N131YV, cancelled Oct 28, 2009
Service difficulty reports · 20
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 = 'N131YV' AND deregistration_id = 'N131YV-2009-10-28' 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR BSAASDR0720Eva Tube · damagedDURING 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 SSDR BSAASDR0719Tube · splitDURING 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 BLESDR BSAASDR0717Tube · damagedTHE 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 BSAASDR0627Switch Actuator · out of adjustDURING 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 ISDR BSAASDR0608Rib · corrodedPITTING 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 68236Brake Assy · icedON 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 FLUIDSDR 65388Switch · failedAFTER TAKE OFF, FLAPS WOULD NOT RETRACT. ACFT RETURNED TO THE FIELD. MAINTENANCE WAS CALLED. REMOVED AND REPLACED FLAP SPLIT FLAP SWITCH.SDR 65355Switch · dirtyAFTER TAKEOFF FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD, MAINTENANCE WAS CALLED. CLEANED FLAP SAFETY SWITCHES.SDR 64468Engine · malfunctionedAFTER 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 60795Annunciator · malfunctionedON 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 SOURCESDR AMWA27Rivet · looseWHILE 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 AMWA26Clip · crackedDURING 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 AMWA25Hinge · crackedDURING 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 048548Gas Generator · failedCREW 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 ENGINESDR 044284Uplock Switch · failedAFTER 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 AIRCRAFSDR MASA97225Switch · dirtyFLT 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 SUBSESDR 97ZZZX3293Attach Bracket · excess wearFLEET 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 97ZZZX3292Attach Bracket · excess wearFLEET 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 95ZZZX4425Actuator · failedHYDRAULIC 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 95ZZZX4424Exhaust Stack · crackedLEFT 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.
Back to N131YV, cancelled Oct 28, 2009