N176YV

Service difficulty reports · 57

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 = 'N176YV' 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.

SDR AMWA88439BCBattery · failedDURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED THEN WENT OUT. MAINTENANCE REMOVED AND REPLACED BATTERY AND CLEARED DISCREPANCY.Nov 6, 2007 · N176YV · Beech 1900D · Battery/Charger SystemSDR AMWA88091BCBattery · dischargedBATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. BATTERY REPLACED BY MAINTENANCE, DISCREPANCY CLEARED. THIS TYPE ANNUNCIATOR DISCREPANCY IS CONSIDERED A NUISANCE ITEM AND DISTRACTION TO CREW.Oct 18, 2007 · N176YV · Beech 1900D · Battery/Charger SystemSDR AMWA87824Hsi · odorELECTRICAL ODOR REPORTED IN COCKPIT ON CLIMBOUT. RETURNED TO FIELD AND MAINTENANCE VERIFIED THAT PROBLEM ORIGINATING IN CAPTAIN'S EHSI. REMOVED AND REPLACED UNIT, OPERATIONAL CHECK WAS SATISFACTORY.Oct 4, 2007 · N176YV · Beech 1900D · Directional Gyro and Indicating SystemSDR AMWA0828013Spar Cap · corrodedBIO CORROSION LT MAIN SPAR, LWR CAP FROM APPROX WS119.5 TO WS122. REPAIRED IAW REPORT NR 6872 REV IR.Oct 2, 2007 · N176YV · Beech 1900D · Wing SparSDR AMWA0828013BFrame · chafedREPAIRED LT AND RT FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT FS 213.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013JFrame · chafedREPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 408.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013DFrame · chafedREPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT FS 243.25, RT.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013CFrame · chafedREPAIRED LT AND RT FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT FS 228.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013GFrame · chafedREPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 318.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013HFrame · chafedREPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT RT FS 363.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013KFrame · chafedREPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 438.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013IFrame · chafedREPAIRED FUSELAGE FRAMES DAMAGED BY FRICTION CHAFING AT LT AND RT FS 378.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013FFrame · chafedREPAIRED FUSELAGE FRAME DAMAGED BY FRICTION CHAFING AT RT FS 303.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013EFrame · chafedREPAIRED LT AND RT FUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING AT FS 258.25.Oct 2, 2007 · N176YV · Beech 1900D · Fuselage Main, FrameSDR AMWA0828013ASkin · damagedRT UPPER WING SKIN BETWEEN WS117.5 AND WS133 HAD NUMEROUS ELONGATED HOLES FROM OVERSIZED RIVETS. REPAIRED IAW REPORT NR 6878-1 REV IR.Oct 2, 2007 · N176YV · Beech 1900D · Wing, Plate/SkinSDR AMWA84517Annunciator · wornUPON DEPART GEAR RETRACTED NORMALLY. NO PROBLEMS UNTIL GEAR EXTENSION. COULD NOT DETERMINE IF GEAR WAS COMPLETELY DOWN. FLEW BY TOWER AND THEY SAID IT APPEARED ONE OF THE GEAR WAS NOT COMPLETELY DOWN. PERFORMED MANUAL EXTENSION, BURNED OFF ADDITIONAL FUELMay 9, 2007 · N176YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR AWM083022B-Nut · looseWHEN CREW ARRIVED AT DESTINATION THEY CALLED INTO MAINT CONTROL AND WROTE UP THE LT BRAKES NOT GETTING FULL BRAKING ACTION. TIGHTENED B-NUT, CLEANED AND BLED BRAKES, OPS CK NORMAL.Mar 3, 2007 · N176YV · Beech 1900D · Landing Gear Brake SystemSDR AMW082983BCBattery · false indicationWHILE IN FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. CREW PROCEEDED TO DESTINATION, LANDED SAFELY WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS. REMOVED AND REPLACEMar 1, 2007 · N176YV · Beech 1900D · Battery/Charger SystemSDR AMWA82619BCBattery · dischargedBATTERY CHARGE LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY TO CLEAR DISCREPANCY. THIS BATTERY CHARGE LIGHT ILLUMINATION IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTION TO THE PILOTS.Jan 22, 2007 · N176YV · Beech 1900D · Battery/Charger SystemSDR AMW1061218001Sensor · failedDURING A LANDING GEAR RETRACT CHECK, IT WAS NOTICED THAT SPARKS AND SMOKE WAS EMITTING FROM THE LIQUID LOW LEVEL SENSOR INSTALLED ON THE LANDING GEAR POWER PACK. THE SENSOR WAS REPLACED AND NO FURTHER PROBLEMS WERE NOTICED.Dec 12, 2006 · N176YV · Beech 1900D · Landing Gear Position and WarningSDR AMW78306Fuel Cap · missingLT FUEL CAP CAME LOOSE ON CLIMB OUT AND WEDGED IN BETWEEN WING AND AILERON. EXTRA TRIM WAS REQUIRED FOR CLIMB, BUT AILERONS REMAINED FULLY CONTROLLABLE IN FLIGHT. THE CREW RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE WAS CALLED AND PERFORMED AILEJul 7, 2006 · N176YV · Beech 1900D · Fuel StorageSDR 1060607019Web · wornHOLE WORN ON WEB OF LT FIREWALL. LOOSE FASTENER FOUND TO HAVE CAME LOOSE AND WORE OUT THE HOLE. EXTRA CARE HAS BEEN TAKEN TO ENSURE THE FASTENER TO BE CHECKED FOR PROPER TORQUE. HOLE REPAIRED IAW MFG FR-CO-01357 REV 1.Jun 13, 2006 · N176YV · Beech 1900D · Nacelle/Pylon, Bulkhead/FirewallSDR 1060406014ASpar · corrodedBIO CORROSION LT MAIN SPAR CAP FLANGE AT WS 124.588 REPAIRED IAW FIELD REPAIR FR-CO-01337 REV.1Apr 26, 2006 · N176YV · Beech 1900D · Wing SparSDR 1060406014Spar · corrodedBIOCORROSION RT MAIN SPAR CAP FLANGE AT WS124.588 REPAIRED IAW FIELD REPAIR FR-CO-01337 REV.1Apr 26, 2006 · N176YV · Beech 1900D · Wing SparSDR 74809Fire Loop · failedWHILE IN ROUTE, THE LT T-HANDLE ILLUMINATED. CREW COMPLIED WITH EMERGENCY CHECKLIST AND DIVERTED DECLARED EMERGENCY AND LANDED SAFELY WITH NO FURTHER INCIDENT. IT WAS THEN FERRIED, MAINTENACE REMOVED AND REPLACED LT FWD FIRE LOOP ASSY.Dec 19, 2005 · N176YV · Beech 1900D · Fire DetectionSDR 74784Brake · weakWHILE TAXING IN, THE CREW NOTICED THE BRAKES WERE SPONGEY. THE AIRCRAFT WAS THEN FERRIED AND MAINTENANCE BLED THE BRAKES. NO PARTS USED.Dec 18, 2005 · N176YV · Beech 1900D · Landing Gear Brake SystemSDR 74798Master Cylinder · failedDURING TAXI IN, THE CREW REPORTED THE BRAKES FEELING SPONGY. THEN FERRIED TO ICT WHERE MAINTENANCE REMOVED AND REPLACED THE MASTER CYLINDER.Dec 18, 2005 · N176YV · Beech 1900D · Master Cylinder/Brake ValveSDR 71037Brake · malfunctionedON TAXI TO GATE BRAKES WERE SPONGY. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. THEREFORE NO PARTS WERE USED.May 26, 2005 · N176YV · Beech 1900D · Landing Gear Brake SystemSDR 70122Brake · dirtyAFTER ARRIVING AT GATE IN DFW, CREW REPORTED LEFT BRAKE WEAK. MAINTENANCE CLEANED THE BRAKES. THEREFORE NO PARTS WERE USED.Apr 4, 2005 · N176YV · Beech 1900D · BrakeSDR 68837Brake · failedAFTER TAXI IN LEFT BRAKE WEAK. REMOVED AND REPLACED LT BRAKE.Feb 1, 2005 · N176YV · Beech 1900D · BrakeSDR 67819Brake Assy · smokeAFTER LANDING IN MIA CREW NOTICED LEFT BRAKES SMOKING. CLEANED LEFT MAIN GEAR BRAKE ASSY. CHECK OK AT THIS TIME.Dec 21, 2004 · N176YV · Beech 1900D · BrakeSDR 64107Socket · dirtyDISPATCH RECEIVED A CALL FROM MGW STATION THAT THEY HAD BEEN CONTACTED BY FLT 4740 AND INFORMED THAT THE AIRCRAFT DID NOT HAVE 3 GOOD DOWN AND LOCK INDICATIONS FOR MAIN LANDING. CREW WAS ADVISED TO FOLLOW CHECKLIST AND DIVERT. THEY LEARNED LATER THAT CREW HADAug 21, 2004 · N176YV · Beech 1900D · Landing Gear Position and WarningSDR 63455Uplock Switch · failedAFTER TAKEOFF WHEN GEAR WAS RETRACTED THE LANDING GEAR IN-TRANSIT LIGHT REMAINED ILLUMINATED. CREW CONTACTED DISPATCH AND MAINTENANCE CONTROL. CREW WAS TOLD TO DIVERT. AIRCRAFT THEN DIVERTED, LANDED WITH NO FURTHER INCIDENTS. REMOVED AND REPLACED RT UPLOCK Jul 29, 2004 · N176YV · Beech 1900D · Landing Gear Position and WarningSDR 63428Brake Assy · malfunctionedWHILE TAXING IN AFTER LANDING IN TPA. CAPTAIN FELT THAT THE LT BRAKE FELT SPONGY. THEN CALLED MAINTENANCE. BRAKES WAS BLEED, OPS CK NORMAL.Jul 28, 2004 · N176YV · Beech 1900D · BrakeSDR 59816Nut · looseON TAKE OFF ROLL CREW NOTED A LACK OF PROPER ACCELERATION. ABORTED TAKE OFF RETURNED TO GATE. FOUND BRAKE ROD NUT LOOSE. IT WAS TIGHTENED.Mar 18, 2004 · N176YV · Beech 1900D · BrakeSDR 57453Brake · inoperativeUPON LANDING RT BRAKES FELT SOFT. MAINTENANCE CALLED. BRAKES WERE BLEED. OPS CK NORMAL.Dec 29, 2003 · N176YV · Beech 1900D · BrakeSDR AMWA44Rib · crackedRIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-46, STRG 101-640000-42 ON RT SIDE AND STRG P/N 101-640000-41, STRG P/N 101-640000-37 (4EA CRACKS TOTAL ON THIS RIB)Sep 2, 2003 · N176YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA43Rib · crackedRIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 STRG P/N 101-640000-42 BOTH RT SIDE AND STRG P/N 101-640000-37 STRG P/N 101-640000-45 ON LT SIDE (4 EA TOTAL CRACKS ON THIS RIB)Sep 2, 2003 · N176YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA42Rib · crackedRIB AT CSS 69.184 CRACKED AT STRG P/N 101-640000-46 FIRST STRG FWD OF AFT SPAR RT SIDE OF VERTICAL STABILIZER.Sep 2, 2003 · N176YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 53866Printed Ckt Board · faultyUPON APPROACH TO VPS LANDING GEAR WOULD NOT EXTEND. A SECOND ATTEMP WAS MADE WITH THE SAME THING NO DOWN AND LOCKED INDICATION FLY BY OF TOWER AT VPS. CONFIRMED GEAR WAS NOT DOWN. GEAR WAS THEN PUMPED DOWN AND LOCKED CONFIRMED BY GEAR DOWN AND LOCK INDICATIAug 26, 2003 · N176YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 98ZZZM891Switch · malfunctionedFLT 5633 - RETURNED TO THE FIELD IN MCI WHEN THE LEFT FIRE LOOP LIGHT CAME ON IN FLIGHT. MCI MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY, BUT DID CHANGE THE T-HANDLE AND RETURNED THE AIRCRAFT TO SERVICE AFTER A TEST FLIGHT THAT PRODUCED NO DISCREPANCY. (Oct 10, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM885Switch · malfunctionedFLT 5665 - ICT-MCI - EN ROUTE, T-HANDLE AND FIRE LOOP ILLUMINATE INTERMITTENTLY. ICT MAINTENANCE FOUND AND REPAIRED CHAFFED WIRES UNDER THE LEFT FORWARD FLOORBOARD AND REPLACED THE LEFT FIRE LOOP TEST SWITCH. THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTOct 10, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM883Harness · looseFLT 5600 - RTF WHEN THE LT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. THE LEFT ENGINEWAS SHUT DOWN. EMERGENCY EQUIPMENT WAS CALLED. AIRCRAFT LANDED WITHOUT INCIDENT. ICT MAINTENANCE THEN RETURNED THE AIRCRAFT TO SERVICE. (M)Oct 9, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM903Fire Loop · malfunctionedFLT 5601 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED FORWARD AND AFT FIRE LOOP DETECTORS, PERFORMED GROUND RUN OPS CHECK NORMAL. (M)Oct 8, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM902Fire Loop · malfunctionedFLT 5601 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED FORWARD AND AFT FIRE LOOP DETECTORS, PERFORMED GROUND RUN OPS CHECK NORMAL. (M)Oct 8, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM901Fire Loop · looseFLIGHT 5609 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED. INTERMITTENTLY IN FLIGHT. MAINTENANCE FOUND LOOSE WIRE AT LOOP CONNECTOR. WIRE WAS RESOLDERED, PERFORMED GROUND RUN OPS CHECK NORMAL. (M)Oct 7, 1998 · N176YV · Beech 1900D · Detection SystemSDR 98ZZZM896Skin · crackedOVERNIGHT MAINTENANCE IN ICT FOUND A 1 INCH CRACK IN TOP SKIN .5 INCH FROM INBOARD AND 9.5 INCH FROM TE ON RHOB FLAP. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M)Mar 28, 1998 · N176YV · Beech 1900D · Trailing Edge FlapsSDR 98ZZZM434Skin · looseIN ICT AT OVERNIGHT DETAIL NR 1 INSPECTION, MAINTENANCE FOUND SEVERAL RIVETS LOOSE AND PULLED THROUGH THE SKIN ON THE BOTTOM SKIN OF RT INBOARD FLAP. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)Jan 17, 1998 · N176YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM1196Brackets · wornFLAP WAS REMOVED FOR A CRACK REPAIR. INSPECTION FOUND ATTACH INBOARD BRACKET BOLT HOLES WORN. REPLACED INBOARD ATTACH BRACKETS, APPLIED DOUBLERS TO BRACKETS IAW TO 1900-27-50-0001. (M)Oct 1, 1997 · N176YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM1195Brackets · wornFLAP WAS REMOVED FOR A CRACK REPAIR. INSPECTION FOUND ATTACH INBOARD BRACKET BOLT HOLES WORN. REPLACED INBOARD ATTACH BRACKETS, APPLIED DOUBLERS TO BRACKETS IAW TO 1900-27-50-0001. (M)Oct 1, 1997 · N176YV · Beech 1900D · Trailing Edge Flaps
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