# N201GL: 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-201
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: March 4, 1996
- Certificate issued: March 25, 2023
- Expires: March 31, 2030
- Mode S code: A1965B
- 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=201GL
- Page: https://openairdocs.org/aircraft/N201GL

From the FAA registry file of October 22, 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/N201GL/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 N201GL.

## FAA accident and incident reports (1)

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 20140913016549I](https://openairdocs.org/incident/20140913016549I), Sep 13, 2014: Beech 1900D (N201GL), Los Angeles, CA, Minor damage. While preparing for departure, great lakes airline flight GLA3048, N201GL, BE1900 was struck by debris caused by jet blast from dal 2332. Two pilots on board,…

## 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 2022FA0000756](https://openairdocs.org/sdr/2022FA0000756), Dec 9, 2022: RIB. CRACKED. CRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FLANGES AT BS 303 AFT FLANGE RADI
- [SDR GLBA2017050400651](https://openairdocs.org/sdr/GLBA2017050400651), May 1, 2017: CABLE. NOT REPORTED. MAINTENANCE REPORTED THAT THE UPPER FORWARD [AIRSTAIR] DOOR REQUIRES REPLACEMENT. REMOVED AND REPLACED THE UPPER FORWARD DOOR CABLE IAW BEECH 1900D AMM 52-10-02
- [SDR GLBA2016082300605](https://openairdocs.org/sdr/GLBA2016082300605), Aug 23, 2016: STRINGER. CRACKED. DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND STRINGER 4R IS CRACKED IN THE RADIUS ON THE FORWARD END. MAJOR REPAIR
- [SDR GLBA2015033000508](https://openairdocs.org/sdr/GLBA2015033000508), Mar 27, 2015: ACM. WORN. PILOT REPORTED THAT THE PRESSURIZATION OPERATIONS CHECKED GOOD DURING RUN-UP, UPON CLIMB PRESSURIZED TO APPROX DIFF OF 3.0 & FAILED TO FURTHER PRESSURIZE. CABIN
- [SDR GLBA2015030900501](https://openairdocs.org/sdr/GLBA2015030900501), Mar 9, 2015: BULKHEAD. BUCKLED. DURING A SCHEDULED INSPECTION, FOUND THE CANTED BULKHEAD AT FS 588.10 BUCKLED FROM STRINGER 12R TO 12L. REPAIRED THE BULKHEAD IAW EO 15-120-53-001. MAJOR REPAIR
- [SDR GLBA2015011200491](https://openairdocs.org/sdr/GLBA2015011200491), Jan 12, 2015: SKIN. CORRODED. DURING A SCHEDULED INSPECTION, FOUND THE UPPER INBD RT WING SKIN TE CHAFED & CORRODED WITH SEVERAL ELONGATED HOLES AT BL 36. CHAFE 8.5 INCHES LONG, 2 INCHES WID
- [SDR GLBA2014121700480](https://openairdocs.org/sdr/GLBA2014121700480), Dec 17, 2014: SKIN. WORN. DURING A SCHEDULED INSPECTION, FOUND THE BELLY SKIN AT BS 220 & STRINGER 15L HAS A .25 INCH HOLE WORN THROUGH THE SKIN. WORN AREA IS FWD & AFT APPROX 25 INCHES 
- [SDR GLBA2014121900484](https://openairdocs.org/sdr/GLBA2014121900484), Dec 17, 2014: SKIN. CRACKED. DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE CARGO BAY LT INNER SKIN AT BS 509.5 & STRINGER 11L, .9 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-059.
- [SDR GLBA2014121700483](https://openairdocs.org/sdr/GLBA2014121700483), Dec 17, 2014: FRAME. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CARGO DOOR UPPER FRAME AT FS 460 & STRINGER 3L, 2.1 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-058.
- [SDR GLBA2014121700481](https://openairdocs.org/sdr/GLBA2014121700481), Dec 17, 2014: FRAME. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THREE CRACKS IN THE CARGO DOOR FUSELAGE FRAME AT BS 509.50 BETWEEN STRINGERS 4 - 5L IN THE BEND RADIUS OF THE FRAME, TWO IN
- [SDR GLBA2014121700482](https://openairdocs.org/sdr/GLBA2014121700482), Dec 17, 2014: FRAME. CRACKED. DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT BS 509.5 & STRINGER 11L, .75 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-057.
- [SDR GLBA2014121500478](https://openairdocs.org/sdr/GLBA2014121500478), Dec 15, 2014: BULKHEAD. CRACKED. MAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CRACK IN THE CANT BULKHEAD FLANGE AT FS 588.10 & BETWEEN STRINGER 8R & 7R, 1.5 INCHES IN LENGTH. RE
- [SDR GLBA2014121500479](https://openairdocs.org/sdr/GLBA2014121500479), Dec 15, 2014: FRAME. CRACKED. MAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CRACK IN THE FUSELAGE FRAME IN THE FLANGE BEND RADIUS AT FS 177.35 BETWEEN STRINGERS 12L & 13L, 1.1
- [SDR GLBA2014091900439](https://openairdocs.org/sdr/GLBA2014091900439), Sep 17, 2014: STRINGER. BENT. MAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND STRINGER 11L BENT APPROX 2 INCHES IN LENGTH BETWEEN FS 513.50 & FS 523.50. REPAIRED THE AFFECTED 
- [SDR GLBA201403140001](https://openairdocs.org/sdr/GLBA201403140001), Mar 13, 2014: CONNECTOR. LOOSE. UPON EXTENDING GEAR ON FINAL, RT GEAR R & H ANNUNCIATORS FAILED TO ILLUMINATE. UPON COMPLETION OF CHECKLIST, ALL OTHER INDICATIONS REVEALED GEAR DOWN & LOCKED. 
- [SDR GLBA2013031500211](https://openairdocs.org/sdr/GLBA2013031500211), Mar 14, 2013: CLAMP. LOOSE. PILOT REPORTED THAT AT ALTITUDE 18500, CABIN ALTITUDE HIGH ANNUCICATOR ILLUMINATED. CABIN ALTITUDE INDICATED 10000 FT AND CABIN INDICATED 800 FT IAW MIN WITH IN
- [SDR GLBA2012100100070](https://openairdocs.org/sdr/GLBA2012100100070), Oct 1, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE HORIZONTAL STAB AFT SPAR WEB AT RELIEF HOLE AT HSS 00.0, .5 INCHES IN LENGTH. REPAIRED IAW EO 11-
- [SDR GLBA2012100100069](https://openairdocs.org/sdr/GLBA2012100100069), Oct 1, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSP FOUND FOUR CRACKS ON THE HORIZONTAL STAB FWD SPAR WEB AT HSS 00.00, 2" IN LENGTH TOTAL. REPAIRED IAW EO 11-1900-55-046.
- [SDR GLBA2012100100072](https://openairdocs.org/sdr/GLBA2012100100072), Sep 29, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT VSS 84.10 AT 20 PERCENT. 1.5 INCHES IN LENGTH. REPAIRED IAW E
- [SDR GLBA2012100100071](https://openairdocs.org/sdr/GLBA2012100100071), Sep 29, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT VSS 84.10 AT 20 PERCENT CHORD, CRACKED FROM FIRST RIVET H
- [SDR GLBA20111204B](https://openairdocs.org/sdr/GLBA20111204B), Dec 4, 2011: BULB. INOPERATIVE. EMERGENCY LIGHTS ON THE CAPTAIN'S SIDE INOP. MX RELAMPED CAPT EMERGENCY LIGHT IAW B-1900 33-60-00-801, ALL CHECKED GOOD.
- [SDR GLBA20111019F](https://openairdocs.org/sdr/GLBA20111019F), Oct 18, 2011: FCU. LEAKING. PILOT REPORTED THAT THERE IS A LEAK COMING FROM THE SMALL DRAIN ON THE LT ENGINE. MX REPLACED THE LT HP FUEL PUMP AND FCU, OPS AND LEAK CHECKED GOOD.
- [SDR GLBA20110829G](https://openairdocs.org/sdr/GLBA20110829G), Aug 29, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP THE FUSELAGE FRAME AT FS 456 & STRINGER 10R CRACKED, .55" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND P
- [SDR GLBA20110829H](https://openairdocs.org/sdr/GLBA20110829H), Aug 29, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP THE CARGO BAY BULKHEAD AT FS 531, LT UPPER OTBD CORNER CRACKED .75" IN LENGTH. REPAIRED THE AFFECTED AREA AND PER
- [SDR GLBA20110823G](https://openairdocs.org/sdr/GLBA20110823G), Aug 22, 2011: FUEL CONTROL. LEAKING. PILOT REPORTED THAT THE RT ENGINE IS LEAKING FUEL FWD OF THE WHEEL WELL, DRIPPING STOPS ATFTER SHUTDOWN. MX REPLACED THE RT FCU IAW TC 1900-7320.00 AND REPLACED
- [SDR GLBA201108101](https://openairdocs.org/sdr/GLBA201108101), Aug 10, 2011: BULB. INOPERATIVE. ON FINAL, DID NOT RECEIVE NOSE GEAR DOWN AND LOCKED INDICATION. MX REPLACED THE LIGHT BULBS, PN: 327 IAW BMM 33-10-05, OPS CKS AND SWING CHECKS GOOD IAW AIM MI 
- [SDR GLBA20110810G](https://openairdocs.org/sdr/GLBA20110810G), Aug 10, 2011: BULB. INOPERATIVE. PILOT REPORTED THAT THEY DID NOT GET A NOSE GEAR DOWN AND LOCK INDICATION WITH THE GEAR DOWN AND LOCKED. MX REPLACED THE LIGHT BULBS, OK FOR SERVICE.
- [SDR GLBA20110719F](https://openairdocs.org/sdr/GLBA20110719F), Jul 18, 2011: PUMP. LEAKING. PILOT REPORTED THAT FUEL WAS LEAKING FROM THE NR2 ENGINE GANG DRAIN. MX REPLACED THE NR2 ENGINE DRIVEN FUEL PUMP IAW BMM 73-10-00.
- [SDR GLBA201105131](https://openairdocs.org/sdr/GLBA201105131), May 13, 2011: UNKNOWN. ODOR. THE PILOT REPORTED THAT DURING DESCENT THEY SMELLED FUEL. MX CLEANED THE EPA CANNISTER AND CHECKED FUEL VALUES ON BOTH ENGINES, PERFORMED FCD 1900-08-30-01 STEP
- [SDR GLBA20100422G](https://openairdocs.org/sdr/GLBA20100422G), Apr 21, 2010: FLOOR SUPPORT. CRACKED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT FS 482 APPROX 24" INBD OF DOOR THRESHOLD. CRACK APPROX 1". CRACK IS AFT OF NUTPLATE IN RADIUS O
- [SDR GLBA20100422F](https://openairdocs.org/sdr/GLBA20100422F), Apr 20, 2010: ANGLE. CRACKED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND AT FS 456 JUST LT OF STRINGER NR 1 FWD OF THE REINFORCING ANGLE ATTACHED TO THE FUSELAGE SECTION CR
- [SDR GLBA201003231](https://openairdocs.org/sdr/GLBA201003231), Mar 23, 2010: BULB. BURNED OUT. THE PILOTS DISCOVERED THAT THE CAPTAINS SIDE INTRUMENT EMERGENCY LIGHT WAS BURN OUT. MAINTENANCE REMOVED AND REPLACED THE BULB AND THE LIGHT OPERATIONALLY CHECK
- [SDR GLBA20091202B](https://openairdocs.org/sdr/GLBA20091202B), Dec 2, 2009: TRANSMITTER. MALFUNCTIONED. RT ENG WENT INTO AND OUT OF FEATHER ON SHORT FINAL. MX TROUBLESHOT THE SYS AND FOUND THE TORQUE INDICATION BAD. MX REMOVED AND REPLACED THE TORQUE TRANSMITTER I
- [SDR GLBA20091127091](https://openairdocs.org/sdr/GLBA20091127091), Nov 27, 2009: AUTOFEATHER SYS. MALFUNCTIONED. SUSPECTED AUTOFEATHER - UPON APPROACH, THE PILOTS REPORTED THAT THE RT PROPELLER AUTOFEATHERED WITH TORQUE AT APPROX 1000 LBS. MX PERFORMED THE AUTOFEATHER OPER
- [SDR GLBA200909291](https://openairdocs.org/sdr/GLBA200909291), Sep 29, 2009: BULB. INOPERATIVE. PILOTS REPORTED THAT ONE EMERGENCY INSTRUMENT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED BULB 1864 BY PUSHING IN AND TURNING THE A QUARTER UNTIL IT 
- [SDR GLBA200930041](https://openairdocs.org/sdr/GLBA200930041), Apr 30, 2009: INDICATOR. ERRATIC. IN CRUISE AT 2300 NR 1 TORQUE GAUGE WAS FLUCTUATING 200-300FT/LBS. COULD HEAR THE CHANGE IN TORQUE. OCCURRED WITH PROP SYNC ON AND OFF. WHEN TORQUE BELOW 2500FT
- [SDR GLBA20090224F](https://openairdocs.org/sdr/GLBA20090224F), Feb 23, 2009: SKIN. CHAFED. DURING ROUTINE SCHEDULED MX A CHAFE WAS FOUND ON THE BELLYSKIN AT APPROX FS 224.0 BETWEEN STRINGER 15L & 16L. ONE OF THEM WAS 2.9 INCHES IN LENGTH AND THE OTHER
- [SDR GLBA20090223P](https://openairdocs.org/sdr/GLBA20090223P), Feb 20, 2009: SKIN. DAMAGED. DURING ROUTINE SCHEDULED MAINTENANCE A HOLE IN THE FUSELAGE WAS FOUND AT F.S. 405.5 LEFT OF STRINGER 14L APPROXIMATELY 1.5 INCHES. HOLE SIZE APPROXIMATELY .375 
- [SDR GLBA20090223N](https://openairdocs.org/sdr/GLBA20090223N), Feb 20, 2009: FRAME. CRACKED. DURING ROUTINE SCHEDULED MAINTENANCE FOUND A FRAME CRACKED ON THE FORWARD SIDE OF THE AIRSTAIR DOOR ENTRANCE FRAME AT THE LOWER SNUBBER MOUNT BRACKET UPPER NUTP
- [SDR GLBA20090220I](https://openairdocs.org/sdr/GLBA20090220I), Feb 20, 2009: FRAME. CRACKED. DURING ROUTINE SCHEDULED MX CRACK WAS FOUND ON FRAME AT STRINGER 9R FS 163.975 STRINGER RELIEF CUTOUT. MAINTENANCE DETERMINED THIS DID NOT MEET THE CRITERIA OF 
- [SDR GLBA20090223H](https://openairdocs.org/sdr/GLBA20090223H), Feb 20, 2009: STRINGER. CRACKED. DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND ON FRAME AT FSS 150.60 STRINGER 9R RELIEF CUTOUT. MAINTENANCE DETERMINED THIS DID NOT MEET THE CRITERIA OF A MAJOR
- [SDR GLBA20090220K](https://openairdocs.org/sdr/GLBA20090220K), Feb 20, 2009: ANGLE. CRACKED. DURING ROUTINE SCHEDULED MX THE LT HEAVY ANGLE WAS FOUND CRACKED AT FS 288.0. MAJOR REPAIR - MAINTENANCE REPAIRED THE RIGHT HAND HEAVY DOUBLER IAW EO 09-201-2. 
- [SDR GLBA20090220L](https://openairdocs.org/sdr/GLBA20090220L), Feb 20, 2009: ANGLE. CRACKED. DURING ROUTINE SCHEDULED MX, THE RT HEAVY ANGLE WAS FOUND CRACKED AT FS 288.0. MAINTENANCE REPAIRED THE RIGHT HAND HEAVY DOUBLER I.A.W. .EO. 09-201-2. REPAIR AP
- [SDR GLBA20090223F](https://openairdocs.org/sdr/GLBA20090223F), Feb 20, 2009: SKIN. CRACKED. DURING ROUTINE SCHEDULED MX THE SKIN OF FUSELAGE WAS FOUND CRACKED AROUND TWO RIVETS ONE ON EACH SIDE OF STRINGER ONE AT F.S. 150.60. MAINTENANCE REMOVED CRACKS
- [SDR GLBA20090223G](https://openairdocs.org/sdr/GLBA20090223G), Feb 19, 2009: SKIN. CORRODED. DURING ROUTINE SCHEDULED MX THE SKIN OF THE FUSELAGE IS CORRODED UNDERNEATH FRAME AT FS 203.25 AT STRINGER 15R TOWARDS 16R. LENGTH IS APPROIMATELY 3.5" AND RUNS
- [SDR GLBA20060966](https://openairdocs.org/sdr/GLBA20060966), Jul 20, 2007: RIB. CRACKED. LT WING RIB OB OF POWER PACK CRACKED AT (L) BRACKET APPROX. 1 INCH BY 1 INCH IN LENGTH ORIGINATING FROM RIVET HEAD. MAINTENANCE REPAIRED THE LT WING RIB OB OF H
- [SDR GLBA20030710](https://openairdocs.org/sdr/GLBA20030710), Aug 31, 2004: SKIN. CORRODED. PAX DOOR HAS CORROSION AROUND DOOR HANDLE, REPAIRED PER EO 04-14.
- [SDR GLBA20030589](https://openairdocs.org/sdr/GLBA20030589), Mar 13, 2004: SHUTOFF VALVE. FAILED. RT ENVIRO FAIL ANN ILLUMINATED, R&R RT PRSOV PN 114-380059-5 MM OPS AND LEAK CK GOOD
- [SDR GLBA20030570](https://openairdocs.org/sdr/GLBA20030570), Feb 24, 2004: WARNING LIGHT. ILLUMINATED. CABIN DOOR ANNUNCIATOR CAME ON,R&R AIRSTAIR DOOR FWD LATCH HANDLE SWITCH PN V3-10108 OPS CK GOOD
- [SDR GLBA20030520](https://openairdocs.org/sdr/GLBA20030520), Dec 29, 2003: BRUSH BLOCK. INOPERATIVE. RT PROP DEICE AND PILOT AND COPILOT W/S NOT HEATING, REMOVED AND REPLACED BRUSH BLOCK PN 4E3196-1GLA AND PROP AMP IND PN 114-380049-5.

All 57: https://openairdocs.org/aircraft/N201GL/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/N201GL/stcs.md

## Earlier aircraft with N201GL

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N201GL before.

- [Cancelled 1977-03-25](https://openairdocs.org/deregistered/N201GL-1977-03-25): Mooney M20J, S/N 24-0029. Exported to Canada. Owner: [G B Dupont Co Inc DBA Great Lakes Aero](https://openairdocs.org/faa-owner/G%20B%20DUPONT%20CO%20INC%20DBA%20GREAT%20LAKES%20AERO), [Pontiac, MI](https://openairdocs.org/faa-place/MI/Pontiac)

## 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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