# N173YV: 1995 Beech 1900D, registration cancelled 2011-12-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 22, 2011 - Exported to: South Africa - 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-173 - Year built: 1995 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: September 29, 1995 - Certificate issued: December 7, 2011 - Last registry action: December 7, 2011 - Mode S code: A1268C - Owner when cancelled: [Specialized Aircraft Services Inc](https://openairdocs.org/faa-owner/SPECIALIZED%20AIRCRAFT%20SERVICES%20INC) - Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita) - Owner type: Corporation - Owner's area on the map: 37.7038° N, 97.2793° W: Placed by OpenAirDocs at the center of ZIP code 67208, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N173YV - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=173YV - Page: https://openairdocs.org/deregistered/N173YV-2011-12-22 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 1900D: https://openairdocs.org/model/beech-1900d.md ## Service difficulty reports (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR GLBA20110218G](https://openairdocs.org/sdr/GLBA20110218G), Feb 18, 2011: BULB. BURNED OUT. PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHTS ON LT SIDE WOULD NOT ILLUMINATE. MX REPLACED THE EMERGENCY LIGHT BULB PN: 1864 IAW BMM 33-10-04, OPS CK GOOD - [SDR GLBA20110121F](https://openairdocs.org/sdr/GLBA20110121F), Jan 21, 2011: STRUCTURE. DAMAGED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE LT STABILON T/E DAMAGED 1.25", 19.375" FROM FUSELAGE AND 26.75" FROM OTBD EDGE. MAINTENANCE REPAIRE - [SDR GLBA20110120G](https://openairdocs.org/sdr/GLBA20110120G), Jan 20, 2011: SKIN. DEBONDED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE AIRSTAIR DOOR LOWER INTERIOR SKIN DEBONDED 17" ALONG THE LOWER EDGE RADIATING UPWARD FROM LOWER EDG - [SDR GLBA20110120F](https://openairdocs.org/sdr/GLBA20110120F), Jan 20, 2011: ATTACH FITTING. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE LT AILERON WEIGHT CLIP CRACKED, R & R LT AILERON TC 1900-2710.00. MX REPAIRED THE AFFECTED AREA AND - [SDR GLBA20100902F](https://openairdocs.org/sdr/GLBA20100902F), Sep 2, 2010: HANDLE. LOOSE. PILOT REPORTED THAT AFTER CLOSING THE AIR STAIR DOOR THE OUTSIDE HANDLE CAME OFF. MAINTENANCE REPLACED THE CABIN DOOR HANDLE SNAP RING PN MS16624-1075, REF MM 5 - [SDR GLBA20100824G](https://openairdocs.org/sdr/GLBA20100824G), Aug 24, 2010: SKIN. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A DENT, TOP OF LEFT AILERON, 1.75" BY .75", 38.125" FROM OB EDGE AND .875" FROM TE. AND - [SDR GLBA20100729F](https://openairdocs.org/sdr/GLBA20100729F), Jul 28, 2010: FAN. FAILED. SIG EVENT - PILOT REPORTED THAT DURING FLIGHT BLOWERS AIRFLOW BECAME VERY WEAK AND A SLIGHT BURNING SMELL WAS THEN NOTICED. MX REPORTED THAT THEY REPLACED THE V - [SDR GLBA20100617F](https://openairdocs.org/sdr/GLBA20100617F), Jun 15, 2010: CONNECTOR. NOT SEATED. SIG EVENT - PILOT REPORTED THAT WHEN ATTEMPTING TO EXTEND THE LANDING GEAR, GEAR DID NOT EXTEND, IN TRANSIT GEAR HANDLE LIGHT CAME ON INTERMITTANTLY, THEN EXTIN - [SDR GLBA200911141](https://openairdocs.org/sdr/GLBA200911141), Nov 14, 2009: WIRE. CHAFED. AIR RETURN - THE PILOTS REPORTED THAT LANDING GEAR CIRCUIT BREAKER POPPED IN CRUISE AND WHICH RESULTED IN A RETURN TO "DEN". MX REPAIRED 4 CHAFED WIRES THAT WER - [SDR GLBA2009100101](https://openairdocs.org/sdr/GLBA2009100101), Oct 1, 2009: LINE. LEAKING. PILOTS REPORTED THE GEAR INSTRANSIT LIGHT DID NOT EXTINGUISH, LANDING GEAR RELAY CIRCUIT BREAKER POPPED AND GEAR HAD TO BE MANUALLY EXTENDED. UPON FURTHER INSPE - [SDR GLBA20090724G](https://openairdocs.org/sdr/GLBA20090724G), Jul 24, 2009: FRAME. CRACKED. DURING ROUTINE SCHEDULED MAINTENANCE A FRAME FLANGE AROUND TWO RIVETS WERE FOUND CRACKED AT FS 544.0 BETWEEN STRINGERS 12L AND 13L. CRACKS RADIATE APPROXIMATELY - [SDR GLBA090722001](https://openairdocs.org/sdr/GLBA090722001), Jul 22, 2009: FRAME. CRACKED. MAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A FRAME FLANGE AROUND 2 RIVETS WERE FOUND CRACKED AT FS 544.0 BETWEEN STRINGERS 12L AND 13L. CRACKS RADIATE APPROX . - [SDR GLBA20090524092](https://openairdocs.org/sdr/GLBA20090524092), May 24, 2009: SENSOR. DIRTY. PILOTS REPORTED A STALL HEAT CAUTION ANNUNCIATOR WOULD NOT TURN OFF WITH THE SWITCH IN THE ON POSITION. MAINTENANCE CLEANED CONNECTIONS ON A1 & A2 STALL WARNING - [SDR GLBA200905241](https://openairdocs.org/sdr/GLBA200905241), May 24, 2009: ANNUNCIATOR. INOPERATIVE. STALL HEAT CAUTION ANNUNCIATOR WILL NOT TURN OFF WITH THE SWITCH IN THE ON POSITION. - [SDR GLBA20090430C](https://openairdocs.org/sdr/GLBA20090430C), Apr 30, 2009: SWITCH. OUT OF ADJUST. CABIN DOOR ANNC CAME ON IN FLIGHT. DIVERTED TO NEAREST SUITABLE AIRPORT. MAINTENANCE TROUBLESHOT THE SYSTEM AND ADJUSTED THE FORWARD AND AFT LATCH SWITCHES. - [SDR GLBA200812011](https://openairdocs.org/sdr/GLBA200812011), Nov 28, 2008: AUTOFEATHER SYS. MALFUNCTIONED. SIGNIFICANT EVENT - FLIGHT 5128 EN ROUTE FROM PIR TO DEN DURING APPROACH INTO DENVER ON FINAL AT ABOUT 6000FT & 160KTS. THE NR 2 ENGINE AUTOFEATHERED 3 TIMES WI - [SDR GLBA200810171](https://openairdocs.org/sdr/GLBA200810171), Oct 16, 2008: RIVET. MISSING. MAJOR REPAIR - DURING ROUTING SCHEDULED MAINTENANCE A CONFORMITY INSPECTION WAS PERFORMED AND FOUR RIVETS WERE FOUND MISSING ON THE HORIZONTAL STABILIZER SPAR C - [SDR BSAASDR0728](https://openairdocs.org/sdr/BSAASDR0728), Dec 28, 2007: TUBE. DEFECTIVE. RIGHT BLEED FAIL ILLUMINATED IN FLIGHT. ITEM INITIALLY DEFERRED. REMOVED AND REPLACED EVA TUBING, RAN AIRCRAFT OPERATIONAL CHECK GOOD. - [SDR BSAASDR0727](https://openairdocs.org/sdr/BSAASDR0727), Dec 11, 2007: PRESSURE SWITCH. DIRTY. RIGHT BLEED AIR FAIL LIGHT ILLUMINATD. THE RIGHT BLEED AIR PRESSURE SWITCH WAS CLEANED AND EVA TUBING INSPECTED FOR LEAKS. AIRCRAFT RAN ON GROUND AT HIGH POWER - [SDR BSAASDR0707](https://openairdocs.org/sdr/BSAASDR0707), Apr 11, 2007: WIRE. CHAFED. WHEN GEAR HANDLE WAS SELECTED DOWN, THE LANDING GEAR INDICATION CD TRIPPED. CREW ABORTED LANDING AND FOLLOWED EMERGENCY PROCEDURES. CREW VERIFIED GEAR WAS DOWN - [SDR BSAASDR0620](https://openairdocs.org/sdr/BSAASDR0620), Aug 19, 2006: SPAR CAP. CORRODED. PITTING CORROSION WAS FOUND IN LT WING JUST AFT OF WING DRAIN ON THE FWD FACE OF THE MAIN SPAR CAP FROM WS125 TO 128, AND ON THE RIB JUST IB OF THE WING DRAIN. - [SDR BSAASDR0619](https://openairdocs.org/sdr/BSAASDR0619), Aug 8, 2006: LATCH. MALFUNCTIONED. DURING CRUISE, A PASSENGER REPORTED TO THE CREW THAT THE RT FWD COWLING HAD COME LOOSE. WHEN THE CREW LANDED, THEY NOTED A YAW UPON TOUCHDOWN. THE IB FWD COWL L - [SDR BSAASDR0602](https://openairdocs.org/sdr/BSAASDR0602), Feb 10, 2006: WINDSCREEN. CRACKED. THE LEFT COCKPIT WINDSHIELD INNER PANE CRACKED DURING CRUISE AS FL230, OAT WAS -40, WINDSHIELD HEAT WAS ON AT THE TIME, AIRCRAFT WAS NOT IN ICING CONDITIONS AT - [SDR BSAASDR0601](https://openairdocs.org/sdr/BSAASDR0601), Jan 28, 2006: SWITCH. MALFUNCTIONED. DURING CLIMB-OUT, CARGO DOOR OPEN ANNUNCIATOR WARNING LIGHT CAME ON AS CREW ASCENDED THROUGH 12,000 FT. CREW RETURNED TO STATION. THE CARGO DOOR OPEN LIGHT WAS - [SDR 1050617008AMW](https://openairdocs.org/sdr/1050617008AMW), Aug 24, 2005: PANEL. FAILED. LEFT WING UPPER BIN EVIDENCE OF DEFORMATION AT TURTLE BACK MOUNT FLANGE AREA. REPAIRED IAW SR-CO-00024. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. - [SDR 1050617009](https://openairdocs.org/sdr/1050617009), Aug 24, 2005: FRAME. CRACKED. CENTER CANTED FRAME AT FS 588. LEFT FLANGE CRACKED AT NUT PLATE AND RIVET, STRINGER 7L AND 8L. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. - [SDR 1050617008](https://openairdocs.org/sdr/1050617008), Aug 23, 2005: FLANGE. WORN. LT UPPER TURTLEBACK FLANGE WORN. CRACKED ON IB EDGE. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. - [SDR 10506017007](https://openairdocs.org/sdr/10506017007), Aug 22, 2005: FRAME. CORRODED. CORROSION FOUND ON INSPECTION FOR ABC STRUCTURAL FS 213.25. MORE INFORMATION TO BE ADDED AT A LATER DATE. - [SDR 62683](https://openairdocs.org/sdr/62683), Jun 30, 2004: VALVE. MALFUNCTIONED. LANDING GEAR FAILED TO EXTEND ON FIRST ATTEMPT. GEAR FINALLY EXTENDED ON THE SECOND ATTEMPT. REMOVED AND REPLACED HYD SERVICE VALVE. OPS CK GOOD. - [SDR 62587](https://openairdocs.org/sdr/62587), Jun 27, 2004: CONTROL HANDLE. MALFUNCTIONED. ON APPROACH TO LANDING. THE FIRST AND SECOND ATTEMPTS TO EXTEND LANDING GEAR FAILED. CREW WIGGLED HANDLE AND GOT GEAR TO EXTEND WITH ALL GEAR INDICATING DOWN LO - [SDR 62453](https://openairdocs.org/sdr/62453), Jun 23, 2004: HANDLE. UNSECURE. CREW NOTICED EMERGENGY EXIT HANDLE STICK OUT WAY FROM FUSELAGE MX RESEATED EXIT. REMOVED AND INSP LT EXIT DOOR REINSTALLED AND SECURED. - [SDR 62001](https://openairdocs.org/sdr/62001), Jun 4, 2004: FIRE LOOP. FAULTY. RT FIRE LOOP ANNUNCIATOR ILLUMINATED IN FLIGHT AND REMAINED ON. FLIGHT CREW LANDED AND TAXIED TO THE GATE WITH NO FURTHER INCIDENT. NO EMERGENCY DECLARED. NO EQ - [SDR 60135](https://openairdocs.org/sdr/60135), Mar 29, 2004: PRESSURE SWITCH. MALFUNCTIONED. UPON GETTING READY TO LAND IN PKB. CREW EXTENDED LANDING GEAR WITH CAUSE LANDING GEAR C/B TO POP AND NOT RESET. CREW CALLED AND DID A FLY BY TO VERIFY GEAR WAS - [SDR 56653](https://openairdocs.org/sdr/56653), Dec 1, 2003: HANDLE. STUCK. WHEN LANDING GEAR WAS PLACED IN DOWN POSITION LANDING GEAR FAILED TO EXTEND GEAR MANUALLY PUMPED DOWN IND THREE GREENS ACFT LANDED WITH NO FURTHER INCIDENT...CA - [SDR 56120](https://openairdocs.org/sdr/56120), Nov 13, 2003: SWITCH. DIRTY. DURING LANDING APPROACH MAIN LANDING GEARS FAILED TO EXTEND. THE CREW MANUALLY PUMPED DOWN THE GEARS. RECEIVED 3 GREEN INDICATIONS, LANDED WITH NO FURTHER INCID - [SDR 55265](https://openairdocs.org/sdr/55265), Oct 15, 2003: LANDING GEAR. FAILED. UPON DECENT FOR LANDING IN MCO. GEAR WOULD NOT EXTEND. IT HAD TO BE EMERGENCY EXTENDED (PUMPED DOWN) CREW GOT THREE DOWN AND LOCKED IND AHD SAFETY WITH NO FURTH - [SDR 55265AMWA](https://openairdocs.org/sdr/55265AMWA), Oct 15, 2003: LANDING GEAR. MALFUNCTIONED. UPON DECENT FOR LANDING IN MCO. GEAR WOULD NOT EXTEND IT HAD TO BE EMERGENCY EXTENDED (PUMPED DOWN). CREW GOT THREE DOWN AND LOCKED INDICATIONS AND LANDING SAFE - [SDR 51904](https://openairdocs.org/sdr/51904), Jun 24, 2003: LEAD. LOOSE. ON FLIGHT 5517, DURING THE FLIGHT THE RIGHT ENGINE ITT WENT TO 1000 DEGREES CELSIUS THEN WENT BACK TO NORMAL. SHORTLY THERE AFTER THE ITT AGAIN WENT TO 1000 DEG - [SDR 045518](https://openairdocs.org/sdr/045518), Nov 30, 2002: CIRCUIT BREAKER. TRIPPED. UPON ARRIVAL, THE MAIN LANDING GEAR WOULD NOT EXTEND TO NORMAL OPERATION. AFTER NOTICING THAT THE CIRCUIT BREAKER HAD POPPED, THE CREW RESET IT THREE TIMES, AFT - [SDR MASA99111](https://openairdocs.org/sdr/MASA99111), Jul 1, 1999: FUEL PUMP. FAILED. FLT 5906 - PIT-FKL - AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A FUEL PUMP FAILURE ON THE NR 1 ENGINE. THE CREW DECLARED AN EMERGENCY, AND RETURNED TO THE FIELD W - [SDR MASA98164](https://openairdocs.org/sdr/MASA98164), Aug 27, 1998: CAM LOCKS. OUT OF ADJUST. DUJ/PIT - FLT 5954 - CREW REPORTED THE PASSENGER DOOR CAMLOCKS WOULD NOT LATCH COMPLETELY. MAINTENANCE RIGGED THE DOOR CAMLOCKS, OPS CHECKED GOOD. AIRCRAFT WAS - [SDR 97ZZZX3236](https://openairdocs.org/sdr/97ZZZX3236), 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 97ZZZX3235](https://openairdocs.org/sdr/97ZZZX3235), 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 ## FAA accident and incident reports (4) 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 20031201031359I](https://openairdocs.org/incident/20031201031359I), Dec 1, 2003: Beech 1900D (N173YV), Pittsburgh, PA. (-23) Flt #5501: (jhw-pit) on final approach to pit airport, the main landing gear failed to extend. Crew had to use manual extension to extend gear. Obtained… - [Incident 20031113028689I](https://openairdocs.org/incident/20031113028689I), Nov 13, 2003: Beech 1900D (N173YV), Raleigh-Durham, NC. (-23) The crew reported the MLG failed to extend on approach to land at krdu. They manually extended the gear and obtained 3 green "down and locked"… - [Incident 20031015026689I](https://openairdocs.org/incident/20031015026689I), Oct 15, 2003: Beech 1900D (N173YV), Orlando, FL. (-23) On October 15, 2003, aircraft N173YV, flight 5543 while enroute from vsp to mco (on approach) the main landing gear would not extend. The crew declared… - [Incident 20021130034619I](https://openairdocs.org/incident/20021130034619I), Nov 30, 2002: Beech 1900D (N173YV), Wichita, MO. (-23) On November 11, 2002, at 10:30 local time, aircraft N173YV enroute from hys to mci flight 8716, the main landing gear failed to extend upon landing. The… --- 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.