# Boeing 737-130 - Type: Aircraft model (FAA registry) - Registry code: 1384435 - Manufacturer (registry): BOEING - Model: 737-130 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 100 - 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-737-130 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 2021-10-11](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 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 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 2019-10-03](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 2018-18-13](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 2018-10-12](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 - [AD 2017-20-12](https://openairdocs.org/ad/2017-20-12): Fuselage, Nacelles/Pylons, Stabilizers, and Wings · Boeing 737-100 Series, 737-200 Series and 737-200C Series. Effective Nov 16, 2017 - [AD 2017-17-04](https://openairdocs.org/ad/2017-17-04): Wings · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Sep 25, 2017 - [AD 2017-13-13](https://openairdocs.org/ad/2017-13-13): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Aug 9, 2017 - [AD 2017-12-05](https://openairdocs.org/ad/2017-12-05): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jul 25, 2017 - [AD 2017-11-01](https://openairdocs.org/ad/2017-11-01): Stabilizers · Boeing 737-100 Series, 737-200 Series and 737-200C Series. Effective Jun 27, 2017 - [AD 2017-04-08](https://openairdocs.org/ad/2017-04-08): Fuselage · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Apr 3, 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 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 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 2013-18-09](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 2010-15-08](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 2005-07-12](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 2004-03-34](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 2003-03-15](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 2002-05-07](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 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 2000-07-06](https://openairdocs.org/ad/2000-07-06) (historical): Forward Cargo Door · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective May 16, 2000 - [AD 99-21-15](https://openairdocs.org/ad/99-21-15) (historical): Fuel Boost Pump Wiring · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Nov 12, 1999 - [AD 99-08-23](https://openairdocs.org/ad/99-08-23) (historical): Aft Pressure Bulkhead · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective May 10, 1999 - [AD 99-05-15](https://openairdocs.org/ad/99-05-15) (historical): Attachment nuts of elevator tab push rod · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Mar 23, 1999 - [AD 99-05-12](https://openairdocs.org/ad/99-05-12) (historical): Center Fuel Tank · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Mar 18, 1999 - [AD 98-22-10](https://openairdocs.org/ad/98-22-10) (historical): Forward Service Door · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 6 more. Effective Nov 12, 1998 - [AD 98-02-01](https://openairdocs.org/ad/98-02-01) (historical): Yaw Damper System · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Feb 17, 1998 - [AD 97-17-01](https://openairdocs.org/ad/97-17-01) (historical): Main Wheel Assemblies · Boeing 737-100 Series and 737-200 Series. Effective Sep 16, 1997 - [AD 97-09-14](https://openairdocs.org/ad/97-09-14) (historical): Aileron and Elevator Power Control Unit · Boeing 737-100 Series, 737-200 Series, 737-200C Series and 3 more. Effective Jun 6, 1997 - [AD 96-17-04](https://openairdocs.org/ad/96-17-04) (historical): Kruegar Flap Actuator · Boeing 737-100 Series, 737-200 Series and 737-200C Series. Effective Sep 17, 1996 - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 - [AD 95-12-17](https://openairdocs.org/ad/95-12-17) (historical): Outboard Chords · Boeing 737-100 Series, 737-200 Series and 737-200C Series. Effective Aug 18, 1995 - [AD 95-04-01](https://openairdocs.org/ad/95-04-01) (historical): AFM - Limitations - Windshear · Boeing 727-100 Series, 727-200 Series, 737-100 Series and 54 more. Effective Mar 8, 1995 - [AD 91-09-14 R1](https://openairdocs.org/ad/91-09-14-R1) (historical): Engine Mount · Boeing 737-100 Series, 737-200 Series and 737-200C Series. Effective May 18, 1994 All 367: https://openairdocs.org/model/boeing-737-130/ads.md ## Information bulletins (advisory) (14) - [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 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-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-08-24](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 (4) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB IAD96IA044](https://openairdocs.org/ntsb/IAD96IA044), Feb 20, 1996: Boeing 737-130 (N33202), Washington, DC, incident, minor damage. Probable cause: excessive airspeed was maintained by the captain during the approach/landing phase of the flight, which resulted in an overrun and an encounter with soft/wet terrain. Factors relating to the incident… - [NTSB NYC93IA059](https://openairdocs.org/ntsb/NYC93IA059), Mar 15, 1993: Boeing 737-130 (N14212), Newark, NJ, incident, no damage. Probable cause: INADEQUATE MAINTENANCE/INSPECTION BY COMPANY MAINTENANCE PERSONNEL, THE MANUFACTURER'S INADEQUATE INSPECTION AND/OR REPLACEMENT PROCEDURES FOR THE AILERON CABLES, AND SUBSEQUENT FAILURE OF THE 'DOWN'… - [NTSB BFO93IA026](https://openairdocs.org/ntsb/BFO93IA026), Feb 13, 1993: Boeing 737-130 (N403PE), Portland, ME, incident, no damage. Probable cause: THE PILOT IN COMMAND'S EXCESSIVE AIRSPEED DURING APPROACH, AND HIS FAILURE TO FOLLOW THE PROPER BRAKING PROCEDURES DURING LANDING AS PER COMPANY TRAINING. FACTORS CONTRIBUTING TO THE ACCIDENT INCLUDE… - [NTSB NYC84IA225](https://openairdocs.org/ntsb/NYC84IA225), Jun 28, 1984: Boeing 737-130 (N417PE), Portland, ME, incident, minor damage ## FAA accident and incident reports (27) 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 19980625023199I](https://openairdocs.org/incident/19980625023199I), Jun 25, 1998: Boeing 737130 (N14209), Newark, NJ. Loss of powr and subsequent engine shutdown due to contained turbine blade failure. - [Incident 19971001045039I](https://openairdocs.org/incident/19971001045039I), Oct 1, 1997: Boeing 737130 (N77204), Newark, NJ. Moving 737 from hangar to gate crossed a hold line sans a clearance. An airecraft had to go around mechanic pilot. - [Incident 19970619020299I](https://openairdocs.org/incident/19970619020299I), Jun 19, 1997: Boeing 737130 (N14211), Chicago, IL, Minor damage. Taxiing for takeoff a fuel truck struck a wing. Slat assembly was replaced. Fuel truck driver fired. New training. - [Incident 19970428011279I](https://openairdocs.org/incident/19970428011279I), Apr 28, 1997: Boeing 737130 (N403PE), Roanoke, VA. Narrative: on 04-28-97, cala flight #1987, ewr-atl cruising at FL 310 experienced a #1 engine fire warning. The flight crew retarded the power lever and… - [Incident 19970220009379I](https://openairdocs.org/incident/19970220009379I), Feb 20, 1997: Boeing 737130 (N403PE), Cleveland, OH. Narrative: flight 640 ord-ewr. Crew shutdown #1 engine due to fire warning indication and diverted to Cleveland without incident. Continental Cleveland… - [Incident 19961109040409I](https://openairdocs.org/incident/19961109040409I), Nov 9, 1996: Boeing 737130 (N77204), Cleveland, OH. Narrative: hyd system "a" failure on approach when gear lowered. #4 slat actuator hyd line found broken. Replaced line acft rtn to suc. Removed & replaced #1 &… - [Incident 19960323007599I](https://openairdocs.org/incident/19960323007599I), Mar 23, 1996: Boeing 737100 (N44214), Buffalo, NY. Narrative: flight 1420 departed ewr at 20:35 enroute to buf while cruising at 23,000 MSL the "a" hydraulic system lost all hydraulic fluid quantity. Aircrft… - [Incident 19960220005189I](https://openairdocs.org/incident/19960220005189I), Feb 20, 1996: Boeing 737130 (N33202), Washington, DC, Minor damage. Narrative: on Tuesday, February 20, 1996, at approximately 1515 local time Continental airlines flight 1156, a Boeing 737, (N33202), arrived at Washington… - [Incident 19950712042899I](https://openairdocs.org/incident/19950712042899I), Jul 12, 1995: Boeing 737130 (N14212), Cleveland, OH. Narrative: coa 1639 was inbound to "cle" over "cxr" VOR. The pilot was issued a descent clearance to 7000, which he read back. Coa 1639 was also issued a… - [Incident 19950129001939I](https://openairdocs.org/incident/19950129001939I), Jan 29, 1995: Boeing 737130 (N16201), Buffalo, NY. Narrative: on January 29, 1995 on flight from newark, NJ to Buffalo, NY Continental flight 1458, a Boeing 737, N16201, was unable to stabilize pressurization… - [Incident 19941117040539I](https://openairdocs.org/incident/19941117040539I), Nov 17, 1994: Boeing 737130 (N16201), Buffalo, NY. Low oil light on. Shutdown. Landed destination. NR6 bearing oil scavage tube fractured. Ferried to cle for service. - [Incident 19930902038089I](https://openairdocs.org/incident/19930902038089I), Sep 2, 1993: Boeing 737130 (N24213), Kansas City, MO, Minor damage. NR1 engine low pressure hydraulic pump light on. Landed safely at destination. A system pressure line was ruptured. - [Incident 19930315011899I](https://openairdocs.org/incident/19930315011899I), Mar 15, 1993: Boeing 737130 (N14212), Newark, NJ. Partial loss of aileron control on climb. Returned. Landed safely. Found broken left aileron control cable. - [Incident 19921012045129I](https://openairdocs.org/incident/19921012045129I), Oct 12, 1992: Boeing 737130 (N77204), St Louis, MO, Minor damage. While taxiing into gate pilot struck baggage carts with left engine. - [Incident 19920610026509I](https://openairdocs.org/incident/19920610026509I), Jun 10, 1992: Boeing 737130 (N77215), Covington - Cin, OH. Lost a system hydraulic quanity on climb. Returned. Landed safely. Replaced left MLG uplock hydraulic line. - [Incident 19920408019039I](https://openairdocs.org/incident/19920408019039I), Apr 8, 1992: Boeing 737130 (N24213), Denver, CO. Rapid decompression en route. Oxygen masks deployed. Returned. NR1 engine sense line blown. Relief valves replaced. - [Incident 19910611035039I](https://openairdocs.org/incident/19910611035039I), Jun 11, 1991: Boeing 737130 (N77204), Rochester, NY. Landing gear down indicator light problem on approach. Landed safely. Left main gear light module had become loose. - [Incident 19901227056329I](https://openairdocs.org/incident/19901227056329I), Dec 27, 1990: Boeing 737130 (N20205), Syracuse, NY, Minor damage. As operator parked tug to hook on to towbar,tug went out of control pinning operator under nose of aircraft. - [Incident 19901116064769I](https://openairdocs.org/incident/19901116064769I), Nov 16, 1990: Boeing 737130 (N59207), Cleveland, OH. Lost a system hydraulic system. Landed safely. Lines were scuffed between engine and pylon area on NR1 engine. - [Incident 19900720035519I](https://openairdocs.org/incident/19900720035519I), Jul 20, 1990: Boeing 737130 (N14211), Pittsburgh, PA. NR1 system hydraulic low pressure light. Precautionary landing, NR1 engine hydraulic pump pressure line leaking. - [Incident 19900413031489I](https://openairdocs.org/incident/19900413031489I), Apr 13, 1990: Boeing 737130 (N403PE), Newark, NJ, Minor damage. Two seagulls injested in NR1 engine on climb. Returned. Landed safely. - [Incident 19881125063329I](https://openairdocs.org/incident/19881125063329I), Nov 25, 1988: Boeing 737130 (N416PE), Buffalo, NY. Lost cabin pressure. Diverted to Buffalo due to passenger medical problem. Forward cargo door seal loose. - [Incident 19870604082479I](https://openairdocs.org/incident/19870604082479I), Jun 4, 1987: Boeing 737130 (N410PE), Portland, ME. Aborted takeoff due airstair ajar warning. Taxied back to gate. Had a faulty microswitch. Replaced. Resumed flight. - [Incident 19860602029239I](https://openairdocs.org/incident/19860602029239I), Jun 2, 1986: Boeing 737130 (N403PE), Orlando, FL. Engine shutdown and returned after oil temperature reached caution range. Suspect fuel heat valve stuck open. - [Incident 19840627039019I](https://openairdocs.org/incident/19840627039019I), Jun 27, 1984: Boeing 737130 (N417PE), Portland, ME, Minor damage. Cockpit had electrical smoke due to failure of capacitor in generator control unit. Antiskid inoperative, tires blew - [Incident 19821222070509I](https://openairdocs.org/incident/19821222070509I), Dec 22, 1982: Boeing 737* (N410PE), Newark, NJ, Minor damage. Overran normal parking position at gate. Hit the portable passenger entry stairs. Mechanics at the controls. - [Incident 19820625059019I](https://openairdocs.org/incident/19820625059019I), Jun 25, 1982: Boeing 737* (N410PE), Sarasota, FL, Minor damage. During departure from gate the marshaller gave forward right turn signal. During turn aircraft struck the stairs. ## Service difficulty reports (287, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CALA9801859](https://openairdocs.org/sdr/CALA9801859), Sep 25, 1998: ACTUATOR. INOPERATIVE. THE GEAR HANDLE WAS PLACED IN THE OFF POSITION AFTER TAKEOFF AND THE NOSE GEAR CAME DOWN. THE GEAR HANDLE WAS PLACED UP AND THE NOSE GEAR RAISED. THE GEAR HANDL - [SDR CALA9801589](https://openairdocs.org/sdr/CALA9801589), Aug 31, 1998: BULB. FAILED. NO NOSE GEAR INDICATION WAS RECEIVED WHEN GEAR WAS EXTENDED ON APPROACH. A GO-AROUND WAS INITIATED AND THE NOSE GEAR LIGHTS DID NOT TEST. THE NOSE GEAR INDICATO - [SDR CALA9801498](https://openairdocs.org/sdr/CALA9801498), Aug 23, 1998: HYD PUMP. LEAKING. THE NR 2 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. THE NR 1 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AND THE EMERGENCY CHECKLIST F - [SDR CALA9801218](https://openairdocs.org/sdr/CALA9801218), Jul 8, 1998: ACCESSORY UNIT. INOPERATIVE. THE GEAR HANDLE STOPPED IN THE OFF POSITION WHEN RAISING THE GEAR AFTER TAKEOFF. THE GEAR TRIGGER WAS PULLED AND THE GEAR CAME UP. MAINTENANCE REMOVED AND REPLA - [SDR CALA9801171](https://openairdocs.org/sdr/CALA9801171), Jun 25, 1998: ENGINE. MALFUNCTIONED. THE NR 1 ENGINE LOST POWER DURING CLIMB-OUT OF EWR AT 1800 FEET. THE ENGINE WENT TO IDLE POWER. THE NR 1 ENGINE WAS SHUT DOWN PER FLIGHT MANUAL AND THE AIRCRAFT - [SDR CALA9801157](https://openairdocs.org/sdr/CALA9801157), Jun 23, 1998: POWER SUPPLY. INOPERATIVE. INSPECTION FOUND FORWARD ENTRY AND SERVICE DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK/POWER SUPPLY WAS REMOVED AND REPLACED. - [SDR CALA9801049](https://openairdocs.org/sdr/CALA9801049), Jun 13, 1998: SWITCH. INOPERATIVE. THE UNSAFE NOSE GEAR INDICATION ILLUMINATED ON APPROACH. TO EWR. THE GEAR WAS CYCLED, APPROPRIATE CHECKLISTS WERE COMPLIED WITH, AND THE AIRCRAFT LANDED WITHOUT - [SDR CALA9801052](https://openairdocs.org/sdr/CALA9801052), Jun 12, 1998: SOCKET. CORRODED. INSPECTION FOUND AFT EXTERIOR EXIT SLIDES INOPERATIVE BOTH SIDES. THE RIGHT EXTERIOR SLIDE LIGHT SOCKET WAS CORRODED. THE SOCKET WAS REPLACED. IN ADDITION, BATT - [SDR CALA9800702](https://openairdocs.org/sdr/CALA9800702), Apr 27, 1998: HYD LINES. PUNCTURED. THE A SYSTEM HYDRAULIC FLUID LEVEL DROPPED TO ZERO WHILE ON DESCENT INTO PHL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND TWO HYDRAULIC FLEX LINES A - [SDR CALA9800680](https://openairdocs.org/sdr/CALA9800680), Apr 19, 1998: TORQUE TUBE. DAMAGED. WHEN FLAPS WERE EXTENDED ON APPROACH, THE FLAP INDICATOR DID NOT MOVE. THE FLAPS WERE LOWERED MANUALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING - [SDR CALA9800648](https://openairdocs.org/sdr/CALA9800648), Apr 8, 1998: FRAME. CORRODED. INSPECTION FOUND BS 706L FRAME LUG HOLE CORRODED AT LT MLG. AN OUTER BUSHING FOR BEAM AND TWO EACH HAT BUSHINGS FOR FRAME LUG WERE FABRICATED AND INSTALLED IAW - [SDR CALA9800647](https://openairdocs.org/sdr/CALA9800647), Apr 7, 1998: FITTING. CRACKED. INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE FRAME TRUNNION BEAM SUPPORT FITTING IN RT WHEEL WELL AT BS 706. THE BEAM WAS REPLACED IAW ECRA 5311-01045. - [SDR CALA9800660](https://openairdocs.org/sdr/CALA9800660), Mar 4, 1998: SKIN. CRACKED. INSPECTION FOUND AN 8 INCH CRACK IN LT FUSELAGE SKIN AT STA 262-274, STRINGER 9L. THE CRACKED AREA OF SKIN WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICA - [SDR CALA9701684](https://openairdocs.org/sdr/CALA9701684), Dec 1, 1997: LINE. LEAKING. THE AIRCRAFT LOST A-HYDRAULIC SYSTEM WHILE EN ROUTE. THE AIRCRAFT WAS DIVERTED TO BUF WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT WING AFT SPAR - [SDR CALA9701680](https://openairdocs.org/sdr/CALA9701680), Nov 26, 1997: HYD LINE. LEAKING. THE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO WHILE ON APPROACH. THE GEAR AND FLAPS WERE EXTENDED BY ALTERNATE MEANS AND THE AIRCRAFT LANDED WITHOUT INCIDENT. - [SDR CALA9701432](https://openairdocs.org/sdr/CALA9701432), Oct 11, 1997: SLIDE. LOW PRESSURE. L-1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED L-1 DOOR SLIDE ASSEMBLY IN ACCORDANCE WITH MM 25-61-311. - [SDR CALA9701355](https://openairdocs.org/sdr/CALA9701355), Sep 12, 1997: HYD LINE. RUPTURED. THE A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE DROPPED TO ZERO WITH ILLUMINATION OF A PUMP LOW PRESSURE LIGHTS. THE A-SYSTEM HYDRAULIC FAILURE CHECKLIST WAS COMPL - [SDR CALA9701279](https://openairdocs.org/sdr/CALA9701279), Sep 1, 1997: ENGINE. FAILED. SPARKS WERE REPORTED COMING FROM THE NR 1 ENGINE EXHAUST WHILE IN FLIGHT. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS - [SDR CALA9701250](https://openairdocs.org/sdr/CALA9701250), Aug 28, 1997: STUD. FAILED. THE NR 1 ENGINE OIL QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF THE LOW OIL PRESSURE LIGHT WHILE ENROUTE FROM CAE TO EWR. THE ENG WAS SHUTDOWN AND T - [SDR CALA9701247](https://openairdocs.org/sdr/CALA9701247), Aug 27, 1997: HYD LINE. LEAKING. THE A SYS HYD LOW PRESSURE LIGHT FLICKERED AND HYD QTY WAS ZERO WHILE EN ROUTE TO EWR. BOTH A HYD LOW PRESSURE LIGHTS ILLUMINATED STEADILY SHORTLY AFTERWARDS. T - [SDR CALA9701234](https://openairdocs.org/sdr/CALA9701234), Aug 23, 1997: DNLOCK ACTUATOR. INOPERATIVE. THE LANDING GEAR WAS EXTREMELY STIFF DURING RETRACTION FROM UP TO OFF WITH NO NOTICEABLE DETENT AT OFF. THE NOSE GEAR EXTENDED APPROXIMATELY 12 TO 15 SECONDS AF - [SDR CALA9701243](https://openairdocs.org/sdr/CALA9701243), Aug 22, 1997: PCU. INOPERATIVE. A/C ATTEMPTED TO BANK LT WITH YAW DAMPER ON AND AUTOPILOT ENGAGED WHILE CLIMBING THRU 17,000 FT. THE YAW DAMPER WAS SWITCHED OFF AND ROLL ARRESTED. BANK ANGLE D - [SDR CALA9701223](https://openairdocs.org/sdr/CALA9701223), Aug 15, 1997: HYD LINE. LEAKING. THE A-SYSTEM HYDRAULIC FLUID QUANTITY DROPPED TO ZERO ACCOMPANIED BY ILLUMINATION OF LOW PRESSURE LIGHT WHILE AT CRUISE. THE AIRCRAFT WAS RETURNED TO EWR WHERE - [SDR CALA9701040](https://openairdocs.org/sdr/CALA9701040), Jul 10, 1997: ACTUATOR. INOPERATIVE. THE LT MLG UNSAFE INDICATOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR HANDLE WAS CYCLED SEVERAL TIMES FROM UP TO NEUTRAL POSITION UNTIL THE LIG - [SDR CALA9700980](https://openairdocs.org/sdr/CALA9700980), Jul 1, 1997: FUEL CONTROL. MALFUNCTIONED. A FUEL ODOR WAS OBSERVED IN THE COCKPIT AND CABIN ON TAKEOFF. THE CREW TURNED OFF THE LEFT PACK AND THE ODOR DISSIPATED. THE FLIGHT CONTINUED TO EWR WITHOUT FUR - [SDR CALA9701028](https://openairdocs.org/sdr/CALA9701028), Jun 28, 1997: ANGLE. CORRODED. INSPECTION FOUND VERTICAL AND HORIZONTAL SUPPORT ANGLES FOR RT UPPER STRUT AND FLOORBEAM CORRODED AT STA 267. THE CORRODED AREA WAS CUT OUT, DOUBLERS, FILLER, A - [SDR CALA9701025](https://openairdocs.org/sdr/CALA9701025), Jun 18, 1997: FRAME. CRACKED. INSPECTION FOUND FIVE EACH CRACKS IN AFT CARGO DOOR FRAME AT BS 827, STRINGER 23R. THE CRACKS WERE 1 TO 2.5 INCHES LONG. THE FRAME WAS REPAIRED IAW SRM 53-10-4 - [SDR CALA9700912](https://openairdocs.org/sdr/CALA9700912), Jun 17, 1997: WIRE HARNESS. DAMAGED. THE APU FIRE LIGHT ILLUMINATED ON SHORT FINAL INTO CLE DURING APU START. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE APU HAD TORCHED - [SDR CALA9700843](https://openairdocs.org/sdr/CALA9700843), Jun 6, 1997: HYDRAULIC LINE. CHAFED. THE A-HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO NEAR ZERO WHILE EN ROUTE. THE HYDRAULIC QUANTITY LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED AT AT - [SDR CALA9700860](https://openairdocs.org/sdr/CALA9700860), May 20, 1997: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED IN TWO PLACES AT STA 360, STRINGER 17L. THE DENTED SECTION OF SKIN WAS REPAIRED IAW SRM 53-30-3, FIGURE 28 AND ECRA 5330-0 - [SDR CALA9700734](https://openairdocs.org/sdr/CALA9700734), May 15, 1997: BATT CHARGER. BURNED. AN ELECTRICAL ODOR WITH A SLIGHT TRACE OF HAZE WAS NOTICED IN THE CABIN WHILE ON DESCENT INTO CLE. THE GASPER FAN AND GALLEY POWER WAS TURNED OFF AND THE ODOR D - [SDR CALA9701024](https://openairdocs.org/sdr/CALA9701024), May 13, 1997: STRINGER. CRACKED. INSPECTION FOUND CRACKS TOTALING 4 INCHES IN LENGTH IN RT WING STRINGER 13, AT WBL 135. REPAIR ANGLES WERE REMOVED AND THE CRACKS WERE STOP DRILLED. THE REPAIR - [SDR CALA9701029](https://openairdocs.org/sdr/CALA9701029), May 12, 1997: ANGLE. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN RT UPPER CORNER OF NOSE WHEEL WELL ANGLE AT STA 267. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-0, 51-10-2, - [SDR CALA9701023](https://openairdocs.org/sdr/CALA9701023), May 12, 1997: STRINGER. CRACKED. INSPECTION FOUND A 5 INCH CRACK IN RT WING STRINGER 13 AT WBL 80. THE STRINGER WAS REPAIRED IAW ECRA 5710-01815. - [SDR CALA9701027](https://openairdocs.org/sdr/CALA9701027), May 8, 1997: SKIN. CRACKED. INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT UPPER FORWARD CORNER OF L-2 DOOR AT STA 947, S7L. THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICA - [SDR CALA9701026](https://openairdocs.org/sdr/CALA9701026), May 8, 1997: SKIN. CRACKED. INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT AFT UPPER CORNER OF L-2 DOOR, STA 986, S7L. THE CRACK WAS ROUTED OUT, DOUBLER AND FILLERS WERE FABRICATED AN - [SDR CALA9701022](https://openairdocs.org/sdr/CALA9701022), May 8, 1997: SKIN. CRACKED. INSPECTION FOUND .5 INCH CRACKS AND CORROSION IN FUSELAGE SKIN AT STA 283, S10R. THE CORROSION WAS REMOVED AND THE CRACKED AREA OF SKIN WAS CUT OUT, A REPAIR WA - [SDR CALA9700940](https://openairdocs.org/sdr/CALA9700940), May 5, 1997: BATTERY PACK. DISCHARGED. THE R-1 DOOR PORTABLE EXIT LIGHT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED IAW MM 33-51-42 AND 33-51-101. - [SDR CALA9700939](https://openairdocs.org/sdr/CALA9700939), May 5, 1997: BATTERY PACK. DISCHARGED. THE R-2 DOOR PORTABLE EXIT LIGHT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED IAW MM 33-50-42 AND 33-51-101. - [SDR CALA9700938](https://openairdocs.org/sdr/CALA9700938), May 5, 1997: BATTERY PACK. DISCHARGED. THE LT ESCAPE HATCH PORTABLE EXIT LIGHT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED IAW MM 33-50-42 AND 33-51-101. - [SDR CALA9700937](https://openairdocs.org/sdr/CALA9700937), May 5, 1997: BATTERY PACK. DISCHARGED. THE L-1 DOOR EXTERIOR EXIT LIGHT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED IAW MM 33-51-71, 33-50-42, AND 33-51-31. - [SDR CALA9700936](https://openairdocs.org/sdr/CALA9700936), May 5, 1997: BATTERY PACK. DISCHARGED. THE R-2 DOOR EXTERIOR EXIT LIGHT FAILED CAPACITY CHECK. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED IAW MM 33-51-71, 33-50-42, AND 33-51-31. - [SDR CALA9700643](https://openairdocs.org/sdr/CALA9700643), May 4, 1997: STRUT. CRACKED. A GRINDING SOUND WAS HEARD COMING FROM LANDING GEAR AREA DURING TAXI. MAINTENANCE FOUND THE NR 2 BRAKE ASSEMBLY DAMAGED DUE TO A SHEARED BOLT AND THE LT MLG INN - [SDR CALA9700620](https://openairdocs.org/sdr/CALA9700620), Apr 28, 1997: FIRE LOOP. CORRODED. EN ROUTE, AT FL310 WHEN ENGINE ANTI-ICE TURNED ON ENGINE FIRE WARNING SOUNDED. FOLLOWED PROCEDURES PER QRH. FIRE WARNING AGAIN SOUNDED SHUTDOWN NR 1 ENGINE, DIS - [SDR CALA9700608](https://openairdocs.org/sdr/CALA9700608), Apr 23, 1997: LINE. CHAFED. LOST A-SYSTEM HYDRAULICS IN FLIGHT. REPLACED NUMBER 2 ENGINE HYDRAULIC SUPPLY LINE AT RIGHT WING ROOT. - [SDR CALA9700648](https://openairdocs.org/sdr/CALA9700648), Apr 22, 1997: SKIN. DENTED. INSPECTION FOUND FUSELAGE SKIN DENTED AT UPPER EDGE OF BULKHEAD STA 178. THE DENTED AREA WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-1 - [SDR CALA9700647](https://openairdocs.org/sdr/CALA9700647), Apr 22, 1997: SKIN. LIGHTNING STRIKE. INSPECTION FOUND A LIGHTNING BURN AT FASTENER HEAD FOURTEEN INCHES AFT OF R-1 DOOR, STRINGER 9L. THE DAMAGED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTA - [SDR CALA9700646](https://openairdocs.org/sdr/CALA9700646), Apr 21, 1997: SKIN. CRACK. INSPECTION FOUND A .0937 INCH CRACK AND CORROSION IN FUSELAGE SKIN AT STA 312, STRINGER 26L. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND - [SDR CALA9700644](https://openairdocs.org/sdr/CALA9700644), Apr 20, 1997: SKIN. CRACKED. INSPECTION FOUND A .125 INCH CRACK IN LT WING LEADING EDGE SKIN AT LE STA 219.67. THE CRACKED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA - [SDR CALA9700645](https://openairdocs.org/sdr/CALA9700645), Apr 18, 1997: BRACKET. CRACKED. INSPECTION FOUND A 1 INCH CRACK AT UPPER ATTACH BRACKET OF R-1 DOOR WEB. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. All 287: https://openairdocs.org/model/boeing-737-130/reports.md ## STCs that may be installed (OpenAirDocs) (237, 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 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 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 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 SA3133NM](https://openairdocs.org/stc/SA3133NM): Installation of Windscreen Stowage Unit. Safran Cabin Inc - [STC SA3936NM](https://openairdocs.org/stc/SA3936NM): Installation of Header and Cabin Divider. Safran Cabin Inc - [STC SA7061NM](https://openairdocs.org/stc/SA7061NM): Installation of Galley No. 3, Galley No. 7, and Fwd RH Coat Closet. Safran Cabin Inc - [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 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 ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH - [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC - [STC ST01829AT](https://openairdocs.org/stc/ST01829AT): Installation of SAF-T-GLO Aerospace Limited's photoluminescent floor proximity emergency escape path marked system (FPEEPMS). STG Aerospace Inc - [STC ST02302CH](https://openairdocs.org/stc/ST02302CH): Install ERDA model 7004 HI-LO table with slide top. Collins Aerospace - [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited - [STC ST02096AT](https://openairdocs.org/stc/ST02096AT): Installation of an AlliedSignal 18 parameter digital flight data recorder (for aircraft not containing a flight data acquisition unit). Woven Electronics, LLC - [STC ST02178AT](https://openairdocs.org/stc/ST02178AT): To upgrade the existing Sundstrand Digital Flight Data Recorder System to 22 Parameter by replacing the existing Flight Data Acquisition Unit with a Teledyne Flight Data Acquisition Unit. Woven Electronics LLC - [STC SA3157SO](https://openairdocs.org/stc/SA3157SO): Installation of a Digital Flight Data Recorder. Acron Aviation Inc - [STC ST02706AT](https://openairdocs.org/stc/ST02706AT): Installation of the L-3 Comm. Corp. micro Quick Access Recorder (QAR). L3Harris Aviation Products Inc - [STC ST03014AT](https://openairdocs.org/stc/ST03014AT): Installation of a Single CMA-900 Flight Management System with Global Position Sensor. Woven Electronics, LLC - [STC ST02580AT](https://openairdocs.org/stc/ST02580AT): Lithium cell battery pack to replace currently approved alkaline battery pack used in escape slide emergency light system. Astronics Luminescent Systems Inc - [STC ST02929AT](https://openairdocs.org/stc/ST02929AT): Installation of an Artex Model C406-1 Emergency Locator Transmitter (ELT). Woven Electronics LLC - [STC ST01651AT](https://openairdocs.org/stc/ST01651AT): Installation of a dual GARMIN 165 Global Positioning System. Technical Aero Services Inc - [STC SA1220NW](https://openairdocs.org/stc/SA1220NW): Installation of Universal flight data recorder. Honeywell International Inc - [STC ST01775SE](https://openairdocs.org/stc/ST01775SE): Installation of a diaper changing table. Commercial Aircraft Interiors - [STC ST00341AT](https://openairdocs.org/stc/ST00341AT): Installation of a RDR-4B Weather Rader/Windshear System. Honeywell International Inc - [STC ST01052SE](https://openairdocs.org/stc/ST01052SE): Installation of the Solid state Flight Data Recorder and Honewell Flight Data Acquisition Management System. Honeywell International Inc - [STC ST01826AT](https://openairdocs.org/stc/ST01826AT): Installation of the AlliedSignal RTA-83A VHF Communication System. Honeywell International Inc - [STC ST01963WI](https://openairdocs.org/stc/ST01963WI): Installation of Integra Pulse Portable Oxygen Bottle. B/E Aerospace - [STC SA8718SW](https://openairdocs.org/stc/SA8718SW): Replace core assembly of AiResearch bleed air precooler, P/N 182400-1-1. Honeywell International Inc - [STC SA4842SW](https://openairdocs.org/stc/SA4842SW): Modification of air to air heat exchanger (P/N 182820-2 Series 2). Honeywell International Inc. Lists 737 Series - [STC ST03574AT](https://openairdocs.org/stc/ST03574AT): Installation of a Talon Aerospace Anti-Collision Light. Aaxico Technical Services Inc - [STC ST04002AT](https://openairdocs.org/stc/ST04002AT): Installation of a Talon LED Replacement Wing and Tail Mounted Anti-Collision Lights. Aaxico Technical Services Inc - [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc - [STC ST02532LA](https://openairdocs.org/stc/ST02532LA): Modify the wing fuel tanks access cover installation by replacing the existing rubstrip and seal with a new encapsulated wire mesh gasket and a new seal. Aviation Devices & Electronic Components LLC - [STC ST10930SC](https://openairdocs.org/stc/ST10930SC): Installation of a TIA Air Coffee MK-1 coffee maker. Safran Cabin Germany Gmbh - [STC SA5458NM](https://openairdocs.org/stc/SA5458NM): Installation of Honeywell Standard windshear systems. Honeywell International Inc - [STC SA8830SW](https://openairdocs.org/stc/SA8830SW): Installation of a C/X band fuselage nose radome shell. The NORDAM Group LLC - [STC ST04426NY](https://openairdocs.org/stc/ST04426NY): 1. Installation of ADS-B Out. Eirtech Aviation Services Limited All 237: https://openairdocs.org/model/boeing-737-130/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Boeing 737-112](https://openairdocs.org/model/boeing-737-112): 0 registered aircraft, registry code 1384412 --- 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.