# N203LG: 1981 Beech B200, registration cancelled 2016-12-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 28, 2016 - Status when cancelled: Valid registration - Airframe: [Beech B200](https://openairdocs.org/model/beech-b200) (registry code 1152922) - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs) - Serial number: BB-926 - Year built: 1981 - Type of aircraft: Fixed wing multi engine - Certificate issued: November 21, 2002 - Last registry action: June 4, 2015 - Mode S code: A19E29 - Owner when cancelled: [Cww Inc](https://openairdocs.org/faa-owner/CWW%20INC) - Location: [Englewood, CO](https://openairdocs.org/faa-place/CO/Englewood) - Owner type: Corporation - Owner's area on the map: 39.5732° N, 104.8649° W: Placed by OpenAirDocs at the center of ZIP code 80112, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N203LG - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=203LG - Page: https://openairdocs.org/deregistered/N203LG-2016-12-28 From the FAA registry file of October 28, 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 B200: https://openairdocs.org/model/beech-b200.md ## Service difficulty reports (12) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CIEA201303260003](https://openairdocs.org/sdr/CIEA201303260003), Mar 22, 2013: ACCESS DOOR. INOPERATIVE. ON DESCENT FROM FL250, THE CABIN PRESSURE SPIKED TO 12500, THE CABIN LIGHTS ILLUMINATED AND THE NO SMOKING/SEATBELT SIGNS ILLUMINATED. THE POWER LEVERS WERE AT - [SDR CIEA201303260002](https://openairdocs.org/sdr/CIEA201303260002), Mar 22, 2013: WARNING SWITCH. INACCURATE. ON DESCENT FROM FL250, THE CABIN PRESSURE SPIKED TO 12500, THE CABIN LIGHTS ILLUMINATED AND THE NO SMOKING/SEATBELT SIGNS ILLUMINATED. THE POWER LEVERS WERE AT - [SDR CIEA201303260001](https://openairdocs.org/sdr/CIEA201303260001), Mar 22, 2013: CONTROLLER. ERRATIC. ON DESCENT FROM FL250, CABIN PRESSURE SPIKED TO 12500, CABIN LIGHTS ILLUMINATED AND NO SMOKING/SEATBELT SIGNS ILLUMINATED. POWER LEVERS WERE AT IDLE DUE TO TURB - [SDR CIEA200900008](https://openairdocs.org/sdr/CIEA200900008), Jun 23, 2009: BRACKET. CRACKED. DURING THE 10000 CYCLE STRUCTURAL INSP, FOUND THE FWD DOOR SUPPORT CABLE EXTRUSION INSIDE THE DOOR IS CRACKED IN TWO PLACES. GAINED ACCESS TO THE FWD HANDRAIL B - [SDR CIEA200900006](https://openairdocs.org/sdr/CIEA200900006), Feb 25, 2009: STRINGER. CRACKED. DURING COMPLIANCE WITH MFG MANDATORY SB 53-2472, REVISION 4, DATED JULY 2003 AND AD 2005-01-18, AMENDMENT 39-13943, EFFECTIVE DATE MARCH 01, 2005 THE LT STRINGE - [SDR CIEA200500013](https://openairdocs.org/sdr/CIEA200500013), Aug 3, 2005: DOWNLOCK SWITCH. FAILED. DURING APPROACH, RT MAIN GEAR DID NOT INDICATE IT WAS DOWN AND LOCKED. DUE TO SERV AT DESTINATION AIRPORT, A/C RETURNED TO ORIG AIRPORT. PILOT CYCLED GEAR SEVER - [SDR CIEA200500008](https://openairdocs.org/sdr/CIEA200500008), Jul 1, 2005: HINGE. CRACKED. AFT LANDING ATTEMPTED TO CLOSE MAIN CABIN ENTRY DOOR & HAD DIFFICULTY. A 5 INCH CRACK NEAR AFT, BOTTOM END OF DOOR, WHERE HINGE IS ATTACHED. DAMAGED - ENTRY DOO - [SDR CIEA200500007](https://openairdocs.org/sdr/CIEA200500007), Jun 28, 2005: OXYGEN MASK. MISMANUFACTURED. DURING THE CLIMB THE CABIN LOST PRESSURIZATION. (NOTE: SEE SEPARATE SDR ON THE PRESSURIZATION ISSUE). AS A RESULT OF THE PRESSURIZATION LOSS THE OXYGEN MASKS DR - [SDR CIEA200500006](https://openairdocs.org/sdr/CIEA200500006), Jun 28, 2005: DOOR SEAL. INOPERATIVE. DURING CLIMB, PAX HEARD WIND NOISE FROM AFT CABIN. BROUGHT TO ATTENTION OF PILOT, NOTICED CABIN PRESSURIZATION WAS DROPPING, RESULTING IN CABIN ALTITUDE CLIMBIN - [SDR CIEA200500005](https://openairdocs.org/sdr/CIEA200500005), Jun 21, 2005: STRUT. CORRODED. DURING SCHEDULED LG INSP, NLG UPPER STRUT HSG WAS FOUND TO BE CORRODED. CORROSION WAS IN 2 AREAS OF STRUT, NEAR TOP CROSS BRACE. CORROSION IN EXCESS OF 70 PERCE - [SDR 0026](https://openairdocs.org/sdr/0026), Mar 12, 2004: WINDSHIELD. CRACKED. DURING CRUISE THE COPILOTS WINDSHIELD INNER PANE SHATTERED. NO DEBRIS FELL INTO THE CABIN OTHER THAN DUST. THE OUTER PANE STAYED IN TACT. THE PILOT DESENDED TO - [SDR 0021](https://openairdocs.org/sdr/0021), Aug 28, 2003: SPROCKET. DEFECTIVE. DURING COMPLIANCE, THE AILERON SPROCKET WAS FOUND TO HAVE A POSSIBLE DEFECT. DOING A VISUAL INSPECTION BETWEEN THE TWO GEARS OF THE AILERON SPROCKET, ON THE LAR ## 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 20041104031589I](https://openairdocs.org/incident/20041104031589I), Nov 4, 2004: Beech B200 (N203LG), Rapid City, SD, Minor damage. (-23) After landing N203LG taxied onto the non-movement area in front of dale aviation. Pilot made a left turn and struck a de-ice stand with the right wing… --- 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.