N218YV, cancelled Aug 18, 2015

Service difficulty reports · 43

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 = 'N218YV' AND deregistration_id = 'N218YV-2015-08-18'
  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 A8OA2014F00068Pressure Switch · defectiveLEFT ENGINE AFX, AUTOFEATHER, ANNUNCIATOR DOES NOT ILLUMINATE WITH POWER LEVERS ABOVE 89-91 PERCENT N1.Feb 9, 2014 · N218YV · Beech 1900D · Propeller Controlling SystemSDR A8OA2013040200004Pressure Switch · defectiveWITH AUTOFEATHER ARMED AND POWERED AND PASSING APPROX 93-94 PERCENT THE AFX ANNUNCIATOR ILLUMINATES. AFTER TROUBLESHOOTING, REMOVED DEFECTIVE RT HIGH OIL PRESSURE SWITCH, INSTALLED NEW SWITCH IAW MM CHAPTER 61-21-01. GROUND RUN UP OPERATED WITHIN SPECIFICATIMar 31, 2013 · N218YV · Beech 1900D · Engine Oil Indicating SystemSDR GLBA20110531FBulkhead · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE BULKHEAD WHERE THE HYD POWERPACK ATTACHES, LT INBD WING, 3.6" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-004. MATERIALS UTILIMay 31, 2011 · N218YV · Beech 1900D · Wing Main, Frame StructureSDR GLBA20110526GSkin · damagedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MX FOUND THE AILERON SCRAPED 32" OF OTBD, TOP LWR AND FWD SKIN DAMAGED AND OTBD 4 RIBS AND DOUBLERS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-27-0May 26, 2011 · N218YV · Beech 1900D · AileronsSDR GLBA20110516HCircuit Board · inoperativeSIG EVENT - PILOT REPORTED THAT THE LT AFX ANNUNCIATOR AND REPEATER FLICKERED AND THEN WENT OUT, CAME BACK ON FOR A WHILE AND WENT OUT AGAIN. MX REPLACED PCB 129.May 14, 2011 · N218YV · Beech 1900D · Propeller/Propulsor System WiringSDR GLBA20110307FStructure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RT STABILON OB TIP DAMAGED WHILE PARKING IN HANGER. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-55-005. MATERIALS UTILIZED ARE INCLMar 5, 2011 · N218YV · Beech 1900D · Stabilizer Control SystemSDR GLBA20110214GStructure · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX THE RT STABILON WAS DAMAGED. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 11-1900-55-003. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Feb 12, 2011 · N218YV · Beech 1900D · Vertical Stabilizer Miscellaneous StructureSDR GLBA20110202FStructure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND 4 CRACKS AROUND THE VENT HOLE IN THE VERT STAB BEHIND THE BULLET CTR WEB, ALL 4 CRACKS ARE .5" IN LENGTH. SUPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAPFeb 2, 2011 · N218YV · Beech 1900D · Horizontal Stabilizer StructureSDR GLBA20100505GStringer · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND IN A CUTOUT AT STRINGER 9AR AND F.S. 177.3. CRACK IS APPROX .8" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-019. MATERIALS UTILIZED ARE INCMay 5, 2010 · N218YV · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA20100505FStringer · crackedDURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND IN A CUTOUT AT STRINGER 9AR AND FS 163.9. CRACK IS APPROX .5" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-018. MATERIALS UTILIZED ARE INCLUDED IN THE EO.May 5, 2010 · N218YV · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2009091409GSkin · crackedMAJOR REPAIR - PILOTS REPORTED THAT THE FUSELAGE WAS PUNCTURED IN THE LT FUSELAGE JUST FWD OF FS 273.25 ON THE UPPER SKIN. DAMAGED AREA APPROX 2.1 INCH BY 3.5 INCH. (2) CRACKS PRESENT. (1) CRACK APPROX 2.3 INCHES AND THE OTHER 1.1 INCH IN LENGTH. MX REPASep 12, 2009 · N218YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090914FSkin · gougedMAJOR REPAIR - PILOTS REPORTED A SMALL DENT IN THE LT FUSELAGE JUST FWD OF FS 258.25 ON THE UPPER SKIN. DAMAGED AREA APPROX .250 INCH BY .750 INCH. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-53-019. RII INSP C/W IAW GLA EO 09-1900-53-019.Sep 12, 2009 · N218YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090720FSkin · crackedDURING ROUTINE SCHEDULED MX TWO CRACKS ON TOP OF FUSELAGE AT FS 150.6 WERE DISCOVERED. TOP CENTERLINE 1 RIVET HEAD SHEARED INBD OF CRACK 1.250 INCHES LONG AND A .250 INCH CRACK LT OF CENTERLINE. MX REPAIRED AFFECTED AREA IAW EO 09-1900-53-009. REPAIR AREA AJul 17, 2009 · N218YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090508CValve · wornFLIGHT 5145 - THE PILOTS REPORTED THAT DURING CRUISE THE VACUUM PRESSURE WAS READING AS LOW AS 3.5 AT FLIGHT LEVEL 220. MAINTENANCE REMOVED AND REPLACED THE VACUUM REGULATOR VALVE IAW B1900D MM 37-00-01. THE OPERATIONAL CHECK WAS GOOD.May 8, 2009 · N218YV · Beech 1900D · Vacuum Distribution SystemSDR GLBA20090408BVor System · inoperativePILOTS REPORTED THAT THE NR 2 NAV RADIO WAS INOPERATIVE AND RETURNED TO DEN. MAINTENANCE REMOVED AND REPLACED THE VOR-ILS RECEIVER IAW MM 34-20-00. OPERATIONAL CHECK WAS GOOD.Apr 8, 2009 · N218YV · Beech 1900D · Visual Omnirange (VOR) SystemSDR GLBA200903211Cable · loosePILOTS REPORTED THAT TAKEOFF ABORTED DUE TO 2 PROP RPM AT 1500. MAINTENANCE FOUND THE GOVERNOR CONTROL CABLE LOOSE FROM FORWARD MOUNT. RE-ATTACHED & SAFETIED. OPERATIONAL CHECKS GOOD I.A..W 61-20-00.Mar 21, 2009 · N218YV · Beech 1900D · Propeller Controlling SystemSDR GLBA20090315AGovernor · low torqueABORTED TAKEOFF BECAUSE THE RT PROPELLER RPM ONLY CAME UP TO 1600 AND THEY THEN ABORTED THE TAKEOFF. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE RIGHT PROPELLER GOVERNOR OUT RIG. MAINTENANCE RIGGED THE ENGINEBY TURNING THE PROP RPM SCREW OUT AND TESTED THMar 3, 2009 · N218YV · Beech 1900D · Propeller GovernorSDR GLBA200910092Switch · out of adjustON FINAL APPROACH THE PILOTS REPORTED THAT THE NR 2 ENGINE BEGAN TO AUTO-FEATHER AT 500 LBS OF TORQUE. MX ADJUSTED THE LT AND RT AUTOFEATHER ARMING SWITCHES IAW B1900D MM 61-21. OPS CHECK WAS GOOD.Jan 5, 2009 · N218YV · Beech 1900D · Propeller Feathering/ReversingSDR GUUA12040702Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET.Dec 4, 2007 · N218YV · Beech 1900D · Elevator Miscellaneous StructureSDR GUUA12040701Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET.Dec 4, 2007 · N218YV · Beech 1900D · Elevator StructureSDR GUUA11240701Annunciator · warning lightFLIGHT: 9269, DURING FLIGHT, RT FIRE DISCHARGE ANUNCIATOR ILLUMINATED. REPLACED TERMINAL ON RT FIRE EXTINGUISHER.Nov 24, 2007 · N218YV · Beech 1900D · Extinguishing SystemSDR GUUA11130701Downlock Switch · looseFLIGHT: 9200, DURING APPROACH LANDING GEAR UNSAFE LIGHTS DID NOT ILLUMINATE (3) GREEN INDICATION DID NOT ILLUMINATE WHEN GEAR HANDLE PLACED IN THE DOWN POSITION. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED CIRCUIT BREAKER 16 AND RESECURED LT MAIN Nov 13, 2007 · N218YV · Beech 1900D · Landing Gear Position and WarningSDR GUUA05200702Switch · out of adjustFLIGHT: 9267 EYW/MIA DURING APPROACH LANDING GEAR HORN AND LIGHT ANNUNCIATED AT ABOUT 75 PERCENT N1 OR ABOUT 500LBS OF TORQUE. SYSTEM WORKS BUT AT A LOWER VALUE THAN NORMAL. ADJUSTED PEDESTAL SWITCHES OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.May 20, 2007 · N218YV · Beech 1900D · Landing Gear Position and WarningSDR GUUA05040703Circuit Breaker · unknownFLIGHT: 9247 FLL/FLL - AFTER TAKEOFF LANDING, GEAR DID NOT RETRACT. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR CONTROL CIRCUIT BREAKER. OPERATIONAL CHECK NORMAL.May 4, 2007 · N218YV · Beech 1900D · Landing Gear System WiringSDR GUUA10100601Unknown · odorDURING FLIGHT, STRONG LUBRICATION SMELL PRESENT IN THE COCKPIT AND CABIN. INSPECTED UNDER FLOORBOARDS IN CABIN AND COCKPIT CLEANED HYDRAULIC FLUID DUE TO OVERSERVICE NO LUBRICATION SMELL NOTED AT THIS TIME.Oct 10, 2006 · N218YV · Beech 1900D · Air Distribution SystemSDR GUUA06110601Actuator · malfunctionedFLIGHT:9280 EYW/TPA AFTER TAKEOFF WHEN LANDING GEAR SELECTED UP THREE GREEN ANNUNCIATOR ILLUMINATED, MOTOR RUNS INTERMITTENT, BREAKER POPS. CONTINUED TO TPA LANDED WITHOUT INCIDENT. MAINTENANCE FERRY TO FLL. REPLACED LEFT MAIN LANDING GEAR ACTUATOR. TEST FJun 11, 2006 · N218YV · Beech 1900D · Landing Gear ActuatorSDR GUUA05180601Valve · faultyFLIGHT: 9235 JAX/TPA DURING APPROACH LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER AND LOWERED LANDING GEAR NORMALLY. REPLACED LANDING GEAR SERVICE VALVE.May 18, 2006 · N218YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA04280601Circuit Breaker · trippedFLIGHT:9266 MHH/PBI AFTER TAKEOFF LANDING GEAR CIRCUIT BREAKER TRIPPED LANDING GEAR WOULD NOT RETRACT. DIVERTED TO FLL LANDED WITHOUT INCIDENT. TROUBLESHOT LANDING GEAR SYSTEM. CHECKED POWER PACK FLUID. LANDING GEAR OPERATIONAL CHECKS NORMAL NO DEFECTS NOTEDApr 28, 2006 · N218YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GUUA04240601Printed Ckt Board · faultyFLIGHT: 9246, AFTER TAKEOFF LANDING GEAR CIRCUIT BREAKER POPPED COULD NOT RETRACT THE LANDING GEAR. DIVERTED, LANDED WITHOUT INCIDENT. REPLACED TIME DELAY PC BOARD.Apr 24, 2006 · N218YV · Beech 1900D · Landing Gear Position and WarningSDR GUUA04160601Elec Connector · dirtyFLIGHT: 9287, DURING APPROACH, LANDING GEAR RELAY CIRCUIT BREAKER POPPED.CLEANED LT AND RT NOSE LANDING GEAR ACTUATOR CONNECTOR PLUGS FOR DOWN LOCK SWITCHES. OPERATIONAL CHECK NORMAL, NO DEFECTS NOTED.Apr 16, 2006 · N218YV · Beech 1900D · Landing Gear Position and WarningSDR GUUA02010601Annunciator · looseEYW/FLL DURING APPROACH LANDING GEAR WARNING SOUNDED. TIGHTENED LANDING GEAR ANNUNCIATOR HOUSING.Feb 1, 2006 · N218YV · Beech 1900D · Landing Gear Position and WarningSDR 65837Gas Generator · malfunctionedDURING CRUISE, OIL PRESSURE LOW ANNUNCIATOR ILLUMINATED, OIL PRESSURE GAUGE INDICATED 50 AND SLOWLY DROPPING, CREW SECURED LT ENGINE AND DECLARED AND EMERGENCY AND LANDED. REMOVED AND REPLACED LT GAS GENERATOR, POWER SECTION AND PROPELLER, RIGGED ENGINE, PEROct 14, 2004 · N218YV · Beech 1900D · Engine (Turbine/Turboprop)SDR 58817Knob · unsecureRT BRAKE WILL NOT RELEASE. RESECURED BRAKE PARKING KNOB, LUBED ACT.Feb 13, 2004 · N218YV · Beech 1900D · BrakeSDR 57171Gyro · inoperativeSHORTLY AFTER DEPARTURE FROM PIT CREW NOTICED CAPT'S GYROSCOPIC DIRECTIONAL COMPASS SYSTEM WASN'T WORKING CORRECTLY. SO DECEIDED TO RETURN TO PIT. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. T/S REPAIRED PINS 5 AND 7 OF CONNECTOR J203 AT NR 1 FLUX DETECTODec 18, 2003 · N218YV · Beech 1900D · Directional Gyro and Indicating SystemSDR AMWA65Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED IN ONE PLACE ON THE RIGHT AND ONE PLACE ON THE LEFT SIDE NEAR THE CENTER STRINGER INTERSECTION. REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE TO BMM POct 10, 2003 · N218YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA64Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE RIGHT SIDE NEAR AFT STRINGERS INTERSECTION REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03.Oct 10, 2003 · N218YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA63Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 54.026 WAS FOUND CRACKED IN THREE PLACES ON THE RIGHT SIDE NEAR THE FORWARD, CENTER AND AFT STRINGERS AND TWO PLACES ON THE LEFT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCOct 10, 2003 · N218YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 048076Keel · gougedWHILE DOING AN INSPECTION, MAINTENANCE DISCOVERED THE LT INBOARD MAIN LANDING GEAR KEEL WAS GOUGED. MAINTENANCE REPAIRED THE KEEL. NO TEARDOWN REPORT WILL BE REQUIRED.Feb 21, 2003 · N218YV · Beech 1900D · Fuselage Main, KeelSDR AMWA13Spar Cap · chafedUPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT SPAR CAP WAS CHAFING THE WHEEL WELL. BLENDED THE CHAFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED.Feb 16, 2003 · N218YV · Beech 1900D · Wing SparSDR 047632Tube · crackedUPON APPROACH FOR LANDING ON FLIGHT 5441 IN CHARLOTTE NORTH CAROLINA, THE LEFT ENGINE TORQUE FELL TO BETWEEN 0-500LBS. ALL THE OTHER ENGINE INDICATIONS WERE NORMAL. THE CREW THEN SHUT DOWN THE ENGINE. THE CREW ALSO DID THE EMERGENCY CHECKLIST AND DECLARED AN EFeb 6, 2003 · N218YV · Beech 1900D · Engine Bleed Air SystemSDR MASA98144Cowling · looseFLT 5499 - JAX-MCO - ON APPROACH, THE CREW NOTICED THE RT PROP PITCH CHANGING UNCOMMANDED. THEY THEN NOTICED THE RT TOP COWLING WAS COMING LOOSE, AND WAS RESTING ON THE PROP GOVERNOR AND BETA VALVE. THE CREW DECLARED AN EMERGENCY, SHUT DOWN THE RT ENGINE, ANJul 18, 1998 · N218YV · Beech 1900D · Engine Cowling SystemSDR MASA98131Computer · malfunctionedFLT 5451 - PFN-MCO - ON SHORT FINAL APPROACH TO MCO, CREW RECEIVED A 'TOO LOW GEAR' AURAL WARNING. INITIATED A GO AROUND AND REQUESTED THE RESCUE TRUCKS STANDBY. ALL OTHER GEAR INDICATIONS WERE NORMAL AND THE GPWS DID NOT ACTIVATE ON THE SECOND APPROACH. THJun 25, 1998 · N218YV · Beech 1900D · Ground Proximity SystemSDR MASA98002Pressure Switch · failedPIT/MBS - FLT 5999 - LEFT AUTOFEATHER FAILED ON CLIMB-OUT. MAINTENANCE REMOVED AND REPLACED PRESSURE SWITCH. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)Jan 1, 1998 · N218YV · Beech 1900D · Propeller Controlling System
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