# Beech 1900 - Type: Aircraft model (FAA registry) - Registry code: 1154160 - Manufacturer (registry): BEECH - Model: 1900 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 19 - Weight class: 12,500 to 19,999 lb - Certification: Type certificated - Data sheet: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs) - Holder: Textron Aviation Inc. - Registered aircraft: 7 - Page: https://openairdocs.org/model/beech-1900 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 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 2014-02-03](https://openairdocs.org/ad/2014-02-03): Flight Controls · Textron 1900, 1900C and 1900D. Effective Mar 7, 2014 - [AD 2013-24-03](https://openairdocs.org/ad/2013-24-03): Stabilizers · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jan 13, 2014 - [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011 - [AD 2009-23-03](https://openairdocs.org/ad/2009-23-03): Flanges · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 14, 2009 - [AD 2009-23-01](https://openairdocs.org/ad/2009-23-01): Main Landing Gear · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 8, 2009 - [AD 2006-18-51](https://openairdocs.org/ad/2006-18-51): Left and right wing rear spar lower caps · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Sep 8, 2006 - [AD 2005-18-21](https://openairdocs.org/ad/2005-18-21): Elevator hinge support attachments · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Sep 13, 2005 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2004-23-02](https://openairdocs.org/ad/2004-23-02): Nose Landing Gear (NLG) Fork · Textron 100, 1900, 1900C and 50 more. Effective Dec 23, 2004 - [AD 2004-17-02](https://openairdocs.org/ad/2004-17-02): Cross shaft attach bolt · Textron 100, 1900, 1900C and 52 more. Effective Oct 4, 2004 - [AD 2004-09-07](https://openairdocs.org/ad/2004-09-07): Canted Bulkhead Located at Fuselage Station (FS) 588.10 · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jun 14, 2004 - [AD 2004-01-13](https://openairdocs.org/ad/2004-01-13): Vent blower assemblies · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 19, 2004 - [AD 2003-20-10](https://openairdocs.org/ad/2003-20-10): Elevator Trim System Maintenance Procedures · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Oct 15, 2003 - [AD 2003-03-18](https://openairdocs.org/ad/2003-03-18): Elevator Control System · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 5, 2003 - [AD 2002-23-11](https://openairdocs.org/ad/2002-23-11): Elevator Balance Weight Attachment Screws · Textron 1900, 1900C, 1900C (C-12J) and 30 more. Effective Jan 10, 2003 - [AD 2001-22-16](https://openairdocs.org/ad/2001-22-16): Engine Truss Assembly · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 17, 2001 - [AD 2001-18-07](https://openairdocs.org/ad/2001-18-07): Flap Flexible Shaft Assemblies · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Oct 12, 2001 - [AD 2000-20-07](https://openairdocs.org/ad/2000-20-07): Cockpit Voice Recorder (CVR) System · Textron 1900, 1900C and 1900D. Effective Nov 22, 2000 - [AD 97-15-13 R2](https://openairdocs.org/ad/97-15-13-R2): Airstair Door Handle and Latch Housing · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective May 28, 1999 - [AD 99-04-08](https://openairdocs.org/ad/99-04-08): Main Landing Gear Hydraulic Actuators · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Mar 26, 1999 - [AD 99-01-03](https://openairdocs.org/ad/99-01-03): Flaps · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 8, 1999 - [AD 98-26-16](https://openairdocs.org/ad/98-26-16): Emergency Exit Doors · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 5, 1999 - [AD 98-21-20](https://openairdocs.org/ad/98-21-20): Exterior Marking Placards · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Nov 20, 1998 - [AD 97-26-15](https://openairdocs.org/ad/97-26-15): Main Landing Gear Actuator · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jan 25, 1998 - [AD 97-25-03](https://openairdocs.org/ad/97-25-03): AFM - Limitations - Power Levers · Textron 100, 1900, 1900C and 44 more. Effective Jan 21, 1998 - [AD 97-06-06](https://openairdocs.org/ad/97-06-06): Pilot and Copilot Chairs Locking Pins · Textron 100, 1900, 1900C and 43 more. Effective May 9, 1997 - [AD 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996 - [AD 96-09-13](https://openairdocs.org/ad/96-09-13): AFM - Icing · Textron 1900, 1900C, 1900D and 7 more. Effective Jun 11, 1996 - [AD 95-14-02](https://openairdocs.org/ad/95-14-02): Instrument Air System · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Aug 31, 1995 - [AD 94-20-05](https://openairdocs.org/ad/94-20-05): Hot Battery Bus · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Oct 14, 1994 - [AD 90-06-13](https://openairdocs.org/ad/90-06-13): Vertical Gyro · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 14 more. Effective Mar 30, 1990 - [AD 85-21-07 R1](https://openairdocs.org/ad/85-21-07-R1): POH/AFM Addendum · Textron 1900, 1900C and 1900C (C-12J). Effective Jul 10, 1987 - [AD 87-04-24](https://openairdocs.org/ad/87-04-24): Elevator Trim Cable System · Textron 1900, 1900C, 200 and 28 more. Effective Apr 14, 1987 - [AD 87-05-02](https://openairdocs.org/ad/87-05-02): POH/AFM Changes · Textron 1900, 1900C and 1900C (C-12J). Effective Mar 23, 1987 Historical (superseded or no longer in force): - [AD 2011-27-51](https://openairdocs.org/ad/2011-27-51) (historical): Flight Controls · Hawker Beechcraft 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jan 18, 2012 - [AD 97-22-16](https://openairdocs.org/ad/97-22-16) (historical): Vent Blower Assembly Bearing · Raytheon 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 5, 1997 - [AD 97-15-13 R1](https://openairdocs.org/ad/97-15-13-R1) (historical): Airstair Door Handle And Latch Housing · Raytheon 1900, 1900C and 1900D. Effective Sep 22, 1997 - [AD 97-15-13](https://openairdocs.org/ad/97-15-13) (historical): Airstair Door Handle And Latch Housing · Raytheon 1900, 1900C and 1900D. Effective Sep 5, 1997 - [AD 97-14-16](https://openairdocs.org/ad/97-14-16) (historical): Outboard Flap Attachment Brackets And Aft Roller Bearings · Raytheon 1900, 1900C and 1900D. Effective Aug 4, 1997 - [AD 97-04-02](https://openairdocs.org/ad/97-04-02) (historical): Exterior Marking Placards For Airstair And Cargo Doors · Raytheon 1900, 1900C and 1900D. Effective Mar 10, 1997 - [AD 95-02-18](https://openairdocs.org/ad/95-02-18) (historical): Engine Truss Assembly · Raytheon 1900, 1900C and 1900D. Effective Mar 25, 1995 - [AD 87-22-01 R1](https://openairdocs.org/ad/87-22-01-R1) (historical): Nose Landing Gear Fork · Raytheon 100 Model or Series (all), 1900, 1900C and 50 more. Effective Sep 30, 1989 ## Information bulletins (advisory) (6) - [SAIB CE-15-15](https://openairdocs.org/saib/CE-15-15): Empennage Horizontal & Vertical Stabilizer Structure. Issued Apr 20, 2015 - [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012 - [SAIB CE-05-83](https://openairdocs.org/saib/CE-05-83): . Issued Aug 26, 2005 - [SAIB CE-02-19](https://openairdocs.org/saib/CE-02-19): . Issued Mar 11, 2002 - [SAIB CE-00-24](https://openairdocs.org/saib/CE-00-24): . Issued Jul 11, 2000 - [SAIB CE-00-15](https://openairdocs.org/saib/CE-00-15): . Issued Jan 21, 2000 ## Registered aircraft (7) - [N125BA](https://openairdocs.org/aircraft/N125BA): [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC), [Provo, UT](https://openairdocs.org/faa-place/UT/Provo), S/N UB-6 - [N127BA](https://openairdocs.org/aircraft/N127BA): [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC), [Provo, UT](https://openairdocs.org/faa-place/UT/Provo), S/N UB-7 - [N192GA](https://openairdocs.org/aircraft/N192GA): [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC), [Provo, UT](https://openairdocs.org/faa-place/UT/Provo), S/N UB-17 - [N20RA](https://openairdocs.org/aircraft/N20RA): [Department Of The Air Force](https://openairdocs.org/faa-owner/DEPARTMENT%20OF%20THE%20AIR%20FORCE), [Hill Afb, UT](https://openairdocs.org/faa-place/UT/Hill%20Afb), built 1985, S/N UB-42 - [N219VP](https://openairdocs.org/aircraft/N219VP): [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC), [Provo, UT](https://openairdocs.org/faa-place/UT/Provo), built 1984, S/N UB-14 - [N3052K](https://openairdocs.org/aircraft/N3052K): [Uas Transervices Inc](https://openairdocs.org/faa-owner/UAS%20TRANSERVICES%20INC), [Boca Raton, FL](https://openairdocs.org/faa-place/FL/Boca%20Raton), built 1987, S/N UB-70 - [N330AF](https://openairdocs.org/aircraft/N330AF): [Uas Transervices Inc](https://openairdocs.org/faa-owner/UAS%20TRANSERVICES%20INC), [Boca Raton, FL](https://openairdocs.org/faa-place/FL/Boca%20Raton), built 1985, S/N UB-38 ## STCs approved for it (122, first 50) - [STC SA00095BO](https://openairdocs.org/stc/SA00095BO): Installation of Pratt & Whitney Engine Services, Inc. Twin Engine Aircraft Data Acquisition System ADAS/ADAS+ Upgrade, P/N TWIN-K-010,. Pratt & Whitney Engine Services Inc. - [STC SA00110AT](https://openairdocs.org/stc/SA00110AT): Installation of a Marathon KSP 400 battery.. Aviall Services, Inc. - [STC SA00120IB](https://openairdocs.org/stc/SA00120IB): Installation of the Universal Kapture Cockpit Voice Recorder (CVR) with Recorder Independent Power Supply (RIPS). Avmax Aviation Services Inc. - [STC SA00128IB](https://openairdocs.org/stc/SA00128IB): Antenna Installation and Bulkhead Feedthrough. Avmax Aviation Services Inc. - [STC SA00161BO (3 OF 3](https://openairdocs.org/stc/SA00161BO%20(3%20OF%203): Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.. Avidyne Corporation - [STC SA00165BO](https://openairdocs.org/stc/SA00165BO): Installation of Avidyne Corporation Datalink Coupler, part number 700-00015-000 per Avidyne Corporation Master Document List, Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions.. Avidyne Corporation - [STC SA00171BO](https://openairdocs.org/stc/SA00171BO): Installation of Pratt & Whitney Engine Services, Inc. Aircraft Data Acquisition System ADAS+, P/N ADAS-K-010.. Pratt & Whitney Engine Services Inc. - [STC SA00196BO](https://openairdocs.org/stc/SA00196BO): Installation of Pratt & Whitney Engine Services, Inc. Data Transmission Unit. Pratt & Whitney Engine Services Inc. - [STC SA00243BO (4 OF 5)](https://openairdocs.org/stc/SA00243BO%20(4%20OF%205)): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).. Icarus Avionics, LLC - [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation - [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation - [STC SA00322BO](https://openairdocs.org/stc/SA00322BO): Installation of a Supplemental Exterior Lighting System. ATI Engineering Services LLC - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA00727AT-D](https://openairdocs.org/stc/SA00727AT-D): Installation of replacement fuel cell assemblies. FFC Manufacturing - [STC SA00741WI](https://openairdocs.org/stc/SA00741WI): Installation of the Concorde RG-380E/K series VRSLA batteries in airplanes listed on the attached FAA approved Model List (AML). Aero-Mach Wilco LLC - [STC SA00749AT](https://openairdocs.org/stc/SA00749AT): Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent). Aero Trim, Inc - [STC SA00775AT](https://openairdocs.org/stc/SA00775AT): Installation of a Bendix/King KLN90B Global Positioning System.. Piedmont Avn Services, Inc - [STC SA00776AT](https://openairdocs.org/stc/SA00776AT): Installation of a Dual Bendix/King Mode S Transponder, Traffic Alert and Collision Avoidance System and Sundstrand Mark VI Ground Proximity Warning System. Piedmont Avn Services, Inc - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA00889DE](https://openairdocs.org/stc/SA00889DE): Installation of Teledyne Battery Products P/N 7638-44 Lead-Acid Battery. Teledyne Battery Products - [STC SA00970CH](https://openairdocs.org/stc/SA00970CH): Installation of various SMR Technologies electrical propeller de-icer models.. SMR Technologies - [STC SA01050WI](https://openairdocs.org/stc/SA01050WI): Installation of Emergency Vision Assurance System (EVAS).. VisionSafe LLC - [STC SA01126WI](https://openairdocs.org/stc/SA01126WI): Replacement of wing tie down ring assembly on Classic Beechcraft model airplanes with one piece machined part number APMA35-115632. DER Associates Ltd. - [STC SA01158WI](https://openairdocs.org/stc/SA01158WI): Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System.. Aero Enhancements Inc. - [STC SA01229SE PAGE 2](https://openairdocs.org/stc/SA01229SE%20PAGE%202): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit.. Med-Pac Inc. - [STC SA01472WI-D](https://openairdocs.org/stc/SA01472WI-D): Modification of a Rockwell Collins Weather Radar System installation. Rockwell Collins Inc - [STC SA01473SE (5 OF 5)](https://openairdocs.org/stc/SA01473SE%20(5%20OF%205)): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc. - [STC SA01487SE (4 OF 5)](https://openairdocs.org/stc/SA01487SE%20(4%20OF%205)): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.. Garmin AT Inc. - [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA01639NY](https://openairdocs.org/stc/SA01639NY): Replacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B.. Scale Modelbuilders Inc. - [STC SA01656LA](https://openairdocs.org/stc/SA01656LA): Installation of Universal Avionics EFI-890R Primary Flight Display/Navigation Display (PFD/ND). Universal Avionics Systems Corp - [STC SA01692SE (PAGE 1 OF 2)](https://openairdocs.org/stc/SA01692SE%20%20(PAGE%201%20OF%202)): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc - [STC SA01695SE (5 OF 5)](https://openairdocs.org/stc/SA01695SE%20(5%20OF%205)): Installation of an antenna. Garmin AT Inc. - [STC SA01714WI (2 OF 2)](https://openairdocs.org/stc/SA01714WI%20(2%20OF%202)): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA01894LA](https://openairdocs.org/stc/SA01894LA): Installation of Universal Avionics Terrain Awareness and Warning System Class A and Class B Displayed on EFI-890. Universal Avionics Systems Corp - [STC SA01923WI](https://openairdocs.org/stc/SA01923WI): Installation of an Auxiliary Aural Alert System.. Hawker Pacific Pty Ltd - [STC SA01933LA-D (1 OF 2)](https://openairdocs.org/stc/SA01933LA-D%20(1%20OF%202)): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA01945NY](https://openairdocs.org/stc/SA01945NY): Cockpit voice recorder replacement with Universal CVR 30B or CVR 120.. MidCanada Mod Center - [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics - [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation - [STC SA02019SE-D (1 OF 3)](https://openairdocs.org/stc/SA02019SE-D%20(1%20OF%203)): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc. - [STC SA02019SE-D (3 OF 3)](https://openairdocs.org/stc/SA02019SE-D%20(3%20OF%203)): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc. - [STC SA02071LA](https://openairdocs.org/stc/SA02071LA): Installation of Dual Universal Avionics Wide Area Augmentation System (WAAS) UNS1 ( )w Flight Management Systems (FMS). Universal Avionics Systems Corp All 122: https://openairdocs.org/model/beech-1900/stcs.md ## NTSB investigations (4) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CEN21LA248](https://openairdocs.org/ntsb/CEN21LA248), Jun 3, 2021: Beech 1900 (N219VP), Denver, CO, substantial damage. Probable cause: The pilot’s failure to properly configure the airplane for landing, which resulted in a gear-up landing. - [NTSB MIA00LA115](https://openairdocs.org/ntsb/MIA00LA115), Mar 19, 2000: Beech 1900 (N199GA), Miami, FL, minor damage. Probable cause: Inadequate visual lookout by the driver of the vehicle. - [NTSB NYC95LA078](https://openairdocs.org/ntsb/NYC95LA078), Mar 25, 1995: Beech 1900C (N34010), Covington, KY, substantial damage. Probable cause: a lack of procedures by the tug operator to prevent inadvertent movement of an unoccupied tug, which resulted in an airplane being struck by an unoccupied tug which moved on its own. - [NTSB SEA93IA050](https://openairdocs.org/ntsb/SEA93IA050), Jan 11, 1993: Beech 1900C (N34010), Riverton, WY, incident, minor damage. Probable cause: THE PILOT'S DISORIENTATION. FACTORS INCLUDE SNOW, FOG, SNOW COVERED TERRAIN, AND A DRAINAGE DITCH. ## FAA accident and incident reports (20) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20210603005949A](https://openairdocs.org/incident/20210603005949A), Jun 3, 2021: Beech 1900 (N219VP), Denver, CO, Substantial damage. On 06/02/2021 at approximately (2000) hrs (MDT), N219VP, sn UB-14, BE-1900, cargo operator [privacy data omitted], during landing runway 17R at Denver… - [Incident 20101130051159I](https://openairdocs.org/incident/20101130051159I), Nov 30, 2010: Beech 1900 (N219VP), Greatfalls, MT, No damage. Pilot stated he departed holman aviation on taxiway 'a' between A1 and A2 at kgtf, he was running the checklist, looking inside the cockpit and veried off the… - [Accident 20000318006449A](https://openairdocs.org/incident/20000318006449A), Mar 18, 2000: Beech 1900 (N199GA), Miami, FL, Minor damage. (-23) On March 18, 2000, at approx.19:00 local, guua flight #9399, N199GA, a BE-1900C was taxiing, with captain^privac^in command, to the gate at night during… - [Incident 19980527024049I](https://openairdocs.org/incident/19980527024049I), May 27, 1998: Beech 1900 (N3052K), Dallas, TX. Water intrusion from airstair door open while on ground. Dripped on vent blower and pc board created inflight smoke. - [Accident 19950325011179A](https://openairdocs.org/incident/19950325011179A), Mar 25, 1995: Beech 1900 (N34010), Covington/Cinci, KY, Substantial damage. Uploading luggage on ramp a unattended tug on other side. Moved and circled into aircraft nose. Tail hit handler. - [Incident 19931226050949I](https://openairdocs.org/incident/19931226050949I), Dec 26, 1993: Beech 1900 (N3052K), Middletown, PA. Gear extended after takeoff. Returned. Landed safely. Found 60 amp circuit breaker popped. Reset breaker. - [Incident 19930111004879I](https://openairdocs.org/incident/19930111004879I), Jan 11, 1993: Beech 1900 (N34010), Riverton, WY, Minor damage. In whiteout conditions pilot turned off runway onto what they thought was taxiway. Struck a ditch. - [Incident 19920121004469I](https://openairdocs.org/incident/19920121004469I), Jan 21, 1992: Beech 1900 (N3052K), Pittsburgh, PA, Minor damage. Found wheel missing on post flight inspection. Found inner wheel bearing had failed. - [Incident 19920115002779I](https://openairdocs.org/incident/19920115002779I), Jan 15, 1992: Beech 1900C (N6800J), Roswell, NM, Minor damage. On landing rollout the two main gear collapsed. - [Incident 19910307009629I](https://openairdocs.org/incident/19910307009629I), Mar 7, 1991: Beech 1900 (N3052K), New York, NY. Flaps failed to retract on departure. Diverted to jfk. Landed safely. Found a faulty flap limit switch. - [Incident 19900614029829I](https://openairdocs.org/incident/19900614029829I), Jun 14, 1990: Beech 1900 (N3052K), Altoona, PA, Minor damage. Struck by lighting in cruise. Lost all communication. Landed safely. Replaced NR2 navigation control head. - [Incident 19900227013569I](https://openairdocs.org/incident/19900227013569I), Feb 27, 1990: Beech 1900 (N3052K), Middletown, PA. Right engine not developing enough power. Precautionary landing. Replaced propeller governor. - [Incident 19891215060099I](https://openairdocs.org/incident/19891215060099I), Dec 15, 1989: Beech 1900 (N3052K), Ithaca, NY. Unsafe gear light after takeoff. Returned. Replaced chaffed wire in uplock switch. - [Incident 19890307025089I](https://openairdocs.org/incident/19890307025089I), Mar 7, 1989: Beech 1900 (N3052K), Pittsburgh, PA. Landed behind DC9 which blew up a great deal of snow. Pulled right on rollout. Windrow from snowplow caused pull. - [Incident 19890304022929I](https://openairdocs.org/incident/19890304022929I), Mar 4, 1989: Beech 1900 (N3052K), Pittsburgh, PA. Right engine torque and prop indicator fluctuating. Engine shut down. Landed safely. Replaced bleed air valve. - [Incident 19880811044139I](https://openairdocs.org/incident/19880811044139I), Aug 11, 1988: Beech 1900 (N3052K), Pittsburgh, PA. Unable to extend landing gear, made a go around. Manually extended landing gear. Landed safely. Cause undetermined. - [Incident 19880520039219I](https://openairdocs.org/incident/19880520039219I), May 20, 1988: Beech 1900 (N7210R), Newark, NJ, Minor damage. Unsafe gear indication. Gear extended manually. Right gear collapsed taxiing to gate despite unsafe gear indication - [Incident 19860620033489I](https://openairdocs.org/incident/19860620033489I), Jun 20, 1986: Beech 1900 (N7210R), Syracuse, NY. Returned with right engine shutdown after compressor bleed air valve failed. Uneventful landing. - [Incident 19851015056939I](https://openairdocs.org/incident/19851015056939I), Oct 15, 1985: Beech 1900 (N20RA), Dallas, TX, Minor damage. While being directed by one ramp attendant, the tail section struck the wingtip of a parked DHC7. - [Incident 19850125004669I](https://openairdocs.org/incident/19850125004669I), Jan 25, 1985: Beech 1900 (N7210R), Binghamton, NY, Minor damage. Left engine power deteriorated and fire from exhaust on takeoff. Shutdown and returned for landing. ## Service difficulty reports (87, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR JIKA2024052901](https://openairdocs.org/sdr/JIKA2024052901), May 24, 2024: HYDRAULIC LINE. CHAFED. DURING LANDING, THE FLIGHT CREW ATTEMPTED TO LOWER THE GEAR NORMALLY. IT WAS OBSERVED THAT THERE WAS A LOW HYDRAULIC LIGHT FLICKER INDICATING A LOSS OF PRESSURE - [SDR JIKA2024021601](https://openairdocs.org/sdr/JIKA2024021601), Feb 13, 2024: WIRE HARNESS. SHORTED. WHEN THE FLIGHT CREW PLACED THE LANDING GEAR HANDLE IN THE DOWN POSITION THE CIRCUIT BREAKER POPPED AND CAUSED THE LANDING GEAR INDICATION LIGHTS TO COMPLETELY - [SDR JIKA2019101701](https://openairdocs.org/sdr/JIKA2019101701), Oct 15, 2019: PACKING. LEAKING. APPROXIMATELY 1HR INTO FLIGHT, RIGHT ENGINE OIL PRESSURE DROPPED TO 40PSI ACCOMPANIED WITH LOW OIL PRESSURE WARNING ANNUNCIATOR LIGHT. CREW COMPLIED WITH CHECKL - [SDR JIKA2018100201](https://openairdocs.org/sdr/JIKA2018100201), Oct 2, 2018: UNKNOWN. SMOKE. THE PILOT REPORTED THAT WHILE INFLIGHT THERE WAS SMOKE OR VAPOR COMING FROM UNDERNEATH THE PILOT AND CO-PILOTS SEATS, WHERE THE FLOOR VENTS ARE LOCATED. THE ENV - [SDR JIKA2018100192701](https://openairdocs.org/sdr/JIKA2018100192701), Oct 1, 2018: CIRCUIT BREAKER. DEFECTIVE. DISCREPANCY: THE PILOT REPORTED ON APPROACH INTO KBUR, THE CREW SELECTED THE GEAR LEVER TO DOWN. THE THREE GREEN GEAR INDICATORS DID NOT ILLUMINATE. THE CREW EL - [SDR JIKA2018060453002](https://openairdocs.org/sdr/JIKA2018060453002), May 30, 2018: FILTER. CONTAMINATED. THE PILOT REPORTED DURING TAKEOFF, THAT THE RIGHT LOW PRESSURE FUEL PUMP FAIL INDICATION ILLUMINATED. THE PILOT ACTIVATED THE RIGHT BOOST PUMP. THE FUEL PUMP FA - [SDR JIKA201806043001](https://openairdocs.org/sdr/JIKA201806043001), May 30, 2018: FILTER. CONTAMINATED. THE PILOT REPORTED AFTER TAKEOFF, THAT THE RIGHT LOW PRESSURE FUEL PUMP FAILED INDICATION ILLUMINATED. THE PILOT ACTIVATED THE RIGHT BOOST PUMP. THE FUEL PUMP F - [SDR JIKA2018032301](https://openairdocs.org/sdr/JIKA2018032301), Mar 23, 2018: UNKNOWN. SMOKE. THE PILOT REPORTED DURING APPROACH, THERE WAS AN UNUSUAL ODOR FOLLOWED BY LIGHT SMOKE IN THE COCKPIT. THE PILOT FOLLOWED PROCEDURES AND TURNED THE BLEED SYSTEM - [SDR JIKA2016052301](https://openairdocs.org/sdr/JIKA2016052301), May 23, 2016: FUEL CELL. LEAKING. EN-ROUTE THE PILOT REPORTED A STRONG FUEL ODOR FROM THE CABIN AREA. DEPRESSURIZED THE CABIN, USED OXYGEN & OPENED THE FRESH AIR VENTS, LANDED WITHOUT INCIDENT. - [SDR JIKA201512081501](https://openairdocs.org/sdr/JIKA201512081501), Dec 3, 2015: FUEL CONTROL. LOW PRESSURE. EN-ROUTE, THE PILOT REPORTED THAT THE RT ENG TORQUE STARTED TO DROP OFF. THE PILOT WAS ABLE TO MATCH TOQUE BY ADVANCING THE RT POWER LEVER. DURING APPROACH, THE - [SDR CA141103001](https://openairdocs.org/sdr/CA141103001), Oct 22, 2014: ENGINE. POWER LOSS. (CAN) DURING THE CRUISE THE CAPTAIN NOTICED THE NR 1 ENGINE SHOWING 93% N1 MAX AND SHORTLY AFTER NOTICING THIS, THE LH GENERATOR FAILED. THE CREW THEN ATTEMPTED - [SDR GLBA2013021500177](https://openairdocs.org/sdr/GLBA2013021500177), Feb 14, 2013: BULB. INOPERATIVE. PILOT REPORTED THAT THE EMERGENCY LIGHTS ON THE F/O'S SIDE DO NOT ILLUMINATE AND ARE ALSO INOPERATIVE IN INDIRECT LIGHT MODE. MX REPLACED THE BULBS AND SECURED - [SDR HSYA20110307001](https://openairdocs.org/sdr/HSYA20110307001), Mar 7, 2011: TORQUE LINK. DAMAGED. RT MLG TORQUE LINK DISCONNECTED AT START OF ACFT TAXING FROM BLOCKS. UPON INSP, MX DISCOVERED INCORRECT WASHER INSTALLATION AT UPPER AND LOWER TORQUE LINK ATTAC - [SDR GUUA94055030609D](https://openairdocs.org/sdr/GUUA94055030609D), Mar 6, 2009: SPAR CAP. CORRODED. DURING SCHEDULED ROUTINE INSP, DISCOVERED RT HORIZONTAL STABILIZER UPPER REAR SPAR CAP HAS EXFOLIATION. REPLACED RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR CAP - [SDR GUUA94055030609C](https://openairdocs.org/sdr/GUUA94055030609C), Mar 6, 2009: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR OTBD HINGE BRACKET HAS SURFACE CORROSION. REPLACED RT ELEVATOR OUTBOARD HINGE BRACKET. - [SDR GUUA94055030609B](https://openairdocs.org/sdr/GUUA94055030609B), Mar 6, 2009: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET. - [SDR GUUA93352011609A](https://openairdocs.org/sdr/GUUA93352011609A), Jan 16, 2009: DOOR. STIFF. DURING SCHEDULED ROUTINE MX, DISCOVERED RT FWD EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT FWD EMERGENCY EXIT DOOR OUTSIDE HANDLE. OPS CHECK OK. - [SDR TAS07003](https://openairdocs.org/sdr/TAS07003), Nov 16, 2007: CAP. CRACKED. MLG ACTUATOR WAS RECEIVED DUE TO INDICATIONS FOUND IN THE END CAP DURING ULTRASONIC TESTING. ACTUATOR WENT THROUGH A PRELIMINARY INSPECTION AND A COMPLETE FUNCT - [SDR TIM2005F00003](https://openairdocs.org/sdr/TIM2005F00003), Apr 4, 2005: SKIN. CORRODED. CORROSION FOUND ON LT AND RT ELEVATOR: AFT LOWER SPAR CAP LT SIDE, AFT LOWER SPAR CAP RT SIDE, LT OB HINGE, RT OB HINGE, RT CENTER HINGE, LT ELEVATOR TRIM TAB P - [SDR TIM2005F00002](https://openairdocs.org/sdr/TIM2005F00002), Apr 4, 2005: SKIN. CORRODED. CORROSION FOUND ON SKIN FS243-FS273 AND STRINGERS 14L-15R. (K) - [SDR HSY2005F00001](https://openairdocs.org/sdr/HSY2005F00001), Jan 14, 2005: SENSOR. DEFECTIVE. (MRR NR 01-011405) LOSS OF NR 1 ENGINE OIL PRESSURE. LOOSE AND LEAKING OIL TEMPERATURE SENSOR. LOOSE BUT IN SERVICEABLE CONDITION. REMOVED TEMPERATURE SENSOR, I - [SDR TIM2004F00000](https://openairdocs.org/sdr/TIM2004F00000), Sep 30, 2004: TUBE. PIN HOLE. WHILE DOING A ROUTINE INSPECTION, IT WAS NOTICED HYDRAULIC FLUID ON THE LOWER PORTION OF THE LT IB WING. AFTER CLEANING THE AREA AND PERFORMING A RETRACTION TES - [SDR GLBA2003072](https://openairdocs.org/sdr/GLBA2003072), Jun 2, 2003: PRESSURE SWITCH. MALFUNCTIONED. RIGHT EVIR ILLUM, ON T/O ROLL. CHECKED THE PRESSURE SOLENOID FOR OPERATION AND LEAKAGE AND RIGHT PROP PRESSURE SWITCH FOR PROPER OPERATION, BOTH GOOD. CHECKED R - [SDR GLBA2003070](https://openairdocs.org/sdr/GLBA2003070), Jun 1, 2003: FILTER. DIRTY. AIRCRAFT WILL NOT PRESSURIZE. CLEANED PRESSURE CONTROLLER FILTER, OPS CHECK GOOD. - [SDR GLBA2003071](https://openairdocs.org/sdr/GLBA2003071), May 30, 2003: SWITCH. OUT OF ADJUST. AIRCRAFT RETURNS, FLAPS WILL NOT RETRACT. ADJUSTED FLAP SAFETY SWITCH, OPS CK GOOD. - [SDR TIM2002F00010](https://openairdocs.org/sdr/TIM2002F00010), Feb 15, 2002: ANGLE. BROKEN. ANGLE LOCATED ABOVE THE ICE DOOR HINGE. THIS ANGLE HOLDS THE LOWER FIRE SEAL BULK HEAD WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, - [SDR AUS20020164](https://openairdocs.org/sdr/AUS20020164), Jan 31, 2002: LIGHT. FAILED. (AUS) RH MAIN LANDING GEAR POSITION LIGHT FAILED. - [SDR TIM2002F00009](https://openairdocs.org/sdr/TIM2002F00009), Jan 16, 2002: BOLT. CORRODED. BOLT PN 908200115, CONNECTING NOSE GEAR DRAG BRACE TO NOSE STRUT, AND BOLT PN 908200111 CONNECTING THE TWO DRAG BRACE HALVES WAS FOUND WITH PITTING TYPE CORROSI - [SDR OYG2002F00000](https://openairdocs.org/sdr/OYG2002F00000), Dec 5, 2001: COWLING. CRACKED. SEVERAL CRACKS WERE FOUND ON THE INSIDE OF THE AIR INLET COWL (HOT LIP) THESE CRACKS RUN HORIZONTALLY AND VERTICALLY ALONG THE WELD THE POSSIBLE CAUSE MIGHT BE - [SDR TIM2002F00004](https://openairdocs.org/sdr/TIM2002F00004), Dec 4, 2001: CABLE. BROKEN. AIRSTAIR DOOR CABLE BROKE, ALLOWING ONE SIDE OF THE DOOR TO REMAIN UNLOCKED. - [SDR 2003F00020](https://openairdocs.org/sdr/2003F00020), Nov 27, 2001: ANGLE. CRACKED. GJT - LEFT ENGINE NACELLE LOWER AFT BULKHEAD HAS SEVERAL CRACKS. REPLACED THE LEFT ENGINE COWLING REINFORCEMENT ANGLE, THE ENGINE TRUSS BRACKET RECEPTACLE, AND - [SDR 2003F00019](https://openairdocs.org/sdr/2003F00019), Nov 27, 2001: BRACKET. CRACKED. GJT - LEFT ENGINE NACELLE LOWER AFT BULKHEAD HAS SEVERAL CRACKS. STRUCTURAL REPAIRS ARE IN PROGRESS. (M) - [SDR TIM2001F00011](https://openairdocs.org/sdr/TIM2001F00011), Oct 16, 2001: WIRE. BROKEN. THE ICE VANE CONTROL WIRE NUMBER 20A20 BROKE AT THE TERMINAL END UNDER THE PANEL AT INST ZONE 245 CAUSING A SHORT WHICH CAUSED SMOKE IN THE COCKPIT. - [SDR TIM2001F00009](https://openairdocs.org/sdr/TIM2001F00009), Oct 15, 2001: BULKHEAD. CRACKED. THE LEFT COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS BROKEN OUT ON THE RIGHT LOWER SIDE. THE LOCATION IS WHERE ONE OF - [SDR 2001F00623](https://openairdocs.org/sdr/2001F00623), Oct 4, 2001: SHAFT. DEFECTIVE. INSPECTION OF FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE RIGHT OUTBOARD FLAP CABLE DEFECTIVE. THE INNER SHAFT RETAINER WAS NOT - [SDR TIM2001F00006](https://openairdocs.org/sdr/TIM2001F00006), May 22, 2001: B-NUT. LOOSE. OIL LINE TO THE TORQUE MANIFOLD, B-NUT CAME LOOSE, OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGINE WAS INSPECTED AS PER MM, LOW OIL PRESSU - [SDR GUU2001F00008](https://openairdocs.org/sdr/GUU2001F00008), Apr 25, 2001: HINGE BRACKET. CORRODED. DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGH - [SDR GUU2001F00007](https://openairdocs.org/sdr/GUU2001F00007), Apr 25, 2001: HINGE BRACKET. CORRODED. DURING SCHEDULED MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS ON INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT - [SDR 2001F00089](https://openairdocs.org/sdr/2001F00089), Apr 24, 2001: HINGE BRACKET. CORRODED. DURING SCHEDULED MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED LEFT E - [SDR 2001F00088](https://openairdocs.org/sdr/2001F00088), Apr 24, 2001: HINGE BRACKET. CORRODED. DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED RIG - [SDR ME42001F00000](https://openairdocs.org/sdr/ME42001F00000), Mar 26, 2001: SPRING. BROKEN. HARTZELL PROPELLER MODEL NUMBER HC-B4MP-3A/M10877K WITH SERIAL NUMBER FW778 WAS RECEIVED FOR HUB REPLACEMENT IAW AD NOTE 96-18-14. DURING THE DISASSEMBLY, THE S - [SDR 20000925SH017](https://openairdocs.org/sdr/20000925SH017), Sep 5, 2000: TRUSS. CRACKED. GJT - RIGHT ENGINE TRUSS MOUNT CRACKED NEAR WELD AT UPPER OUTBOARD ATTACH POINT. AREA ''A''. CRACKED AT TYPICAL LOCATION AS IDENTIFIED IN AD 95-02-18, BEECH SB - [SDR 20000725AP006](https://openairdocs.org/sdr/20000725AP006), Apr 26, 2000: BRACKET. CORRODED. DURING ROUTINE MAINTENANCE, RIGHT MIDDLE ELEVATOR ATTACH BRACKET HINGE CORRODED. REMOVED AND REPLACED MIDDLE ELEVATOR HINGE ATTACH BRACKET. (M) - [SDR MASA00018](https://openairdocs.org/sdr/MASA00018), Feb 10, 2000: BULB. UNSERVICEABLE. FLT 6202 - FLG-PHX - DURING STANDARD PRE-FLIGHT CHECK, THE CREW NOTED THE INSTRUMENT EMERGENCY LIGHT ON THE CAPTAINS SIDE WAS INOPERATIVE. THIS ITEM WAS DEFERRE - [SDR 20000725AP004](https://openairdocs.org/sdr/20000725AP004), Jul 1, 1999: TRUSS. CRACKED. C-2 INSPECTION, RIGHT ENGINE TRUSS HAS A CRACK AT INBOARD COWLING ATTACH BRACKET. REMOVED AND REPLACED RIGHT ENGINE TRUSS. (M) - [SDR 98ZZZM612](https://openairdocs.org/sdr/98ZZZM612), Jul 26, 1998: SWITCH. OUT OF ADJUST. FLT 9472 - TLH-TPA - GEAR WARNING HORN SOUNDS WITH GEAR UP AND FLAPS IN APPROACH POSITION. ADJUSTED APPROACH LIMITS SWITCH. OPERATIONAL CHECKS SATISFACTORY. (M) - [SDR 98ZZZM613](https://openairdocs.org/sdr/98ZZZM613), Jul 25, 1998: LEVER. OUT OF ADJUST. FLT 9483 - MIA-MCO - GEAR WARNING HORN SOUNDS WITH GEAR UP AND FLAPS MOVED INTO APPROACH. REPOSITIONED FLAP SELECTOR LEVER GUARD. OPERATIONAL CHECKS SATISFACTOR - [SDR 98ZZZX2865](https://openairdocs.org/sdr/98ZZZX2865), Jul 16, 1998: ACM. MALFUNCTIONED. RSW/MIA - FLT 9283 - ON TAKEOFF, SMOKEY SMELL WHEN ACM IS SELECTED. SMELL DISSIPATED AFTER 30 SECONDS. RAN AIRCRAFT ENGINES WITH ACM RUNNING. COULD NOT DUPLICAT - [SDR 98ZZZX2261](https://openairdocs.org/sdr/98ZZZX2261), Jun 4, 1998: BEARING. FAILED. TACHOMETER/GENERATOR WAS OVERHAULED 55.9 HOURS AGO. UNIT STOPPED WORKING. ON REMOVAL, FOUND DRIVE SHAFT SNAPPED IN TWO. ON DI SASSEMBLY, FOUND BOTH BEARINGS HAD - [SDR 98ZZZX2410](https://openairdocs.org/sdr/98ZZZX2410), Jun 3, 1998: LINE. CRACKED. EYW/MIA - FLT 5300 - LANDING GEAR DOES NOT RETRACT. REMOVED AND REPLACED RIGHT HAND 'UP' HYDRAULIC LINE. (X) All 87: https://openairdocs.org/model/beech-1900/reports.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Raytheon 1900](https://openairdocs.org/model/raytheon-1900): 0 registered aircraft, registry code 7150020 --- 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.