# Service difficulty reports: N131YV, cancelled Oct 28, 2009 A list on [N131YV, cancelled Oct 28, 2009](https://openairdocs.org/deregistered/N131YV-2009-10-28.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR BSAASDR0720](https://openairdocs.org/sdr/BSAASDR0720.md): Eva Tube · damaged · Jun 2, 2007 · N131YV · Beech 1900D · Pneumatic Distribution System > DURING CLIMB TO ALTITUDE, THE RT BLEED AIR FAIL ANNUNCIATOR LIGHT CAME ON AT 12,500FT. CREW FOLLOWED CHECKLIST PROCEDURES, SHUT OFF BLEED ON RIGHT SIDE AND RETURNED TO STATION, LIGHT WENT OUT AT 8,000FT DURING RETURN TO STATION. INITIALLY DEFERRED RT BLEED S - [SDR BSAASDR0719](https://openairdocs.org/sdr/BSAASDR0719.md): Tube · split · Jun 2, 2007 · N131YV · Beech 1900D · Pneumatic Distribution System > DURING CLIMB TO ALTITUDE, THE RT BLEED AIR FAIL ANNUNCIATOR LIGHT CAME ON AT 16,800FT. CREW FOLLOWED CHECKLIST PROCEDURES, SHUT OFF BLEED ON RIGHT SIDE AND RETURNED TO STATION, LIGHT WENT OUT AT 7,000FT DURING RETURN TO STATION. INITIALLY DEFERRED THE RT BLE - [SDR BSAASDR0717](https://openairdocs.org/sdr/BSAASDR0717.md): Tube · damaged · May 31, 2007 · N131YV · Beech 1900D · Pneumatic Distribution System > THE RIGHT BLEED AIR FAIL LIGHT CAME ON. CREW WAS CLOSEST TO DESTINATION, AND LANDED WITHOUT INCIDENT. FOUND & REPLACED DAMAGED EVA TUBING UNDER RT WING PANEL 611 NEAR NACELLE. SYSTEM OPS CHECK & LEAK CHECK GOOD. - [SDR BSAASDR0627](https://openairdocs.org/sdr/BSAASDR0627.md): Switch Actuator · out of adjust · Dec 28, 2006 · N131YV · Beech 1900D · Door Warning System > DURING CLIMBOUT APPROXIMATELY 30 MINUTES INTO THE FLIGHT, THE CABIN DOOR WARNING LIGHT CAME ON. CREW FOLLOWED CHECKLIST PROCEDURES & RETURNED TO STATION. DISCREPANCY WAS INITIALLY DEFERRED IAW MEL 52-1 AFTER IT WAS DETERMINED THAT THE INDICATION SYSTEM WAS I - [SDR BSAASDR0608](https://openairdocs.org/sdr/BSAASDR0608.md): Rib · corroded · Feb 28, 2006 · N131YV · Beech 1900D · Wing, Rib/Bulkhead > PITTING CORROSION WAS FOUND ON THE RIGHT WING INBOARD MILLED RIB ON THE LOWER FLANGE ADJACENT, BUT NOT AFFECTING, THE RIVET HOLE INBOARD OF THE WING DRAIN LOCATED JUST OUTBOARD OF THE NACELLE IN THE WING LEADING EDGE. THE DAMAGE AREA IS APPROXIMATELY.3 INCH - [SDR 68236](https://openairdocs.org/sdr/68236.md): Brake Assy · iced · Jan 5, 2005 · N131YV · Beech 1900D · Brake > ON TAXI OUT, A/C SLOWED TO A STOP ON THE ACTIVE TAXI WAY ENTERING THE RUNWAY AND WOULD NOT PROGRESS FWD. MX REMOVED ICE FROM THE BRAKES, A/C THEN WAS ABLE TO MOVE AND RETURNED TO GATE WITH NO FURTHER INCIDENT. CLEANED LEFT AND RIGHT BRAKES WITH DEICING FLUID - [SDR 65388](https://openairdocs.org/sdr/65388.md): Switch · failed · Sep 28, 2004 · N131YV · Beech 1900D · Trailing Edge Flap Control System > AFTER TAKE OFF, FLAPS WOULD NOT RETRACT. ACFT RETURNED TO THE FIELD. MAINTENANCE WAS CALLED. REMOVED AND REPLACED FLAP SPLIT FLAP SWITCH. - [SDR 65355](https://openairdocs.org/sdr/65355.md): Switch · dirty · Sep 27, 2004 · N131YV · Beech 1900D · Trailing Edge Flap Control System > AFTER TAKEOFF FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD, MAINTENANCE WAS CALLED. CLEANED FLAP SAFETY SWITCHES. - [SDR 64468](https://openairdocs.org/sdr/64468.md): Engine · malfunctioned · Aug 31, 2004 · N131YV · Beech 1900D · Engine (Turbine/Turboprop) > AFTER TAKEOFF CREW TURN ON BLEED MODE MAN COOL. CAPTAIN NOTED ITT WAS CLIMBING AT 780C. TORQUE HAD DROPPED TO 2500LB. TEMP STABILIZED BUT TORQUE CONTINUED TO DROP. THEN IT GOT TO 2000LB CREW DECLARED EMERGENCY AND RETURNED TO FIELD. LANDED SAFELY WITH NO - [SDR 60795](https://openairdocs.org/sdr/60795.md): Annunciator · malfunctioned · Apr 23, 2004 · N131YV · Beech 1900D · Landing Gear Position and Warning > ON APPROACH TO DRO WHEN GEAR WAS EXTENED. 3 GREENS WOULD NOT ILLUM LANDING GEAR IND C.B. POPPED GREEN NOTIFIED. MX CTRL ADVISED TO RETURN TO FMN. AIRCRAFT THEN RETURNED TO FMN DECLARED EMERGENCY AND LANDED WITH NO FURTHER INCIDENT. R & R ANNUNCIATOR PWR SOURCE - [SDR AMWA27](https://openairdocs.org/sdr/AMWA27.md): Rivet · loose · Jul 24, 2003 · N131YV · Beech 1900D · Fasteners > WHILE PERFORMING AN ABC STRUCTURAL INSPECTION, TWO RIVETS WERE FOUND TO BE LOOSE ON THE RIGHT SIDE OF THE FUSELAGE AT APPROXIMATELY FS 220.75, STRINGER 5R. REPAIR ACCOMPLISHED. NO TEAR DOWN REPORT WILL BE REQUIRED. - [SDR AMWA26](https://openairdocs.org/sdr/AMWA26.md): Clip · cracked · Jul 24, 2003 · N131YV · Beech 1900D · Fuselage Miscellaneous Structure > DURING ABC CHECK, A RIGHT HAND CLIP WAS FOUND CRACKED. REPLACED CLIP IN ACCORDANCE WITH BEECH SRM 53-90-23. NO TEAR DOWN REPORT WILL BE REQUIRED. - [SDR AMWA25](https://openairdocs.org/sdr/AMWA25.md): Hinge · cracked · Jul 24, 2003 · N131YV · Beech 1900D · Fuselage, Door Hinge > DURING ABC CHECK, THE CARGO DOOR HINGE WAS FOUND CRACKED. REPLACED HINGE IN ACCORDANCE WITH BEECH SRM 52-90-01. NO TEAR DOWN REPORT WILL BE REQUIRED. - [SDR 048548](https://openairdocs.org/sdr/048548.md): Gas Generator · failed · Mar 7, 2003 · N131YV · Beech 1900D · Turbine Engine Compressor Section > CREW WAS ON TAKE OFF ROLL WHEN POWER WAS APPLIED TO THE NR 2 ENGINE. THE CREW HEARD A LOUD BANG FROM THE RIGHT SIDE OF THE AIRCRAFT. THEY ABORTED THE TAKE OFF AND TAXIED BACK DOWN TO THE GATE. THEY PROCEEDED TO PERFORM A CHECKLIST BY VISUALLY INSPECTING ENGINE - [SDR 044284](https://openairdocs.org/sdr/044284.md): Uplock Switch · failed · Oct 22, 2002 · N131YV · Beech 1900D · Main Landing Gear > AFTER TAKE OFF FROM ENID OKLAHOMA TO DENVER COLORADO ON FLIGHT 2501, THE CREW RETRACTED THE LANDING GEAR AFTER A POSITIVE RATE OF CLIMB WAS ESTABLISHED. WHEN THE GEAR WAS SELECTED UP, THE GEAR TRANSIT INTRANSIT LIGHT WOULD NOT EXTINGUISH. THEREFORE THE AIRCRAF - [SDR MASA97225](https://openairdocs.org/sdr/MASA97225.md): Switch · dirty · Nov 16, 1997 · N131YV · Beech 1900D · Door Warning System > FLT 5323 - BOSPQI - CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. PILOT DECLARED AN EMERGENCY AND AIRCRAFT DIVERTED TO MHT. ONCE ON THE GROUND VERIFIED DOOR CLOSED AND MAINTENANCE ACTION WAS DEFERRED PER MEL 5202. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSE - [SDR 97ZZZX3293](https://openairdocs.org/sdr/97ZZZX3293.md): Attach Bracket · excess wear · Jul 11, 1997 · N131YV · 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 97ZZZX3292](https://openairdocs.org/sdr/97ZZZX3292.md): Attach Bracket · excess wear · Jul 11, 1997 · N131YV · 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 95ZZZX4425](https://openairdocs.org/sdr/95ZZZX4425.md): Actuator · failed · Jul 12, 1995 · N131YV · Beech 1900D · Landing Gear Actuator > HYDRAULIC MAIN GEAR ACTUATOR ON RIGHT MAIN GEAR LEAKING FLUID FROM THREADED PISTON HOUSING NEAR FORWARD BOSS. REMOVED AND REPLACED MAIN GEAR ACTUATOR WITH NEW SERVICEABLE ACTUATOR PER BEECH MM, OPERATIONAL AND LEAK CHECK GOOD. - [SDR 95ZZZX4424](https://openairdocs.org/sdr/95ZZZX4424.md): Exhaust Stack · cracked · Jul 12, 1995 · N131YV · Beech 1900D · Engine Collector/Tailpipe/Nozzle > LEFT ENGINE OUTBOARD EXHAUST STACK CRACKED ABOUT 1.50 INCHES LONG AT BLAST TUBE EXHAUST PORT. CRACK AT WELD BEAD PROGRESSING CIRCUMFERENTIALLY AROUND TUBE. REMOVED AND REPLACED EXHAUST STACK. ## 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 = 'N131YV' AND deregistration_id = 'N131YV-2009-10-28' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N131YV-2009-10-28/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.