# Service difficulty reports: N143YV, cancelled Oct 6, 2010 A list on [N143YV, cancelled Oct 6, 2010](https://openairdocs.org/deregistered/N143YV-2010-10-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AMWA188150](https://openairdocs.org/sdr/AMWA188150.md): Actuator · malfunctioned · May 20, 2008 · N143YV · Beech 1900D · Landing Gear Actuator > ON APPROACH FOR LANDING, WHEN GEAR WAS EXTENDED, LT MAIN GEAR HAD NO DOWN AND LOCKED INDICATION. CREW COMPLETED EMERGENCY CHECKLIST AND DECLARED EMERGENCY. CREW AND TOWER CONFIRMED GEAR DOWN BUT UNABLE TO TELL IF IT WAS LOCKED. FLIGHT LANDED SAFELY AND TAXIED - [SDR AMWA87499](https://openairdocs.org/sdr/AMWA87499.md): Brake Assy · weak · Sep 17, 2007 · N143YV · Beech 1900D · Landing Gear Brake System > AFTER LANDING, THE NIGHT CREW CALLED MAINT CONTROL TO REPORT CAPT'S BRAKES FELT SPONGY. MAINTENANCE BLED BRAKES AS NEEDED. - [SDR AMWA86534](https://openairdocs.org/sdr/AMWA86534.md): Brake · weak · Aug 8, 2007 · N143YV · Beech 1900D · Landing Gear Brake System > WHEN AIRCRAFT LANDED CREW CALLED MAINT CONTROL AND WROTE BRAKES UP AS BEING SPONGY. MAINTENANCE BLED BRAKES, OPS NORMAL. - [SDR AMW070206033](https://openairdocs.org/sdr/AMW070206033.md): Spar Cap · corroded · Feb 26, 2007 · N143YV · Beech 1900D · Wing Spar > BIO-CORROSION ON RT SPAR CAP FLANGE AT WS124. REPAIRED IAW AERODESIGN ENGINEERING REPORT NR6556-1. - [SDR AMWA080299](https://openairdocs.org/sdr/AMWA080299.md): Valve · malfunctioned · Oct 20, 2006 · N143YV · Beech 1900D · Landing Gear Brake System > ON LANDING THE LT BRAKE PEDAL BLED OFF PRESSURE. THE AIRCRAFT MADE IT TO THE GATE SAFELY WITH NO FURTHER INCIDENT. THE AIRCRAFT WAS THEN FERRIED SO MAINTENANCE COULD ATTEND TO THE PROBLEM. MAINTENANCE THEN REMOVED AND REPLACED THE LT MLG BRAKE LINE, REFLARED - [SDR AMWA080281](https://openairdocs.org/sdr/AMWA080281.md): Brake Cable · worn · Oct 19, 2006 · N143YV · Beech 1900D · Brake > UPON LANDING, THE LT BRAKE BLED OFF PRESSURE. CREW NOTICED THE LT BRAKE WASN'T WORKING. AIRCRAFT MADE IT TO THE GATE WITHOUT FURTHER NOTICE. MAINTENANCE HAD TO DRIVE IN. TO BLEED BRAKES, OPS CHECKED NORMAL. WHEN AIRCRAFT ARRIVED IN MAINTENANCE, MAINTENANCE RE - [SDR AMWA078615](https://openairdocs.org/sdr/AMWA078615.md): Switch · dirty · Jul 25, 2006 · N143YV · Beech 1900D · Propeller Controlling System > RT AUTO FEATHER CYCLED IN AND OUT OF FEATHER ON APPROACH INTO PIT. MAINTENANCE WAS CALLED AND RAN AIRCRAFT, FOUND RT P/L SWITCH INTERMITTENT. CLEANED AND RESEATED CONNECTION. GROUND RAN AIRCRAFT AGAIN, OPS CHECK NORMAL. - [SDR AMWA77207](https://openairdocs.org/sdr/AMWA77207.md): Uplock Switch · out of adjust · Apr 27, 2006 · N143YV · Beech 1900D · Landing Gear Position and Warning > ATER TAKE OFF, CREW ATTEMPTED TO RAISE LANDING GEAR, CREW OBSERVED NO GEAR UP AND LOCKED INDICATION GEAR IND DOWN AND LOCKED CONTINUOSLY W/ GEAR IN TRANSIT ILLUM UNTIL GEAR HANDLE BACK IN DOWN POSITION CREW LANDED IN ART WITH NO FURTHER INCIDENT. MAINTENANCE A - [SDR 77207](https://openairdocs.org/sdr/77207.md): Landing Gear · warning light · Apr 27, 2006 · N143YV · Beech 1900D · Landing Gear Position and Warning > AFTER TAKEOFF, CREW ATTEMPTED TO RAISE LANDING GEAR, CREW OBSERVED NO GEAR UP AND LOCKED INDICATION. GEAR IND DOWN AND LOCKED CONTINUOUSLY W/ GEAR IN TRANSIT ILLUM UNTIL GEAR HANDLE BACK IN DOWN POSITION. CREW LANDED IN ART WITH NO FURTHER INCIDENT. MORE INFO - [SDR 73843](https://openairdocs.org/sdr/73843.md): Brake · weak · Nov 1, 2005 · N143YV · Beech 1900D · Landing Gear Brake System > UPON LANDING, CAPT'S NOTED BOTH BRAKES WEAK WHEN APPLIED. CREW TAXIED TO THE GATE WITH NO FURTHER INCIDENT. PHONED MAINTENANCE CONTROL, OUTSIDE MAINTENANCE WAS CALLED AND BRAKES WERE BLED. OPS CHECK NORMAL. THEREFORE NO PARTS WERE USED. - [SDR 1050812038AMW](https://openairdocs.org/sdr/1050812038AMW.md): Angle · cracked · Aug 24, 2005 · N143YV · Beech 1900D · Fuselage Miscellaneous Structure > AT FS 303 RIGHT HEAVY ANGLE CRACKED. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. - [SDR 1050812038](https://openairdocs.org/sdr/1050812038.md): Structure · corroded · Aug 24, 2005 · N143YV · Beech 1900D · Wing Miscellaneous Structure > LT COLLECTOR TANK CORROSION AND SURFACE CORROSION AROUND DRAINS. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE. - [SDR 71342](https://openairdocs.org/sdr/71342.md): Brake · malfunctioned · Jun 17, 2005 · N143YV · Beech 1900D · Brake > AFTER LANDING IN DUJ AND TAXIING TO GATE WITH NO INCIDENT, CREW CALLED MAINTENANCE TO WRITE UP THE RIGHT BRAKE AS WEAK. MAINTENANCE BLED BRAKE. THEREFORE NO PARTS WERE USED. - [SDR 69761](https://openairdocs.org/sdr/69761.md): Annunciator · illuminated · Mar 15, 2005 · N143YV · Beech 1900D · Airfoil Anti/De-ice System > THE PILOTS TOOK OFF FROM DUJ ABOUT 60NM FROM PKB. ON LAST FLIGHT OF THE DAY CHECKS, NOTICED THAT WHEN THE SURFACE DEICE WAS CYCLED THAT THE TAIL DEICE AND INBOARD WING DEICE ANNUNCIATORS REMAINED ILLUMINATED, ALONG WITH ABNORMAL INDICATIONS ON THE VACUUM AND - [SDR 69268](https://openairdocs.org/sdr/69268.md): Handle · unsecure · Feb 21, 2005 · N143YV · Beech 1900D · Emergency Exits > UPON OST FERRY FLIGHT WALK AROUND INSPECTION, CREW NOTICED EMERGENCY EXIT DOOR 6A EXIT HANDLE PARTIALLY OUT. ADVISED MX CONTROL AND EXPERIENCED NO FURTHER INCIDENT. THE DOOR WAS RESECURED, THEREFORE NO PARTS WERE USED. - [SDR 68657](https://openairdocs.org/sdr/68657.md): Annunciator · illuminated · Jan 23, 2005 · N143YV · Beech 1900D · Door Warning System > AFTER T/O FROM PIT TO DUJ, CARGO DOOR ANNUNCIATOR ILLUMINATED. A/C RETURNED TO FIELD WITH NO FURTHER INCIDENT. NO DAMAGE FOUND ON AIRCRAFT. LOCKED CARGO DOOR AND PRESSURIZED AIRCRAFT. NO DEFECTS NOTED. - [SDR 54885](https://openairdocs.org/sdr/54885.md): Indicator · fluctuates · Oct 2, 2003 · N143YV · Beech 1900D · Engine BMEP/Torque Indicating > DURING TAKE OFF RIGHT TORQUE WENT TO ZERO. TAKE OFF WAS ABORTED AND AIRCRAFT RETURNED TO MAINT. REMOVED AND REAPLCED GAUGE.P/N 114-3800-653 S/N 132. - [SDR 54388AMWA](https://openairdocs.org/sdr/54388AMWA.md): Reservoir · malfunctioned · Sep 14, 2003 · N143YV · Beech 1900D · Hydraulic Reservoir, Main > LANDING GEAR FAILED TO EXT & MANUAL EXTENDED (MSS). REMOVED AND REPLACED HYD RESERVOIR & POWER PACK ASSY TEST NORM. - [SDR 048029](https://openairdocs.org/sdr/048029.md): Engine · leaking · Feb 19, 2003 · N143YV · Beech 1900D · Engine (Turbine/Turboprop) > ON FLIGHT 5427 FROM SHREVEPORT LOUISIANA TO NEW ORLEANS LOUISIANA, UPON TAKE OFF ROLL AT 60-70 KIAS, THE TORQUE SURGED TO MAXIMUM. THE LEFT PROP RPM DROPPED TO APPROXIMATELY 1000-1200 RPM. THE TAKE OFF WAS ABORTED. THE CREW RETURNED THE THE GATE WHERE MAINTENA - [SDR AMWA044664](https://openairdocs.org/sdr/AMWA044664.md): Engine · failed · Nov 1, 2002 · N143YV · Beech 1900D · Engine (Turbine/Turboprop) > THE CREW OF FLIGHT 2500, ABORTED A TAKEOFF AT THE BEGINNING OF THE ROLL WHEN A LOUD BANG WAS HEARD. THE NOISE HAD CAME FROM THE LEFT ENGINE. THE CREW NEVER REACHED TAKEOFF POWER. THE LEFT ENGINE KEPT RUNNING FOR APPROXIMATELY 2-3 MINUTES AFTER THE OCCURRENC - [SDR 99ZZZX828](https://openairdocs.org/sdr/99ZZZX828.md): Indication · malfunctioned · Dec 2, 1998 · N143YV · Beech 1900D · Trailing Flap Position Indicating System > LEB/PHL - FLT 5272 - ON APPROACH TO PHL, CREW REPORTED AN ABNORMAL FLAPS INDICATOR TO THE PHL TOWER. THE TOWER DISPATCHED THE RESCUE EQUIPMENT. CAPTAIN COMPLETED THE ABNORMAL CHECKLIST AND LANDED WITHOUT INCIDENT. MAINTENANCE T/S THE SYSTEM, NO DISCREPANCIE - [SDR 97ZZZX3302](https://openairdocs.org/sdr/97ZZZX3302.md): Attach Bracket · excess wear · Jul 11, 1997 · N143YV · 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 97ZZZX3301](https://openairdocs.org/sdr/97ZZZX3301.md): Attach Bracket · excess wear · Jul 11, 1997 · N143YV · 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. ## 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 = 'N143YV' AND deregistration_id = 'N143YV-2010-10-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N143YV-2010-10-06/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.