# N231YV: 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-231
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: August 16, 1996
- Certificate issued: March 25, 2023
- Expires: March 31, 2030
- Mode S code: A20E71
- 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=231YV
- Page: https://openairdocs.org/aircraft/N231YV

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/N231YV/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

None matched to N231YV.

## FAA accident and incident reports (5)

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 20100319030359I](https://openairdocs.org/incident/20100319030359I), Mar 19, 2010: Beech 1900D (N231YV), Ontario, CA, No damage. The # 1 engine bleed air annuciator light illuminated during take off roll. The pilot aborted and safely returned to the gate. Contract maintenance discovered…
- [Incident 20021030030839I](https://openairdocs.org/incident/20021030030839I), Oct 30, 2002: Beech 1900D (N231YV), PA. (-23) On September 30, 2002, at 20:15 local time, aircraft N231YV while en route from pit to lbr, nose landing gear annunciator did not illuminate after the…
- [Incident 20020911027289I](https://openairdocs.org/incident/20020911027289I), Sep 11, 2002: Beech 1900D (N231YV), Orlando, FL. (-23) On September 11, 2002 at 19:15 local time, aircraft N231YV'S cabin door annunciator illuminated in climb phase of flight. Aircraft returned to field with…
- [Incident 20010110000279I](https://openairdocs.org/incident/20010110000279I), Jan 10, 2001: Beech 1900D (N231YV), Kansas City, MO. (-23) On 01/01/01 flying from lit to mci lef tprop RPM suddenly dropped to 1000 and then continued dropping slowly to 500. Manually feathered left prop without…
- [Incident 19970912030179I](https://openairdocs.org/incident/19970912030179I), Sep 12, 1997: Beech 1900D (N231YV), Kansas City, MO. Narrative: aircraft was inbound to the Kansas City International Airport (mci) from garden city, Kansas when approximately 20NM northwest of mci flight…

## Service difficulty reports (90, 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 GLBA2017110300689](https://openairdocs.org/sdr/GLBA2017110300689), Nov 2, 2017: CABLE. BROKEN. MAINTENANCE REPORTED THAT THE LOWER FORWARD AIRSTAIR DOOR HANDRAIL CABLE WAS BROKEN INTERNALLY. REMOVED AND REPLACED THE FORWARD LOWER DOOR CABLE, P/N OFF/ON: 1
- [SDR GLBA2017072100676](https://openairdocs.org/sdr/GLBA2017072100676), Jul 18, 2017: COVER. WORN. MAINTENANCE REPORTED THAT THE AFT BOTTOM CABLE SHEATH WAS WORN ON THE PAX DOOR. REPLACED THE CABLE IAW MM 52-10-02.
- [SDR GLBA2017031300641](https://openairdocs.org/sdr/GLBA2017031300641), Mar 11, 2017: BRAKE SYS. CONTAMINATED. THE CREW REPORTED THE LEFT HAND BRAKE HAS TO BE PUMPED TO WORK, IT'S SPONGY. BOTH CAPTAIN AND COPILOT BRAKES ARE SPONGY ON LT SIDE. MAINTENANCE BLED THE LT BRAK
- [SDR GLBA2017030900639](https://openairdocs.org/sdr/GLBA2017030900639), Mar 7, 2017: BRAKE SYS. CONTAMINATED. CAPTAIN'S AND FIRST OFFICER'S LEFT BRAKE PEDALS WERE EXTREMELY SPONGY AND WENT TO FLOOR WITH VERY LITTLE TO NO BRAKING ABILITY. MAINTENANCE BLED THE LT BRAKE SY
- [SDR GLBA2017030700638](https://openairdocs.org/sdr/GLBA2017030700638), Mar 5, 2017: MASTER CYLINDER. CONTAMINATED. SIG EVENT - THE CREW REPORTED THAT THE CAPTAIN'S LEFT HAND BRAKE WAS SPONGY AND INEFFECTIVE. MAINTENANCE BLED THE CAPTAIN'S LEFT HAND BRAKE IAW BEECH 32-40-05. 
- [SDR GLBA2016060600591](https://openairdocs.org/sdr/GLBA2016060600591), Jun 3, 2016: MASTER CYLINDER. WORN. PILOT REPORTED THAT THE CAPTAINS SIDE LT BRAKE PEDAL IS NOT HOLDING & WENT TO THE FLOOR. REPLACED THE CAPTAINS LT BRAKE CYLINDER IAW 32-40-06, PN 90-380001-33 &
- [SDR GLBA2016042500583](https://openairdocs.org/sdr/GLBA2016042500583), Apr 24, 2016: PCB. FAULTY. PILOT REPORTED THAT THE AUTOFEATHER ARMED WITH N1 ABOUT 95%, AFX DISABLE ILLUMINATED & RT AUTOFEATHER FAILED TO ARM. REPLACED PCB A123, PN ON & OFF 129-364091-9
- [SDR GLBA2016042500582](https://openairdocs.org/sdr/GLBA2016042500582), Apr 23, 2016: UNKNOWN. MALFUNCTIONED. PILOT REPORTED THAT AFTER TAKEOFF, POWER WAS APPLIED, AFX DISABLE ANNUNCIATOR ILLUMINATED & RT AUTOFEATHER DISARMED, THEN REARMED. THEN AFTER ROTATION, RT AUTOF
- [SDR GLBA2016020900565](https://openairdocs.org/sdr/GLBA2016020900565), Feb 8, 2016: CONTROL HANDLE. BROKEN. PILOT REPORTED THAT THE LG FAILED TO EXTEND NORMALLY, FOLLOWED CHECKLIST. PERFORMED MANUAL EXTENSION, DOWN WITH 3 GREENS. JACKED ACFT RETRACTED GEAR 10 TIMES, N
- [SDR GLBA2015110900557](https://openairdocs.org/sdr/GLBA2015110900557), Nov 9, 2015: SPAR CAP. CORRODED. MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE RT REAR LOWER WING SPAR CAP FROM WING STATION 215.08 - 310. CORROSION ON THE AFT FLANGE GOING UP ON THE T
- [SDR GLBA2015110900556](https://openairdocs.org/sdr/GLBA2015110900556), Nov 9, 2015: SPAR. CORRODED. MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE RT REAR WING SPAR OTBD WEB CORRODED. REPAIRED IAW EO 15-1900-57-003.
- [SDR GLBA2014101600456](https://openairdocs.org/sdr/GLBA2014101600456), Oct 16, 2014: SKIN. CRACKED. DURING A SCHEDULED INSPECTION FOUND CRACK IN THE LT AFT FUSELAGE SKIN AT BS 549.25 BETWEEN STRINGERS 12 - 13L, 1.1 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-
- [SDR GLBA2014101600455](https://openairdocs.org/sdr/GLBA2014101600455), Oct 16, 2014: STRUCTURE. DAMAGED. DURING A SCHEDULED INSPECTION FOUND MULTIPLE FASTENER HOLES ELONGATED BETWEEN BS 531 - 557.5. ELONGATION RANGING FROM .20 INCHES TO .30 INCHES, FASTENER HOLES A
- [SDR GLBA2014101400454](https://openairdocs.org/sdr/GLBA2014101400454), Oct 14, 2014: SKIN. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE EMERGENCY EXIT DOOR 6C RT AFT INSIDE SKIN 0.875 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-52-005. MAJOR REPAI
- [SDR GLBA2014101000453](https://openairdocs.org/sdr/GLBA2014101000453), Oct 10, 2014: SKIN. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FUSELAGE SKIN AT FS 249.25 & STRINGER 12L UNDER LT VORTEX GEN 1.75 INCHES IN LENGTH. REPAIRED THE AFFECTED AR
- [SDR GLBA2014100900451](https://openairdocs.org/sdr/GLBA2014100900451), Oct 9, 2014: BULKHEAD. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CANTED BULKHEAD AT FS 588.10 & STRINGER 8L .65 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL R
- [SDR GLBA2014100900452](https://openairdocs.org/sdr/GLBA2014100900452), Oct 9, 2014: SKIN. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE UPPER FWD CORNER OF A/S DOOR CUT OUT FS 150.6 PROTRUDING UPWARD .75 INCHES IN LENGTH. REPAIRED THE AFFECTED A
- [SDR GLBA2014100800450](https://openairdocs.org/sdr/GLBA2014100800450), Oct 8, 2014: SPAR. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE AFT CTR HORIZONTAL STAB SPAR WEB, .125 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED 
- [SDR GLBA2014100800449](https://openairdocs.org/sdr/GLBA2014100800449), Oct 8, 2014: BULKHEAD. BUCKLED. DURING A SCHEDULED INSPECTION FOUND THE CANTED BULKHEAD AT FS 588.10 BUCKLED FROM STRINGER 12R TO STRINGER 11L. PREVIOUS REPAIR DOUBLER BETWEEN STRINGER 11L & 1
- [SDR GLBA2014100700448](https://openairdocs.org/sdr/GLBA2014100700448), Oct 7, 2014: FRAME. CRACKED. DURING A SCHEDULED INSPECTION FOUND 2 CRACKS IN THE FUSELAGE FRAME AT FS 183.25 AT 2 LOCATIONS. 1ST AT INBD CORNER AREA AT ENVIRONMENTAL DUCT CUT OUT, ONE CRACK
- [SDR GLBA2014092600446](https://openairdocs.org/sdr/GLBA2014092600446), Sep 26, 2014: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION FOUND A LIGHTNING STRIKE ON THE OTBD TE LT ELEVATOR JUST OTBD OF THE MOST OTBD STATIC WICK. SKIN HAS .5 INCH X .25 INCH DAMAGE STA
- [SDR GLBA2014082900435](https://openairdocs.org/sdr/GLBA2014082900435), Aug 29, 2014: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION MAINTENANCE, FOUND WING SKIN BENT UPWARDS ON TRAILING EDGE BETWEEN WS 114.25 & 124.25. REPAIRED IAW EO 14-1900-57-006.
- [SDR GLBA2013013000166](https://openairdocs.org/sdr/GLBA2013013000166), Jan 30, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 107 AND STRINGER 8R, FRAME CRACK PROTRUDING OUT OF RIVET, .5 INCH IN LENGTH. REPAIRED IAW EO 13-1900-5
- [SDR GLBA2013013000165](https://openairdocs.org/sdr/GLBA2013013000165), Jan 30, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS AT FS 107 AND STRINGER 8L IN THE BEND RADIUS, CRACK PROTRUDING OUT OF RIVET, 1.25 INCHES IN LENGTH. REPAI
- [SDR GLBA2013013000164](https://openairdocs.org/sdr/GLBA2013013000164), Jan 30, 2013: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 456 AT THE GAS STRUT UPPER INBD NUTPLATE BETWEEN STRINGERS 3L AN
- [SDR GLBA2012030901](https://openairdocs.org/sdr/GLBA2012030901), Mar 8, 2012: RIB. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE LT CENTER WING L/E INBD RIB AND REINFORCEMENT STRAP 1.5" FWD OF SPAR, 1" IN LENGTH. REPAIRED THE AFF
- [SDR GLBA2012030101](https://openairdocs.org/sdr/GLBA2012030101), Mar 1, 2012: SPAR CAP. CHAFED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CHAFE ON THE LT WING FWD LOWER SPAR CAP AT BL 29.5, APPROX 1" BY .312" AT WIDEST POINT, .125" TO .
- [SDR GLBA20111111F](https://openairdocs.org/sdr/GLBA20111111F), Nov 10, 2011: CABLE. FRAYED. PILOT REPORTED THAT THE TOP AFT AIRSTAIR DOOR CABLE IS FRAYED. MX REPLACED THE TOP AFT DOOR CABLE, OPS CHECKED GOOD.
- [SDR GLBA20110823H](https://openairdocs.org/sdr/GLBA20110823H), Aug 23, 2011: SKIN. DEBONDED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP MX FOUND THE RT WINGLET DEBONDED AT THE INBD EDGES AND A HOLE IN THE L/E NEXT TO THE UNDER LIGHT DAM. MX REPLACED
- [SDR GLBA20110818K](https://openairdocs.org/sdr/GLBA20110818K), Aug 17, 2011: RAIL. WORN. AIRSTAIR DOOR AFT UPPER HAND RAIL WORN. MX REPLACED THE RAIL IAW BMM 52-10-02, OPS CK GOOD.
- [SDR GLBA20110810F](https://openairdocs.org/sdr/GLBA20110810F), Aug 9, 2011: SCREW. MISSING. PILOT REPORTED THAT A SCREW WAS MISSING FROM THE CABIN DOOR. MX REPLACED THE SCREW.
- [SDR GLBA20110808H](https://openairdocs.org/sdr/GLBA20110808H), Aug 5, 2011: GOVERNOR. INOPERATIVE. PILOT REPORTED THAT DURING THE AFX TEST, RT PROP DID NOT FEATHER. MX RESEATED A173 PCB IAW MI 24-01 AND REPLACED THE RT OVERSPEED GOV IAW BMM 61-20-01, PN: 2109
- [SDR GLBA20110803H](https://openairdocs.org/sdr/GLBA20110803H), Aug 3, 2011: CAP. DAMAGED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE RT STABILON END CAP DAMAGED FROM TE FWD 10.7" AND FROM T/E OTBD TIP 7" GOING 2.5" PAST SPLICE. MX R
- [SDR GLBA20110801J](https://openairdocs.org/sdr/GLBA20110801J), Jul 30, 2011: SWITCH. INOPERATIVE. PILOT REPORTED THAT THE LT AUTOFEATHER INTERMITTENT AFX REPEATER AND LT AUTOFEATHER ANNC WENT OFF DURING TAKEOFF ROLL, ABORTED AND EXITED RUNWAY. MX REPLACE THE
- [SDR GLBA20110727J](https://openairdocs.org/sdr/GLBA20110727J), Jul 26, 2011: PCB. INOPERATIVE. PILOT REPORTED THAT ON DECENT THE RT AUTOFEATHER DID NOT ARM. MX REPLACED PCB A123 PN: 129-304091-9 SN: 735599 IAW AIM MI 24-01, OPS CK GOOD.
- [SDR GLBA20110727H](https://openairdocs.org/sdr/GLBA20110727H), Jul 26, 2011: PCB. INOPERATIVE. PILOT REPORTED THAT THE LT AUTOFEATHER SYS DID NOT ARM ON TAKEOFF ROLL. MX REPLACED PCB A123 IAW AIM MI 24-01.
- [SDR GLBA20110711N](https://openairdocs.org/sdr/GLBA20110711N), Jul 10, 2011: PCB. INOPERATIVE. PILOT REPORTED THAT THE LT AUTOFEATHER DISARMED ON TAKEOFF ROLL AT 65 KNOTS, ABORTED TAKEOFF. MX WAS ABLE TO DUPLICATE BY MOVING J2 CONNECTOR OF A123PCB, R & R 
- [SDR GLBA20110711H](https://openairdocs.org/sdr/GLBA20110711H), Jul 8, 2011: CONNECTOR. GROUNDED. PILOT REPORTED THAT WITH THE GEAR HANDLE IN THE UP POSITION "AUTOFEATHER OFF" ANNUNCIATOR ILLUMINATED WITH THE AUTOFEATHER SWITCH IN THE ARM AND OFF POSITION. M
- [SDR GLBA20110629F](https://openairdocs.org/sdr/GLBA20110629F), Jun 29, 2011: SKIN. DEBONDED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE AIRSTAIR DOOR EXTERIOR SKIN DEBONDING IN A 7" X 7" AREA AROUND THE PRESSURE LOCK. MX REPAIRED THE A
- [SDR GLBA20110627J](https://openairdocs.org/sdr/GLBA20110627J), Jun 27, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP MX FOUND A CRACK IN THE AIR STAIR DOOR LOWER FRAME AT THE LOWER AFT CORNER, .75" IN LENGTH. MAINTENANCE REPAIRED 
- [SDR GLBA20110627H](https://openairdocs.org/sdr/GLBA20110627H), Jun 27, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 456 AND STRINGER 10R, .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA 
- [SDR GLBA20110627G](https://openairdocs.org/sdr/GLBA20110627G), Jun 27, 2011: SKIN. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE INNER SKIN OF THE EMERGENCY EXIT AT 6A, VERT LENGTH 3.25"M ABD HORZ 3". MX REPAIRED THE 
- [SDR GLBA20100826F](https://openairdocs.org/sdr/GLBA20100826F), Aug 25, 2010: VALVE. INOPERATIVE. PILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND ON FINAL APPROACH, GEAR FAILED TO EXTEND AND LANDING GEAR RELAY TRIPPED, GEAR WAS MANUALLY EXTENDED SUCCESSF
- [SDR GLBA201008231](https://openairdocs.org/sdr/GLBA201008231), Aug 23, 2010: POWERPACK. FAILED. PILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND ON FINAL APPROACH, INTRANSIT LIGHT WAS ON AND NOTICED THAT THE GEAR RELAY CB POPPED, EXTENDED THE LANDING GE
- [SDR GLBA201005301](https://openairdocs.org/sdr/GLBA201005301), May 30, 2010: BULB. BURNED OUT. PILOT REPORTED AFTER LANDING THAT THE EMERGENCY INSTRUMENT LIGHT SECOND FROM THE LEFT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT IAW 1
- [SDR GLBA20100112F](https://openairdocs.org/sdr/GLBA20100112F), Jan 12, 2010: SKIN. CRACKED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND BETWEEN 2 RIVETS AT FS 290 AND BL 30L ON THE BOTTOM OF THE LT LOWER FUSELAGE AFT OF THE FWD WING SP
- [SDR GLBA20100107F](https://openairdocs.org/sdr/GLBA20100107F), Jan 7, 2010: SKIN. CRACKED. DURING ROUTINE SCHEDULED MX, A SMALL CRACK IN THE SKIN WAS FOUND AT FS 265 2.5" OTBD OF STR 13R. CRACK APPROX .250" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND
- [SDR GLBA20100104J](https://openairdocs.org/sdr/GLBA20100104J), Jan 4, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MX 2 CRACKS WERE FOUND AT THE AIRSTAIR DOOR FUSELAGE FRAME AT FS 150 AT THE LWR STRUT MOUNT AREA. CRACKS MEASURE 1" AND 
- [SDR GLBA20100104H](https://openairdocs.org/sdr/GLBA20100104H), Jan 4, 2010: STRINGER. CRACKED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND AT STRINGER 4R CUTOUT AT FS 288. IT EXTENDS OUTWARD AND DOWNWARD AT A 45 DEG ANGLE. CRACK IS APPROX
- [SDR GLBA20100104G](https://openairdocs.org/sdr/GLBA20100104G), Jan 4, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MX CRACK WAS FOUND IN THE RT SIDEWALL FRAME AT TS 164 AND STRINGER 9AR CUTOUT. CRACK IS APPROX 1.75" IN LENGTH. MX REPAI

All 90: https://openairdocs.org/aircraft/N231YV/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/N231YV/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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