N23YV

Cancelled 2006

Deregistered aircraft · 1992 Beech 1900D · U/A Canada PT6A series

Cancelled
May 2, 2006
Exported to
South Africa
Status when cancelled
Valid registration
Serial number
UE-23
Year built
1992
Type
Fixed wing multi engine
Engine
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
Owner type
Corporation

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.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N23YV and the event date: up to this one’s cancellation.

Service difficulty reports · 15

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

SDR 58279Bleed Valve · malfunctionedON APPROACH FOR LANDING NR 2 ENGINE BEGAN COMPRESSOR STALL CAUSING ERRATIC TORQUE READINGS AND FLAMES TO BE EMITTED FROM EXHAUST STACKS. CREW DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. REMOVED AND REPLACED NR 2 ENG BLEED VALVE, OPSJan 26, 2004 · N23YV · Beech 1900D · Compressor Bleed ValveSDR AMWA70Rib · crackedWHILE 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 CRACKS TO RIB FLANGE IN ACCORDANCE BMM P/N 114-590021-9, 51-70-03.Nov 5, 2003 · N23YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA69Rib · crackedWHILE 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, CENTER STRINGERS AND TWO PLACES ON THE LEFT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/Nov 5, 2003 · N23YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA117Stringer Clip · crackedWHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, STRINGER 13R WAS FOUND TO HAVE A CRACKED CLIP.Oct 30, 2003 · N23YV · Beech 1900D · Fuselage Main, Longeron/StringerSDR AMWA116Rivet · chafedWHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE LEFT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFED.Oct 30, 2003 · N23YV · Beech 1900D · FastenersSDR AMWA115Plate · chafedWHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, THE RIGHT WING ROOT PRESSURE PLATE WAS FOUND TO HAVE A RIVET HEAD CHAFE.Oct 30, 2003 · N23YV · Beech 1900D · Wing, Plate/SkinSDR AMWA114Stringer · crackedWHILE PERFORMING A SCHEDULED ABC STRUCTURAL INSPECTION, SKIN UNDER STRINGER 10R WAS FOUND CRACKED.Oct 30, 2003 · N23YV · Beech 1900D · Fuselage Main, Longeron/StringerSDR AMWA82Rib · crackedWHILE 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 INTERSECTION. REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03.Oct 15, 2003 · N23YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA61Rib · crackedWHILE 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 AND AFT STRINGER INTERSECTION. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE WITH BMM P/N 114-590021-9, 51Oct 15, 2003 · N23YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR MASA98157Emergency Door · mis-alignedFLT 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 REMOVED AND REINSTALLED THE DOOR. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 21, 1998 · N23YV · Beech 1900D · Emergency ExitsSDR MASA98105Stop · out of adjustDURING ROUTINE INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR NOT FLUSH WITH EXTERIOR SURFACE. MAINTENANCE RERIGGED DOOR STOPS. PRESSURE CHECKED, OPS CHECK GOOD. (M)May 17, 1998 · N23YV · Beech 1900D · Emergency ExitsSDR MASA97046Wire · brokenAIRSHUTTLE 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 SHORTED WIRE BETWEEN THE AUDIO SELECT PANEL AND THE NR 1 COMM. REMOVED AND REPLACED THE NR 1 COMM COJul 13, 1997 · N23YV · Beech 1900D · VHF Communications SystemSDR 97ZZZX3265Attach Bracket · excess wearFLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. Jul 11, 1997 · N23YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX3264Attach Bracket · excess wearFLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. Jul 11, 1997 · N23YV · Beech 1900D · Trailing Edge FlapsSDR 95ZZZX6315Sun Gear · failedPOWER 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 INVESTIGATION.Oct 3, 1995 · N23YV · Beech 1900D · Turbine Section