# N23YV: 1992 Beech 1900D, registration cancelled 2006-05-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 2, 2006
- Exported to: South Africa
- Status when cancelled: Valid registration
- Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162)
- Engine: [U/A Canada PT6A series](https://openairdocs.org/engine/u-a-canada-pt6a-series) (registry code 61508)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs)
- Serial number: UE-23
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: September 25, 1992
- Certificate issued: July 29, 2004
- Last registry action: July 29, 2004
- Mode S code: A20861
- Owner when cancelled: [Dunnerstock Development Inc](https://openairdocs.org/faa-owner/DUNNERSTOCK%20DEVELOPMENT%20INC)
- Location: [Springdale, AR](https://openairdocs.org/faa-place/AR/Springdale)
- Owner type: Corporation
- Owner's area on the map: 36.3265° N, 93.9979° W: Placed by OpenAirDocs at the center of ZIP code 72756, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N23YV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=23YV
- Page: https://openairdocs.org/deregistered/N23YV-2006-05-02

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 (15)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 58279](https://openairdocs.org/sdr/58279), Jan 26, 2004: BLEED VALVE. MALFUNCTIONED. ON APPROACH FOR LANDING NR 2 ENGINE BEGAN COMPRESSOR STALL CAUSING ERRATIC TORQUE READINGS AND FLAMES TO BE EMITTED FROM EXHAUST STACKS. CREW DECLARED EMERGENCY
- [SDR AMWA70](https://openairdocs.org/sdr/AMWA70), Nov 5, 2003: RIB. CRACKED. WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 69.184 WAS FOUND CRACKED AT FWD CENTER STRINGER INTERSECTION. REPAIRED CR
- [SDR AMWA69](https://openairdocs.org/sdr/AMWA69), Nov 5, 2003: RIB. CRACKED. WHILE PERFORMING AND INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 54.026 WAS FOUND CRACKED IN TWO PLACES ON THE RIGHT SIDE NEAR THE FWD, C
- [SDR AMWA117](https://openairdocs.org/sdr/AMWA117), Oct 30, 2003: STRINGER CLIP. CRACKED. WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, STRINGER 13R WAS FOUND TO HAVE A CRACKED CLIP.
- [SDR AMWA116](https://openairdocs.org/sdr/AMWA116), Oct 30, 2003: RIVET. CHAFED. WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE LEFT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFED.
- [SDR AMWA115](https://openairdocs.org/sdr/AMWA115), Oct 30, 2003: PLATE. CHAFED. WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE RIGHT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFE.
- [SDR AMWA114](https://openairdocs.org/sdr/AMWA114), Oct 30, 2003: STRINGER. CRACKED. WHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, SKIN UNDER STRINGER 10R WAS FOUND CRACKED.
- [SDR AMWA82](https://openairdocs.org/sdr/AMWA82), Oct 15, 2003: RIB. CRACKED. WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED ON THE LEFT SIDE NEAR THE FWD STRINGER INTERSECT
- [SDR AMWA61](https://openairdocs.org/sdr/AMWA61), Oct 15, 2003: RIB. CRACKED. WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED IN TWO PLACES ON THE RIGHT SIDE BY THE FOWARD AN
- [SDR MASA98157](https://openairdocs.org/sdr/MASA98157), Aug 21, 1998: EMERGENCY DOOR. MIS-ALIGNED. FLT 5320 - FLL-TPA - DURIG PRE-FLIGHT WALK AROUND, CREW NOTICED THAT THE RIGHT REAR EMERGENCY EXIT EXTERIOR HANDLE WAS NOT FLUSH WITH THE DOOR. MAINTENANCE REMO
- [SDR MASA98105](https://openairdocs.org/sdr/MASA98105), May 17, 1998: STOP. OUT OF ADJUST. DURING ROUTINE INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR NOT FLUSH WITH EXTERIOR SURFACE. MAINTENANCE RERIGGED DOOR STOPS. PRESSURE CHECKED, OPS CHECK GOOD. 
- [SDR MASA97046](https://openairdocs.org/sdr/MASA97046), Jul 13, 1997: WIRE. BROKEN. AIRSHUTTLE 5308 - GNV-MIA - ON LANDING, THE NR 1 COMM WENT BLAND AND EMITTED SMOKE. THE RADIO WAS SWITCHED TO OFF AND THE SMOKE STOPPED. MAINTENANCE FOUND A SHO
- [SDR 97ZZZX3265](https://openairdocs.org/sdr/97ZZZX3265), Jul 11, 1997: ATTACH BRACKET. EXCESS WEAR. FLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 13
- [SDR 97ZZZX3264](https://openairdocs.org/sdr/97ZZZX3264), Jul 11, 1997: ATTACH BRACKET. EXCESS WEAR. FLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 13
- [SDR 95ZZZX6315](https://openairdocs.org/sdr/95ZZZX6315), Oct 3, 1995: SUN GEAR. FAILED. POWER SECTION FAILURE WAS CAUSED BY THE SUN GEAR FAILURE. THE SUN GEAR, CARRIER, CARRIER GEARS, PT SHAFT, AND THE RING GEAR WERE SENT TO PW & C FOR INVESTIGATIO

## 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 19970703025239I](https://openairdocs.org/incident/19970703025239I), Jul 3, 1997: Beech 1900D (N23YV), Pensacola, FL, Minor damage. Landed last third runway. Pilot took over. Heavy braking. Blew tire. Ran off. Hit lights. Taxied to ramp.

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