N139ZV, cancelled Jul 2, 2012

Service difficulty reports · 35

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

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N139ZV' AND deregistration_id = 'N139ZV-2012-07-02'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR BSAASDR0721Wire · chafedWHEN 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 GEAR DOWN MICROSWITCH WAS FOUND UNDER THE CABIN FLOOR BENEATH SEAT 4A. THE WIRE WAS GROUNDING ON A DEJun 7, 2007 · N139ZV · Beech 1900D · Landing Gear System WiringSDR BSAASDR0718Actuator · malfunctionedTHE LANDING GEAR CIRCUIT BREAKER TRIPPED WHEN CREW SELECTED GEAR DOWN DURING APPROACH. GEAR WAS EXTENDED MANUALLY AND CREW LANDED WITHOUT INCIDENT. AFTER EXTENSIVE TROUBLESHOOTING, THE RIGHT MAIN LANDING GEAR ACTUATOR WAS CHANGED DUE TO A SUSPECTED FAULT IN Jun 7, 2007 · N139ZV · Beech 1900D · Landing Gear ActuatorSDR BSAASDR0716Diode · intermittentTHE LANDING GEAR CONTROL CIRCUIT BREAKER TRIPPED WHEN GEAR DOWN WAS SELECTED. CREW EXTENDED GEAR BY MANUALLY PUMPING GEAR DOWN. REPLACED DIODES FOR THE LANDING GEAR SELECT SOLENOID, MULTIPLE GEAR SWINGS AND OPERATIONAL CHECK FLIGHT WERE BOTH GOOD.May 30, 2007 · N139ZV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR BSAASDR0712Switch · inoperativeDURING 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 EXTENDED THE GEAR. CREW LANDED WITH NO FURTHER INCIDENT. ALL WIRING & COMPONENTS IN THE LANDING GEAMay 12, 2007 · N139ZV · Beech 1900D · Landing Gear SelectorSDR BSAASDR0711Landing Gear · failedDURING APPROACH, WHEN CREW SELECTED GEAR DOWN, THE LANDING GEAR CONTROL RELAY CIRCUIT BREAKER TRIPPED HALFWAY THROUGH THE GEAR EXTENSION. CREW ABORTED LANDING, PERFORMED MANUAL EXTENSION AND LANDED WITH NO FURTHER INCIDENT. THE GEAR CB WAS RESET, AND THE GEAMay 11, 2007 · N139ZV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR BSAASDR0706Wire · chafedWHEN 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 THEN PUMPED GEAR DOWN USING MANUAL EXTENSION SYSTEM. CREW LANDED WITH NO FURTHER INCIDENT. THE GEAApr 3, 2007 · N139ZV · Beech 1900D · Landing Gear System WiringSDR 2007F00028Unknown · unknownTHIS AIRCRAFT HAS HAD MULTIPLE REOCCURRING GEAR MALFUNCTIONS. ON NUMEROUS OCCASIONS AC HAS HAD THE LANDING GEAR CIRCUIT BREAKER POP IN-FLIGHT WHICH HAS RESULTED IN A MANUAL PUMPING OF LANDING GEAR HYD SYS. AC HAS BEEN BROUGHT TO MAINTENANCE HANGAR FOR THESE Apr 3, 2007 · N139ZV · Beech 1900D · Landing Gear SystemSDR BSAASDR0705Relay · arcedWHEN 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 GEAR HANDLE IN UP POSITION, RESET CB, & PLACED GEAR HANDLE IN DOWN POSITION, & CB POPPED AGAIN. CMar 13, 2007 · N139ZV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR BSAASDR0704Wire · chafedWHEN 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 RELAY CONTROL CB WAS FOUND POPPED. THE CREW ABORTED THE LANDING AND DECLARED AN EMERGENCY. EMERGENCYMar 7, 2007 · N139ZV · Beech 1900D · Landing Gear System WiringSDR BSAASDR0703Circuit Board · malfunctionedWHEN 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 THE 2 AMP CONTROL CB POPPED. GEAR HANDLE WAS PUT BACK UP, THE CB WAS RESET, AND THE CB POPPED AGAIMar 1, 2007 · N139ZV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR BSAASDR0618Sense Line · brokenON 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 LANDING, THE CREW REPORTED THE ENGINE RESTARTED WITHOUT INPUT FROM THE CREW, BUT THE PROP REMAINED FEATAug 2, 2006 · N139ZV · Beech 1900D · Fuel Controlling SystemSDR BSAASDR0615Connector · disconnectedTHE 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 CONNECTORS ON THE CAB ALT HI PRESSURE SWITCH WAS FOUND DISCONNECTED. THE CONNECTOR WAS REINSTALLED. THE CRJun 7, 2006 · N139ZV · Beech 1900D · Cabin Pressure IndicatorSDR BSAASDR0611Regulator · malfunctionedDURING CLIMBOUT THE RIGHT BLEED AIR FAIL LIGHT CAME ON. CREW FOLLOWED PROCEDURES, AND SHUT DOWN RIGHT BLEED SYSTEM AND RETURNED TO THE STATION. MAINTENANCE FOUND THE RIGHT BLEED AIR VALVE AT TOO HIGH A PRESSURE AND REPLACED THE VALVE.Apr 25, 2006 · N139ZV · Beech 1900D · Pneumatic Distribution SystemSDR BSAASDR0610Precooler · malfunctionedDURING 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 DEGREES F. MAINTENANCE FOUND THE LEFT BLEED INOPERATIVE, AND FOUND BOTH LEFT ENGINE PRECOOLER VALVES STIApr 23, 2006 · N139ZV · Beech 1900D · Heating SystemSDR BSAASDR0603Wire · out of positionNR 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 CHECKED AFTER ARRIVAL, VISUAL AND OPERATIONAL INSPECTION REVEALED NO DEFECTS, WITH THE FIRE DETECTER WIFeb 16, 2006 · N139ZV · Beech 1900D · Fire Protection System WiringSDR BSAASDR0604Fire Detector · shortedDURING CRUISE, LEFT FIRE DETECTOR LOOP LIGHT CAME ON AND STAYED ILLUMINATED, CREW LANDED WITH NO FURTHER INCIDENT. REPLACED FORWARD FIRE DETECTOR LOOP DUE TO FINDING CENTER WIRE SHORTED TO SHIELD. SYSTEM OPS CK GOOD.Feb 16, 2006 · N139ZV · Beech 1900D · Fire DetectionSDR 68346Master Cylinder · damagedALL 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 (OFF), S/N 3119 (OFF).Jan 10, 2005 · N139ZV · Beech 1900D · Master Cylinder/Brake ValveSDR 66793Brake Assy · malfunctionedCREW REPORTED CAPT'S RIGHT BRAKE SPONGY ON LANDING. PRESSURE RT BLEED RT BRAKES.Nov 15, 2004 · N139ZV · Beech 1900D · BrakeSDR 66593Brake · malfunctionedCAPT REPORTS RT BRAKE SPONGY. BLED RT BRAKES.Nov 8, 2004 · N139ZV · Beech 1900D · BrakeSDR 66603Master Cylinder · failedUPON 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 CYLINDER AND BLED BRAKES. OPS CK NORMAL P/N 90-380001-33 S/N 3273 P/N 90-380001-33 (OFF) S/N 3123 (Nov 8, 2004 · N139ZV · Beech 1900D · BrakeSDR 65218Rod End · out of adjustWHEN CREW WENT TO CLOSE AIRSTAIR DOOR, DOOR WOULD NOT CLOSE PROPERLY PASSENGERS WHERE DEPLANED AND MAINTENANCE CALLED. ADJUSTED ASD COUNTER BALANCE RODENDS, CK GOOD.Sep 23, 2004 · N139ZV · Beech 1900D · Passenger/Crew DoorsSDR 62040Cable · out of adjustUPON 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 NEVER BOARDED. AIRCRAFT DID NOT LEAVE GATE. RE-ADJUSTED UPPER, FWD AIRSTAIR DOOR CABLE, OPS CHECK NJun 6, 2004 · N139ZV · Beech 1900D · Entrance StairsSDR AMWA110Rib · crackedDURING 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 STRINGER P/N 101-640000-46 & 101-640000-38. LT STRINGER P/N 101-640000-39 & 101-640000-45.Dec 22, 2003 · N139ZV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA109Rib · crackedDURING 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 HOLE. RT STRINGER P/N 101-640000-45, 101-640000-42 & 101-640000-38. LT STRINGER P/N 101-640000-43, 10Dec 22, 2003 · N139ZV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA107Rib · crackedDURING INSPECTION, ONE CRACK FOUND ON THIS RIB ON THE LT SIDE AT STRINGER TO RIB INTERSECTION STRINGER. P/N 101-640000-39.Dec 22, 2003 · N139ZV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA108Rib · crackedDURING 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.Dec 22, 2003 · N139ZV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA58Engine · fireFIRE STARTED IN LEFT ENGINE. FIRE WAS EXTINGUISHED BY MOTORING OF ENGINE.Sep 20, 2003 · N139ZV · Beech 1900D · Fire DetectionSDR AMWA21Bulkhead · crackedWHILE TROUBLESHOOTING A PRESSURIZATION DISCREPANCY USING A PRESSURE CART, AIR FLOW WAS NOTED COMING FROM UNDER THE RIGHT AVIONICS SHELF. FURTHER INVESTIGATION REVEALED A CRESENT SHAPED CRACK IN THE FWD PRESSURE BULKHEAD AT FS 84 BELOW THE SHELF. THE CRACK RUAug 13, 2003 · N139ZV · Beech 1900D · Fuselage Main, BulkheadSDR 2003F00575Pressure Blkhd · crackedWHILE TROUBLESHOOTING A PRESSURIZATION DISCREPANCY USING A PRESSURE CART, AIR FLOW WAS NOTED COMING FROM UNDER THE RIGHT AVIONICS SELF. FURTHER INVESTIGATION REVEALED A CRESENT SHAPED CRACK IN THE FORWARD PRESSURE BULKHEAD AT FS. 84, BELOW SELF. THE CRACK RUNAug 13, 2003 · N139ZV · Beech 1900D · Fuselage Main, BulkheadSDR AMWA7Truss · crackedWHILE 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. MAINTENANCE REMOVED AND REPLACED IT WITH ANOTHER ENGINE TRUSS. TEARDOWN REPORT WILL BE AVAILABLE AT A LATERJan 29, 2003 · N139ZV · Beech 1900D · Engine Mount SectionSDR 046592Valve · out of adjustON TAXI, THE LEFT PROPELLER FAILED TO FEATHER MANUALLY. THE AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE FEATHER VALVE. NO PARTS WERE USED. TEARDOWN REPORT WILL NOT BE REQUIRED.Jan 9, 2003 · N139ZV · Beech 1900D · Propeller Feathering/ReversingSDR 2002F00271Door · out of rigFOUND 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 PFN FOR REPAIR WITH NO FURTHER INCIDENT. (M)Feb 23, 2002 · N139ZV · Beech 1900D · Emergency ExitsSDR 98ZZZM893Skin · crackedDURING ACCEPTANCE INSPECTION ICT MAINTENANCE, FOUND THE OUTBOARD ATTACH POINT INBOARD ACCESS HOLE ON THE RT INBOARD FLAP HAD SMALL CRACK FROM IT. REPAIRED CRACK IAW AMWA TO 1900-27-00-0001. (M)Mar 30, 1998 · N139ZV · Beech 1900D · Trailing Edge FlapsSDR MASA97002Gear · collapsedFLT 5326 - FLT CREW ABORTED TAKEOFF, ON LANDING, THE NOSE GEAR COLLAPSED CAUSING DAMAGE TO THE PROPELLERS AND FUSELAGE. AIRCRAFT DAMAGE WAS REPAIRED. GROUND OPS CHECK WAS PERFORMED NO DISCREPANCIES WERE NOTED. TEST FLIGHT WAS PERFORMED SATISFACTORILY AND AIJan 10, 1997 · N139ZV · Beech 1900D · Nose/Tail Landing GearSDR 95ZZZZ214Fuel Flow Gauge · inoperativeFUEL FLOW INDICATOR ON RT SIDE INOPERATIVE. SUGGEST IMPROVEMENT OF INTERNAL COMPONENTS TO INCREASE RELIABILITY.Mar 27, 1995 · N139ZV · Beech 1900D · Fuel Flow Indicating
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