# N261GL: 1996 Raytheon 1900D

- Status: Valid registration
- Airframe: [Raytheon 1900D](https://openairdocs.org/model/raytheon-1900d) (registry code 7150005, 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-261
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: December 17, 1996
- Certificate issued: March 25, 2023
- Expires: March 31, 2030
- Mode S code: A28355
- 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=261GL
- Page: https://openairdocs.org/aircraft/N261GL

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 (Raytheon 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/N261GL/ads.md

## Information bulletins (advisory) (10 in force)

- [SAIB 2026-02](https://openairdocs.org/saib/2026-02): Elevator Tab Control System. Issued Jan 21, 2026
- [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012
- [SAIB CE-05-83](https://openairdocs.org/saib/CE-05-83): . Issued Aug 26, 2005
- [SAIB CE-00-24](https://openairdocs.org/saib/CE-00-24): . Issued Jul 11, 2000
- [SAIB CE-00-15](https://openairdocs.org/saib/CE-00-15): . Issued Jan 21, 2000
- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015
- [SAIB NE-12-04](https://openairdocs.org/saib/NE-12-04): Turbine/ Turboprop Engine: Reduction Gearbox. Issued Nov 1, 2011
- [SAIB NE-10-47](https://openairdocs.org/saib/NE-10-47): Turbine Engine Compressor Section. Issued Aug 30, 2010
- [SAIB NE-06-34](https://openairdocs.org/saib/NE-06-34): . Issued Mar 21, 2006
- [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA08IA096](https://openairdocs.org/ntsb/SEA08IA096), Mar 26, 2008: Raytheon 1900D (N261GL), Page, AZ, incident, minor damage. Probable cause: The flight crew’s unprofessional behavior and deviation from standard operating procedures which resulted in an in-flight emergency.

## 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 20121130026259I](https://openairdocs.org/incident/20121130026259I), Nov 30, 2012: Raytheon Aircraft Company 1900D (N261GL), Minneapolis, MN, Minor damage. Aircraft was on runway 17 awaiting takeoff clearance. When cleared for takeoff, the captain placed his hands on the power levers and immediately heard a fire…
- [Incident 20080326835639I](https://openairdocs.org/incident/20080326835639I), Mar 26, 2008: Beech 1900D (N261GL), Page, AZ, Minor damage. (-23) On March 26,2008, at 1220 MST, a Raytheon aircraft company 1900D, operating as great lakes airlines flight 5187, N261GL, returned to land due to an open…

## Service difficulty reports (67, 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 GLBA2017121800698](https://openairdocs.org/sdr/GLBA2017121800698), Dec 15, 2017: COUPLING. LEAKING. CREW REPORTED THAT THERE WAS A HYDRAULIC LEAK IN THE RIGHT FRONT PART OF THE RIGHT WHEEL [WELL]. 6-7 INCH PUDDLE BUT COULD SEE NO ACTUAL DRIPS. MAINTENANCE TROU
- [SDR GLBA2016120900623](https://openairdocs.org/sdr/GLBA2016120900623), Dec 8, 2016: HANDLE. CORRODED. DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND CORROSION AROUND AND THROUGH BOLTS OF INTERIOR HANDLE BELLCRANK ASSY. ON AIRSTAIR DOOR, THE BELLCRANK ATTACHMEN
- [SDR GLBA2016111800617](https://openairdocs.org/sdr/GLBA2016111800617), Nov 18, 2016: FRAME. CRACKED. DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND FUSELAGE FRAME AT BS 183.25 BETWEEN STRINGERS 2R AND 3R CRACKED AT THE INBOARD LOWER CORNER AREA OF DUCT CUTOUT
- [SDR GLBA2015011100492](https://openairdocs.org/sdr/GLBA2015011100492), Jan 11, 2015: ELBOW. CRACKED. WHILE IN CRUISE RT ENG LOW OIL PSI LIGHT CAME ON WITH NO OTHER ABNORMALITIES NOTED, IE LOUD BANG FLUX IN PWR, LOOKED OIL PSI GAUGE NOTICED GAUGE RAPIDLY DECREAS
- [SDR GLBA2015011200492](https://openairdocs.org/sdr/GLBA2015011200492), Jan 11, 2015: UNKNOWN. MALFUNCTIONED. WHILE IN CRUISE RT ENG LOW OIL PSI LIGHT CAME ON WITH NO OTHER ABNORMALITIES NOTED, IE LOUD BANG FLUX IN POWER, LOOKED OIL PSI GAUGE NOTICED GAUGE RAPIDLY DECRE
- [SDR GLBA2014070300419](https://openairdocs.org/sdr/GLBA2014070300419), Jul 2, 2014: LINE. RUPTURED. LANDING GEAR FAILED TO EXTEND NORMALLY, GEAR INTRANSIT LIGHT ILLUMINATED, WITH GEAR SELECTED DOWN. TRANSIT LIGHT FAILED TO EXTINGUISH NORMALLY, HYD FLUID LOW AN
- [SDR GLBA2013102300344](https://openairdocs.org/sdr/GLBA2013102300344), Oct 23, 2013: STRINGER. CORRODED. DURING A SCHEDULED INSPECTION FOUND CORROSION ON STRINGER 16 AT FS 243.25, RUNS APPROX 6 INCHES. REPAIRED IAW EO 13-1900-53-075. MAJOR REPAIR.
- [SDR GLBA2013102200343](https://openairdocs.org/sdr/GLBA2013102200343), Oct 22, 2013: SKIN. CORRODED. DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CORRODED AT FS 243.25 AND STRINGER 16. REPAIRED IAW EO 13-1900-53-076. MAJOR REPAIR.
- [SDR GLBA2013082100295](https://openairdocs.org/sdr/GLBA2013082100295), Aug 20, 2013: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CHAFED, FWD OF FS 370.25 BETWEEN STRINGER 15--16L. REPAIRED IAW EO 13-1900-53-056.
- [SDR GLBA2013082100298](https://openairdocs.org/sdr/GLBA2013082100298), Aug 20, 2013: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION, FOUND STRINGER 15L FLANGE DAMAGED AT 2 LOCATIONS FROM THE VENT BLOWER BRACKET, CHAFED AT FS 368.25 AND 370.25, CHAFED HALF WAY TH
- [SDR GLBA2013082100297](https://openairdocs.org/sdr/GLBA2013082100297), Aug 20, 2013: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION, FOUND STRINGER 16 CHAFED AT FOUR LOCATIONS FROM THE VENT BLOWER DUCT HARDWARE-SCREWS, DAMAGE AT TOP OF STRINGER BETWEEN BS 370.25
- [SDR GLBA2013082100296](https://openairdocs.org/sdr/GLBA2013082100296), Aug 20, 2013: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN AT FS 368.25 - 370.25 HAS TWO HOLES WORN THRU SKIN, HOLES NEXT TO STRINGER 15L, FWD AREA, HOLE J SHAPED IS .85" 
- [SDR GLBA2013052000251](https://openairdocs.org/sdr/GLBA2013052000251), May 20, 2013: SKIN. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT LOWER BELLY SKIN OVER THE WING SPAR AT FS 288, 2.25 INCHES IN LENGTH. REPAIRED IAW EO 13-1900-53-
- [SDR GLBA2013051600250](https://openairdocs.org/sdr/GLBA2013051600250), May 15, 2013: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE SPAR CAP, RT VERT STAB, SECOND FASTENER DOWN FROM THE TOP, .375" IN LENGTH. REPAIRED IAW EO 13-1900-5
- [SDR GLBA2013051600249](https://openairdocs.org/sdr/GLBA2013051600249), May 15, 2013: RIB. CHAFED. DURING A SCHEDULED ROUTINE INSPECTION FOUND CHAFED AREA ON THE LT RIB 1 AT JUNCTION WITH WING SPAR, FLANGE PORTION OF RIB 1 WORN DOWN TO DOUBLER FLANGE, 1.5"*.7
- [SDR GLBA2013051600248](https://openairdocs.org/sdr/GLBA2013051600248), May 15, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 107 AT THE INTERSECTION OF LONGERON UNDER RT FINGER DOUBLER, .5" IN LENGTH. REPAIRED IAW EO 13-1900-53
- [SDR GLBA2013011400150](https://openairdocs.org/sdr/GLBA2013011400150), Jan 12, 2013: DIODE. FAILED. PILOT REPORTED THAT THE INST EMERGENCY LIGHTS FAILED TO ILLUMINATE WITH THE INSTRUMENT EMERGENCY LIGHT SWITCH. MX REPLACED DIODES, OPS CHECKED GOOD.
- [SDR GLBA2013010800148](https://openairdocs.org/sdr/GLBA2013010800148), Jan 7, 2013: FUSE. INOPERATIVE. PILOT REPORTED THAT THE EMERGENCY INSTRUMENT LIGHTS ARE INOPERATIVE. MX REPLACED THE HOT BATTERY FUSE, OPS CHECKED GOOD.
- [SDR GLBA2012112600117](https://openairdocs.org/sdr/GLBA2012112600117), Nov 26, 2012: CURRENT LIMITER. FAILED. PILOT REPORTED THAT 2 MINUTES INTO CRUISE, HAD SMOKE AND FUMES IN COCKPIT AND COMING FROM THE EYEBALL VENTS IN CABIN, CLOSED LT BLEED AIR AND SMOKE CLEARED, DEC
- [SDR GLBA2012111200105](https://openairdocs.org/sdr/GLBA2012111200105), Nov 9, 2012: BULB. MISSING. PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT BULB IS MISSING. MX REPLACED THE BULB, OPS CK GOOD.
- [SDR GLBA2012091700057](https://openairdocs.org/sdr/GLBA2012091700057), Sep 17, 2012: SKIN. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE VERTICAL STAB RT SIDE AFT LWR SPAR SKIN 8.5" UP FROM BOTTOM, 3" IN LENGTH. REPAIRED IAW EO 12-190
- [SDR GLBA2012091700056](https://openairdocs.org/sdr/GLBA2012091700056), Sep 17, 2012: ATTACH FITTING. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT SPAR CAP ON VERTICAL STAB AT HORIZONTAL STAB ATTACHMENT FITTING AT 2ND FASTENER FROM TOP, VSS 84.1
- [SDR GLBA2012022102](https://openairdocs.org/sdr/GLBA2012022102), Feb 21, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND 4 CRACKS ON THE HORIZONTAL STAB REAR SPAR WEB AROUND ACCESS HOLE AT HSS. 00.0. REPAIRED THE AFFECTED AREA AND PERFOR
- [SDR GLBA20120214F](https://openairdocs.org/sdr/GLBA20120214F), Feb 14, 2012: SKIN. CORRODED. DURING A SCHEDULED ROUTINE INSP FOUND BELLY CORROSION AT FS 198.25 BETWEEN STRINGER 15 AND 16L, AREA BETWEEN A DOUBLE ROW OF FASTENERS, AREA .75" BY .5". REPAIR
- [SDR GLBA20120214G](https://openairdocs.org/sdr/GLBA20120214G), Feb 14, 2012: DOOR FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND THE A/S DOOR ENTRANCE LOWER FRAME CRACKED IN THE AFT CORNER AT FS 176 AND STRINGER 11L, .1250" IN LENGTH. REPAIRED T
- [SDR GLBA201112052](https://openairdocs.org/sdr/GLBA201112052), Dec 2, 2011: DOOR. OPEN. DURING THE PASSENGER BRIEFING (WITH ENGINES NOT RUNNING), A PASSENGER OPENED UP THE 6C EMERGENCY EXIT DOOR. MX REINSTALLED THE EMERGENCY EXIT DOOR.
- [SDR GLBA20111027G](https://openairdocs.org/sdr/GLBA20111027G), Oct 26, 2011: SEAL. DIRTY. PILOT REPORTED THAT THE CABIN DOOR WAS SQUEELING IN FLIGHT. MX CLEANED THE DOOR SEAL, PRESSURIZATION CHECKS GOOD, OK FOR SERVICE.
- [SDR GLBA20110420G](https://openairdocs.org/sdr/GLBA20110420G), Apr 19, 2011: DOOR FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER GARGO DOOR FUSELAGE FRAME AT FS 460 AND STRINGER 3L CRACKED 1.3" IN LENGTH. MA
- [SDR GLBA20110214F](https://openairdocs.org/sdr/GLBA20110214F), Feb 13, 2011: BLOWER. WORN. PILOT REPORTED THAT WHEN BLOWER IS PLACED TO AUTO, IT GAVE OFF AN ELECTRICAL ODOR, WHEN TURNED OFF, ODOR WENT AWAY. MAINTENANCE REPLACED THE FORWARD BLOWER ASSY
- [SDR GLBA201010311](https://openairdocs.org/sdr/GLBA201010311), Oct 31, 2010: BULB. MISSING. PILOT REPORTED THAT ONE OF THERE EMERGENCY LIGHTS ON THE CAPTAIN'S SIDE IS MISSING A BULB. MAINTENANCE REPLACED THE MISSING BULB PN 1864 AND FILTER PN D165-100-
- [SDR GLBA201009141](https://openairdocs.org/sdr/GLBA201009141), Sep 14, 2010: ENGINE. LOW TORQUE. INCREASING POWER ON APPROACH, LT ENGINE REMAINED AROUND 500 LBS TORQUE, DID NOT RESPOND TO POWER LEVER INPUT WHILE RT ENGINE SPOOLED TO APPROX 1200 TORQUE. LT E
- [SDR GLBA20100830F](https://openairdocs.org/sdr/GLBA20100830F), Aug 30, 2010: SKIN. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE LOWER FWD SKIN ON THE 6A EMERGENCY EXIT DOOR, 1.2" IN LENGTH. MAINTENANCE REPAIRED THE A
- [SDR GLBA20100827F](https://openairdocs.org/sdr/GLBA20100827F), Aug 27, 2010: FRAME. CRACKED. DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A THE CARGO PARTITION FUSELAGE ATTACH POINT HOLES ARE WORN, TOP LEFT, TOP CENTER, AND TOP RIGHT. MAINTE
- [SDR GLBA20100826G](https://openairdocs.org/sdr/GLBA20100826G), Aug 26, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK ON THE LT HEAVY FRAME ANGLE AT FS 288 FWD BEND RADIUS, 1.4" IN LENGTH. MAINTENANCE REPAIRED THE
- [SDR GLBA20100309G](https://openairdocs.org/sdr/GLBA20100309G), Mar 8, 2010: SKIN. DENTED. MAJOR REPAIR - DURING A POSTFLIGHT INSP, A DENT WAS FOUND ON THE LT SIDE OF THE ACFT 6" AFT OF THE FWD CARGO DOOR BULKHEAD 6" FROM THE BOTTOM, APPROX 2" IN LENG
- [SDR GLBA100307001](https://openairdocs.org/sdr/GLBA100307001), Mar 7, 2010: SKIN. DENTED. DURING A POSTFLIGHT INSP, A DENT WAS FOUND ON THE LT SIDE OF THE ACFT 6" AFT OF THE FWD CARGO DOOR BULKHEAD 6" FROM THE BOTTOM, APPROX 2" IN LENGTH. MX REPAIRED
- [SDR GLBA20090921G](https://openairdocs.org/sdr/GLBA20090921G), Sep 18, 2009: DOOR LATCH. LACK OF LUBE. DURING ROUTINE SCHEDULED MAINTENANCE THE EMERGENCY EXT DOOR 6C DID NOT OPEN PROPERLY. MAINTENANCE LUBED THE LATCH MECHANICAL SHAFT, RE-INSTALLED THE DOOR I.A.W.
- [SDR GLBA20090921F](https://openairdocs.org/sdr/GLBA20090921F), Sep 18, 2009: DOOR. STIFF. DURING ROUTINE SCHEDULED MAINTENANCE THE EMERGENCY EXT DOOR 4C DID NOT OPEN PROPERLY. MAINTENANCE LUBED THE LATCH MECHANICAL SHAFT, RE-INSTALLED THE DOOR IAW MM
- [SDR GLBA20090512F](https://openairdocs.org/sdr/GLBA20090512F), May 12, 2009: HANDLE. MISALIGNED. FLT 5091 - ENROUTE, PILOTS REPORTED THAT THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE J-HOOK DID RELEASE. THEY TRIED A COUPLE TIME TO GET THE GEAR TO COME UP. 
- [SDR GLBA20090420G](https://openairdocs.org/sdr/GLBA20090420G), Apr 16, 2009: FRAME. CRACKED. DURING A SCHEDULED STRUCTURAL CHECK, MX DISCOVERED A CRACK ON THE RT HEAVY ANGLE AT FA 288.0. LENGTH OF CRACK APPROX 1.5 INCH LONG. MX REPAIRED THE RT HEAVY ANG
- [SDR GLBA20090420F](https://openairdocs.org/sdr/GLBA20090420F), Apr 16, 2009: SKIN. CRACKED. DURING A SCHEDULED STRUCTURAL CHECK MX DISCOVERED A CRACK ON THE LT FUSELAGE SKIN JUST INBD OF THE LT WING BOTTOM WING PANEL AT F.S. 303.25. CRACK APPROXIMATELY
- [SDR GLBA20061085](https://openairdocs.org/sdr/GLBA20061085), Mar 28, 2008: FRAME. BENT. FRAME SECTION AT FS 469 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 469 STRINGER 3L IAW SRM 51-40. P/N NR 129-440044-75.
- [SDR GLBA20061087](https://openairdocs.org/sdr/GLBA20061087), Mar 28, 2008: FRAME. BENT. FRAME SECTION AT FS 495.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 495.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-71.
- [SDR GLBA20061086](https://openairdocs.org/sdr/GLBA20061086), Mar 28, 2008: FRAME. BENT. FRAME SECTION AT FS 482.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 482.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-73
- [SDR 20061087](https://openairdocs.org/sdr/20061087), Mar 28, 2008: FRAME. BENT. FRAME SECTION AT FS. 495.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 495.75 STRINGER 3L IAW SRM 51-40. PN 129-440044-71.
- [SDR 20061086](https://openairdocs.org/sdr/20061086), Mar 28, 2008: FRAME. BENT. FRAME SECTION AT FS 482.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 482.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-73.
- [SDR 20061085](https://openairdocs.org/sdr/20061085), Mar 28, 2008: FRAME. BENT. FRAME SECTION AT FS 469 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 469 STRINGER 3L IAW SRM 51-40. P/N 129-40044-75.
- [SDR GLBA20061009](https://openairdocs.org/sdr/GLBA20061009), Oct 8, 2007: HINGE FITTING. DAMAGED. CARGO DOOR HINGE HALF FORWARD AND AFT LUGS MISSING AND SEVERAL LOOSE RIVETS. MAINTENANCE REPLACED HINGE HALF ON CARGO DOOR IAW SRM 52-90. RII INSPECTION COMPLIE
- [SDR GLBA20061007](https://openairdocs.org/sdr/GLBA20061007), Oct 1, 2007: STRINGER SPLICE. CORRODED. BELLY CORROSION FOUND AT APPROXIMATELY FS 246 TO FS 250 ON STRINGER 15R. MAINTENANCE REPLACED DAMAGED STRINGER SECTION PER ENGINEERING ORDER 07-UE261-01. APPROX
- [SDR GLBA20061008](https://openairdocs.org/sdr/GLBA20061008), Oct 1, 2007: FRAME. CRACKED. FRAME CRACKED AT STRINGER CUTOUT FS 177 AT STRINGER 9AR. REPAIRED FRAME AT STRINGER RELIEF HOLE FS 177 AND STRINGER 9AR IAW 1900D SRM 51-70. REPAIR DIMENSIONS 4

All 67: https://openairdocs.org/aircraft/N261GL/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 (Raytheon 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/N261GL/stcs.md

## Related

- Other Raytheon 1900D aircraft: https://openairdocs.org/model/raytheon-1900d/aircraft.md
- The Pratt & Whitney PT6A series engine: https://openairdocs.org/engine/pratt-whitney-pt6a-series.md

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