# Service difficulty reports: N826AW A list on [N826AW](https://openairdocs.org/aircraft/N826AW.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 · 259 reports - [SDR AALA202609306484](https://openairdocs.org/sdr/AALA202609306484.md): Power Supply · inoperative · Sep 28, 2026 · N826AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: MID AND AFT EMERGENCY EXIT LIGHTS WILL NOT TURN OFF. MAINTENANCE REPLACED FORWARD EMERGENCY LIGHT POWER SUPPLY. OPS CHECKS SATISFACTORY REFERENCE AMM 33-51-38. - [SDR AALA202608118246](https://openairdocs.org/sdr/AALA202608118246.md): Probe · faulted · Aug 10, 2026 · N826AW · Airbus A319132 · Engine (Turbine/Turboprop) > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO BOS DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 IS CREATING SIGNIFICANTLY LESS THRUST THAN ENGINE 1 WHICH WAS CREATING A YAWING MOMENT - THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE - [SDR AALA202606285042](https://openairdocs.org/sdr/AALA202606285042.md): Panel · fault message · Jun 24, 2026 · N826AW · Airbus A319132 · Door Warning System > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ORD SHORTLY AFTER TAKEOFF BECAUSE OF A MAIN CABIN DOOR 1L PRESSURIZATION WARNING LIGHT. LIGHT CAME ON AS THE AIRCRAFT ACCELERATED AND EXTINGUISHED BELOW 180 KNOTS. THE AIRCRAFT LANDE - [SDR AALA202606104568](https://openairdocs.org/sdr/AALA202606104568.md): Elec Connector · disconnected · Jun 9, 2026 · N826AW · Airbus A319132 · Light System Wiring > AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT SEAT 9C FOUND INOPERATIVE. MAINTENANCE FOUND LIGHT HARNESS ASSEMBLY UNPLUGGED AND RECONNECTED LIGHT PER AMM 33-51-18. - [SDR AALA202510201061](https://openairdocs.org/sdr/AALA202510201061.md): Accumulator · low pressure · Oct 20, 2025 · N826AW · Airbus A319132 · Passenger/Crew Doors > AIRCRAFT WAS NOT GROUNDED: R1 DOOR EMERGENCY ACCUMULATOR REQUIRES SERVICE. MAINTENANCE SERVICED R1 DOOR EMERGENCY ACCUMULATOR BOTTLE IAW AMM 52-10-00. - [SDR AALA202508298251](https://openairdocs.org/sdr/AALA202508298251.md): Attach Bolt · corroded · Aug 25, 2025 · N826AW · Airbus A319132 · Wing, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 8 (LOWER MID) ON LH WING L=0.443 INCH, W=0.167 INCH AND D=0.002 INCH. MAINTENANCE REPLACED ATTACHE BOTL AT SLAT TRACK 8 ON LH WING. - [SDR AALA202508298555](https://openairdocs.org/sdr/AALA202508298555.md): Attach Bolt · corroded · Aug 25, 2025 · N826AW · Airbus A319132 · Wing, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 8 (LOWER FWD) ON LH WING L=0.445 INCH, W=0.169 INCH AND D=0.001 INCH. MAINTENANCE REPLACED ATTACH BOLT AT SLAT TRACK 8 ON LH WING. - [SDR AALA202508294542](https://openairdocs.org/sdr/AALA202508294542.md): Attach Bolt · corroded · Aug 25, 2025 · N826AW · Airbus A319132 · Wing, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 7 (LOWER BOLT) ON LH WING L=0.449 INCH, W=0.170 INCH AND D=0.002 INCH. MAINTENANCE REPLACED ATTACH BOLT AT SLAT TRACK 7 ON LH WING. - [SDR AALA202508298290](https://openairdocs.org/sdr/AALA202508298290.md): Attach Bolt · corroded · Aug 25, 2025 · N826AW · Airbus A319132 · Wing, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION BOLT ATTACHMENT SLAT TRACK 3 (LOWER BOLT) ON LH WING L: 0.450 INCH, W: 0.171 INCH, D: 0.001 INCH. MAINTENANCE REPLACED ATTACH BOLT AT SLAT TRACK 3 ON LH WING. - [SDR AALA202508020199](https://openairdocs.org/sdr/AALA202508020199.md): Floor Support · corroded · Jul 19, 2025 · N826AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM Y1162.5 BTW FR68 AND FR69 AT AFT GALLEY AREA CORRODED AREA IS L= 0.537 IN W=0.258 IN D=0.030 IN. MAINTENANCE REPLACED FLOOR BEAM Y1162.5 LOC BTW FR68 TO FR69 AT AFT GALLEY IAW A319 SRM 51-72-11-911-001, DWG D5 - [SDR AALA202507210529](https://openairdocs.org/sdr/AALA202507210529.md): Hinge Arm · excess play · Jul 18, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 1 LH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM #1 LH ON HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202507216218](https://openairdocs.org/sdr/AALA202507216218.md): Hinge Arm · excess play · Jul 18, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 2 LH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM #2 LH ON HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202507219753](https://openairdocs.org/sdr/AALA202507219753.md): Hinge Arm · excess play · Jul 18, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 3 LH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM #3 LH ON HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202507217387](https://openairdocs.org/sdr/AALA202507217387.md): Hinge Arm · excess play · Jul 18, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 4 LH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM #4 LH ON HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202507218789](https://openairdocs.org/sdr/AALA202507218789.md): Hinge Arm · excess play · Jul 18, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 LH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM #5 LH ON HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202507211099](https://openairdocs.org/sdr/AALA202507211099.md): Hinge Arm · excess play · Jul 18, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 LH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM #5 LH ON HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202507174356](https://openairdocs.org/sdr/AALA202507174356.md): Hinge Arm · excess play · Jul 16, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 5 RH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM #5 RH ON HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202507176566](https://openairdocs.org/sdr/AALA202507176566.md): Hinge Arm · excess play · Jul 16, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM 6 RH ON HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM #6 RH ON HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A. - [SDR AALA202507161247](https://openairdocs.org/sdr/AALA202507161247.md): Hinge Arm · excess play · Jul 14, 2025 · N826AW · Airbus A319132 · Horizontal Stabilizer Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #1 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42. - [SDR AALA202507165297](https://openairdocs.org/sdr/AALA202507165297.md): Hinge Arm · excess play · Jul 14, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #3 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42. - [SDR AALA202507163674](https://openairdocs.org/sdr/AALA202507163674.md): Hinge Arm · excess play · Jul 14, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #2 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42. - [SDR AALA202507164101](https://openairdocs.org/sdr/AALA202507164101.md): Hinge Arm · excess play · Jul 14, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #4 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42. - [SDR AALA202508091691](https://openairdocs.org/sdr/AALA202508091691.md): Fitting · corroded · Jul 10, 2025 · N826AW · Airbus A319132 · Nacelle/Pylon, Attach Fittings > AIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON MEASURE OF CORROSION ARE: L=13.600 INCH, W:1.345 INCH, D:0.009 INCH. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON IAW A319 SRM 54-51-12-300-002. - [SDR AALA202508014380](https://openairdocs.org/sdr/AALA202508014380.md): Fitting · corroded · Jul 2, 2025 · N826AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING LH SIDE FWD GALLEY AREA, MEASURE OF CORROSION: L=0.494 INCH, W=0.423 INCH, D=0.020 INCH. MAINTENANCE REPLACED CENTER FITTING LOC BTW FR16 TO FR 20 STR 23 LH SIDE FWD GALLEY AREA I.A.W A319 SRM 51-42-11-80 - [SDR AALA202507218072](https://openairdocs.org/sdr/AALA202507218072.md): Fitting · corroded · Jul 2, 2025 · N826AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING LH SIDE AFT GALLEY AREA MEASURES OF CORROSION ARE: L= 0.823IN W= 0.291IN D= 0.040IN. MAINTENANCE REPLACED CENTER FITTING LOC. FR 66 TO FR 68 AT LEVEL STRG 23 LH SIDE AFT GALLEY AREA IAW A319 SRM 51-72-11- - [SDR AALA202509020866](https://openairdocs.org/sdr/AALA202509020866.md): Angle · corroded · Jul 1, 2025 · N826AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION INTERNAL STRUCTURE ANGLE FR71 AT DOOR CUT OUT IN THS COMPARMENT CORRODED AREA IS L=2.917 IN W=0.828 IN D= 0.015 IN. REPLACED ANGLE LOC FR71 AT DOOR CUT OUT IN THS COMPARMENT IAW A319 SRM 51-42-11-801, A319 SRM 51-72-11- - [SDR AALA202508291665](https://openairdocs.org/sdr/AALA202508291665.md): Stiffener · cracked · Jul 1, 2025 · N826AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON OPEN HOLE ON CENTER WING BOX FR36 FRONT SPAR VERTICAL STRINGER ZONE 2, CRACK DIRECTION AT 12 O CLOCK, D= 0.110 INCH. MAINTENANCE REPLACED STIFFENER LOCATED ON FR1 (Z-169) FWD FACE FWD PRESSURE BULKHEAD IA - [SDR AALA202508299397](https://openairdocs.org/sdr/AALA202508299397.md): Floorbeam · cracked · Jul 1, 2025 · N826AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACKS INDICATION FOUND ON OPEN HOLE ON CENTER WING BOX FR36 FRONT SPAR VERTICAL STRINGER 2 ZONE 1,CRACKS DIRECTION AT 11 O CLOCK, 3 O CLOCK AND 5 O CLOCK, D= 0.105 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR (PARTIAL REPLACE - [SDR AALA202508266025](https://openairdocs.org/sdr/AALA202508266025.md): Floorbeam · cracked · Jul 1, 2025 · N826AW · Airbus A319132 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CRACKS INDICATION FOUND ON OPEN HOLE ON CENTER WING BOX FR36 FRONT SPAR VERTICAL STRINGER 3 ZONE 1,D= 0.115 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR (PARTIAL REPLACEMENT) ON FLOOR BEAM Y254 LOC. AT LEVEL FR36 FLOOR STRUCT - [SDR AALA202508269578](https://openairdocs.org/sdr/AALA202508269578.md): Floorbeam · cracked · Jul 1, 2025 · N826AW · Airbus A319132 · Fuselage Main, Floor Beam > AIRCRAFT IN BASE MAINTENANCE: CRACKS INDICATION FOUND ON OPEN HOLE ON CENTER WING BOX FR36 FRONT SPAR VERTICAL STRINGER 4 ZONE 1, CRACKS DIRECTION AT 12 O CLOCK, 5 O CLOC K AND 3 O CLOCK, D= 0.112 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR (PARTIAL REPLA - [SDR AALA202507280422](https://openairdocs.org/sdr/AALA202507280422.md): Bushing · migrated · Jul 1, 2025 · N826AW · Airbus A319132 · Elevator Structure > AIRCRAFT IN BASE MAINTENANCE: MIGRATED PLAIN BUSHING HINGE FITTING 1 O/B ON LH ELEVATOR. MAINTENANCE REPAIRED O/B LUG OF HINGE FITTING #1 AT LH ELEVATOR AND REPLACED BUSHING IAW A319 SRM 55-26-41-300-010. - [SDR AALA202508015973](https://openairdocs.org/sdr/AALA202508015973.md): Shear Plate · cracked · Jun 28, 2025 · N826AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R LOC. BTW FR69 AND FR70 AT AFT GALLEY AREA MEASURES OF CRACK IS L=0.812. MAINTENANCE REPLACED SHEAR PLATE LOC. STR 23 R BTW FR69 AND FR70 AT AFT GALLEY AREA I.A.W A319 SRM 51-42-11-801 AND DWG D53474180. - [SDR AALA202507301363](https://openairdocs.org/sdr/AALA202507301363.md): Floor Support · corroded · Jun 28, 2025 · N826AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y765 BTW FR64 AND FR65 AT AFT GALLEY AREA MEASURES OF CORROSION ARE L= 1.62 IN, W= 0.621 IN, D= 0.0405 IN. MAINTENANCE REPLACED FLOOR BEAM AND FASTENERS LOC. AT LEVEL FR64 TO FR 66 -Y765 AT AFT GALLEY AREA I - [SDR AALA202507285101](https://openairdocs.org/sdr/AALA202507285101.md): Floor Support · corroded · Jun 28, 2025 · N826AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR SUPPORT -Y765 LOC AT LEVEL FR70 AT AFT GALLEY AREA CORRODED AREA IS L=1.66 IN, W=1.33 IN, D=0.0298 IN MAINTENANCE REPLACED FLOOR SUPPORT -Y765 LOC ON FR66 TO FR70 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801 AND DW - [SDR AALA202507289662](https://openairdocs.org/sdr/AALA202507289662.md): Floor Support · corroded · Jun 28, 2025 · N826AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y160 LOC AT LEVEL FR68 TO FR70 AT AFT GALLEY AREA CORRODED AREA L=1.209 IN W=0.945 IN D=0.029 IN. MAINTENANCE REPLACED FLOOR BEAM -Y160 LOC. FROM FR68 TO FR70 ON AFT GALLEY AREA IAW A319 SRM 51-42-11-801 AND - [SDR AALA202507219632](https://openairdocs.org/sdr/AALA202507219632.md): Floor Support · corroded · Jun 28, 2025 · N826AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y1162.5 BTW FR68 AND FR69 AT AFT GALLEY AREA, MEASURES ARE: L= 1.08 IN, W= 0.972 IN, D= 0.0215 IN. MAINTENANCE REPLACED FLOOR BEAM -Y1162.5 BTW FR68 AND FR69 AT AFT GALLEY AREA IAW A319 SRM 51-72-11-911-00 - [SDR AALA202507210865](https://openairdocs.org/sdr/AALA202507210865.md): Floor Support · corroded · Jun 28, 2025 · N826AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y1292 BTW FR65 AND FR66 AT AFT GALLEY AREA MEASURES ARE: L= 1.141 IN, W= 0.884 IN, D= 0.0245 IN. MAINTENANCE REPLACED FLOOR BEAM -Y1292 BTW FR64 AND FR66 AT AFT GALLEY AREA IAW - [SDR AALA202507141660](https://openairdocs.org/sdr/AALA202507141660.md): Floor Support · corroded · Jun 28, 2025 · N826AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM +Y1292 BTW FR65 AND FR66 AT AFT GALLEY AREA L= 3.43 IN, W= 2.00 IN, D= 0.0230 IN. MAINTENANCE REPLACED FLOOR BEAM Y1292 LOC BTW FR64 AND FR66 AT AFT GALLEY AREA IAW A319 SRM 51-42-11-801 A319 SRM 51-72-11 - [SDR AALA202602093161](https://openairdocs.org/sdr/AALA202602093161.md): Skin · cracked · Jun 26, 2025 · N826AW · Airbus A319132 · Fuselage Main, Plate/Skin > COMPONENT IN SHOP MAINTENANCE: CRACK IN SIDE SHELL AT FR 35, S30R. REPAIRED SIDE SHELL PER EA 366098. - [SDR AALA202508190109](https://openairdocs.org/sdr/AALA202508190109.md): Stringer · corroded · Jun 26, 2025 · N826AW · Airbus A319132 · Fuselage Main, Longeron/Stringer > AIRCRAFT IN BASE MAINTENANCE: CORROSION STRINGER 41R FR63 AFT CARGO COMPARTMENT MEASURE OF CORROSION ARE: L= 9.00 IN, W= 1.47 IN. MAINTENANCE REPLACED STRINGER 41RH LOC BTW FR61 TO FR64 AT CARGO COMPARTMENT IAW A319 SRM 51-42-11-801 AND DWG D53476324 AND DWG - [SDR AALA202508010261](https://openairdocs.org/sdr/AALA202508010261.md): Oxygen Gen · broken · Jun 26, 2025 · N826AW · Airbus A319132 · Passenger Oxygen System > AIRCRAFT IN BASE MAINTENANCE: BROKEN ON EMERGENCY OXYGEN CONTAINER ASSY ROW 9 LH SIDE IN PASSENGER CABIN. MAINTENANCE REPLACED EMERGENCY OXYGEN CONTAINER ASSY ROW 9 LH SIDE IN PASSENGER CABIN IAW AMM 35-21-41-000-001-A AND AMM 35-21-41-400-001-A. - [SDR AALA202508013006](https://openairdocs.org/sdr/AALA202508013006.md): Oxygen Gen · inoperative · Jun 26, 2025 · N826AW · Airbus A319132 · Passenger Oxygen System > AIRCRAFT IN BASE MAINTENANCE: BROKEN ON EMERGENCY OXYGEN CONTAINER ASSY ROW 13 RH SIDE IN PASSENGER CABIN. MAINTENANCE REPLACED EMERGENCY OXYGEN CONTAINER ASSY ROW 13 RH SIDE IN PASSENGER CABIN IAW AMM 35-21-41-000-001-A AND AMM 35-21-41-400-001-A. - [SDR AALA202509035981](https://openairdocs.org/sdr/AALA202509035981.md): Window Frame · cracked · Jun 25, 2025 · N826AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LOWER RADIUS OF THE WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE LH. CRACK L= 0.098 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR OF MIRROR FITTING REPAIR LH LOC ON CENTER WINDSHIELD FRAME - [SDR AALA202509032061](https://openairdocs.org/sdr/AALA202509032061.md): Fitting · cracked · Jun 25, 2025 · N826AW · Airbus A319132 · Fuselage Miscellaneous Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING OF THE WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE RH. CRACK L= 0.157 INCH. MAINTENANCE D5348004121101. - [SDR AALA202509039074](https://openairdocs.org/sdr/AALA202509039074.md): Frame · cracked · Jun 25, 2025 · N826AW · Airbus A319132 · Fuselage Main, Frame > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LOWER RADIUS OF THE WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE RH. CRACK L= 0.197 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR OF MIRROR FITTING REPAIR RH LOC ON CENTER WINDSHIELD FRAME - [SDR AALA202509023860](https://openairdocs.org/sdr/AALA202509023860.md): Fitting · cracked · Jun 25, 2025 · N826AW · Airbus A319132 · Fuselage Main, Structure > AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING OF THE WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE LH. CRACK L= 0.157 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ( REPLACED CONTINUITY FITTING) WINDSHIELD LOWER ATTACHMENT AREA - [SDR AALA202508097995](https://openairdocs.org/sdr/AALA202508097995.md): Light · cracked · Jun 24, 2025 · N826AW · Airbus A319132 · Emergency Lighting > AIRCRAFT IN BASE MAINTENANCE: CRACK ON EMERGENCY EXIT LIGHTS ON UPPER SIDEWALL PANELS NEXT TO EMERGENCY EXIT DOOR 834/844 IN PASSENGER CABIN. MAINTENANCE REPLACED ON EMERGENCY EXIT LIGHTS ON UPPER SIDEWALL PANELS NEXTTO EMERGENCY EXIT DOOR 834/844 IN PASSENG - [SDR AALA202505014069](https://openairdocs.org/sdr/AALA202505014069.md): Lamp · inoperative · Apr 29, 2025 · N826AW · Airbus A319132 · Emergency Lighting > AIRCRAFT WAS NOT GROUNDED: RED EMERGENCY LIGHT ON AFT LEFT LAVATORY INOP. MAINTENANCE REPLACED LAMP FOR RED EMERGENCY LIGHT ON AFT LEFT LAVATORY IAW AMM 33-51-18. - [SDR AALA202410087356](https://openairdocs.org/sdr/AALA202410087356.md): Connector · loose · Oct 3, 2024 · N826AW · Airbus A319132 · Fire Protection System Wiring > AIRCRAFT WAS NOT GROUNDED: APU FIRE EXTINGUISHER DISCHARGE LIGHT COMING ON INTERMITTENTLY IN CRUISE. **SUPPLEMENTAL REPORT FOR AALA202410077356: MAINTENANCE FOUND A LOOSE CONNECTOR AT THE APU FIRE BOTTLE, CLEANED AND RESECURED CONNECTOR. A SATISFACTORY OPERAT - [SDR AALA202410077356](https://openairdocs.org/sdr/AALA202410077356.md): Warning Light · illuminated · Oct 3, 2024 · N826AW · Airbus A319132 · Extinguishing System > AIRCRAFT WAS NOT GROUNDED: APU FIRE EXTINGUISHER DISCHARGE LIGHT COMING ON INTERMITTENTLY IN CRUISE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN) Next page: https://openairdocs.org/aircraft/N826AW/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 = 'N826AW' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N826AW/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.