# N154GL: 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-154
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: May 30, 1995
- Certificate issued: June 12, 2023
- Expires: June 30, 2030
- Mode S code: A0D9AC
- 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=154GL
- Page: https://openairdocs.org/aircraft/N154GL

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/N154GL/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 N154GL.

## FAA accident and incident reports (2)

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 20080213010699I](https://openairdocs.org/incident/20080213010699I), Feb 13, 2008: Beech 1900D (N154GL), Hays, KS, No damage. (-23) On January 30, 2008, at 0754 local time, the flight crew for great lakes aviation ltd, (glba) operating as flight no 5041 departing great bend, KS, (gbd)…
- [Incident 20040622014439I](https://openairdocs.org/incident/20040622014439I), Jun 22, 2004: Beech 1900D (N154GL), Denver, CO. (-23) After departure from Denver co (den) to garden city KS (dck), at approximately 12,500 feet MSL at climb power the #1 engine began to experience…

## Service difficulty reports (58, 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 GLBA2014091100437](https://openairdocs.org/sdr/GLBA2014091100437), Sep 11, 2014: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A LIGHTNING STRIKE ON THE OTBD RT ELEVATOR TE JUST OTBD OF THE OTBD MOST STATIC WICK CAUSING DAMAGE TO THE FIBER
- [SDR GLBA2014012300373](https://openairdocs.org/sdr/GLBA2014012300373), Jan 22, 2014: SPAR. CRACKED. DURING A SCHEDULED INSPECTION MX ACCOMPLISH PROACTIVE REPAIR TO THE RT VERTICAL SPAR CAP ANGLE IAW EO 14-1900-55-001. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED
- [SDR GLBA2014011600371](https://openairdocs.org/sdr/GLBA2014011600371), Jan 15, 2014: SKIN. DENTED. DURING A SCHEDULED INSPECTION, MX FOUND THE LT AFT SKIN DENTED AT BS 446 BETWEEN STRINGERS 11-12L. REPAIREDS IAW EO 14-1900-53-005.
- [SDR GLBA2014011300368](https://openairdocs.org/sdr/GLBA2014011300368), Jan 13, 2014: FRAME. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK AT BS 183 & STRINGER 9R FRAME ANGLE, .375 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-003.
- [SDR GLBA2014011300367](https://openairdocs.org/sdr/GLBA2014011300367), Jan 13, 2014: DOOR FRAME. CRACKED. DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE PAX DOOR CUTOUT LOWER FRAME AT APPROXIMATELY FS 172 LOWER AFT CORNER, 1 INCH IN LENGTH. REPAIRED IAW EO 13-1
- [SDR GLBA2014011300370](https://openairdocs.org/sdr/GLBA2014011300370), Jan 13, 2014: SKIN. CRACKED. DURING A SCHEDULED INSPECTION, FOUND TWO CRACKS AT BS 150 & STRINGER 1 EXTERIOR FUSELAGE SKIN PROTRUDING OUT OF RIVETS ON EITHER SIDE OF STRINGER, .25 INCHES IN
- [SDR GLBA2014011300369](https://openairdocs.org/sdr/GLBA2014011300369), Jan 13, 2014: DOOR. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THE EMERGENCY DOOR CRACKED, 4C AT THE RT FWD ASSEMBLY, 1.125 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-52-001.
- [SDR GLBA2013090900307](https://openairdocs.org/sdr/GLBA2013090900307), Sep 6, 2013: WIRE. DAMAGED. PILOT REPORTED THAT THE RT FIRE LOOP AND TEE HANDLE ANNUNCIATORS FLICKERED DURING CLIMB OUT. MAINTENANCE TROUBLESHOT SYSTEM, NO FAULTS FOUND MEGGED WIRE W16A22 
- [SDR GLBA2013070500269](https://openairdocs.org/sdr/GLBA2013070500269), Jul 3, 2013: BLOWER. ODOR. PILOT REPORTED A FOUL ODOR EMINATING FROM THE ENVIROMENTAL SYS WITH A NOTIABLE VIBRATION IN THE BACK OF THE ACFT. MX CLEANED THE ENVIRO VENT BLOWER AND SECURED 
- [SDR GLBA2012082300037](https://openairdocs.org/sdr/GLBA2012082300037), Aug 23, 2012: ATTACH ANGLE. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS AT THE RT ANGLE AT FS 107.00 AS IT ATTACHES TO THE LONGERON, RT ANGLE AT THE UPPER END OF THE BEND RADIUS
- [SDR GLBA2012082300038](https://openairdocs.org/sdr/GLBA2012082300038), Aug 23, 2012: ATTACH ANGLE. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE LT SIDEWALL AT FS 107.00, LT ANGLE UPPER INBD FLANGE PORTION IN THE BEND RADIUS AS IT ATTACHED TO THE 
- [SDR GLBA2012082300036](https://openairdocs.org/sdr/GLBA2012082300036), Aug 23, 2012: LONGERON. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT LONGERON AT JUNCTION WITH RT ANGLE AT FS 107.00 CRACKED FROM THE INBD FLANGE AT THE LONGERON TO THE BEND RAD
- [SDR GLBA2012082100035](https://openairdocs.org/sdr/GLBA2012082100035), Aug 20, 2012: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND VERT STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD IS CRACKED AT THE UPPER END AT VSS 84.10, BEGINNING AT THE TOP E
- [SDR GLBA2012082100034](https://openairdocs.org/sdr/GLBA2012082100034), Aug 20, 2012: PRESSURE BLKHD. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND RT LWR FWD PRESSURE BULKHEAD CRACKED AROUND FASTENERS ALONG THE BULKHEADS INBD EDGE, FOUND 2 CRACKS APPROX .1 INCH I
- [SDR GLBA2012082100033](https://openairdocs.org/sdr/GLBA2012082100033), Aug 20, 2012: PRESSURE BLKHD. CRACKED. DURING A SCHEDULED INSPECTION, FOUND LT LWR FWD PRESSURE BULKHEAD IS CRACKED ALONG THE INBD EDGE DOUBLE ROW OF FASTENER, 3 CRACKS .2 INCHES IN LENGTH RADIUS FRO
- [SDR GLBA2012061900001](https://openairdocs.org/sdr/GLBA2012061900001), Jun 19, 2012: WEB. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE HORIZONTAL STAB AFT WEB AT HSS 0.00, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW EO 12-1900-55-017.
- [SDR GLBA20111227F](https://openairdocs.org/sdr/GLBA20111227F), Dec 24, 2011: SWITCH. DIRTY. CABIN DOOR ANNUNCIATOR ILLUMINATED ON DESCENT THEN EXTINGUISHED SHORTLY AFTER. MX CLEANED THE SWITCH, OPS CHECKED GOOD.
- [SDR GLBA20111109F](https://openairdocs.org/sdr/GLBA20111109F), Nov 8, 2011: WIRE. DAMAGED. PILOT REPORTED THEAT THE CABIN DOOR ANNUNCIATOR EXTINGUISHES WHEN DOOR IS OPEN AND HANDLE IS CLOSED. MX REPAIRED SPLICE D436, OPS CHECKED GOOD.
- [SDR GLBA20111003J](https://openairdocs.org/sdr/GLBA20111003J), Oct 2, 2011: CIRCUIT BOARD. MALFUNCTIONED. PILOT REPORTED THAT DURING RUNUP THE AFX DISABLE ANNUNCIATOR WON'T ILLUMINATE ON THE RT AUTOFEATHER TEST. MX RERACKED THE A123 PCB IAW MI 24-01, OPS CHECKED GOO
- [SDR GLBA20110906F](https://openairdocs.org/sdr/GLBA20110906F), Sep 2, 2011: SWITCH. INOPERATIVE. PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR DOES NOT EXTINGUISH. MX REPAIRED MULTIPLE WIRES TO SPLICE D436, REPLACED FWD MICROSWITCH REF 14.12.10, RIGGED SWI
- [SDR GLBA201108081](https://openairdocs.org/sdr/GLBA201108081), Aug 7, 2011: VALVE. FAILED. LANDING GEAR FAILED TO EXTEND ON APPROACH. DID NOT HEAR THE PUMP TURN ON WHEN MOVING THE LANDING GEAR CONTROL HANDLE. PUMPED GEAR DOWN MANUALLY, HAD ALL 5 GREEN
- [SDR GLBA20110706H](https://openairdocs.org/sdr/GLBA20110706H), Jul 5, 2011: SUPPORT. FAILED. PILOT REPORTED THAT THE CABIN DOOR STRAP SUPPORT ON THE LT SIDE IS COMING APART. MX REINSTALLED A FASTENER ON THE LT CABIN DOOR STRAP SUPPORT IAW BMM 52-10-60, 
- [SDR GLBA20110519F](https://openairdocs.org/sdr/GLBA20110519F), May 19, 2011: SKIN. DEBONDED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE AS DOOR SKIN DEBONDED AT THE LOWER BOTTOM, DEBONDED FROM FORWARD EDGE TO THE AFT EDGE
- [SDR GLBA20110518F](https://openairdocs.org/sdr/GLBA20110518F), May 17, 2011: SKIN. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE BELLY SKIN AT FS 300 AND RT WING IB BULK HEAD, 1" IN LENGTH. MAINTENANCE R
- [SDR GLBA20110516L](https://openairdocs.org/sdr/GLBA20110516L), May 16, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND CRACKS AT F.S. 456 BETWEEN STRINGERS 3L AND 4L AT THE UPPER IB NUTPLATE AREA, 1.9" IN LEN
- [SDR GLBA20110516K](https://openairdocs.org/sdr/GLBA20110516K), May 16, 2011: FRAME. CRACKED. MAJOR REPAIR. DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE FRAME AT FS 456 AND S10R, .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED 
- [SDR GLBA20100904A](https://openairdocs.org/sdr/GLBA20100904A), Sep 4, 2010: TUBE. LEAKING. PILOT REPORTED THAT THEY NOTICED SMOKE/FUMES IN THE CABIN PRIOR TO TAKEOFF, SUSPECT VAPOR CYCLE SYSTEM LEAK. MAINTENANCE REPLACED THE TUBE FROM RECEIVER-DRIER T
- [SDR GLBA20100805FA](https://openairdocs.org/sdr/GLBA20100805FA), Aug 3, 2010: ENGINE. OVERTORQUED. PILOT REPORTED THAT UPON APPROACH, RT POWER LEVER STUCK WITH AN OVERTORQUE INDICATION, PERFORMED PRECAUTIONARY RT ENGINE SHUTDOWN. RT PROPELLER CONTINUED TO WIN
- [SDR GLBA2010051601](https://openairdocs.org/sdr/GLBA2010051601), May 16, 2010: BEARING. FAILED. PILOTS REPORTED, WHILE PERFORMING A 2ND START FOR NR 2 ENG. NR 2 STARTER SEEMED TO TURN ON & OFF VERY QUICKLY WHEN IGNITION & ENG START SWITCH IN ON. DURING ENG
- [SDR GLBA20091116F](https://openairdocs.org/sdr/GLBA20091116F), Nov 12, 2009: BRACE. CHAFED. MX DISCOVERED THAT THERE WAS CHAFING ON THE FWD RT SIDE OF THE RT MLG BRACE CTR TUBE APPROX 11 INCHES FROM TOP. CHAFE IS APPROX AT A 45 DEGREE ANGLE AND MEASURE
- [SDR GLBA20090909H](https://openairdocs.org/sdr/GLBA20090909H), Sep 8, 2009: SKIN. CRACKED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE BELLY SKIN AT B.L. 29.0 AND F.S. 303.25. CRACK IS APPROXIMATELY 2.250" IN LENGTH. M
- [SDR GLBA20090502A](https://openairdocs.org/sdr/GLBA20090502A), May 2, 2009: CIRCUIT BOARD. LOOSE. RIGHT ENVIRO FAIL ANNUNCIATOR ILLUMINATED DURING TAKEOFF WITH TAKEOFF POWER AND BLEED AIR VALVES CLOSED. MAINTENANCE RE-SEATED THE PRINTED CIRCUIT BOARD AND OPE
- [SDR GLBA20090424B](https://openairdocs.org/sdr/GLBA20090424B), Apr 24, 2009: GENERATOR. FAILED. PILOTS REPORTED THE THE LEFT DC GENERATOR FELL OFFLINE ON TAKEOFF ROLL. MAINTENANCE PERFORMED AN OPERATIONAL CHECK PER MM 24-00-00-001. NO FAULTS WERE FOUND AND
- [SDR GLBA20090312A](https://openairdocs.org/sdr/GLBA20090312A), Mar 12, 2009: RELAY. DETERIORATED. PILOTS REPORTED THAT THE FLAPS STUCK INTERMITTENTLY AT 17 DEGREES AND EVENTUALLY CAME UP UPON LANDING. MAINTENANCE REMOVED AND REPLACED FLAP RELAY I.A.W. BMM 27
- [SDR GLBA20090301B](https://openairdocs.org/sdr/GLBA20090301B), Mar 1, 2009: INDICATOR. WORN. FLIGHT 5014- NO AIRSPEED INDICATION ON CA AIRSPEED ON T/O ROLL. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIRSPEED INDICATOR IAW TASKCARD 1900.3411.00-1. OPERAT
- [SDR GLBA20061099](https://openairdocs.org/sdr/GLBA20061099), May 2, 2008: SKIN. DAMAGED. RT UPPER ICE SHIELD DIVIDED INTO (2) PIECES AT APPROXIMATE LOCATION OF STRINGER 8R FROM F.S. 183.25 TO F.S. 220.75. MAINT REPLACED THE RT UPPER ICE SHILED IAW. 
- [SDR GLBA20061098](https://openairdocs.org/sdr/GLBA20061098), May 1, 2008: FRAME. CRACKED. FUSELAGE FRAME AT FS 177.3 CRACKED AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY .6 INCH IN LENGTH. MAINTENANCE REPAIRED FUSELAGE FRAME AT FS 177.3 AT STRINGER 9R 
- [SDR GLBA20061097](https://openairdocs.org/sdr/GLBA20061097), May 1, 2008: FRAME. CRACKED. FUSELAGE FRAME CRACK AT FS 163.97 AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY .5 INCH IN LENGTH. MAINT REPAIRED FUSELAGE FRAME AT FS 163.97 AT STRINGER 9R RELIEF
- [SDR GLBA20061096](https://openairdocs.org/sdr/GLBA20061096), May 1, 2008: FRAME. CRACKED. FUSELAGE FRAME AT FS 451 CRACKED ON THE TOP SIDEOF STRINGER 10R. CRACK APPROXIMATELY 1.1 INCH LENGTH. MAINT REPAIRED FUSELAGE FRAME FLANGE AT FS 451 STRINGER 10
- [SDR GLBA20061095](https://openairdocs.org/sdr/GLBA20061095), May 1, 2008: STRINGER. CRACKED. STRINGER 10R CRACKED AT F.S. 451. CRACK LENGTH APPROXIMATELY.5 INCH. MAINT REPAIRED STRINGER 10R FLANGE AT F.S. 451 I.A.W. BEECH 1900D SRM 51-70. REPAIR DIMENSI
- [SDR GLBA20061054](https://openairdocs.org/sdr/GLBA20061054), Jan 30, 2008: ENGINE. DETERIORATED. ENGINE SHUTDOWN, FLT 5041 ENROUTE 10 MILES OUT ON FINAL THE NR1 ENGINE FEATHERED INFLIGHT AND THE PILOTS PERFORMED THE ENG SECURE PROCEDURES AND SHUTDOWN THE EN
- [SDR GLBA20060961](https://openairdocs.org/sdr/GLBA20060961), Jul 2, 2007: TORQUEMETER. MALFUNCTIONED. ABORTED TAKEOFF, FLIGHT 5063, UPON TAKEOFF PILOTS REPORTED THAT THE LT TORQUE INDICATOR STUCK AND WOULD NOT WORK CORRECTLY. AIRCRAFT RETURNED TO GATE. MAINTENAN
- [SDR 20030785](https://openairdocs.org/sdr/20030785), Jan 26, 2005: SPAR. CRACKED. DURING ROUTINE STRUCTURAL "I" INSPECTION, FOUR CRACKS WERE IDENTIFIED EMANATING FROM THE DE-ICE HOLE ON THE HORIZONTAL CENTER MAIN SPAR CENTER WEB SKIN APPROX 1
- [SDR GLBA20030683](https://openairdocs.org/sdr/GLBA20030683), Jul 29, 2004: SKIN. CRACKED. CRACK IN FUSELAGE SKIN FWD AND LEFT OF LWR COMM ANTENNA, PERFORMED MAJOR REPAIR TO FUSELAGE SKIN.
- [SDR GLBA20030652](https://openairdocs.org/sdr/GLBA20030652), Jun 22, 2004: COMPRESSOR. STALLED. NR 1 ENG COMPRESSOR STALLS, SHUT DOWN ENG IN FLT RETURNED TO DEN. REMOVED AND REPLACED ENG PN PT6A-67D.
- [SDR GLBA20030598](https://openairdocs.org/sdr/GLBA20030598), Mar 28, 2004: WIRE. BROKEN. LOOSE WIRE CAUSED SPARK ON F.O. YOKE, REMOVED BROKEN WIRE OPS CK GOOD
- [SDR GLBA20030594](https://openairdocs.org/sdr/GLBA20030594), Mar 21, 2004: INDICATOR. FROZEN. RT N1 INDICATOR SPIKED & FROZE AT 98 PERCENT, PREFORMED OPS CK FOUND NO DEFECTS SWAPPED GAUGES PN 130-380044-5 CND
- [SDR GLBA20030527](https://openairdocs.org/sdr/GLBA20030527), Jan 7, 2004: FLAP. STUCK. FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION
- [SDR GLBA2003527](https://openairdocs.org/sdr/GLBA2003527), Jan 7, 2004: FLAP. STUCK. FLAPS STUCK AT 17 DEG, PENDING CORRECTIVE ACTION
- [SDR GLBA2003153](https://openairdocs.org/sdr/GLBA2003153), Nov 20, 2003: INDICATOR. MALFUNCTIONED. LT ENGINE ITT EXCEEDED 900C ON ADVANCEMENT OF POWER ON TAKE OFF ROLL, REMOVED AND REPLACED LT ITT GAUGE.

All 58: https://openairdocs.org/aircraft/N154GL/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/N154GL/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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