N242YV, cancelled Aug 16, 2011

Service difficulty reports · 18

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 = 'N242YV' AND deregistration_id = 'N242YV-2011-08-16'
  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 AMWA88632Control Panel · failedALL (3) BUSS TIE ENUNCIATORS ILLUMINATED IN FLIGHT, REQUIRING MANUAL EXTENSION OF LANDING GEAR AND EMERGENCY LANDING. MAINTENANCE REPLACED LT DC POWER PANEL AND CLEARED DISCREPANCY.Nov 17, 2007 · N242YV · Beech 1900D · Landing Gear Position and WarningSDR AMWA84414Motor · loosePILOT REPORTED FLAPS INOPERATIVE. SUBSEQUENT INVESTIGATION BY MAINTENANCE PERSONNEL FOUND THAT THE FLAP MOTOR MOUNTING SCREWS (2 EA) HAD COME LOOSE AND BACKED OUT OF THE FLAP GEARBOX ASSEMBLY. FLAP MOTOR, GEARBOX, AND HARDWARE WERE REMOVED FROM AIRCRAFT AND May 5, 2007 · N242YV · Beech 1900D · Trailing Edge Flap Control SystemSDR AMW1061104009Rivet · shearedFOUND SHEARED RIVETS ON LT WING AFT SPAR, FORWARD + AFT FLANGE AT W.S. 115.5 AND STRETCHED RIVETS ON BOTH FORWARD AND AFT FLANGE FROM WS 115 TO 123.5. FOUND DURING SERVICE BULLETIN: 57-3815. RIVETS REMOVED, EDDY CURRENT PERFORMED. HOLES REAMED AND LOCK FASTENNov 10, 2006 · N242YV · Beech 1900D · Wing SparSDR AMW1061019035Seat Track · wornSEAT TRACK WORN AND GOUGED. REPAIR COMPLIED WITH IAW MFG FR-CO-00532, FR-CO-00216, FR-CO-01271, FR-CO-1303, FR-CO-01365.Nov 9, 2006 · N242YV · Beech 1900D · Fuselage, Seat/Cargo Attach FittingsSDR 75059Brake Pads · malfunctionedUPON ARRIVING INTO DUJ, THE CREW CALLED IN AND WROTE UP THE BRAKES AS BEING SPONGY. MAINTENANCE THEN CHANGED LEFT I/B BRAKE ASSY, AND BLED ALL BRAKES.Jan 2, 2006 · N242YV · Beech 1900D · Landing Gear Brake SystemSDR 69805Line · brokenON CLIMBOUT NR 1 PROP RPM DECREASED WITH NO PROP LEVER INPUT. PLACED PROP TO FULL RPM POSITION & RPM DECREASE. TRIED TO MATCH RPM ON BOTH ENG, STOPPED WHEN NR 2 GOOD ENG WAS 1300 RPM. ENG HAD OUT OF SYNC PROP BEAT, ACFT YAWING. TORQUE ON NR 1 ENG ROSE, RPMMar 16, 2005 · N242YV · Beech 1900D · Fuel Controlling SystemSDR 66391Hydraulic Line · looseRIGHT BRAKES ARE WEAK. TIGHTENED LINE ON THE HYDRAULIC LINE AFT ON LANDING GEAR AND BLED BRAKES.Nov 2, 2004 · N242YV · Beech 1900D · Hydraulic System, MainSDR 54987Indicator · fluctuatesON TAKE OFF CREW NOTICED A 4O TO 50 KNT SPLIT BETWEEN THE CPT AND FO AIRSPEED IND. FO READING LOW DREW ABORTED TAKEOFF AND RETURNED TO GATE.Oct 6, 2003 · N242YV · Beech 1900D · Airspeed/Mach IndicatorSDR 52413Engine · malfunctionedON FLIGHT 5496, THE AIRCRAFT UPON REACHING CRUISE ALTITUDE NOTED LT ENGINE TORQUE HAD INCREASED ABOVE LIMITATIONS (4500 TO 4600 LBS FOR ABOUT 10 SECONDS). THE CREW THEN EXECUTED A PRECAUTIONARY SHUT OFF OF LEFT ENGINE AND RETURNED TO FIELD. THEY LANDED SAFELJul 9, 2003 · N242YV · Beech 1900D · Engine (Turbine/Turboprop)SDR 050683Rod · disconnectedWHILE EN ROUTE ON FLIGHT 5598 FROM MORGANTOWN PENNSYLVANIA TO PITTSBURGH PENNSYLVANIA, THE RIGHT ENGINE DISPLAYED RAPIDLY INCREASING AND UNCONTROLLABLE RISE IN TORQUE AND FUEL FLOW. THE CREW EVALUATED THE SITUATION AND AGREED TO PERFORM A PRECAUTIONARY ENGINEMay 14, 2003 · N242YV · Beech 1900D · Fuel Controlling SystemSDR 049569Wire · brokenWHILE ON APPROACH ON FLIGHT 5478 FROM PHILADELPHIA PENNSYLVANIA TO ITHACA NEW YORK, THE LANDING GEAR FAILED TO EXTEND ON NORMAL EXTENSION. AFTER THE CREW PERFORMED AND EMERGENCY EXTENSION ALL THREE GREEN GEAR INDICATIONS WERE GOOD. THE AIRCRAFT LANDED WITH NO Apr 7, 2003 · N242YV · Beech 1900D · Landing Gear Position and WarningSDR 047205Switch · dirtyAFTER DEPARTING, THE CREW HAD THE PASSENGER DOOR ANNUNCIATOR ILLUMINATE. THE CREW THEN DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED THE SWITCHES. NO PARTS WERE USED. TEARDJan 24, 2003 · N242YV · Beech 1900D · Door Warning SystemSDR 98ZZZM899Skin · crackedOVERNIGHT MAINTENANCE IN ICT, FOUND TWO .5 INCH CRACKS IN BOTTOM SKIN EXTENDING FROM TWO ADJACENT RIVETS ON THE CENTER SPAR ON THE LEFT OUTBOARD FLAP. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M)Apr 3, 1998 · N242YV · Beech 1900D · Trailing Edge FlapsSDR 98ZZZM892Skin · crackedOVERNIGHT MAINTENANCE ICT, FOUND .5 INCH CRACK IN THE RT OUTBOARD FLAP TE 7 INCH FROM INBOARD END. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M)Apr 3, 1998 · N242YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM967Seat · crackedAT ICT, AN OVERNIGHT INSPECTION FOUND THAT SEATBACK 5F WAS BROKEN. REMOVED AND REPLACED SEAT BACK IAW MM 25-20. REPAIRED SEATBACK PER STANDARD PRACTICES. (M)Aug 15, 1997 · N242YV · Beech 1900D · Passenger Compartment EquipmentSDR 97ZZZM962Dovetail · crackedDURING AN ICT OVERNIGHT MAINTENANCE INSPECTION, RIGHT DOVE TAIL FOUND TO BE CRACKED. REPAIR IAW WITH BEECHCRAFT SRM 51-00 AND TO 1900-00-0001. (M)Jul 20, 1997 · N242YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX4238Skin · crackedTHE LEFT OUTBOARD FLAP HAS A 1.50 INCH CRACK ON THE LEADING EDGE. STOP DRILLED AND INSTALLED DOUBLER IAW AMWA T.O. 1900-27-00-0001. (X)Jun 25, 1997 · N242YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX2777Wheel Assy · crackedDURING REPLACEMENT OF TIRE, MAINTENANCE NOTICED THE INBOARD HALF OF THE WHEEL ASSY HAD A 8.5 INCH CRACK IN THE TIRE BEAD AREA.Apr 28, 1997 · N242YV · Beech 1900D · Wheel/Ski/Float
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