# N353NW: 1998 Airbus Industrie A320-212

- Status: Valid registration
- Airframe: [Airbus Industrie A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (registry code 3930322, 182 seats)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM) (Airbus SAS) (OpenAirDocs)
- Serial number: 786
- Year built: 1998
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 14, 1998
- Certificate issued: December 31, 2009
- Expires: June 30, 2029
- Mode S code: A3F133
- Registered owner: [Delta Air Lines Inc](https://openairdocs.org/faa-owner/DELTA%20AIR%20LINES%20INC)
- Location: [Atlanta, GA](https://openairdocs.org/faa-place/GA/Atlanta)
- Owner type: Corporation
- Owner's area on the map: 33.6604° N, 84.3865° W: Placed by OpenAirDocs at the center of ZIP code 30354, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=353NW
- Page: https://openairdocs.org/aircraft/N353NW

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every CFM International CFM56 model are included.

## ADs that may apply (OpenAirDocs): 411 in force

### Matched by airframe (Airbus Industrie A320-212)

- [AD 2026-17-04](https://openairdocs.org/ad/2026-17-04): Landing Gear · Airbus A318-111, A318-112, A318-121 and 46 more. Effective Oct 1, 2026
- [AD 2026-17-01](https://openairdocs.org/ad/2026-17-01): Fuselage · Airbus A320-211, A320-212, A320-214 and 12 more. Effective Oct 1, 2026
- [AD 2026-14-04](https://openairdocs.org/ad/2026-14-04): Fuselage · Airbus A319-111, A319-112, A319-113 and 56 more. Effective Aug 14, 2026
- [AD 2026-12-02](https://openairdocs.org/ad/2026-12-02): Fuselage · Airbus A318-111, A318-112, A318-121 and 46 more. Effective Jul 14, 2026
- [AD 2026-10-17](https://openairdocs.org/ad/2026-10-17): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Jul 6, 2026
- [AD 2026-10-15](https://openairdocs.org/ad/2026-10-15): Fuselage · Airbus A318-111, A318-112, A318-122 and 35 more. Effective Jul 6, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2026-09-17](https://openairdocs.org/ad/2026-09-17): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 45 more. Effective Jun 18, 2026
- [AD 2026-09-16](https://openairdocs.org/ad/2026-09-16): Fuselage · Airbus A319-111, A319-112, A319-113 and 33 more. Effective Jun 18, 2026
- [AD 2026-11-04](https://openairdocs.org/ad/2026-11-04): Stabilizers · Airbus A319-111, A319-112, A319-113 and 40 more. Effective Jun 15, 2026
- [AD 2026-09-03](https://openairdocs.org/ad/2026-09-03): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 45 more. Effective Jun 12, 2026
- [AD 2026-03-10](https://openairdocs.org/ad/2026-03-10): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 45 more. Effective Apr 8, 2026
- [AD 2025-23-09](https://openairdocs.org/ad/2025-23-09): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Jan 13, 2026
- [AD 2025-24-51](https://openairdocs.org/ad/2025-24-51): Flight controls · Airbus A319-111, A319-112, A319-113 and 37 more. Effective Jan 6, 2026
- [AD 2025-20-19](https://openairdocs.org/ad/2025-20-19): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Jan 2, 2026
- [AD 2025-20-15](https://openairdocs.org/ad/2025-20-15): Fuselage · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jan 2, 2026
- [AD 2025-19-08](https://openairdocs.org/ad/2025-19-08): Wings · Airbus A319-111, A319-113, A319-112 and 17 more. Effective Dec 30, 2025
- [AD 2025-18-03](https://openairdocs.org/ad/2025-18-03): Oxygen · Airbus A318-111, A318-112, A318-121 and 70 more. Effective Oct 20, 2025
- [AD 2025-16-10](https://openairdocs.org/ad/2025-16-10): Flight controls · Airbus A318-111, A318-112, A318-121 and 44 more. Effective Sep 22, 2025
- [AD 2025-16-04](https://openairdocs.org/ad/2025-16-04): Equipment/furnishings · Airbus A318-111, A318-112, A318-121 and 46 more. Effective Sep 18, 2025
- [AD 2025-17-17](https://openairdocs.org/ad/2025-17-17): Landing Gear · Airbus A318-111, A318-112, A318-121 and 46 more. Effective Sep 17, 2025
- [AD 2025-13-10](https://openairdocs.org/ad/2025-13-10): Wings · Airbus A319-111, A319-112, A319-113 and 36 more. Effective Aug 14, 2025
- [AD 2025-10-07](https://openairdocs.org/ad/2025-10-07): Fuselage · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jun 26, 2025
- [AD 2025-09-05](https://openairdocs.org/ad/2025-09-05): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Jun 5, 2025
- [AD 2025-02-04](https://openairdocs.org/ad/2025-02-04): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Mar 17, 2025
- [AD 2025-01-02](https://openairdocs.org/ad/2025-01-02): Fuselage · Airbus A319-111, A319-112, A319-113 and 20 more. Effective Mar 11, 2025
- [AD 2024-26-05](https://openairdocs.org/ad/2024-26-05): Oxygen · Airbus A300 B4-601, A300 B4-603, A300 B4-620 and 87 more. Effective Mar 11, 2025
- [AD 2024-25-12](https://openairdocs.org/ad/2024-25-12): Landing gear · Airbus A319-111, A319-112, A319-113 and 35 more. Effective Mar 7, 2025
- [AD 2025-03-08](https://openairdocs.org/ad/2025-03-08): Flight Controls · Airbus A318-111, A318-112, A318-121 and 70 more. Effective Feb 26, 2025
- [AD 2024-26-04](https://openairdocs.org/ad/2024-26-04): Pneumatic · Airbus A318-111, A318-112, A318-121 and 44 more. Effective Feb 18, 2025
- [AD 2024-24-10](https://openairdocs.org/ad/2024-24-10): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jan 13, 2025
- [AD 2024-24-09](https://openairdocs.org/ad/2024-24-09): Equipment/Furnishings · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jan 13, 2025
- [AD 2024-19-15](https://openairdocs.org/ad/2024-19-15): Oxygen · Safran Aerosystems Oxygen Cylinder, Valve Assembly, Oxygen Valve and 103 more. Effective Nov 26, 2024
- [AD 2024-12-01](https://openairdocs.org/ad/2024-12-01): Wings · Airbus A318-111, A318-112, A318-121 and 25 more. Effective Aug 13, 2024
- [AD 2024-11-01](https://openairdocs.org/ad/2024-11-01): Electrical Power · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 94 more. Effective Jul 3, 2024
- [AD 2024-08-08](https://openairdocs.org/ad/2024-08-08): Electrical Power · Airbus A300 B4-2C, A300 B4-103, A300 B4-203 and 94 more. Effective Jun 6, 2024
- [AD 2024-04-04](https://openairdocs.org/ad/2024-04-04): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Apr 22, 2024
- [AD 2023-25-12](https://openairdocs.org/ad/2023-25-12): Doors · Airbus A318-112, A319-115, A319-132 and 16 more. Effective Feb 7, 2024
- [AD 2023-23-11](https://openairdocs.org/ad/2023-23-11): Landing gear · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Jan 23, 2024
- [AD 2023-23-08](https://openairdocs.org/ad/2023-23-08): Electric and electronic common installation · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Jan 5, 2024
- [AD 2023-20-12](https://openairdocs.org/ad/2023-20-12): Equipment/Furnishings · Airbus A318-111, A318-112, A318-121 and 38 more. Effective Nov 21, 2023
- [AD 2023-18-02](https://openairdocs.org/ad/2023-18-02): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Oct 24, 2023
- [AD 2023-13-03](https://openairdocs.org/ad/2023-13-03): Doors · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Sep 5, 2023
- [AD 2023-13-01](https://openairdocs.org/ad/2023-13-01): Fuel · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jul 12, 2023
- [AD 2023-09-11](https://openairdocs.org/ad/2023-09-11): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Jul 10, 2023
- [AD 92-02-14 R1](https://openairdocs.org/ad/92-02-14-R1): Equipment/Furnishings · Airbus A320-211, A320-212 and A320-231. Effective Jun 2, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-06-08](https://openairdocs.org/ad/2023-06-08): Fuselage · Airbus A319-111, A319-112, A319-113 and 20 more. Effective May 18, 2023
- [AD 2023-05-14](https://openairdocs.org/ad/2023-05-14): Equipment/furnishings · Airbus A318-111, A318-112, A319-111 and 22 more. Effective May 12, 2023
- [AD 2023-01-01](https://openairdocs.org/ad/2023-01-01): Landing gear · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Mar 8, 2023

### Matched by engine (CFM International CFM56 series)

- [AD 2023-05-05](https://openairdocs.org/ad/2023-05-05): Turbine Engine Compressor Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 98 more. Effective May 10, 2023
- [AD 2022-02-03](https://openairdocs.org/ad/2022-02-03): Turbine Engine Accessory Drive · CFM International CFM56-3, CFM56-3B, CFM56-3C and 34 more. Effective Mar 22, 2022
- [AD 2021-16-08](https://openairdocs.org/ad/2021-16-08): Turbine Section · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 55 more. Effective Sep 28, 2021
- [AD 2018-26-01](https://openairdocs.org/ad/2018-26-01): Turbine Engine Compressor Section · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jan 10, 2019
- [AD 2018-09-51](https://openairdocs.org/ad/2018-09-51): Engine · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Jun 7, 2018
- [AD 2017-14-08](https://openairdocs.org/ad/2017-14-08): Turbine Engine Compressor Section · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Aug 18, 2017
- [AD 2017-05-09](https://openairdocs.org/ad/2017-05-09): Accessory Gearboxes · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Apr 13, 2017
- [AD 2016-14-10](https://openairdocs.org/ad/2016-14-10): High-pressure turbine (HPT) disks · CFM International CFM56-3, CFM56-3B and CFM56-3C with STC SE00034EN. Effective Aug 9, 2016
- [AD 2016-02-04](https://openairdocs.org/ad/2016-02-04): Turbine rear frames (TRFs) · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/3 and 33 more. Effective Mar 1, 2016
- [AD 2015-18-04](https://openairdocs.org/ad/2015-18-04): 73-tooth gearshaft located in the engine accessory gearbox (AGB) · CFM International CFM56-3, CFM56-7B20, CFM56-7B20/2 and 47 more. Effective Oct 20, 2015
- [AD 2015-04-02](https://openairdocs.org/ad/2015-04-02): Dual engine thrust instability event · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 46 more. Effective Mar 31, 2015
- [AD 2013-14-06](https://openairdocs.org/ad/2013-14-06): Hydro-mechanical unit (HMU) fuel control · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Sep 3, 2013
- [AD 2012-02-03](https://openairdocs.org/ad/2012-02-03): Engine · CFM International CFM56-5B1/3, CFM56-5B2/3, CFM56-5B3/3 and 8 more. Effective Mar 15, 2012
- [AD 2010-13-09](https://openairdocs.org/ad/2010-13-09): Stage 3 low-pressure turbine (LPT) · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 88 more. Effective Jul 26, 2010
- [AD 2010-12-03](https://openairdocs.org/ad/2010-12-03): Fan blades · CFM International CFM56-3 and CFM56-3B. Effective Jul 13, 2010
- [AD 2010-09-14](https://openairdocs.org/ad/2010-09-14): Exhaust gas temperature (EGT) · CFM International CFM56-5B1/2P, CFM56-5B1/P, CFM56-5B2/2P and 16 more. Effective Jun 8, 2010
- [AD 2010-01-05](https://openairdocs.org/ad/2010-01-05): LP turbine rear frames · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B20/3 and 25 more. Effective Feb 18, 2010
- [AD 2009-18-01](https://openairdocs.org/ad/2009-18-01): LP turbine rear frames · CFM International CFM56-5B1/3, CFM56-5B1/P, CFM56-5B2/3 and 19 more. Effective Oct 1, 2009
- [AD 2009-11-02](https://openairdocs.org/ad/2009-11-02): HPC 4-9 spools · CFM International CFM56-2, CFM56-2A, CFM56-2B and 109 more. Effective Jun 23, 2009
- [AD 2008-03-09](https://openairdocs.org/ad/2008-03-09): Low pressure turbine rear frames (TRFs) · CFM International CFM56-7B18, CFM56-7B20, CFM56-7B22 and 10 more. Effective Mar 10, 2008
- [AD 2007-24-04](https://openairdocs.org/ad/2007-24-04): Low pressure turbine (LPT) · CFM International CFM56-5C4/1. Effective Dec 6, 2007
- [AD 2007-03-15](https://openairdocs.org/ad/2007-03-15): Exhaust gas temperature (EGT) harness · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 34 more. Effective Mar 19, 2007
- [AD 2006-26-01](https://openairdocs.org/ad/2006-26-01): Fuel filters · CFM International CFM56-2, CFM56-2A, CFM56-2B and 93 more. Effective Jan 3, 2007
- [AD 2005-10-05](https://openairdocs.org/ad/2005-10-05): Air turbine starters · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 50 more. Effective Jun 14, 2005
- [AD 97-09-02 R3](https://openairdocs.org/ad/97-09-02-R3): High pressure turbine rotor (HPTR) front shafts · CFM International CFM56-5C2, CFM56-5C3/G and CFM56-5C4. Effective Oct 14, 2004
- [AD 2004-10-13](https://openairdocs.org/ad/2004-10-13): Service main fuel pumps · CFM International CFM56-3, CFM56-5, CFM56-5-A1/F and 4 more. Effective Jun 24, 2004
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2002-16-18](https://openairdocs.org/ad/2002-16-18): Low pressure turbine (LPT) nozzle segments · CFM International CFM56-5B1, CFM56-5B1/2P, CFM56-5B1/P and 33 more. Effective Sep 18, 2002
- [AD 2002-13-03](https://openairdocs.org/ad/2002-13-03): Turbofan Engines · CFM International CFM56-2, CFM56-2A, CFM56-2B and 55 more. Effective Aug 1, 2002
- [AD 2002-02-13](https://openairdocs.org/ad/2002-02-13): Magnetic Drain Plug · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 33 more. Effective Mar 21, 2002
- [AD 2001-11-05](https://openairdocs.org/ad/2001-11-05): No. 4 Bearings · CFM International CFM56-2, CFM56-2B, CFM56-3 and 45 more. Effective Jun 11, 2001
- [AD 2001-09-17](https://openairdocs.org/ad/2001-09-17): Fuel Manifold and CJ9L Harness · CFM International CFM56-5C2, CFM56-5C2/4, CFM56-5C2/F and 13 more. Effective May 14, 2001
- [AD 2001-04-06](https://openairdocs.org/ad/2001-04-06): Fan Disk · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Apr 4, 2001
- [AD 2001-02-12](https://openairdocs.org/ad/2001-02-12): On-Wing Torque Inspection · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 11 more. Effective Feb 14, 2001
- [AD 2000-15-01](https://openairdocs.org/ad/2000-15-01): Fuel Leakage · CFM International CFM56-2, CFM56-2A, CFM56-2B and 39 more. Effective Oct 2, 2000
- [AD 2000-05-22](https://openairdocs.org/ad/2000-05-22): CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective May 2, 2000
- [AD 99-06-16](https://openairdocs.org/ad/99-06-16): High Pressure Turbine Rotor (HPTR) Front Air Seal · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Apr 21, 1999
- [AD 98-21-23](https://openairdocs.org/ad/98-21-23): Electronic Engine Control · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Nov 2, 1998
- [AD 98-19-20](https://openairdocs.org/ad/98-19-20): Hydromechanical Unit · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 7 more. Effective Oct 7, 1998
- [AD 98-14-51](https://openairdocs.org/ad/98-14-51): Accessory Gearbox · CFM International CFM56-7B20, CFM56-7B20/2, CFM56-7B22 and 10 more. Effective Oct 1, 1998
- [AD 98-19-10](https://openairdocs.org/ad/98-19-10): Accessory Gearbox · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Sep 28, 1998
- [AD 98-12-32](https://openairdocs.org/ad/98-12-32): High Pressure Turbine Rotor Disks · CFM International CFM56-2, CFM56-2A, CFM56-2B and 3 more. Effective Jul 20, 1998
- [AD 98-10-11](https://openairdocs.org/ad/98-10-11): Accessory Gearbox · CFM International CFM56-3, CFM56-3B, CFM56-3C and 31 more. Effective Jun 3, 1998
- [AD 98-07-02](https://openairdocs.org/ad/98-07-02): Air/oil Seal · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Mar 30, 1998
- [AD 98-02-04](https://openairdocs.org/ad/98-02-04): Low Pressure Turbine Case · CFM International CFM56-5B1/2P, CFM56-5B2/2P, CFM56-5B3/2P and 1 more. Effective Mar 23, 1998
- [AD 89-23-06 R1](https://openairdocs.org/ad/89-23-06-R1): Magnetic Chip Detector · CFM International CFM56-2, CFM56-2A, CFM56-3 and 8 more. Effective Jan 28, 1998
- [AD 97-08-01](https://openairdocs.org/ad/97-08-01): Fan Disks · CFM International CFM56-3, CFM56-3B and CFM56-3C. Effective Jun 23, 1997
- [AD 97-06-01](https://openairdocs.org/ad/97-06-01): High Pressure Compressor Rotor (HPCR) Stage 1-2 Spool · CFM International CFM56-5, CFM56-5B1, CFM56-5B1/2P and 28 more. Effective Jun 3, 1997
- [AD 97-05-13](https://openairdocs.org/ad/97-05-13): Air Turbine Engine Starter · CFM International CFM56-5, CFM56-5-A1/F, CFM56-5A4 and 3 more. Effective Jun 3, 1997
- [AD 96-25-11](https://openairdocs.org/ad/96-25-11): Redesigned Fan Blades · CFM International CFM56-3B and CFM56-3C. Effective Jan 29, 1997

### Historical (superseded or no longer in force)

- [AD 2025-17-07](https://openairdocs.org/ad/2025-17-07) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 44 more. Effective Oct 1, 2025
- [AD 2025-10-12](https://openairdocs.org/ad/2025-10-12) (historical): Fuselage · Airbus A319-111, A319-112, A319-113 and 55 more. Effective Jul 2, 2025
- [AD 2025-03-07](https://openairdocs.org/ad/2025-03-07) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Mar 21, 2025
- [AD 2025-03-06](https://openairdocs.org/ad/2025-03-06) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Mar 21, 2025
- [AD 2024-25-06](https://openairdocs.org/ad/2024-25-06) (historical): Landing Gear · Airbus A318-111, A318-112, A318-121 and 44 more. Effective Dec 30, 2024
- [AD 2024-19-13](https://openairdocs.org/ad/2024-19-13) (historical): Time Limits/Maintenance Checks · Airbus A320-211, A320-212, A320-214 and 43 more. Effective Nov 26, 2024
- [AD 2024-04-07](https://openairdocs.org/ad/2024-04-07) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Apr 22, 2024
- [AD 2024-04-03](https://openairdocs.org/ad/2024-04-03) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Apr 19, 2024
- [AD 2023-25-09](https://openairdocs.org/ad/2023-25-09) (historical): Oxygen · Airbus A318-111, A318-112, A318-121 and 69 more. Effective Feb 7, 2024
- [AD 2023-13-11](https://openairdocs.org/ad/2023-13-11) (historical): Oxygen · AVOX Systems Oxygen valve assemblies (body and gage assemblies), Oxygen cylinder and valve assemblies, A300 B2-1A and 102 more. Effective Sep 5, 2023
- [AD 2023-13-10](https://openairdocs.org/ad/2023-13-10) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Sep 5, 2023
- [AD 2023-09-01](https://openairdocs.org/ad/2023-09-01) (historical): Pneumatic · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jun 26, 2023
- [AD 2023-05-02](https://openairdocs.org/ad/2023-05-02) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Apr 18, 2023
- [AD 2023-04-06](https://openairdocs.org/ad/2023-04-06) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Apr 10, 2023
- [AD 2022-24-05](https://openairdocs.org/ad/2022-24-05) (historical): Equipment/Furnishings · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Jan 9, 2023
- [AD 2022-22-10](https://openairdocs.org/ad/2022-22-10) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Dec 30, 2022
- [AD 2022-18-09](https://openairdocs.org/ad/2022-18-09) (historical): Equipment/Furnishings · Airbus A319-111, A319-112, A319-113 and 24 more. Effective Oct 20, 2022
- [AD 2022-15-05](https://openairdocs.org/ad/2022-15-05) (historical): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Aug 31, 2022
- [AD 2022-14-10](https://openairdocs.org/ad/2022-14-10) (historical): Wings · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Aug 19, 2022
- [AD 2022-09-16](https://openairdocs.org/ad/2022-09-16) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Jun 30, 2022
- [AD 2022-08-08](https://openairdocs.org/ad/2022-08-08) (historical): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective May 26, 2022
- [AD 2022-07-08](https://openairdocs.org/ad/2022-07-08) (historical): Time Limits/Maintenance Checks, Flight Controls · Airbus A318-111, A318-112, A318-121 and 43 more. Effective May 19, 2022
- [AD 2022-07-15](https://openairdocs.org/ad/2022-07-15) (historical): Landing gear · Airbus A318-111, A318-112, A318-121 and 43 more. Effective May 2, 2022
- [AD 2022-06-02](https://openairdocs.org/ad/2022-06-02) (historical): Equipment/furnishings · Airbus A318-111, A318-112, A319-111 and 22 more. Effective Apr 26, 2022
- [AD 2022-04-09](https://openairdocs.org/ad/2022-04-09) (historical): Oxygen System · Airbus A300 B2-1A, A300 B2-1C, A300 B2K-3C and 94 more. Effective Apr 4, 2022
- [AD 2022-04-03](https://openairdocs.org/ad/2022-04-03) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Mar 30, 2022
- [AD 2022-02-11](https://openairdocs.org/ad/2022-02-11) (historical): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Mar 15, 2022
- [AD 2021-23-15](https://openairdocs.org/ad/2021-23-15) (historical): Equipment/Furnishings · Airbus A319-111, A319-112, A319-113 and 20 more. Effective Jan 10, 2022
- [AD 2021-25-14](https://openairdocs.org/ad/2021-25-14) (historical): Wings · Airbus A319-111, A319-112, A319-113 and 20 more. Effective Jan 5, 2022
- [AD 2021-22-04](https://openairdocs.org/ad/2021-22-04) (historical): Wings · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Dec 27, 2021
- [AD 2021-20-08](https://openairdocs.org/ad/2021-20-08) (historical): Electrical Power · Airbus A318-111, A318-112, A318-121 and 72 more. Effective Nov 18, 2021
- [AD 2021-16-01](https://openairdocs.org/ad/2021-16-01) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Sep 28, 2021
- [AD 2020-26-01](https://openairdocs.org/ad/2020-26-01) (historical): Landing gear · Airbus A318-111, A318-112, A318-121 and 16 more. Effective Jan 4, 2021
- [AD 2020-25-03](https://openairdocs.org/ad/2020-25-03) (historical): Equipment/furnishings · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Dec 28, 2020
- [AD 2020-22-16](https://openairdocs.org/ad/2020-22-16) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Dec 10, 2020
- [AD 2020-21-11](https://openairdocs.org/ad/2020-21-11) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Nov 20, 2020
- [AD 2020-21-10](https://openairdocs.org/ad/2020-21-10) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Nov 19, 2020
- [AD 2020-20-05](https://openairdocs.org/ad/2020-20-05) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 42 more. Effective Nov 19, 2020
- [AD 2020-16-01](https://openairdocs.org/ad/2020-16-01) (historical): Fire protection · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Aug 19, 2020
- [AD 2020-06-10](https://openairdocs.org/ad/2020-06-10) (historical): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective May 4, 2020
- [AD 2020-06-18](https://openairdocs.org/ad/2020-06-18) (historical): Flight controls · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Apr 2, 2020
- [AD 2020-01-17](https://openairdocs.org/ad/2020-01-17) (historical): Equipment/ furnishings · Airbus A318-111, A318-112, A318-121 and 43 more. Effective Feb 14, 2020
- [AD 2019-24-13](https://openairdocs.org/ad/2019-24-13) (historical): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Feb 3, 2020
- [AD 2019-23-01](https://openairdocs.org/ad/2019-23-01) (historical): Time Limits/ Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 37 more. Effective Jan 9, 2020
- [AD 2019-20-10](https://openairdocs.org/ad/2019-20-10) (historical): Fuselage · Airbus A318-111, A318-112, A318-121 and 24 more. Effective Dec 18, 2019
- [AD 2019-20-03](https://openairdocs.org/ad/2019-20-03) (historical): Information systems · Airbus A340-312, A340-313, A318-111 and 48 more. Effective Nov 19, 2019
- [AD 2019-19-15](https://openairdocs.org/ad/2019-19-15) (historical): Time Limits/ Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 36 more. Effective Nov 14, 2019
- [AD 2019-18-07](https://openairdocs.org/ad/2019-18-07) (historical): Fuselage · Airbus A319-111, A319-112, A319-113 and 20 more. Effective Oct 31, 2019
- [AD 2019-14-04](https://openairdocs.org/ad/2019-14-04) (historical): Time Limits/Maintenance Checks · Airbus A318-111, A318-112, A318-121 and 37 more. Effective Aug 29, 2019
- [AD 2019-12-07](https://openairdocs.org/ad/2019-12-07) (historical): Landing gear · Airbus A318-111, A318-112, A318-121 and 25 more. Effective Aug 1, 2019

All 588: https://openairdocs.org/aircraft/N353NW/ads.md

## Information bulletins (advisory) (10 in force)

- [SAIB NE-19-03](https://openairdocs.org/saib/NE-19-03): Escape Slide Maintenance Tasks and Intervals - JASC 2565. Issued Feb 19, 2019
- [SAIB NM-15-02](https://openairdocs.org/saib/NM-15-02): Cabin Equipment/Furnishings. Issued Nov 6, 2014
- [SAIB NM-14-21](https://openairdocs.org/saib/NM-14-21): Communications: Honeywell RTA 44D VHF Transceivers. Issued Jun 3, 2014
- [SAIB NM-13-24](https://openairdocs.org/saib/NM-13-24): Air Conditioning System: Air Distribution Fan. Issued Mar 21, 2013
- [SAIB NM-13-03](https://openairdocs.org/saib/NM-13-03): Hydraulic Power System: Power Transfer Unit. Issued Oct 23, 2012
- [SAIB NM-06-57](https://openairdocs.org/saib/NM-06-57): Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.. Issued Jul 27, 2006
- [SAIB NE-08-17R3](https://openairdocs.org/saib/NE-08-17R3): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued May 28, 2014
- [SAIB NE-13-33R2](https://openairdocs.org/saib/NE-13-33R2): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jan 28, 2014
- [SAIB NE-12-29](https://openairdocs.org/saib/NE-12-29): Engine Fuel Distribution  CFM56-5B LPTACC Fuel Manifold. Issued Apr 27, 2012
- [SAIB NE-06-02](https://openairdocs.org/saib/NE-06-02): . Issued Oct 18, 2005
- [SAIB NE-13-33R1](https://openairdocs.org/saib/NE-13-33R1) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued Jun 24, 2013
- [SAIB NE-13-33](https://openairdocs.org/saib/NE-13-33) (historical): Turbine Engine Air Inlet Section - LP Turbine, Stage 1 Nozzle Vanes. Issued May 13, 2013
- [SAIB NE-08-17R2](https://openairdocs.org/saib/NE-08-17R2) (historical): Turbine Section - Propulsion Technology LLC Unapproved Repair. Issued Mar 7, 2011
- [SAIB NE-08-17R1](https://openairdocs.org/saib/NE-08-17R1) (historical): Propulsion Technology LLC Unapproved Repair. Issued May 22, 2008
- [SAIB NE-08-17](https://openairdocs.org/saib/NE-08-17) (historical): Propulsion Technologies International Unapproved Repair. Issued May 14, 2008

## NTSB investigations

None matched to N353NW.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20020911024109I](https://openairdocs.org/incident/20020911024109I), Sep 11, 2002: Airbus A320212 (N353NW), Fort Smith, AR. (-23) On September 11, 2002, [privacy data omitted] was a passenger on northwest flight 979 from memphis, Tennessee, to las vegas, Nevada. The passenger,…

## Service difficulty reports (183, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DALA2026092705364](https://openairdocs.org/sdr/DALA2026092705364), Sep 26, 2026: COMPUTER. MALFUNCTIONED. DURING DECENT FOR APPROACH, WITH SPEED BRAKES DEPLOYED. AIRCRAFT MADE AN UNCOMMANDED RIGHT ROLL WITH NOTICEABLE BANK. T/S IAW TSM 27-10-00-810-842A, PERFORMED O
- [SDR DALA2026092105249](https://openairdocs.org/sdr/DALA2026092105249), Sep 20, 2026: DOOR SILL. CORRODED. PAX CABIN, PASSENGER DOOR CUTOUT, LOWER SILL BEAM I/B FLANGE WITH CORROSION LOC. AT FR67+450MM. REPLACED LOWER SILL BEAM P/N: 5348004320601, LOCATED AT PAX CABI
- [SDR DALA2026092105246](https://openairdocs.org/sdr/DALA2026092105246), Sep 17, 2026: DOOR SILL. CORRODED. PAX CABIN, CREW DOOR CUTOUT, LOWER SILL BEAM I/B FLANGE WITH CORROSION LOC. AT FR67+450MM. C/A: PERFORMED REPAIR AT PASSENGER CABIN, CREW DOOR CUTOUT LOWER SILL
- [SDR DALA2026092105245](https://openairdocs.org/sdr/DALA2026092105245), Sep 17, 2026: BEAM. CORRODED. PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR67+430MM Y1292. REPLACED LONGITUDINAL BEAM P/N: D5347218820400 AT Y1292 BTW FR68 TO FR69 I/A/
- [SDR DALA2026091705192](https://openairdocs.org/sdr/DALA2026091705192), Sep 16, 2026: FLOOR SUPPORT. CORRODED. LEVEL 2 CORROSION, PASSENGER CABIN LONGITUDINAL BEAM -Y1292, FR68 (COUPLING AREA), UPPER I/B AND AT FR66 UPPER AND LOWER I/B COUPLING ANGLES WITH ELONGATED HOLE
- [SDR DALA2026091705191](https://openairdocs.org/sdr/DALA2026091705191), Sep 16, 2026: FLOOR SUPPORT. CORRODED. LEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC.BTW FR66+220MM TO FR68-Y1292. REPLACED LONGITUDINAL FLOOR SUPPORT D5347218920200
- [SDR DALA2026091705190](https://openairdocs.org/sdr/DALA2026091705190), Sep 16, 2026: SKIN. DENTED. NOSE FWD EXTERNAL FUSELAGE, AT FR11 BETWEEN -Z 88 AND -Z 263, L/ H SIDE, SKIN WITH DENTS. C/A: PERFORMED REPAIR AT FWD EXTERNAL FUSELAGE SKIN SECTION AT FR11 BE
- [SDR DALA2026091705189](https://openairdocs.org/sdr/DALA2026091705189), Sep 16, 2026: SKIN. SCRATCHED. NOSE FWD EXTERNAL FUSELAGE, AT FR10 -Z361 L/H SIDE, SKIN WITH SCRATCH. PERFORMED REPAIR AT FWD EXTERNAL FUSELAGE SKIN SECTION AT FR 10 -Z361 LH SIDE AS PER DELT
- [SDR DALA2026091705188](https://openairdocs.org/sdr/DALA2026091705188), Sep 16, 2026: COUPLING. CORRODED. LEVEL 2 CORROSION, PAX CABIN LONGITUDINAL BEAM AT FR68 Y1292 COUPLING AREA, I/B UPPER COUPLING ANGLE WITH CORROSION. FOUND DURING PROCESS WITH ORNRC 200-337. RE
- [SDR DALA2026091505146](https://openairdocs.org/sdr/DALA2026091505146), Sep 14, 2026: SEAT TRACK. CORRODED. PAX CABIN, LONGITUDINAL BEAM WITH CORROSION AT SEAT TRACK CROWN AREA LOC. BTW FR65 TO FR 66 -Y765. REPLACED SEAT TRACK BEAM P/N 14N00031-103 AT Y-765 BETWEEN FR
- [SDR DALA2026091505145](https://openairdocs.org/sdr/DALA2026091505145), Sep 14, 2026: BEAM. CORRODED. LEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR66 Y765. C/A: REPLACED SEAT TRACK BEAM P/N 14N00031-103 AT Y 765 BETWEEN F
- [SDR DALA2026091505144](https://openairdocs.org/sdr/DALA2026091505144), Sep 14, 2026: BEAM. CORRODED. LEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR66+70MM Y1292. C/A: REPLACED SEAT TRACK BEAM P/N 14N00031-101 AT Y1292 BET
- [SDR DALA2026091305112](https://openairdocs.org/sdr/DALA2026091305112), Sep 12, 2026: SKIN. CORRODED. LEVEL 2 CORROSION, LOWER FUSELAGE AFT CARGO COMPARTMENT FROM FR56 TO FR 57 BETWEEN STRG-42L AND STRG-43L AFT ATG4 ANTENNA INTERNAL DOUBLER WITH CORROSION. PERFO
- [SDR DALA2026091305111](https://openairdocs.org/sdr/DALA2026091305111), Sep 12, 2026: SHEAR PLATE. CORRODED. LEVEL 2 CORROSION, PAX CABIN, LATERAL SHEAR PLATE WITH CORROSION LOC.BTW FR 69 TO FR 70 STR 23L. REPLACED SHEAR PLATE AT PAX CABIN BETWEEN FR 69 TO FR 70 STG 23
- [SDR DALA2026091705193](https://openairdocs.org/sdr/DALA2026091705193), Sep 11, 2026: SKIN. DAMAGED. DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR FUSELAGE SKIN R EPAIR AT FR11LH, -Z88 & -Z263 PER ER/A 636719-14. C/A: SECTION I IS LIMITED TO SOONER OF 60000F
- [SDR DALA2026091305108](https://openairdocs.org/sdr/DALA2026091305108), Sep 11, 2026: SHEAR PLATE. CORRODED. LEVEL 2 CORROSION, PAX CABIN, LATERAL SHEAR PLATE WITH CORROSION LOC. BTW FR69 TO FR70 STGR 23R. REPLACED SHEAR PLATE P/N: D5347112420300 LOCATED BTW FR69 TO FR
- [SDR DALA2026091305105](https://openairdocs.org/sdr/DALA2026091305105), Sep 10, 2026: SKIN. DAMAGED. ER/A 636728-14 IS ISSUED FOR FUSELAGE SKIN REPAIR INSTALLED AT F R56/57, S42/43LH WHICH WAS INSTALLED PER SRM 53-00-11-300-013. F OLLOW ON ACTION IS REQUIRED. S
- [SDR DALA2026091305107](https://openairdocs.org/sdr/DALA2026091305107), Sep 9, 2026: ANCHOR FITTING. CORRODED. LEVEL 2 CORROSION, LOWER FUSELAGE, RT MLG ANCHORAGE FITTING WITH CORROSION. REPAIRED RH MLG RETRACTION JACK ANCHORAGE FITTING LUG BARE, UPPER AND LOWER BEARING 
- [SDR DALA2026091305106](https://openairdocs.org/sdr/DALA2026091305106), Sep 9, 2026: ANCHOR FITTING. CORRODED. LEVEL 2 CORROSION, LOWER FUSELAGE, LH MLG ANCHORAGE FITTING WITH CORROSION. C/A: REPAIRED LH MLG RETRACTIION JACK ANCHORAGE FITTING LUG BARE UPPER AND LOWER BEA
- [SDR DALA2026091005067](https://openairdocs.org/sdr/DALA2026091005067), Sep 9, 2026: SKIN. DAMAGED. UPPER FUSELAGE FROM FR 29 TO FR 30 BETWEEN STRG 1L TO STGR 1R PCS/TIMING ANTENNA AREA BELOW COVER PLATE WITH SCRATCHES. PERFORMED PERMANENT MAJOR REPAIR AT FWD 
- [SDR DALA2026091005066](https://openairdocs.org/sdr/DALA2026091005066), Sep 9, 2026: BEAM. CORRODED. LEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR 68 Y765. REPLACED LONGITUDINAL P/N D5347219220000 AT Y 765 BTW FR66 TO FR
- [SDR DALA2026091005065](https://openairdocs.org/sdr/DALA2026091005065), Sep 8, 2026: SKIN. DAMAGED. ER/A 636530-14 ISSUED FOR SKIN REPAIR INSTALLED BETWEEN FR29 & F R30, S1 LH & RH. PERFORM SECTION II THE SOONER OF 30600FC/61200FH AFTER SECTION I AND EVERY SOO
- [SDR DALA2026090705012](https://openairdocs.org/sdr/DALA2026090705012), Sep 4, 2026: SEAT TRACK. CORRODED. LEVEL 2 CORROSION, PASSENGER CABIN BETWEEN FR 16 - 20, Y-1292 SEAT TRACK CORRODED. REPLACED THE SEAT TRACK BTWN FR 12 - 24 IAW SRM 53-11-15- 01A, FIG 001, ITEM 
- [SDR DALA2026090705011](https://openairdocs.org/sdr/DALA2026090705011), Sep 4, 2026: LIGHT. CORRODED. LEVEL 2 CORROSION, UPPER FUSELAGE, PASSENGER CABIN ON FR16 AT Y254 SEAT TRACK CORRODED. REPLACED THE SEAT TRACK BTWN FR 12 TO FR 24, AT Y:254 IAW SRM 53-11-14-0
- [SDR DALA2026090705009](https://openairdocs.org/sdr/DALA2026090705009), Sep 2, 2026: SEAT TRACK. CORRODED. LEVEL 2 CORROSION, UPPER FUSELAGE, PASSENGER CABIN, FR 20 AT Y 765 SEAT TRACK CORRODED. REPLACED THE SEAT TRACK, FR 12 & FR 24 IAW SRM 53-11-15-01A, FIGURE 001,
- [SDR DALA2026090705008](https://openairdocs.org/sdr/DALA2026090705008), Sep 2, 2026: SEAT TRACK. CORRODED. LEVEL 2 CORROSION, UPPER FUSELAGE, PASSENGER CABIN ON FR 20 AT Y-765 SEAT TRACK WITH CORROSION. REPLACED PASSENGER CABIN SEAT TRACK AT Y-765 BETWEEN FR12 AND FR
- [SDR DALA2026072804386](https://openairdocs.org/sdr/DALA2026072804386), Jul 23, 2026: O-RING. CRACKED. ON CLIMB OUT THROUGH HIGH 20'S GOT A HYD Y RSVR LO LVL ECAM. SYSTEM PAGE SHOWED Y HYD QUANTITY DECREASING. FOUND O-RING / PACKING ON SOLENOID / PRIORITY VALVE C
- [SDR DALA2026031701841](https://openairdocs.org/sdr/DALA2026031701841), Mar 14, 2026: SLAT. DAMAGED. PILOTS REPORTED FOUND DAMAGE ON RT #1 SLAT & FUSELAGE FROM FUELER STAIRS CONTACT. REPAIR DAMAGE ON RT #1 SLAT PER A320 SRM 57-40-00-283-002 PARA. 2.A(2). NO FUR
- [SDR DALA2026012800694](https://openairdocs.org/sdr/DALA2026012800694), Jan 24, 2026: REPAIR. NONE. EXISTING REPAIR DOUBLER ON AREA FR68 RT AT LEVEL DOOR STOP 1, S22R. REFERENCE WORK CARD 5311-01244-02B AND SB A320-53-1491. COMPLIED WITH ER/A 616797-14AD REV B
- [SDR DALA2026012800693](https://openairdocs.org/sdr/DALA2026012800693), Jan 22, 2026: FRAME. DAMAGED. INSPECTION ERA 616797-14 REV. B. REPAIR AT FR68 & STR22R, FRAME WEB HORIZONTAL FLANGE REQUIRES FOLLOW ON INSPECTIONS PRIOR TO 54,670 TFC AND EVERY 16,200 FC THE
- [SDR DALA2025100807318](https://openairdocs.org/sdr/DALA2025100807318), Oct 7, 2025: MICROPHONE. INOPERATIVE. FO'S O2 MASK MICROPHONE NOT WORKING. RESET MASK, OPS CKS NORMAL. (LP: 7376134)
- [SDR DALA2025100707311](https://openairdocs.org/sdr/DALA2025100707311), Oct 1, 2025: MICROPHONE. INOPERATIVE. F.O O2 MASK MICROPHONE NOT TESTING. C/A: REPACKED O2 MASK OPS CKD PER A320 AMM35-13 CKD NORMAL. (LP: 7276102)
- [SDR DALA2025090106464](https://openairdocs.org/sdr/DALA2025090106464), Sep 1, 2025: ECS. CONTAMINATED. AFTER START OF BOTH ENGINES FA NOTIFIED CREW OF BURNT RUBBER SMELL IN BACK OF CABIN THRU CENTER OF CABIN. SECURED BOTH PACKS AND COMPLIED WITH EQRH. SMELL DISCI
- [SDR DALA2025071805419](https://openairdocs.org/sdr/DALA2025071805419), Jul 17, 2025: HYDRAULIC LINE. BROKEN. SHIP 3253 - ATB - DUE TO LOSS OF THE GREEN HYDRAULIC SYSTEM SHORTLY AFTER TAKE-OFF. FOUND BROKEN HYDRAULIC LINE AT RH MLG LOCKSTAY ACTUATOR SWIVEL FITTING. MAIN
- [SDR DALA2025011000206](https://openairdocs.org/sdr/DALA2025011000206), Dec 30, 2024: CABLE. BROKEN. SHIP 3253 DISC: DURING SERVICE, MANUAL RELEASE HANDLE CABLE BROKE ON RIGHT SIDE. C/A: FWD RT MLG DOOR GROUND OPEN CABLE TO MEL 32-12-01 CAT C PLACARDS INSTALLED
- [SDR DALA2024101310017](https://openairdocs.org/sdr/DALA2024101310017), Oct 8, 2024: FLANGE. NONE. SHIP 3253 DISC: WEB HORIZONTAL FLANGE / CRACK. ER/A 616797-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. C/A: ER/A 
- [SDR DALA2024101310016](https://openairdocs.org/sdr/DALA2024101310016), Oct 8, 2024: FRAME. CRACKED. SHIP 3253 DISC: DTE, ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL. A320 / 3253 / FUSELAGE / FRAMES/FORMERS / FR68 & STR22R / FRAME WEB HORIZONTAL FLANGE
- [SDR DALA2024101310015](https://openairdocs.org/sdr/DALA2024101310015), Oct 8, 2024: FRAME. CRACKED. SHIP 3253 DISC: DTE, ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL. A320 / 3253 / FUSELAGE / FRAMES/FORMERS / FR68 & STR22R / FRAME WEB HORIZONTAL FLANGE
- [SDR DALA2024101310014](https://openairdocs.org/sdr/DALA2024101310014), Oct 8, 2024: FRAME. CRACKED. SHIP 3253 DISC: DTE, ER/A 616797-14AD REV A REQUIRES STAGE 3 DTA APPROVAL. A320 / 3253 / FUSELAGE / FRAMES/FORMERS / FR68 & STR22R / FRAME WEB HORIZONTAL FLANGE
- [SDR DALA2024091508991](https://openairdocs.org/sdr/DALA2024091508991), Sep 12, 2024: LIFE RAFT. OUT OF POSITION. SHIP 3253 DISC: DURING 1A AIRFRAME CHECK FOUND LIFE RAFT AT OVERHEAD BIN 32ABC UNABLE TO SEE PRESSURE GAUGE. C/A: REMOVED AND REPLACED LIFE RAFT ASSEMBLY REF A3
- [SDR DALA2024071307097](https://openairdocs.org/sdr/DALA2024071307097), Jul 5, 2024: LENS. DAMAGED. SHIP 3253 DISC: PATH WAY LIGHT LENS DAMAGED AT 1C AND 4C. C/A: REPLACED LIGHT LENS PER CMM 25-20-148. (LP: 0430284)
- [SDR DALA2024071207054](https://openairdocs.org/sdr/DALA2024071207054), Jul 5, 2024: LAMP. INOPERATIVE. SHIP 3253 DISC: 16F EMERGENCY EXIT HANDLE LIGHT INOP. C/A: RELAMPED EMERGENCY EXIT HANDLE LIGHT REF A320 AMM 33-51-11-000- 001-A. OPS CK GOOD. (LP: 6204543)
- [SDR DALA2024071207055](https://openairdocs.org/sdr/DALA2024071207055), Jul 4, 2024: LIGHT. INOPERATIVE. SHIP 3253 DISC: 13D EMERGENCY LIGHT INOP. C/A: REPLACED LIGHT ASSEMBLY OPS CK GOOD REMOVED PLACARDS, CLEARED MEL. OK FOR SVC. (LP: 6204542)
- [SDR DALA2024061406074](https://openairdocs.org/sdr/DALA2024061406074), Jun 13, 2024: LINE. CHAFED. SHIP 3253 - MISC/DE - DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM (HYD Y RSVR LO LVL ECAM). CORRECTIVE ACTION: FOUND #2 ENGINE T/R LOCK ACTUATOR LINE DAMAGED (CHAFFE
- [SDR DALA2024041904582](https://openairdocs.org/sdr/DALA2024041904582), Apr 17, 2024: FRAME. CRACKED. SHIP 3253 DISC: CRACK INDICATION FOUND ON FRAME WEB HORIZONTAL FLANGE LOCATED ON FR68 AT LEVEL OF STRINGER 22R, CRACK LENGHT= 1.0 INCH APPROX. C/A: ACCOMPLISHED
- [SDR DALA2024041904577](https://openairdocs.org/sdr/DALA2024041904577), Apr 17, 2024: FRAME. CRACKED. SHIP 3253 DISC: CRACK INDICATION FOUND ON FRAME WEB HORIZONTAL FLANGE LOCATED ON FR68 AT LEVEL OF STRINGER 22R, CRACK LENGHT= 1.0 INCH APPROX. C/A: ACCOMPLISHED
- [SDR DALA2024041904579](https://openairdocs.org/sdr/DALA2024041904579), Apr 16, 2024: FRAME. CRACKED. DURING C-CK AND WHILE ACCOMPLISHING 5311-01244-01B, CRACK FOUND IN FR68 RT, WEB AT STR 22R. PER ER/A 616797-14AD REV A, DTE STAGE 2 ACCOMPLISHED. DTE STAGE 3 IS
- [SDR DALA2024041504404](https://openairdocs.org/sdr/DALA2024041504404), Apr 13, 2024: PIN. BROKEN. BROKEN PIN INTERNAL MECHANISM EVACUATION SLIDE AT PASSENGER DOOR 831. REMOVED SLIDE RAFT IN UNSERVICEABLE CONDITION PN D30664-705 SN A6282RP. AS PER AMDS CARD 2
- [SDR DALA2024022602585](https://openairdocs.org/sdr/DALA2024022602585), Feb 23, 2024: OXYGEN MASK. NO TEST. SHIP 3253 DISC: F/O MASK IS NOT TESTING. C/A: SWAPPED F/O'S AND PRIMARY OBSERVERS O2 MASK STORAGE BOX R/R PRIMARY OBERSERVERS O2 MASK STOWAGE BOX PER A320 AMM 3
- [SDR DALA2023032302195](https://openairdocs.org/sdr/DALA2023032302195), Mar 22, 2023: UNKNOWN. UNKNOWN. SHIP 3253 - ATO - DUE TO BRAKE SYS 2 FAULT. CORRECTIVE ACTION: PLACED ON MEL DEFERRAL. LATER, WIRING CHECK C/W AND R/R BSCU PER A320 AMM 32-42-34. OPS CHECK GOO

All 183: https://openairdocs.org/aircraft/N353NW/reports.md

## STCs that may be installed (OpenAirDocs) (285, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Airbus Industrie A320-212)

- [STC ST03438NY](https://openairdocs.org/stc/ST03438NY): Installation of Adams Rite Lavatory Equipment. Delta Engineering Corporation
- [STC ST12434AC](https://openairdocs.org/stc/ST12434AC): Replacement of the wing fuel tank access panel gasket. Aviation Devices & Electronic Components, LLC
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST02228SE](https://openairdocs.org/stc/ST02228SE): Installation of Bin NuLook. Safran Cabin, Inc
- [STC ST04474NY](https://openairdocs.org/stc/ST04474NY): Activation of Wireless Local Area Network (WLAN) system. Jet Aviation AG
- [STC ST04254NY](https://openairdocs.org/stc/ST04254NY): Installation of Viasat Satcom Software. ALOFT AeroArchitects
- [STC ST02159SE-D](https://openairdocs.org/stc/ST02159SE-D): Installation of an interior reconfiguration. B/E Aerospace, Inc. - FSI
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST03416NY](https://openairdocs.org/stc/ST03416NY): Installation of Intelsat Connectivity Antenna (with demod option). Delta Engineering Corporation
- [STC ST02913NY](https://openairdocs.org/stc/ST02913NY): Installation of a Panasonic Avionics Corporation Global Communications Suite (GCS) and/or In-Flight Entertainment System. Delta Engineering Corporation
- [STC ST04209AT](https://openairdocs.org/stc/ST04209AT): Installation of a passenger interior configuration. Aero Design Services, Inc
- [STC ST04170AT](https://openairdocs.org/stc/ST04170AT): Installation / Activation of an IFE System. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04370AT](https://openairdocs.org/stc/ST04370AT): Cabin Interior Reconfiguration. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04386AT](https://openairdocs.org/stc/ST04386AT): Description of Type Design Change: Interior Reconfiguration in an Airbus A320 Series Aircraft. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST04387AT](https://openairdocs.org/stc/ST04387AT): Class Divider Installation. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST12107NY](https://openairdocs.org/stc/ST12107NY): Update of Cabin Interior. Delta Engineering Corporation
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST03741NY](https://openairdocs.org/stc/ST03741NY): Viasat KA SATCOM Antenna System Installation, approve configurations. ALOFT AeroArchitects
- [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc
- [STC ST03742NY](https://openairdocs.org/stc/ST03742NY): Viasat KA Cabin Distribution System Installation. ALOFT AeroArchitects
- [STC ST02890NY](https://openairdocs.org/stc/ST02890NY): Installation of a Panasonic Avionics Corporation Global Communications Suite Antenna. Delta Engineering Corporation
- [STC ST04759NY](https://openairdocs.org/stc/ST04759NY): Installation of a single cockpit USB charger. Eirtech Aviation Services Inc
- [STC ST02356LA](https://openairdocs.org/stc/ST02356LA): Installation of Inflight Warning Systems Fan Vibration Monitor Unit. Astronics Advanced Electronic Systems (AES)
- [STC ST02699LA](https://openairdocs.org/stc/ST02699LA): Installation of Vogt Aero Nickel Cadmium Battery P/N 2758-LMVA or 2758-RMVA. Vogt Aero LLC
- [STC ST01739NY](https://openairdocs.org/stc/ST01739NY): Electromagnetic Compatibility Testing of Aircraft Transmitting Portable Electronic Devices (T-PEDs) as non-interference tolerance testing. Anuvu IFC Corporation
- [STC ST04462CH](https://openairdocs.org/stc/ST04462CH): Installation of Row 44 Broadband Antenna System Provisions. Anuvu IFC Corporation
- [STC ST12229IB](https://openairdocs.org/stc/ST12229IB): Installation of Thinkom antenna on the top rear fuselage. EAD Aerospace Airworthiness T/A Eclipse Technics
- [STC ST04288CH](https://openairdocs.org/stc/ST04288CH): Installation of an Automatic Dependent Surveillance Broadcast Out (ADS-B Out) Transponder System with Honeywell Integrated Multi-Mode Receiver (IMMR), Model Number IMMR 20.1 installed with TSO-C190 compliant GPS antenna. Amphenol Cable and Interconnect Technologies Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST04292CH](https://openairdocs.org/stc/ST04292CH): Installation of JADE SATCOM Antenna System Provisions. Amphenol Cable and Interconnect Technologies Inc
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA5880NM](https://openairdocs.org/stc/SA5880NM): Installation of video/cart stowage unit. Safran Cabin Inc
- [STC ST01818LA](https://openairdocs.org/stc/ST01818LA): Installation of Forward RH Stowage. Safran Cabin Inc
- [STC ST02395LA](https://openairdocs.org/stc/ST02395LA): Interior Installations and Modifications. Safran Cabin Inc
- [STC ST02735LA](https://openairdocs.org/stc/ST02735LA): Installation of modular lower deck Cargo Loading System (CLS). Telair International
- [STC ST03417NY](https://openairdocs.org/stc/ST03417NY): Installation with demod option of Intelsat Cabin Connectivity System. Delta Engineering Corporation
- [STC ST04089NY](https://openairdocs.org/stc/ST04089NY): Installation of Cabin Seating. Delta Engineering Corporation
- [STC ST04003CH](https://openairdocs.org/stc/ST04003CH): Installation of a Kontron Stored Content Wireless In-Flight Entertainment (IFE) System. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST02801LA](https://openairdocs.org/stc/ST02801LA): Installation of ELT Kannad 406 AF and associated equipment. Allegiant Air LLC
- [STC ST03450CH](https://openairdocs.org/stc/ST03450CH): Certification of Radio Frequency Compatibility with Wireless Data Technologies. Amphenol Cable and Interconnect Technologies Inc
- [STC ST00950CH](https://openairdocs.org/stc/ST00950CH): Installation of an AlliedSignal CAS-81A TCAS II system. Amphenol Cable and Interconnect Technologies Inc
- [STC ST02612CH](https://openairdocs.org/stc/ST02612CH): Installation of AD Aerospace Cockpit Door Monitoring System. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST02626CH](https://openairdocs.org/stc/ST02626CH): Installation of ECS EZMount® mechanical mounting assemblies on lower frames of cockpit sliding windows. Amphenol Cable and Interconnect Technologies Inc
- [STC ST03176NY](https://openairdocs.org/stc/ST03176NY): Installation of a Gogo ATG4 system. Amphenol Cable and Interconnect Technologies Inc
- [STC ST04328CH](https://openairdocs.org/stc/ST04328CH): Installation and activation of the RAVE Wireless Broadband System. Amphenol Cable and Interconnect Technologies Inc
- [STC ST04334CH](https://openairdocs.org/stc/ST04334CH): Installation and activation of an ARINC 791 SATCOM System. Amphenol Cable and Interconnect Technologies Inc

All 285: https://openairdocs.org/aircraft/N353NW/stcs.md

## Related

- Other Airbus Industrie A320-212 aircraft: https://openairdocs.org/model/airbus-industrie-a320-212/aircraft.md
- The CFM International CFM56 series engine: https://openairdocs.org/engine/cfm-international-cfm56-series.md

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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.