# Boeing 737-296

- Type: Aircraft model (FAA registry)
- Registry code: 1384486
- Manufacturer (registry): BOEING
- Model: 737-296
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 124
- Weight class: 20,000 lb and over
- 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-737-296

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-737-296/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 (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 19931018045489I](https://openairdocs.org/incident/19931018045489I), Oct 18, 1993: Boeing 737201 (N238US), Washington, DC. NR1 engine failed on climbout. Returned. Found the turbine had failed.

## Service difficulty reports (60, newest 50)

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

- [SDR CA050125007](https://openairdocs.org/sdr/CA050125007), Jan 21, 2005: SKIN. CRACKED. (CAN) AN OUTER FUSELAGE CRACK WAS FOUND DURING A PHASE EIGHT CHECK AT STRINGER 16L, STATION 727+14.5 APPROXIMATELY 1.5 INCHES IN LENGTH. FUSELAGE CRACK REPAIRED
- [SDR CA041201004](https://openairdocs.org/sdr/CA041201004), Nov 29, 2003: SKIN. CRACKED. (CAN) TWO INCH CRACK WAS FOUND ON OUTER FUSELAGE BETWEEN STA 727A, 727B AT STR. 16L. FUSELAGE CRACK REPAIRED IAW SRM 53-30-3 FIG.48 SHEET 34 DETAIL XII. TIMES- 
- [SDR CA031117003](https://openairdocs.org/sdr/CA031117003), Nov 11, 2003: SKIN. CRACKED. (CAN) 2.34 CRACK IN FUSELAGE TOP OF S18L BETWEEN BS 727A AND BS 727B. REPAIRED IAW SRM 53-30-3,FIG 48, SHEET 33, DETAIL XI REFERENCE PROCEDURE IV AND VII. AIRCR
- [SDR CA031117002](https://openairdocs.org/sdr/CA031117002), Nov 11, 2003: SKIN. CRACKED. (CAN) 3 INCH CRACK IN FUSELAGE SKIN AFT OF REAR WING TO BODY FAIRING TOP OF 18L BETWEEN BS 747 - BS 767. REPAIRED SRM IAW 53-30-3 FIG 48 (SHEET 33) DETAIL XI, R
- [SDR CA021018004](https://openairdocs.org/sdr/CA021018004), Oct 17, 2002: SKIN. CRACKED. (CAN) TWO INCH CRACK FOUND ON FUSELAGE SKIN ABOVE STRINGER 16 LT, AT BODY STATION 787. CRACK REPAIR CARRIED OUT IAW SRM 53-30-3.
- [SDR CA020702005](https://openairdocs.org/sdr/CA020702005), Jun 29, 2002: ENGINE. LEAKING. (CAN) NR 2 ENGINE HAD REPORT LOW OIL QUANTITY ON ARRIVAL. MAINTENANCE SERVICED ENGINE WITH 11 LITRES. OIL TRENDS DID NOT INDICATE HIGH CONSUMPTION. RAN ENGINE A
- [SDR CA020730007](https://openairdocs.org/sdr/CA020730007), Jun 27, 2002: SKIN. CRACKED. (CAN) TWO FATIGUE CRACKS FOUND IN RT FUSELAGE SKIN BETWEEN STA. 727A & 727B AND BETWEEN STR 14R & 19R ABOVE EXISTING REPAIR AT SAME LOCATION. ONE CRACK IS HORIZ
- [SDR CA010727027](https://openairdocs.org/sdr/CA010727027), Jul 5, 2001: CLAMP. (CAN) HYDRAULIC LOSS OF SYSTEM A AFTER TAKE OFF, AIRCRAFT RETURNED. BROKEN CLAMP ON THE RETURN FILTER BOWL. NEW CLAMP INSTALLED, AND FILTER ELEMENT CHANGED.
- [SDR 2001F00149](https://openairdocs.org/sdr/2001F00149), Jul 5, 2001: ENGINE. DAMAGED. SAL - FLT TA220 - DURING INITIAL TAKEOFF, A STRONG NOISE WAS HEARD, WHEN APPLYING TAKEOFF TRUST, REJECTED THE TAKEOFF AND STRONG VIBRATION WAS FELT IN THE NR 2 
- [SDR CA010703002](https://openairdocs.org/sdr/CA010703002), Jun 11, 2001: SKIN. CRACKED. (CAN) CRACK IN FUSELAGE SKIN LEFT SIDE BETWEEN FUSELAGE STATIONS 747 AND 767, STRINGER 17L REPAIRED AS PER SRM 53-30-3, TABLE 1, METHOD 1, PAGES 87,88 & 88A.
- [SDR CA010625004](https://openairdocs.org/sdr/CA010625004), Jun 11, 2001: SKIN. CRACKED. (CAN) CRACK IN FUSELAGE SKIN LEFT SIDE, BETWEEN FUSELAGE STATIONS 747 AND 767, STRINGER 17L. REPAIRED AS PER SRM 53-30-3, TABLE 1, METHOD 1, PAGES 87,88 & 88A.
- [SDR 2001F00081](https://openairdocs.org/sdr/2001F00081), Apr 16, 2001: HOSE. LEAKING. FLT 410 - SAL - DURING CLIMB, THE CAPTAIN REPORTED THAT DURING INITIAL CLIMB THERE WAS A DIFFERENCE OF 100 FEET BETWEEN CAPTAIN AND FIRST OFFICER ALTIMETER, AT 
- [SDR CA010502004](https://openairdocs.org/sdr/CA010502004), Apr 5, 2001: MODULE. DEFECTIVE. (CAN) AS THE POWER LEVERS WERE ADVANCED FOR TAKEOFF AT 1.2 EPR A WARNING HORN SOUNDED. THE TAKEOFF WAS REJECTED AND THE AIRCRAFT PROCEEDED BACK TO THE GATE WITH
- [SDR CA010105005](https://openairdocs.org/sdr/CA010105005), Dec 21, 2000: BUSHING. DAMAGED. (CAN) A/C 732, NR 2 ENGINE SHUT DOWN DUE LOW OIL QUANTITY AND PRESSURE WARNING. FOUND BUSHING BANJO PULLED OUT FROM GEARBOX HOUSING. THREAD FAILURE CONFIRMED. W
- [SDR CA010119003](https://openairdocs.org/sdr/CA010119003), Dec 17, 2000: FITTING. BROKEN. (CAN) DURING INSPECTION THE LEFT OUTBOARD FORE FLAP ATTACHMENT BRACKET WAS FOUND CRACKED.
- [SDR 20001212SH001](https://openairdocs.org/sdr/20001212SH001), Nov 26, 2000: LINE. DAMAGED. SAL - FLT TA-380 - AFTER TAKEOFF, THE FIRST OFFICER AIRSPEED INDICATOR WENT TO ZERO KNOTS AND FIRST OFFICER''S ALTIMETER HAD A READ-OUT OF 4,000 FEET AT FL 260.
- [SDR CA001201005](https://openairdocs.org/sdr/CA001201005), Nov 12, 2000: INDICATOR. INACCURATE. (CAN) LOG SEQUENCE 0154872. APPROXIMATELY 20 MINUTES FROM LANDING FUEL QUANTITY INDICATORS SHOWED 3000 POUND IMBALANCE. SUSPECTED A FUEL LEAK AND DECLARED AN EM
- [SDR CA001107021](https://openairdocs.org/sdr/CA001107021), Oct 17, 2000: CONTROLLER. FAILED. (CAN) CAPTAINS NR 2 SLIDING WINDOW - EXTERIOR PANE SHATTERED ON CLIMB OUT. WINDOW HEAT SHORTED RESULTING IN SPARKS AND SMOKE FROM ARCING.WINDOW AND CONTROLLER R
- [SDR CA001122003](https://openairdocs.org/sdr/CA001122003), Sep 20, 2000: CONTROL UNIT. FAILED. (CAN) EN ROUTE CREW REPORTED AILERONS WERE STIFF, BEYOND 5 DEGREES INPUT WITH AUTOPILOT SELECTED OFF. AUTOPILOT ON AILERONS WERE BETTER. AIRCRAFT TAKEN OUT OF S
- [SDR CA000901004](https://openairdocs.org/sdr/CA000901004), Aug 15, 2000: ENGINE. OVERTEMP. (CAN) AC 734, AUGUST 15/2000, YYZ, LOG SEQUENCE 0295891. AIR TURNBACK DUE NR 2 ENGINE EGT AT 520 DEGREES AFTER CLIMB. ON TAKEOFF, NR 2 EGT APPROACHED 590 DEGREE
- [SDR 20001004AP002](https://openairdocs.org/sdr/20001004AP002), Jun 23, 2000: CONTROL BOX. INOPERATIVE. SAL-MIA - FLT TA314 - DURING CRUISE, THE AIRCRAFT HAD PITCH OSCILLATIONS WITH AUTOPILOT ENGATED, DUE THIS SITUATION THE AIRCRAFT RETURNED TO SAL AIRPORT. AFTER 
- [SDR CA000224015](https://openairdocs.org/sdr/CA000224015), Feb 15, 2000: SHAFT. BINDING. (CAN) START LEVER STIFF AND SPONGY. FOUND ENGINE CROSS SHAFT BINDING. INNER AND OUTER CROSS SHAFT REPLACED.
- [SDR USAA000161](https://openairdocs.org/sdr/USAA000161), Feb 7, 2000: SKIN. CRACKED. CLT - FOUND 2 CRACKS 1.75 INCH AND 1.5 INCH, LEFT FUSELAGE SKIN STATION 759 AND 781 AT STRINGER 17L. REPAIRED WITH DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA000162](https://openairdocs.org/sdr/USAA000162), Feb 7, 2000: SKIN. CRACKED. CLT - FOUND 1 INCH SKIN CRACK LEFT FUSE SKIN BETWEEN STATION 763 AND 764, STRINGER 19L. REPAIRED DOUBLER PER SRM 53-30-3. (M)
- [SDR USAA991262](https://openairdocs.org/sdr/USAA991262), Nov 13, 1999: SKIN. CRACKED. TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A SECTION OF SKIN REMOVED TO GAIN ACCESS TO AFT PRESSURE BULKHEAD SKIN. INSTALLED DOUBLER PER BOEING DWG 65C281
- [SDR USAA991261](https://openairdocs.org/sdr/USAA991261), Nov 13, 1999: BULKHEAD. CORRODED. TPA - DURIGN CX-2 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA AFT PRESSURE BULKHEAD STATION 1016, LOWER CENTER FUSELAGE WEB AND STIFFENERS, CORROSION LEVEL 2
- [SDR USAA991248](https://openairdocs.org/sdr/USAA991248), Nov 13, 1999: SKIN. CRACKED. TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH SKIN CRACK STATION 1156 BETWEEN STRINGER 2L AND 3L. INSTALLED DOUBLER PER SB 737-53-1095. (M)
- [SDR USAA990867](https://openairdocs.org/sdr/USAA990867), Aug 12, 1999: AILERON. MISSING. PIT - DURING FLIGHT THERE WAS A VIBRATION AND A PASSENGER NOTICED A PORTION OF THE RIGHT AILERON OUTBOARD END TRAILING EDGE COMING OFF OF AIRCRAFT. REPAIRED PER
- [SDR USAA990861](https://openairdocs.org/sdr/USAA990861), Aug 2, 1999: SKIN. CRACKED. BOS - DURING RON, FOUND 1.25 INCH CRACK IN SKIN AT STRINGER 16L STATION 767. INSTALLED DOUBLER .080/2024T42 FASTENER 20426D5 PER SRM 53-30-3 FIG 6. (M)
- [SDR USAA990469](https://openairdocs.org/sdr/USAA990469), May 17, 1999: SKIN. CRACKED. CLT - DURING UNSCHEDULED MAINTENANCE, FOUND 2.75 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT STRINGER 17R, 5 INCHES FORWARD OF STATION 727B FRAME. REMOVED DAMA
- [SDR USAA990468](https://openairdocs.org/sdr/USAA990468), May 17, 1999: SKIN. CRACKED. CLT - DURING UNSCHEDULED MAINTENANCE, FOUND 1 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT S18R, 2 INCH FORWARD OF STATION 727B FRAME. CRACK CUT OUT, INSTALLED 
- [SDR USAA990467](https://openairdocs.org/sdr/USAA990467), May 17, 1999: SKIN. CRACKED. CLT - DURING UNSCHEDULED MAINTENANCE, FOUND 1.9 INCH LONG CRACK ON FUSELAGE EXTERIOR SKIN AT S17R, 5 INCH FORWARD OF STATION 747 FRAME. INSTALLED DOUBLER PER SR
- [SDR 20000424AP011](https://openairdocs.org/sdr/20000424AP011), Mar 19, 1999: FIRE DETECTOR. MALFUNCTIONED. CUN - FLT TA410 - ENGINE NR 2 OVERHEAT LIGHT CAME ON, THEN FIRE WARNING LIGHT CAME ON, THE QRH PROCEDURES WERE ACCOMPLISHED BY THE CREW, DUE THIS SITUATION THE 
- [SDR 20000420AP003](https://openairdocs.org/sdr/20000420AP003), Mar 19, 1999: FIRE LOOP. DAMAGED. DURING FLIGHT TA410 (SAL-IAH) ENGINE NR 2 OVERHEAT LIGHT CAME ON, THEN FIRE WARNING LIGHT CAME ON, THE QRH PROCEDURES WERE ACCOMPLISHED BY THE CREW, DUE TO THIS
- [SDR USAA980564](https://openairdocs.org/sdr/USAA980564), Oct 30, 1998: FLOOR ANGLE. CORRODED. TPA - DURING C-1 CHECK VISUAL INSPECTION, FOUND ANGLE CORRODED AT LAV ATTACH POINT TO FLOOR AFT LAV ATTACH ANGLE FLOORBOARD. FABRICATED DOUBLER PER EA 62883. (M
- [SDR CA981125020](https://openairdocs.org/sdr/CA981125020), Oct 24, 1998: VALVE. MALFUNCTIONED. (CAN) RETURN TO GATE DUE THRUST REVERSER ISOLATION VALVE LIGHT ON AT ROTATION. VALVE REPLACED.
- [SDR CA980916023](https://openairdocs.org/sdr/CA980916023), Aug 25, 1998: CSD. MALFUNCTIONED. (CAN) NR 1 ENGINE GENERATOR AND CONSTANT SPEED DRIVE (CSD) WENT FULL VOLTS AND FREQUENCY. THE GENERATOR WAS TURNED OFF. VIBRATION WAS NOTICED, SO THE CSD WAS DI
- [SDR CA980707021](https://openairdocs.org/sdr/CA980707021), Jun 10, 1998: DOOR. CHAFED. (CAN) NOSE LANDING GEAR DOOR WORN ON INNER SURFACE. NO MENTION OF CLEARANCE CHECK IN AMM. DOOR REPLACED.
- [SDR USAA980167](https://openairdocs.org/sdr/USAA980167), Apr 20, 1998: SKIN. LIGHTNING STRIKE. ROA - DURING B-CHECK VISUAL INSPECTION, FOUND .75 INCH DAMAGED AREA (LIGHTNING STRIKE) AT BS 737-B STR 10, RT FUSELAGE SKIN. REMOVED DAMAGED AREA AND INSTALLED 
- [SDR USAA980166](https://openairdocs.org/sdr/USAA980166), Apr 20, 1998: SKIN. LIGHTNING STRIKE. ROA - DURING B-CHECK, VISUAL INSPECTION FOUND .50 INCH DAMAGED AREA (LIGHTNING STRIKE) BS 569, STR 7, RT FUSELAGE SKIN. REMOVED DAMAGED AREA, AND INSTALLED DOUB
- [SDR CA971216021](https://openairdocs.org/sdr/CA971216021), Mar 17, 1998: TRANSMITTER. FAILED. (CAN) AIR TURN BACK TO BLOCKS DUE TO STICK SHAKER STALL WARNING AT TAKEOFF. REPLACED FLAP POSITION TRANSMITTER.
- [SDR CA971113018](https://openairdocs.org/sdr/CA971113018), Oct 22, 1997: PUMP. WORN. (CAN) 5 PUMPS REPLACED IN LH AND RH CENTRE FUEL TANK DUE TO IMPELLER WEAR AT TIPS CAUSES LOW FLOW AND FUEL PRESSURE WARNING LIGHTS.
- [SDR CA970731003](https://openairdocs.org/sdr/CA970731003), Jul 21, 1997: SWITCH. INTERMITTENT. (CAN) HISTORY OF THRUST REVERSER ISOLATION LIGHT ON BRIEFLY AFTER TAKEOFF. ON NEXT FLIGHT ISOLATION LIGHT REMAINED ON.AIRCRAFT RETURNED. SWITCH S529 REPLACED.
- [SDR CA970626003](https://openairdocs.org/sdr/CA970626003), Jun 23, 1997: PLUG. LEAKING. (CAN) ON TAKEOFF ROLL A FLICKERING WARNING LIGHT WAS OBSERVED. THE TAKEOFF WAS ABORTED. MAINTENANCE FOUND THE MAGNETIC PLUG ON THE #2 ENGINE CONSTANT SPEED SPEE
- [SDR CA970618008](https://openairdocs.org/sdr/CA970618008), Jun 16, 1997: PUSH PULL ROD. THREADS WORN. (CAN) RH ELEVATOR TAB OUTER PUSH PULL ROD FOUND WITH EYE AND JAM NUT BACKED OFF. THREADED END OF ROD DESTROYED DUE TO VIBRATION OF EYE END. ROD AND TWO EYE ENDS
- [SDR USAASB97035](https://openairdocs.org/sdr/USAASB97035), Jan 28, 1997: BLEED VALVE. FAILED. MSP - FL 856 - AFTER TAKEOFF FROM MSP, THE NR 2 ENGINE EGT BEGAN TO RISE AND THE EPR STARTED TO DROP. DURING CLIMB, CAPTAIN HAD TO KEEP PULLING THE NR 2 THROTTL
- [SDR USAA970036](https://openairdocs.org/sdr/USAA970036), Jan 23, 1997: STRINGER. CORROSION. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION APPROXIMATELY 6 INCH IN LENGTH STRINGER 26L AT STATION 296. INSTALLED STRINGER REPAIR, REPAIRED PER SR
- [SDR USAA970035](https://openairdocs.org/sdr/USAA970035), Jan 23, 1997: STRINGER. CORROSION. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH STRINGER 25L AT STATION 305. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. COR
- [SDR USAA970034](https://openairdocs.org/sdr/USAA970034), Jan 23, 1997: SKIN. CRACKED. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 727 PLUS 16 STRINGER 15R SKIN. REMOVED EXISTING REPAIR, INSTALLED NEW REPAIR DOUBLER, REPAIRED P
- [SDR USAA970033](https://openairdocs.org/sdr/USAA970033), Jan 23, 1997: STRINGER. CORROSION. INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CORROSION BS 366 STRINGER 27L. INSTALLED STRINGER REPAIR, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C

All 60: https://openairdocs.org/model/boeing-737-296/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-737-296/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [CN0940-126](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195470018320261023152341.0001): Connecting Components fuel and old quantity systems 10-60479. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces 10-60479-126 · Oct 6, 2026
- [CN0940-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184070989720261023152340.0001): Connecting Components fuel and old quantity systems 10-60479. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces 10-60479-12 · Oct 6, 2026
- [BACC45FN16-24S6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107326955020261023152330.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN16-24S6 · Oct 1, 2026
- [BACC45FT12-3P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155878922920260930182547.0001): CONNECTORELECTRICAL, PLUG, THREADED COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT12-3P · Aug 28, 2026
- [BACC45FM14-7P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135686645620260930182802.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, THREADED COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FM14-7P · Aug 28, 2026
- [BACC45FT14C7S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199507869320260930182717.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14C7S · Aug 27, 2026
- [BACC45FT24-61S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186761362020260930182743.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT24-61S · Aug 27, 2026
- [BACC45FT14-7S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184013327720260930182709.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14-7S · Aug 27, 2026
- [BACC45FT22-55P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171501174220260930182735.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT22-55P · Aug 27, 2026
- [BACC45FT14-15P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165466197120260930182704.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14-15P · Aug 27, 2026
- [BACC45FT18-31P8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161525476620260930182729.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT18-31P8 · Aug 27, 2026
- [BACC45FT14A15S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153107963320260930182711.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14A15S · Aug 27, 2026
- [BACC45FT14-7P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148466137220260930182707.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14-7P · Aug 27, 2026
- [BACC45FT16A24S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146691485420260930182723.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT16A24S · Aug 27, 2026
- [BACC45FT18A14P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145731144020260930182733.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT18A14P · Aug 27, 2026
- [BACC45FT18-31P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145575888520260930182728.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT18-31P · Aug 27, 2026
- [BACC45FT16-24S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141666623420260930182720.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT16-24S · Aug 27, 2026
- [BACC45FT22C19P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137895329020260930182741.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT22C19P · Aug 27, 2026
- [BACC45FT24-43P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136970635420260930182742.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT24-43P · Aug 27, 2026
- [BACC45FT12D12S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136412214920260930182659.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT12D12S · Aug 27, 2026
- [BACC45FT14-15S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135401631720260930182705.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14-15S · Aug 27, 2026
- [BACC45FT16-24P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134808604120260930182719.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT16-24P · Aug 27, 2026
- [BACC45FT14C7P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126934506520260930182716.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14C7P · Aug 27, 2026
- [BACC45FT14-12S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123926255620260930182702.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14-12S · Aug 27, 2026
- [BACC45FT22-55S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121937758820260930182739.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT22-55S · Aug 27, 2026
- [BACC45FT14-12P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121847286720260930182701.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT14-12P · Aug 27, 2026
- [BACC45FT16C24P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107257413020260930182726.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT16C24P · Aug 27, 2026
- [69-38947EV-21](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136065364220260930205555.0001): Yoke Clip. EVCO, LLC · PMA PQ00044CB · Replaces 69-38947-21 · Aug 12, 2026
- [AR90128-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135733898020260909151857.0001): Water HeaterAssembly. Adams Rite Aerospace Inc · PMA PQ1155NM · Replaces ModificationArticle · Aug 12, 2026
- [69-38947EV-21](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105135663220260930205555.0001): Yoke Clip. EVCO, LLC · PMA PQ00044CB · Replaces 69-38947-13 · Aug 12, 2026
- [M10004-904](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149735087420261008200309.0001): O-Ring. Ametek Ameron LLC d/b/a Mass Systems · PMA PQ1432NM · Replaces 10004-904 · Aug 6, 2026
- [P/N 10-60552-5 (90G97)](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181023003720260728151343.0001): Pressure Switches. Custom Control Sensors, LLC · PMA PQ00077WB · Replaces P/N 10-60552-5 (90G97) · Jul 16, 2026
- [P/N 10-60552-1 (90G37)](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162270991520260728151342.0001): Pressure Switches. Custom Control Sensors, LLC · PMA PQ00077WB · Replaces P/N 10-60552-1 (90G37) · Jul 16, 2026
- [P/N 10-60552-11 (90G183)](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139345379120260728151342.0001): Pressure Switches. Custom Control Sensors, LLC · PMA PQ00077WB · Replaces P/N 10-60552-11 (90G183) · Jul 16, 2026
- [P/N 10-60552-31 (90G223)](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130839397920260728151342.0001): Pressure Switches. Custom Control Sensors, LLC · PMA PQ00077WB · Replaces P/N 10-60552-31 (90G223) · Jul 16, 2026
- [BACC45FT12-12S6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197910571520260826222401.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT12-12S6 · Jul 15, 2026
- [BACC45FN22-55P7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194446924520260826222344.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN22-55P7 · Jul 15, 2026
- [BACC45FN22-55P6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193033459820260826222343.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN22-55P6 · Jul 15, 2026
- [BACC45FT12-12S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190576214820260826222400.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT12-12S · Jul 15, 2026
- [BACC45FN22-19S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183841433220260826222339.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN22-19S · Jul 15, 2026
- [BACC45FN16-24S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182342286120260826222324.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN16-24S · Jul 15, 2026
- [BACC45FN16-10P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169591347020260826222318.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN16-10P · Jul 15, 2026
- [BACC45FN24B43P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168386460720260826222351.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN24B43P · Jul 15, 2026
- [BACC45FT10C5P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161094607620260826222356.0001): CONNECTOR, ELECTRICAL, PLUG, STRAIGHT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FT10C5P · Jul 15, 2026
- [BACC45FN20-25S](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157933263020260826222332.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN20-25S · Jul 15, 2026
- [BACC45FN16-24P7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154001420620260826222322.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN16-24P7 · Jul 15, 2026
- [BACC45FN22-55P9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152824894920260826222346.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN22-55P9 · Jul 15, 2026
- [BACC45FN18-31P](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151553927320260826222328.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN18-31P · Jul 15, 2026
- [BACC45FN16-24P6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145134619920260826222320.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN16-24P6 · Jul 15, 2026
- [BACC45FN22-55P8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141418831320260826222345.0001): CONNECTOR, ELECTRICAL, RECEPTACLE, FLANGE MOUNT, BAYONET COUPLING. Cinch Connectivity Solutions · PMA PQ0779SW · Replaces BACC45FN22-55P8 · Jul 15, 2026

All of them: https://openairdocs.org/model/boeing-737-296/pma.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.