# N139ZV: 1931 Beech 1900D, registration cancelled 2012-07-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 2, 2012 - Exported to: Canada - 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-139 - Year built: 1931 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: March 16, 1995 - Certificate issued: December 21, 2009 - Last registry action: January 4, 2010 - Mode S code: A09EF3 - Owner when cancelled: [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC) - Location: [Provo, UT](https://openairdocs.org/faa-place/UT/Provo) - Owner type: Corporation - Owner's area on the map: 40.2272° N, 111.6958° W: Placed by OpenAirDocs at the center of ZIP code 84601, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N139ZV - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=139ZV - Page: https://openairdocs.org/deregistered/N139ZV-2012-07-02 From the FAA registry file of November 3, 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 (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR BSAASDR0721](https://openairdocs.org/sdr/BSAASDR0721), Jun 7, 2007: WIRE. CHAFED. WHEN CREW SELECTED GEAR DOWN, THE LANDING GEAR CONTROL CB IMMEDIATELY TRIPPED. CREW EXTENDED GEAR AND LANDED WITH NO FURTHER INCIDENT. A CHAFED WIRE FOR THE GEA - [SDR BSAASDR0718](https://openairdocs.org/sdr/BSAASDR0718), Jun 7, 2007: ACTUATOR. MALFUNCTIONED. THE LANDING GEAR CIRCUIT BREAKER TRIPPED WHEN CREW SELECTED GEAR DOWN DURING APPROACH. GEAR WAS EXTENDED MANUALLY AND CREW LANDED WITHOUT INCIDENT. AFTER EXTENS - [SDR BSAASDR0716](https://openairdocs.org/sdr/BSAASDR0716), May 30, 2007: DIODE. INTERMITTENT. THE LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED WHEN GEAR DOWN WAS SELECTED. CREW EXTENDED GEAR BY MANUALLY PUMPING GEAR DOWN. REPLACED DIODES FOR THE LANDING - [SDR BSAASDR0712](https://openairdocs.org/sdr/BSAASDR0712), May 12, 2007: SWITCH. INOPERATIVE. DURING APPROACH WHEN CREW SELECTED GEAR DOWN THE LANDING GEAR RELAY CONTROL CB TRIPPED WHEN THE GEAR WAS HALFWAY DOWN. CREW ABORTED THE APPROACH AND MANUALLY EX - [SDR BSAASDR0711](https://openairdocs.org/sdr/BSAASDR0711), May 11, 2007: LANDING GEAR. FAILED. DURING APPROACH, WHEN CREW SELECTED GEAR DOWN, THE LANDING GEAR CONTROL RELAY CIRCUIT BREAKER TRIPPED HALFWAY THROUGH THE GEAR EXTENSION. CREW ABORTED LANDING, - [SDR BSAASDR0706](https://openairdocs.org/sdr/BSAASDR0706), Apr 3, 2007: WIRE. CHAFED. WHEN THE GEAR WAS SELECTED DOWN, & THE GEAR DIDN'T EXTEND, CREW FOUND 2 AMP GEAR CONTROL CB TRIPPED. CREW RESET CB, & TRIED AGAIN, THE CB TRIPPED AGAIN. CREW TH - [SDR 2007F00028](https://openairdocs.org/sdr/2007F00028), Apr 3, 2007: UNKNOWN. UNKNOWN. THIS AIRCRAFT HAS HAD MULTIPLE REOCCURRING GEAR MALFUNCTIONS. ON NUMEROUS OCCASIONS AC HAS HAD THE LANDING GEAR CIRCUIT BREAKER POP IN-FLIGHT WHICH HAS RESULTED - [SDR BSAASDR0705](https://openairdocs.org/sdr/BSAASDR0705), Mar 13, 2007: RELAY. ARCED. WHEN THE GEAR WAS SELECTED DOWN DURING APPROACH THE GEAR DIDN'T EXTEND. THE CREW FOUND THE 2 AMP GEAR CONTROL CIRCUIT BREAKER POPPED. CREW ABORTED LANDING, PUT - [SDR BSAASDR0704](https://openairdocs.org/sdr/BSAASDR0704), Mar 7, 2007: WIRE. CHAFED. WHEN THE GEAR WAS SELECTED DOWN, THE GEAR DIDN'T EXTEND. THE RED GEAR HANDLE LIGHT DIDN'T COME ON & THE GREEN GEAR DOWN LIGHTS DIDN'T COME ON. THE 2AMP GEAR REL - [SDR BSAASDR0703](https://openairdocs.org/sdr/BSAASDR0703), Mar 1, 2007: CIRCUIT BOARD. MALFUNCTIONED. WHEN GEAR HANDLE WAS SELECTED DOWN DURING APPROACH, THE GEAR DIDN'T EXTEND, THE RED UNSAFE LIGHT CAME ON, AND THE GREEN GEAR DOWN LIGHTS STAYED OFF. CREW FOUND - [SDR BSAASDR0618](https://openairdocs.org/sdr/BSAASDR0618), Aug 2, 2006: SENSE LINE. BROKEN. ON SHORT FINAL, CREW NOTED A NR 2 ENGINE SURGE, THEN THE ENGINE SEEMED TO QUIT. THE PROP AUTOFEATHER SYSTEM WORKED CORRECTLY AND THE PROP FEATHERED. AFTER LANDI - [SDR BSAASDR0615](https://openairdocs.org/sdr/BSAASDR0615), Jun 7, 2006: CONNECTOR. DISCONNECTED. THE AIRCRAFT DID NOT PRESSURIZE & THE CABIN WARNING LIGHT CAB ALT HI DIDN'T COME ON WHEN THE CABIN ALTITUDE WENT ABOVE 10,000FT. ONE OF THE ELECTRICAL CONNECTOR - [SDR BSAASDR0611](https://openairdocs.org/sdr/BSAASDR0611), Apr 25, 2006: REGULATOR. MALFUNCTIONED. DURING CLIMBOUT THE RIGHT BLEED AIR FAIL LIGHT CAME ON. CREW FOLLOWED PROCEDURES, AND SHUT DOWN RIGHT BLEED SYSTEM AND RETURNED TO THE STATION. MAINTENANCE FOUN - [SDR BSAASDR0610](https://openairdocs.org/sdr/BSAASDR0610), Apr 23, 2006: PRECOOLER. MALFUNCTIONED. DURING CRUISE, CREW NOTED A SMELL OF BURNING RUBBER, ACCOMPANIED BY LOW CABIN PRESSURE LIMITED TO 4 PSI AND THE CABIN TEMPERATURE WOULD ONLY WARM UP TO 45 DEGRE - [SDR BSAASDR0603](https://openairdocs.org/sdr/BSAASDR0603), Feb 16, 2006: WIRE. OUT OF POSITION. NR 1 ENGINE FIRE WARNING LIGHT CAME ON BRIEFLY 3-5 SECONDS, WHILE IN CRUISE, AND WENT OUT AS CAPTAIN BEGAN TO REACH FOR THE EMERGENCY CHECKLIST. SYSTEM WAS CHEC - [SDR BSAASDR0604](https://openairdocs.org/sdr/BSAASDR0604), Feb 16, 2006: FIRE DETECTOR. SHORTED. DURING CRUISE, LEFT FIRE DETECTOR LOOP LIGHT CAME ON AND STAYED ILLUMINATED, CREW LANDED WITH NO FURTHER INCIDENT. REPLACED FORWARD FIRE DETECTOR LOOP DUE TO FI - [SDR 68346](https://openairdocs.org/sdr/68346), Jan 10, 2005: MASTER CYLINDER. DAMAGED. ALL FOUR BRAKE PEDALS SPONGY ON LANDING. REMOVED AND REPLACED RT SIDE OUTBOUND MASTER BRAKE CYCLINDER. P/N 90-380001-33 (OFF), S/N 7984 (ON), P/N 90-380001-33 ( - [SDR 66793](https://openairdocs.org/sdr/66793), Nov 15, 2004: BRAKE ASSY. MALFUNCTIONED. CREW REPORTED CAPT'S RIGHT BRAKE SPONGY ON LANDING. PRESSURE RT BLEED RT BRAKES. - [SDR 66593](https://openairdocs.org/sdr/66593), Nov 8, 2004: BRAKE. MALFUNCTIONED. CAPT REPORTS RT BRAKE SPONGY. BLED RT BRAKES. - [SDR 66603](https://openairdocs.org/sdr/66603), Nov 8, 2004: MASTER CYLINDER. FAILED. UPON TAXI IN, CAPT EXPERIENCED RT BRAKE PERFORMANCE SPONGY, A/C CONTINUED TO GATE/HANGAR WITH NO FURTHER INCIDENT. REMOVED AND REPLACED CAPT'S RT BRAKE MASTER C - [SDR 65218](https://openairdocs.org/sdr/65218), Sep 23, 2004: ROD END. OUT OF ADJUST. WHEN CREW WENT TO CLOSE AIRSTAIR DOOR, DOOR WOULD NOT CLOSE PROPERLY PASSENGERS WHERE DEPLANED AND MAINTENANCE CALLED. ADJUSTED ASD COUNTER BALANCE RODENDS, CK - [SDR 62040](https://openairdocs.org/sdr/62040), Jun 6, 2004: CABLE. OUT OF ADJUST. UPON FIRST FLIGHT OF THE DAY INITIAL WALK AROUND INSPECTION, CAPTAIN NOTICED PAX MAIN DOOR SLIGHTLY LOOSE WHEN FULLY CLOSED WITH INDICATOR FULLY IN VIEW. PAX NE - [SDR AMWA110](https://openairdocs.org/sdr/AMWA110), Dec 22, 2003: RIB. CRACKED. DURING INSPECTION FOUR CRACKS FOUND ON THIS RIB, TWO ON THE LT SIDE AND TWO ON THE RT SIDE LOCATED ON STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT S - [SDR AMWA109](https://openairdocs.org/sdr/AMWA109), Dec 22, 2003: RIB. CRACKED. DURING INSPECTION, FIVE CRACKS FOUND IN THIS RIB, THREE ON THE RT SIDE AND TWO ON THE LT SIDE LOCATED ON THE STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOL - [SDR AMWA107](https://openairdocs.org/sdr/AMWA107), Dec 22, 2003: RIB. CRACKED. DURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON THE LT SIDE AT STRINGER TO RIB INTERSECTION STRINGER. P/N 101-640000-39. - [SDR AMWA108](https://openairdocs.org/sdr/AMWA108), Dec 22, 2003: RIB. CRACKED. DURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON RT SIDE ON STRINGER TO RIB INTERSECTION ON THE FIRST RIVET HOLE. RT STRINGER P/N 101-640000-46. - [SDR AMWA58](https://openairdocs.org/sdr/AMWA58), Sep 20, 2003: ENGINE. FIRE. FIRE STARTED IN LEFT ENGINE. FIRE WAS EXTINGUISHED BY MOTORING OF ENGINE. - [SDR AMWA21](https://openairdocs.org/sdr/AMWA21), Aug 13, 2003: BULKHEAD. CRACKED. WHILE TROUBLESHOOTING A PRESSURIZATION DISCREPANCY USING A PRESSURE CART, AIR FLOW WAS NOTED COMING FROM UNDER THE RIGHT AVIONICS SHELF. FURTHER INVESTIGATION R - [SDR 2003F00575](https://openairdocs.org/sdr/2003F00575), Aug 13, 2003: PRESSURE BLKHD. CRACKED. WHILE TROUBLESHOOTING A PRESSURIZATION DISCREPANCY USING A PRESSURE CART, AIR FLOW WAS NOTED COMING FROM UNDER THE RIGHT AVIONICS SELF. FURTHER INVESTIGATION RE - [SDR AMWA7](https://openairdocs.org/sdr/AMWA7), Jan 29, 2003: TRUSS. CRACKED. WHILE PERFORMING AN "H" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND A CRACK LOCATED ON THE TRUSS. THE CRACK IS YET TO BE DETERMINED OF THE LOCATION. MAINTEN - [SDR 046592](https://openairdocs.org/sdr/046592), Jan 9, 2003: VALVE. OUT OF ADJUST. ON TAXI, THE LEFT PROPELLER FAILED TO FEATHER MANUALLY. THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE FEATHER VALVE. NO P - [SDR 2002F00271](https://openairdocs.org/sdr/2002F00271), Feb 23, 2002: DOOR. OUT OF RIG. FOUND DURING PREFLIGHT CHECK, THE RAMP AGENT FOUND THE HANDLE TO THE EMEGENCY EXIT DOOR NOT FLUSH, MAINTENANCE FOUND THE DOOR TO BE OUT OF RIG, WAS FERRIED TO P - [SDR 98ZZZM893](https://openairdocs.org/sdr/98ZZZM893), Mar 30, 1998: SKIN. CRACKED. DURING ACCEPTANCE INSPECTION ICT MAINTENANCE, FOUND THE OUTBOARD ATTACH POINT INBOARD ACCESS HOLE ON THE RT INBOARD FLAP HAD SMALL CRACK FROM IT. REPAIRED CRACK - [SDR MASA97002](https://openairdocs.org/sdr/MASA97002), Jan 10, 1997: GEAR. COLLAPSED. FLT 5326 - FLT CREW ABORTED TAKEOFF, ON LANDING, THE NOSE GEAR COLLAPSED CAUSING DAMAGE TO THE PROPELLERS AND FUSELAGE. AIRCRAFT DAMAGE WAS REPAIRED. GROUND OPS - [SDR 95ZZZZ214](https://openairdocs.org/sdr/95ZZZZ214), Mar 27, 1995: FUEL FLOW GAUGE. INOPERATIVE. FUEL FLOW INDICATOR ON RT SIDE INOPERATIVE. SUGGEST IMPROVEMENT OF INTERNAL COMPONENTS TO INCREASE RELIABILITY. ## NTSB investigations (1) 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 NYC97FA045](https://openairdocs.org/ntsb/NYC97FA045), Jan 10, 1997: Beech 1900D (N139ZV), Bangor, ME, substantial damage. Probable cause: The inadequate flight and winter operations training provided by the operator, and the pilot's improper decision to abort the takeoff while airborne above V1, due to a false stall warning horn. Also… ## FAA accident and incident reports (3) 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 20070512008409I](https://openairdocs.org/incident/20070512008409I), May 12, 2007: Beech 1900D (N139ZV), Springfield, IL, No damage. (-23) During approach when crew selected gear down the landing gear relay control cb tripped when the gear was halfway down. The crew aborted the approach and… - [Incident 20020215008339I](https://openairdocs.org/incident/20020215008339I), Feb 15, 2002: Beech 1900D (N139ZV), Jacksonville, FL. (-23) On February 15, 2002, at 08:12 local time, aircraft N139YV left engine oil pressure dropped to 75 PSI on climb out. The flight crew complied with the… - [Accident 19970110000309A](https://openairdocs.org/incident/19970110000309A), Jan 10, 1997: Beech 1900D (N139ZV), Bangor, ME, Substantial damage. Crashed on takeoff, attained altitude of 400FT before dropping to runway and breaking in two. (.4)during takeoff roll, as the fo rotated the airplane, 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.