# N103SW: 2003 Bombardier BD-700-1A10

- Status: Valid registration
- Airframe: Bombardier BD-700-1A10 (registry code 1390006, TCDS T00003NY (OpenAirDocs match))
- Engine: BMW Rolls BR-700 series (registry code 09500)
- Serial number: 9129
- Year built: 2003
- Type: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: June 26, 2004
- Certificate issued: September 10, 2018
- Expires: September 30, 2028
- Mode S code: A0117E
- Registered owner: Tvpx Aircraft Solutions Inc Trustee
- Location: North Salt Lake, UT
- Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs)
- Page: https://openairdocs.org/aircraft/N103SW

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.

## ADs matched by airframe (Bombardier BD-700-1A10) (OpenAirDocs)

- [AD 2026-15-09](https://openairdocs.org/ad/2026-15-09): Landing Gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 3, 2026
- [AD 2026-11-07](https://openairdocs.org/ad/2026-11-07): Equipment/furnishings · Bombardier BD-700-1A10, BD-700-1A11 and BD-700-2A12. Effective Jul 20, 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 2026-09-18](https://openairdocs.org/ad/2026-09-18): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 26, 2026
- [AD 2026-08-04](https://openairdocs.org/ad/2026-08-04): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 29, 2026
- [AD 2025-14-51](https://openairdocs.org/ad/2025-14-51): Indicating/Recording System · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 4, 2026
- [AD 2025-16-07](https://openairdocs.org/ad/2025-16-07): Oxygen · Bombardier BD-700-1A10. Effective Sep 18, 2025
- [AD 2025-12-01](https://openairdocs.org/ad/2025-12-01): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 17, 2025
- [AD 2025-07-11](https://openairdocs.org/ad/2025-07-11): Hydraulic Power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 2, 2025
- [AD 2025-09-04](https://openairdocs.org/ad/2025-09-04): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 6, 2025
- [AD 2024-26-09](https://openairdocs.org/ad/2024-26-09): Time Limits/Maintenance Checks; Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 11, 2025
- [AD 2024-23-02](https://openairdocs.org/ad/2024-23-02): Landing Gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 15, 2025
- [AD 2024-23-08](https://openairdocs.org/ad/2024-23-08): Wings · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 6, 2025
- [AD 2024-07-09](https://openairdocs.org/ad/2024-07-09): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 17, 2024
- [AD 2024-03-08](https://openairdocs.org/ad/2024-03-08): Pneumatic · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 3, 2024
- [AD 2024-02-05](https://openairdocs.org/ad/2024-02-05): Wings · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 9, 2024
- [AD 2023-24-08](https://openairdocs.org/ad/2023-24-08): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Feb 6, 2024
- [AD 2023-12-02](https://openairdocs.org/ad/2023-12-02): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 7, 2023
- [AD 2023-13-15](https://openairdocs.org/ad/2023-13-15): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 27, 2023
- [AD 2023-08-01](https://openairdocs.org/ad/2023-08-01): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 20, 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 2023-05-11](https://openairdocs.org/ad/2023-05-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 12, 2023
- [AD 2022-24-01](https://openairdocs.org/ad/2022-24-01): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 9, 2023
- [AD 2022-25-13](https://openairdocs.org/ad/2022-25-13): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 13, 2023
- [AD 2022-14-07](https://openairdocs.org/ad/2022-14-07): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 19, 2022
- [AD 2022-13-05](https://openairdocs.org/ad/2022-13-05): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 11, 2022
- [AD 2022-11-17](https://openairdocs.org/ad/2022-11-17): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 22, 2022
- [AD 2022-12-01](https://openairdocs.org/ad/2022-12-01): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 19, 2022
- [AD 2021-21-04](https://openairdocs.org/ad/2021-21-04): Powerplant · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 8, 2021
- [AD 2021-10-22](https://openairdocs.org/ad/2021-10-22): Fuel · Bombardier BD-700-1A10. Effective Jul 6, 2021
- [AD 2021-08-11](https://openairdocs.org/ad/2021-08-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 27, 2021
- [AD 2021-03-17](https://openairdocs.org/ad/2021-03-17): Lights · Bombardier BD-700-1A10. Effective Mar 30, 2021
- [AD 2020-12-14](https://openairdocs.org/ad/2020-12-14): Electrical power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 8, 2020
- [AD 2020-12-15](https://openairdocs.org/ad/2020-12-15): Pneumatic · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 24, 2020
- [AD 2020-05-27](https://openairdocs.org/ad/2020-05-27): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 7, 2020
- [AD 2020-03-21](https://openairdocs.org/ad/2020-03-21): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 12, 2020
- [AD 2020-02-15](https://openairdocs.org/ad/2020-02-15): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 12, 2020
- [AD 2019-12-02](https://openairdocs.org/ad/2019-12-02): Electrical Power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 12, 2019
- [AD 2019-03-22](https://openairdocs.org/ad/2019-03-22): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 15, 2019
- [AD 2018-25-07](https://openairdocs.org/ad/2018-25-07): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 15, 2019
- [AD 2018-22-08](https://openairdocs.org/ad/2018-22-08): Fire protection · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 10, 2018
- [AD 2018-20-20](https://openairdocs.org/ad/2018-20-20): Flilght Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Nov 20, 2018
- [AD 2018-21-03](https://openairdocs.org/ad/2018-21-03): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective Nov 19, 2018
- [AD 2018-09-15](https://openairdocs.org/ad/2018-09-15): Engine · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 15, 2018
- [AD 2017-22-14](https://openairdocs.org/ad/2017-22-14): Navigation · Bombardier BD-100-1A10 (Challenger 300), BD-500-1A10, BD-500-1A11 and 13 more. Effective Dec 20, 2017
- [AD 2017-19-11](https://openairdocs.org/ad/2017-19-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Oct 23, 2017
- [AD 2017-14-15](https://openairdocs.org/ad/2017-14-15): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 31, 2017
- [AD 2016-17-16](https://openairdocs.org/ad/2016-17-16): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Oct 5, 2016
- [AD 2016-15-06](https://openairdocs.org/ad/2016-15-06): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 8, 2016
- [AD 2016-15-03](https://openairdocs.org/ad/2016-15-03): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 31, 2016
- [AD 2016-10-06](https://openairdocs.org/ad/2016-10-06): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 23, 2016
- [AD 2016-01-12](https://openairdocs.org/ad/2016-01-12): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Feb 25, 2016
- [AD 2015-17-05](https://openairdocs.org/ad/2015-17-05): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 29, 2015
- [AD 2014-26-09](https://openairdocs.org/ad/2014-26-09): Ice and Rain Protection · Bombardier BD-700-1A10. Effective Feb 19, 2015
- [AD 2014-20-03](https://openairdocs.org/ad/2014-20-03): Fire Protection · Bombardier BD-700-1A10 and BD-700-1A11. Effective Nov 5, 2014
- [AD 2012-03-05](https://openairdocs.org/ad/2012-03-05): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 23, 2012
- [AD 2011-01-10](https://openairdocs.org/ad/2011-01-10): Hydraulic power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Feb 9, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-23-08](https://openairdocs.org/ad/2010-23-08): Electrical power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 14, 2010
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2009-15-03](https://openairdocs.org/ad/2009-15-03): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 19, 2009
- [AD 2006-19-04](https://openairdocs.org/ad/2006-19-04): Honeywell COM unit and Mode S transponder · Bombardier BD-700-1A10, BD-700-1A11, 550 and 26 more. Effective Oct 17, 2006
- [AD 2006-18-08](https://openairdocs.org/ad/2006-18-08): Nosewheel tires · Bombardier BD-700-1A10, BD-700-1A11, Aviation Tires and 7 more. Effective Oct 11, 2006

Historical (superseded or no longer in force): AD 2023-03-06, AD 2021-10-02, AD 2016-25-18, AD 2014-03-05, AD 2008-24-12, AD 2006-22-05

## ADs matched by engine (BMW Rolls BR-700 series) (OpenAirDocs)

- [AD 2026-21-04](https://openairdocs.org/ad/2026-21-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Nov 23, 2026
- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2023-17-11](https://openairdocs.org/ad/2023-17-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Sep 20, 2023
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021
- [AD 2021-14-03](https://openairdocs.org/ad/2021-14-03): Turbine Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 19, 2021
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2014-12-03](https://openairdocs.org/ad/2014-12-03): Fuel metering units (FMUs) · Rolls-Royce Deutschland BR700-725A1-12. Effective Jul 17, 2014
- [AD 2014-08-05](https://openairdocs.org/ad/2014-08-05): Low-pressure compressor (LPC) case ice impact panels · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 23, 2014
- [AD 2014-07-02](https://openairdocs.org/ad/2014-07-02): High-pressure (HP) compressor stages 1 to 6 rotor disc assemblies · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 8, 2014
- [AD 2013-12-03](https://openairdocs.org/ad/2013-12-03): Fuel pump tube · Rolls-Royce Deutschland BR700-725A1-12. Effective Jun 14, 2013
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2012-14-01](https://openairdocs.org/ad/2012-14-01): LP compressor booster rotor · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Oct 19, 2012
- [AD 2009-07-01 R1](https://openairdocs.org/ad/2009-07-01-R1): High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 6, 2012
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2009-21-04](https://openairdocs.org/ad/2009-21-04): Engine Failure · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Dec 3, 2009
- [AD 2009-04-13](https://openairdocs.org/ad/2009-04-13): Low pressure (LP) compressor (fan) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Mar 26, 2009
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2005-16-12](https://openairdocs.org/ad/2005-16-12): Independent Overspeed Protection (IOP) unit. · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 26, 2005
- [AD 2000-25-51](https://openairdocs.org/ad/2000-25-51): High Pressure Turbine Disks · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Feb 20, 2001
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

Historical (superseded or no longer in force): AD 2022-24-06, AD 2013-05-13, AD 2012-26-14, AD 2009-07-01, AD 2003-07-11, AD 2001-05-06

## Information bulletins (advisory)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15): Navigation System
- [SAIB NM-15-02](https://openairdocs.org/saib/NM-15-02): Cabin Equipment/Furnishings
- [SAIB NM-11-34](https://openairdocs.org/saib/NM-11-34): Doors: Passenger/Crew Doors, Tensator Springs of the Door Actuator

## Earlier aircraft with N103SW

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N103SW before.

- [Cancelled 2006-04-21](https://openairdocs.org/deregistered/N103SW-2006-04-21): Boeing 737-2H4, S/N 23109, built 1984. Exported to Lebanon. Owner: Jet Midwest Inc, Kansas City, KS

## Service difficulty reports (134)

- [SDR SWAA043344](https://openairdocs.org/sdr/SWAA043344), Nov 15, 2004: SKIN. RIGHT WING NR 5 L/E SLAT DELAMINATED.  REMOVED AND REPLACED NR 5 L/E SLAT PER MM.
- [SDR SWAA042795](https://openairdocs.org/sdr/SWAA042795), Sep 27, 2004: SKIN. DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 847, STRINGER 24L, CRACKED.  REPAIRED SKIN PER EA.
- [SDR SWAA042793](https://openairdocs.org/sdr/SWAA042793), Sep 26, 2004: SKIN. DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN AT BS 787, STRINGER 18L, CRACKED.  REPAIRED SKIN PER EA.
- [SDR SWAA041786](https://openairdocs.org/sdr/SWAA041786), Jun 25, 2004: BATTERY. DURING SCHEDULED PM CHECK, FOUND AFT CABIN OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHTS INOP.  REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK PER MM.
- [SDR SWAA041535](https://openairdocs.org/sdr/SWAA041535), Jun 1, 2004: CASTING. DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD NR 5 GROUND SPOILER ACTUATOR CASTING, CRACKED.  REMOVED AND REPLACED NR 5 ACTUATOR CASTING PER MM AND SRM.
- [SDR SWAA040444](https://openairdocs.org/sdr/SWAA040444), Feb 12, 2004: CABLE. ABORTED TAKEOFF, NR 2 THRUST LEVER MOVEMENT RESTRICTED.  ADJUSTED NR 2 ENGINE THRUST REVERSER FOLLOW-UP CABLE PER MM.
- [SDR SWAA040351](https://openairdocs.org/sdr/SWAA040351), Feb 2, 2004: SWITCH. INFLIGHT SHUTDOWN, AIRTURN BACK, DECLARED EMERGENCY, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT.  LIGHT WOULD NOT EXTINGUISH.  REMOVED AND REPLAC
- [SDR SWAA032427](https://openairdocs.org/sdr/SWAA032427), Nov 3, 2003: LIGHT. DURING SCHEDULED PM CHECK, FOUND EEPLS INOP AT ROW 3 AND ROW 8.  RELAMPED EEPLS PER MM.
- [SDR SWAA031989](https://openairdocs.org/sdr/SWAA031989), Sep 4, 2003: SKIN. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 575, STR 10R.  REPAIRED SKIN PER SRM.
- [SDR SWAA031951](https://openairdocs.org/sdr/SWAA031951), Aug 31, 2003: SKIN. DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B + 16, STR 17R.  REPAIRED SKIN PER SRM.

---
From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.