N165YV
Service difficulty reports · 60
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 = 'N165YV' AND registry_match = 'registration' 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 = 'N165YV' AND registry_match = 'registration' 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 GLBA2017083100683Snubber · inoperativeMAINTENANCE REPORTED THAT THE CABIN DOOR FREE FALLS OPEN. REMOVED & REPLACED CABIN DOOR SNUBBER IAW MM 52-10-01. OPS CHECKED GOODSDR GLBA2017082800682Rib · crackedMAJOR REPAIR - MAINTENANCE REPORTED THAT THE LEFT HAND ELEVATOR'S OUTBOARD MOUNT BRACKET IS LOOSE AND BOTH ATTACHING RIBS ARE CRACKED. RIVET HOLES ARE CRACKED ON MAIN SPAR WHERE RIBS ATTACH. ELEVATOR WAS REMOVED FOR INSPECTION ON 08/21/17. MAJOR REPAIR DETERMISDR GLBA2017053000663Cable · bentMAINTENANCE REPORTED THAT THE LOWER FORWARD AIRSTAIR DOOR CABLE ROD WAS BENT. REMOVED AND REPLACED THE LOWER FORWARD AIRSTAIR DOOR HANDRAIL CABLE IAW BMM 52-10-02, OPS CHECKED GOOD.SDR GLBA2016082400606Trim Panel · unsecurePILOT REPORTED THAT THE AIRSTAIR DOOR AFT TRIM IS LOOSE AND BINGING THE DOOR, PREVENTING THE DOOR FROM OPENING. MAINTENANCE REPLACED THE NUTS AND SECURED THE TRIM PIECE, DOOR OPERATES NORMALLY.SDR GLBA2015092900550Clevis · bentDURING A MX INSPECTION, FOUND THAT THE AIRSTAIR DOOR LOWER FWD HANDRAIL CABLE CLEVIS WAS BENT. R & R THE CABLE ASSEMBLY IAW BMM 52-10-02. PN ON & OFF 1440-43GLA.SDR GLBA2015091600537Tire · blownTHE NR 1 TIRE BLEW ON LANDING. THE TIRE DEVELOPED A FLAT SPOT DURING BRAKING THAT RESULTED IN LOSS OF TIRE PRESS. R & R THE NR 1 WHEEL ASSEMBLY IAW TC 1900-3240.00. PN 5006028-5, SN ON 1325, SN OFF 1681. OK FOR CONTINUED SERVICE.SDR GLBA2015022700500Master Cylinder · wornPILOT REPORTED THAT THE LT BRAKE WAS INOPERATIVE FROM THE CAPTAIN SEAT, EXTREMELY SOFT FROM THE FIRST OFFICER SEAT. REPLACED O RINGS ON THE SWIVEL FITTINGS ON THE NR 1 BRAKE. REPLACED THE CAPTAINS LT MASTER CYLINDER IAW BMM 32-40-06. OPERATIONS CHECK & LEAKSDR GLBA2014120100474Cam Lock · lack of lubePILOT REPORTED THAT THE MAIN CABIN DOOR HANDLE IS VERY DIFFICULT TO MOVE WHEN THE DOOR IS BROUGHT TO THE CLOSED POSITION, HANDLE IN NORMAL FASHION WITH DOOR OPEN. LUBRICATED THE CAM LOCKS OPERATIONS CHECKED GOOD IAW BMM 12-20-00, OPERATIONS CHECKED GOOD.SDR GLBA2014092200444Skin · dentedMAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND DENT IN THE VERT STAB LE, DENT AREA BEGINS AT CSS 54.026, JUST ABOVE RIB UPWARD TO CSS 66.00, DEPTH APPROX .5 INCHES TO .75 INCHES, ALLOWING FOR ORIGINAL CONTOUR AT LE. REPAIRED THE AFFECTED AREA & SDR GLBA2014092200445Structure · crackedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT FWD VERT STAB HAT SECTION AT FWD FLANGE BEND RADIUS, .20% CHORD & VSS 90.0, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-55-009. MATERIASDR GLBA2014091900442Rib · crackedMAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT WING INBD RIB AT JUNCTION WITH WING SPAR FS 288, RIB ANGLE DOUBLER CRACKED 1.1 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-190SDR GLBA2014091900440Frame · crackedMAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE FUSELAGE FRAME CHANNEL AT FS 177.35 & STRINGER 13L IN THE FRAME FLANGE BEND RADIUS, .7 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 1SDR GLBA2014091900441Frame · crackedMAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT FUSELAGE FRAME AT FS 177.35 & STRINGER 9AR RADIATING UPWARD FROM STRINGER 9AR CUT OUT, .5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IASDR V0DR20140908002Wheel · crackedRECEIVED VENT BLOWER IN FOR OVERHAUL. THE TECHNICIAN WAS REASSEMBLING THE VENT BLOWER, AFTER GETTING THE BLOWER ASSEMBLY TOGETHER HE PREPARED THE VENT BLOWER TO RUN IN THE BRUSHES. NOTED THAT WITH POWER APPLIED TO THE VENT BLOWER A NOISE, FAINT, WAS HEARD UPSDR V0DR20140908001O-Ring · deterioratedCUSTOMER REPORTED POSSIBLE OIL COMING FROM PROPELLER HUB & BLADE SOCKETS. RECEIVED PROPELLER ASSEMBLY IN, PRIOR TO DISASSEMBLY TECHNICIANS APPLIED PRESS FOR TROUBLESHOOTING PURPOSES, BUT NO DROP IN AIR PRESS WAS NOTED. THE TECHNICIANS PROCEEDED TO DISASSEMBLSDR GLBA2013082300302Handle · unsecurePILOT REPORTED THAT THE OUTSIDE HANDLE ON OVERWING EXIT 4C DOES NOT STAY SECURE IN FLIGHT. MX RESECURED THE OUTSIDE DOOR HANDLE. OPS CHECK GOOD REF BMM 52-20-00-201. LATER THAT DAY MX REEXAMINED DURING SCHEDULED MX, NOTING THAT EMERGENCY EXIT 4C EXTERIOR HANDSDR GLBA2013082300301Handle · unsecurePILOT REPORTED THE 4C OUTER HANDLE ON THE OVERWING EXIT IS POPPED. MX SECURED THE EMERGENCY EXIT OUTER HANDLE. OPS CHECKED GOOD REF BMM 52-20-00-201.SDR GLBA2013062400264Motor · odorPILOT REPORTED THAT THEY SMELLED ELECTRICAL SMOKE IN THE AFT CABIN DURING SHUTDOWN. REPLACED THE FLAP MOTOR, SYS OPS CHECKED GOOD, NO BURNING ODOR NOTED.SDR GLBA2012111400111Bulkhead · gougedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A GOUGE IN THE UPPER PRESSURE BULKHEAD AT FS 84.00 AT ANGLE ATTACH AREA ABOVE CENTER AVIONICS SHELF, TORN IN A TRIANGLE SHAPE 1.35",.8",.7". MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-069.SDR GLBA2012111200106Bulkhead · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND SEVEN CRACKS IN THE RT FWD PRESSURE BULKHEAD AT FASTENERS, THE OTBD ROW TO DOUBLE ROW TO FASTENERS AT THE INBD EDGE OF BULKHEAD, 2.375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-068.SDR GLBA2012051601Actuator · inoperativePILOT REPORTED LANDING GEAR FAILED TO EXTEND NORMALLY, PERFORMED MANUAL EXTENSION, DECLARED EMERGENCY, LANDED SAFELY. MX MEGGED WIRING FROM TB150 TO ALL ACTUATORS, HANDLE TO PCB A316 AND TO SERVO VALVE, ALL CHECKED GOOD, R & R RT ACTUATOR, IAW TC 1900-3230-10SDR GLBA2012051401Actuator · inoperativePILOT REPORTED THAT THE LANDING GEAR FAILED TO EXTEND NORMALLY, PERFORMED MANUAL EXTENSION, DECLARED AN EMERGENCY, LANDED SAFELY. MX WAS ABLE TO DUPLICATE PROBLEM, REPLACED RT MLG ACTUATOR. REF TC 1900-3230.10, OPS CHECKED GOOD.SDR GLBA2012051101Powerpack · malfunctionedPILOT REPORTED ON APPROACH, LANDING GEAR WOULD NOT EXTEND, DECLARED AN EMERGENCY, MANUALLY PUMPED GEAR DOWN, 3 GREENS, LANDED SAFELY. MX REPLACED THE HYD POWER PACK IAW BMM 32-30-04.SDR GLBA2012050701Wire · damagedPILOT REPORTED THAT WHEN THEY TURNED ON THE MASTER PANEL LIGHT SWITCH, NOTICED AN ELECTRICAL BURNING ODOR, NO SMOKE NOTED, TURNED SWITCH OFF, ODOR WENT AWAY. MX REPAIRED A WIRE ON THE PROPELLER AMP INDICATOR, NO ODOR NOTED.SDR GLBA20110912GAnnunciator · inoperativePILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR DID NOT ILLUMINATE WITH THE PRESS-TO-TEST. MAINTENANCE REPLACED THE AUTOFEATHER ANNUNCIATOR, OPS CHECKED GOOD.SDR GLBA20110805HSeal · out of positionPILOT REPORTED THAT THE EMERGENCY EXIT DOOR AT 4C MAKES A LOUD SOUND DURING FLIGHT. MX REMOVED 4C EMER EXIT DOOR AND FOUND TRIM SEAL MISPLACED, REPOSITIONED SEAL AND INSTALLED EXIT DOOR IAW BMM 52-20-00, PRESURIZED ACFT IAW BMM 21-30-00, NO DEFECTS NOTED.SDR GLBA20110805GBulb · inoperativePILOT REPORTED THAT THE LIGHT IN THE AS DOOR WINDOW DOES NOT COME ON WHEN PUSHED. MX REPLACED THE BULB IAW BMM 33-20-01, OPS CHECKED GOOD.SDR GLBA20110715FOxygen Mask · stuckPILOT REPORTED THAT WHEN SELECTING EMERGENCY POSITION ON THE CAPT'S O2 MASK, IT WILL NOT MOVE FROM NORMAL POSITION TO 100 PERCENT. MX REPLACED THE MASK PN: 359-62612 SN OFF 9444, SN ON 12065 IAW MM 35-10-00, OPS CK GOOD.SDR GLBA20110706MCable · worn"SUP" - DURING A WALK-AROUND, THE PILOT FOUND THE FWD BOTTOM A/S DOOR CABLE ROD END BENT. MX R & R THE FWD BOTTOM A/S DOOR CABLE IAW BMM 52-10-02, PN: 1440-43GLA.SDR GLBA20110706LPanel · looseDURING AN INSPECTION, THE PILOT FOUND THE EMERGENCY EXIT INTERIOR PANEL LOOSE. MX RESECURED SPRINGS ON EMERGENCY EXIT INTERIOR PANEL BUTTON IAW BMM 52-20-00.SDR GLBA20110630OSwitch · false activationPILOT REPORTED THAT WHILE CLIMBING THROUGH 8,000 FT HAD A CABIN DOOR ANNUNCIATOR ILLUMINATE, NO EMERGENCY DECLARED, RETURN TO BASE. MX CHECKED CABIN DOOR SWITCHES FOR LOOSE CONNECTIONS, LUBRICATED. SWITCHES OPS CHECKED GOOD REF AIM 12-10-0, CHAP 12. REMOVEDSDR GLBA20110601FSkin · debondedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE AS DOOR SKIN DEBONDED FROM FWD TO AFT EDGE FROM THE LWR EDGE, AREA OF 24" BY 6". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-005 SDR GLBA20110601JFrame · crackedDURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND FRAME CRACK AT FS 164 & STRINGER 9AR AT THE STRINGER CUTOUT, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-038. MATERIALS UTILIZED ARE SDR GLBA20110601GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE SKIN AT FS 150 & STRINGER 9AL AT THE LOWER SNUBBER MOUNT AND AS DOOR FUSELAGE FRAME CRACKED AT SNUBBER UP MOUNT NUTPLATE AREA, BOTH 1.3" IN LENGTH. MAINTENANCE REPAIRED THE ASDR GLBA20110601HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE FRAME AT FS 456 AT STRINGER 10R CUTOUT, LWR INBD EDGE, .25" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-037. MATERIALS UTILIZED ASDR GLBA20110405HStringer · bentMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND STRINGER 12L BENT AT FS 47.5, STRINGER 12L BENT 5" FROM FS 47.5 GOING AFT ALONG STRINGER. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-19SDR GLBA201006151Unknown · odorSIG EVENT - CREW AND PASSENGERS SMELT SMOKE FOR APPROX. 15 SECONDS DURING DESCENT INTO OLF, SMELL CLEARED AND NO FURTHER EVIDENCE OF FIRE, SWEPT CABIN, CARGO, AND COCKPIT WITH NO EVIDENCE OF FIRE. MAINTENANCE INSPECTED ENVIRONMENTAL SYSTEM, FOUND NO EVIDENCE OSDR GLBA20090808AAutofeather Sys · malfunctionedRT AUTOFEATHER ARM ANNUNCIATOR DID NOT ARM WHEN POWER APPLIED FOR TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE.SDR GLBA20090410BIndicator · fluctuatesDURING FLIGHT NOTICED 2 PERCENT FLUCTUATION ON NR 1 N 1 GAUGE AND FLUCTUATIONS ON NR 1 TORQUE GAUGE CONTINUED UNTIL SHUTDOWN. MAINTENANCE R & R LT BETA BLOCK AND RIGGED BETA VALVE LOW PITCH STOP PER MM 76-10-00. MAINTENANCE ADDITIONALLY R & R TACH GENERATOR ISDR GLBA20090304ISkin · dentedDURING ROUTINE SHEDULED MAINTENANCE THE LT WING, OUTBOARD LEADING EDGE WAS FOUND DENTED AND REQUIRES REPLACEMENT. REPAIRED LT LEADING EDGE SECTION FROM WS 223-271. WORK PERFORMED PER FR-CO-01895 REV.2. STEPS 1 -15, 16 LEAK CHECK OF AFFECTED AREAS PERFORMESDR GLBA20090227FFuel Tank · damagedMAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE DAMAGE ON THE LEFT AFT AUXILIARY FUEL TANK WALL WAS DISCOVERED. MAINTENANCE REMOVED AFT WALL OF THE LEFT HAND AUX FUEL TANK. FABRICATED NEW, ALODINED AND PRIMED. REINSTALLED AFT WALL PER EO 09-UE165-02.SDR GLBA20090220ASkin · distortedMAJOR REPAIR - LEFT HAND INBOARD WING UPPER AFT WING SKIN OUT OF CONTOUR AT STATIONS F.S. 301 W.S. 70 .022" F.S. 311 W.S. 70 .032", F.S. 319 W.S. 70 .035" F.S. 329 W.S. 70 .035". MAINTENANCE REPLACED LT UPPER INBOARD SKIN IAW E.O.-09-165-01.SDR BSAASDR0710Bypass Valve · malfunctionedINITIAL REPORT - DURING CLIMB, THE RIGHT ENVIR FAIL LIGHT CAME ON, CREW RETURNED TO STATION WITH NO FURTHER INCIDENT. INITIALLY DEFERRED PER MEL 21-4. THE PRECOOLER BYPASS VALVE AND THE PRESSURE REGULATOR VALVE WERE REMOVED AND REPLACED. SYSTEM OPERATIONALSDR BSAASDR0614Skin · corrodedLEVEL 1 SURFACE CORROSION WAS FOUND IN THE LEFT AND RIGHT WINGS IN THE AREA OF THE QUICK DRAINS OUTBOARD OF THE NACELLES AND FORWARD OF THE SPAR AT WS 125 TO 128. CORROSION WAS EVALUATED, DETERMINED TO BE LEVEL 1 SURFACE CORROSION, IT WAS CLEANED OFF, AND THESDR 69959Wire · damagedCREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT. FIRST OFFICER OBSERVED SMOKE FROM AVIONICS BAY AREA. ALL AIRCRAFT SYSTEMS WERE OPERATING NORMALLY. REMOVED AND REPLACED INVERTER. NR 1 INVERTER WIRING AT A226 PANEL BROKEN AND LOOSE CAUSING ARCING. REPAIREDSDR 63379Hydraulic System · lowRECEIVED CALL FROM CAPTAIN HIS LT BRAKE WAS BLEEDING OFF. THEN CALLED MAINTENANCE IN PIT. BLEED LT BRAKE AND SERVICED HYDRAULIC BRAKE GROUND CK GOOD. LEAK CK GOODSDR 63383Brake · lowRECEIVED CALL FROM CREW ABOUT BRAKES FEELING SPONGY. CALLED PIT MAINTENANCE. BLEED LT AND RT BRAKES. SERVICED BRAKE HYDRAULIC RESERVIOR LEAK CK GOOD.SDR 60371Brake · malfunctionedCREW CALLED REPORTING BRAKES FELT SOFT. MAINTENANCE CALLED PIT.SDR 58644Solenoid · wornAFTER ARRIVAL TO PIT ON FLIGHT 5528. RIGHT PROP WENT INTO GROUND FINE. CORRECTIVE ACTION TAKEN R/R LOW PITCH SOLENOID CLEVIS HARDWARE RIGGED.SDR 58596Propeller · out of adjustWHILE TAXIING IN ON FLIGHT 5433, THE RIGHT PROP STUCK IN LOW PITCH. THE AIRCRAFT ARRIVED AT THE GATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE LOW PITCH. NO PARTS WERE USED.
Back to N165YV