONAL CHECK OF THE EMERGENCY LIGHTS WAS ACCOMPLIS - [SDR AALA202301042843](https://openairdocs.org/sdr/AALA202301042843.md): Smoke Detector · false indication · Jan 2, 2023 · N839AW · Airbus A319132 · Smoke Detection > AIRCRAFT WAS NOT GROUNDED: SMOKE LAVATORY SMOKE ECAM DURING DESCENT. NO SMOKE OR ODORS DETECTED IN FORWARD LAVATORY. MAINTENANCE PERFORMED RESET PER TSM 24-00-00 WITH NO FAULTS NOTED. - [SDR AALA202205042308](https://openairdocs.org/sdr/AALA202205042308.md): O-Ring · leaking · May 2, 2022 · N839AW · Airbus A319132 · Hydraulic System, Main > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO ORD DUE TO LOSS OF GREEN HYDRAULIC SYSTEM FLUID. THE AIRCRAFT LANDED SAFELY AND WAS TOWED TO THE GATE. MAINTENANCE FOUND A DAMAGED O-RING FOR THE GREEN HYDRAULIC SYSTEM POWER TRANSFER UNIT MANIFOLD CAUSING - [SDR AALA202112238887](https://openairdocs.org/sdr/AALA202112238887.md): Splice · corroded · Dec 23, 2021 · N839AW · Airbus A319132 · Fuselage Main, Longeron/Stringer > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER SPLICE BETWEEN FR 64 AND FR 65 AT S44 AND BUTT LINE 0. REPAIRED STRINGER SPLICE PER SRM 53-41-13-300-004 FIG 001. - [SDR AALA202111302990](https://openairdocs.org/sdr/AALA202111302990.md): Flashlight · discharged · Nov 29, 2021 · N839AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: #4 FLIGHT ATTENDANT SEAT FLASH LIGHT USED/ SEAL BROKEN. REPLACED FLASHLIGHT (AALA202111302990) AND BATTERY PER EMERGENCY EQUIPMENT DRAWING 26X25D1218 (AALA202111303557) - [SDR AALA202111303557](https://openairdocs.org/sdr/AALA202111303557.md): Battery · discharged · Nov 29, 2021 · N839AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: #4 FLIGHT ATTENDANT SEAT FLASH LIGHT USED/ SEAL BROKEN. REPLACED FLASHLIGHT (AALA202111302990) AND BATTERY PER EMERGENCY EQUIPMENT DRAWING 26X25D1218 (AALA202111303557) - [SDR AALA2020061769009](https://openairdocs.org/sdr/AALA2020061769009.md): Smoke Detector · false indication · Jun 15, 2020 · N839AW · Airbus A319132 · Smoke Detection > AIRCRAFT NOT GROUNDED. AVIONICS SMOKE CAUTION ON ECAM. PERFORMED RESET OF AVIONICS SMOKE DETECTION SYSTEM AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 26-15-00. - [SDR AALA202004219017](https://openairdocs.org/sdr/AALA202004219017.md): Engine · power loss · Apr 20, 2020 · N839AW · Airbus A319132 · Fuel Controlling System > AIRCRAFT WAS GROUNDED: ON TAKEOFF, WHEN THRUST LEVERS WERE PLACED IN FLEX DETENT, THERE WAS A SIGNIFICANT DIFFERENCE IN ENGINE EPR. #1 EPR, WE BELIEVE ACHIEVED APPROX. 1.4, WHILE #2 ACHIEVED APPROX..1.2. REJECTED TAKEOFF APPROX. 70 KNOTS. REMOVED AND REPLACED - [SDR AALA201912249016](https://openairdocs.org/sdr/AALA201912249016.md): Plug · defective · Dec 20, 2019 · N839AW · Airbus A319132 · Fuel Control/Turbine Engines > AIRCRAFT WAS GROUNDED: ON TAKEOFF DURING STABILIZING ENGINES AT 1.05 EPR NR 2 ENGINE SLOWTO RESPOND 6-8 SECONDS SLOWER THAN ENGINE NR 1. SUPPLEMENTAL REPORT: REPLACED EEC DATA PLUG WITH CORRECT RATING PER EA 300711 AND TASK CARD 26P32072022. (CLOSED) - [SDR AALA2019120969022](https://openairdocs.org/sdr/AALA2019120969022.md): Fitting · worn · Nov 22, 2019 · N839AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR ATTACHMENT FITTING ON KEEL BEAM AFT LUG WORN AT FR 42 AND S42R. REPLACED FITTING PER EA 300673. - [SDR AALA201904259001](https://openairdocs.org/sdr/AALA201904259001.md): Water Heater · faulty · Apr 24, 2019 · N839AW · Airbus A319132 · Potable Water System > AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS SMOKE SMELL IN FWD PORTION OF CABIN GALLEY/ LAV AREA. MAINTENANCE REMOVED AND REPLACED FWD LAV WATER HEATER IAW 38-12-16. LEAK CHECK PERFORMED, CHECKS GOOD. - [SDR AALA201903279033](https://openairdocs.org/sdr/AALA201903279033.md): Plug · leaking · Mar 24, 2019 · N839AW · Airbus A319132 · APU Oil System > A STRONG MUSTY ODOR FOR THE LAST 5 MINUTES OF FLIGHT IN COCKPIT AND CABIN. APU WAS OFF AT THE TIME. THE AIRCRAFT WAS GROUNDED. APU FACTORY GEAR BOX PLUG LEAKING OIL DOWN ON INLET AND INGESTED, IN INTAKE. MAINTENANCE REMOVED AND REPLACED THE APU IAW CARD 26L - [SDR AALA2019030189008](https://openairdocs.org/sdr/AALA2019030189008.md): Bulb · burned out · Feb 26, 2019 · N839AW · Airbus A319132 · Passenger Compartment Lighting > DURING DESCENT, FROM FL 180 UNTILL LANDING, ENCOUNTERED A CABIN ODOR MORE NOTICEABLE IN THE FLIGHT DECK AND IT CONTINUED AFTER LANDING. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED WORKCARD 26L0021001 & 26L0021002 WITH NO ODOR NOTED IN FLIGHT DECK OR CABIN. MA - [SDR AALA2018102429037](https://openairdocs.org/sdr/AALA2018102429037.md): Fan · burned · Oct 21, 2018 · N839AW · Airbus A319132 · Air Distribution Fan > LEFT RECIRCULATION FAN 15HG HAD A BURNING ODOR AND GRINDING SOUND. REPLACED THE FAN IAW AMM 21-21-51. OPS CHECKED GOOD. - [SDR AALA2018100219032](https://openairdocs.org/sdr/AALA2018100219032.md): Battery · inoperative · Sep 30, 2018 · N839AW · Airbus A319132 · Emergency Equipment > FLIGHT ATTENDANT REAR JUMP SEAT NR 4 FLASHLIGHT INOPERATIVE. REPLACED BATTERY IAW MM 25-65-00. - [SDR AALA201809139015](https://openairdocs.org/sdr/AALA201809139015.md): Fitting · corroded · Sep 4, 2018 · N839AW · Airbus A319132 · Fuselage Miscellaneous Structure > CORROSION WAS FOUND ON THE CORNER FITTING AT FRAME 68, STRINGER 23L. REPLACED THE FITTING IAW SRM 51-72-11, DRAWINGS D53480505, AND D53480019. - [SDR AALA201809289005](https://openairdocs.org/sdr/AALA201809289005.md): Box Beam · cracked · Sep 1, 2018 · N839AW · Airbus A319132 · Fuselage Main, Structure > A CRACK INDICATION WAS FOUND ON THE FRAME 43, -Y1650, SIDE BOX BEAM FLANGE. REPAIRED THE SIDE BOX BEAM FLANGE IAW EO 5315Y066-001. - [SDR AALA201809289004](https://openairdocs.org/sdr/AALA201809289004.md): Box Beam · cracked · Sep 1, 2018 · N839AW · Airbus A319132 · Fuselage Main, Structure > A CRACK INDICATION WAS FOUND ON THE FRAME 43, -Y1650, SIDE BOX BEAM FLANGE. REPAIRED THE SIDE BOX BEAM FLANGE IAW EA 5315Y066-001. - [SDR AALA201809289003](https://openairdocs.org/sdr/AALA201809289003.md): Box Beam · cracked · Sep 1, 2018 · N839AW · Airbus A319132 · Fuselage Main, Structure > A CRACK INDICATION WAS FOUND ON THE FRAME 43, Y1650 SIDE BOX BEAM FLANGE. REPAIRED THE SIDE BOX BEAM FLANGE IAW EO CARD 5315Y066-001. - [SDR AALA201809129009](https://openairdocs.org/sdr/AALA201809129009.md): Floor Panel · delaminated · Sep 1, 2018 · N839AW · Airbus A319132 · Fuselage Floor Panel > DELAMINATION FOUND ON FLOOR PANEL 242DF IN THE PASSENGER CABIN. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REVISION H. - [SDR AALA201809129010](https://openairdocs.org/sdr/AALA201809129010.md): Floor Panel · delaminated · Sep 1, 2018 · N839AW · Airbus A319132 · Fuselage Floor Panel > DELAMINATION FOUND ON FLOOR PANEL 251TF. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REV.H. Next page: https://openairdocs.org/aircraft/N839AW/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 = 'N839AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N839AW/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.