# N169GL: 1995 Beech 1900D

- Status: Valid registration
- Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162, 19 seats)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (Textron Aviation Inc.) (OpenAirDocs)
- Serial number: UE-169
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: September 26, 1995
- Certificate issued: March 25, 2023
- Expires: March 31, 2030
- Mode S code: A113BE
- 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=169GL
- Page: https://openairdocs.org/aircraft/N169GL

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/N169GL/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 DCA13FA148](https://openairdocs.org/ntsb/DCA13FA148), Sep 1, 2013: Beech 1900D (N169GL), Telluride, CO, substantial damage. Probable cause: Failure of the left main landing gear actuator internal lock to engage in the locked position for undetermined reasons.

## 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 20180109000569I](https://openairdocs.org/incident/20180109000569I), Jan 9, 2018: Beech 1900D (N169GL), Prescott, AZ, Minor damage. On 01/09/2017 at 19:39 MDT, N169GL, a Beech 1900D aircraft sustained minor damage (broken pilots right hand rudder pedal arm to rudder pedal attach point)…
- [Accident 20130901025629A](https://openairdocs.org/incident/20130901025629A), Sep 1, 2013: Beech 1900D (N169GL), Telluride, CO, Substantial damage. Great lakes airlines Beech 1900-D , aircraft N169GL flight 7125 left main landing gear collapsed during landing on runway 27 at Telluride regional airport…

## Service difficulty reports (68, 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 TIMA20260425001](https://openairdocs.org/sdr/TIMA20260425001), Apr 25, 2026: BLOWER MOTOR. INOPERATIVE. WAS IN CRUISE FROM MKG TO IND FOR ABOUT 5 MINUTES. BEGAN TO SMELL ODOR. GOT SLIGHTLY STRONGER WITHIN ABOUT 2 MINUTES. CHOSE TO DIVERT TO SBN. ON APPROACH/FINAL 
- [SDR TIMA20240724009](https://openairdocs.org/sdr/TIMA20240724009), Jul 24, 2024: LANDING GEAR. FAULTED. DURING FLINAL APPROACH, ALL THREE BUSS TIE ANNUCIATOR LIGHTS ILLUMINATED INDICATING A FAILURE OF THE CENTER BUS. I VERIFIED THE STATUS OF THE ELECTRICAL SYSTEM 
- [SDR TIMA20240705007](https://openairdocs.org/sdr/TIMA20240705007), Jul 5, 2024: ENGINE. LOW TORQUE. AFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISING PROPERLY AND INCORRECT ENGINE CONTROL / FEEL, PILOT NOTICED IMPROPER POWER OUT OF LEFT ENGINE AN
- [SDR GLBA2018011100699](https://openairdocs.org/sdr/GLBA2018011100699), Jan 9, 2018: RUDDER PEDAL. SHEARED. PILOTS REPORTED THAT WHILE TAXING OFF THE RUNWAY, WHEN RIGHT RUDDER PRESSURE WAS APPLIED, THE CAPTAIN'S RIGHT RUDDER PEDAL ASSEMBLY SHEARED OFF, FLOPS LOOSE ON 
- [SDR GLBA2014112100467](https://openairdocs.org/sdr/GLBA2014112100467), Nov 20, 2014: UNKNOWN. MALFUNCTIONED. PILOT REPORTED THAT DURING GEAR RETRACTION, LG HANDLE LIGHT REMAINED ON & LG HANDLE CB POPPED. WENT THROUGH CHECKLIST & MANUALLY EXTENDED GEAR, GOT THREE GREENS
- [SDR GLBA2013092600325](https://openairdocs.org/sdr/GLBA2013092600325), Sep 26, 2013: STRUCTURE. DAMAGED. DURING A SCHEDULED INSPECTION, FOUND DAMAGE ON THE BOTTOM SIDE OF THE WING TIP, APPROXIMENTLY 3 INCHES FROM WING TIP, DAMAGE DOES NOT APPEAR TO PENATRATE HONEYC
- [SDR GLBA2013092000322](https://openairdocs.org/sdr/GLBA2013092000322), Sep 20, 2013: FRAME. CRACKED. DURING A SCHEDULED INSP FOUND A CRACK IN THE FUSELAGE FRAME DOUBLER AT BS 177.35 AND STRINGER 13L 1.2 INCHES FROM OTBD EDGE RADIATING INBD, CRACK IS IN THE FLAN
- [SDR GLBA2013092000321](https://openairdocs.org/sdr/GLBA2013092000321), Sep 20, 2013: FRAME. CRACKED. DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT BS 177.35 AND STRINGER 13L AT THE FRAME FLANGE BEND RADIUS 1.2 INCHES FROM THE OTBD EDGE R
- [SDR GLBA2013092000320](https://openairdocs.org/sdr/GLBA2013092000320), Sep 20, 2013: BULKHEAD. CHAFED. DURING A SCHEDULED INSPECTION, FOUND A CHAFE IN THE LT WING TO FUSELAGE BULKHEAD AT STRINGER 12L BETWEEN BS 258.25 - 273.25, AREA OF BULKHEAD THAT MEETS AT BELL
- [SDR GLBA2013091900318](https://openairdocs.org/sdr/GLBA2013091900318), Sep 18, 2013: DOOR FRAME. CRACKED. DURING A SCHEDULED INSPECTION, MX FOUND THE CARGO DOOR FWD FRAME AT FS 456 CRACKED AT THE UPPER INBD GAS STRUT MOUNT ATTACHING NUT PLATE. THE CRACKS RADIATE UPW
- [SDR GLBA2013091900319](https://openairdocs.org/sdr/GLBA2013091900319), Sep 18, 2013: FRAME. CRACKED. DURING A SCHEDULED INSPECTION, MX FOUND THE RT SIDEWALL AT FS 164.415 & STRINGER 9AR, FRAME CUTOUT FOR STRINGER CRACKED .25". REPAIRED IAW EO 13-1900-53-063. MA
- [SDR GLBA2013091900316](https://openairdocs.org/sdr/GLBA2013091900316), Sep 18, 2013: SPAR CAP. CRACKED. DURING A SCHEDULED INSPECTION, MX FOUND THE LT FWD SPAR CAP ON THE VERTICAL STABILIZER CRACKED AT THE SECOND HOLE. THE CRACK IS APPROXIMATELY .1250 INCHES IN LE
- [SDR GLBA2013091900315](https://openairdocs.org/sdr/GLBA2013091900315), Sep 18, 2013: SPAR CAP. CRACKED. DURING A SCHEDULED INSPECTION, MX FOUND THE RT FWD SPAR CAP ON THE VERTICAL STABILIZER CRACKED AT THE THIRD HOLE. THE CRACK IS APPROXIMATELY .1250" IN LENGTH. R
- [SDR GLBA2013091900314](https://openairdocs.org/sdr/GLBA2013091900314), Sep 18, 2013: SPAR. CRACKED. DURING A SCHEDULED INSPECTION, MX FOUND THE AFT MIDDLE SPAR WEB ON THE HORIZONTAL STABILIZER CRACKED. REPAIRED IAW EO 13-1900-55-022. MAJOR REPAIR.
- [SDR GLBA2013091900313](https://openairdocs.org/sdr/GLBA2013091900313), Sep 18, 2013: RIB. CRACKED. DURING A SCHEDULED INSPECTION, MX NOTED THAT THE RT WING INBD RIB FLANGE AND DOUBLER WERE CRACKED. REPAIRED IAW EO 13-1900-57-016. MAJOR REPAIR.
- [SDR GLBA2013091900317](https://openairdocs.org/sdr/GLBA2013091900317), Sep 18, 2013: DOOR FRAME. CRACKED. DURING A SCHEDULED INSPECTION, MX FOUND THAT THE AIRSTAIR DOOR LOWER AFT FRAME CORNER AREA AT APPROXIMATELY FS 172.35 WAS CRACKED, 1.2" IN THE OTBD UPPER BEND R
- [SDR GLBA2013091600311](https://openairdocs.org/sdr/GLBA2013091600311), Sep 14, 2013: KEELBEAM. BENT. LT INBD KEEL WEB ASSY APPEARS BENT, FWD UPPER EDGE OF WEB ASSY APPEARS TO BE DEFLECTED OTBD APPROXIMATELY .125". LOCATION BL 91.75. REPAIRED IAW EO 13-1900-54-0
- [SDR GLBA2013091100308](https://openairdocs.org/sdr/GLBA2013091100308), Sep 10, 2013: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN AND FASTENER DAMAGED AT FS 468.25 BETWEEN STRINGERS 13 - 14L. REPAIRED IAW EO 13-1900-53-058.
- [SDR GLBA2013090300303](https://openairdocs.org/sdr/GLBA2013090300303), Sep 2, 2013: ACTUATOR. FAILED. PILOT REPORTED THAT WHEN SELECTING THE GEAR DOWN, HAD NO LT MAIN INDICATION AND GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED, LANDING GEAR RELAY CIRCUIT BREAKER W
- [SDR GLBA201300145](https://openairdocs.org/sdr/GLBA201300145), Jan 5, 2013: WIRE. BROKEN. PILOT REPORTED THAT WHEN THE LANDING GEAR HANDLE WAS SELECTED TO THE UP POSITION, THE RT MAIN DID NOT FULLY RETRACT, LANDING CIRCUIT BREAKER TRIPPED AND HAD TO 
- [SDR GLBA201209071](https://openairdocs.org/sdr/GLBA201209071), Sep 6, 2012: LANDING GEAR. MALFUNCTIONED. LANDING GEAR FAILED TO EXTEND NORMALY. LANDING GEAR LIGHTS DID NOT ILLUMINATE. MX INSPECTED ALL SYS WIRING AND REPLACED THE LANDING CONTROL HANDLE, PERFORMED SE
- [SDR GLBA201209031](https://openairdocs.org/sdr/GLBA201209031), Sep 3, 2012: BULB. INOPERATIVE. EMERGENCY INSTRUMENT LIGHT ON F/O'S SIDE INOPERATIVE. MX REPLACED THE BULB, OPS CK GOOD.
- [SDR GLBA2012071900016](https://openairdocs.org/sdr/GLBA2012071900016), Jul 19, 2012: PRESSURE BLKHD. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE LT LWR FWD PRESSURE BULKHEAD AT THE INBD EDGE DOUBLER ROW OF FASTENERS, 1.1" IN LENGTH. REPAIRED IA
- [SDR GLBA201112053](https://openairdocs.org/sdr/GLBA201112053), Dec 3, 2011: DOWNLOCK SWITCH. FAILED. PILOT REPORTED THAT THE LANDING GEAR INTRANSIT LIGHT ILLUMINATED IN FLIGHT WITH TORQUE AT 3000LB AND AIRSPEED 210KNOTS SLOWED TO 170 AND PUT GEAR DOWN NORMAL AP
- [SDR GLBA20111024F](https://openairdocs.org/sdr/GLBA20111024F), Oct 21, 2011: ANNUNCIATOR. INOPERATIVE. PILOT REPORTED THAT THE LT AND RT LANDING GEAR INDICATION IS INTERMITTENT. MX REPLACED THE ANNUNCIATOR ASSY PN: 90-42291-2, GEAR SWING OPS CKS GOOD, NO DEFECTS 
- [SDR GLBA20110726G](https://openairdocs.org/sdr/GLBA20110726G), Jul 25, 2011: FUSE. OPEN. PILOT REPORTED THAT THE AIR STAIR DOOR WAS INOP. MX REPLACED THE FUSE IN THE BATTERY BOX PNMDL5, IAW BMM 33-20-00, OPS CHECKED GOOD.
- [SDR GLBA20110726F](https://openairdocs.org/sdr/GLBA20110726F), Jul 25, 2011: CONNECTOR. CORRODED. PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR WAS INOPERATIVE. MX FOUND CORROSION ON THE WIRE PINS, REPLACED A401 P1, P2, P3, & P4, SP11 12,13,114,15, & 16 IAW
- [SDR GLBA201104153](https://openairdocs.org/sdr/GLBA201104153), Apr 14, 2011: BULB. INOPERATIVE. PILOT REPORTED THAT DURING THERE POST FLIGHT INSP THEY FOUND BOTH INSTRUMENT EMERGENCY LIGHTS ON THE CAPTAIN'S SIDE ARE OUT. MAINTENANCE INSPECTED THE SYSTEM AN
- [SDR GLBA20110223A](https://openairdocs.org/sdr/GLBA20110223A), Feb 23, 2011: INDICATOR. READS LOW. RIGHT ENGINE TORQUE GAUGE WENT DOWN ON CLIMB OUT. ALL OTHER ENGINE INDICATIONS WERE NORMAL,NOTICED ON TAXI IN TORQUE GAUGE WAS BELOW ZERO. MAINTENANCE PERFORMED
- [SDR GLBA20110203F](https://openairdocs.org/sdr/GLBA20110203F), Feb 3, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE FRAME AT FS 280.73 AT STRINGER 5R CUTOUT, .2" IN LENGTH. MAINTENANC PERFORMED ANOTHER I
- [SDR GLBA20110204H](https://openairdocs.org/sdr/GLBA20110204H), Feb 3, 2011: SKIN. DEBONDED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND THE AIRSTAIR DOOR LOWER INNER SKIN DEBONDED, AREA 16" X 6" FROM LOWER EDGE INWARD TO STOP HINGE. MAINT
- [SDR GLBA20110204F](https://openairdocs.org/sdr/GLBA20110204F), Feb 3, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND 2 CRACKS AT THE FRAME FS 456.0 RADIATING FROM STRINGER 9AR CUTOUT, UPPER CRACK .6" IN LENGTH, LOWER CR
- [SDR GLBA20110204G](https://openairdocs.org/sdr/GLBA20110204G), Feb 3, 2011: STRINGER. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE STRINGER 9AR AT FS 451.0, .4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PER
- [SDR GLBA201006051](https://openairdocs.org/sdr/GLBA201006051), Jun 4, 2010: ACTUATOR. MALFUNCTIONED. WHEN LANDING GEAR HANDLE WAS PLACED IN DOWN POSITION WE SAW 3 GREEN, HANDLE INTRANSIT LIGHTS, LG RELAY CB POPPED AND J HOOK CAME DOWN INT LOCKED POSITION OR LES
- [SDR GLBA20091223A](https://openairdocs.org/sdr/GLBA20091223A), Dec 23, 2009: HANDLE. DETERIORATED. LANDING GEAR WOULD NOT COME DOWN PERFORMED CHECKLIST AND HAND PUMPED THE GEAR ALL 3 GREEN ANNUNCIATORS ILLUMINATED. MX REMOVED AND REPLACED THE LANDING GEAR CON
- [SDR GLBA200912111](https://openairdocs.org/sdr/GLBA200912111), Dec 11, 2009: LANDING GEAR. INOPERATIVE. LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MX JACKED THE ACFT AND PERFORMED A GEAR RETRACTION AND EXTENSION TEST IAW MM 32-30-00. THE OPS CHECK WAS GOOD ON T
- [SDR GLBA20091130G](https://openairdocs.org/sdr/GLBA20091130G), Nov 29, 2009: AUTOFEATHER SYS. MALFUNCTIONED. SUSPECTED AUTOFEATHER - PILOTS REPORTED THE RT PROP AUTOFEATHERED IN FLIGHT WHILE REDUCING TORQUE FROM 2500 LBS TO 500 LBS. TOR4QUE LEVELS WERE EVEN THROUGHOUT 
- [SDR GLBA20090805G](https://openairdocs.org/sdr/GLBA20090805G), Aug 2, 2009: UPLOCK SWITCH. OUT OF ADJUST. PILOTS REPORTED THAT THE MLG DID NOT RETRACT AFTER TAKEOFF AND IN TRANSIT LIGHTS DID NOT COME ON AND 3 GREEN STILL ANNUNCIATED. PILOTS CYCLED MLG HANDLE WITH TH
- [SDR GLBA200908041](https://openairdocs.org/sdr/GLBA200908041), Aug 2, 2009: LANDING GEAR. MALFUNCTIONED. AFTER TAKE OFF LANDING GEAR WOULD NOT RETRACT
- [SDR GLBA2009072302](https://openairdocs.org/sdr/GLBA2009072302), Jul 21, 2009: LANDING GEAR. MALFUNCTIONED. LANDING GEAR WOULD NOT RETRACT AFTER T/O.
- [SDR GLBA200907231](https://openairdocs.org/sdr/GLBA200907231), Jul 21, 2009: LANDING GEAR. MALFUNCTIONED. AIR RETURN PILOTS REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE JACKED AIRCRAFT ON RAMP AND PERFORMED 6 GEAR RETRACTION AND EXTENS
- [SDR GLBA20061102](https://openairdocs.org/sdr/GLBA20061102), May 12, 2008: FRAME. CRACKED. FRAME AT FS 177.35 CRACKED AT STRINER 9R RELIEF CUTOUT.** MAINT REPAIRED CRACK AT STRINGER RELIEFHOLE AT STRINGER 9R AND FS 177.35 IAW SRM 51-70. REPAIR APPROXI
- [SDR GLBA20061101](https://openairdocs.org/sdr/GLBA20061101), May 12, 2008: DOOR FRAME. CRACKED. AIRSTAIR DOOR FRAME ANGLE CRACKED AT LOWER SNUBBER MOUNT NUTPLATES. MAINT INSTALLED INSERT AND REPAIR PIECE CUT FROM NEW ANGLE IAW. SRM 53-90-28 AND MFG NEW COV
- [SDR GLBA20061000](https://openairdocs.org/sdr/GLBA20061000), Sep 17, 2007: SKIN. CRACKED. BELLY SKIN CRACKED AT WING SPAR FS 290.5 AT BL 29.06 CRACK LENGTH APPROXIMATELY 1.250 INCHES. MAINTENANCE REPAIRED SKIN CRACK AT LT WING SPAR AREA FS 290 AND BL
- [SDR GLBA20060837](https://openairdocs.org/sdr/GLBA20060837), Oct 11, 2006: SPAR. CRACKED. RIGHT WING AT BL 114.25 AND F.S. 330 FOUND A .094 CRACK ON AFT SPAR, REPAIR PENDING.
- [SDR 20030850](https://openairdocs.org/sdr/20030850), May 23, 2005: POWERPACK. MALFUNCTIONED. UPON APPROACH WHEN LANDING GEAR SELECTED DOWN, GEAR WOULD NOT EXTEND. FLIGHT CREW USED THE MANUAL GEAR DOWN HAND PUMP TO EXTEND GEAR SUCCESSFULLY AND LANDED. MA
- [SDR GLBA20030723](https://openairdocs.org/sdr/GLBA20030723), Sep 20, 2004: LINE. LEAKING. LANDING GEAR WILL NOT EXTEND, MANUALLY EXTENDED, FOUND BAD HYD LINE. REMOVED AND REPLACED, OPS CK GOOD.
- [SDR GLBA20030724](https://openairdocs.org/sdr/GLBA20030724), Sep 20, 2004: LINE. INOPERATIVE. LANDING GEAR WILL NOT EXTEND. MANUALLY EXTENDED, REMOVED AND REPLACED HYDRAULIC LINE, PN 101-388016-7.
- [SDR GLBA20030547](https://openairdocs.org/sdr/GLBA20030547), Jan 31, 2004: CONTROL CABLE. INOPERATIVE. EMERGENCY LANDING FOR LOSS OF ELEV TRIM CONTROL, R & R FWD ELEV TRIM TAB CABLE PN 114-524037-25.
- [SDR GLBA2003102](https://openairdocs.org/sdr/GLBA2003102), Jul 7, 2003: RELAY. FAILED. LANDING GEAR HAD TO BE MANUALLY EXTENDED. REPLACED K3 RELAY, OPS CHECK GOOD.

All 68: https://openairdocs.org/aircraft/N169GL/reports.md

## Service difficulty reports on N169GL not matched to an aircraft (1)

They name N169GL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR GLBA20091008G](https://openairdocs.org/sdr/GLBA20091008G), Oct 5, 2009: ANGLE. CRACKED. MAJOR REPAIR - DURING ROUTINE SHEDULED MAINTENANCE, A CRACK WAS FOUND ON THE LT HEAVY ANGLE AT FS 288. CRACK IS LOCATED AT THE BEND RADIUS APPROXIMATELY 1.6 IN 

## 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/N169GL/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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