# Service difficulty reports: N818AW A list on [N818AW](https://openairdocs.org/aircraft/N818AW.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 6 · 267 reports - [SDR AALA202610197215](https://openairdocs.org/sdr/AALA202610197215.md): Brake · dragging · Oct 17, 2026 · N818AW · Airbus A319132 · Landing Gear Brake System > AIRCRAFT WAS GROUNDED: WHILE TAXIING, WE NOTICED THAT THE AC WAS UNUSUALLY DIFFICULT TO TURN AND MANEUVER. IT REQUIRED SIGNIFICANTLY MORE ENGINE POWERTHAN NORMAL TO TAXI, AND ALSO HAD TO APPLY MORE BRAKE PRESSURETHAN USUAL.DESPITE NOT USING EXCESSIVE BRAKING, - [SDR AALA202609175127](https://openairdocs.org/sdr/AALA202609175127.md): Bearing · worn · Sep 13, 2026 · N818AW · Airbus A319132 · Passenger/Crew Doors > AIRCRAFT WAS GROUNDED: THE NUMBER 4 FLIGHT ATTENDANT REPORTED POST FLIGHT THAT CATERING WAS UNABLE TO OPEN DOOR 2L - MAINTENANCE FOUND THE DOOR UPPER HINGE FITTING SPHERICAL BEARING WORN AND DROPPING OUT OF ITS RACE - MAINTENANCE REPLACED THE SPHERICAL BEARING - [SDR AALA202609061700](https://openairdocs.org/sdr/AALA202609061700.md): Hydraulic System · leaking · Sep 4, 2026 · N818AW · Airbus A319132 · Hydraulic System, Main > AIRCRAFT WAS GROUNDED: AN EMERGENCY DECLARED & ACFT DIVERTED TO CLT DUE TO THE FLT CREW REPORTING AN GREEN HYD OVERHEAT ECAM MESSAGE DISPLAYED AT CRUISE. FLT CREW ACCOMPLISHED ECAM PROCEDURES & OVERHEAT MESSAGE CLEARED. FLT CREW RESET THE PUMP PER PROCEDURE & - [SDR AALA202608119096](https://openairdocs.org/sdr/AALA202608119096.md): Brake Sys · contaminated · Aug 9, 2026 · N818AW · Airbus A319132 · Landing Gear Brake System > AIRCRAFT WAS GROUNDED: BRAKE PEDALS SPONGY AND UNRESPONSIVE AT INITIAL APPLICATION THEN GRAB EXCESSIVELY AS PEDAL PRESSURE IS INCREASED - MAINTENANCE ACCOMPLISHED FILLING AND BLEEDING OF ALT BRAKE SYSTEM PER AMM TASK 32-43-00-612-001-A. - MAINTENANCE PURGED LA - [SDR AALA202607215471](https://openairdocs.org/sdr/AALA202607215471.md): Arming Lever · sticking · Jul 17, 2026 · N818AW · Airbus A319132 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED ARMING LEVER FOR 1L IS EXTREMELY HARD TO ARM THE DOOR. MAINTENANCE PERFORMED LUBRICATION OF THE DOOR ARMING/DISARMING MECHANISM PER AMM 12-22-52 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA202607150312](https://openairdocs.org/sdr/AALA202607150312.md): Sensor · leaking · Jul 12, 2026 · N818AW · Airbus A319132 · Airborne Auxiliary Power Unit (APU) System > AIRCRAFT WAS GROUNDED: MUSTY SOCK SMELL DURING DESCENT AT 18,000'. FLIGHT CREW DID FUMES REMOVAL PROCEDURE AND FUMES DISSIPATED. MAINTENANCE ACCOMPLISHED SMOKE, ODOR, FUMES TROUBLESHOOTING TASK CARD 26L00021001 AND FOUND THE APU IGV DRAIN WITH SIGNS OF OIL LEA - [SDR AALA202604306337](https://openairdocs.org/sdr/AALA202604306337.md): Light · broken · Apr 27, 2026 · N818AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: SEAT ROW 15 ABC HAS BROKEN EMERGENCY EXIT LIGHT. MAINTENANCE REPLACED THE DAMAGED EMERGENCY LIGHT HOUSING AT ROW15 ABC IAW CMM 25-22-52. - [SDR AALA202603117217](https://openairdocs.org/sdr/AALA202603117217.md): Accumulator · low pressure · Mar 10, 2026 · N818AW · Airbus A319132 · Service Doors > AIRCRAFT WAS NOT GROUNDED: RH AFT DOOR ACCUMULATOR REQUIRES SERVICING. MAINTENANCE SERVICED ACCUMULATOR TO CORRECT TOLERANCE PER AMM 52-10-00. - [SDR AALA202603119392](https://openairdocs.org/sdr/AALA202603119392.md): Accumulator · low pressure · Mar 10, 2026 · N818AW · Airbus A319132 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: LH FWD DOOR ACCUMULATOR REQUIRES SERVICING. MAINTENANCE SERVICED ACCUMULATOR TO CORRECT TOLERANCE PER AMM 52-10-00. - [SDR AALA202510029048](https://openairdocs.org/sdr/AALA202510029048.md): Lubrication Unit · leaking · Sep 18, 2025 · N818AW · Airbus A319132 · APU Oil System > AIRCRAFT WAS GROUNDED: IN CRUISE FLIGHT AT FL370, ONE HOUR INTO FLIGHT, FA NOTICED STRONG DIRTY SOCK ODOR IN AFT L LAVATORY. ODOR DISSIPATED AFTER 20 MINUTES. **SUPPLEMENTAL SDR FOR AALA202509229048. MAINTENANCE REPLACED OIL LUBE MODULE IAW AMM 49-91-45. - [SDR AALA202509229048](https://openairdocs.org/sdr/AALA202509229048.md): Unknown · odor · Sep 18, 2025 · N818AW · Airbus A319132 · Air Distribution System > AIRCRAFT WAS GROUNDED: IN CRUISE FLIGHT AT FL370, ONE HOUR INTO FLIGHT, FA NOTICED STRONG DIRTY SOCK ODOR IN AFT L LAVATORY. ODOR DISSIPATED AFTER 20 MINUTES. (OPEN) - [SDR AALA202507285093](https://openairdocs.org/sdr/AALA202507285093.md): Light · inoperative · Jul 19, 2025 · N818AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: EMERGENCY SEAT ROW LIGHT IS INOP AT ROW 8ABC. MAINTENANCE REPLACED EEPL & HOUSING IAW CMM 25-22-52. - [SDR AALA202507215093](https://openairdocs.org/sdr/AALA202507215093.md): Light · inoperative · Jul 19, 2025 · N818AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: EMERGENCY SEAT ROW LIGHT IS INOP AT ROW 8ABC. (OPEN) - [SDR AALA202501270522](https://openairdocs.org/sdr/AALA202501270522.md): Girt Bar · misinstalled · Jan 23, 2025 · N818AW · Airbus A319132 · Escape Slide > AIRCRAFT IN BASE MAINTENANCE: R1 SLIDE ARMED INDICATION INTERMITTENT ON POST CHECK FCF. MAINTENANCE INSTALLED CORRECTLY GIRT BAR ASSEMBLY ESCAPE SLIDE R1 IAW AMM 25-62-44-400-802-A STEP 4.A (5).(D) 2. AND PERFORMED OPERATIONAL TEST EMERGENCY ESCAPE SLIDE RELEA - [SDR AALA202501219575](https://openairdocs.org/sdr/AALA202501219575.md): Plate · cracked · Dec 11, 2024 · N818AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED BELLY FAIRING SUPPORT STRUCTURAL PLATE FASTENER HOLE AT FR 42 BETWEEN -Y254 AND -Y1682. REPAIRED PLATE PER EA 360673. - [SDR AALA202412236783](https://openairdocs.org/sdr/AALA202412236783.md): Plate · cracked · Dec 3, 2024 · N818AW · Airbus A319132 · Nacelle/Pylon, Plate/Skin > AIRCRAFT IN BASE MAINTENANCE: CRACK ON PYLON PLATE, LEFT HAND INBOARD SIDE AT LEVEL RIB 9. REPLACED PLATE PER SRM-51-42-11-801. - [SDR AALA202412232154](https://openairdocs.org/sdr/AALA202412232154.md): Bracket · cracked · Nov 30, 2024 · N818AW · Airbus A319132 · Nacelle/Pylon, Main Frame > AIRCRAFT IN BASE MAINTENANCE: CRACKED CROSSOVER BEAM BRACKET ON LEFT HAND PYLON. REPLACED BEAM BRACKET PER AMM 78-32-44. - [SDR AALA202501214053](https://openairdocs.org/sdr/AALA202501214053.md): Fitting · none · Nov 28, 2024 · N818AW · Airbus A319132 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LEFT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 4 AT Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 359886. REPLACED LEFT HAND CONTI - [SDR AALA202501217632](https://openairdocs.org/sdr/AALA202501217632.md): Fitting · none · Nov 28, 2024 · N818AW · Airbus A319132 · Standard Practices/Structures > AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 4 AT Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 359886. REPLACED RIGHT HAND CON - [SDR AALA202412234335](https://openairdocs.org/sdr/AALA202412234335.md): Hinge Arm · excess play · Nov 28, 2024 · N818AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM # 2 ON RH HORIZONTAL STABILIZER IAWAMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202412232236](https://openairdocs.org/sdr/AALA202412232236.md): Hinge Arm · excess play · Nov 28, 2024 · N818AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM # 6 ON RH HORIZONTAL STABILIZER IAWAMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202412237524](https://openairdocs.org/sdr/AALA202412237524.md): Hinge Arm · excess play · Nov 28, 2024 · N818AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 ON RH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM # 4 ON RH HORIZONTAL STABILIZER IAWAMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202412239846](https://openairdocs.org/sdr/AALA202412239846.md): Support Bracket · cracked · Nov 28, 2024 · N818AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK SUPPORT BRACKET LOCATED FACE ATTACH FR 1 UPPER AREA ON FORWARD PRESSURE BULKHEAD AT FR 1, WL Z-169. REPLACED STIFFENER PER SRM 51-72-11. - [SDR AALA202412164534](https://openairdocs.org/sdr/AALA202412164534.md): Hinge · excess play · Nov 28, 2024 · N818AW · Airbus A319132 · Horizontal Stabilizer Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY IN ELEVATOR HINGE ARM 5 ON LEFT HAND HORIZONTAL STABILIZER. REPLACED ELEVATOR HINGE ARM NUMBER 5 ON LEFT HAND HORIZONTAL STABILIZER. PER AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202412095768](https://openairdocs.org/sdr/AALA202412095768.md): Hinge Arm · excess play · Nov 28, 2024 · N818AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM # 6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202412090300](https://openairdocs.org/sdr/AALA202412090300.md): Hinge Arm · excess play · Nov 28, 2024 · N818AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM # 4 ON LH HORIZONTAL STABILIZER IAWAMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202412062374](https://openairdocs.org/sdr/AALA202412062374.md): Hinge Arm · excess play · Nov 28, 2024 · N818AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM # 3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202412062191](https://openairdocs.org/sdr/AALA202412062191.md): Hinge Arm · excess play · Nov 28, 2024 · N818AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM # 2 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202412023148](https://openairdocs.org/sdr/AALA202412023148.md): Hinge Arm · excess play · Nov 28, 2024 · N818AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM # 1 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202412233590](https://openairdocs.org/sdr/AALA202412233590.md): Door Frame · cracked · Nov 26, 2024 · N818AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CREW DOOR 842 CUT OUT LOCATED AT FR 68 UPPER CORNER. REPLACED UPPER CORNER PER SRM SRM 51-42-11. - [SDR AALA202412137480](https://openairdocs.org/sdr/AALA202412137480.md): Fitting · corroded · Nov 25, 2024 · N818AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11. - [SDR AALA202412093116](https://openairdocs.org/sdr/AALA202412093116.md): Support · corroded · Nov 25, 2024 · N818AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL AT LEVEL FR 68 AND STR 23 LEFT-HAND SIDE IN AFT GALLEY AREA, REPLACED EXISTING REPAIR LOCATED ON LOWER SILL PER SRM 53-41-14-300-001. - [SDR AALA202501239509](https://openairdocs.org/sdr/AALA202501239509.md): Shear Plate · cracked · Nov 24, 2024 · N818AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11. - [SDR AALA202501155066](https://openairdocs.org/sdr/AALA202501155066.md): Shear Plate · cracked · Nov 24, 2024 · N818AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 L BTW FR69 TO FR70 AT AFT GALLEY AREA MEASURE OF CRACK IS L= 0.776 INCH. MAINTENANCE REPLACED SHEAR PLATE AND FASTENERS LOCATED STR 23 L BTW FR69 TO FR70 AT AFT GALLEY AREA I.A.W A319 SRM 51-42-11-801, SR - [SDR AALA202412127766](https://openairdocs.org/sdr/AALA202412127766.md): Support · corroded · Nov 24, 2024 · N818AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SILL AT LEVEL FR 68 RIGHT HAND SIDE AT AFT GALLEY AREA. REPAIRED SILL PER SRM 53-41-14. - [SDR AALA202412097246](https://openairdocs.org/sdr/AALA202412097246.md): Floor Support · corroded · Nov 24, 2024 · N818AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR SUPPORTLOCATED AT -Y1292 BETWEEN FR 64 TO FR 66 IN AFT GALLEY AREA, REPLACED FLOOR SUPPORT PER SRM 51-72-11-801. - [SDR AALA202501116137](https://openairdocs.org/sdr/AALA202501116137.md): Frame · cracked · Nov 22, 2024 · N818AW · Airbus A319132 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACK FRAME 57 AT LEVEL STRG 23R IN PASSENGER CABIN (L=1.774 IN). MAINTENANCE REPLACED FRAME 57 AT LEVEL STRG 18R THRU 23R IN PASSENGER CABIN IAW A319SRM 51-42-11-801 DWG E53476200, E53476500 AND DWG E53476324. - [SDR AALA202501111233](https://openairdocs.org/sdr/AALA202501111233.md): Shear Plate · cracked · Nov 22, 2024 · N818AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK WEB LOCATED BTW FR 57 AND FR 58 AT LEVEL OF STRG 23 R IN PASSENGER CABIN, CRACK MEASURE L: 0.334. MAINTENANCE REPLACED WEB (SHEAR PLATE) LOC BTW FR 57 AND FR 58 AT LEVEL STRG 23R IN PASSENGER CABIN IAW A319 SRM 51-42-11-801 - [SDR AALA202501219913](https://openairdocs.org/sdr/AALA202501219913.md): Window Frame · cracked · Nov 20, 2024 · N818AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CENTER POST AREA AT FR 4 AND Y0. REPAIRED WINDSHIELD FRAMING PER EA 359886. - [SDR AALA202501194423](https://openairdocs.org/sdr/AALA202501194423.md): Hinge · out of limits · Nov 20, 2024 · N818AW · Airbus A319132 · Fuselage, Door Hinge > AIRCRAFT IN BASE MAINTENANCE: OUT LIMIT LH AFT DOOR 6MM IAW JC 26C71032007. MAINTENANCE REPLACED HARDWARE, FORWARD AND AFT HINGE FITTINGS ON NLG AFT DOOR ASSY LH IAW AMM 32-22-00-220-002-A, AMM 52-82-00-200-002-A, CMM 52-82-32, CMM 52-82-32-000-803-C01, CMM 5 - [SDR AALA202501213556](https://openairdocs.org/sdr/AALA202501213556.md): Window Frame · cracked · Nov 19, 2024 · N818AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CENTER POST AREA AT FR 4 AND Y0. REPAIRED WINDSHIELD FRAMING PER EA 359886. - [SDR AALA202410074836](https://openairdocs.org/sdr/AALA202410074836.md): Cover · warped · Oct 1, 2024 · N818AW · Airbus A319132 · Passenger/Crew Doors > L1 DOOR PLASTIC CASING / COVER WARPED; GATE AGENT REPORTS DOOR DIFFICULT TO CLOSE. MAINTENANCE REPLACED DOOR COVER 831FZ AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. - [SDR AALA202408195635](https://openairdocs.org/sdr/AALA202408195635.md): Fitting · worn · Aug 12, 2024 · N818AW · Airbus A319132 · Fuselage Main, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU LEFT HAND LATERAL FITTING WORN BETWEEN FR 23 AND FR 24 AT S32L. REPLACED LEFT HAND LATERAL FITTING PER EA 356990. - [SDR AALA202408192503](https://openairdocs.org/sdr/AALA202408192503.md): Fitting · worn · Aug 12, 2024 · N818AW · Airbus A319132 · Fuselage Main, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: AFT AVIONIC COMPARTMENT RACK 80VU RIGHT HAND LATERAL FITTING WORN BETWEEN FR 23 AND FR 24 AT S32R. REPLACED RIGHT HAND LATERAL FITTING PER EA 356990. - [SDR AALA202408059649](https://openairdocs.org/sdr/AALA202408059649.md): Hose · ruptured · Aug 3, 2024 · N818AW · Airbus A319132 · Hydraulic System, Main > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO IAD DUE TO THE YELLOW HYDRAULIC SYSTEM LOST ALL QUANTITY INFLIGHT. THE AIRCRAFT LANDED SAFELY AT IAD AND WAS TOWED TO THE GATE. MAINTENANCE FOUND THE HYDRAULIC FLEX LINE GOING TO THE - [SDR AALA202406202607](https://openairdocs.org/sdr/AALA202406202607.md): Connector · unsecure · Jun 19, 2024 · N818AW · Airbus A319132 · Light System Wiring > AIRCRAFT WAS GROUNDED: DURING PS CHECK EMERGENCY POWER SUPPLY UNIT INITIAL LOAD AFT LEFT FLAGGED. RESCURED CANNON PLUG. - [SDR AALA202406191561](https://openairdocs.org/sdr/AALA202406191561.md): Connector · unsecure · Jun 19, 2024 · N818AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT INTERNAL LOAD EMERGENCY LEFT MESSAGE DISPLAYED DURING SYSTEM TEST. MAINTENANCE RE-SECURED CANNON PLUG PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED. - [SDR AALA202406195305](https://openairdocs.org/sdr/AALA202406195305.md): Bottle · low pressure · Jun 19, 2024 · N818AW · Airbus A319132 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: MAINTENANCE FOUND L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE AT 1300PSI AT 80 DEGREES. MAINTENANCE SERVICED THE L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00. - [SDR AALA202406036166](https://openairdocs.org/sdr/AALA202406036166.md): Light · inoperative · Jun 2, 2024 · N818AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: NUMEROUS CABIN EXIT SIGN LIGHTS REPORTED AS HAVING MULTIPLE BULBS INOPERATIVE. REMOVED AND REPLACED AFT CABIN EXIT SIGN LIGHTS ASSEMBLY. - [SDR AALA202403153341](https://openairdocs.org/sdr/AALA202403153341.md): Bottle · low pressure · Mar 12, 2024 · N818AW · Airbus A319132 · Emergency Equipment > AIRCRAFT WAS NOT GROUNDED: L2 PASSENGER DOOR DAMPER AND EMERGENCY OPERATION CYLINDER IS BELOW PS CHECK LIMITS READING 1400 PSI AT 70 DEGREES. SERVICED L2 PASSENGER DOOR DAMPER AND EMERGENCY OPERATION CYLINDER. Next page: https://openairdocs.org/aircraft/N818AW/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 = 'N818AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N818AW/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.