# N176YV: 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-176
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: October 20, 1995
- Mode S code: A131B1
- Registered owner: [Hill Air Executive Inc](https://openairdocs.org/faa-owner/HILL%20AIR%20EXECUTIVE%20INC)
- Location: [Fort Pierce, FL](https://openairdocs.org/faa-place/FL/Fort%20Pierce)
- Owner type: Corporation
- Owner's area on the map: 27.4631° N, 80.3066° W: Placed by OpenAirDocs at the center of ZIP code 34949, 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=176YV
- Page: https://openairdocs.org/aircraft/N176YV

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/N176YV/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 N176YV.

## 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 20071004022859I](https://openairdocs.org/incident/20071004022859I), Oct 4, 2007: Beech 1900D (N176YV), Kansas City, MO, No damage. (-23) After take off from mci, the crew noted the captain's eadi had failed and smelled of electrical. Returned to field and told tower what was wrong. Ground…
- [Incident 20060707013689I](https://openairdocs.org/incident/20060707013689I), Jul 7, 2006: Beech 1900D (N176YV), Pittsburgh, PA. (-23) The aircraft landed on runway 10L after reporting an unspecified mechanical problem while inbound. The ARFF responded and the aircraft taxied to the ramp…
- [Incident 20051219029929I](https://openairdocs.org/incident/20051219029929I), Dec 19, 2005: Beech 1900D (N176YV), Mcalester, OK. (-23) During cruise flight from hro to dfw, air midwest airlines flight 2628 experienced a left fire "t" handle warning light. Crew shut down left engine and…
- [Incident 20040318005639I](https://openairdocs.org/incident/20040318005639I), Mar 18, 2004: Beech 1900D (N176YV), Tampa, FL. (-23) On take off roll, crew noted a lack of proper acceleration. The crew verified both engines were producing adequate power and the parking brake was…
- [Incident 20030826021799I](https://openairdocs.org/incident/20030826021799I), Aug 26, 2003: Beech 1900D (N176YV), Valparaiso, FL. (-23) During final approach to vps, the landing gear was selected down. No down and lock indication was observed on any landing gear. One recycle attempt was…
- [Incident 20020712027259I](https://openairdocs.org/incident/20020712027259I), Jul 12, 2002: Beech 1900D (N176YV), Panama City, FL. (-23) During climb at 18000' on flight 5635 (pfn-tpa) a loud bang was heard followed by the illumination of the cabin door master warning annunciator. Flight…

## Service difficulty reports (57, 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 AMWA88439BC](https://openairdocs.org/sdr/AMWA88439BC), Nov 6, 2007: BATTERY. FAILED. DURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED THEN WENT OUT. MAINTENANCE REMOVED AND REPLACED BATTERY AND CLEARED DISCREPANCY.
- [SDR AMWA88091BC](https://openairdocs.org/sdr/AMWA88091BC), Oct 18, 2007: BATTERY. DISCHARGED. BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. BATTERY REPLACED BY MAINTENANCE, DISCREPANCY CLEARED. THIS TYPE ANNUNCIATOR DISCREPANCY IS CONSIDERED A NUISAN
- [SDR AMWA87824](https://openairdocs.org/sdr/AMWA87824), Oct 4, 2007: HSI. ODOR. ELECTRICAL ODOR REPORTED IN COCKPIT ON CLIMBOUT. RETURNED TO FIELD AND MAINTENANCE VERIFIED THAT PROBLEM ORIGINATING IN CAPTAIN'S EHSI. REMOVED AND REPLACED UNI
- [SDR AMWA0828013](https://openairdocs.org/sdr/AMWA0828013), Oct 2, 2007: SPAR CAP. CORRODED. BIO CORROSION LT MAIN SPAR, LWR CAP FROM APPROX WS119.5 TO WS122. REPAIRED IAW REPORT NR 6872 REV IR.
- [SDR AMWA0828013B](https://openairdocs.org/sdr/AMWA0828013B), Oct 2, 2007: FRAME. CHAFED. REPAIRED LT AND RT FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT FS 213.25.
- [SDR AMWA0828013J](https://openairdocs.org/sdr/AMWA0828013J), Oct 2, 2007: FRAME. CHAFED. REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 408.25.
- [SDR AMWA0828013D](https://openairdocs.org/sdr/AMWA0828013D), Oct 2, 2007: FRAME. CHAFED. REPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT FS 243.25, RT.
- [SDR AMWA0828013C](https://openairdocs.org/sdr/AMWA0828013C), Oct 2, 2007: FRAME. CHAFED. REPAIRED LT AND RT FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT FS 228.25.
- [SDR AMWA0828013G](https://openairdocs.org/sdr/AMWA0828013G), Oct 2, 2007: FRAME. CHAFED. REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 318.25.
- [SDR AMWA0828013H](https://openairdocs.org/sdr/AMWA0828013H), Oct 2, 2007: FRAME. CHAFED. REPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT RT FS 363.25.
- [SDR AMWA0828013K](https://openairdocs.org/sdr/AMWA0828013K), Oct 2, 2007: FRAME. CHAFED. REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 438.25.
- [SDR AMWA0828013I](https://openairdocs.org/sdr/AMWA0828013I), Oct 2, 2007: FRAME. CHAFED. REPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 378.25.
- [SDR AMWA0828013F](https://openairdocs.org/sdr/AMWA0828013F), Oct 2, 2007: FRAME. CHAFED. REPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT RT FS 303.25.
- [SDR AMWA0828013E](https://openairdocs.org/sdr/AMWA0828013E), Oct 2, 2007: FRAME. CHAFED. REPAIRED LT AND RT FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING AT FS 258.25.
- [SDR AMWA0828013A](https://openairdocs.org/sdr/AMWA0828013A), Oct 2, 2007: SKIN. DAMAGED. RT UPPER WING SKIN BETWEEN WS117.5 AND WS133 HAD NUMEROUS ELONGATED HOLES FROM OVERSIZED RIVETS. REPAIRED IAW REPORT NR 6878-1 REV IR.
- [SDR AMWA84517](https://openairdocs.org/sdr/AMWA84517), May 9, 2007: ANNUNCIATOR. WORN. UPON DEPART GEAR RETRACTED NORMALLY. NO PROBLEMS UNTIL GEAR EXTENSION. COULD NOT DETERMINE IF GEAR WAS COMPLETELY DOWN. FLEW BY TOWER AND THEY SAID IT APPEARED 
- [SDR AWM083022](https://openairdocs.org/sdr/AWM083022), Mar 3, 2007: B-NUT. LOOSE. WHEN CREW ARRIVED AT DESTINATION THEY CALLED INTO MAINT CONTROL AND WROTE UP THE LT BRAKES NOT GETTING FULL BRAKING ACTION. TIGHTENED B-NUT, CLEANED AND BLED BR
- [SDR AMW082983BC](https://openairdocs.org/sdr/AMW082983BC), Mar 1, 2007: BATTERY. FALSE INDICATION. WHILE IN FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. CREW PROCEEDED TO DESTINATION, LANDED SAFELY WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE LIGHT ILLUMINATIO
- [SDR AMWA82619BC](https://openairdocs.org/sdr/AMWA82619BC), Jan 22, 2007: BATTERY. DISCHARGED. BATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE W
- [SDR AMW1061218001](https://openairdocs.org/sdr/AMW1061218001), Dec 12, 2006: SENSOR. FAILED. DURING A LANDING GEAR RETRACT CHECK, IT WAS NOTICED THAT SPARKS AND SMOKE WAS EMITTING FROM THE LIQUID LOW LEVEL SENSOR INSTALLED ON THE LANDING GEAR POWER PACK
- [SDR AMW78306](https://openairdocs.org/sdr/AMW78306), Jul 7, 2006: FUEL CAP. MISSING. LT FUEL CAP CAME LOOSE ON CLIMB OUT AND WEDGED IN BETWEEN WING AND AILERON. EXTRA TRIM WAS REQUIRED FOR CLIMB, BUT AILERONS REMAINED FULLY CONTROLLABLE IN FLIGH
- [SDR 1060607019](https://openairdocs.org/sdr/1060607019), Jun 13, 2006: WEB. WORN. HOLE WORN ON WEB OF LT FIREWALL. LOOSE FASTENER FOUND TO HAVE CAME LOOSE AND WORE OUT THE HOLE. EXTRA CARE HAS BEEN TAKEN TO ENSURE THE FASTENER TO BE CHECKED F
- [SDR 1060406014A](https://openairdocs.org/sdr/1060406014A), Apr 26, 2006: SPAR. CORRODED. BIO CORROSION LT MAIN SPAR CAP FLANGE AT WS 124.588 REPAIRED IAW FIELD REPAIR FR-CO-01337 REV.1
- [SDR 1060406014](https://openairdocs.org/sdr/1060406014), Apr 26, 2006: SPAR. CORRODED. BIOCORROSION RT MAIN SPAR CAP FLANGE AT WS124.588 REPAIRED IAW FIELD REPAIR FR-CO-01337 REV.1
- [SDR 74809](https://openairdocs.org/sdr/74809), Dec 19, 2005: FIRE LOOP. FAILED. WHILE IN ROUTE, THE LT T-HANDLE ILLUMINATED. CREW COMPLIED WITH EMERGENCY CHECKLIST AND DIVERTED DECLARED EMERGENCY AND LANDED SAFELY WITH NO FURTHER INCIDENT. 
- [SDR 74784](https://openairdocs.org/sdr/74784), Dec 18, 2005: BRAKE. WEAK. WHILE TAXING IN, THE CREW NOTICED THE BRAKES WERE SPONGEY. THE AIRCRAFT WAS THEN FERRIED AND MAINTENANCE BLED THE BRAKES. NO PARTS USED.
- [SDR 74798](https://openairdocs.org/sdr/74798), Dec 18, 2005: MASTER CYLINDER. FAILED. DURING TAXI IN, THE CREW REPORTED THE BRAKES FEELING SPONGY. THEN FERRIED TO ICT WHERE MAINTENANCE REMOVED AND REPLACED THE MASTER CYLINDER.
- [SDR 71037](https://openairdocs.org/sdr/71037), May 26, 2005: BRAKE. MALFUNCTIONED. ON TAXI TO GATE BRAKES WERE SPONGY. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. THEREFORE NO PARTS WERE USED.
- [SDR 70122](https://openairdocs.org/sdr/70122), Apr 4, 2005: BRAKE. DIRTY. AFTER ARRIVING AT GATE IN DFW, CREW REPORTED LEFT BRAKE WEAK. MAINTENANCE CLEANED THE BRAKES. THEREFORE NO PARTS WERE USED.
- [SDR 68837](https://openairdocs.org/sdr/68837), Feb 1, 2005: BRAKE. FAILED. AFTER TAXI IN LEFT BRAKE WEAK. REMOVED AND REPLACED LT BRAKE.
- [SDR 67819](https://openairdocs.org/sdr/67819), Dec 21, 2004: BRAKE ASSY. SMOKE. AFTER LANDING IN MIA CREW NOTICED LEFT BRAKES SMOKING. CLEANED LEFT MAIN GEAR BRAKE ASSY. CHECK OK AT THIS TIME.
- [SDR 64107](https://openairdocs.org/sdr/64107), Aug 21, 2004: SOCKET. DIRTY. DISPATCH RECEIVED A CALL FROM MGW STATION THAT THEY HAD BEEN CONTACTED BY FLT 4740 AND INFORMED THAT THE AIRCRAFT DID NOT HAVE 3 GOOD DOWN AND LOCK INDICATIONS 
- [SDR 63455](https://openairdocs.org/sdr/63455), Jul 29, 2004: UPLOCK SWITCH. FAILED. AFTER TAKEOFF WHEN GEAR WAS RETRACTED THE LANDING GEAR IN-TRANSIT LIGHT REMAINED ILLUMINATED. CREW CONTACTED DISPATCH AND MAINTENANCE CONTROL. CREW WAS TOLD TO 
- [SDR 63428](https://openairdocs.org/sdr/63428), Jul 28, 2004: BRAKE ASSY. MALFUNCTIONED. WHILE TAXING IN AFTER LANDING IN TPA. CAPTAIN FELT THAT THE LT BRAKE FELT SPONGY. THEN CALLED MAINTENANCE. BRAKES WAS BLEED, OPS CK NORMAL.
- [SDR 59816](https://openairdocs.org/sdr/59816), Mar 18, 2004: NUT. LOOSE. ON TAKE OFF ROLL CREW NOTED A LACK OF PROPER ACCELERATION. ABORTED TAKE OFF RETURNED TO GATE. FOUND BRAKE ROD NUT LOOSE. IT WAS TIGHTENED.
- [SDR 57453](https://openairdocs.org/sdr/57453), Dec 29, 2003: BRAKE. INOPERATIVE. UPON LANDING RT BRAKES FELT SOFT. MAINTENANCE CALLED. BRAKES WERE BLEED. OPS CK NORMAL.
- [SDR AMWA44](https://openairdocs.org/sdr/AMWA44), Sep 2, 2003: RIB. CRACKED. RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-46, STRG 101-640000-42 ON RT SIDE AND STRG P/N 101-640000-41, STRG P/N 101-640000-37 (4EA CRACKS TOTAL ON THIS 
- [SDR AMWA43](https://openairdocs.org/sdr/AMWA43), Sep 2, 2003: RIB. CRACKED. RIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 STRG P/N 101-640000-42 BOTH RT SIDE AND STRG P/N 101-640000-37 STRG P/N 101-640000-45 ON LT SIDE (4 EA TOTAL
- [SDR AMWA42](https://openairdocs.org/sdr/AMWA42), Sep 2, 2003: RIB. CRACKED. RIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 FIRST STRG FWD OF AFT SPAR RT SIDE OF VERTICAL STABILIZER.
- [SDR 53866](https://openairdocs.org/sdr/53866), Aug 26, 2003: PRINTED CKT BOARD. FAULTY. UPON APPROACH TO VPS LANDING GEAR WOULD NOT EXTEND. A SECOND ATTEMP WAS MADE WITH THE SAME THING NO DOWN AND LOCKED INDICATION FLY BY OF TOWER AT VPS. CONFIRMED
- [SDR 98ZZZM891](https://openairdocs.org/sdr/98ZZZM891), Oct 10, 1998: SWITCH. MALFUNCTIONED. FLT 5633 - RETURNED TO THE FIELD IN MCI WHEN THE LEFT FIRE LOOP LIGHT CAME ON IN FLIGHT. MCI MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY, BUT DID CHANGE THE
- [SDR 98ZZZM885](https://openairdocs.org/sdr/98ZZZM885), Oct 10, 1998: SWITCH. MALFUNCTIONED. FLT 5665 - ICT-MCI - EN ROUTE, T-HANDLE AND FIRE LOOP ILLUMINATE INTERMITTENTLY. ICT MAINTENANCE FOUND AND REPAIRED CHAFFED WIRES UNDER THE LEFT FORWARD FLOORBO
- [SDR 98ZZZM883](https://openairdocs.org/sdr/98ZZZM883), Oct 9, 1998: HARNESS. LOOSE. FLT 5600 - RTF WHEN THE LT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. THE LEFT ENGINEWAS SHUT DOWN. EMERGENCY EQUIPMENT WAS CALLED. AIRCRAFT LANDED WITHOUT INCI
- [SDR 98ZZZM903](https://openairdocs.org/sdr/98ZZZM903), Oct 8, 1998: FIRE LOOP. MALFUNCTIONED. FLT 5601 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED FORWARD AND AFT FIRE LOOP DETECTORS, PERFORME
- [SDR 98ZZZM902](https://openairdocs.org/sdr/98ZZZM902), Oct 8, 1998: FIRE LOOP. MALFUNCTIONED. FLT 5601 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED FORWARD AND AFT FIRE LOOP DETECTORS, PERFORME
- [SDR 98ZZZM901](https://openairdocs.org/sdr/98ZZZM901), Oct 7, 1998: FIRE LOOP. LOOSE. FLIGHT 5609 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED. INTERMITTENTLY IN FLIGHT. MAINTENANCE FOUND LOOSE WIRE AT LOOP CONNECTOR. WIRE WAS RESOL
- [SDR 98ZZZM896](https://openairdocs.org/sdr/98ZZZM896), Mar 28, 1998: SKIN. CRACKED. OVERNIGHT MAINTENANCE IN ICT FOUND A 1 INCH CRACK IN TOP SKIN .5 INCH FROM INBOARD AND 9.5 INCH FROM TE ON RHOB FLAP. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001.
- [SDR 98ZZZM434](https://openairdocs.org/sdr/98ZZZM434), Jan 17, 1998: SKIN. LOOSE. IN ICT AT OVERNIGHT DETAIL NR 1 INSPECTION, MAINTENANCE FOUND SEVERAL RIVETS LOOSE AND PULLED THROUGH THE SKIN ON THE BOTTOM SKIN OF RT INBOARD FLAP. REPAIRED I
- [SDR 97ZZZM1196](https://openairdocs.org/sdr/97ZZZM1196), Oct 1, 1997: BRACKETS. WORN. FLAP WAS REMOVED FOR A CRACK REPAIR. INSPECTION FOUND ATTACH INBOARD BRACKET BOLT HOLES WORN. REPLACED INBOARD ATTACH BRACKETS, APPLIED DOUBLERS TO BRACKETS IAW
- [SDR 97ZZZM1195](https://openairdocs.org/sdr/97ZZZM1195), Oct 1, 1997: BRACKETS. WORN. FLAP WAS REMOVED FOR A CRACK REPAIR. INSPECTION FOUND ATTACH INBOARD BRACKET BOLT HOLES WORN. REPLACED INBOARD ATTACH BRACKETS, APPLIED DOUBLERS TO BRACKETS IAW

All 57: https://openairdocs.org/aircraft/N176YV/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/N176YV/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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