# N220GL: 1996 Beech 1900D

- Status: Valid registration
- Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162, 19 seats)
- Engine: [Pratt & Whitney Canada PT6A-6 series](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-6-series) (registry code 52150)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (Textron Aviation Inc.) (OpenAirDocs)
- Serial number: UE-220
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: June 11, 1996
- Certificate issued: March 25, 2023
- Expires: March 31, 2030
- Mode S code: A1E1A2
- 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=220GL
- Page: https://openairdocs.org/aircraft/N220GL

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 Canada PT6A-6 model are included.

## ADs that may apply (OpenAirDocs): 66 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 Canada PT6A-6 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 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 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 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 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 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 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 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

All 74: https://openairdocs.org/aircraft/N220GL/ads.md

## Information bulletins (advisory) (9 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-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 N220GL.

## 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 20111106025559I](https://openairdocs.org/incident/20111106025559I), Nov 6, 2011: Beech 1900D (N220GL), Denver, CO, No damage. On final approach into north platte NE, landing gear would not extend. Landing gear relay circuit breaker had "popped" (open). Crew requested proper clearance…

## Service difficulty reports (70, 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 GLBA2014081400428](https://openairdocs.org/sdr/GLBA2014081400428), Aug 13, 2014: SKIN. DAMAGED. DURING A SCHEDULED INSPECTION FOUND A .05 INCH HOLE IN THE BELLY SKIN NEAR THE ADF ANTENNA AT APPROX FS 219. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED
- [SDR GLBA2014062300417](https://openairdocs.org/sdr/GLBA2014062300417), Jun 21, 2014: CONNECTOR. UNSECURE. SIG EVENT PILOT REPORTED THAT AN UNSCHEDULED AUTO FEATHER ACTIVATION ON THE RT ENG, ON APPROACH SEVERAL TIMES UNTIL THE SYS WAS TURNED OFF. SECURED THE RT LP AF
- [SDR GLBA2014010800364](https://openairdocs.org/sdr/GLBA2014010800364), Jan 8, 2014: DOOR FRAME. CRACKED. DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE LOWER AIRSTAIR DOOR FRAME AT BS 172.0, 1.4 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-001.
- [SDR GLBA2013042600243](https://openairdocs.org/sdr/GLBA2013042600243), Apr 25, 2013: CONNECTOR. DAMAGED. PILOT REPORTED THAT THERE WAS A STRANGE ODOR IN THE COCKPIT. MX REPAIRED SEVERAL WIRES AT A CONNECTOR & CHANGED SEVERAL PCBS.
- [SDR GLBA2013040800227](https://openairdocs.org/sdr/GLBA2013040800227), Apr 8, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE FRAME FLANGE AT FS 177.35 AND STRINGER 13L, 1.5" IN LENGTH. REPAIRED IAW EO 13-1900-53-031. MAJOR REP
- [SDR GLBA2013040800226](https://openairdocs.org/sdr/GLBA2013040800226), Apr 8, 2013: LONGERON. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE COCKPIT RT SIDEWALL LONGERON AT FS 107, AT JUNCTION WITH SIDEWALL FRAME, .75" IN LENGTH. REPAIRED IAW
- [SDR GLBA2013040800225](https://openairdocs.org/sdr/GLBA2013040800225), Apr 8, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE COCKPIT RT SIDE WALL FRAME AT FS 107 AT THE UPPER 2 FASTENER HOLES, RADIATES FROM EACH HOLE UPWARD, 1
- [SDR GLBA2013040800224](https://openairdocs.org/sdr/GLBA2013040800224), Apr 8, 2013: SKIN. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FUSELAGE SKIN AT THE UPPER FWD AREA OF A/S DOOR CUTOUT, RADIATES FROM FASTENER UPWARD & DOWNWARD A
- [SDR GLBA2013040800223](https://openairdocs.org/sdr/GLBA2013040800223), Apr 8, 2013: SKIN. CRACKED. DURING A SCHEDULED ROUTINE INSP FOUND 2 CRACKS IN THE UPPER FUSELAGE SKIN AT FS 150 AND STRINGER 1 ON THE LT & RT SIDE OF STRINGER 1, .7" IN LENGTH. REPAIRED IA
- [SDR GLBA2013040100220](https://openairdocs.org/sdr/GLBA2013040100220), Mar 28, 2013: CIRCUIT BREAKER. TRIPPED. PILOT REPORTED THAT UPON EXTENDING THE GEAR THE LANDING GEAR CIRCUIT BREAKER TRIPPED, RAN MANUAL GEAR EXTENTION CHECKLIST, GEAR EXTENDED NORMALLY, A HIGH PITCH 
- [SDR GLBA2013022800188](https://openairdocs.org/sdr/GLBA2013022800188), Feb 19, 2013: PLENUM. DEBONDED. LT OTBD PLENUM PANEL DEBONDED APPROX 5" FROM THE TOP OF PANEL TO APPROX 15" DOWN, THE FULL WIDTH OF THE HONEYCOMB. REPAIRED IAW WITH A FIELD REPAIR.
- [SDR GLBA2012111400107](https://openairdocs.org/sdr/GLBA2012111400107), Nov 14, 2012: SCREW. LOOSE. PILOT REPORTED THAT ON SHORTLY AFTER LEVELING OFF FROM DECENT NR 1 ENG BEGAN TO TQ SURGE PAST AT 4500 FT LBS REDUCED PWR PROP BEGAN TO SURGE RAN MEM ITEMS BROUG
- [SDR GLBA2012090500046](https://openairdocs.org/sdr/GLBA2012090500046), Sep 5, 2012: WEB. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS IN THE HORIZONTAL STAB FWD WEB AT HSS 00.00 PROTRUDING FROM GROMMET HOLE, ONE INCH IN LENGTH. REPAIRED 
- [SDR GLBA2012090400044](https://openairdocs.org/sdr/GLBA2012090400044), Sep 2, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT 20 PERCENT CHORD AND APPROX VSS 84.10 PROTRUDING FROM THE 2ND
- [SDR GLBA2012090400045](https://openairdocs.org/sdr/GLBA2012090400045), Aug 31, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT 20 PERCENT CHORD AND APPROX VSS 84.10, EXTENDING FROM TOP OF AN
- [SDR GLBA2012070500011](https://openairdocs.org/sdr/GLBA2012070500011), Jul 5, 2012: RIB. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RIB ON LT INBD WING, INBD RT AT BL 29.06 AND FS 288.00, 2" IN LENGTH. REPAIRED THE AFFECTED AREA IAW
- [SDR GLBA2012070500009](https://openairdocs.org/sdr/GLBA2012070500009), Jul 5, 2012: SPAR. CHAFED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE SPAR CHAFED AT LT INBD WING LWR FWD AREA, .02380 DEEP. REPAIRED THE AFFECTED AREA IAW EO 12-1900-57-007.
- [SDR GLBA2012030500011](https://openairdocs.org/sdr/GLBA2012030500011), Mar 5, 2012: SPAR. CRACKED. "SUP" - MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND A CRACK AT IN THE CENTER WEB OF THE REAR SPAR OF HORZ STAB, CRACK RADIATES FROM THE UPPER RT OF THE
- [SDR GLBA2012030501](https://openairdocs.org/sdr/GLBA2012030501), Mar 5, 2012: SKIN. DENTED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A DENT IN THE LT WING L/E AT WS 236 MEASURING 4.2" LONG AND 1.5" DEEP.
- [SDR GLBA20120116F](https://openairdocs.org/sdr/GLBA20120116F), Jan 13, 2012: PLACARD. MISSING. PILOT REPORTED THAT THE EMERGENCY EVACUATION PLACARD AT 7A IS MISSING. MX REPLACED PLACARD AT SEAT 7A IAW AIM 5.2.2.
- [SDR GLBA20111219G](https://openairdocs.org/sdr/GLBA20111219G), Dec 18, 2011: PCB. INOPERATIVE. PILOT REPORTED THAT THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF, LANDING GEAR RELAY CB TRIPPED. MX REPLACED THE PCB A316, IAW MI 24-01, OPS CHECKED GOOD IA
- [SDR GLBA20111212J](https://openairdocs.org/sdr/GLBA20111212J), Dec 10, 2011: CIRCUIT BOARD. MALFUNCTIONED. PILOT REPORTED THAT THE RT ENGINE WILL NOT AUTOFEATHER DURING TEST. MX RESEATED THE A123 PCB, OPS CHECKED GOOD.
- [SDR GLBA20111212H](https://openairdocs.org/sdr/GLBA20111212H), Dec 9, 2011: CONNECTOR. DIRTY. PILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR ILLUMINATED. MX CLEANED P277 CONNECTOR AT A123 PCB REF AIM 14.2.0, SYS OPS CHECKED GOOD.
- [SDR GLBA20111130F](https://openairdocs.org/sdr/GLBA20111130F), Nov 29, 2011: SKIN. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE LT BELLY SKIN AT FS 300, 2.2" FROM BELLY SKIN LT OTBD EDGE, 1.1" IN LENGTH. MX REPAIR
- [SDR GLBA20111130G](https://openairdocs.org/sdr/GLBA20111130G), Nov 29, 2011: SKIN. DEBONDED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE AS DOOR INNER SKIN DEBONDED FROM FWD EDGE TO AFT EDGE INWARD FROM LWR EDGE 1.2", DEBONDED 3" AT 
- [SDR GLBA20111109J](https://openairdocs.org/sdr/GLBA20111109J), Nov 8, 2011: WIRE. DAMAGED. PILOT REPORTED THAT UPON GEAR RETRACTION THE INTRANSIT LIGHT STAYED ILLUMINATED AND THE LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED, MANUALLY EXTENDED GEAR WITH 
- [SDR GLBA20111109G](https://openairdocs.org/sdr/GLBA20111109G), Nov 8, 2011: PCB. INOPERATIVE. "SUP" - PILOT REPORTED THAT THE AFX DISABLE WILL NOT ILLUMINATE DURING AUTOFEATHER TEST. MX REPLACED PCB 129-364091-9 SN: 559895, REF MM 61-21-00, OPS CK GOOD.
- [SDR GLBA20111108F](https://openairdocs.org/sdr/GLBA20111108F), Nov 7, 2011: LANDING GEAR. MALFUNCTIONED. PILOT REPORTED THAT ON GEAR RETRACTION THE INTRANSIT LIGHT STAYED ILLUMINATED AND LDG GEAR RELAY CB TRIPPED, MANUALLY EXTENDED GEAR WITH ALL NORMAL INDICATIONS.
- [SDR GLBA20111106A](https://openairdocs.org/sdr/GLBA20111106A), Nov 6, 2011: PCB. INOPERATIVE. UPON SELECTING LANDING GEAR HANDLE DOWN, CB LANDING GEAR RELAY POPPED IMMEDIATELY. GEAR PUMP NOT HEARD. MANUAL GEAR EXTENSION SUCCESSFUL. MX WAS ABLE TO DUPLICA
- [SDR GLBA20110914F](https://openairdocs.org/sdr/GLBA20110914F), Sep 13, 2011: SOCKET. DIRTY. PILOT REPORTED THAT THE CABIN DOOR INSP LIGHT IS INOPERATIVE. MX CLEANED THE SOCKET AND RESECURED THE BULB, OPS CHECKED GOOD.
- [SDR GLBA20110815G](https://openairdocs.org/sdr/GLBA20110815G), Aug 13, 2011: FUSE. INOPERATIVE. PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHTS SWITCH DOES NOT ILLUMINATE ANY INSTRUMENT INDIRECT LIGHTS. MX REPLACED A HOT BUSS FUSE IN THE BATTERY BOX, P
- [SDR GLBA20110815F](https://openairdocs.org/sdr/GLBA20110815F), Aug 12, 2011: SWITCH. MALFUNCTIONED. PILOT REPORTED THE THE INSTRUMENT EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN THE BUTTON IS PRESSED. MX INSPECTED AND FOUND THAT THE SYS OPERATED NORMAL, OPS CHECKE
- [SDR GLBA20110725H](https://openairdocs.org/sdr/GLBA20110725H), Jul 22, 2011: SOLENOID VALVE. INOPERATIVE. PILOT REPORTED THAT THE LANDING GEAR DID NOT COME DOWN WHEN SELECTED, LANDING GEAR RELAY CB POPPED, J-HOOK DID ENGAGE. MX REPLACED THE LANDING GEAR HANDLE AND R
- [SDR GLBA20110722G](https://openairdocs.org/sdr/GLBA20110722G), Jul 21, 2011: HANDLE. INOPERATIVE. PILOT REPORTED THAT THE LANDING GEAR DID NOT COME DOWN WHEN THE HANDLE WAS PLACED IN THE DOWN POSITION, LANDING GEAR RELAY CIRCUIT BREAKER POPPED. MAINTENANCE R
- [SDR GLBA20110718K](https://openairdocs.org/sdr/GLBA20110718K), Jul 17, 2011: WIRE. DAMAGED. PILOT REPORTED THAT THE CABIN DOOR LOCK OBSERVATION LIGHT WAS INOP. MEL 88657. MAINTENANCE REPAIRED THE WIRE SPLICE D4436 AT THE DOOR ENTRY, IAW 33-20-07, OPS C
- [SDR GLBA20110718F](https://openairdocs.org/sdr/GLBA20110718F), Jul 15, 2011: CONNECTOR. LOOSE. PILOT REPORTED THAT WHEN THE GEAR WAS SLECTED DOWN, GEAR UNSAFE LIGHTS ILLUMINATED, & HOOK ENGAGED, LT CIRCUIT BREAKER POPPED, RAN CK, MANUALLY EXTENDED GEAR, U
- [SDR GLBA20110711M](https://openairdocs.org/sdr/GLBA20110711M), Jul 9, 2011: SWITCH. FAILED. SIG EVENT - PILOT REPORTED THAT THE AIRSTAIR DOOR INSP LIGHT IS NOT ILLUMINATING. MEL 88288. MAINTENANCE REPLACED THE AIRSTAIR DOOR LOCK OBSERVATION LIGHT SWITC
- [SDR GLBA20100611L](https://openairdocs.org/sdr/GLBA20100611L), Jun 11, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN THE FRAME ANGLE AT FS 150 AT THE ATTACH POINT FOR THE LOWER PAX DOOR STRUT MOUNTS UPPE
- [SDR GLBA20100611K](https://openairdocs.org/sdr/GLBA20100611K), Jun 11, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 164 AT CUTOUT FOR STRINGER 9AR, .15" IN LENGTH. MAINTENANCE REPAIRED T
- [SDR GLBA20100611H](https://openairdocs.org/sdr/GLBA20100611H), Jun 11, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN THE FRAME AT FS 456 AT STRINGER 10R CUTOUT, .4" IN LENGTH. MAINTENANCE REPAIRED THE AF
- [SDR GLBA20100611J](https://openairdocs.org/sdr/GLBA20100611J), Jun 11, 2010: STRINGER. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND IN STRINGER 10R AT RIVET 1.2" FORWARD OF FRAME AT FS 451, CRACK PASS THROUGH RIVET HOLE .
- [SDR GLBA20091026G](https://openairdocs.org/sdr/GLBA20091026G), Oct 20, 2009: ENGINE. SMOKE. PILOTS REPORTED THAT AFTER ENGINE START UP A RAMP AGENT NOTICED SMOKE COMING FROM THE OIL HEATER EXIT ON THE NR 1 ENGINE AND THERE WAS A SMOKE ODOR IN THE CABIN
- [SDR GLBA20090606B](https://openairdocs.org/sdr/GLBA20090606B), Jun 6, 2009: BLOWER. SMOKE. PILOTS REPORTED THAT ENVIRONMENTAL SMOKE AND FUMES WERE PRESENT IN THE COCKPIT. THE BLOWERS SEEMED TO MAKE THE SITUATION WORSE. PILOTS DECLARED AN EMERGENCY. TH
- [SDR GLBA20090326A](https://openairdocs.org/sdr/GLBA20090326A), Mar 26, 2009: CIRCUIT BOARD. MALFUNCTIONED. PILOTS REPORTED A LEFT HAND FIRE LOOP ANNUNCIATOR REPEATEDLY TRIPPED IN FLIGHT. ALSO STARTED TRIPPING LEFT HAND T-HANDLE AND MASTER WARNING ANNUNCIATOR (FLASHES
- [SDR GLBA20061109](https://openairdocs.org/sdr/GLBA20061109), Jun 2, 2008: SKIN. DAMAGED. MAJOR REPAIR - DURING ROUTINE MX INSPECTION A REPORT OF A FUEL LEAK WAS REPORTED ON THE LEFT LEADING EDGE NEAR THE FUEL BARRIER BOX AT WS 194.8 WING SKIN. ALSO 
- [SDR GLBA20060988](https://openairdocs.org/sdr/GLBA20060988), Aug 22, 2007: SPAR. CRACKED. MAJOR REPAIR - UPON ROUTINE INSPECTION THE HORIZONTAL STABILIZER SPAR WEB WAS FOUND TO HAVE TWO CRACKS RADIATING FROM DEICE TUBE HOLE APPROXIMATELY 1/4 INCH & 1
- [SDR GLBA20060981](https://openairdocs.org/sdr/GLBA20060981), Aug 20, 2007: ANGLE. CRACKED. MAJOR REPAIR - LT HEAVY ANGLE CRACKED AT F.S. 288. APPROXIMATELY 2 INCHES IN LENGTH. MAINTENANCE REPAIRED THE LT HEAVY ANGLE AT F.S. 288.0 I.A.W. BEECH 1900D SR
- [SDR GLBA2006980](https://openairdocs.org/sdr/GLBA2006980), Aug 20, 2007: ANGLE. CRACKED. MAJOR REPAIR - RT HEAVY ANGLE CRACKED AT F.S. 288. MAINTENANCE REPAIRED R/H HEAVY ANGLE AT F.S. 288. IAW BEECH 1900 SRM 53-90. REPAIR LENGTH APPROX 13 1/2 INCHE
- [SDR GLBA20060979](https://openairdocs.org/sdr/GLBA20060979), Aug 20, 2007: FRAME. CRACKED. MAJOR REPAIR - FUSELAGE FRAME CRACKED AT F.S. 177.35 RT STRINGER 9 AT RELIEF HOLE. MAINTENANCE STOP DRILLED AND PATCHED AFFECTED AREAS I.A.W. BEECH SRM 51-70. P
- [SDR GLBA20060914](https://openairdocs.org/sdr/GLBA20060914), Feb 19, 2007: SHIMMY DAMPENER. MISSING. UPON PRE-FLIGHT INSPECTION, PILOT REPORT OF SHIMMY DAMPENER DAMAGE/MISSING AND SUSPECTED DAMAGE TO STRUCTURE IN SURROUNDING AREA WAS ALSO REPORTED. MAINTENANCE 

All 70: https://openairdocs.org/aircraft/N220GL/reports.md

## STCs that may be installed (OpenAirDocs) (203, 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 203: https://openairdocs.org/aircraft/N220GL/stcs.md

## Related

- Other Beech 1900D aircraft: https://openairdocs.org/model/beech-1900d/aircraft.md
- The Pratt & Whitney Canada PT6A-6 series engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-6-series.md

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