# Boeing 737-281

- Type: Aircraft model (FAA registry)
- Registry code: 138448P
- Manufacturer (registry): BOEING
- Model: 737-281
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 134
- Weight class: 20,000 lb and over
- Cruise speed: 388 mph
- Certification: Type certificated
- Data sheet: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Holder: The Boeing Company
- Registered aircraft: 0
- Page: https://openairdocs.org/model/boeing-737-281

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2026-13-13](https://openairdocs.org/ad/2026-13-13): Navigation · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 9 more. Effective Jul 1, 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 2026-09-12](https://openairdocs.org/ad/2026-09-12): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 17, 2026
- [AD 2025-02-02](https://openairdocs.org/ad/2025-02-02): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Mar 17, 2025
- [AD 2023-13-12](https://openairdocs.org/ad/2023-13-12): Oxygen · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 17 more. Effective Sep 5, 2023
- [AD 2023-12-13](https://openairdocs.org/ad/2023-12-13): Navigation · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 9 more. Effective Jun 21, 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 2022-25-15](https://openairdocs.org/ad/2022-25-15): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jan 26, 2023
- [AD 2022-24-09](https://openairdocs.org/ad/2022-24-09): Air conditioning · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 12 more. Effective Jan 26, 2023
- [AD 2021-25-05](https://openairdocs.org/ad/2021-25-05): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Feb 22, 2022
- [AD 2021-25-09](https://openairdocs.org/ad/2021-25-09): Flight Control System · Boeing 737-200 Series and 737-200C Series. Effective Feb 1, 2022
- [AD 2021-10-11](https://openairdocs.org/ad/2021-10-11): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jul 29, 2021
- [AD 2021-08-12](https://openairdocs.org/ad/2021-08-12): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective May 28, 2021
- [AD 2021-08-04](https://openairdocs.org/ad/2021-08-04): Oxygen · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 23 more. Effective May 26, 2021
- [AD 2020-26-09](https://openairdocs.org/ad/2020-26-09): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jan 27, 2021
- [AD 2020-26-04](https://openairdocs.org/ad/2020-26-04): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jan 25, 2021
- [AD 2020-21-02](https://openairdocs.org/ad/2020-21-02): Fire protection · Airbus Canada Limited Partnership BD-500-1A10, BD-500-1A11, A330-201 and 45 more. Effective Nov 19, 2020
- [AD 2020-02-16](https://openairdocs.org/ad/2020-02-16): Fuselage · Boeing 737-200 Series, 737-200C Series, 737-300 Series and 2 more. Effective Mar 18, 2020
- [AD 2019-23-16](https://openairdocs.org/ad/2019-23-16): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Feb 3, 2020
- [AD 2019-23-14](https://openairdocs.org/ad/2019-23-14): Nitrogen Generation System · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jan 21, 2020
- [AD 2019-16-12](https://openairdocs.org/ad/2019-16-12): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Oct 9, 2019
- [AD 2019-15-07](https://openairdocs.org/ad/2019-15-07): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Sep 19, 2019
- [AD 2019-14-15](https://openairdocs.org/ad/2019-14-15): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Sep 19, 2019
- [AD 2019-14-02](https://openairdocs.org/ad/2019-14-02): Hydraulic power · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 11 more. Effective Aug 27, 2019
- [AD 2019-13-02](https://openairdocs.org/ad/2019-13-02): Fuselage · Boeing 737-200 Series, 737-200C Series, 737-300 Series and 2 more. Effective Aug 23, 2019
- [AD 2019-10-03](https://openairdocs.org/ad/2019-10-03): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jul 11, 2019
- [AD 2019-09-01](https://openairdocs.org/ad/2019-09-01): Ice and rain protection · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 26, 2019
- [AD 2019-08-03](https://openairdocs.org/ad/2019-08-03): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 17, 2019
- [AD 2019-08-02](https://openairdocs.org/ad/2019-08-02): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 13, 2019
- [AD 2019-01-06](https://openairdocs.org/ad/2019-01-06): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Mar 19, 2019
- [AD 2018-23-12](https://openairdocs.org/ad/2018-23-12): Equipment/furnishings · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 180 more. Effective Dec 28, 2018
- [AD 2018-21-08](https://openairdocs.org/ad/2018-21-08): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Nov 20, 2018
- [AD 2018-19-20](https://openairdocs.org/ad/2018-19-20): Fuselage · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 1 more. Effective Oct 31, 2018
- [AD 2018-18-13](https://openairdocs.org/ad/2018-18-13): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Oct 18, 2018
- [AD 2018-18-03](https://openairdocs.org/ad/2018-18-03): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Oct 15, 2018
- [AD 2018-17-23](https://openairdocs.org/ad/2018-17-23): Fueslage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Oct 4, 2018
- [AD 2018-16-09](https://openairdocs.org/ad/2018-16-09): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Sep 10, 2018
- [AD 2018-12-05](https://openairdocs.org/ad/2018-12-05): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jul 13, 2018
- [AD 2018-09-13](https://openairdocs.org/ad/2018-09-13): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 19, 2018
- [AD 2018-09-08](https://openairdocs.org/ad/2018-09-08): Fuselage · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 1 more. Effective Jun 8, 2018
- [AD 2018-10-12](https://openairdocs.org/ad/2018-10-12): Wings, Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 7, 2018
- [AD 2018-09-01](https://openairdocs.org/ad/2018-09-01): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 4, 2018
- [AD 2018-04-12](https://openairdocs.org/ad/2018-04-12): Fuel · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Apr 9, 2018
- [AD 2018-04-08](https://openairdocs.org/ad/2018-04-08): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Apr 3, 2018
- [AD 2018-04-06](https://openairdocs.org/ad/2018-04-06): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Mar 30, 2018
- [AD 2018-01-08](https://openairdocs.org/ad/2018-01-08): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Feb 16, 2018
- [AD 2017-25-10](https://openairdocs.org/ad/2017-25-10): Stabilizers · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jan 18, 2018
- [AD 2017-24-05](https://openairdocs.org/ad/2017-24-05): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jan 2, 2018
- [AD 2017-23-07](https://openairdocs.org/ad/2017-23-07): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Dec 26, 2017
- [AD 2017-23-05](https://openairdocs.org/ad/2017-23-05): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Dec 20, 2017

Historical (superseded or no longer in force):

- [AD 2022-05-04](https://openairdocs.org/ad/2022-05-04) (historical): Navigation · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 9 more. Effective Feb 24, 2022
- [AD 2021-14-20](https://openairdocs.org/ad/2021-14-20) (historical): Cabin Altitude Pressure Switches · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 12 more. Effective Jul 20, 2021
- [AD 2021-07-02](https://openairdocs.org/ad/2021-07-02) (historical): Ice and rain protection · Boeing 737-200 Series. Effective Apr 20, 2021
- [AD 2017-25-12](https://openairdocs.org/ad/2017-25-12) (historical): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jan 22, 2018
- [AD 2017-23-02](https://openairdocs.org/ad/2017-23-02) (historical): Fuselage · Boeing 737-200 Series, 737-200C Series, 737-300 Series and 2 more. Effective Dec 20, 2017
- [AD 2015-16-01](https://openairdocs.org/ad/2015-16-01) (historical): Air Conditioning · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 9 more. Effective Sep 15, 2015
- [AD 2014-03-06](https://openairdocs.org/ad/2014-03-06) (historical): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Apr 9, 2014
- [AD 2014-05-02](https://openairdocs.org/ad/2014-05-02) (historical): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Apr 8, 2014
- [AD 2013-24-13](https://openairdocs.org/ad/2013-24-13) (historical): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 8 more. Effective Jan 7, 2014
- [AD 2013-18-08](https://openairdocs.org/ad/2013-18-08) (historical): JASC Code 53, Fuselage · Boeing 737-200 Series, 737-200C Series, 737-300 Series and 2 more. Effective Nov 6, 2013
- [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013
- [AD 2012-19-11](https://openairdocs.org/ad/2012-19-11) (historical): Air Conditioning · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 9 more. Effective Nov 7, 2012
- [AD 2012-18-13](https://openairdocs.org/ad/2012-18-13) (historical): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Oct 24, 2012
- [AD 2012-12-05](https://openairdocs.org/ad/2012-12-05) (historical): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jul 23, 2012
- [AD 2010-25-06](https://openairdocs.org/ad/2010-25-06) (historical): Fuselage · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 1 more. Effective Feb 1, 2011
- [AD 2010-15-08](https://openairdocs.org/ad/2010-15-08) (historical): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Aug 31, 2010
- [AD 2009-21-10](https://openairdocs.org/ad/2009-21-10) (historical): Oxygen · Airbus A300, Model B4-605R, A300, Model B4-620, A300, Model B4-622 and 138 more. Effective Dec 17, 2009
- [AD 2009-16-14](https://openairdocs.org/ad/2009-16-14) (historical): Forward entry door · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Sep 9, 2009
- [AD 2008-13-12 R1](https://openairdocs.org/ad/2008-13-12-R1) (historical): Upper frame to side frame splice of the fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Dec 1, 2008
- [AD 2008-17-03](https://openairdocs.org/ad/2008-17-03) (historical): Body station frame · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Sep 23, 2008
- [AD 2008-13-12](https://openairdocs.org/ad/2008-13-12) (historical): Upper frame to side frame splice of the fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Aug 12, 2008
- [AD 2008-11-04](https://openairdocs.org/ad/2008-11-04) (historical): Upper and lower hinge cutouts · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 25, 2008
- [AD 2008-10-09](https://openairdocs.org/ad/2008-10-09) (historical): FAA-approved maintenance program · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 12, 2008
- [AD 2008-05-06](https://openairdocs.org/ad/2008-05-06) (historical): Longitudinal floor beam web · Boeing 737-100 Series, 737-200 Series, 737-300 Series and 2 more. Effective Apr 8, 2008
- [AD 2007-26-04](https://openairdocs.org/ad/2007-26-04) (historical): Forward fastener row · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jan 22, 2008
- [AD 2007-11-07](https://openairdocs.org/ad/2007-11-07) (historical): Fuel boost pump · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 6, 2007
- [AD 2006-07-12](https://openairdocs.org/ad/2006-07-12) (historical): Fuselage skin at certain lap joints · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective May 5, 2006
- [AD 2005-20-03](https://openairdocs.org/ad/2005-20-03) (historical): Intercostal webs, attachment clips, and stringer splice channels · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 2 more. Effective Nov 1, 2005
- [AD 2005-20-01](https://openairdocs.org/ad/2005-20-01) (historical): Stiffeners at left buttock line (LBL) and right buttock line (RBL) · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Nov 1, 2005
- [AD 2005-13-30](https://openairdocs.org/ad/2005-13-30) (historical): Fuselage skin panels · Boeing 737-100 Series, 737-200 Series and 737-200C Series. Effective Aug 1, 2005
- [AD 2005-12-05](https://openairdocs.org/ad/2005-12-05) (historical): Flight deck door · Reinforced cockpit door (Safran Cabin STC ST01335LA or 2 others). Effective Jul 19, 2005
- [AD 2005-07-12](https://openairdocs.org/ad/2005-07-12) (historical): Doorstop intercostal strap · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective May 12, 2005
- [AD 2004-18-06](https://openairdocs.org/ad/2004-18-06) (historical): Upper and lower skin panels of the fuselage · Boeing 737-200 Series, 737-200C Series, 737-300 Series and 2 more. Effective Oct 13, 2004
- [AD 2004-03-34](https://openairdocs.org/ad/2004-03-34) (historical): Door mounted escape slides · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Mar 24, 2004
- [AD 2003-24-08](https://openairdocs.org/ad/2003-24-08) (historical): Left and right outbaord mid-flaps · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Dec 4, 2003
- [AD 2003-14-04](https://openairdocs.org/ad/2003-14-04) (historical): Flight Deck Door Pressure Relief Latch Assemblies · Boeing 737-200 Series, 737-300 Series, 737-400 Series and 14 more. Effective Jul 25, 2003
- [AD 2003-08-15](https://openairdocs.org/ad/2003-08-15) (historical): Fuselage Lap Joints and Stringer Clips · Boeing 737-200 Series, 737-200C Series, 737-300 Series and 2 more. Effective May 12, 2003
- [AD 2003-03-15](https://openairdocs.org/ad/2003-03-15) (historical): Airplane Flight Manual (AFM) - Oxygen Masks · Boeing 707 Series (all), 720 Series (all), 727 Series (all) and 75 more. Effective Mar 7, 2003
- [AD 2002-22-05](https://openairdocs.org/ad/2002-22-05) (historical): Outboard mid-flap · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Nov 15, 2002
- [AD 2002-10-11](https://openairdocs.org/ad/2002-10-11) (historical): Aft Pressure Bulkhead at Body Station (BS) 1016 · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 27, 2002
- [AD 2002-07-08](https://openairdocs.org/ad/2002-07-08) (historical): Lap Joints of the Fuselage · Boeing 737-200 Series, 737-200C Series, 737-300 Series and 2 more. Effective May 17, 2002
- [AD 2002-05-07](https://openairdocs.org/ad/2002-05-07) (historical): Inboard Tracks of the Outboard Flaps · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Apr 22, 2002
- [AD 2002-01-01](https://openairdocs.org/ad/2002-01-01) (historical): Elevator Tab Assembly · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Feb 19, 2002
- [AD 2001-24-02](https://openairdocs.org/ad/2001-24-02) (historical): Shoulder Restraint Harness Attachment · Boeing 707-100 Long Body, 707-100B Long Body, 707-300 Series (all) and 20 more. Effective Jan 4, 2002
- [AD 2000-06-13 R1](https://openairdocs.org/ad/2000-06-13-R1) (historical): Aft Cargo Door · Boeing 737-200 Series, 737-200C Series, 737-300 Series and 1 more. Effective Aug 15, 2001
- [AD 2001-08-07](https://openairdocs.org/ad/2001-08-07) (historical): Main Deck Cargo Door Frames · Boeing 737-200 Series and 737-300 Series with STC SA2969SO. Effective May 29, 2001
- [AD 2000-25-07](https://openairdocs.org/ad/2000-25-07) (historical): Wing Outboard Flap · Boeing 737-100 Series, 737-200 Series and 737-200C Series. Effective Jan 2, 2001
- [AD 2000-17-04](https://openairdocs.org/ad/2000-17-04) (historical): Fuselage Lap Joint · Boeing 737-100 Series, 737-200 Series and 737-200C Series. Effective Sep 11, 2000
- [AD 2000-17-51](https://openairdocs.org/ad/2000-17-51) (historical): Main Deck Cargo Door · Boeing 737-200 Series and 737-300 Series with STC SA2969SO. Effective Aug 30, 2000
- [AD 2000-13-51](https://openairdocs.org/ad/2000-13-51) (historical): Main Deck Cargo Door · Boeing 737-200 Series and 737-300 Series with STC SA2969SO. Effective Jul 25, 2000

All 438: https://openairdocs.org/model/boeing-737-281/ads.md

## Information bulletins (advisory) (17)

- [SAIB 2026-18](https://openairdocs.org/saib/2026-18): NOSE/TAIL LANDING GEAR, Installation of AeroControlex STC ST01255CH may allow water to leak and freeze on the nose wheel steering cables and prevent pilot from steering. Issued Oct 23, 2026
- [SAIB 2026-01](https://openairdocs.org/saib/2026-01): PITOT/STATIC ANTI-ICE SYSTEM. Issued Jan 8, 2026
- [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-17-17](https://openairdocs.org/saib/NM-17-17): Oxygen System. Issued Jun 19, 2017
- [SAIB NM-17-10](https://openairdocs.org/saib/NM-17-10): Maintenance Practices. Issued Apr 13, 2017
- [SAIB NM-17-06](https://openairdocs.org/saib/NM-17-06): Fuselage: Chem-Mill Skin Panels. Issued Jan 4, 2017
- [SAIB NM-15-03](https://openairdocs.org/saib/NM-15-03): Flight Controls. Issued Nov 24, 2014
- [SAIB NM-15-02](https://openairdocs.org/saib/NM-15-02): Cabin Equipment/Furnishings. Issued Nov 6, 2014
- [SAIB NM-12-11](https://openairdocs.org/saib/NM-12-11): Equipment/Furnishings: Buffet/Galleys. Issued Jan 10, 2012
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008
- [SAIB NM-08-43](https://openairdocs.org/saib/NM-08-43): Cabin Equipment/Furnishings - Seats. Issued Sep 3, 2008
- [SAIB NM-08-24](https://openairdocs.org/saib/NM-08-24): Water/Waste: Freezing Potable Water Lines. Issued May 22, 2008
- [SAIB NM-07-47](https://openairdocs.org/saib/NM-07-47): Boeing Model 737 Series Forward Airstairs. Issued Sep 6, 2007
- [SAIB NM-07-36](https://openairdocs.org/saib/NM-07-36): Grounding plate and bonding jumper to improve electrical bonds between pitot probes and airplane structure. Issued Jun 8, 2007
- [SAIB NM-07-12](https://openairdocs.org/saib/NM-07-12): Wire bundle W138 and add protection sleeves to the wire bundles for the equipment cooling blowers. Issued Nov 27, 2006
- [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 NM-06-56](https://openairdocs.org/saib/NM-06-56): . Issued Jul 19, 2006

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (5)

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 19990107015539I](https://openairdocs.org/incident/19990107015539I), Jan 7, 1999: Boeing 737281 (N219US), Minneapolis, MN. (-5) Aircraft aborted takeoff at 70 KTS due to dual bleed indication. Maintenance personnel determined that APU bleed valve failed in open postion. Replaced…
- [Incident 19981226042259I](https://openairdocs.org/incident/19981226042259I), Dec 26, 1998: Boeing 737281 (N219US), Kansas City, MO. (-5) December 26, 1998, vanguard airlines Boeing 737-281, N219US, departed Kansas City International Airport, and returned to mci due to a cracked sliding…
- [Incident 19970124006839I](https://openairdocs.org/incident/19970124006839I), Jan 24, 1997: Boeing 737281 (N219US), Denver, CO. Narrative: vanguard flight 612 returned to the field (dia) after flying for approximately 20 minutes, enroute to (mci) Kansas city, MO. (PIC) pilot in command…
- [Incident 19960415013459I](https://openairdocs.org/incident/19960415013459I), Apr 15, 1996: Boeing 737281 (N219US), Dallas-Ft Worth, TX. Narrative: vanguard airlines (vam) flt 126 departed dfw for ict on takeoff/rotation the stick shaker activated. The crew made a turn back and landed…
- [Incident 19891220065419I](https://openairdocs.org/incident/19891220065419I), Dec 20, 1989: Boeing 737281 (N219US), Miami, FL, Minor damage. Blew a tire on takeoff roll. Pilot knew nothing about tire blowing out until he landed at destination.

## Service difficulty reports (120, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR ABXA201004120047](https://openairdocs.org/sdr/ABXA201004120047), Mar 27, 2010: BEAM. CRACKED. RIGHT ENGINE PYLON OUTBOARD BEAM THAT RUNS ACROSS LOWER PART OF HYD BAY ACCESS DOOR IS CRACKED AT 3RD NUT PLATE HOLE FROM FWD END. REMOVED DAMAGED SECTION OF RI
- [SDR CA041105003](https://openairdocs.org/sdr/CA041105003), Nov 4, 2004: FIRE LOOP. INOPERATIVE. (CAN) ENGINE NR 1 FIRE WARNING AT 8000 ASL ON APPROACH. FIRE BOTTLES AND SQUIBS REPLACED IAW MM. NR 1 LOWER FIRE LOOP REPLACED AND CONNECTOR D1098 IAW MM. SYSTE
- [SDR CA040825010](https://openairdocs.org/sdr/CA040825010), Aug 21, 2004: LINE. RUPTURED. (CAN) HYDRAULIC QUANTITY INDICATOR SHOWED RAPID DEPLETION TO 1 GAL AFTER TAKEOFF. FOUND RUPTURED HYDRAULIC LINE P/N BACH8B04NN0214T IN NOSE LANDING GEAR WHEEL W
- [SDR CA031208004](https://openairdocs.org/sdr/CA031208004), Dec 1, 2003: CONTROL VALVE. MALFUNCTIONED. (CAN) ON CLIMB OUT THROUGH 25,000 FT. FLIGHT CREW REPORTED, DUCT OVERHEAT ON RT PACK. COULD NOT CONTROL TEMPERATURE WITH RT PACK ON. AIRCRAFT LOST ALL PRESSURIZ
- [SDR CA030902002](https://openairdocs.org/sdr/CA030902002), Aug 25, 2003: CIRCUIT BOARD. FAILED. (CAN) AIRCRAFT REPORTS SHORTLY AFTER TAKE OFF ROTATION, NUMEROUS THREE PHASE CIRCUIT BREAKERS (2 AND 3 THRUST REVERSER, GASPER FAN AND PANEL INSTRUMENT INDICATO
- [SDR CA030611002](https://openairdocs.org/sdr/CA030611002), Jun 9, 2003: PCU. BROKEN. (CAN) DURING LANDING THROUGH APPROXIMATELY 60 KNOTS, AIRCRAFT EXPERIENCED A COMPLETE LOSS OF 'A' SYSTEM HYDRAULICS. (NOTE: 'A' PUMPS ON WITH LOW PRESSURE LIGHTS
- [SDR CA030313007](https://openairdocs.org/sdr/CA030313007), Mar 11, 2003: ENGINE. FAILED. (CAN) FLIGHT 41, NR 1 ENG FAILURE ON CLIMBOUT SHORTLY AFTER TAKEOFF THROUGH 3200 FT ASL, CREW HEARD A BANG FROM NR 1 ENG AFTER CLIMB THRUST WAS SET & FLAPS HAD 
- [SDR CA030224003](https://openairdocs.org/sdr/CA030224003), Feb 20, 2003: FIRE LOOP. MALFUNCTIONED. (CAN) CREW REPORTED, AT CRUISING ALTITUDE, 20 MINUTES OUT OF YLW THEY EXPERIENCED A VIBRATION FOLLOWED BY AN APU FIRE WARNING. CREW SHUTDOWN APU WITH THE FIRE H
- [SDR CA021209007](https://openairdocs.org/sdr/CA021209007), Nov 29, 2002: BOLT. CRACKED. (CAN) ON APPROACH FLIGHT CREW REPORTED UPON SELECTION OF FLAPS TO NR 1 POSITION THE NR 4 SLAT HUNG UP UNTIL FLAPS WERE SELECTED TO '15' POSITION. ALL INDICATION
- [SDR CA020823003](https://openairdocs.org/sdr/CA020823003), Aug 14, 2002: HOUSING. SPLIT. (CAN) ON APPROACH CREW REPORTED COMPLETE LOSS OF HYD FLUID FROM 'A' SYS UPON SELECTION OF FLAPS & MLG. CREW CONDUCTED MISSED APPROACH & PROCEEDED TO COMPLETE 'L
- [SDR CA020429003](https://openairdocs.org/sdr/CA020429003), Apr 29, 2002: A/C PACK. SMOKE. (CAN) SHORTLY AFTER TAKOFF, F/A NOTIFIED CREW BOTH SMOKE DETECTORS HAD ACTIVATED AND THERE WAS A SMELL OF SMOKE IN THE CABIN. AIRCRAFT IMMEDIATELY RETURNED TO Y
- [SDR CA020422006](https://openairdocs.org/sdr/CA020422006), Apr 15, 2002: STRUCTURE. DAMAGED. (CAN) DURING REGULAR SCHEDULED MAINTENANCE INSPECTION (AD:02-01-01)THE RT ELEVATOR FAILED THE TAB HINGE FREEPLAY CHECK AT THE NR 2 ELEVATOR TAB HINGE POSITION -
- [SDR CA020405001](https://openairdocs.org/sdr/CA020405001), Mar 30, 2002: STRUCTURE. CRACKED. (CAN) SCHEDULED MAINTENANCE;DURING REGULAR SCHEDULED MAINITENANCE INSPECTION, MAINTENANCE ENGINEER SUSPECTED A CRACK AT THE NOSE LANDING GEAR ACTUATOR ATTACH SU
- [SDR CA020319004](https://openairdocs.org/sdr/CA020319004), Mar 17, 2002: DUCT. MISSING. (CAN) SHORTLY AFTER DEPARTING, FLIGHT CREW RECEIVED A NR 1 ENGINE OVERHEAT INDICATION AND IMMEDIATELY RETURNED TO BASE - AIRCRAFT LANDED WITHOUT INCIDENT. MAINT
- [SDR CA020204002](https://openairdocs.org/sdr/CA020204002), Feb 1, 2002: BULLET. SEPARATED. (CAN) FLT CREW RPTED DURING CLIMB AFTER TAKEOFF THEY EXPERIENCED SERIES OF LOUD BANGS FROM NR 2 ENGINE ACCOMPANIED BY ABNORMAL HIGH EGT & LOW N 2 RPM. ALL IND.S
- [SDR CA010907014](https://openairdocs.org/sdr/CA010907014), Aug 31, 2001: TIRE. SEPARATED. (CAN) RECAP SEPARATED FROM TIRE ON TAKEOFF FROM YVR WAS NOT NOTICED UNTIL AIRCRAFT ARRIVED IN YLW. NO OTHER REPORTABLE DAMAGE AS A RESULT OF THIS INCIDENT.
- [SDR CA010921007](https://openairdocs.org/sdr/CA010921007), Aug 16, 2001: ENGINE. FAILED. (CAN) ENROUTE FROM YVR TO YYC EXPERIENCED COMPRESSOR STALL ON NR 1 ENGINE. UPON ESTABLISHING CRUISE POWER SETTNG, CREW HEARD LOUD POP, FOLLOWED 20 SEC LATER BY 
- [SDR CA010625028](https://openairdocs.org/sdr/CA010625028), Jun 14, 2001: CONNECTOR. MISINSTALLED. (CAN) IN TROUBLE SHOOTING A HISTORY OF INTERMITTENT ANTI-SKID PROBLEMS IT WAS DISCOVERED THAT THE HYDRAULIC BRAKE PRESSURE LINES FROM THE AIRFRAME TO THE TOP OF
- [SDR CA010406005](https://openairdocs.org/sdr/CA010406005), Mar 24, 2001: CONNECTOR. DAMAGED. (CAN) THE AIRCRAFT WAS DEPARTING WHEN THE CREW EXPERIENCED AN APU FIRE INDICATION. THEY FOLLOWED PROCEDURES INCLUDING DISCHARGING THE EXTINGUISHER BOTTLE THEN R
- [SDR CA010322012](https://openairdocs.org/sdr/CA010322012), Mar 17, 2001: COMPRESSOR. MAKING METAL. (CAN) THE AIRCRAFT WAS CLIMBING OUT OF VANCOUVER WHEN THE APU DID AN AUTO SHUT DOWN AND THE APU FIRE HANDLE ILLUMINATED. THE FIRE HANDLE WAS PULLED BUT THE BOTT
- [SDR CA010129013](https://openairdocs.org/sdr/CA010129013), Dec 17, 2000: TRANSMITTER. FAILED. (CAN) ON CLIMB ENGINE OIL PRESSURE WAS NOTICED TO DROP TO 41 PSI AND DID NOT RESPOND TO THROTTLE MOVEMENT. THE FLIGHT CREW ELECTED TO RETURN WHERE MAINTENANCE R
- [SDR CA001122029](https://openairdocs.org/sdr/CA001122029), Nov 14, 2000: FIRE LOOP. CHAFED. (CAN) APU FIRE WARNING IN CRUISE, APU FIRE HANDLED & WARNING CEASED, BOTTLE DISCHARGED. AIRCRAFT CARRIED OUT A NORMAL LANDING. MAINTENANCE INSPECTED APU & AREA 
- [SDR CA001016008](https://openairdocs.org/sdr/CA001016008), Sep 22, 2000: STATOR. CRACKED. (CAN) DURING A SCHEDULED C-2 FAN CHANGE ON WING THE 2ND STAGE STATOR WAS FOUND COMPLETELY CRACKED THROUGH A ONE BLADE LOCATION, INBOARD OF THE MID SPAN SHROUD. 
- [SDR CA000905017](https://openairdocs.org/sdr/CA000905017), Aug 28, 2000: FAN BLADE. BIRD STRIKE. (CAN) ON ROTATION AT TAKEOFF CREW REPORTED THEY HEARD A BANG & FELT THE AIRCRAFT YAW TO THE RIGHT. THE CREWFLEW AROUND TO REDUCE THE FUEL LOAD AND RETURNED TO T
- [SDR CA000905016](https://openairdocs.org/sdr/CA000905016), Aug 18, 2000: BLEED VALVE. FAILED. (CAN) ON TWO OCCASIONS, THE CREW EXPERIENCED A FIRE INDICATION ON THE APU WHILE THE AIRCRAFT WAS AT CRUISING ALTITUDE. ON BOTH OCCASIONS, THE APU SHUT DOWN AND 
- [SDR CA000804016](https://openairdocs.org/sdr/CA000804016), Jul 22, 2000: MOTOR. SEIZED. (CAN) DURING THE CLIMB FROM 4XS (SASKATOON) THE CREW BECAME AWARE OF A STRANGE ODOR / SMELL IN THE CABIN. THERE WAS NO SMOKE OBSERVED BUT THE CREW ELECTED TO RE
- [SDR CA000511009](https://openairdocs.org/sdr/CA000511009), Apr 26, 2000: ATTACH FITTING. BROKEN. (CAN) ON APPROACH WHEN LANDING GEAR LOWERED CREW REPORTED A BANGING NOISE FROM THE AREA OF THE NOSE. INSPECTION AT THE GATE FOUND THE TAXI LIGHT SUPPORT HAD BRO
- [SDR CA000128017](https://openairdocs.org/sdr/CA000128017), Jan 23, 2000: GEARBOX. LEAKING. (CAN) OIL FILTER BYPASS SW BANJO FITTING HAD STRIPPED THREADS CAUSING OIL LEAK.
- [SDR AU000128017](https://openairdocs.org/sdr/AU000128017), Jan 23, 2000: OIL FILTER. LEAKING. (AU) OIL FILTER BYPASS SW BANJO FITTING HAD STRIPPED THREADS CAUSING OIL LEAK.
- [SDR P2EA99354](https://openairdocs.org/sdr/P2EA99354), Dec 3, 1999: FLOORBEAM. CORRODED. SJO - C-CHECK, FLOORBEAM WEB CORRODED AT BS 259.5, FROM WL 208.5 TO WL 206, BETWEEN LBL 13 INCH TO RBL 13 INCH. DEFECT SIZE, LENGTH 16 INCHES, WIDTH 5 INCHES. R
- [SDR P2EA99351](https://openairdocs.org/sdr/P2EA99351), Dec 3, 1999: FLOORBEAM. CORRODED. SJO - C-CHECK, FLOORBEAM CORROSION AT BS 259.5, WL 208.5, BETWEEN LBL 20 AND RBL 15 INCHES. DEFECT SIZE, LENGTH 14 INCHES, WIDTH 4 INCHES. REPAIRED FLOORBEAM AN
- [SDR P2EA99350](https://openairdocs.org/sdr/P2EA99350), Dec 3, 1999: ANGLE. CORRODED. SJO - C-CHECK, FLOOR SUPPORT ANGLE CORRODED AT BS 270, WL 208.5, BETWEEN RBL 17 INCHE LBL 10 INCH. DEFECT SIZE, LENGTH 10 INCH, WIDTH 2 INCH. REPAIRED FLOOR SUP
- [SDR P2EA99342](https://openairdocs.org/sdr/P2EA99342), Dec 3, 1999: SKIN. DELAMINATED. SJO - C-CHECK, LEFT AC BAY DOOR DELAMINATED. REPAIRED LEFT AC BAY DOOR PER EO COO-CMP-3-53-704-99 DATED DECEMBER 4, 1999. (M)
- [SDR P2EA99335](https://openairdocs.org/sdr/P2EA99335), Dec 2, 1999: BULKHEAD. CRACKED. SJO - C-CHECK, WEB CRACKED AT BS 178, LBL 10 INCHES, WL 235. DEFECT SIZE, LENGTH .375 INCH. REPAIRED BULKHEAD WEB AT BS 178 FROM LBL 7 TO LBL 17.5, BETWEEN WL 2
- [SDR P2EA99352](https://openairdocs.org/sdr/P2EA99352), Dec 1, 1999: RIB. CRACKED. SJO - C-CHECK ITEM, SUPPORT RIB CRACKED AT RT WING SLAT STATION 25. DEFECT SIZE, LENGTH .75 INCH. REPLACED SLAT TRACK SUPPORT RIB AT SLAT STATION 25 PER SRM 51-
- [SDR P2EA99345](https://openairdocs.org/sdr/P2EA99345), Dec 1, 1999: SKIN. DENTED. SJO - C-CHECK, E/E DOOR HAS A DENT OUT OF LIMITS, DEFECT SIZE, LENGTH 1.75 INCH, WIDTH 1.5 INCH, DEPTH .045 INCH. REPLACED DOOR SKIN PER SRM 51-10-1, PAGE 5 AND
- [SDR P2EA99355](https://openairdocs.org/sdr/P2EA99355), Nov 30, 1999: SKIN. CRACKED. SJO - C-CHECK, FUSELAGE SKIN CRACKED FROM BS 727 TO BS 727A BETWEEN STRINGER 14 RT AND 16 RT. DEFECT SIZE LENGTH 1.75 INCH. REPAIRED FUSELAGE SKIN SECTION FROM 
- [SDR P2EA99336](https://openairdocs.org/sdr/P2EA99336), Nov 30, 1999: SKIN. CRACKED. SJO - C-CHECK, FUSELAGE SKIN CRACKED FROM BS 268 TO BS 277, BETWEEN STRINGER 15 RT AND 16 RT. DEFECT SIZE 1 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 263.5 T
- [SDR P2EA99311](https://openairdocs.org/sdr/P2EA99311), Nov 12, 1999: TRANSMITTER. INOPERATIVE. FLT 588 - MCI - ABORTED TAKEOFF, NO EMERGENCY DECLARED. DURING TAKEOFF ROLL, NR 2 EPR GAUGE READS ZERO. REPLACED NR 2 EPR TRANSMITTER AND NR 2 EPR INDICATOR PER
- [SDR P2EA99253](https://openairdocs.org/sdr/P2EA99253), Oct 5, 1999: SKIN. CRACKED. SJO - C-CHECK, LEFT RAM DOOR INNER SKIN CRACKED, DEFECT SIZE, LENGTH 3 INCHES AND WIDTH 1 INCH. REPAIRED RAM DOOR INTERNAL SKIN PER COOPESA EO COO-3-52-708-99 D
- [SDR P2EA99220](https://openairdocs.org/sdr/P2EA99220), Jul 20, 1999: DOOR. MISSING. NSP - FLT 707 - THIS IS A SUPPLEMENTAL/CLOSING ACTION FOR MRR 99220. ON WALK-AROUND INSPECTION AFTER FLIGHT MAINTENANCE, CREW DISCOVERED THE CENTER BOOST PUMP D
- [SDR P2EA99195](https://openairdocs.org/sdr/P2EA99195), May 25, 1999: PUMP. LEAKING. PIT - FLT 588 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. TOTAL LOSS OF SYSTEM 'A' HYDRAULICS. FOUND NR 2 ENGINE SYSTEM 'A' HDYRAULIC PUMP SHAFT SEAL BLOWN. RE
- [SDR CA990603008](https://openairdocs.org/sdr/CA990603008), May 11, 1999: CONTROL ROD. CRACKED. (CAN) DURING INSPECTION, THE THRUST REVERSER FOLLOW-UP CONTROL ROD FORWARD ROD END BEARING WAS FOUND ADRIFT, FURTHER INSPECTION FOUND THE ROD END WAS CRACKED AN
- [SDR P2EA99090](https://openairdocs.org/sdr/P2EA99090), Mar 12, 1999: MECHANISM. WORN. MCI - FLT 819 - RETRACTING FLAPS FROM 5 TO 1 DEGREE OUT OF MDW, FELT HEAVY FLUTTER. GOING FROM FLAPS 1 TO 5 ON LANDING AT MCI FELT MINOR FLUTTER. LANDING AT MCI
- [SDR P2EA99001](https://openairdocs.org/sdr/P2EA99001), Jan 7, 1999: VALVE. FAILED. MSP - FLT 404 - DURAL BLEED INDICATION DURING TAKEOFF. ABORTED TAKEOFF AT 70 KNOTS, RETURNED TO GATE. DEFERRED PER MEL 36-6, CI M219725 ASSIGNED. FEF CI M219725
- [SDR P2EA98312](https://openairdocs.org/sdr/P2EA98312), Dec 26, 1998: WINDOW. CRACKED. MCI - FLT 586 - THE AIRCRAFT DEPARTED MCI AND 35 MINUTES INTO FLIGHT THE FIRST OFFICERS SLIDING WINDOW CRACKED. THE AIRCRAFT RETURNED TO MCI WITHOUT INCIDENT. M
- [SDR P2EA98311](https://openairdocs.org/sdr/P2EA98311), Dec 15, 1998: SKIN. CRACKED. SJO - NR 1 THRUST REVERSER LOWER BUCKET EXTERNAL SKIN CRACKED, DEFECT SIZE LENGTH 2.75 INCH. REPAIRED THRUST REVERSER PER COOPESA EO COO-3-78-754-98 DATED DEC 1
- [SDR P2EA98305](https://openairdocs.org/sdr/P2EA98305), Dec 8, 1998: SKIN. DAMAGED. SJO - PROVISIONAL REPAIR AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED FUSELAGE SKIN SECTION FROM BS 299 TO BS 305 BETWEEN STRINGER 12 RT AND STRINGER 14 R
- [SDR P2EA98296](https://openairdocs.org/sdr/P2EA98296), Dec 1, 1998: SLAT. DELAMINATED. SJO - NR 5 SLAT DELAMINATED, DEFECT SIZE TOTAL 400 SQ INCH. REPAIRED NR 5 SLAT PER COOPESA EO COO-3-57-719-98 DATED DEC 2, 1998. DOCUMENTED ON FAA FORM 8110-3. 
- [SDR P2EA98307](https://openairdocs.org/sdr/P2EA98307), Nov 27, 1998: SKIN. DELAMINATED. SJO - NR 5 SPOILER DELAMINATED, DEFECT SIZE TOTAL 234 SQUARE INCH. REPAIRED NR 5 SPOILER PER COOPESA EO C00-3-57-709-98 DATED NOV 30, 1998. (M)

All 120: https://openairdocs.org/model/boeing-737-281/reports.md

## STCs that may be installed (OpenAirDocs) (642, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST03438NY](https://openairdocs.org/stc/ST03438NY): Installation of Adams Rite Lavatory Equipment. Delta Engineering Corporation
- [STC ST02269NY](https://openairdocs.org/stc/ST02269NY): Installation of Self Illuminating Floor Path Marking System. Lufthansa Technik AG
- [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 ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST00555AT](https://openairdocs.org/stc/ST00555AT): Installation of Airshow 210 system. AIRCRAFT RECONFIG TECHNOLOGIES, LLC. Lists 737 Series
- [STC ST02193AT-D](https://openairdocs.org/stc/ST02193AT-D): Installation of Collins 5 ATI EHSI System. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02272AT-D](https://openairdocs.org/stc/ST02272AT-D): Installation of a Position Light Power Control. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [STC ST02626AT-D](https://openairdocs.org/stc/ST02626AT-D): Installation of a Cabin Divider. AIRCRAFT RECONFIG TECHNOLOGIES, LLC
- [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 ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST03363AT](https://openairdocs.org/stc/ST03363AT): Installation of a single Universal Avionics Class "A" TAWS system. ARC145 LLC
- [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF
- [STC SA2542WE](https://openairdocs.org/stc/SA2542WE): Installation of wing-tip mounted logo lights. The Boeing Company
- [STC ST09191AC](https://openairdocs.org/stc/ST09191AC): Installation of DeVore wing fwd position light assembly. (737 ALL). The Boeing Company
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC SA1188NW](https://openairdocs.org/stc/SA1188NW): Installation of Spacemaker II interior conversion kit. Safran Cabin Inc
- [STC SA1971NM](https://openairdocs.org/stc/SA1971NM): Installation of coat closet/class divider/closet units. Safran Cabin Inc
- [STC SA2077NM](https://openairdocs.org/stc/SA2077NM): Install overhead storage Quikbin retrofit kits. Safran Cabin Inc
- [STC SA2366NM](https://openairdocs.org/stc/SA2366NM): Installation of Spacemaker II interior retrofit kit. Safran Cabin Inc
- [STC SA3133NM](https://openairdocs.org/stc/SA3133NM): Installation of Windscreen Stowage Unit. Safran Cabin Inc
- [STC SA3456NM](https://openairdocs.org/stc/SA3456NM): Installation of cabin divider. Safran Cabin Inc
- [STC SA3493NM](https://openairdocs.org/stc/SA3493NM): Installation of windscreen and coatroom. Safran Cabin Inc
- [STC SA3652NM](https://openairdocs.org/stc/SA3652NM): Installation of overhead bins, 'Carry-All Extension Kit'. Safran Cabin Inc
- [STC SA3936NM](https://openairdocs.org/stc/SA3936NM): Installation of Header and Cabin Divider. Safran Cabin Inc
- [STC SA4783NM](https://openairdocs.org/stc/SA4783NM): Installation of a modular lavatory(retrofit installation). Safran Cabin Inc
- [STC SA5532NM](https://openairdocs.org/stc/SA5532NM): Installation of stowage unit. Safran Cabin Inc
- [STC SA883NW](https://openairdocs.org/stc/SA883NW): Installation of the Mark I interior conversion kit. Safran Cabin Inc
- [STC ST00030SE](https://openairdocs.org/stc/ST00030SE): Installation of SpaceMaker II interior. Safran Cabin Inc
- [STC ST00035LB](https://openairdocs.org/stc/ST00035LB): Installation of galley modules. Safran Cabin Inc
- [STC ST00062LA](https://openairdocs.org/stc/ST00062LA): Installation of galley modules and stowage units. Safran Cabin Inc
- [STC ST00351SE](https://openairdocs.org/stc/ST00351SE): Installation of SpaceMaker I interior modular kit. Safran Cabin Inc
- [STC ST00683LA](https://openairdocs.org/stc/ST00683LA): Installation of a FWD R/H Coat Closet. Safran Cabin Inc
- [STC ST01066LA](https://openairdocs.org/stc/ST01066LA): Installation of a R/H windscreen. Safran Cabin Inc
- [STC ST01335LA](https://openairdocs.org/stc/ST01335LA): Installation of a reinforced cockpit door. Safran Cabin Inc
- [STC ST02178LA](https://openairdocs.org/stc/ST02178LA): Installation of a windscreen. Safran Cabin Inc
- [STC ST03381NY](https://openairdocs.org/stc/ST03381NY): Installation of Apple iPad EFB Provisions. Avionics Design Services Ltd
- [STC SA3140NM](https://openairdocs.org/stc/SA3140NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc
- [STC ST01738AT](https://openairdocs.org/stc/ST01738AT): Installation of additional sensors (from 11 to 18) for recording additional parameters on Digital Flight Data Recorders (DFDR) manufactured by L-3 Com (formerly Loral/Fairchild) and Allied Signal. Acron Aviation Inc
- [STC SA1097NW](https://openairdocs.org/stc/SA1097NW): Installation of Winters AirStair at the aft passenger entrance. Dow Aero LLC
- [STC ST00840CH](https://openairdocs.org/stc/ST00840CH): Installation of Single and Dual Honeywell HT-9100 GNSS GPS Navigation Systems with provisions for Single or Dual DME. Amphenol Cable and Interconnect Technologies Inc
- [STC ST01060CH](https://openairdocs.org/stc/ST01060CH): Installation of GPS antenna provisions. Amphenol Cable and Interconnect Technologies Inc
- [STC ST01798CH](https://openairdocs.org/stc/ST01798CH): Installation of a Honeywell Enhanced Ground Proximity Warning System per Electronic Cable Specialists Master Data List ECS-201532 latest FAA approved revision. Amphenol Cable and Interconnect Technologies, Inc
- [STC ST01118CH](https://openairdocs.org/stc/ST01118CH): Installatin of an Electronic Cable Specialist Laptop Stowage/Charger Assembly (Class 1 Electronic Flight Bag provisions). Amphenol Cable and Interconnect Technologies, Inc
- [STC ST02637CH](https://openairdocs.org/stc/ST02637CH): Installation of ECS EZMount® mechanical mounting assemblies. Amphenol Cable and Interconnect Technologies Inc
- [STC ST11887IB](https://openairdocs.org/stc/ST11887IB): Installation of Dual Universal Avionics EFI-890R Advanced Flight Display System. Mid Canada Mod Center
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST01804LA](https://openairdocs.org/stc/ST01804LA): Installation of Lower Cargo Smoke Detection and Fire Suppression System. Aero Technik Inc

All 642: https://openairdocs.org/model/boeing-737-281/stcs.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Boeing 737-205](https://openairdocs.org/model/boeing-737-205): 3 registered aircraft, registry code 1384456
- [Boeing 737-200](https://openairdocs.org/model/boeing-737-200): 1 registered aircraft, registry code 1384451
- [Boeing 737-201](https://openairdocs.org/model/boeing-737-201): 1 registered aircraft, registry code 1384454
- [Boeing 737-209](https://openairdocs.org/model/boeing-737-209): 1 registered aircraft, registry code 13844AE
- [Boeing 737-230](https://openairdocs.org/model/boeing-737-230): 0 registered aircraft, registry code 1384401
- [Boeing 737-248](https://openairdocs.org/model/boeing-737-248): 0 registered aircraft, registry code 1384402
- [Boeing 737-204](https://openairdocs.org/model/boeing-737-204): 0 registered aircraft, registry code 1384458
- [Boeing 737-212](https://openairdocs.org/model/boeing-737-212): 0 registered aircraft, registry code 1384461
- [Boeing 737-217](https://openairdocs.org/model/boeing-737-217): 0 registered aircraft, registry code 1384464
- [Boeing 737-266](https://openairdocs.org/model/boeing-737-266): 0 registered aircraft, registry code 1384466
- [Boeing 737-219](https://openairdocs.org/model/boeing-737-219): 0 registered aircraft, registry code 1384469
- [Boeing 737-214](https://openairdocs.org/model/boeing-737-214): 0 registered aircraft, registry code 138446R

---
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.