# N195GL: 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-195
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: January 30, 1996
- Certificate issued: March 25, 2023
- Expires: March 31, 2030
- Mode S code: A17B5F
- 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=195GL
- Page: https://openairdocs.org/aircraft/N195GL

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/N195GL/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 CEN10LA315](https://openairdocs.org/ntsb/CEN10LA315), Jun 12, 2010: Beech 1900D (N195GL), Denver, CO, substantial damage. Probable cause: The pre-existent damage of the right-hand landing gear actuator attachment lug which led to fatigue cracking and eventual overload failure resulting in a collapsed gear upon landing.

## FAA accident and incident reports (4)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20100612039289A](https://openairdocs.org/incident/20100612039289A), Jun 12, 2010: Beech 1900D (N195GL), Denver, CO, Substantial damage. On June 14, 2010, glba director of ops reported:this part 91 reposition flight was to be operated from den to cys it returned to land in den. The crew reported…
- [Incident 20090204001129I](https://openairdocs.org/incident/20090204001129I), Feb 4, 2009: Beech 1900D (N195GL), Manhattan, KS, Minor damage. (-23) Great lakes 5117, operating as a 121 domestic revenue flight, departed Kansas city international airport (mci) and was enroute to Manhattan, Kansas…
- [Incident 20031105029649I](https://openairdocs.org/incident/20031105029649I), Nov 5, 2003: Beech 1900D (N195GL), Brookings, SD, Substantial damage. (-23) The aircraft was approximately 10 miles west of Brookings, SD descending to bkx. The aircraft hit multiple large birds. There was damage to the radome,…
- [Incident 20010821032669I](https://openairdocs.org/incident/20010821032669I), Aug 21, 2001: Beech 1900D (N195GL), Garden City, KS, Minor damage. (-23) Airport mower was mowing around light along taxiway without clearance. Aircraft taxied along taxiway and failed to recognize that wing tip would not…

## Reports on N195GL not matched to an aircraft (2)

They name N195GL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 19911101055409I](https://openairdocs.org/incident/19911101055409I), Nov 1, 1991: Beech 1900C (N195GL), Omaha, NE. Experienced NR2 engine decoupling and automatic shutdown. Diverted to Omaha. Landed safely.
- [Incident 19910911046759I](https://openairdocs.org/incident/19910911046759I), Sep 11, 1991: Beech 1900C (N195GL), Grand Forks, ND. Unsafe gear indication on final. Used emergency procedures. Landed safely. O ring failed on hydraulic accumulator.

## Service difficulty reports (85, 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 GLBA2018030800702](https://openairdocs.org/sdr/GLBA2018030800702), Mar 6, 2018: CABLE. FRAYED. MAINTENANCE REPORTED THAT THE AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE IS FRAYED. MAINTENANCE REMOVED AND REPLACED AIRSTAIR DOOR LOWER FORWARD HANDRAIL CABLE 
- [SDR GLBA2017121500697](https://openairdocs.org/sdr/GLBA2017121500697), Dec 15, 2017: DOOR FRAME. CRACKED. MAJOR REPAIR - MAINTENANCE NOTED THAT THE FUSELAGE DOOR FRAME WAS CRACKED AT STRINGER 11L AND FS 171.0. CRACK IS APPROXIMATELY 1.1 INCHES IN LENGTH. ** SUPPLEME
- [SDR GLBA2017081800678](https://openairdocs.org/sdr/GLBA2017081800678), Aug 15, 2017: HINGE. LOOSE. MAINTENANCE REPORTED THAT THE AIRCRAFT SIDE OF THE AIRSTAIR DOOR HINGE HAD AFT RIVETS WHICH WERE LOOSE. REMOVED AND REPLACED LOOSE RIVETS REF SRM 51-40-03.
- [SDR GLBA2017063000669](https://openairdocs.org/sdr/GLBA2017063000669), Jun 28, 2017: CABLE. WORN. MAINTENANCE REPORTED THAT THE UPPER AFT AIRSTAIR CABLE IS WORN. REMOVED AND REPLACED THE UPPER AFT AIRSTAIR CABLE IAW AMM 52-10-02.
- [SDR GLBA2017063000668](https://openairdocs.org/sdr/GLBA2017063000668), Jun 28, 2017: CABLE. WORN. MAINTENANCE REPORTED THAT THE UPPER FWD AIRSTAIR CABLE IS WORN. REMOVED AND REPLACED THE UPPER FWD AIRSTAIR CABLE IAW AMM 52-10-02. PN OFF/ON: 1440-42GLA, NSN.
- [SDR GLBA2017051000654](https://openairdocs.org/sdr/GLBA2017051000654), May 8, 2017: CIRCUIT BREAKER. POPPED. SIG EVENT, THE CREW DECLARED AN EMERGENCY ON APPROACH FOR LANDING [GEAR] FAILED TO EXTEND NORMALLY. IN TRANSIT LIGHT ILLUMINATED. MAINTENANCE FOUND 60A(CB11) PO
- [SDR GLBA2017041300648](https://openairdocs.org/sdr/GLBA2017041300648), Apr 11, 2017: PRESSURE SWITCH. DIRTY. THE CREW NOTED THAT THEY EXPERIENCED AN UNSCHEDULED AUTOFEATHER CYCLING DURING APPROACH TO LAND. THE ISSUE OCCURRED ON THE RIGHT ENGINE. MAINTENANCE REMOVED AND
- [SDR GLBA2017020300632](https://openairdocs.org/sdr/GLBA2017020300632), Feb 2, 2017: CABLE. BROKEN. MAINTENANCE NOTED THAT THE LOWER FWD AIRSTAIR DOOR CABLE WAS BROKEN.
- [SDR GLBA2017012500630](https://openairdocs.org/sdr/GLBA2017012500630), Jan 23, 2017: CABLE. BROKEN. SIG EVENT, PILOT REPORTED THAT THE A/S DOOR CABLE BROKE. ** SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPERW
- [SDR GLBA2016071300596](https://openairdocs.org/sdr/GLBA2016071300596), Jul 12, 2016: SNUBBER. DISCONNECTED. PILOT REPORTED THAT THE AIRSTAIR DOOR SNUBBER ARM CENTER PIVOT BOLT WAS DISCONNECTED. OPEN
- [SDR GLBA2015032300506](https://openairdocs.org/sdr/GLBA2015032300506), Mar 23, 2015: SKIN. CRACKED. DURING A SCHEDULED INSPECTION MX FOUND 2 CRACKS IN THE LT FUSELAGE SKIN UNDER THE VORTEX GEN MOUNT AREA. FWD SKIN CRACK IS .9" IN LENGTH AT FS 238.25, STRINGER 
- [SDR GLBA2015032000505](https://openairdocs.org/sdr/GLBA2015032000505), Mar 20, 2015: FRAME. CRACKED. DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE FRAME REPAIR & FRAME AT FS 163.975, STRINGER 10R, FRAME CRACK BEYOND STOP DRILL, .65" IN LENGTH. 
- [SDR GLBA2015031900503](https://openairdocs.org/sdr/GLBA2015031900503), Mar 19, 2015: CHANNEL. CRACKED. DURING A SCHEDULED INSPECTION MX FOUND A CRACK IN THE FUSELAGE CHANNEL AT BS 177.35, IN THE BEND RADIUS AT THE OTBD END OF THE CHANNEL, 1.2 INCH IN LENGTH. REPA
- [SDR GLBA2015031900504](https://openairdocs.org/sdr/GLBA2015031900504), Mar 19, 2015: FRAME. CRACKED. DURING A SCHEDULED INSPECTION, MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS AT THE OTBD END OF THE FRAME, 1.25" IN LENGTH. REPAIRED TH
- [SDR GLBA2015010200488](https://openairdocs.org/sdr/GLBA2015010200488), Dec 30, 2014: SNUBBER. LOW PRESSURE. THE AIR STAIR DOOR OPENS REALLY FAST & FOUND THAT THE DOOR SNUBBER PRESS READ 500 PSI. SERVICED THE AIR STAIR DOOR SNUBBER AS NEEDED IAW MI 52-01. OPERATIONS CH
- [SDR GLBA2014020400375](https://openairdocs.org/sdr/GLBA2014020400375), Feb 3, 2014: BRAKE SYS. MALFUNCTIONED. SIG EVENT PILOT REPORTED THAT THE RT BRAKE PEDAL GOES COMPLETELY TO THE FLOOR ON THE CAPTAIN`S & FIRST OFFICER'S SIDE, RIGHT BRAKE COMPLETELY INEFFECTIVE. SUPPL
- [SDR GLBA2013110100347](https://openairdocs.org/sdr/GLBA2013110100347), Nov 1, 2013: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION, FOUND A DENT FROM A BIRD STRIKE ON THE LT WING L/E BETWEEN WS 236.62 AND 223.48 AND HAS A FUEL LEAK DUE TO THE DAMAGE. REPAIRED I
- [SDR GLBA2012121000132](https://openairdocs.org/sdr/GLBA2012121000132), Dec 10, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT THE EDGE OF A LIGHTNING HOLE, HORIZONTAL STABILIZER AFT SPAR WEB CENTERLINE AT HSS 0.00, .1" IN LENGTH. M
- [SDR GLBA2012120700130](https://openairdocs.org/sdr/GLBA2012120700130), Dec 7, 2012: SKIN. CORRODED. DURING A SCHEDULED ROUTINE INSPECTION FOUND CORROSION AT FS 228.25, ON SKIN, CORROSION FOUND JUST OTBD OF THIS REPAIR, STRINER 14R 4" OTBD. MX REPAIRED THE AFFE
- [SDR GLBA2012120600129](https://openairdocs.org/sdr/GLBA2012120600129), Dec 5, 2012: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT SPAR CAP ANGLE ON VERTICAL STAB AT SECOND FASTENER FROM THE TOP, .75" IN LENGTH. MX REPAIRED THE 
- [SDR GLBA2012120600128](https://openairdocs.org/sdr/GLBA2012120600128), Dec 5, 2012: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND 2 CRACKS IN THE RT SPAR CAP ANGLE ON VERT STAB AT SECOND FASTENER FROM THE TOP, 1.25" IN LENGTH. MX REPAIRED THE AFF
- [SDR GLBA2012120600127](https://openairdocs.org/sdr/GLBA2012120600127), Dec 5, 2012: SKIN. CORRODED. DURING A SCHEDULED ROUTINE INSPECTION FOUND BELLY CORROSION AT FS 243.25, APPROX 1" LEFT OF STRINGER 16. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-074. MA
- [SDR GLBA20111216F](https://openairdocs.org/sdr/GLBA20111216F), Dec 15, 2011: FILTER. LEAKING. PILOT REPORTED THAT THERE IS A FUEL LEAK AROUND THE NR 1 ENG FUEL FILTER. MX REPLACED THE NR1 ENG FUEL FILTER.
- [SDR GLBA20110824G](https://openairdocs.org/sdr/GLBA20110824G), Aug 23, 2011: SWITCH. OUT OF ADJUST. PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED WHEN TAKEOFF POWER WAS APPLIED. MX ADJUSTED THE DOOR LATCH SWITCH IAW MM 52-70-00, OPS CK GOOD.
- [SDR GLBA20110817H](https://openairdocs.org/sdr/GLBA20110817H), Aug 16, 2011: LAMP. INOPERATIVE. PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHTS ARE INOP ON THE F/O'S SIDE. MX REPLACED THE LAMP IAW BMM 33-10-04, OPS CK GOOD.
- [SDR GLBA20110725J](https://openairdocs.org/sdr/GLBA20110725J), Jul 25, 2011: SKIN. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE EMERGENCY EXIT AT SEAT 6A SKIN CRACKED IN LOWER FWD CORNER, 1.25" INCHES IN LENGTH. MX REPAIRED THE
- [SDR GLBA20110722H](https://openairdocs.org/sdr/GLBA20110722H), Jul 22, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE CARGO DOOR UPPER FRAME AT FS 509.50 BETWEEN STRINGERS 3L & 4L, 3.75" IN LE
- [SDR GLBA20110714F](https://openairdocs.org/sdr/GLBA20110714F), Jul 13, 2011: PROPELLER. MALFUNCTIONED. THE PILOT REPORTED THAT ON APPROACH, AT 500' AGL WITH BOTH TORQUES AROUND 750LBS THE RT ENGINE CYCLED INTO AND OUT OF FEATHER TWICE, ADDED POWER TO 1500LBS AND 
- [SDR GLBA20101105A](https://openairdocs.org/sdr/GLBA20101105A), Nov 5, 2010: PRESSURE SWITCH. MALFUNCTIONED. LT SIDE PROP AUTOFEATHER W/ 1000LBS TQ SHORT FINAL. STOPPED AUTOFEATHERING ABOVE 1000 LBS TQ. MX INSPECTED THE SYS AND ADJUSTED THE FLIGHT IDLE TORQUE IAW AIM C
- [SDR GLBA20100823G](https://openairdocs.org/sdr/GLBA20100823G), Aug 23, 2010: SKIN. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A 1.1" CRACK IN THE LOWER LEFT FUSELAGE SKIN AT B.L. 26.8 AND F.S. 301.6. MAINTENANCE RE
- [SDR GLBA20100812F](https://openairdocs.org/sdr/GLBA20100812F), Aug 12, 2010: SKIN. DEBONDED. DURING A SCHEDULED ROUNTINE INSP, FOUND THE AIRSTAIR DOOR SKIN DEBONDING ON THE LOWER AFT, APPROX 19" IN LENGTH. MX REPLACED THE AIRSTAIR DOOR BONDED SKIN IAW B
- [SDR GLBA20100618G](https://openairdocs.org/sdr/GLBA20100618G), Jun 12, 2010: SPAR. DAMAGED. MAJOR REPAIR UPON SUBSEQUENT INSPECTION MAINTENANCE FOUND LEFT FORWARD SPAR AFT LOWER FLANGE FOUND TO HAVE BEEN DAMAGED BY LEFT DRAG BRACE NEXT TO UPLOCK BRACKE
- [SDR GLBA20100615F](https://openairdocs.org/sdr/GLBA20100615F), Jun 12, 2010: ARM. FAILED. SIG EVENT - UPON LANDING IN "DEN" THE LEFT HAND MAIN LANDING GEAR COLLAPSED CAUSING SIGNIFICANT DAMAGE TO THE LEFT MAIN LANDING GEAR AND ASSOCIATED SPAR AREA. I
- [SDR GLBA201005122](https://openairdocs.org/sdr/GLBA201005122), May 11, 2010: SWITCH. DETERIORATED. PILOTS REPORTED THAT THE RIGHT AUTOFEATHER CYCLED DURING LANDING. MAINTENANCE REMOVED AND REPLACED THE LEFT PRESSURE SWITCH. THE OPERATIONAL CHECK WAS GOOD IAW 
- [SDR GLBA201005121](https://openairdocs.org/sdr/GLBA201005121), May 10, 2010: SWITCH. MALFUNCTIONED. PILOTS REPORTED THAT THE AUTOFEATHER SEQUENCE CYCLED MULTIPLE TIMES DURING LANDING FLARE. MAINTENANCE ADJUSTED THE RIGHT AUTOFEATHER ARMING SWITCH IN THE PEDEST
- [SDR GLBA20091111F](https://openairdocs.org/sdr/GLBA20091111F), Nov 10, 2009: SPAR. DAMAGED. DURING ROUTINE SCHEDULED MX, DISCOVERED 2 LOCK FASTENER HOLES MISDRILLED (HOLES ARE STEPPED) AT/ON THE LT WING, AFT WING SPAR ON THE FWD SIDE OF THE SPAR AT WS 
- [SDR GLBA20091110H](https://openairdocs.org/sdr/GLBA20091110H), Nov 6, 2009: SPAR. DAMAGED. DURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, A HOLE WAS FOUND TO BE STEPPED AND OVERSIZED AT THE LEFT HAND WING SPAR W.S. 104.0. APPROXIMAT
- [SDR GLBA20091110G](https://openairdocs.org/sdr/GLBA20091110G), Nov 6, 2009: SPAR. DAMAGED. DURING ROUTINE SCHEDULED MAINTENANCE AFTER REMOVAL OF A FASTENER, PART OF AN EXISTING RIVET WAS IN THE HOLE UPON REMOVING THE RIVET THE DIAMETER OF THE HOLE WAS
- [SDR GLBA20091110F](https://openairdocs.org/sdr/GLBA20091110F), Nov 6, 2009: SPAR. DAMAGED. DURING ROUTINE SCHEDULED MX, A STEPPED LOCK FASTENER WAS FOUND IN THE LT WING SPAR AT WS 124.588. DEPTH OF THE STEP IS APPROX .150" DEEP. MAINTENANCE REPAIRED T
- [SDR GLBA20091104F](https://openairdocs.org/sdr/GLBA20091104F), Nov 4, 2009: ANGLE. CRACKED. DURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND HEAVY ANGLE WAS FOUND CRACKED IN THE RADIUS AT F.S. 303.25. CRACK LENGTH APPROXIMATELY 2" LONG EXTENDING 1" FO
- [SDR GLBA200908122](https://openairdocs.org/sdr/GLBA200908122), Aug 12, 2009: LATCH. OUT OF RIG. PILOTS REPORTED THAT THE 6C EMERGENCY EXIT HANDLE APPEARED TO BE UNLOCKED FROM THE OUTSIDE. MX RIGGED THE 6C DOOR LATCH AND OPS CHECKED GOOD.
- [SDR GLBA200908121](https://openairdocs.org/sdr/GLBA200908121), Aug 11, 2009: HANDLE. LOOSE. DURING ROUTINE WALK AROUND PILOTS REPORTED THAT LT OVERWING EXIT HANDLE APPEARED TO BE UNSECURED. MX ENSURED THAT LATCH WAS SECURED MM 52-20-00. SUBSEQUENT INSP
- [SDR GLBA20090703A](https://openairdocs.org/sdr/GLBA20090703A), Jul 3, 2009: TACH GENERATOR. DETERIORATED. ABORTED TAKEOFF, PILOTS REPORTED THAT AT TAKEOFF POWER THE PROPELLER RPM ON THE LT SIDE EXCEEDED 2000 RPM AND THE TAKEOFF WAS ABORTED. MX REMOVED AND REPLACED N
- [SDR GLBA200906011](https://openairdocs.org/sdr/GLBA200906011), Jun 1, 2009: INDICATOR. MALFUNCTIONED. NR 2 TORQUE GAUGE DROPPED TO 0 ON TAKEOFF ROLL. THE NR 2 TORQUE GAUGE DROPPED TO ZERO. MX REMOVED AND REPLACED THE NR 2 TORQUE GAUGE IAW MM 31-10-00. OPS CHECK 
- [SDR GLBA2009022809G](https://openairdocs.org/sdr/GLBA2009022809G), Feb 23, 2009: KEEL. CRACKED. MAJOR REPAIR - DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE LEFT INBOARD KEEL. MAINTENANCE REPAIRED THE LEFT HAND INBOARD KEEL AT FS 321 IAW ENGINEERIN
- [SDR GLB2008F00005](https://openairdocs.org/sdr/GLB2008F00005), Jun 18, 2008: ANGLE. CRACKED. LT HEAVY ANGLE CRACKED APPROX 1.125 INCH IN LENGTH AT FORWARD BEND RADIUS AT FS 288.0. REPAIRED LT HEAVY ANGLE AT FS 288 IAW SRM 53.90. REPAIR AREA APPROX 13.12
- [SDR GLBA20060919](https://openairdocs.org/sdr/GLBA20060919), Feb 26, 2007: SKIN. MISREPAIRED. UPON ROUTINE INSPECTIONS MAINTENANCE FOUND THAT A REPAIR MUST CONFORM WITH SRM TECHNICAL DATA SPECIFICATIONS AT FS 126 TO FS 131.3 STRINGER 3R TO APPROXIMATELY 
- [SDR GLBA20060918](https://openairdocs.org/sdr/GLBA20060918), Feb 26, 2007: STRINGER. CRACKED. UPON ROUTINE INSPECTIONS, MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 177.3 RT STRINGER 9AL. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 177.3 RT ST
- [SDR GLBA20060917](https://openairdocs.org/sdr/GLBA20060917), Feb 26, 2007: STRINGER. CRACKED. UPON ROUTINE INSPECTIONS MAINTENANCE FOUND A STRINGER RELIEF HOLE CRACKED AT FS 163.9 RT STRINGER 9AL. MAINTENANCE REPAIRED THE AFFECTED AREA AT FS 163.9 RT STR
- [SDR GLBA20060911](https://openairdocs.org/sdr/GLBA20060911), Feb 20, 2007: SKIN. CRACKED. UPON ROUTINE INSPECTION MAINTENANCE FOUND THE BELLY SKIN CRACKED AT APPROXIMATELY F.S. 298.0, B.L. 27.0. MAINTENANCE REPAIRED BELLY SKIN AT APPROXIMATELY F.S.29

All 85: https://openairdocs.org/aircraft/N195GL/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/N195GL/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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