# Service difficulty reports: N135YV, cancelled Oct 5, 2010 A list on [N135YV, cancelled Oct 5, 2010](https://openairdocs.org/deregistered/N135YV-2010-10-05.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AMWA89766BC](https://openairdocs.org/sdr/AMWA89766BC.md): Battery · discharged · Jan 24, 2008 · N135YV · Beech 1900D · Battery/Charger System > AFTER TAKEOFF, BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY. - [SDR AMWA89557BC](https://openairdocs.org/sdr/AMWA89557BC.md): Battery · discharged · Jan 10, 2008 · N135YV · Beech 1900D · Battery/Charger System > BATTERY CHARGE ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY. - [SDR AMWA89551BC](https://openairdocs.org/sdr/AMWA89551BC.md): Gcu · malfunctioned · Jan 10, 2008 · N135YV · Beech 1900D · DC Generating System > DURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT PARALLELED BOTH GCU'S AND CLEARED DISCREPANCY. - [SDR AMWA107120502](https://openairdocs.org/sdr/AMWA107120502.md): Doubler · chafed · Dec 7, 2007 · N135YV · Beech 1900D · Wing Miscellaneous Structure > AFT 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. - [SDR 2007FA0000467](https://openairdocs.org/sdr/2007FA0000467.md): Skin · damaged · Mar 16, 2007 · N135YV · Beech 1900D · Vertical Stabilizer, Plate/Skin > VERTICAL 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 WORKED - [SDR AMW1070126025](https://openairdocs.org/sdr/AMW1070126025.md): Bolt · bent · Jan 29, 2007 · N135YV · Beech 1900D · Rudder Control System > WHILE 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, - [SDR AMW78361](https://openairdocs.org/sdr/AMW78361.md): Wire · chafed · Jul 11, 2006 · N135YV · Beech 1900D · Flight Control System Wiring > CREW 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 NOR - [SDR AMW78340](https://openairdocs.org/sdr/AMW78340.md): Cable · inoperative · Jul 10, 2006 · N135YV · Beech 1900D · Passenger/Crew Doors > AFTER 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 DEF - [SDR AMW78333](https://openairdocs.org/sdr/AMW78333.md): Cable Assy · misrigged · Jul 9, 2006 · N135YV · Beech 1900D · Entrance Stairs > AIRSTAIR 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 C - [SDR 76460](https://openairdocs.org/sdr/76460.md): Windshield · broken · Mar 20, 2006 · N135YV · Beech 1900D · Flight Compartment Windows > CAPT'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. - [SDR 1050902038](https://openairdocs.org/sdr/1050902038.md): Intercostal · cracked · Sep 19, 2005 · N135YV · Beech 1900D · Fuselage Miscellaneous Structure > INTERCOSTAL ABOVE CARGO DOOR CRACKED AT FS 468, 482 AND 495. MAINTENANCE WAS DOING A STRUCTURAL REPAIR. - [SDR 65672](https://openairdocs.org/sdr/65672.md): Handle · unsecure · Oct 8, 2004 · N135YV · Beech 1900D · Emergency Exits > PREFLIGHT 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. - [SDR 60796](https://openairdocs.org/sdr/60796.md): Wire · damaged · Apr 23, 2004 · N135YV · Beech 1900D · Landing Gear System Wiring > WITH 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 TB - [SDR 52531](https://openairdocs.org/sdr/52531.md): Gas Generator · failed · Jul 13, 2003 · N135YV · Beech 1900D · Turbine Section > ON 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 IN - [SDR MASA99159](https://openairdocs.org/sdr/MASA99159.md): Switch · malfunctioned · Sep 24, 1999 · N135YV · Beech 1900D · Autopilot System > FLT 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 OU - [SDR MASA97157](https://openairdocs.org/sdr/MASA97157.md): Downlock Switch · out of adjust · Sep 21, 1997 · N135YV · Beech 1900D · Landing Gear Position and Warning > AIRSHUTTLE 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 SWIT - [SDR 97ZZZX3226](https://openairdocs.org/sdr/97ZZZX3226.md): Attach Bracket · excess wear · Jul 11, 1997 · N135YV · Beech 1900D · Trailing Edge Flaps > FLEET 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. - [SDR 97ZZZX3225](https://openairdocs.org/sdr/97ZZZX3225.md): Attach Bracket · excess wear · Jul 11, 1997 · N135YV · Beech 1900D · Trailing Edge Flaps > FLEET 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. - [SDR 95ZZZX4167](https://openairdocs.org/sdr/95ZZZX4167.md): Skin · delaminated · Jun 3, 1995 · N135YV · Beech 1900D · Wing, Plate/Skin > DURING 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 PAN ## 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 = 'N135YV' AND deregistration_id = 'N135YV-2010-10-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N135YV-2010-10-05/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.