# Service difficulty reports: N242YV, cancelled Aug 16, 2011 A list on [N242YV, cancelled Aug 16, 2011](https://openairdocs.org/deregistered/N242YV-2011-08-16.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AMWA88632](https://openairdocs.org/sdr/AMWA88632.md): Control Panel · failed · Nov 17, 2007 · N242YV · Beech 1900D · Landing Gear Position and Warning > ALL (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. - [SDR AMWA84414](https://openairdocs.org/sdr/AMWA84414.md): Motor · loose · May 5, 2007 · N242YV · Beech 1900D · Trailing Edge Flap Control System > PILOT 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 - [SDR AMW1061104009](https://openairdocs.org/sdr/AMW1061104009.md): Rivet · sheared · Nov 10, 2006 · N242YV · Beech 1900D · Wing Spar > FOUND 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 FASTEN - [SDR AMW1061019035](https://openairdocs.org/sdr/AMW1061019035.md): Seat Track · worn · Nov 9, 2006 · N242YV · Beech 1900D · Fuselage, Seat/Cargo Attach Fittings > SEAT TRACK WORN AND GOUGED. REPAIR COMPLIED WITH IAW MFG FR-CO-00532, FR-CO-00216, FR-CO-01271, FR-CO-1303, FR-CO-01365. - [SDR 75059](https://openairdocs.org/sdr/75059.md): Brake Pads · malfunctioned · Jan 2, 2006 · N242YV · Beech 1900D · Landing Gear Brake System > UPON 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. - [SDR 69805](https://openairdocs.org/sdr/69805.md): Line · broken · Mar 16, 2005 · N242YV · Beech 1900D · Fuel Controlling System > ON 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, RPM - [SDR 66391](https://openairdocs.org/sdr/66391.md): Hydraulic Line · loose · Nov 2, 2004 · N242YV · Beech 1900D · Hydraulic System, Main > RIGHT BRAKES ARE WEAK. TIGHTENED LINE ON THE HYDRAULIC LINE AFT ON LANDING GEAR AND BLED BRAKES. - [SDR 54987](https://openairdocs.org/sdr/54987.md): Indicator · fluctuates · Oct 6, 2003 · N242YV · Beech 1900D · Airspeed/Mach Indicator > ON 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. - [SDR 52413](https://openairdocs.org/sdr/52413.md): Engine · malfunctioned · Jul 9, 2003 · N242YV · Beech 1900D · Engine (Turbine/Turboprop) > ON 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 SAFEL - [SDR 050683](https://openairdocs.org/sdr/050683.md): Rod · disconnected · May 14, 2003 · N242YV · Beech 1900D · Fuel Controlling System > WHILE 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 ENGINE - [SDR 049569](https://openairdocs.org/sdr/049569.md): Wire · broken · Apr 7, 2003 · N242YV · Beech 1900D · Landing Gear Position and Warning > WHILE 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 - [SDR 047205](https://openairdocs.org/sdr/047205.md): Switch · dirty · Jan 24, 2003 · N242YV · Beech 1900D · Door Warning System > AFTER 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. TEARD - [SDR 98ZZZM899](https://openairdocs.org/sdr/98ZZZM899.md): Skin · cracked · Apr 3, 1998 · N242YV · Beech 1900D · Trailing Edge Flaps > OVERNIGHT 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) - [SDR 98ZZZM892](https://openairdocs.org/sdr/98ZZZM892.md): Skin · cracked · Apr 3, 1998 · N242YV · Beech 1900D · Trailing Edge Flaps > OVERNIGHT 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) - [SDR 97ZZZM967](https://openairdocs.org/sdr/97ZZZM967.md): Seat · cracked · Aug 15, 1997 · N242YV · Beech 1900D · Passenger Compartment Equipment > AT 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) - [SDR 97ZZZM962](https://openairdocs.org/sdr/97ZZZM962.md): Dovetail · cracked · Jul 20, 1997 · N242YV · Beech 1900D · Trailing Edge Flaps > DURING 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) - [SDR 97ZZZX4238](https://openairdocs.org/sdr/97ZZZX4238.md): Skin · cracked · Jun 25, 1997 · N242YV · Beech 1900D · Trailing Edge Flaps > THE 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) - [SDR 97ZZZX2777](https://openairdocs.org/sdr/97ZZZX2777.md): Wheel Assy · cracked · Apr 28, 1997 · N242YV · Beech 1900D · Wheel/Ski/Float > DURING REPLACEMENT OF TIRE, MAINTENANCE NOTICED THE INBOARD HALF OF THE WHEEL ASSY HAD A 8.5 INCH CRACK IN THE TIRE BEAD AREA. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N242YV-2011-08-16/reports --- 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.