# N202UX: 1996 Beech 1900D

- Status: Valid registration
- Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162, 19 seats)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (Textron Aviation Inc.) (OpenAirDocs)
- Serial number: UE-202
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: March 8, 1996
- Certificate issued: March 25, 2023
- Expires: March 31, 2030
- Mode S code: A19B49
- Registered owner: [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC)
- Location: [Provo, UT](https://openairdocs.org/faa-place/UT/Provo)
- Owner type: Corporation
- Owner's area on the map: 40.2272° N, 111.6958° W: Placed by OpenAirDocs at the center of ZIP code 84601, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=202UX
- Page: https://openairdocs.org/aircraft/N202UX

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included.

## ADs that may apply (OpenAirDocs): 77 in force

### Matched by airframe (Beech 1900D)

- [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 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [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 2004-17-02](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 2003-09-12](https://openairdocs.org/ad/2003-09-12): Rivets · Textron 1900D. Effective Jun 27, 2003
- [AD 2003-04-26](https://openairdocs.org/ad/2003-04-26): AC Inverter and Inverter Sync Wire Shield · Textron 1900D. Effective Apr 21, 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 2002-14-19](https://openairdocs.org/ad/2002-14-19): Collins Air Data Computers (ADC) · Boeing DC-8-11, DC-8-12, DC-8-21 and 36 more. Effective Aug 23, 2002
- [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 2001-15-17](https://openairdocs.org/ad/2001-15-17): Transponder Control Panels · Bombardier ATR42-200, ATR42-300, ATR42-320 and 30 more. Effective Aug 20, 2001
- [AD 2001-11-03](https://openairdocs.org/ad/2001-11-03): Blower Motor Circuit · Textron 1900D, 58, 58A and 5 more. Effective Jul 20, 2001
- [AD 2001-04-05](https://openairdocs.org/ad/2001-04-05): Global Positioning System · Textron 1900D with STC SA00245WI-D. Effective Apr 9, 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 2000-19-04](https://openairdocs.org/ad/2000-19-04): Wing Fuel Quantity Wiring Harness · Textron 1900C, 1900C (C-12J) and 1900D. Effective Oct 31, 2000
- [AD 99-18-15](https://openairdocs.org/ad/99-18-15): Landing Gear Emergency Hand Pumps · Textron 1900D, B200, B300 and 1 more. Effective Sep 27, 1999
- [AD 99-16-12](https://openairdocs.org/ad/99-16-12): Electric Elevator Trim · Textron 1900D. Effective Sep 27, 1999
- [AD 99-12-07](https://openairdocs.org/ad/99-12-07): Passenger Oxygen Container And Mask Assembly · Textron 1900D. Effective Jul 23, 1999
- [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 99-09-15](https://openairdocs.org/ad/99-09-15): Flight Control Mechanism · Textron 1900D, 58, 58A and 5 more. Effective May 18, 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 98-13-11](https://openairdocs.org/ad/98-13-11): Ground Idle Low Pitch Stop System · Textron 1900D. Effective Aug 3, 1998
- [AD 98-09-12](https://openairdocs.org/ad/98-09-12): Inspect Communication Systems · Textron 1900D. Effective Jun 12, 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 97-17-08](https://openairdocs.org/ad/97-17-08): Propeller Mounting Bolts · Textron 1900D. Effective Sep 24, 1997
- [AD 97-10-14](https://openairdocs.org/ad/97-10-14): Stabilon Attachment Angles · Textron 1900D. Effective Jul 7, 1997
- [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 97-03-01](https://openairdocs.org/ad/97-03-01): Right-Hand Exhaust Stacks · Textron 1900D. Effective Mar 14, 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 96-22-12](https://openairdocs.org/ad/96-22-12): Inspect fuel filter assembly · Textron 1900C, 1900C (C-12J), 1900D and 1 more. Effective Dec 13, 1996
- [AD 96-15-01](https://openairdocs.org/ad/96-15-01): Windshield Heat Control Circuit Breakers · Textron 1900D. Effective Sep 19, 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 95-26-14](https://openairdocs.org/ad/95-26-14): Inspect Cabin Partition Bracket · Textron 1900D. Effective Jan 31, 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 95-02-17](https://openairdocs.org/ad/95-02-17): Elevator Trim Tab Control Cable · Textron 1900D. Effective Apr 17, 1995

### Matched by engine (Pratt & Whitney PT6A series)

- [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024
- [AD 2022-08-13](https://openairdocs.org/ad/2022-08-13): Turbine Section · Pratt & Whitney Canada PT6A-34, PT6A-34B, PT6A-34AG and 2 more. Effective May 27, 2022
- [AD 2016-05-13](https://openairdocs.org/ad/2016-05-13): Corrosion and perforation of the two-ply Cu-Be bellows in Woodward FCUs. · Pratt & Whitney Canada PT6A-60AG, PT6A-65AG, PT6A-67AF and 1 more. Effective Apr 22, 2016
- [AD 2014-17-08 R1](https://openairdocs.org/ad/2014-17-08-R1): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Jun 5, 2015
- [AD 2014-11-05](https://openairdocs.org/ad/2014-11-05): Reinforcement liner to the power turbine (PT) containment   
  ring and, for certain PT containment rings, adding scallops · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 18 more. Effective Aug 5, 2014
- [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012
- [AD 2011-25-12](https://openairdocs.org/ad/2011-25-12): Sun gear · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Dec 28, 2011
- [AD 2011-20-51](https://openairdocs.org/ad/2011-20-51): Gears · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Nov 1, 2011
- [AD 2004-25-18](https://openairdocs.org/ad/2004-25-18): Propeller governor assemblies · Pratt & Whitney Canada PT6A-60A and PT6A-65B. Effective Jan 18, 2005
- [AD 2002-23-13](https://openairdocs.org/ad/2002-23-13): Turbine Exhaust Ducts · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 20 more. Effective Dec 31, 2002
- [AD 2001-20-01](https://openairdocs.org/ad/2001-20-01): Compressor Bleed Valve Assembly · Pratt & Whitney Canada PT6A-114A and PT6A-25C. Effective Nov 5, 2001
- [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997
- [AD 95-13-08](https://openairdocs.org/ad/95-13-08): Compressor Turbine Disk · Pratt & Whitney Canada PT6A-67D. Effective Jul 12, 1995
- [AD 93-23-06](https://openairdocs.org/ad/93-23-06): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50. Effective Jan 26, 1994
- [AD 92-15-11](https://openairdocs.org/ad/92-15-11): Compressor Delivery Air Line (P3) Filter Assembly · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-21 and 7 more. Effective Aug 17, 1992
- [AD 90-12-05](https://openairdocs.org/ad/90-12-05): Engine Overhaul · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 3 more. Effective May 30, 1990
- [AD 86-10-05](https://openairdocs.org/ad/86-10-05): First Stage Compressor Hub · Pratt & Whitney Canada PT6A-42. Effective Jun 5, 1986
- [AD 80-08-12](https://openairdocs.org/ad/80-08-12): Fuel Pump Drive Coupling Splines · Pratt & Whitney Canada PT6A-11, PT6A-112, PT6A-135 and 24 more. Effective Apr 18, 1980
- [AD 80-04-02](https://openairdocs.org/ad/80-04-02): Push-Pull Control Terminal · Pratt & Whitney Canada PT6A-20, PT6A-6A, PT6A-6B and 1 more. Effective Feb 8, 1980
- [AD 78-17-07](https://openairdocs.org/ad/78-17-07): Fuel Control Unit · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Aug 31, 1978
- [AD 78-12-04](https://openairdocs.org/ad/78-12-04): No. 2 Bearing Pressure Oil Transfer Tube Assembly · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Jun 19, 1978
- [AD 75-06-01](https://openairdocs.org/ad/75-06-01): Gearbox Deterioration · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 11 more. Effective Apr 1, 1977
- [AD 75-11-04](https://openairdocs.org/ad/75-11-04): Reduction Gearbox Engine Distress · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 8 more. Effective May 20, 1975
- [AD 70-16-01](https://openairdocs.org/ad/70-16-01): Turbo Propeller Governors · Pratt & Whitney Canada PT6A-11, PT6A-11AG, PT6A-15AG and 5 more. Effective Aug 4, 1970
- [AD 69-23-06](https://openairdocs.org/ad/69-23-06): Fuel Pumps · Pratt & Whitney Canada PT6A-20, PT6A-27, PT6A-28 and 4 more. Effective Nov 15, 1969
- [AD 68-05-03](https://openairdocs.org/ad/68-05-03): Reverse Mode · Pratt & Whitney Canada PT6A-20 and PT6A-6B. Effective Feb 28, 1968

### 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 2006-24-11](https://openairdocs.org/ad/2006-24-11) (historical): Forward, vertical, and aft flanges · Hawker Beechcraft 1900C, 1900C (C-12J) and 1900D. Effective Dec 11, 2006
- [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 2014-17-08](https://openairdocs.org/ad/2014-17-08) (historical): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Oct 8, 2014
- [AD 88-24-02](https://openairdocs.org/ad/88-24-02) (historical): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50

All 87: https://openairdocs.org/aircraft/N202UX/ads.md

## Information bulletins (advisory) (10 in force)

- [SAIB 2026-02](https://openairdocs.org/saib/2026-02): Elevator Tab Control System. Issued Jan 21, 2026
- [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-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
- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015
- [SAIB NE-12-04](https://openairdocs.org/saib/NE-12-04): Turbine/ Turboprop Engine: Reduction Gearbox. Issued Nov 1, 2011
- [SAIB NE-10-47](https://openairdocs.org/saib/NE-10-47): Turbine Engine Compressor Section. Issued Aug 30, 2010
- [SAIB NE-06-34](https://openairdocs.org/saib/NE-06-34): . Issued Mar 21, 2006
- [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003

## NTSB investigations (1)

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 DEN05IA046](https://openairdocs.org/ntsb/DEN05IA046), Jan 4, 2005: Beech 1900D (N202UX), Denver, CO, incident, minor damage. Probable cause: the tug driver's failure to maintain operational control of the tug, resulting in impact with an airplane. Contributing factors include the tug driver's improper procedure, the tug driver's…

## FAA accident and incident reports (4)

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 20090125000809I](https://openairdocs.org/incident/20090125000809I), Jan 25, 2009: Beech 1900D (N202UX), Cheyenne, WY, Minor damage. While on approach into cys, crew had to place the window deice on hi heat to keep up with the ice. Crew maintained an airspeed of 150-140 KTS IAS on the…
- [Incident 20060831017789I](https://openairdocs.org/incident/20060831017789I), Aug 31, 2006: Beech 1900D (N202UX), Denver, CO. (-23) The first officer was flying the aircraft on flight 5182 from santa fe, NM to Denver co. the first officer reported that the right elevator control yoke…
- [Incident 20060202001689I](https://openairdocs.org/incident/20060202001689I), Feb 2, 2006: Beech 1900D (N202UX), Denver, CO, Minor damage. (-23) Captain's windshield heat cycled on and off with the switch in the off position. Descending into Denver the crew smelled smoke, shortly after that, smoke…
- [Incident 20050103000799I](https://openairdocs.org/incident/20050103000799I), Jan 3, 2005: Beech 1900D (N202UX), Denver, CO, Minor damage. (-23) Flight 5039 a BE-1900-D operated by glba had just completed boarding at den for a flight to mck. The engines had not been started and the air stair door…

## Service difficulty reports (77, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR GLBA2017022700635](https://openairdocs.org/sdr/GLBA2017022700635), Feb 24, 2017: DOWNLOCK SWITCH. INOPERATIVE. PILOTS REPORTED THAT THEY RECEIVED A GPWS WARNING FOR AN UNSAFE GEAR CONDITION DURING A RETURN TO FIELD FOR A CABIN DOOR ANNUNCIATOR. THE CREW MANUALLY EXTENDED
- [SDR GLBA2017022400634](https://openairdocs.org/sdr/GLBA2017022400634), Feb 22, 2017: SHAFT. WORN. MAINTENANCE NOTED THAT THE PAX DOOR HANDLE WAS LOOSE. REMOVED AND REPLACED THE PAX DOOR HANDLE SHAFT AND ROLL PIN IAW AMM 52-10-05. OPS CHECKED GOOD.
- [SDR GLBA2016111700616](https://openairdocs.org/sdr/GLBA2016111700616), Nov 16, 2016: CABLE. BROKEN. SIG EVENT, PILOT REPORTED THAT THE LOWER FORWARD CABIN DOOR CABLE BROKEN (HANDRAIL CABLE). MAINTENANCE REMOVED AND REPLACED THE LOWER FORWARD MAIN CABIN DOOR CA
- [SDR GLBA2016072600600](https://openairdocs.org/sdr/GLBA2016072600600), Jul 23, 2016: BOLT. DISLODGED. MAINTENANCE PERSONNEL NOTED THAT THE AIRSTAIR DOOR ACCUMULATOR TOP ATTACH BOLT FELL OUT OF THE HOUSING. MAINTENANCE ATTACHED THE AIRSTAIR DOOR SNUBBER TOP BOLT 
- [SDR GLBA2016072600001](https://openairdocs.org/sdr/GLBA2016072600001), Jul 23, 2016: BOLT. UNSECURE. SIGNIFICANT EVENT, PILOT NOTED THAT THE CABIN DOOR SNUBBER TOP ATTACH BOLT FELL OUT. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AN
- [SDR GLBA2016070800593](https://openairdocs.org/sdr/GLBA2016070800593), Jul 5, 2016: BOLT. BROKEN. PILOT REPORTED THAT THE ATTACHING BULT ON THE CABIN DOOR BROKE. MAINTENANCE REPLACED THE BOLT ON THE LOWER END OF THE CABIN DOOR STRUT IAW MM 52-10-01(1)(B) STE
- [SDR GLBA2016040700578](https://openairdocs.org/sdr/GLBA2016040700578), Apr 6, 2016: SKIN. CRACKED. MAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND THE FUSELAGE BELLY SKIN CORRODED & CRACKED AT FS 213.25 & STRINGER 14R, .2" IN LENGTH. SUPPLEMENTAL INFORMATIO
- [SDR GLBA2015111600558](https://openairdocs.org/sdr/GLBA2015111600558), Nov 15, 2015: BOLT. UNSECURE. PILOT REPORTED THAT THE DOOR SNUBBER BOLT CAME OFF. APPLIED LOCTITE 242 TO THE BOLT THREADS & REINSTALLED THE BOLT IAW TC 1900-5210 01 STEP 13. OPERATIONAL CHEC
- [SDR GLBA2015032500507](https://openairdocs.org/sdr/GLBA2015032500507), Mar 24, 2015: FAN. MALFUNCTIONED. PILOT REPORTED THAT THERE WAS LIGHT SMOKE COMING FROM THE FLOOR VENTS. REPLACED THE AFT VENT BLOWER IAW AIM 21-07. OPERATIONS CHECKED GOOD.
- [SDR GLBA2014110400463](https://openairdocs.org/sdr/GLBA2014110400463), Nov 2, 2014: SHIMMY DAMPENER. FAULTY. DURING TAXI OUT, THE CREW NOTED THAT THE ACFT WOULD NOT STEER TO THE RT WITH MAX DIFFERENTIAL BRAKING POWER & NOSE WHEEL STEERING. TOWED THE ACFT BACK TO THE GA
- [SDR GLBA2014082900434](https://openairdocs.org/sdr/GLBA2014082900434), Aug 29, 2014: FRAME. CORRODED. DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CORROSION ON THE FUSELAGE FRAME AT FS 198.25 BETWEEN STRINGERS 15L & 14L, UPPER SURFACE, AREA CORRODED 2.25 INCH
- [SDR GLBA2014082500432](https://openairdocs.org/sdr/GLBA2014082500432), Aug 25, 2014: RIB. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE RT WING INBD RIB AT BL 29 & WING SPAR, RIB FLANGE CRACKED AT JUNCTION WITH WING SPAR, APPROX 1 INCHES IN LENG
- [SDR GLBA2014082600433](https://openairdocs.org/sdr/GLBA2014082600433), Aug 25, 2014: REPAIR. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE LT HEAVY CLOSING ANGLE REPAIR AT FS 288.00, IN THE BEND RADIUS OF THE REPAIR ANGLE, .65 INCHES IN LENGTH. REP
- [SDR GLBA2014082500431](https://openairdocs.org/sdr/GLBA2014082500431), Aug 25, 2014: FRAME. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FLANGE RADIUS ON THE FRAME AT FS 451 & STRINGER 10R .5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFO
- [SDR GLBA2014052700415](https://openairdocs.org/sdr/GLBA2014052700415), May 25, 2014: ACTUATOR. FAILED. PILOT REPORTED THAT WHILE COMING IN ON FINAL SELECTED THE GEAR DOWN & AFTER THE LG CYCLED, THE LT GEAR FAILED TO ILLUMINATE DOWN & LOCKED, RAN CHECKLIST, FAILED
- [SDR GLBA2013122300363](https://openairdocs.org/sdr/GLBA2013122300363), Dec 20, 2013: LATCH. LACK OF LUBE. PILOT REPORTED THAT THE EMERGENCY EXIT DOOR AT 6C, EXTERIOR LATCH IS NOT STOWED. R & R 6C EMERGENCY DOOR IAW AMM 52-20-00, OPS CHECKED GOOD. LUBRICATED LATCH IA
- [SDR GLBA2013121300354](https://openairdocs.org/sdr/GLBA2013121300354), Dec 12, 2013: UNKNOWN. ODOR. PILOT REPORTED FUEL LEAKING ON THE RT WING LOWER SURFACE AT THE WING ROOT AT THE MID CHORD, ALSO HAS A STRONG FUEL ODOR IN CABIN. MAINTENANCE INSPECTED AUX TANK
- [SDR GLBA2013102200342](https://openairdocs.org/sdr/GLBA2013102200342), Oct 21, 2013: INDICATOR. MALFUNCTIONED. PILOT REPORTED AFTER TAKE OFF, LT PROP RPM ROSE TO 1730 FOR 15 SECS, PULLED BACK PROP LEVERS AND CONTINUED TO CLIMB, LEVELED OFF AND TRIED TO SYNC PROPS, RECEIV
- [SDR GLBA2012122100138](https://openairdocs.org/sdr/GLBA2012122100138), Dec 21, 2012: SPAR. CHAFED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CHAFED SPAR .035 ON TOP AND BOTTOM FLANGES AT HSS 98.197 AND A .5" CRACK EXTENDING FROM A RIVET HOLE ON THE BACK 
- [SDR GLBA2012113000124](https://openairdocs.org/sdr/GLBA2012113000124), Nov 30, 2012: SKIN. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND T/E DAMAGE .35" -.35" ON THE OTBD END OF THE LT ELEVATOR. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-27-005. MAJOR
- [SDR GLBA2012112800121](https://openairdocs.org/sdr/GLBA2012112800121), Nov 28, 2012: LONGERON. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS COMING OUT OF A RIVET HOLE ON LONGERON UNDER FINGER DOUBLER AT FS 107, .5" IN LENGTH. MX REPAIRED THE AFF
- [SDR GLBA2012112800120](https://openairdocs.org/sdr/GLBA2012112800120), Nov 28, 2012: STRUCTURE. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS COMING OUT OF RIVET HOLE, ONE CRACK COMING OUT OF ANOTHER RIVET HOLE ON THE LONGERON UNDER FINGER DOUBLER
- [SDR GLBA2012112600116](https://openairdocs.org/sdr/GLBA2012112600116), Nov 26, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND THE LT VERTICAL FWD SPAR CAP ANGLE HAS A CRACK AT TWO RIVETS AT FSS 84.10 AND 20 PERCENT CHORD, .25" IN LENGTH. MX R
- [SDR GLBA2012112600115](https://openairdocs.org/sdr/GLBA2012112600115), Nov 26, 2012: WEB. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE HORIZONTAL STABILIZER AFT SPAR WEB HAS A CRACK PROTRUDING OUT OF THE ACCESS HOLE AT HSS 00.00, .5" IN LENGTH. M
- [SDR GLBA2012112600114](https://openairdocs.org/sdr/GLBA2012112600114), Nov 26, 2012: ANGLE. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND THE VERTICAL STABILIZER RT FWD SPAR CAP ANGLE CRACKED BY TOP RIVET AT FSS 84.10 AND 20 PERCENT CHORD, .25" IN LENGTH
- [SDR GLBA2012112600113](https://openairdocs.org/sdr/GLBA2012112600113), Nov 26, 2012: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND FUSELAGE FRAME AT FS 107 AND STRINGER 8R CRACKED AT INBD FLANGE AT UPPER FASTENER HOLE, .5" IN LENGTH. MX REPAIRED T
- [SDR GLBA2012112600112](https://openairdocs.org/sdr/GLBA2012112600112), Nov 26, 2012: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND FUSELAGE FRAME AT FS 107.00 AND STRINGER 8L CRACKED AT INBD FLANGE TO UPPER FASTENER HOLD, .5" IN LENGTH. MX REPAIR
- [SDR GLBA2012081300030](https://openairdocs.org/sdr/GLBA2012081300030), Aug 11, 2012: SKIN. DENTED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A DENT AT WS 290.06 ON RT WING, 9" BY 4" AREA. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED 
- [SDR GLBA2012061211](https://openairdocs.org/sdr/GLBA2012061211), Jun 9, 2012: WIRE. BROKEN. LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED IN FLIGHT. CREW NOTICED ROUGHLY 10 MINUTES IN TO THE FLIGHT. MX REPAIRED A BROKEN WIRE BY SEAT 2A IAW WM 20-10-00, OP
- [SDR GLBA201206111](https://openairdocs.org/sdr/GLBA201206111), Jun 8, 2012: RELAY. FAILED. ON SELECTING GEAR DOWN ON APPROACH. LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED IMMEDIATELY. AFTER PERFORMING "FAILURE OF LANDING GEAR TO EXTEND NORMALLY" CHECKL
- [SDR GLBA20111122F](https://openairdocs.org/sdr/GLBA20111122F), Nov 21, 2011: DRAIN. LEAKING. THE FUEL PUMP FCU DRAIN IS DRIPPING ON THE LT ENGINE. MX BAGGED ALL DRAINS ON THE LEFT ENGINE, NO LEAKS NOTED.
- [SDR GLBA20111028F](https://openairdocs.org/sdr/GLBA20111028F), Oct 28, 2011: UNKNOWN. ODOR. PILOT REPORTED A BURNED RUBBER ODOR IN COCKPIT. MX INSPECTED AND FOUND NO ODORS IN THE COCKPIT OR CABIN, INSPECTED WINDSHIELD HEAT SYS, NO DEFECTS FOUND, RAN AC
- [SDR GLBA201110281](https://openairdocs.org/sdr/GLBA201110281), Oct 28, 2011: UNKNOWN. ODOR. BURNED RUBBER SMELL IN COCKPIT.
- [SDR GLBA20111017G](https://openairdocs.org/sdr/GLBA20111017G), Oct 14, 2011: PUMP. LEAKING. "SUP" -MX REPORTED THAT THE LT HP FUEL PUMP WAS LEAKING. MX REPLACED THE FCU, OPS CK GOOD.
- [SDR GLBA20111005F](https://openairdocs.org/sdr/GLBA20111005F), Oct 3, 2011: ANNUNCIATOR. NO INDICATION. PILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR IS NOT ILLUMINATING WHEN AUTOFEATHER SWITCH IS IN THE OFF POSITION. MX REPLACED LT UPLOCK SWITCH, OPS CHECKE
- [SDR GLBA20110929F](https://openairdocs.org/sdr/GLBA20110929F), Sep 28, 2011: PCB. INOPERATIVE. PILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR WILL NOT ILLUMINATE IN OFF OR TEST MODE. MX REPLACED THE PCB. OPS CHECKED GOOD.
- [SDR GLBA20110926H](https://openairdocs.org/sdr/GLBA20110926H), Sep 24, 2011: BULB. INOPERATIVE. PILOT REPORTED THAT THE H ON RT MAIN DOWN AND LOCKED ANNUNCIATOR DOES NOT ILLUMINATE. MX REPLACED THE BULB IAW BMM 33-10-00, OPS CHECKED GOOD.
- [SDR GLBA20110922F](https://openairdocs.org/sdr/GLBA20110922F), Sep 21, 2011: LINE. LEAKING. PILOT REPORTED THAT FUEL WAS LEAKING FROM THE RT WING OR WHEEL WELL. MX TIGHTENED THE LINE ON THE RT FUEL VENT IAW BMM 28-20-01, LEAK CHECKED GOOD.
- [SDR GLBA20110902F](https://openairdocs.org/sdr/GLBA20110902F), Sep 1, 2011: AUTOFEATHER SYS. MALFUNCTIONED. PILOT REPORTED THAT THE PROP WENT INTO AUTOFEATHER ON FINAL, THEN CAME BACK OUT, FELT LIKE THE RT SIDE. MX TROUBLESHOT THE SYS IAW WITH THE RUNSHEET AND BMM 61-
- [SDR GLBA20110824F](https://openairdocs.org/sdr/GLBA20110824F), Aug 23, 2011: POWER LEVER. SPLIT. PILOT REPORTED THAT WITH THE TORQUE SET AT 1000 LBS, RT PROP CYCLED IN & OUT OF FEATHER 3 TIMES WITH THE AFX ARMED. MX FOUND SPLIT IN THE POWER LEVERS, RIGGED L
- [SDR GLBA20110822J](https://openairdocs.org/sdr/GLBA20110822J), Aug 19, 2011: PUMP. LEAKING. PILOT REPORTED THAT THERE IS A FUEL LEAK FROM THE HIGH PRESSURE FUEL PUMP DRAIN ON THE LEFT ENGINE. MX REPLACED THE LEFT HIGH PRESSURE FUEL PUMP IAW 73-10-02 AN
- [SDR GLBA20110725F](https://openairdocs.org/sdr/GLBA20110725F), Jul 24, 2011: SOLENOID. DIRTY. PILOT REPORTED THAT THE RT ENGINE WENT INTO AUTOFEATHER DURING FLARE. MAINTENANCE CLEANED THE LOW PITCH STOP SOLENOID, PERFORMED AUTOFEATHER OPS CHECKED IAW 61-
- [SDR GLBA20110713G](https://openairdocs.org/sdr/GLBA20110713G), Jul 13, 2011: SKIN. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE LT BELLY SKIN AT FS 288 & WING SPAR JUNCTION CRACKED, 1.1" IN LENGTH. MAINTENANCE REP
- [SDR GLBA20110713F](https://openairdocs.org/sdr/GLBA20110713F), Jul 13, 2011: SKIN. LOOSE. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE RT BELLY SKIN AT FS 288 & WING SPAR JUNCTION HAS A PATCH WITH LOOSE FASTENERS. MAINTE
- [SDR GLBA20110712K](https://openairdocs.org/sdr/GLBA20110712K), Jul 12, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE RH HEAVY ANGLE CRACKED IN THE BEND RADIUS AT FS 288, FWD LEADING EDGE OF ANGLE, 2" IN
- [SDR GLBA20110712J](https://openairdocs.org/sdr/GLBA20110712J), Jul 12, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE LH HEAVY ANGLE CRACKED IN THE BEND RADIUS AT FS 288, FWD EDGE OF ANGLE, 1.75" IN LENG
- [SDR GLBA20110712G](https://openairdocs.org/sdr/GLBA20110712G), Jul 12, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE FUSELAGE FRAME AT FS 456 & STRINGER 10R IS CRACKED AT THE LOWER RADIUS OF THE CUTOUT,
- [SDR GLBA20110712H](https://openairdocs.org/sdr/GLBA20110712H), Jul 12, 2011: SKIN. CORRODED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE FUSELAGE BELLY SKIN AT FS 213.25 AND STRINGER 15R CORRODED IN AN AREA OF 1" BY .75". 
- [SDR GLBA20110706N](https://openairdocs.org/sdr/GLBA20110706N), Jul 4, 2011: GROUND WIRE. BROKEN. PILOT REPORTED THAT THE LT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED IN FLT. MX FOUND BROKEN GROUND WIRE MAKING INTERMITTENT CONNECTION. R & R JACK KNIFE SP
- [SDR GLBA20110112F](https://openairdocs.org/sdr/GLBA20110112F), Jan 12, 2011: SKIN. DAMAGED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE AIRSTAIR DOOR DAMAGED FROM FS 150.1 TO 177.35, 2" WIDE & 22" LONG ON THE BOTTOM OF THE DOOR INSIDE 

All 77: https://openairdocs.org/aircraft/N202UX/reports.md

## STCs that may be installed (OpenAirDocs) (243, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Beech 1900D)

- [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 SA02309SE](https://openairdocs.org/stc/SA02309SE): Installation of the Garmin G950 Integrated Avionics and Display System. AeroMech Incorporated
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12400WI](https://openairdocs.org/stc/SA12400WI): Installation of Garmin Avionics Modernization Package. Alpine Aviation, Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [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 SA02133SE](https://openairdocs.org/stc/SA02133SE): Installation of a Luma Technologies LT-4500 Series Integrated Light\Emitting Diode (LED) Display Panel and LT-3500 LED light modules. Luma Technologies LLC
- [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc
- [STC SA12345IB](https://openairdocs.org/stc/SA12345IB): Replacement of the Halon Type 1211 portable fire extinguisher with the Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC ST00052BO](https://openairdocs.org/stc/ST00052BO): Installation of a Rockwell Collins TCAS-94 Traffic Alert and Collision Avoidance Systemm (TCAS II)with dual Rockwell Collins TVI-920D TA/RA/VSI indicators and dual Rockwell Collins TDR-94D mode S transponders. Ameriflight LLC
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA12202IB](https://openairdocs.org/stc/SA12202IB): Installation of Garmin GWX Weather Radar System. Maxcraft Avionics Ltd
- [STC SA12133IB](https://openairdocs.org/stc/SA12133IB): Manufacture and Installation of EVASAIR Loading System Installation. Exploits Valley Air Services Ltd
- [STC SA11300DS](https://openairdocs.org/stc/SA11300DS): Upgrade previously installed Collins Aerospace Radar Altimeter. BHE & Associates Ltd
- [STC SA8695SW](https://openairdocs.org/stc/SA8695SW): Installation of a TCAS 791(TCAS I). Acron Aviation Inc
- [STC SA9210SC-D](https://openairdocs.org/stc/SA9210SC-D): Installation of the L-3 Communications Avionics Systems Infrared Imaging System (IRIS). Acron Aviation Inc
- [STC SA00349WI](https://openairdocs.org/stc/SA00349WI): Installation of a right-hand forward lavatory and toilet. Exploits Valley Air Service Ltd
- [STC SA00968NY](https://openairdocs.org/stc/SA00968NY): Configuration 1: Installation of Flight Data Recorder on a Raytheon Beechcraft 1900D in accordance with Design Maintenance Analysis Inc. MDL 1900, Revision 1 dated 8/26/99. Configuration 2: Installation of sensors and accelerometers. KGB Aviation Services LLC
- [STC ST02754NY](https://openairdocs.org/stc/ST02754NY): Replacement of JET PS835C or PS835D Battery packs with Securaplane XL244-D Battery Packs. Securaplane Technologies Inc
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA00322BO](https://openairdocs.org/stc/SA00322BO): Installation of a Supplemental Exterior Lighting System. ATI Engineering Services LLC
- [STC SA02264SE](https://openairdocs.org/stc/SA02264SE): Manufacture and installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc
- [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC SA00199IB](https://openairdocs.org/stc/SA00199IB): Manufacture and Installation, Emergency Evacuation Configuration. Bartel Mechanical and Aerospace
- [STC SA01050WI](https://openairdocs.org/stc/SA01050WI): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC. Lists 1900 Series
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA00128IB](https://openairdocs.org/stc/SA00128IB): Antenna Installation and Bulkhead Feedthrough. Avmax Aviation 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 SA02821AT](https://openairdocs.org/stc/SA02821AT): Installation of a Sandel Model ST3400 Terrain Awareness and Warning System (TAWS), with optional capability as a Traffic Collision Avoidance System (TCAS) Control Display Unit (CDU) or Radio Magnetic Indicator (RMI). Woven Electronics LLC
- [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 ST02793AT](https://openairdocs.org/stc/ST02793AT): Installation of a Honeywell Model MK VI Enhanced Ground Proximity Warning System (EGPWS). Woven Electronics, LLC
- [STC ST02794AT](https://openairdocs.org/stc/ST02794AT): Installation of a Garmin Model GPS 400 Global Positioning System (GPS). Woven Electronics, LLC
- [STC SA00083IB](https://openairdocs.org/stc/SA00083IB): Installation of 1900D Cargo Provisions. MUSKOKA MOD CENTRE INC
- [STC SA00078IB](https://openairdocs.org/stc/SA00078IB): Installation of Barrier Net in aircraft forward cabin. Exploits Valley Air Services
- [STC SA04786NY](https://openairdocs.org/stc/SA04786NY): Installation of new Emergency Exit on forward right hand side of aircraft cabin. Exploits Valley Air Services
- [STC SA00073IB](https://openairdocs.org/stc/SA00073IB): Installation of 1900D Cargo Provisions. ICARUS AERO INC
- [STC SA00070IB](https://openairdocs.org/stc/SA00070IB): Installation of the Cockpit Emergency Hatch. ICARUS AERO INC
- [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 SA02204CH](https://openairdocs.org/stc/SA02204CH): Installation of Parker Hannifin Nose Wheel conversion Kit. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA1789GL](https://openairdocs.org/stc/SA1789GL): Installation of Cleveland main wheels and brakes. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA01094DE](https://openairdocs.org/stc/SA01094DE): Installation of Pratt & Whitney Engine Services FAST (digital engine management) system. Pratt & Whitney Engine Services Inc
- [STC SA00033IB](https://openairdocs.org/stc/SA00033IB): Installation of Cargo Conversion. Exploits Valley Air Services Ltd
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA04675NY](https://openairdocs.org/stc/SA04675NY): Installation of Cargo Conversion. Exploits Valley Air Services Ltd
- [STC SA04634NY](https://openairdocs.org/stc/SA04634NY): Modification of the Brake Master Cylinder. Marsh Brothers Aviation Inc
- [STC SA00748DE](https://openairdocs.org/stc/SA00748DE): Installation of the Rockwell Collins IDS-3000 system with new Primary Flight Displays, Multi-Function Display, Display Control Panels, Audio Panels, and Engine Insturmentation. Textron Aviation Inc
- [STC SA04459NY](https://openairdocs.org/stc/SA04459NY): Installation of MT-Propeller Entwicklung GmbH model MTV-27-1-( )-C-F-R(P)/CFR260-65( ) 5-blade, constant speed, full feathering, reversible propellers and spinners. MT- Propeller Entwicklung GmbH
- [STC SA2841CE](https://openairdocs.org/stc/SA2841CE): Install a privacy partition and a non-belted toilet in aft cabin. Textron Aviation Inc
- [STC SA2842CE](https://openairdocs.org/stc/SA2842CE): Install a mid-baggage cargo net, option 1, or an aft bulkhead partition, option 2, in the aft cabin. Textron Aviation Inc

All 243: https://openairdocs.org/aircraft/N202UX/stcs.md

## Related

- Other Beech 1900D aircraft: https://openairdocs.org/model/beech-1900d/aircraft.md
- The Pratt & Whitney PT6A series engine: https://openairdocs.org/engine/pratt-whitney-pt6a-series.md

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