N182YV, cancelled Mar 8, 2012

Service difficulty reports · 50

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 = 'N182YV' AND deregistration_id = 'N182YV-2012-03-08'
  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 GLBA20111003HUplock Switch · inoperativePILOT REPORTED THAT THE GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER THE GEAR WAS RETRACTED. MX REPLACE THE RT LANDING GEAR UPLOCK SWITCH PN: H11-1541GLA IAW TC 1900-3260-00, SYS OPS CHECKED GOOD.Oct 1, 2011 · N182YV · Beech 1900D · Landing Gear Position and WarningSDR GLBA20110930FLine · leakingPILOT REPORTED THAT FUEL WAS DRIPPING FROM HYD LINES IN LT WHEEL WELL. MX CLEANED AND INSPECTED THE AREA, NO LEAK FOUND.Sep 29, 2011 · N182YV · Beech 1900D · Fuel StorageSDR GLBA20110927FHandle · unsecurePILOT REPORTED THAT THE DOOR HANDLE ON THE FWD RT EMERGENCY EXIT DOOR APPEARS TO BE RECESSED. MX RESECURED THE EMER EXIT DOOR IAW BMM 52-20-00, OK FOR SERVICE.Sep 26, 2011 · N182YV · Beech 1900D · Emergency ExitsSDR GLBA20110926KExtinguisher · overservicedPILOT REPORTED THAT THE PASSENGER FIRE EXTINGUISHER READ OUT IN THE RED, OVER CHARGED. MX REPLACED THE FIRE EXTINGIUSHER.Sep 24, 2011 · N182YV · Beech 1900D · Fire Bottle, PortableSDR GLBA20110915FPcb · inoperativePILOT REPORTED THAT AUTOFEATHER ANNUNCIATOR IS INOPERATIVE. REPLACED THE AUTOFEATHER PCB REF BMM 20-00-01, OPS CHECKED GOOD.Sep 14, 2011 · N182YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110914001Annunciator · inoperativePILOT REPORTED THAT AUTOFEATHER ANNUNCIATOR IS INOPERATIVE. OPENSep 14, 2011 · N182YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20110816GLanding Gear · malfunctionedPILOT REPORTED THAT WHILE ON A CHECK FLIGHT THE LANDING GEAR WAS SELECTED DOWN, NOTHING HAPPENED AND HAD TO MANUALLY EXTEND THE GEAR, GOT 3 GREENS AND LANDING. MX INSPECTED THE SYS, RESET CB IN LT WHEEL WELL AND CHECKED RELAY K13, PERFORMED GEAR SWINGS IAW AIAug 15, 2011 · N182YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20110722FCable · brokenPILOT REPORTED THAT THE SNUBBER CABLE BROKE UPON OPENING THE AS DOOR. MX REPLACED THE CABLE IAW BMM 52-10-01-201, PN: 129-514119-1GLA.Jul 21, 2011 · N182YV · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110718GBulb · missingDURING PREFLIGHT THE PILOT FOUND THE INST EMERGENCY LIGHT BULB MISSING. MX REPLACED THE EMERGENCY LIGHT BULB, PN: 1864 IAW BMM 33-10-04.Jul 15, 2011 · N182YV · Beech 1900D · Emergency LightingSDR GLBA20110621FUplock Switch · failed"SUP" - SIG EVENT - PILOT REPORTED THAT WHEN THE RETRACTED THE GEAR, THE INTRANSIT LIGHT WOULD NOT EXTINGUISH, LANDING GEAR EXTENDED WITH 3 GREENS WITH NO INTRANSIT LIGHT. MX REPLACED THE NLG UPLOCK SWITCH, OPS CHECK GOOD.Jun 20, 2011 · N182YV · Beech 1900D · Landing Gear Position and WarningSDR GLBA20110525GPump · wornPILOT REPORTED THAT THE RT FUEL PSI LOW LIGHT ILLUMINATED DURING FLIGHT, TURNED STANDBY PUMP ON AND LIGHT EXTINGUISHED. MX R & R THE RT LOW PRESS FUEL PUMP IAW BMM 23-10-00, LEAK AND OPS CK GOOD, PN 114-3890425 SN ON: B-952-019 SN OFF: B1448.May 24, 2011 · N182YV · Beech 1900D · Fuel Boost PumpSDR GLBA20110524FSwitch · out of rigPILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED AT FLIGHT LEVEL 240, MAX DIFF WAS 4.7, MAX DIFF DIDN'T CHANGE. PUT ON MEL. MAINTENANCE FOUND THE PRESSURE LOCK SWITCH SLIGHTLY OUT OF RIG, RE-ADJESTED PRESSURE LOCK SWITCH IAW BMM 52-70-02, ALL CHECKS May 23, 2011 · N182YV · Beech 1900D · Door Warning SystemSDR GLBA20110516GPlacard · misinstalled- SIG EVENT - PILOT REPORTED THAT THE EMERGENCY EXIT PLACARD IS AT THE WRONG SEAT. PLACARD IS IN 7C AND SHOULD BE IN 5C. MX INSTALLED THE PLACARD IN THE PROPER LOCATION.May 15, 2011 · N182YV · Beech 1900D · Placards and MarkingsSDR GLBA20110420JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 500 AND STRINGERS 4L & 5L CRACKED AT THE STRUT MOUNT UPPER IB NUTPLATE AREA, .65" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REApr 19, 2011 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20110420HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT FS 456 AND STRINGER 3L & 4L AT THE GAS STRUCT MOUNT UPPER IB NUTPLATE AREA, .25" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMEDApr 19, 2011 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20110420FSpar · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A CRACK RADIATING FROM THE DEICE TUBING HOLE IN THE HORIZONTAL STAB MAIN SPAR CENTER WEB, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IApr 19, 2011 · N182YV · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA20110418FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME AT F.S. 456 AND STRINGER 9AR CRACKED .15" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-023. MATERApr 18, 2011 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20110418GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CRACKED .2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-025. MATERIApr 18, 2011 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA201007121Spline · strippedPILOT REPORTED THAT DURING TAKEOFF (CLIMB OUT) ENROUTE, NR 1 ENGINE FAILED & AUTOFEATHERED, ENGINE SHUTDOWN BY ITSELF, THE AIRCRAFT LANDED BACK AT FIELD WITHOUT INCIDENT. MX INSPECTED NR 1 ENGINE GAS GENERATOR FOR ROTATION, NO OBSTRUCTIONS IN THE INTAKE, CHECKJul 12, 2010 · N182YV · Beech 1900D · Engine Fuel PumpSDR GLBA20100628FSwitch · dirtySMOKE/SMELL - PILOTS REPORTED THAT WITH THE BATTERY ON, ALL OF THE ANNUNCIATORS REMAINED ILLUMINATED WITH A SLIGHT BURNING SMELL BEING NOTICED. MX REMOVED AND CLEANED THE MICRO SWITCHES ON THE PUSH TO TEST SWITCH. THE OPS CHECK WAS GOOD. REF MM 33-10-00.Jun 27, 2010 · N182YV · Beech 1900D · Indicating/Recording SystemSDR GLBA20100324FSkin · dentedMAJOR REPAIR - PILOTS REPORTED THAT A BIRD STRIKE OCCURRED ON SHORT FINAL ON THE LT WING, LT OTBD SECTION OF THE WING. BETWEEN WING SIDE 249.5 & WING SIDE 261.5. DENT IS APPROX 12" IN LENGTH AND APPROX .5" IN DEPTH.Mar 23, 2010 · N182YV · Beech 1900D · Wing, Plate/SkinSDR GLBA20100129FSkin · damagedCOMPONENT REPAIR - DURING A LIGHTINING STRIKE INSP OF THE ACFT AN EXIT HOLE WAS FOUND ON THE LT ELEVATOR. THE ELEVATOR WAS REMOVED AND REPLACED. IAW MM 27-30-00. EXIT HOLE IS ON OTBD. T/E HOLE .75" WIDE X .5" DEEP. DETERMINATION THAT THE ELEVATOR REQUIRED AJan 25, 2010 · N182YV · Beech 1900D · Elevator, Plate/SkinSDR GLBA20091104HSkin · crackedDURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND IN THE RIGHT HAND FUSELAGE SKIN AT F.S. 498.25 ABOVE STRINGER 10R. THE CRACK RADIATES THROUGH A RIVET HOLE. MAINTENANCE REPAIRED THE AFT FUSELAGE SKIN AT F.S. 498.25 AND COMPLIED WITH REQUIRED RII INSPECTINov 4, 2009 · N182YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20091104JFrame · bentDURING ROUTINE SCHEDULED MAINTENANCE A FRAME WAS FOUND BENT AT F.S. 451 BETWEEN STRINGER 6R & 7R. DAMAGE FOUND UNDER PREVIOUS REPAIR TO FUSELAGE SKIN. MAINTENANCE REPLACED THE DAMAGED FRAME AND PERFORMED THE REQUIRED II INSPECTIONS AT F.S. 451 BETWEEN STRINGERNov 4, 2009 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20091104GSkin · crackedDURING ROUTINE SCHEDULED MAINTENANCE THE FUSELAGE SKIN WAS FOUND CRACKED AT F.S. 447 BETWEEN STRINGERS 6R AND 7R. CRACK LOCATED AT UPPER FORWARD CORNER OF A PREVIOUS REPAIR. CRACK IS APPROXIMATELY .5" IN LENGTH. MAINTENANCE REPAIRED THE SKIN AND PERFORMED THE Nov 4, 2009 · N182YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20091030GFrame · bentSCHEDULED MAINTENANCE A FUSELAGE FRAME WAS FOUND BENT AT FS 198.25 ON THE LEFT HAND SIDE OF THE FUSELAGE AT STRINGER 6L. MAINTENANCE REPAIRED THE FRAME AND PERFORMED THE REQUIRED RII INSPECTIONS AT FS 198.25 AT STRINGER 6L IAW EO 09-1900-53-025 REV.1. MATERIALOct 29, 2009 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20091030JFrame · bentDURING ROUTINE SCHEDULED MAINTENANCE STRINGER 6L WAS FOUND BENT JUST AFT OF FUSELAGE FRAME AT F.S. 198.25. MAINTENANCE REPAIRED STRINGER 6L AND PERFORMED THE REQUIRED RII INSPECTIONS AT F.S. 198.25 IAW EO 09-1900-53-026 R1. MATERIALS UTILIZED ARE INCLUDED IN TOct 29, 2009 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20091030LAngle · crackedDURING ROUTINE SCHEDULED MAINTENANCE A PREVIOUS REPAIR WAS FOUND CRACKED ON THE RIGHT HAND HEAVY ANGLE AT F.S. 303.25. CRACK LENGTH APPROXIMATELY 1". MAINTENANCE REPAIRED THE RIGHT HAND HEAVY ANGLE AND PERFORMED THE REQUIRED RII INSPECTIONS IAW E.O. 09-1900-53Oct 26, 2009 · N182YV · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20091030HAngle · crackedDURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND HEAVY ANGLE WAS FOUND CRACKED IN BEND RADIUS AT F.S. 303.25 AFT OF FUSELAGE FRAME. CRACK LENGTH APPROXIMATELY 1". PREVIOUS REPAIR INSTALLED BETWEEN F.S. 288 & 303.25. MAINTENANCE REPAIRED THE HEAVY ANGLE AT F.SOct 26, 2009 · N182YV · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20090928GSkin · damagedUPON INSPECTION OF THE ACFT A LIGHTNING STRIKE WAS FOUND ON THE RT ELEVATOR TOP SKIN. MAINTENANCE REMOVED AND REPLACED THE ELEVATOR I.A.W. 27-30-00. MX REMOVED AND REPLACED THE ELEVATOR HOWEVER THE ELEVATOR WAS REPAIRED AND THE RII INSPECTIONS COMPLIED WITH IASep 25, 2009 · N182YV · Beech 1900D · Elevator, Plate/SkinSDR GLBA2009Skin · crackedMAJOR REPAIR - WHILE PERFORMING OTHER MAINTENANCE RELATED TO AN ANTENNA REPLACEDMENT A RIVET HEAD WAS FOUND MISSING AND TWO SMALL CRACKS WERE FOUND THAT WERE APPROXIMATELY .2" IN LENGTH EMMANATING FROM RIVET HOLE ON THE TOP AT F.S. 150.6 TO RIGHT OF THE CENTERSep 9, 2009 · N182YV · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20090424FSkin · leakingDURING SCHEDULED MX A FUEL LEAK WAS FOUND ON THE LT WING LE ON A PREVIOUS REPAIR FROM APPROX WS 239 TO WS 249.75. MX REPAIRED THE LT WING LE PREVIOUS REPAIR IAW EO-09-1900-57-004. ALL RII INSP REQUIREMENTS COMPLIED WITH IAW EO-09-1900-57-004.Apr 21, 2009 · N182YV · Beech 1900D · Wing, Plate/SkinSDR GLBA200903212Actuator · wornPILOTS REPORTED THAT DURING GEAR EXTENSION THE LEFT MAIN GEAR WAS FLICKERING ON AND OFF AND REC IN TRANSIT LIGHTS WERE ILLUMINATED. THEY RECYCYLED THE LANDING GEAR AND STILL HAD NO GREEN LIGHTS ON THE LEFT MAIN GEAR. THEY PERFORMED A MANUAL GEAR EXTENSION AND Mar 21, 2009 · N182YV · Beech 1900D · Landing Gear ActuatorSDR BSAASDR0725Skin · tornRIGHT FLAP HUMP MISSING LARGE SECTION OF SHEET METAL. FLAP WAS REMOVED AND REPLACED.Oct 5, 2007 · N182YV · Beech 1900D · Trailing Edge FlapsSDR BSAASDR0607Spar Cap · damagedPITTING CORROSION WAS FOUND ON THE RIGHT WING ON THE LOWER WING SPAR CAP IN THE THIRD ELEMENT SPAR STRAP JUST AFT OF THE WING DRAIN LOCATED JUST OUTBOARD OF THE NACELLE IN THE WING LEADING EDGE. THE DAMAGE AREA IS APPROXIMATELY .5 INCH WIDE AND WENT INTO THE Feb 27, 2006 · N182YV · Beech 1900D · Wing SparSDR 67971Annunciator · failedTAIL DE-ICE ANNUNCIATOR FAILED IN FLIGHT DURING ICING CONDITIONS, AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED TAIL DE-ICE SENSOR AND SERVICED TUBES, OPS CHECK GOOD.Dec 26, 2004 · N182YV · Beech 1900D · Landing Gear Position and WarningSDR 63594Fire Detector · malfunctionedON TAKEOFF ROLL OUT, FLIGHT CREW OBSERVED LT ENGINE FIRE BOTTLE DISCHARGED ANNUN. ILLUMINATED. CREW ABORTED TAKE OFF AND RETURNED TO THE GATE WITH NO FURTHER INCIDENT. THE BOTTLE WAS SAID THAT IT WAS NOT DISCHARGED. REMOVED AND REPLACED 173 PC BOARD FIRE DETAug 2, 2004 · N182YV · Beech 1900D · Fire DetectionSDR 58784Pressure Switch · inoperativeAFTER DEPARTING FROM MSS. CREW CLIMBED THROUGH INCING CONDITIONS AND FOUND TAIL DE-ICE TO BE INOP. IN BOTH MODES. THEY DIVERTED TO DUJ. UNDER A DISPATCH DECLARED EMERGENCY AND LANDED SAFELY WITH NOT FURTHER INCIDENTS.CORRECTIVE ACTION THAT WAS TAKEN IS R&R'D TFeb 12, 2004 · N182YV · Beech 1900D · Ice DetectionSDR 58604Annunciator · false indicationWHILE ON FLIGHT, PASSENGER DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CAPTAIN FOLLOWED PROCEDURES TO LAND AT AN ALTERNATE FIELD TRI. CREW INSPECTED DOOR AND FOUND ANNUNCIATOR GAVE FALSE ILLUMINATION. THIS ITEM WAS DEFERRED. THEN PROCEEDED TO FINAL DESTINAFeb 5, 2004 · N182YV · Beech 1900D · Door Warning SystemSDR 54574Switch · out of adjustMASTER WARNING ILLUM WITH A CABIN DOOR ANNUNCIATOR. TAKEOFF WAS ABORTER AFT RETURNED TO GATE. ADJUSTED CABIN DOOR ANNUNCIATOR LIGHT SWITCH.Sep 20, 2003 · N182YV · Beech 1900D · Door Warning SystemSDR AMWA33Rib · crackedRIB CRACKED AT CSS 69.184 AT STRG P/N 101-640000-46 RT AND STRG P/N 101-640000-45 LT SIDE (2EA CRACK AT THIS RIB).Sep 7, 2003 · N182YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA32Rib · crackedRIB AT CS 54.026 CRACKED AT STRG. P/N 101-640000-46 STRG P/N 101-640000-47 ON RT SIDE AND STRG P/N 101-640000-39 LT SIDE (3EA CRACKS ON THIS RIB).Sep 7, 2003 · N182YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA31Rib · crackedRIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-39, 1EA CRACK AT THIS RIB.Sep 7, 2003 · N182YV · Beech 1900D · Vertical Stabilizer, Spar/RibSDR AMWA8Spar Cap · chafedUPON A DETAILED INSPECTION MAINTENANCE FOUND THE ELECTRIC LINE CHAFING ON RIGHT FORWARD WING SPAR IN THE WHEEL WELL. BLENDED LOWER WING SPAR CAP IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT IS REQUIRED.Feb 12, 2003 · N182YV · Beech 1900D · Wing SparSDR 97ZZZM968Turbine · failedIN MCI, THE RIGHT ENGINE HAD A CONTAINED ENGINE FAILURE DURING START. REMOVED AND REPLACED RIGHT ENGINE GAS GENERATOR AND POWER SECTION. TEAR DOWN INSP REVEALED THE COMPRESSOR TURBINE CENTER BOLT AND KEY WASHER WAS NOT SUFFICIENTLY LUBRICATED AT INSTALLATIONAug 9, 1997 · N182YV · Beech 1900D · Turbine SectionSDR 97ZZZX4237Dovetail Blkhd · crackedDURING BEECH TEMP. REV 5-6 FLAP INSPECTION, THE LEFT INBOARD FLAP DOVETAIL BULKHEAD WAS FOUND WITH A CRACK. STOP DRILLED AND INSTALLED DOUBLER IAW AMWA T.O. 1900-27-00-0001. (X)Jun 28, 1997 · N182YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM977Bracket · wornAT ICT OVERNIGHT MAINTENANCE INSPECTION PER BEECH TEMP REV 5-6, FOUND LHOB FLAP. INBOARD ATTACH BRACKET WORN. REMOVED AND REPLACED ATTACH BRACKET IAW SRM 57-00 AND 51-40.Jun 28, 1997 · N182YV · Beech 1900D · Trailing Edge FlapsSDR 96ZZZM1243P3 Line · looseFLT 5627 - AFTER TAKEOFF RIGHT ENGINE ROLLED BACK TORQUE AND THEN STABILIZED AT ABOUT 1000 FT/LBS OF TORQUE, AIRCRAFT. RETURNED TO FIELD AT MCI. MAINTENANCE TIGHTENED P3 LINE C/W FLIGHT TEST RETURNED AIRCRAFT TO SERVICE. (M)Jul 17, 1996 · N182YV · Beech 1900D · Fuel Controlling SystemSDR 96ZZZX1754Blade · splitDURING ROUTINE MAINTENANCE, THE TRAILING EDGE WAS FOUND SPLIT APROXIMATELY 1.5 INCHES. REPAIRED IAW HARTZELL MM AND FORM 8110-3.Feb 18, 1996 · N182YV · Beech 1900D · Propeller Blade SectionSDR 96ZZZX1753Blade · splitDURING ROUTINE MAINTENANCE, PROPELLER BLADE, SN 1655, WAS FOUND TO HAVE A 4 INCH SPLIT ON TRAILING EDGE. REPAIRED IAW HARTZELL MM AND FORM 8110-3 FROM HARTZELL.Feb 10, 1996 · N182YV · Beech 1900D · Propeller Blade Section
Back to N182YV, cancelled Mar 8, 2012