N178YV

Service difficulty reports · 47

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 = 'N178YV' 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 GLBA2013100800337Skin · dentedDURING A SCHEDULED INSPECTION FOUND A DENT AFTER A BIRD STRIKE TO THE RIGHT WING AT WS 264.74 AND 283.74, 19" LONG X 1.75" DEEP. REPAIRED AREA IAW EO 13-1900-57-018. MAJOR REPAIR.Oct 5, 2013 · N178YV · Beech 1900D · Wing, Plate/SkinSDR GLBA2013021400176Unknown · odorPILOT REPORTED THAT THERE WAS A STRONG ELECTRICAL ODOR IN THE COCKPIT. MX INSPECTED ACFT DUCT SYS, RAN ACFT AND OPS CHECKED SYS WITH FLIGHT CREW, NO DEFECTS NOTED.Feb 13, 2013 · N178YV · Beech 1900D · Air Distribution SystemSDR GLBA2012112700118Switch · failedPILOT REPORTED GLARE SHIELD EMERGENCY LIGHTS FAIL TO ILLUMINATE ON CAPTAIN`S SIDE. MAINTENANCE REPLACED THE SWITCH, OPS CHECKED GOOD.Nov 26, 2012 · N178YV · Beech 1900D · Emergency LightingSDR GLBA2012110100101Skin · dentedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A DENT IN THE RT FUSELAGE LOCATED BETWEEN STRINGERS 10R AND 11R AT FS 228.25 AND 243.25 IN A AREA OF 6" BY 4.6", WITH A DEPTH OF .15". REPAIRED IAW EO 12-1900-53-063. MAJOR REPAIRNov 1, 2012 · N178YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2012103000095Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT UPPER 2ND FASTENER HOLE, CRACK RADIATES UPWARD AND DOWNWARD AT THE OB EDGE OF FASTENER HOLE, .2 ICHES IN LENGTH. REPAIRED IAW EO 12-1900-55-052. MAJOR REPAIROct 30, 2012 · N178YV · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012103000094Spar · misrepaired- DURING A SCHEDULED ROUTINE INSP FOUND THAT THE HORIZONTAL STAB FWD SPAR WEB MISREPAIRED. REPAIRED IAW EO 12-1900-55-053. MAJOR REPAIROct 30, 2012 · N178YV · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012103000097Spar Cap · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT THE UPPER FASTENER HOLE AT VSS 84.10, 20 PERCENT, CRACK RADIATES DOWNWARD & OTBD FROM FASTENER HOLE, .15 INCHES IN LENGTH. REPAIRED IAW EO 12-1900-55-054. MAJOOct 30, 2012 · N178YV · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA2012102900092Structure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 451 AND STRINGER 10R IN THE BEND RADIUS PROTRUDING UPWARD, .5" IN LENGTH. REPAIRED IAW EO 12-190 0-53-059.Oct 29, 2012 · N178YV · Beech 1900D · Fuselage Main, StructureSDR GLBA2012102900091Structure · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND CRACK AT A PREVIOUS REPAIR AT FS 163.97 AND STRINGER 9AR FRAME PROTRUDING OUT OF A STOP DRILL, .25" IN LENGTH. REPAIRED IAW EO 12-1900-53-060.Oct 29, 2012 · N178YV · Beech 1900D · Fuselage Main, FrameSDR GLBA2012072500019Fuse · inoperativePILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT IS INOPERATIVE. MX REPLACED THE SYS FUSE, OPS CHECKED GOOD.Jul 24, 2012 · N178YV · Beech 1900D · Emergency LightingSDR GLBA201206112Actuator · failedCREW TRIED TO EXTENDED THE GEAR NORMALLY BUT THE GEAR FAILED TO EXTEND. CREW RAN CHECKLIST AND EXTENDED THE GEAR MANUALLY. AFTER MANUAL EXTENSION THERE WERE NO ABNORMAL INDICATIONS NOTED. MX R & R RT MAIN LANDING GEAR ACTUATOR IAW TC 1900-3230.10, REV 1. OPJun 8, 2012 · N178YV · Beech 1900D · Landing Gear ActuatorSDR GLBA2012040501Spar · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A SMALL CRACK ON THE HORIZONTAL STAB AFT SPAR CENTER WEB AT 2-OCLOCK POSITION AS VIEWED FROM REAR, .125" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW FR EO 02Apr 5, 2012 · N178YV · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA20120103FSeat Track · wornMAJOR REPAIR - SEAT TRACK AT FS 423 AND WL 95, CORNER WORN .05", .12" ON LT SIDEWALL. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-001. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Jan 2, 2012 · N178YV · Beech 1900D · Fuselage, Seat/Cargo Attach FittingsSDR GLBA201109072Lamp · burned outINSTRUMENT EMERGENCY LIGHT ON CAPTAIN'S SIDE BURNED OUT. MX REPLACED THE BULB IAW BMM 33-10-04, OPS CHECKED GOOD.Sep 6, 2011 · N178YV · Beech 1900D · Emergency LightingSDR GLBA20110907FBulb · inoperativePILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT ON THE CA'S SIDE BURNED OUT. MX REPLACED THE BULB PN: 1864, IAW BMM 33-10-04, OPS CK GOOD.Sep 6, 2011 · N178YV · Beech 1900D · Emergency LightingSDR GLBA20110831GUnknown · smokePILOT REPORTED THAT SMOKE WAS COMING FROM UNDER THE GLARESHIELD. MX RAN ENGINES, WS HEAT, AND BLEEDS, NO SMOKE NOTED AT THIS TIME.Aug 29, 2011 · N178YV · Beech 1900D · Instrument PanelSDR GLBA201104141Unknown · odorPASSENGERS REPORTED A STRONG FUELD SMELL IN THE BACK OF THE AIRCRAFT. MAINTENANCE RAN BOTH ENGINES AND INSPECTED FOR FUEL LEAKS AND ODORS INSIDE IN THE AIRCRAFT, COULD NOT DUPLICATE ANY ODORS OR LEAKS, OK FOR SERVICE.Apr 14, 2011 · N178YV · Beech 1900D · Air Distribution SystemSDR GLBA20110215FStructure · crackedDURING A SCHEDULED ROUNTINE INSP MX, FOUND THE RT STABILON HAS A .5" HOLE 9" FROM T/E CORNER, CRACK RADIATED FROM INBD EDGE OF HOLE 1" IN LENGTH. MAINTENANCE COULD NOT REPAIR RT STABILON, REPLACED RT STABILON IAW BMM 55-10-01-201, NO RII REQUIRED FOR INSTALLAFeb 15, 2011 · N178YV · Beech 1900D · Vertical Stabilizer Miscellaneous StructureSDR GLBA20101215FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE INNER SKIN OF THE 6A EMERGENCY EXIT DOOR LOWER FWD CORNER, .7" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-52-007. MATERIALS UTILDec 15, 2010 · N178YV · Beech 1900D · Emergency ExitsSDR GLBA20101213FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE DOME SKIN AT FS 150 AND RT OF STRINGER NR 1, .75" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-063. MATERIALS UTILIZDec 13, 2010 · N178YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20101213GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE RT FUSELAGE FRAME AT FS 456 & STR 10R AT THE STRINGER CUTOUT, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-062. Dec 13, 2010 · N178YV · Beech 1900D · Fuselage Main, FrameSDR GLBA200909011Landing Gear · malfunctionedPILOTS REPORTED THEY HEARD LOUD MOTOR NOISE ON AND OFF. CONSISTENTLY WITH THE MOTOR NOISE THEY NOTICED THE DC LOAD WOULD GAIN 10-20 PERCENT. AFTER SEVERAL MIN OF THE THIS THEY NOTICED THE GEAR HANDLE IN TRANSIT LIGHT ILLUMINATED. IT EXTINGUISHED SHORTLY AFTSep 1, 2009 · N178YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20090821APower Cable · out of rigAIR RETURN, DUE TO UNAVAILABILITY OF PWR ON THE NR 2 ENG. PILOTS REPORTED THAT AN AIR RETURN OCCURRED DUE TO THE UNAVAILABILITY OF PWR ON NR 2 ENG. MX RIGGED RT ENG PWR CABLE ROD END IAW. OPS CHECK WAS GOOD. RII INSP COMPLIED IAW TASKCARD 4.3.13 AND WAS FOUAug 21, 2009 · N178YV · Beech 1900D · Power LeverSDR GLBA20090605GSkin · crackedMAJOR REPAIR, DURING ROUTINE MX A CRACK WAS FOUND ON THE RUDDER TRIM ROD CUT OUT. APPROX RUDDER STA CSS 31.20. CRACK APPROX .375 INCH LONG. MX REMOVED DAMAGED AND REPAIRED THE AFFECTED AREA IAW EO-09-1900-27-001. RII INSPECTIONS COMPLIED WITH AND RUDDER BALANJun 4, 2009 · N178YV · Beech 1900D · Rudder, Plate/SkinSDR GUU2008F00035Brake · weakFLIGHT 9148 MHH/FLL. PILOT REPORTED FIRST OFFICER LT RUDDER PEDAL GOES TO THE FLOOR WHEN DEPRESSED AND NO BRAKES. BACK BLED BRAKE SYSTEM. OPERATIONAL CHECK NORMAL. (S)Aug 4, 2008 · N178YV · Beech 1900D · Landing Gear Brake SystemSDR GUUA05110804Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED RT CTR ELEVATOR HINGE BRACKET HAS CORROSION. REPLACED RT CTR ELEVATOR HINGE BRACKET.May 11, 2008 · N178YV · Beech 1900D · Elevator Miscellaneous StructureSDR GUUA05110803Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT OB ELEVATOR HINGE BRACKET HAS CORROSION. REPLACED LT OB ELEVATOR HINGE BRACKET.May 11, 2008 · N178YV · Beech 1900D · Elevator Miscellaneous StructureSDR GUUA11090703Brake · weakFLIGHT: 9171 MHH/MIA, DURING TAXI LT BRAKE WILL NOT STOP AIRCRAFT WHEN FULLY DEPRESSED. INSPECTED UNDER FLOOR FOR LEAKS. BLED LT BRAKE ASSEMBLIES. OPEARATIONAL CHECK GOOD.Nov 9, 2007 · N178YV · Beech 1900D · Landing Gear Brake SystemSDR GUUA11090702Brake · weakFLIGHT: 9180 FPO/MIA, DURING TAXI LT BRAKE WILL NOT STOP AIRCRAFT WHEN DEPRESSED FULLY. PERFORMED LT BRAKE BLEEDING. OPERATIONAL CHECK GOOD.Nov 9, 2007 · N178YV · Beech 1900D · Landing Gear Brake SystemSDR GUUA12150601Unknown · smokeFLIGHT:9279 PBI/NAS AFTER TAKEOFF ODOR OF SMOKE IN THE COCKPIT AND CABIN. RETURNED TO PBI LANDED WITHOUT INCIDENT. RAN AIRCRAFT WITH ALL EQUIPMENT ON NO SIGN OF SMOKE ODOR NOTED. TEST FLIGHT SATISFACTORY.Dec 15, 2006 · N178YV · Beech 1900D · Air Distribution SystemSDR GUUA05020601Transfer Tube · leakingFLIGHT: 9259 FLL/MHH DURING FLIGHT SMELL OF FUEL IN THE COCKPIT. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED RT ENGINE FUEL NOZZLE TRANSFER TUBES AT THE THREE O CLOCK POSITION.May 2, 2006 · N178YV · Beech 1900D · Engine Fuel DistributionSDR GUU2005F00007Gasket · leakingDURING FLIGHT, RT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. SECURED THE RT ENGINE. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT ENGINE OVERSPEED GOVERNOR GASKET. OPS LEAK CHECK NORMAL. (K)Mar 9, 2005 · N178YV · Beech 1900D · Turbine Engine Oil SystemSDR 60419Downlock Switch · dirtyON LANDING APPROACH IN EYW. AIRCRAFT LOST ALL INDICATION ON POSITION OF RT LANDING GEAR. CREW ABORTED LANDING. CYCLED GEAR AND GOT THREE DOWN AND LOCKED INDICATION. LANDED SAFELY WITH NO FURTHER INCIDENT. CLEANED DOWNLOCK SWITCHES. JACKED AIRCRAFT AND PERFORMApr 8, 2004 · N178YV · Beech 1900D · Landing Gear Position and WarningSDR 58728Switch · stuckAFTER TAKEOFF FLAPS STUCK AT A PLACE IN BETWEEN 17 DEGREES & 34 DEGREES. CREW THEN DECIDED TO RETURN TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENTS. CLEANED LT / RT SPLIT FLAP SWITCHES OPS CK NORMAL.Feb 10, 2004 · N178YV · Beech 1900D · Trailing Edge Flap Control SystemSDR AMWA24Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.Aug 18, 2003 · N178YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA23Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.Aug 18, 2003 · N178YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA22Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.Aug 18, 2003 · N178YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR 2002F00231Warning Horn · false activationON DECEMBER 22, 2001, THE STALL WARNING HORN SOUNDED IMMEDIATELY AFTER TAKEOFF. THE PILOT REPORTED THAT THE HORN WOULD NOT SILENCE, AND THEN RETURNED THE AIRCRAFT TO ICT WITHOUT ANY FURTHER INCIDENT. MAINTNANCE CORRECTED THE PROBLEM, AND RETURNED TO THE AIRCDec 22, 2001 · N178YV · Beech 1900D · Stall Warning SystemSDR 97ZZZM1087Fuel Control · wornFLT CREW IN ICT REPORTED LEFT ENGINE RESPONDING SLOW TO POWER LEVER INPUT. MAINTENANCE IN ICT INSPECTED AND FOUND THE FUEL CONTROL UNIT CONTROL ARM ASSEMBLY WORN. MAINTENANCE REPLACED FUEL CONTROL UNIT IAW EMM 72-00 AND MM 76-00 AND RETURNED TO THE AIRCRAFT Sep 28, 1997 · N178YV · Beech 1900D · Fuel Control/Turbine EnginesSDR 97ZZZX4244Skin · crackedDURING DETAIL NR 1 WING INSPECTION, FOUND RIGHT OUTBOARD FLAP SKIN HAS A .25 INCH CRACK. STOP-DRILLED CRACK. PATCHED OVER CRACK USING FLAP STOCK, THREE ORIGINAL RIVETS, AND FOUR ADDITIONAL RIVETS IAW T.O. 1900-27-00-0001. (X)Sep 2, 1997 · N178YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX4236Dovetail Blkhd · crackedDURING BEECH TEMP. REV. 5-6 INSPECTION, FOUND 1 INCH CRACK AT LEFT INBOARD FLAP. DOVE TAIL BULKHEAD UPPER ROW. REPAIRED IAW T.O. 1900-27-00-0001. (X)Jul 17, 1997 · N178YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM961Skin · crackedAT ICT, OVERNIGHT MAINTENANCE INSPECTION FOUND A 1 INCH CRACK IN LEFT OUTBOARD FLAP APPROX 31 INCHES FROM OUTBOARD EDGE OF FLAP STOP. DRILLED CRACK USING A SIZE .09375 DRILL BIT. FABRICATED AND INSTALLED A 2.5 INCH BY 2.5 PATCH USING FLAP SKIN STOCK IAW BEECJul 13, 1997 · N178YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX4239Brackets · wornDURING BEECH TEMP. REV. 5-6 INSPECTION, FOUND INBOARD AND OUTBOARD ATTACHING BRACKETS AT INBOARD ATTACHING POINT WORN. REMOVED AND REPLACED BRACKETS AND RE-ASSEMBLED IAW SRM 57-00. (X)Jul 2, 1997 · N178YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM965Skin · crackedDURING BEECH TEMP REV INSPECTION, FOUND CRACK APPROX 1 INCH LONG ON FLAP LEADING EDGE. REPAIRED CRACKED IAW AMWA TO 1900-27-00-0001.Jun 30, 1997 · N178YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM246Ice Vane · missing rivetDURING AN ROUTINE INSPECTION, A RIVET IN THE ICE VANE WAS FOUND MISSING. INSPECTION OF THE COMPRESSOR REVEALED THE BLIND RIVET WENT THOUGH THE ENGINE. THE GAS GEN WAS REPLACED DUE TO FOD. (M)Jan 16, 1997 · N178YV · Beech 1900D · Air Intake Anti/De-Ice SystemSDR 96ZZZM381Ice Vane · crackedDURING ROUTINE MAINTENANCE, THE RIGHT FIXED ICE VALVE WAS FOUND TO TO HAVE SEVERAL CRACKS.Dec 19, 1995 · N178YV · Beech 1900D · Air Intake Anti/De-Ice SystemSDR 96ZZZX128Windshield · crackedCAPTAIN'S WINDSHIELD CRACKED ALONG THE OUTBOARD EDGE OF WINDSHIELD APPROXIMATELY 14 INCHES LONG. REMOVED AND REPLACED WINDSHIELD. AIRCRAFT HAD 74 FLIGHT HOURS AND 119 CYCLES SINCE NEW FROM BEECHCRAFT.Nov 14, 1995 · N178YV · Beech 1900D · Flight Compartment Windows
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