N135YV, cancelled Oct 5, 2010

Service difficulty reports · 19

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 = 'N135YV' AND deregistration_id = 'N135YV-2010-10-05'
  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 AMWA89766BCBattery · dischargedAFTER TAKEOFF, BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY.Jan 24, 2008 · N135YV · Beech 1900D · Battery/Charger SystemSDR AMWA89557BCBattery · dischargedBATTERY CHARGE ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY.Jan 10, 2008 · N135YV · Beech 1900D · Battery/Charger SystemSDR AMWA89551BCGcu · malfunctionedDURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT PARALLELED BOTH GCU'S AND CLEARED DISCREPANCY.Jan 10, 2008 · N135YV · Beech 1900D · DC Generating SystemSDR AMWA107120502Doubler · chafedAFT ACM SCREEN ASSEMBLY CHAFING INTO DOUBLER P/N 114-120022-11 IN RT WING CENTER SECTION, WS 67.05. REPAIRED IAW SRM 51-40-02 AND CLEARED DISCREPANCY.Dec 7, 2007 · N135YV · Beech 1900D · Wing Miscellaneous StructureSDR 2007FA0000467Skin · damagedVERTICAL STABILIZER LEADING EDGE SKIN ATTACH RIVETS WORKING. FOUND THAT THE ORIGINAL UNIVERSAL HEAD RIVETS WERE REPLACED WITH FLUSH RIVETS. THE SKIN WAS COUNTERSUNK TO ACCOMMODATE THE RIVETS, HOWEVER THE SKIN WAS TOO THIN TO COUNTERSINK AND EVENTUALLY WORKEDMar 16, 2007 · N135YV · Beech 1900D · Vertical Stabilizer, Plate/SkinSDR AMW1070126025Bolt · bentWHILE PERFORMING THE INSPECTION REQUIREMENTS OF THE RUDDER SYSTEM FOR THE NR 6 DETAIL INSPECTION, IT WAS DISCOVERED THAT THE RUDDER HAD EXCESSIVE UP AND DOWN MOVEMENT. THE FIRST ACTION IS TO CHECK THE TORQUE OF THE RUDDER CONTROL HORN PIVOT BOLT (ITEM NR 312, Jan 29, 2007 · N135YV · Beech 1900D · Rudder Control SystemSDR AMW78361Wire · chafedCREW EXPERIENCED UNCOMMANDED ELECTRIC TRIM MOVEMENT INBOUND TO CNY. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND CHAFED WIRES AT CONNECTOR FOR F/O'S YOKE. REMOVED AND REPLACED THE CONNECTOR AND PINS. ALL OPS CHECKS NORJul 11, 2006 · N135YV · Beech 1900D · Flight Control System WiringSDR AMW78340Cable · inoperativeAFTER ARRIVING, CREW CLOSED PAX DOOR CABLE IN DOOR. WHEN CREW TRIED TO REOPEN DOOR INTERNAL DOOR CABLE BROKE. MAINTENANCE REMOVED AND REPLACED THE DOOR CABLE. WHEN MAINTENANCE WAS REPAIRING THE DOOR THEY FOUND CABIN DOOR ANNUNC SWITCH BROKEN. SYSTEM WAS DEFJul 10, 2006 · N135YV · Beech 1900D · Passenger/Crew DoorsSDR AMW78333Cable Assy · misriggedAIRSTAIR DOOR WILL NOT OPEN FROM INSIDE OR OUT. DISCOVERED BY CREW AFTER AIRCRAFT WAS DEPLANED. THE AIRSTAIR DOOR HANDLE MOVES BUT THE FORWARD CAM LOCKS DO NOT. MAINTENANCE WAS CALLED AND REMOVED AND REPLACED THE FORWARD LOWER AIRSTAIR DOOR CABLE. RIGGED CJul 9, 2006 · N135YV · Beech 1900D · Entrance StairsSDR 76460Windshield · brokenCAPT'S WINDSHIELD SHATTERED IN FLIGHT. NO BIRD WAS SEEN BY EITHER CREW MEMBER. CREW DECLARED AN EMERGENCY AND LANDED AT NECT SUITABLE AIRPORT. MORE INFORMATION TO COME AS IT IS RECEIVED.Mar 20, 2006 · N135YV · Beech 1900D · Flight Compartment WindowsSDR 1050902038Intercostal · crackedINTERCOSTAL ABOVE CARGO DOOR CRACKED AT FS 468, 482 AND 495. MAINTENANCE WAS DOING A STRUCTURAL REPAIR.Sep 19, 2005 · N135YV · Beech 1900D · Fuselage Miscellaneous StructureSDR 65672Handle · unsecurePREFLIGHT INSPECTION REVEALED THAT EMERGENCY EXIT 6F OUTSIDE HANDLE NOT STOWED COMPLETELY. MX STOWED HANDLE A/C RETURNED TO SERVICE. CHECKED DOOR, STOWED LATCH, OPS CK NORMAL.Oct 8, 2004 · N135YV · Beech 1900D · Emergency ExitsSDR 60796Wire · damagedWITH GEAR SELECTED DOWN LT DOWN AND LOCK INDICATOR DID NOT ILLUMINATE. EMERGENCY DECLARED GEAR PUMPED DOWN. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REPAIRED WIRE W/SPLICE IN LT NACELLE TBApr 23, 2004 · N135YV · Beech 1900D · Landing Gear System WiringSDR 52531Gas Generator · failedON FLIGHT 702 FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO, TAKEOFF WAS NORMAL. AS THEY DID THE INITIAL CLIMBOUT, THE CREW RECEIVED A LOW OIL PRESSURE INDICATION (ANNUNCIATOR). THE LEFT ENGINE OIL PRESSURE GAUGE INDICATED A RAPID AND CONTINUOUS DROP INJul 13, 2003 · N135YV · Beech 1900D · Turbine SectionSDR MASA99159Switch · malfunctionedFLT 5347 - BOS-HYA - ON TAXI OUT, THE CREW HEAD A POPPING NOSE COMING FROM THE PEDESTAL. THE RUDDER BOOST YAW DAMP C/B POPPED WHEN THIS HAPPENED AND THIS CAUSED THERE TO BE SPARKS IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE AND MAINTEANCE WAS CALLED OUSep 24, 1999 · N135YV · Beech 1900D · Autopilot SystemSDR MASA97157Downlock Switch · out of adjustAIRSHUTTLE 5945, DUJ-PIT, ON APPROACH, THE PILOT SELECTED GEAR DOWN BUT DID NOT RECEIVE NOSE DOWNLOCK INDICATION THE GEAR UNSAFE WARNING HORN DID SOUND. THE CREW DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE RIGGED THE DOWNLOCK SWITSep 21, 1997 · N135YV · Beech 1900D · Landing Gear Position and WarningSDR 97ZZZX3226Attach 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 · N135YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX3225Attach 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 · N135YV · Beech 1900D · Trailing Edge FlapsSDR 95ZZZX4167Skin · delaminatedDURING AIRCRAFT REPOSITIONING FLIGHT FROM BRADFORD, PA TO JAMESTOWN, NY, PILOT FELT VIBRATION IN AIRFRAME. AIRCRAFT LANDED WITHOUT INCIDENT. DURING POST-FLIGHT INSPECTION, FOUND LT INBOARD WING PANEL (TOP) HAD STARTED TO DELAMINATE. REMOVED AND REPLACED PANJun 3, 1995 · N135YV · Beech 1900D · Wing, Plate/Skin
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