# N245GL: 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-245
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: October 14, 1996
- Certificate issued: March 25, 2023
- Expires: March 31, 2030
- Mode S code: A24333
- 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=245GL
- Page: https://openairdocs.org/aircraft/N245GL

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/N245GL/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 N245GL.

## 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 20040915023069I](https://openairdocs.org/incident/20040915023069I), Sep 15, 2004: Beech 1900D (N245GL), Liberal, KS. (-23) On climbout the pilot reported number two engine returned to idle with the power lever full forward. The number two prop went into autofeather. The…

## Service difficulty reports (81, 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 2022FA0000757](https://openairdocs.org/sdr/2022FA0000757), May 17, 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 FORWARD AND AFT FLANGES AT FUSELA
- [SDR GLBA2017120100693](https://openairdocs.org/sdr/GLBA2017120100693), Nov 30, 2017: CLEVIS. BENT. MAINTENANCE REPORTED THAT THE LOWER FORWARD AIRSTAIR DOOR HANDRAIL CLEVIS WAS BENT. REMOVED AND REPLACED LOWER FORWARD HANDRAIL IAW AMM 52-10-02-201, OPS CHECK 
- [SDR GLBA2017051900657](https://openairdocs.org/sdr/GLBA2017051900657), May 18, 2017: CONTROL HANDLE. INOPERATIVE. THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT EXTEND NORMALLY, LANDING GEAR CIRCUIT RELAY CIRCUIT BREAKER WAS TRIPPED, EXTENDED GEAR MANUALLY. ALL INDICATIO
- [SDR GLBA2017041000647](https://openairdocs.org/sdr/GLBA2017041000647), Apr 8, 2017: CABLE. WORN. MAINTENANCE REPORTED THAT THE MAIN CABIN DOOR FORWARD TOP CABLE IS WORN. REMOVED AND REPLACED THE UPPER FORWARD AIRSTAIR DOOR HANDRAIL CABLE IAW BMM 52-10-02.
- [SDR GLBA2017033100645](https://openairdocs.org/sdr/GLBA2017033100645), Mar 29, 2017: CABLE. LOOSE. MAINTENANCE REPORTED THAT THE UPPER AFT AIRSTAIR DOOR HANDRAIL CABLE WAS TOO LOOSE. RESECURED UPPER AFT AIRSTAIR DOOR HANDRAIL CABLE WITH PROPER TENSION IAW BMM
- [SDR GLBA2017032400644](https://openairdocs.org/sdr/GLBA2017032400644), Mar 23, 2017: CABLE. BROKEN. MAINTENANCE NOTED THAT THE FWD LOWER AIRSTAIR DOOR CABLE WAS BROKEN. REPLACED FORWARD LOWER AIRSTAIR DOOR CABLE, AND AFT LOWER CABLE P/N 1440-43GLA IAW AMM 52-1
- [SDR GLBA2017031700643](https://openairdocs.org/sdr/GLBA2017031700643), Mar 15, 2017: CABLE. LOOSE. MAINTENANCE NOTED THAT THE UPPER FORWARD AIRSTAIR DOOR HANDRAIL CABLE HAS IMPROPER TENSION. ADJUSTED THE CABLE IAW MM 52-10-02.
- [SDR GLBA2017022100633](https://openairdocs.org/sdr/GLBA2017022100633), Feb 18, 2017: CABLE. LOOSE. MAINTENANCE REPORTED THAT THE UPPER FORWARD PAX DOOR HANDRAIL CABLE TENSION IS TOO LOW. SECURED THE CABLE WITH PROPER TENSION IAW BMM 52-10-02.
- [SDR GLBA2016110700621](https://openairdocs.org/sdr/GLBA2016110700621), Dec 7, 2016: WARNING SYSTEM. MALFUNCTIONED. SIG EVENT, PILOT REPORTED THAT WHEN EXTENDING THE LANDING GEAR, LT MAIN GEAR ANNC FAILED TO ILLUMINATE WITH GEAR DOWN, LANDING GEAR INTRANSIT LIGHT DID NOT ILLU
- [SDR GLBA2016052700589](https://openairdocs.org/sdr/GLBA2016052700589), May 23, 2016: WARNING SYSTEM. FALSE ACTIVATION. THE CABIN DOOR ANNC ILLUMINATED IN FLIGHT, CREW DECLARED AN EMER, INDICATION SYS WAS MEL'D. SUPPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE RE
- [SDR GLBA2015111700560](https://openairdocs.org/sdr/GLBA2015111700560), Nov 16, 2015: WARNING SYSTEM. FALSE ACTIVATION. PILOT REPORTED THAT WHILE IN CRUISE, THE DISCHARGE LIGHT ON THE NR 1 FIRE EXTINGUISHER ILLUMINATED. REPLACED SOFT SPLICE, PN M81714/11-20D, ON WIRE W23B22 IAW E
- [SDR GLBA2015100500555](https://openairdocs.org/sdr/GLBA2015100500555), Nov 2, 2015: CONNECTOR. DIRTY. PILOT REPORTED THAT THE NR 1 ENG EXTINGUISHER ANNC DISCHARGE NR 1 LIGHT ILLUMINATED, ON CLIMB OUT. FOUND NO CONTINUITY BETWEEN PIN M OF CONNECTOR P281 & THE FIR
- [SDR GLBA2014112600470](https://openairdocs.org/sdr/GLBA2014112600470), Nov 26, 2014: SKIN. CRACKED. MAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE LT SIDE BELLY SKIN AT BL 29.06 & WING SPAR, .5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND 
- [SDR GLBA2014111700466](https://openairdocs.org/sdr/GLBA2014111700466), Nov 17, 2014: FRAME. CRACKED. MAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FRAME FLANGE AT FS 177.35 BETWEEN STRINGERS 13L & 14L IN THE FRAME FLANGE BEND RADIUS AT OTBD EN
- [SDR GLBA2014111300464](https://openairdocs.org/sdr/GLBA2014111300464), Nov 12, 2014: SKIN. CRACKED. MAJOR REPAIR DURING A SCHEDULED INSPECTION FOUND THE EMER EXIT 6A EXTERIOR BONDED SKIN CRACKED AT THE INTERIOR LOWER AFT CORNER, 1.2 INCHES IN LENGTH. REPAIRED 
- [SDR GLBA2014091600438](https://openairdocs.org/sdr/GLBA2014091600438), Sep 16, 2014: SKIN. CRACKED. DURING A SCHEDULED INSPECTION FOUND A 7/8 INCH LONGITUDINAL CRACK ON THE UPPER FUSELAGE AT APPROX FUSELAGE STATION 214.25 ON FUSELAGE SKIN 27 APPROX 2 INCHES RI
- [SDR GLBA2014071400421](https://openairdocs.org/sdr/GLBA2014071400421), Jul 12, 2014: UPLOCK SWITCH. FAULTY. PILOT REPORTED THAT ON MLG EXTENSION THE CREW HEARD THE MOTOR RUN FOR APPROX 15 SECONDS THEN THE CB NEXT TO THE GEAR HANDLE POPPED. RAN CHECKLIST & MANUALLY EXT
- [SDR GLBA2014070100418](https://openairdocs.org/sdr/GLBA2014070100418), Jul 1, 2014: UPLOCK SWITCH. MALFUNCTIONED. PILOT REPORTED THAT THE CIRCUIT BREAKER TRIPPED ON THE LANDING GEAR CONTROL, RAN CHECKLIST, PROCEEDED TO DESTINATION & USED THE MANUAL EXTENSION. MAINTENANCE R 
- [SDR GLBA2013120500353](https://openairdocs.org/sdr/GLBA2013120500353), Dec 4, 2013: HYDRAULIC SYSTEM. CONTAMINATED. PILOT REPORTED THAT AFTER SELECTING GEAR DOWN, LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. RAN THROUGH CHECK LIST, MANUALLY EXTENDED GEAR, ALL INDICATIONS SHOWE
- [SDR GLBA2013112200351](https://openairdocs.org/sdr/GLBA2013112200351), Nov 21, 2013: HANDLE. SEPARATED. PILOT REPORTED THAT THE AIR STAIR DOOR HANDLE CAME OFF. INSTALLED A NEW SNAP RING & REINSTALLED DOOR HANDLE, IAW BMM 52-10-05, OPS CHECKED GOOD.
- [SDR GLBA2013112100350](https://openairdocs.org/sdr/GLBA2013112100350), Nov 20, 2013: TERMINAL. OUT OF POSITION. PILOT REPORTED THAT SPARKS WERE COMING OUT FROM BEHIND THE ICE PROTECTION PANEL. THE RT PITOT TERMINAL CONTACTING THE MOUNTING STRUCTURE REPOSITIONS THE RT PITO
- [SDR GLBA2013091300309](https://openairdocs.org/sdr/GLBA2013091300309), Sep 12, 2013: ACTUATOR. FAILED. PILOT REPORTED THAT THEY LOWERED GEAR HANDLE, LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED, GEAR DID NOT MOVE, HYD POWER PACK DID NOT START AND LANDING GEAR HANDL
- [SDR GLBA2013011500158](https://openairdocs.org/sdr/GLBA2013011500158), Jan 15, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND FRAME CRACKED AT THE AFT LOWER CARGO DOOR FRAME AT FS 509.5, 2 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-002.
- [SDR GLBA2013011500157](https://openairdocs.org/sdr/GLBA2013011500157), Jan 15, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND FRAME CRACKED AT FS 107, LT SIDE FRAME BEHIND FINGER DOUBLER IN THE BEND RADIUS, 1" IN LENGTH. REPAIRED IAW EO 13-1
- [SDR GLBA2013011500156](https://openairdocs.org/sdr/GLBA2013011500156), Jan 15, 2013: SKIN. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND SKIN CRACKED AT FS 438 AND JUST ABOVE STRINGER 8L PROTRUDING OUT OF RIVET, .25" IN LENGTH. REPAIRED IAW EO 13-1900-
- [SDR GLBA2013011400155](https://openairdocs.org/sdr/GLBA2013011400155), Jan 14, 2013: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE RT VERTICAL STAB FWD SPAR CAP ANGLE BY THE TOP RIVET GOING TOWARDS THE BEND RADIUS, 1" IN LENGTH. RE
- [SDR GLBA2013011400154](https://openairdocs.org/sdr/GLBA2013011400154), Jan 14, 2013: STRUCTURE. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT INBD WING, INBD LOWER AFT CORNER BY SPAR RIB FLANGE , 1" IN LENGTH. REPAIRED IAW EO 13-1900-57-00
- [SDR GLBA2013011400153](https://openairdocs.org/sdr/GLBA2013011400153), Jan 14, 2013: SKIN. CORRODED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND BELLY SKIN CORRODED BETWEEN STRINGERS 14R AND 15R AT FRAME LOCATION AT FS 243.25. REPAIRED IAW EO 13-1900-53-001.
- [SDR GLBA2012103000096](https://openairdocs.org/sdr/GLBA2012103000096), Oct 29, 2012: OIL SYSTEM. LEAKING. PILOT REPORTED THAT THE OIL PRESSURE ON NR 1 ENGINE DROPPED TO 50 PSI REDUCED POWER TO IDLE OIL PRESSURE CONTINUED TO DROP TO 40 PSI LOW OIL PRESSURE ANNUNCIATO
- [SDR GLBA2012083100042](https://openairdocs.org/sdr/GLBA2012083100042), Aug 30, 2012: ATTACH FITTING. CRACKED. VERTICAL STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD IS CRACKED AT THE UPPER END AT VSS 84.10. CRACK IS .7500 INCH IN LENGTH, BEGINNING AT THE SECOND FASTENE
- [SDR GLBA2012042301](https://openairdocs.org/sdr/GLBA2012042301), Apr 20, 2012: CIRCUIT BOARD. DAMAGED. PILOT REPORTED THAT THE LT AUTOFEATHER SYS DISARMED AND REARMED REPEATEDLY DURING FLIGHT. MX REPLACED THE PCB A123, OPS CHECKED GOOD.
- [SDR GLBA2012022401](https://openairdocs.org/sdr/GLBA2012022401), Feb 24, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE HORIZONTAL STAB FWD SPAR WEB JUST INBD OF RT HSS 5.000 OTBD UPPER CORNER. REPAIRED IAW EO 12-1900-55
- [SDR GLBA2012022002](https://openairdocs.org/sdr/GLBA2012022002), Feb 20, 2012: BULKHEAD. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT A SCREW HOLE ON THE AFT PRESSURE BULKHEAD, BEHIND AFT WALL AT 1 O`CLOCK POSITION, 1" IN LENGTH. REPAIRED
- [SDR GLBA2012022001](https://openairdocs.org/sdr/GLBA2012022001), Feb 20, 2012: STRINGER. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS AT STRINGER 10L AND FS 165.4 AND WS 236 FROM A SCREW HOLE, EA CRACK .375 EACH. REPAIRED IAW EO 12-1900-55-
- [SDR GLBA20111229A](https://openairdocs.org/sdr/GLBA20111229A), Dec 29, 2011: BULB. INOPERATIVE. ONE INSTRUMENT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECKED GOOD.
- [SDR GLBA201112024](https://openairdocs.org/sdr/GLBA201112024), Nov 30, 2011: PUMP. LEAKING. FUEL LEAKING OUT OF MAIN DRAIN LT NACELLE. MX R & R LT LOW PRESSURE FUEL PUMP.
- [SDR GLBA20111017F](https://openairdocs.org/sdr/GLBA20111017F), Oct 15, 2011: SWITCH. OUT OF ADJUST. PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE RIGGED CABIN DOOR ANNUNCIATOR CENTER LATCH SWITCH IAW BMM 52-70-02, OPS CHECKE
- [SDR GLBA20110923F](https://openairdocs.org/sdr/GLBA20110923F), Sep 23, 2011: SKIN. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON AN REPAIR AT FS 164.415 AND STRINGER 9R, .75" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL
- [SDR GLBA20110921J](https://openairdocs.org/sdr/GLBA20110921J), Sep 21, 2011: DOOR FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE CARGO DOOR FRAME, FWD SIDE, FS 456, BETWEEN STRINGER 3L AND 4L, .7" IN LENGTH. MX REPA
- [SDR GLBA20110921G](https://openairdocs.org/sdr/GLBA20110921G), Sep 20, 2011: STRINGER. CORRODED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND CORROSION ON 2" OF STRINGER 16 AT FS 228.25, BELLY OF FUSELAGE. MX REPAIRED THE AFFECTED AREA AND PERFORME
- [SDR GLBA20110921F](https://openairdocs.org/sdr/GLBA20110921F), Sep 20, 2011: SKIN. CORRODED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, FOUND BELLY CORROSION AT FS 228.25 MEASURING 7.5", 13" INBD OF LT TRANSPONDER ANTENNA, 12" INBD OF RT TRANSPONDE
- [SDR V0DR2011010](https://openairdocs.org/sdr/V0DR2011010), May 3, 2011: SLIP RING. DETERIORATED. DURING SCHEDULED MX, A MECHANIC NOTED THAT DURING CLEANING OF THE PROP DEICE SLIP RING THAT THE DIELECTRIC FILLER IN BETWEEN COPPER RINGS APPEARED TO BE DETERIO
- [SDR GLBA20100630K](https://openairdocs.org/sdr/GLBA20100630K), Jun 30, 2010: SKIN. CORRODED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP FOUND CORROSION ON BELLY SKIN AT FS 213.25 BETWEEN STRINGER 16L AND 15L, WITH AN AREA OF 1" BY .75". MAINTENANCE
- [SDR GLBA20100630J](https://openairdocs.org/sdr/GLBA20100630J), Jun 30, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 288.00 AT STRINGER 4R CUTOUT, .35" IN LENGTH. MAINTENANCE REPAIRED TH
- [SDR GLBA20100630F](https://openairdocs.org/sdr/GLBA20100630F), Jun 30, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 177.35 AT STRINGER 6R CUTOUT, .3" IN LENGTH. MAINTENANCE REPAIRED THE
- [SDR GLBA20100630H](https://openairdocs.org/sdr/GLBA20100630H), Jun 30, 2010: STRINGER. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND AT FS 451 ON THE STRINGER 10R ON THE HORIZONTAL PORTION OF THAT STRINGER, .45" IN LENGTH
- [SDR GLBA20100630G](https://openairdocs.org/sdr/GLBA20100630G), Jun 30, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT F.S. 456 AT STRINGER 10R CUTOUT, .4" IN LENGTH. MAINTENANCE REPAIRED THE
- [SDR GLBA20100113G](https://openairdocs.org/sdr/GLBA20100113G), Jan 13, 2010: SKIN. CRACKED. MAJOR REPAIR - DURING A ROUTINE DE-ICE REPLACEMENT, A CRACK WAS FOUND ON THE RT WING AT WS 190.74 AT THE WING BOOT TUBE CONNECTION HOLE, PROTRUDING INBD. CRACK 
- [SDR GLBA20090409A](https://openairdocs.org/sdr/GLBA20090409A), Apr 9, 2009: TRANSDUCER. MALFUNCTIONED. AIR RETURN - PILOTS REPORTED A LIGHTNING STIKE ON THE NOSE WHICH RESULTED IN A RUNWAWAY RUDDER BOOST SITUATION IF THE RUDDER BOOST SWITCH WAS "ON". RUDDER BOOST
- [SDR GLBA20090408F](https://openairdocs.org/sdr/GLBA20090408F), Apr 7, 2009: SWITCH. OUT OF ADJUST. SIGNIFICANT EVENT-SUSPECTED AUTOFEATHER -PILOTS REPORTED THAT THE NR 2 ENGINE PROPELLER FEATHERED VIOLENTLY IN AIR WITH PROPELLERS FULL FWD AND REDUCING POWER. 

All 81: https://openairdocs.org/aircraft/N245GL/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/N245GL/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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