# N210GL: 1996 Beech 1900D, registration cancelled 2026-06-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 29, 2026 - Exported to: Australia - Status when cancelled: Valid registration - Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162) - 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) (OpenAirDocs) - Serial number: UE-210 - Year built: 1996 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: April 10, 1996 - Certificate issued: June 12, 2026 - Last registry action: June 12, 2026 - Mode S code: A1BA23 - Owner when cancelled: [Tvpx Ars Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20ARS%20INC%20TRUSTEE) - Location: [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake) - Owner type: Corporation - Owner's area on the map: 40.8386° N, 111.9179° W: Placed by OpenAirDocs at the center of ZIP code 84054, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N210GL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=210GL - Page: https://openairdocs.org/deregistered/N210GL-2026-06-29 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 (62, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TIMA20250215002](https://openairdocs.org/sdr/TIMA20250215002), Feb 15, 2025: UNKNOWN. ODOR. WHILE IN CRUISE FLIGHT AT 10,000FT PILOT BEGAN TO SMELL SOMETHING SUSPICIOUS. MOMENTS LATER THE PILOT EXPERIENCED A LEFT AC BUS FAILURE AND BEGAN TO SEE SMOKE C - [SDR GLBA2015042700515](https://openairdocs.org/sdr/GLBA2015042700515), Apr 25, 2015: CHECK VALVE. LEAKING. SIG EVENT, PILOT REPORTED THAT THERE WAS A STRONG SMELL OF FUEL IN CABIN. REMOVED FLOORBOARDS & INSPECTED FUEL TRANSFER LINES, PRESSURIZED & LEAK CHECKED FUEL L - [SDR GLBA2014022800389](https://openairdocs.org/sdr/GLBA2014022800389), Feb 26, 2014: MOTOR. FAULTY. PILOT REPORTED THAT THERE WAS A STRONG BURNING SMELL COMING FROM THE CABIN & IS IRRITATING TO TO EYES. TROUBLESHOT BURNING SMELL COMING FROM FLAP GEAR BOX MOTOR - [SDR GLBA2014021300383](https://openairdocs.org/sdr/GLBA2014021300383), Feb 12, 2014: MOTOR. FAULTY. PILOT REPORTED THAT WHEN THEY WENT TO EXTEND THE FLAPS HAD A STRONG ELECTRICAL SMELL & THE FLAPS DID NOT EXTEND. MAINTENANCE R&R FLAP GEAR BOX MOTOR P/N 100-524 - [SDR GLBA2013091300310](https://openairdocs.org/sdr/GLBA2013091300310), Sep 12, 2013: SKIN. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THE LT LOWER BELLY SKIN AT FS 288 CRACKED, 1.75" IN LENGTH. REPAIRED IAW EO 13-1900-53-059. MAJOR REPAIR. - [SDR GLBA2013090900306](https://openairdocs.org/sdr/GLBA2013090900306), Sep 6, 2013: FIRE LOOP. CHAFED. SIG EVENT - PILOT REPORTED THAT THE RT FIREWALL FUEL VALVE T-HANDLE FLICKERED ON AND OFF IN FLIGHT. MX TESTED FIRE LOOP ON RT SIDE, TESTED NORMAL. INSPECTED FWD - [SDR GLBA2013052900255](https://openairdocs.org/sdr/GLBA2013052900255), May 29, 2013: PRESSURE BLKHD. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND 4 CRACKS IN THE FWD PRESSURE BULKHEAD, RT WEB AT FS 84.00, CRACKS AT THE INBD EDGE OF WEB ATTACHING FASTENERS, 2" I - [SDR GLBA2013052900254](https://openairdocs.org/sdr/GLBA2013052900254), May 29, 2013: PRESSURE BLKHD. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND 7 CRACKS IN THE FWD PRESSURE BULKHEAD, LT WEB AT FS 84.00, CRACKS AT INBD EDGE OF WEB ATTACHING FASTENERS, 3.5" IN - [SDR GLBA2013052800253](https://openairdocs.org/sdr/GLBA2013052800253), May 28, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE FRAME AT FS 177.35 IN THE BEND RADIUS, 1" LENGTH. REPAIRED IAW EO 13-1900-53-043. MAJOR REP - [SDR GLBA2013052800252](https://openairdocs.org/sdr/GLBA2013052800252), May 28, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 CRACKS AT THE CARGO DOOR FUSELAGE FRAME AT FS 509 BETWEEN STRINGER 4L & 5L, LOCATED IN THE BEND RADIUS OF THE FRA - [SDR GLBA2013040100222](https://openairdocs.org/sdr/GLBA2013040100222), Apr 1, 2013: STRUCTURE. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE TEE SECTION OF THE LT HORIZONTAL STAB LOWER AT HSS 5.000 AND 10.5 PERCENT AT A SCREW HOLE, .5" IN LE - [SDR GLBA2013032900219](https://openairdocs.org/sdr/GLBA2013032900219), Mar 28, 2013: SKIN. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK EXTENDING FROM A SCREW HOLE ON THE TOP SIDE OF THE LT HORIZONTAL STAB AT HSS 5.000 AND 10.5 PERCENT CHORD, O - [SDR GLBA2013032900218](https://openairdocs.org/sdr/GLBA2013032900218), Mar 28, 2013: STRUCTURE. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE RT HORIZONTAL STAB LOWER TEE SECTION AT HSS 5.000 AND 10.5 PERCENT CHORD, 1.5" IN LENGTH. REPAIRED IA - [SDR GLBA2012120400126](https://openairdocs.org/sdr/GLBA2012120400126), Dec 4, 2012: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE, RADIATES FROM THE UPPER FWD TASTENER UPWARD TO EDGE OF SPAR CAP, .375" IN LENG - [SDR GLBA2012083100043](https://openairdocs.org/sdr/GLBA2012083100043), Aug 31, 2012: SKIN. BURNED. .5 X .5 INCH BURN HOLE IN TOP AND BOTTOM SKIN, 3.8750" CENTER FROM OTBD TIP OF LT ELEVATOR T/E. REPAIRED THE AFFECTED AREA IAW EO 12-1900-27-002. - [SDR GLBA2012040203](https://openairdocs.org/sdr/GLBA2012040203), Apr 2, 2012: SKIN. DAMAGED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND THE RT FUSELAGE FS 288 HAS ELONGATED HOLES FROM ATTACHING FAIRING PANEL TO FS 327. REPAIRED THE AFFECTED AREA AND P - [SDR GLBA2012040202](https://openairdocs.org/sdr/GLBA2012040202), Apr 2, 2012: FAIRING. DAMAGED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE FUSELAGE FARING, RT SIDE UNDER AFT WING, AFT OF FS 363.250, 2.25 INCHES JUST ABOVE STRINGER 1R, .687 - [SDR GLBA2012032101](https://openairdocs.org/sdr/GLBA2012032101), Mar 20, 2012: SPAR. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS AT A MACHINED HOLE AT 2, 8, 10, & 4 O'CLOCK POSITIONS AT THE HORIZONTAL STAB AFT SPAR WE - [SDR GLBA201203191205](https://openairdocs.org/sdr/GLBA201203191205), Mar 19, 2012: SKIN. CHAFED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND 2 RIVET HEADS CHAFING ON A PREVIOUS REPAIR OF THE LOWER RT WING WHERE THE FUSELAGE MEETS THE WING. REPAIRED IAW EO - [SDR GLBA2012031904](https://openairdocs.org/sdr/GLBA2012031904), Mar 19, 2012: ATTACH FITTING. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK AT THE NUTPLATE, FWD CARGO DOOR SNUBBER FUSELAGE ATTACH POINT, UPPER IB NUTPLATE FS 456, .35" IN LENGTH. RE - [SDR GLBA2012031903](https://openairdocs.org/sdr/GLBA2012031903), Mar 19, 2012: SKIN. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FUSELAGE SKIN, LT BELLY AT FS 303.25 WHERE THE FUSELAGE MEETS THE WING, 5" IN LENGTH. REPAIRED IAW E - [SDR GLBA2012031902](https://openairdocs.org/sdr/GLBA2012031902), Mar 19, 2012: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 150.6 BETWEEN STRINGERS 2R AND 3R, .9" IN LENGTH. REPAIRED IAW EO 12-1900-53-016. MAJOR - [SDR GLBA2012031901](https://openairdocs.org/sdr/GLBA2012031901), Mar 19, 2012: DOUBLER. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT DOUBLER, FWD END, FS 288, 1.2" IN LENGTH. REPAIRED IAW EO 12-1900-53-017. - [SDR GLBA2012022101](https://openairdocs.org/sdr/GLBA2012022101), Feb 18, 2012: WARNING LIGHT. FALSE ACTIVATION. PILOT REPORTED THAT THE GEAR INTRANSIT LIGHT ILLUMINATED IN FLIGHT, RAN CHECKLIST, GEAR OPERATED NORMALLY TO THE EXTENDED POSITION, EMERGENCY DECLARED, LANDED S - [SDR GLBA20120209F](https://openairdocs.org/sdr/GLBA20120209F), Feb 8, 2012: CIRCUIT BOARD. DAMAGED. PILOT REPORTED THAT THE LANDING GEAR DID NOT EXTEND WHEN SELECTED AND RELAY CIRCUIT BREAKER TRIPPED, MANUALLY EXTENDED GEAR, NO IN-TRANSIT LIGHTS, LANDED SAFELY - [SDR GLBA20111208F](https://openairdocs.org/sdr/GLBA20111208F), Dec 7, 2011: ACTUATOR. INOPERATIVE. PILOT REPORTED THAT THE LEFT GEAR INDICATION DID NOT SHOW DOWN AND LOCKED UNTIL APPROX 25 SECONDS AFTER THE HANGLE WAS PLACED IN THE DOWN POSITION. MX REPLACED - [SDR GLBA20111128F](https://openairdocs.org/sdr/GLBA20111128F), Nov 27, 2011: SOLENOID. DIRTY. PILOT REPORTED THAT THE ACFT YAWED TO THE LT IN THE LANDING FLARE. MX CLEANED THE LOW PITCH SOLENOID, OPS CHECKED GOOD. - [SDR GLBA20110809F](https://openairdocs.org/sdr/GLBA20110809F), Aug 8, 2011: WIRE. CHAFED. PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR REMAINS EXTINGUISHED WHEN THE DOOR IS OPENED UP UNTIL ABOUT A FOOT OPEN. MX INSPECTED WIRE AT AIRSTAIR DOOR FOUND - [SDR GLBA20110803G](https://openairdocs.org/sdr/GLBA20110803G), Aug 2, 2011: SWITCH. INOPERATIVE. PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR GOES OUT WITHOUT LOCKING THE DOOR. MX CLEANED THE MICRO SWITCHES, OPS CK GOOD. - [SDR GLBA20110802G](https://openairdocs.org/sdr/GLBA20110802G), Aug 1, 2011: SWITCH. INOPERATIVE. PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR WENT OUT BEFORE THE DOOR WAS LOCKED. MX CLEANED THE CABIN DOOR MICRO SWITCH REF AIM 14.3.0, OK FOR SERVICE. - [SDR GLBA20110801H](https://openairdocs.org/sdr/GLBA20110801H), Jul 29, 2011: ACTUATOR. INOPERATIVE. PILOT REPORTED THAT THE LT MLG BOTH GREEN "L" AND "H" ANNUNCIATORS FLICKERED THEN EXTINGUISHED THEN REILLUMINATED, NO UNSAFE INDICATIONS ON APPROACH & LANDING. - [SDR GLBA20110706P](https://openairdocs.org/sdr/GLBA20110706P), Jul 4, 2011: SWITCH. OUT OF RIG. PILOT REPORTED THAT UPON RAISING THE LANDING GEAR WHILE FLAPS AT 17 DEGREES. TAKEOFF GEAR WARNING HORN SOUNDED AND COULD NOT BE SILENCED. IN TRANSIT LIGHT REMAI - [SDR GLBA20110606G](https://openairdocs.org/sdr/GLBA20110606G), Jun 4, 2011: SWITCH. STUCK. PILOT REPORTED THAT WITH THE CABIN DOOR OPEN THE CABIN ANNC DID NOT ILLUMINATE. MX CLEANED THE MICRO SWITCH, SYS OPS CK GOOD. - [SDR GLBA20110603F](https://openairdocs.org/sdr/GLBA20110603F), Jun 1, 2011: KEELBEAM. GOUGED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A GOUGE IN THE RT OTBD KEEL BY A CLAMP ON THE RETRACT/EXTEND LINE FOR THE LT MLG ACTUATOR. MX REP - [SDR GLBA20110602F](https://openairdocs.org/sdr/GLBA20110602F), Jun 1, 2011: KEELBEAM. GOUGED. MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A GOUGE IN THE LT OTBD KEEL BY A CLAMP ON THE RETRACT/EXTEND LINE FOR THE LT MLG ACTUATOR. MX REP - [SDR GLBA20101206A](https://openairdocs.org/sdr/GLBA20101206A), Dec 6, 2010: BLEED AIR SYS. INOPERATIVE. CLIMBING THROUGH 20,000 FT COULDN'T GET CABIN TO QUIT CLIMBING, HAD TO DEPLOY MASKS & RETURN TO DEPARTURE, DIR STUCK AT 3.4 PSI WOULD NOT GO HIGHER. STOWED & RE - [SDR GLBA20100819F](https://openairdocs.org/sdr/GLBA20100819F), Aug 18, 2010: FASTENER. LOOSE. SIG EVENT - PILOT REPORTED THAT AN OVERWHELMING ODOR OF FUEL ENTER THE CABIN AND COCKPIT. MAINTENANCE FOUND LOOSE FASTENERS JUST OUTBOARD OF RT NACELLE AT FORWA - [SDR GLBA20100818B](https://openairdocs.org/sdr/GLBA20100818B), Aug 18, 2010: FUEL SYS. LEAKING. OVERWHELMING ODORS OF JET FUEL PRESENT IN CABIN COCKPIT EXTREMELY BAD TO A POINT OF BEING NAUSEATING AND AFFECTING SAFETY SLOW DRIP UNDER RT NACELLE DIFFERENT A - [SDR GLBA20100802J](https://openairdocs.org/sdr/GLBA20100802J), Aug 2, 2010: BULKHEAD. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION A CRACK WAS FOUND AT THE AFT CARGO BAY FLOORBOARD FORWARD SUPPORT BULKHEAD AT F.S. 531.0 LH SIDE WHERE IT ATTACHES TO THE - [SDR GLBA20100802K](https://openairdocs.org/sdr/GLBA20100802K), Aug 2, 2010: BULKHEAD. BUCKLED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A BULKHEAD AT FS 531 AFT CARGO FLOORBOARD FORWARD SUPPORT BUCKLED ABOUT 11/32" AT TOP, TOTAL DAMAGE AREA A - [SDR GLBA20100730F](https://openairdocs.org/sdr/GLBA20100730F), Jul 30, 2010: SKIN. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION A CRACK IN THE SKIN WAS FOUND ON THE EMERGENCY EXIT DOOR 6A, LOWER FORWARD CORNER, 2" IN LENGTH. MAINTENAN - [SDR GLBA20100728F](https://openairdocs.org/sdr/GLBA20100728F), Jul 27, 2010: FRAME. CRACKED. DURING A SCHEDULED ROUNTINE INSP A CRACK WAS FOUND IN THE FRAME ANGLE AT FS 303, .5" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRE - [SDR GLBA20100729G](https://openairdocs.org/sdr/GLBA20100729G), Jul 27, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, A2 CRACKS WAS FOUND IN THE FRAME AT FS 456 AND STRINGER 10R CUTOUT, .45" AND .5" IN LENGTH. MAINTENANCE REPAIRE - [SDR GLBA20100409F](https://openairdocs.org/sdr/GLBA20100409F), Apr 9, 2010: SKIN. PUNCTURED. COMPONENT MAJOR REPAIR - UPON RECEIVING A SERVICEABLE AIRSTAIR DOOR THAT WAS PURCHASED, IT WAS DETERMINED THAT IT REQUIRED A MAJOR REPAIR ON THE EXTERIOR DOOR S - [SDR GLBA20090807F](https://openairdocs.org/sdr/GLBA20090807F), Aug 6, 2009: UNKNOWN. ODOR. PILOTS REPORTED THAT A STRONG FUEL ODOR FROM THE VENTS IN THE FLIGHT DECK AND CABIN WAS PRESENT. MAINTENANCE INSPECTED THE NR 1 AND 2 ENGINES FOR LEAKS OF WHICH - [SDR GLBA20090504F](https://openairdocs.org/sdr/GLBA20090504F), Apr 28, 2009: STRUCTURE. CORRODED. MAJOR REPAIR - AIRSTAIR DOOR WAS FOUND CORRODED ON LOWER END CLOSURE AREA. MAINTENANCE REMOVED A SECTION OF THE LOWER INNER DOOR PAN, CLEANED CORROSIONFROM INNE - [SDR GLBA200904225](https://openairdocs.org/sdr/GLBA200904225), Apr 22, 2009: PRESSURE SWITCH. WORN. ON APPROACH AT 500 LBS TORQUE, WHILE LEVELING ALTITUDE AND ADVANCING POWER THE R/H ENGINE ATTEMPTED FEATHER CAUSING CYCLES SIMILAR TO AUTOFEATHER TEST. MAINTENA - [SDR GLBA20090205A](https://openairdocs.org/sdr/GLBA20090205A), Feb 5, 2009: CIRCUIT BOARD. SHORTED. SUSPECTED AUTO FEATHER - PILOTS REPORTED THAT ON SHORT FINAL THE RT ENGINE CYCLED IN AND OUT OF FEATHER. MX R&R THE A123 PRINTED CIRCUIT BOARD AND OPS CHECKED T - [SDR GLBA200901093](https://openairdocs.org/sdr/GLBA200901093), Jan 7, 2009: SWITCH. DIRTY. SIGNIFICANT EVENT - PILOTS REPORTED THAT THE RT ENG AUTOFEATHERED IN FLIGHT AND CAUSED SURGES AND EXTREME YAWING MOTION. MX CLEANED AFX SWITCHES IAW BMM 61-21-0 - [SDR GLBA20061041](https://openairdocs.org/sdr/GLBA20061041), Jan 1, 2008: BULB. BURNED OUT. SMOKE/ODOR - PILOTS REPORTED THE GLARESHIELD INSTRUMENT EMERGENCY LIGHTS WERE SMOKING ON THE GROUND AFTER STARTING ENGINES. REMOVED EMERGENCY FUSE F127. MAINTEN All 62: https://openairdocs.org/deregistered/N210GL-2026-06-29/reports.md ## NTSB investigations (2) 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 ENG12IA014](https://openairdocs.org/ntsb/ENG12IA014), Feb 17, 2012: Beech 1900D (N210GL), Denver International Airport, CO, incident, minor damage. Probable cause: A failure of the nose landing gear end cap due to fatigue. Contributing to the failure were the ineffective inspection and the unknown effect of grain direction on fatigue life. - [NTSB DEN04IA059](https://openairdocs.org/ntsb/DEN04IA059), Apr 9, 2004: Beech 1900D (N210GL), Denver, CO, incident, no damage. Probable cause: arcing of the windshield deicing system. Factors contributing to the incident were the improper inspection of the windshield's exterior seal, deterioration of the windshield seal, and water… ## Other aircraft with N210GL - [Cancelled (date not recorded)](https://openairdocs.org/deregistered/N210GL-undated): Cessna 172A, S/N 46919. Triennial form not returned --- 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.