# N208GL: 1996 Beech 1900D, registration cancelled 2026-08-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 18, 2026 - Exported to: Australia - Status when cancelled: Valid registration - Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162) - 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) (OpenAirDocs) - Serial number: UE-208 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: March 18, 1996 - Certificate issued: March 25, 2023 - Last registry action: March 25, 2023 - Mode S code: A1B05C - Owner when cancelled: [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 was based - The mark today: https://openairdocs.org/aircraft/N208GL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=208GL - Page: https://openairdocs.org/deregistered/N208GL-2026-08-18 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Beech 1900D: https://openairdocs.org/model/beech-1900d.md ## Service difficulty reports (74, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR GLBA2017110600690](https://openairdocs.org/sdr/GLBA2017110600690), Nov 3, 2017: CABLE. FRAYED. MAINTENANCE REPORTED THAT THE LOWER FORWARD AIRSTAIR DOOR HAND RAIL CABLE WAS FRAYED. REMOVED AND REPLACED THE HAND RAIL CABLE IAW MM 52-10-02. - [SDR GLBA2017070600672](https://openairdocs.org/sdr/GLBA2017070600672), Jul 3, 2017: SEAL. DETERIORATED. MAINTENANCE REPORTED THAT THE AIRSTAIR DOOR INNER HANDLE SEAL DETERIORATED. INSTALLED NEW INNER DOOR HANDLE SEAL IAW SRM 51-30-05. - [SDR GLBA2017052200659](https://openairdocs.org/sdr/GLBA2017052200659), May 18, 2017: CAM. OUT OF RIG. MAINTENANCE FOUND THE PAX DOOR CAMS OUT OF ADJUSTMENT. RIGGED THE PAX DOOR CAMS IAW BMM 52-10-00-C, OPS & RIG CHECKED GOOD. - [SDR GLBA2017052200658](https://openairdocs.org/sdr/GLBA2017052200658), May 18, 2017: STRUT. LOW PRESSURE. MAINTENANCE REPORTED THAT THE AIRSTAIR DOOR STRUT REQUIRED SERVICING. SERVICED THE DOOR STRUT ASSY IAW AMM 12-10-00-11A. - [SDR GLBA2017051900656](https://openairdocs.org/sdr/GLBA2017051900656), May 17, 2017: HANDLE. UNSECURE. MAINTENANCE REPORTED THAT THE AIRSTAIR DOOR HANDLE FELL OFF. REINSTALLED AIRSTAIR DOOR HANDLE AND RE-RIGGED THE AIRSTAIR DOOR. - [SDR GLBA2017030200637](https://openairdocs.org/sdr/GLBA2017030200637), Feb 28, 2017: CABLE. DAMAGED. DURING SCHEDULED MAINTENANCE,THE UPPER AFT HANDRAIL CABLE ON THE PASSENGER DOOR WAS DAMAGED. REMOVED AND REPLACED THE PASSENGER DOOR UPPER AFT CABLE IAW BMM 52- - [SDR GLBA2016112900618](https://openairdocs.org/sdr/GLBA2016112900618), Nov 26, 2016: RUDDER PEDAL. STIFF. PILOT REPORTED THAT DURING TAXI THE RUDDER PEDELS ARE EXTREMELY STIFF MAKING IT HARD TO TAXI. MANTENANCE RERACKED THE YAW DAMP COMPUTER, TAXI CHECKS NORMAL. - [SDR GLBA2016010600563](https://openairdocs.org/sdr/GLBA2016010600563), Dec 19, 2015: DOUBLER. CRACKED. MAJOR REPAIR, DURING A SCHEDULED INSPECTION, MX FOUND THE RT SIDE WALL AT FS 163.97 & STRINGER 9 AR, REPAIR DOUBLER CRACKED. REPAIRED THE AFFECTED AREA & PERFOR - [SDR GLBA2014011300366](https://openairdocs.org/sdr/GLBA2014011300366), Jan 12, 2014: DOWNLOCK SWITCH. FAULTY. PILOT REPORTED THAT EN ROUTE TO DVL GOT A GPWS C/O & FLICKERING IN TRANSIT LIGHTS WITH 3 GREEN DOWN LOCK INDICATED. FOLLOWED CHECKLIST, HAD NO CHANGE, WAS REROU - [SDR GLBA2013082200299](https://openairdocs.org/sdr/GLBA2013082200299), Aug 22, 2013: DOOR. FAILED. MX REPORTED THAT THE 4C EMERGENCY DOOR COULDN'T BE OPENED FROM THE INSIDE. R & R EMERGENCY EXIT IAW MM 52-20-00. - [SDR GLBA2013082200300](https://openairdocs.org/sdr/GLBA2013082200300), Aug 21, 2013: SKIN. CORRODED. DURING A SCHEDULED INSPECTION, FOUND BELLY SKIN CORROSION AT FS 213.25, STRINGER 15R. REPAIRED IAW EO 13-1900-53-057. MAJOR REPAIR. - [SDR GLBA2013031200201](https://openairdocs.org/sdr/GLBA2013031200201), Mar 10, 2013: CONTROLLER. MALFUNCTIONED. CABIN OXYGEN CONTROL PULLED DUE TO CABIN ALTITUDE EXCEEDING 10000FT AND CABIN ALTITUDE INCREASING AT 4000FT IAW MIN CREW TRIED TO RESET SYS, ADJ CABIN HEAT, RAN - [SDR GLBA2013022700187](https://openairdocs.org/sdr/GLBA2013022700187), Feb 26, 2013: SKIN. CRACKED. EMERGENCY EXIT 6A SKIN PANEL LOWER FWD CORNER CRACKED IN 2 LOCATIONS. 1 CRACK IS 1.4" IN LENGTH, THE OTHER CRACK IS 1.8" IN LENGTH. REPAIRED IAW EO 13-1900-52-0 - [SDR GLBA2013002600186](https://openairdocs.org/sdr/GLBA2013002600186), Feb 26, 2013: SKIN. CRACKED. FUSELAGE SKIN CRACKED AT FS 150.60 & STRINGER 1. CRACK ON LT SIDE OF STRINGER 1 IS .25" IN LENGTH, CRACK ON RT SIDE OF STRINGER 1 IS .65" IN LENGTH. REPAIRED IA - [SDR GLBA2013022600185](https://openairdocs.org/sdr/GLBA2013022600185), Feb 26, 2013: SKIN. CORRODED. BELLY SKIN CORROSION AT FS 228.25 BETWEEN STRINGERS 16 & 15R. CORROSION INDICATIONS RUN ON FRAME AREA BETWEEN STRINGERS 16 & 15R. REPAIRED IAW EO 13-1900-53-015 - [SDR GLBA2013022800189](https://openairdocs.org/sdr/GLBA2013022800189), Feb 25, 2013: FRAME. CRACKED. FUSELAGE FRAME DOUBLER AT FS 177.25 & STRINGER 13L CRACKED 1.2" IN LENGTH IN FLANGE BEND RADIUS TO SECOND FASTENER FROM THE OTBD EDGE OF DOUBLER. REPAIRED IAW E - [SDR GLBA2013022600184](https://openairdocs.org/sdr/GLBA2013022600184), Feb 25, 2013: FRAME. CRACKED. RIGHT SIDEWALL AT FS 107, FRAME CRACKED AT UPPER FASTENER AREA. LONGERON AT FS 107 CRACKED. REPAIRED IAW EO 13-1900-53-014. MAJOR REPAIR. - [SDR GLBA2013022600183](https://openairdocs.org/sdr/GLBA2013022600183), Feb 25, 2013: RIB. CRACKED. LEFT WING INBD RIB AT 288 & BL 29.0 CRACKED. CRACK 1" IN LENGTH FROM OTBD EDGE INWARD TO BEND RADIUS AREA. REPAIRED IAW EO 13-1900-57-006. MAJOR REPAIR. - [SDR GLBA2013022600182](https://openairdocs.org/sdr/GLBA2013022600182), Feb 25, 2013: RIB. CRACKED. RT INBD WING RIB AND DOUBLER AT AT 288 & BL 29.0 CRACKED & WORN. CRACK IS 1.0" IN LENGTH. REPAIRED IAW EO 13-1900-57-005. MAJOR REPAIR. - [SDR GLBA2012091000051](https://openairdocs.org/sdr/GLBA2012091000051), Sep 10, 2012: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT SPAR CAP ANGLE AT 20 PERCENT AT VSS 84.10, 1.25" IN LENGTH. REPAIRED AFFECTED AREA - [SDR GLBA2012091000050](https://openairdocs.org/sdr/GLBA2012091000050), Sep 10, 2012: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT AT VXX 84.10, 1.25" IN LENGTH. REPAIRED AFFECTED AREA - [SDR GLBA2012091000052](https://openairdocs.org/sdr/GLBA2012091000052), Sep 10, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSP FOUND A CRACK IN THE HORIZONTAL STAB AFT SPAR WEB AT HSS 00.00 AT THE LIGHTENING HOLE, .125" IN LENGTH. REPAIRED AFFECTED AREA I - [SDR GLBA201205291](https://openairdocs.org/sdr/GLBA201205291), May 28, 2012: BULB. INOPERATIVE. LEFT INSTRUMENT/EMERGENCY LIGHT FLICKERS. MX REPLACED THE BULB, IAW BMM 33-10-04, OPS CHECKED GOOD. - [SDR GLBA20111114L](https://openairdocs.org/sdr/GLBA20111114L), Nov 14, 2011: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 288 AND STRINGER 4R, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFOR - [SDR GLBA20111114K](https://openairdocs.org/sdr/GLBA20111114K), Nov 14, 2011: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSP, FOUND A CRACK IN THE FUSELAGE FRAME ANGLE AT FS 150 AND STRINGER 9AL AT THE AS DOOR STRUT LWR MOUNT UPPER AFT INNER NUTPLATE AR - [SDR GLBA20111005G](https://openairdocs.org/sdr/GLBA20111005G), Oct 3, 2011: SPRING. DAMAGED. PILOT REPORTED THAT THE EMERGENCY EXIT AT SEAT 4C INNER PANEL LOOSE. MX REPLACED THE RETAINER SPRING ON THE DOOR PANEL. - [SDR GLBA20110825F](https://openairdocs.org/sdr/GLBA20110825F), Aug 24, 2011: GOVERNOR. INOPERATIVE. PILOT REPORTED THAT WHEN PERFORMING THE FEATHER TEST THE CB POPS. MX REPLACED THE RT OVERSPEED GOV AND PCB A123 IAW 61-20-01 , MI 24-01, AND TC 1900-7100, OPS C - [SDR GLBA20110822F](https://openairdocs.org/sdr/GLBA20110822F), Aug 20, 2011: OXYGEN MASK. LEAKING. PILOT REPORTED THAT THE FO'S OXY MASK WAS LEAKING AFTER SWITCHING TO EMERGENCY AND BACK TO OFF. MX REPLACED THE F/O'S OXY MASK IAW BMM 35-10-01, OPS CHECKED GOO - [SDR GLBA20110819H](https://openairdocs.org/sdr/GLBA20110819H), Aug 18, 2011: PCB. UNKNOWN. PILOT REPORTED THAT DURING THE AUTOFEATHER TEST ON THE RT SIDE, THE AUTOFEATHER CB POPPED AND THE RT PROP DID NOT FEATHER. MX CLEANED AND INSPECTED THE PCB, RES - [SDR GLBA20110811G](https://openairdocs.org/sdr/GLBA20110811G), Aug 10, 2011: PCB. INOPERATIVE. MX REPORTED THAT DURING ENGINE RUNS THE AUTOFEATHER CB POPPED DURING THE AFX TEST. MX REPLACED THE AUTOFEATHER RELAY PCB IAW AIM MI 24-01, OPS CK GOOD. PN: 129- - [SDR GLBA20100604F](https://openairdocs.org/sdr/GLBA20100604F), Jun 3, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION A CRACK IN THE FRAME AT FS 456 AND STRINGER 10R, FOUND IN THE STRINGER CUTOUT, .45" IN LENGTH. MAINTENANCE - [SDR GLBA20100604G](https://openairdocs.org/sdr/GLBA20100604G), Jun 3, 2010: SKIN. MISREPAIRED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A REPAIR WAS FOUND ON THE BELLY SKIN AT F.S. 265.75 BETWEEN STRINGER 13R AND 12R, REPAIR DOES NOT CONFORM. - [SDR GLBA20100601G](https://openairdocs.org/sdr/GLBA20100601G), Jun 1, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A CRACK WAS FOUND IN THE FRAME RADIUS, RT SIDE AT FS 451.0 AT STRINGER 10R, 1.0" IN LENGTH. MAINTENANCE REPAIRE - [SDR GLBA20100601H](https://openairdocs.org/sdr/GLBA20100601H), Jun 1, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A CRACK WAS FOUND AT THE CUTOUT AT FS 177.35 AND STRINGER 5R, .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND - [SDR GLBA06012010001](https://openairdocs.org/sdr/GLBA06012010001), Jun 1, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A CRACK WAS FOUND AT THE CUTOUT AT FS 177.35 AND STRINGER 5R, .2" IN LENGTH. SUPLEMENTAL INFORMATION WILL BE SU - [SDR GLBA20100601F](https://openairdocs.org/sdr/GLBA20100601F), May 31, 2010: SKIN. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK WAS FOUND AT A RIVET ON AN ANGLE AT F.S. 451 AND STRINGER 11L, BELOW FLOOR BOARD, LEFT SIDE OF FUS - [SDR GLBA2010051203](https://openairdocs.org/sdr/GLBA2010051203), May 12, 2010: LANDING GEAR. MALFUNCTIONED. PILOTS REPORTED THAT WHEN THE GEAR WAS SELECTED TO THE DOWN POSITION, THE NOSE WHEEL ANNUNCIATOR DID NOT ILLUMINATE & THE IN TRANSIT LIGHT ILLUMINATED. PERFORME - [SDR GLBA20091002F](https://openairdocs.org/sdr/GLBA20091002F), Sep 29, 2009: UPLOCK SWITCH. OUT OF ADJUST. AIR RETURN - PILOTS REPORTED THAT A GEAR UNSAFE LIGHT WAS ILLUMINATED AFTER GEAR RETRACTION AND THEY MANUALLY EXTENDED THE GEAR. MAINTENANCE ADJUSTED THE RIGHT - [SDR GLBA20090929G](https://openairdocs.org/sdr/GLBA20090929G), Sep 28, 2009: UPLOCK SWITCH. INTERMITTENT. AIR RETURN - PILOTS REPORTED THE THE LANDING GEAR WOULD NOT RAISE AFTER TAKE OFF. RED UNSAFE LIGHTS WERE ON. PILOTS RECYCLED THE GEAR THEN IT WOULD NOT LWR. GEA - [SDR GLBA20090910A](https://openairdocs.org/sdr/GLBA20090910A), Sep 10, 2009: TURBINE WHEEL. DAMAGED. PILOTS REPORTED THAT UPON TAKEOFF WITH TORQUE ONLY AT 3200 FOOT LBS. RT ITT EXCEEDED 800 C. AND THE TAKEOFF WAS THEN ABORTED. MX PERFORMED MANY CHECKS INCLUDING - [SDR GLBA20090629F](https://openairdocs.org/sdr/GLBA20090629F), Jun 23, 2009: SHAFT. CORRODED. DURING MX IT WAS DISCOVERED THAT THE LT EXIT DOOR AT ROW 6A WOULD NOT LATCH SHUT PROPERLY. MX REMOVED AND REPLACED THE EXIT DOOR WHICH WAS REMOVED FROM ACFT IN - [SDR GLBA20090409F](https://openairdocs.org/sdr/GLBA20090409F), Apr 6, 2009: CAM. WORN. PILOTS REPORTED THAT THE ACFT YAWS VIOLENTLY TO THE LT ON FLAIR (LANDING). MX REMOVED AND REPLACED THE RT ENGINE PROPELLER CAM/LEVER IAW MM 76-10-00. GROUND RUN - [SDR GLBA20090224M](https://openairdocs.org/sdr/GLBA20090224M), Feb 23, 2009: INSULATION. OUT OF POSITION. SMOKE SMELL - ENROUTE FROM "DEN" TO "CYS" THE PILOTS REPORTED A BURNING SMELL AFTER OPENING THE BLEEDS AFTER TAKEOFF. MX FOUND A PIECE OF SIDEWALL INSULATION AG - [SDR GLBA200901091](https://openairdocs.org/sdr/GLBA200901091), Jan 8, 2009: SKIN. CRACKED. MAJOR REPAIR - DURING SCHEDULED STRUCTURAL INSPECTION THE LT BELLY SKIN WAS FOUND CRACKED APPROXIMATELY 6" IN LENGTH AT APPROXIMATELY BL 265 8.5" AFT AS WING SP - [SDR GLBA20061082](https://openairdocs.org/sdr/GLBA20061082), Mar 13, 2008: SKIN. CRACKED. CRACK ON BELLY SKIN AT FS 303.25 AT BL 29.06. CRACK APPROX 2.250 INCH. MAINT STOP DRILLED AND PATCHED AFFECTED AREA IAW SRM 51-70. DAMAGED AREA APPROX 6.3 BY 4. - [SDR GLBA20060986](https://openairdocs.org/sdr/GLBA20060986), Aug 15, 2007: SPAR. CRACKED. MAJOR REPAIR - HORIZONTAL STAB SPAR WEB CRACKED AROUND DE-ICE TUBE HOLE. MAINTENANCE REPAIRED HORZONTAL STAB SPAR WEB I.A.W. BEECH 1900D SRM 55-91. REPAIR APPRO - [SDR GLBA20060984](https://openairdocs.org/sdr/GLBA20060984), Aug 14, 2007: SKIN. CANNING. EVIDENCE OF OIL CANNING PRESENT AT FS 202.25 2 INCHES FROM CENTER OF REPAIR TO STRINGER 15 R APPROXIMATELY 2 INCHES SQUARE. MAINTENANCE REPAIRED AFFECTED AREA I - [SDR GLBA20060985](https://openairdocs.org/sdr/GLBA20060985), Aug 14, 2007: HINGE. CRACKED. MAINTENANCE DISCOVERED BOTH CARGO DOOR HINGES CRACKED. MAINTENANCE REMOVED AND REPLACED CARGO DOOR HINGES IAW EO 05-02 . DOOR HINGE PN 129-440049-1. FUSELAGE PN - [SDR GLBA20060983](https://openairdocs.org/sdr/GLBA20060983), Aug 14, 2007: STRINGER. CRACKED. (2) CRACKS FOUND ON STRINGER 10R AT F.S. 451.0. FORWARD CRACK .5625 INCH LONG AFT CRACK .2500 INCH LONG. MAINTENANCE REPAIRED CRACKS ON STRINGER 10R AT F.S. 451 - [SDR GLBA20060982](https://openairdocs.org/sdr/GLBA20060982), Aug 13, 2007: ANGLE. CRACKED. RT HEAVY ANGLE CRACKED AT RADIUS AT FS 288. CRACK IS APPROXIMATELY 2.2500 INCH LONG. MAINTENANCE REPAIRED THE RT HEAVY ANGLE IAW SRM 53-90. REPAIR APPOXIMATELY All 74: https://openairdocs.org/deregistered/N208GL-2026-08-18/reports.md ## 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 20030221004039I](https://openairdocs.org/incident/20030221004039I), Feb 21, 2003: Beech 1900D (N208GL), Denver, CO, Minor damage. (-23) This incident occurred while maintenance personnel were operating the aircraft for troubleshooting. Counseled the A&P mechanic on the importance of… - [Incident 20000716035449I](https://openairdocs.org/incident/20000716035449I), Jul 16, 2000: Beech 1900D (N208GL), Denver, CO, Minor damage. (-23)Flight departed grand juncton, CO for Denver, CO. No passengers on board. Crew reported hearing an unusual noise during gear retraction. A landing gear… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.