# N165YV: 1995 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-165
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: August 24, 1995
- Certificate issued: March 25, 2023
- Expires: March 31, 2030
- Mode S code: A1067B
- 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=165YV
- Page: https://openairdocs.org/aircraft/N165YV

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/N165YV/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 NYC97IA123](https://openairdocs.org/ntsb/NYC97IA123), Jun 19, 1997: Beech 1900D (N165YV), Clarksburg, WV, incident, minor damage. Probable cause: The right outboard flap detaching from the flap aft roller bearings, at the flap track, which was a result of the manufacturer's inadequate inspection program.

## FAA accident and incident reports (6)

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 20030331003809I](https://openairdocs.org/incident/20030331003809I), Mar 31, 2003: Beech 1900D (N165YV), Kansas City, MO. (-23) On March 31, 2003, flight 5443 at 1500 local time, aircraft s/n UE-165 while enroute from dodge city, KS, to Kansas City, MO, the landing gear failed to…
- [Incident 20011201038379I](https://openairdocs.org/incident/20011201038379I), Dec 1, 2001: Beech 1900D (N165YV), Clarksburg, WV. (-23) On the 01, December 2001, at 10:15 local time; aircraft N165YV on take off roll environmental bleed air failed. Take off was aborted, and the aircraft…
- [Incident 20010807019349I](https://openairdocs.org/incident/20010807019349I), Aug 7, 2001: Beech 1900D (N165YV), Pittsburgh, PA. (-23) On August 7, 2001 air midwest flight #5503, tail number N165YV was on approach to runway 28R at pit when the crew noted that the right engine oil…
- [Incident 20010125000699I](https://openairdocs.org/incident/20010125000699I), Jan 25, 2001: Beech 1900D (N165YV), Pittsburgh, PA, Minor damage. (-23) On 1-25-01, at 19:23 local time, amwa flight 588, N165YV, a BE-1900-D, departed pit enroute to fkl and returned after takeoff to pit, due to aft cargo…
- [Incident 20010119000269I](https://openairdocs.org/incident/20010119000269I), Jan 19, 2001: Beech 1900D (N165YV), Pittsburgh, PA. (-23) On 01-19-01, a BE-1900-D, amwa flight #5571, registered as N165YV, was reported to have aborted takeoff on runway 10C due to a number one fire warning…
- [Incident 19970619020319I](https://openairdocs.org/incident/19970619020319I), Jun 19, 1997: Beech 1900D (N165YV), Clarksburg, WV, Minor damage. During flap extend on approach loud pop. Ailerons became stiff. Landed. Flap attach fastener broke jamming ailerons

## Service difficulty reports (60, 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 GLBA2017083100683](https://openairdocs.org/sdr/GLBA2017083100683), Aug 29, 2017: SNUBBER. INOPERATIVE. MAINTENANCE REPORTED THAT THE CABIN DOOR FREE FALLS OPEN. REMOVED & REPLACED CABIN DOOR SNUBBER IAW MM 52-10-01. OPS CHECKED GOOD
- [SDR GLBA2017082800682](https://openairdocs.org/sdr/GLBA2017082800682), Aug 28, 2017: RIB. CRACKED. MAJOR REPAIR - MAINTENANCE REPORTED THAT THE LEFT HAND ELEVATOR'S OUTBOARD MOUNT BRACKET IS LOOSE AND BOTH ATTACHING RIBS ARE CRACKED. RIVET HOLES ARE CRACKED O
- [SDR GLBA2017053000663](https://openairdocs.org/sdr/GLBA2017053000663), May 28, 2017: CABLE. BENT. MAINTENANCE REPORTED THAT THE LOWER FORWARD AIRSTAIR DOOR CABLE ROD WAS BENT. REMOVED AND REPLACED THE LOWER FORWARD AIRSTAIR DOOR HANDRAIL CABLE IAW BMM 52-10-
- [SDR GLBA2016082400606](https://openairdocs.org/sdr/GLBA2016082400606), Aug 23, 2016: TRIM PANEL. UNSECURE. PILOT REPORTED THAT THE AIRSTAIR DOOR AFT TRIM IS LOOSE AND BINGING THE DOOR, PREVENTING THE DOOR FROM OPENING. MAINTENANCE REPLACED THE NUTS AND SECURED THE TR
- [SDR GLBA2015092900550](https://openairdocs.org/sdr/GLBA2015092900550), Sep 27, 2015: CLEVIS. BENT. DURING A MX INSPECTION, FOUND THAT THE AIRSTAIR DOOR LOWER FWD HANDRAIL CABLE CLEVIS WAS BENT. R & R THE CABLE ASSEMBLY IAW BMM 52-10-02. PN ON & OFF 1440-43GLA
- [SDR GLBA2015091600537](https://openairdocs.org/sdr/GLBA2015091600537), Sep 15, 2015: TIRE. BLOWN. THE NR 1 TIRE BLEW ON LANDING. THE TIRE DEVELOPED A FLAT SPOT DURING BRAKING THAT RESULTED IN LOSS OF TIRE PRESS. R & R THE NR 1 WHEEL ASSEMBLY IAW TC 1900-3240
- [SDR GLBA2015022700500](https://openairdocs.org/sdr/GLBA2015022700500), Feb 26, 2015: MASTER CYLINDER. WORN. PILOT REPORTED THAT THE LT BRAKE WAS INOPERATIVE FROM THE CAPTAIN SEAT, EXTREMELY SOFT FROM THE FIRST OFFICER SEAT. REPLACED O RINGS ON THE SWIVEL FITTINGS ON T
- [SDR GLBA2014120100474](https://openairdocs.org/sdr/GLBA2014120100474), Nov 29, 2014: CAM LOCK. LACK OF LUBE. PILOT REPORTED THAT THE MAIN CABIN DOOR HANDLE IS VERY DIFFICULT TO MOVE WHEN THE DOOR IS BROUGHT TO THE CLOSED POSITION, HANDLE IN NORMAL FASHION WITH DOOR OPE
- [SDR GLBA2014092200444](https://openairdocs.org/sdr/GLBA2014092200444), Sep 22, 2014: SKIN. DENTED. MAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND DENT IN THE VERT STAB LE, DENT AREA BEGINS AT CSS 54.026, JUST ABOVE RIB UPWARD TO CSS 66.00, DEPTH
- [SDR GLBA2014092200445](https://openairdocs.org/sdr/GLBA2014092200445), Sep 22, 2014: STRUCTURE. CRACKED. DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT FWD VERT STAB HAT SECTION AT FWD FLANGE BEND RADIUS, .20% CHORD & VSS 90.0, 1 INCH IN LENGTH. 
- [SDR GLBA2014091900442](https://openairdocs.org/sdr/GLBA2014091900442), Sep 18, 2014: RIB. CRACKED. MAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT WING INBD RIB AT JUNCTION WITH WING SPAR FS 288, RIB ANGLE DOUBLER CRACKED 1.1 
- [SDR GLBA2014091900440](https://openairdocs.org/sdr/GLBA2014091900440), Sep 17, 2014: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE FUSELAGE FRAME CHANNEL AT FS 177.35 & STRINGER 13L IN THE FRAME FLANGE BEND RADIUS
- [SDR GLBA2014091900441](https://openairdocs.org/sdr/GLBA2014091900441), Sep 17, 2014: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT FUSELAGE FRAME AT FS 177.35 & STRINGER 9AR RADIATING UPWARD FROM STRINGER 9AR C
- [SDR V0DR20140908002](https://openairdocs.org/sdr/V0DR20140908002), Sep 8, 2014: WHEEL. CRACKED. RECEIVED VENT BLOWER IN FOR OVERHAUL. THE TECHNICIAN WAS REASSEMBLING THE VENT BLOWER, AFTER GETTING THE BLOWER ASSEMBLY TOGETHER HE PREPARED THE VENT BLOWER TO
- [SDR V0DR20140908001](https://openairdocs.org/sdr/V0DR20140908001), Sep 8, 2014: O-RING. DETERIORATED. CUSTOMER REPORTED POSSIBLE OIL COMING FROM PROPELLER HUB & BLADE SOCKETS. RECEIVED PROPELLER ASSEMBLY IN, PRIOR TO DISASSEMBLY TECHNICIANS APPLIED PRESS FOR TRO
- [SDR GLBA2013082300302](https://openairdocs.org/sdr/GLBA2013082300302), Aug 22, 2013: HANDLE. UNSECURE. PILOT REPORTED THAT THE OUTSIDE HANDLE ON OVERWING EXIT 4C DOES NOT STAY SECURE IN FLIGHT. MX RESECURED THE OUTSIDE DOOR HANDLE. OPS CHECK GOOD REF BMM 52-20-00
- [SDR GLBA2013082300301](https://openairdocs.org/sdr/GLBA2013082300301), Aug 22, 2013: HANDLE. UNSECURE. PILOT REPORTED THE 4C OUTER HANDLE ON THE OVERWING EXIT IS POPPED. MX SECURED THE EMERGENCY EXIT OUTER HANDLE. OPS CHECKED GOOD REF BMM 52-20-00-201.
- [SDR GLBA2013062400264](https://openairdocs.org/sdr/GLBA2013062400264), Jun 24, 2013: MOTOR. ODOR. PILOT REPORTED THAT THEY SMELLED ELECTRICAL SMOKE IN THE AFT CABIN DURING SHUTDOWN. REPLACED THE FLAP MOTOR, SYS OPS CHECKED GOOD, NO BURNING ODOR NOTED.
- [SDR GLBA2012111400111](https://openairdocs.org/sdr/GLBA2012111400111), Nov 13, 2012: BULKHEAD. GOUGED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A GOUGE IN THE UPPER PRESSURE BULKHEAD AT FS 84.00 AT ANGLE ATTACH AREA ABOVE CENTER AVIONICS SHELF, TORN IN A TRIA
- [SDR GLBA2012111200106](https://openairdocs.org/sdr/GLBA2012111200106), Nov 12, 2012: BULKHEAD. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND SEVEN CRACKS IN THE RT FWD PRESSURE BULKHEAD AT FASTENERS, THE OTBD ROW TO DOUBLE ROW TO FASTENERS AT THE INBD EDGE
- [SDR GLBA2012051601](https://openairdocs.org/sdr/GLBA2012051601), May 15, 2012: ACTUATOR. INOPERATIVE. PILOT REPORTED LANDING GEAR FAILED TO EXTEND NORMALLY, PERFORMED MANUAL EXTENSION, DECLARED EMERGENCY, LANDED SAFELY. MX MEGGED WIRING FROM TB150 TO ALL ACTUATO
- [SDR GLBA2012051401](https://openairdocs.org/sdr/GLBA2012051401), May 12, 2012: ACTUATOR. INOPERATIVE. PILOT REPORTED THAT THE LANDING GEAR FAILED TO EXTEND NORMALLY, PERFORMED MANUAL EXTENSION, DECLARED AN EMERGENCY, LANDED SAFELY. MX WAS ABLE TO DUPLICATE PROBL
- [SDR GLBA2012051101](https://openairdocs.org/sdr/GLBA2012051101), May 10, 2012: POWERPACK. MALFUNCTIONED. PILOT REPORTED ON APPROACH, LANDING GEAR WOULD NOT EXTEND, DECLARED AN EMERGENCY, MANUALLY PUMPED GEAR DOWN, 3 GREENS, LANDED SAFELY. MX REPLACED THE HYD POWER 
- [SDR GLBA2012050701](https://openairdocs.org/sdr/GLBA2012050701), May 4, 2012: WIRE. DAMAGED. PILOT REPORTED THAT WHEN THEY TURNED ON THE MASTER PANEL LIGHT SWITCH, NOTICED AN ELECTRICAL BURNING ODOR, NO SMOKE NOTED, TURNED SWITCH OFF, ODOR WENT AWAY. MX
- [SDR GLBA20110912G](https://openairdocs.org/sdr/GLBA20110912G), Sep 11, 2011: ANNUNCIATOR. INOPERATIVE. PILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR DID NOT ILLUMINATE WITH THE PRESS-TO-TEST. MAINTENANCE REPLACED THE AUTOFEATHER ANNUNCIATOR, OPS CHECKED GOO
- [SDR GLBA20110805H](https://openairdocs.org/sdr/GLBA20110805H), Aug 4, 2011: SEAL. OUT OF POSITION. PILOT REPORTED THAT THE EMERGENCY EXIT DOOR AT 4C MAKES A LOUD SOUND DURING FLIGHT. MX REMOVED 4C EMER EXIT DOOR AND FOUND TRIM SEAL MISPLACED, REPOSITIONED SEA
- [SDR GLBA20110805G](https://openairdocs.org/sdr/GLBA20110805G), Aug 4, 2011: BULB. INOPERATIVE. PILOT REPORTED THAT THE LIGHT IN THE AS DOOR WINDOW DOES NOT COME ON WHEN PUSHED. MX REPLACED THE BULB IAW BMM 33-20-01, OPS CHECKED GOOD.
- [SDR GLBA20110715F](https://openairdocs.org/sdr/GLBA20110715F), Jul 13, 2011: OXYGEN MASK. STUCK. PILOT REPORTED THAT WHEN SELECTING EMERGENCY POSITION ON THE CAPT'S O2 MASK, IT WILL NOT MOVE FROM NORMAL POSITION TO 100 PERCENT. MX REPLACED THE MASK PN: 359-
- [SDR GLBA20110706M](https://openairdocs.org/sdr/GLBA20110706M), Jul 4, 2011: CABLE. WORN. "SUP" - DURING A WALK-AROUND, THE PILOT FOUND THE FWD BOTTOM A/S DOOR CABLE ROD END BENT. MX R & R THE FWD BOTTOM A/S DOOR CABLE IAW BMM 52-10-02, PN: 1440-43GL
- [SDR GLBA20110706L](https://openairdocs.org/sdr/GLBA20110706L), Jul 4, 2011: PANEL. LOOSE. DURING AN INSPECTION, THE PILOT FOUND THE EMERGENCY EXIT INTERIOR PANEL LOOSE. MX RESECURED SPRINGS ON EMERGENCY EXIT INTERIOR PANEL BUTTON IAW BMM 52-20-00.
- [SDR GLBA20110630O](https://openairdocs.org/sdr/GLBA20110630O), Jun 30, 2011: SWITCH. FALSE ACTIVATION. PILOT REPORTED THAT WHILE CLIMBING THROUGH 8,000 FT HAD A CABIN DOOR ANNUNCIATOR ILLUMINATE, NO EMERGENCY DECLARED, RETURN TO BASE. MX CHECKED CABIN DOOR SWITCH
- [SDR GLBA20110601F](https://openairdocs.org/sdr/GLBA20110601F), Jun 1, 2011: SKIN. DEBONDED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE AS DOOR SKIN DEBONDED FROM FWD TO AFT EDGE FROM THE LWR EDGE, AREA OF 24" BY 6". MAIN
- [SDR GLBA20110601J](https://openairdocs.org/sdr/GLBA20110601J), Jun 1, 2011: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND FRAME CRACK AT FS 164 & STRINGER 9AR AT THE STRINGER CUTOUT, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFF
- [SDR GLBA20110601G](https://openairdocs.org/sdr/GLBA20110601G), Jun 1, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE SKIN AT FS 150 & STRINGER 9AL AT THE LOWER SNUBBER MOUNT AND AS DOOR FUSEL
- [SDR GLBA20110601H](https://openairdocs.org/sdr/GLBA20110601H), Jun 1, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE FRAME AT FS 456 AT STRINGER 10R CUTOUT, LWR INBD EDGE, .25" IN LENGTH. MX REPAIRED THE A
- [SDR GLBA20110405H](https://openairdocs.org/sdr/GLBA20110405H), Apr 5, 2011: STRINGER. BENT. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND STRINGER 12L BENT AT FS 47.5, STRINGER 12L BENT 5" FROM FS 47.5 GOING AFT ALONG STRINGER
- [SDR GLBA201006151](https://openairdocs.org/sdr/GLBA201006151), Jun 15, 2010: UNKNOWN. ODOR. SIG EVENT - CREW AND PASSENGERS SMELT SMOKE FOR APPROX. 15 SECONDS DURING DESCENT INTO OLF, SMELL CLEARED AND NO FURTHER EVIDENCE OF FIRE, SWEPT CABIN, CARGO, A
- [SDR GLBA20090808A](https://openairdocs.org/sdr/GLBA20090808A), Aug 8, 2009: AUTOFEATHER SYS. MALFUNCTIONED. RT AUTOFEATHER ARM ANNUNCIATOR DID NOT ARM WHEN POWER APPLIED FOR TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE.
- [SDR GLBA20090410B](https://openairdocs.org/sdr/GLBA20090410B), Apr 10, 2009: INDICATOR. FLUCTUATES. DURING FLIGHT NOTICED 2 PERCENT FLUCTUATION ON NR 1 N 1 GAUGE AND FLUCTUATIONS ON NR 1 TORQUE GAUGE CONTINUED UNTIL SHUTDOWN. MAINTENANCE R & R LT BETA BLOCK AN
- [SDR GLBA20090304I](https://openairdocs.org/sdr/GLBA20090304I), Mar 3, 2009: SKIN. DENTED. DURING ROUTINE SHEDULED MAINTENANCE THE LT WING, OUTBOARD LEADING EDGE WAS FOUND DENTED AND REQUIRES REPLACEMENT. REPAIRED LT LEADING EDGE SECTION FROM WS 223-2
- [SDR GLBA20090227F](https://openairdocs.org/sdr/GLBA20090227F), Feb 26, 2009: FUEL TANK. DAMAGED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE DAMAGE ON THE LEFT AFT AUXILIARY FUEL TANK WALL WAS DISCOVERED. MAINTENANCE REMOVED AFT WALL OF THE LEFT HAN
- [SDR GLBA20090220A](https://openairdocs.org/sdr/GLBA20090220A), Feb 12, 2009: SKIN. DISTORTED. MAJOR REPAIR - LEFT HAND INBOARD WING UPPER AFT WING SKIN OUT OF CONTOUR AT STATIONS F.S. 301 W.S. 70 .022" F.S. 311 W.S. 70 .032", F.S. 319 W.S. 70 .035" F.S. 
- [SDR BSAASDR0710](https://openairdocs.org/sdr/BSAASDR0710), Apr 30, 2007: BYPASS VALVE. MALFUNCTIONED. INITIAL REPORT - DURING CLIMB, THE RIGHT ENVIR FAIL LIGHT CAME ON, CREW RETURNED TO STATION WITH NO FURTHER INCIDENT. INITIALLY DEFERRED PER MEL 21-4. THE PRECO
- [SDR BSAASDR0614](https://openairdocs.org/sdr/BSAASDR0614), Jun 6, 2006: SKIN. CORRODED. LEVEL 1 SURFACE CORROSION WAS FOUND IN THE LEFT AND RIGHT WINGS IN THE AREA OF THE QUICK DRAINS OUTBOARD OF THE NACELLES AND FORWARD OF THE SPAR AT WS 125 TO 12
- [SDR 69959](https://openairdocs.org/sdr/69959), Mar 25, 2005: WIRE. DAMAGED. CREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT. FIRST OFFICER OBSERVED SMOKE FROM AVIONICS BAY AREA. ALL AIRCRAFT SYSTEMS WERE OPERATING NORMALLY. REMOVED AND
- [SDR 63379](https://openairdocs.org/sdr/63379), Jul 26, 2004: HYDRAULIC SYSTEM. LOW. RECEIVED CALL FROM CAPTAIN HIS LT BRAKE WAS BLEEDING OFF. THEN CALLED MAINTENANCE IN PIT. BLEED LT BRAKE AND SERVICED HYDRAULIC BRAKE GROUND CK GOOD. LEAK CK GO
- [SDR 63383](https://openairdocs.org/sdr/63383), Jul 26, 2004: BRAKE. LOW. RECEIVED CALL FROM CREW ABOUT BRAKES FEELING SPONGY. CALLED PIT MAINTENANCE. BLEED LT AND RT BRAKES. SERVICED BRAKE HYDRAULIC RESERVIOR LEAK CK GOOD.
- [SDR 60371](https://openairdocs.org/sdr/60371), Apr 7, 2004: BRAKE. MALFUNCTIONED. CREW CALLED REPORTING BRAKES FELT SOFT. MAINTENANCE CALLED PIT.
- [SDR 58644](https://openairdocs.org/sdr/58644), Feb 6, 2004: SOLENOID. WORN. AFTER ARRIVAL TO PIT ON FLIGHT 5528. RIGHT PROP WENT INTO GROUND FINE. CORRECTIVE ACTION TAKEN R/R LOW PITCH SOLENOID CLEVIS HARDWARE RIGGED.
- [SDR 58596](https://openairdocs.org/sdr/58596), Feb 5, 2004: PROPELLER. OUT OF ADJUST. WHILE TAXIING IN ON FLIGHT 5433, THE RIGHT PROP STUCK IN LOW PITCH. THE AIRCRAFT ARRIVED AT THE GATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE LOW PITC

All 60: https://openairdocs.org/aircraft/N165YV/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/N165YV/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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