N237YV, cancelled Feb 10, 2012

Service difficulty reports · 34

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 = 'N237YV' AND deregistration_id = 'N237YV-2012-02-10'
  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 GLBA20110802FPlacard · delaminatedPILOT REPORTED THAT THE AIR STAIR DOOR PLACARD DELAMINATED. MX REPLACED THE PLACARD.Aug 1, 2011 · N237YV · Beech 1900D · Placards and MarkingsSDR GLBA20110801GMount · wornMX FOUND THE AIRSTAIR DOOR LOWER COUNTER BALANCE HAS A WORN MOUNT HOLE. MX REPLACED THE LOWER BALANCE MOUNT IAW BMM 52-10-01, PN: 126-514105-33, OPS CK GOOD.Jul 29, 2011 · N237YV · Beech 1900D · Passenger/Crew DoorsSDR GLBA20110706FTire · failedPILOT REPORTED THAT THE LT INBD MAIN TIRE STRIPPED OF ITS CORD AFTER TOUCHDOWN, SHIMMY ON TOUCHDOWN. MX REPLACED THE NR 2 WHEEL ASSY IAW IAM TC 1900-3240-01.Jul 5, 2011 · N237YV · Beech 1900D · Wheel/Ski/FloatSDR GLBA20100309FFrame · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK IN THE FRAME RADIUS AT THE AIRSTAIR DOOR ENTRANCE FWD FRAME AT FS 177.350 AT APPROX STR 12L WAS FOUND, CRACK APPROX .5". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW Mar 8, 2010 · N237YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20100302GFrame · crackedUPON ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT THE RADIUS OF FRAME AT FS 177.350 AT APPROX STR 12L CRACK IS APPROX 2" LONG. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-007. MATERIALS UTILIZED ARE INCLUDED IN THEMar 2, 2010 · N237YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20100302FASpar · damagedMAJOR REPAIR - UPON ROUTINE SCHEDULED MX A LOCK FASTENER HOLE IN THE LT WING SPAR AT APPROX WS 93.250 WAS FOUND STEPPED. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-57-002. MATERIALS UTILIZED ARE INCLUDED IN THE EO.Mar 1, 2010 · N237YV · Beech 1900D · Wing SparSDR GLBA20100302FFrame · crackedMAJOR REPAIR - UPON ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT THE RADIUS OF FRAME AT FS 177.350 AT APPROX STR 12L. CRACK IS APPROX 2" LONG.Mar 1, 2010 · N237YV · Beech 1900D · Wing SparSDR GLBA20100118ABoot · sparksSPARKS WERE COMING FROM NR 1 PROP WHEN DE-ICE WAS ENGAGED HAD LARGE BURN MARK ON BOOT. MX R & R THE LT PROPELLER IAW TASKCARD 1900-6110.00. THE OPS CHECK AND LEAK CHECK WERE GOOD PN HC-E4A-3J SN ON HJ2050, SN OFF HJ1695. RII INSPECTIONS WAS SATISFACTORY IAW Jan 18, 2010 · N237YV · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice SystemSDR GLBA20091120FBleed Air Sys · contaminatedSMOKE/SMELL - PILOTS REPORTED THAT BURNING ODOR WAS PRESENT FROM THE CAPTAINS SIDE THAT SMELLED LIKE PLASTIC. NO SMOKE WAS OBSERVED. MX CLEANED GLYCOL FROM WINDOW DRIP TRAY AND INSPECTED THE FUEL PANEL FOR ANY EVIDENCE OF GLYCOL. NONE NOTED. MX RAN THE ACNov 17, 2009 · N237YV · Beech 1900D · Air Distribution SystemSDR GLBA200910211Bearing · deterioratedUPON LANDING, IT FELT LIKE THE LT BRAKE WAS SLUGGISH AND THE SWA THE LT MAIN TIRE OUTSIDE WHEEL FALL OFF OF THE HUB ASSY. MX REMOVED AND REPLACED THE LT MLG IAW MM 32-10-00, RII INSP COMPLIED IAW TASKCARD 4.3.6 AND RII OF UP/DOWN/SAFETY SWITCH INSTALLATION WAOct 20, 2009 · N237YV · Beech 1900D · Wheel/Ski/FloatSDR GLBA200907061Engine · power lossON CLIMB THROUGH 9000 FT, NR 2 PROP RPM DROPPED TO 500 RPM & TORQUES INCREASED TO 4700 FT LBS. SUSPECTED GOVERNOR FAILURE, SET MAX PWR, PROP LEVERS FULL FWD, & VERIFIED MLG & FLAPS UP. NR 2 ENG TORQUE STAYED AT 4700 FT LBS FOR APPROX 30 SEC & RE-SET TO 2000 FJul 6, 2009 · N237YV · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA20090531FCircuit Board · inoperativeTHE PILOTS REPORTED THAT THE AFX SYS FEATHERED THE NR 1 PROPELLER WHILE ON FINAL WITH PROPS FULL FWD AND TORQUE AT 1000 LBS. MX REMOVED AND REPLACED THE A123 PRINTED CIRCUIT BOARD IAW MM 20-00-01. OPS CHECKS WERE NORMAL.May 29, 2009 · N237YV · Beech 1900D · Propeller/Propulsor System WiringSDR GLBA20090522GPressure Switch · wornAFX ANNUNCIATORS AND REPEATER LIGHTS WOULD NOT ILLUMINATE WHEN POWER ADVANCED ABOVE 1000 FT LBS ON TAKEOFF ROLL. MAINT REMOVED AND REPLACED THE HIGH PRESSURE SWITCH CONNECTOR PLUG IAW GMM 9.3.0. MAINT ALSO REMOVED AND REPLACED THE NR1 AUTOFEATHER HIGH PRESSUMay 18, 2009 · N237YV · Beech 1900D · Propeller Feathering/ReversingSDR GLBA20090520FCircuit Board · failedPILOTS REPORTED THAT THE AFX ANNUNCIATORS AND REPEATER LIGHTS EXTINGUISHED AFTER V. THE AFX FAULT ANNUNCIATOR DID NOT ILLUMINATE. MAINT REMOVED AND REPLACED THE PRINTED CIRCUIT BOARD A123 IAW 1900D MM 61-20-00. MAINT ADDTIONALLY COMPLIED WITH FLEET CAMPAIGN DIMay 18, 2009 · N237YV · Beech 1900D · Propeller Indication SystemSDR GLBA20090329AWindshield · crackedPILOTS REPORTED THAT THE CAPTAINS WINDSHIELD CRACKED ON/IN CRUISE FLIGHT. AIRCRAFT RETURNED TO "DEN". MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDOW IAW SRM 56-10-00.Mar 29, 2009 · N237YV · Beech 1900D · Flight Compartment WindowsSDR GLBA200811131Stringer · crackedDURING CONFORMITY CHECKS A CRACK WAS FOUND AT STRINGER CUTOUT AT FS 177 AND 9R. CRACK RADIATES .2 INCH. REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW B1900D SRM 51-70 AT FS 177. REPAIR AREA APPROX 4.6 INCHES BY 2.6 INCHES. 2024 T3, .071 INCHES, MS20470 RINov 11, 2008 · N237YV · Beech 1900D · Fuselage Main, Longeron/StringerSDR BSAASDR0715Warning System · malfunctionedON DESCENT THE RT BLEED FAIL ANNUNCIATOR ILLUMINATED. THE CREW LANDED WITH NO FURTHER INCIDENT. EXTENSIVE TROUBLESHOOTING WAS COMPLETED WITH NO DEFECTS FOUND & MULTIPLE GROUND RUNS WERE COMPLETED, BUT COULD NOT DUPLICATE THE PROBLEM.May 20, 2007 · N237YV · Beech 1900D · Pneumatic Indicating SystemSDR BSAASDR0621Spar Cap · corrodedLEVEL 3 PITTING CORROSION WAS FOUND INITIALLY AROUND THE QUICK DRAIN IN THE 3RD INTERIOR SKIN DOUBLER. THIS CORROSION STARTED FROM THE UNTREATED EDGE OF THE QUICK DRAIN FITTING HOLE IN THE WING SKIN, AND PROGRESSED IN ALONG THE BOND LINE BETWEEN THE SKINS. WOct 20, 2006 · N237YV · Beech 1900D · Wing SparSDR 58290Indicator · stuckON TAKEOFF ROLL THE LT PROP INDICATOR BEGAN TO READ HIGH, IT THEN WENT TO 2000 AND STUCK. CREW ABORTED TAKEOFF AND RETURNED TO GATE, ON SHUT DOWN INDICATOR STUCK AT 600. THERE WAS NO FURTHER INCIDENT OCCUR. COULD NOT DUPLICATE THE PROBLEM.Jan 26, 2004 · N237YV · Beech 1900D · Propeller Indication SystemSDR 52776AMWA1Generator · failedON FLIGHT 5521 TAXING OUT, THE CREW NOTICED THE RT GENERATOR WOULD NOT STAY ONLINE. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE FOUND THAT THE RIGHT GENERATOR WILL NOT ENERGIZE. MAINTENANCE REMOVED AND REPLACED GENERATOR, GCU AND REPAIRED A WIREJul 20, 2003 · N237YV · Beech 1900D · DC Generating SystemSDR 52776Starter Gen · failedON FLIGHT 5521 TAXING OUT, THE CREW NOTICED THE RIGHT GENERATOR WOULD NOT STAY ON LINE. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE FOUND THAT THE RIGHT GENERATOR WILL NOT ENERGIZE. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACEDJul 20, 2003 · N237YV · Beech 1900D · Starter-GeneratorSDR AMWA17Finger Doubler · crackedWHILE PERFORMING AN "A" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND THAT THE FINGER DOUBLER WAS CRACKED. MAINTENANCE REMOVED AND REPAIRED THE FINGER DOUBLER. NO TEARDOWN REPORT WILL BE REQUIRED.Mar 5, 2003 · N237YV · Beech 1900D · Fuselage, Powerplant Attach FittingsSDR AMWA18Plate · damagedWHILE PERFORMING AN "A" CHECK ON THE LT ENGINE TRUSS, MAINTENANCE FOUND THAT THE LEFT PRESSURE PLATES HAVE RIVET HEAD CONTACT. MAINTENANCE REPAIRED THE PRESSURE PLATE PER THE STANDARD REPAIR MANUAL 57-95-02. NO TEARDOWN REPORT WILL BE REQUIRED.Mar 5, 2003 · N237YV · Beech 1900D · Fuselage, Powerplant Attach FittingsSDR 2002F00272Door · out of rigDURING CREW CHANGE, THE ON COMING CREW FOR AIRCRAFT FOUND THE RIGHT FORWARD EMERGENCY EXIT DOOR NOT FLUSH WITH THE EXTERIOR OF THE AIRCRAFT. AIRCRAFT MAINTENANCE FOUND THE DOOR TO BE OUT OF RIG, AND ADJUSTED THE DOOR PER MAINTENANCE INSTRUCTION. RETURNED TO Feb 25, 2002 · N237YV · Beech 1900D · Emergency ExitsSDR 98ZZZM895Skin · crackedICT OVERNIGHT MAINTENANCE, FOUND LEFT INBOARD FLAP TOP SKIN CRACKED AT INBOARD ATTACH BRACKET. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)May 23, 1998 · N237YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX4233Skin · crackedICT - OVERNIGHT, MAINTENANCE FOUND A CRACK 2 INCHES LONG AT TRAILING EDGE 16 INCHES OUT. STOP DRILLED AND PATCHED IAW SRM 51.00 AND TO 1900-27-00-0001. (X)Sep 17, 1997 · N237YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM976Skin · crackedDURING A NIGHT INSPECTION, AT ICT, REPAIRED 2 INCHES LONG Y SHAPED CRACK ON RHIB FLAP TOP SKIN IAW WITH TO 1900-27-0001. (M)Aug 26, 1997 · N237YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM975Skin · crackedAT ICT, AN OVERNIGHT MAINTENANCE INSPECTION, FOUND A CRACK ON THE LHOB. REPAIRED CRACK ON LHOB FLAP TOP SKIN IAW TO 1900-27-00-0001.Aug 22, 1997 · N237YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM907Flap · crackedRIGHT INBOARD FLAP HAS A .5 INCH CRACK IN TOP SKIN 10 INCHES IN FROM OUTBOARD END ADN 3 INCHES UP FROM TRAILING EDGE. STOP DRILLED CRACK AND PATCH IAW TO 1900-27-00-0001. (M)Aug 6, 1997 · N237YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM940Dovetail Blkhead · crackedREPLACED LOOSE RIVETS IN DOVETAIL. INSTALLED DOUBLER OVER CRACK IN DOVETAIL BULKHEAD IAW SRM 51-40. REPLACED ACTUATOR ATTACH BRACKET. WORK ACCOMPLISHED IAW TO 1900-27-00-0001. (M)Jun 19, 1997 · N237YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM972Bulkhead · crackedDURING BEECH TEMP REV 5-6, AN INSPECTION, FOUND THREE CRACKS ON RHIB FLAP DOVETAIL BULKHEAD. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)Jun 17, 1997 · N237YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM971Dovetail · crackedDURING BEECH TEMP REV 5-6 AN INSPECTION, FOUND A CRACK ON THE INBOARD SIDE OF RIGHT DOVETAIL 7 INCH FROM LEADING EDGE. REPAIRED IAW AMWA TO 1900-27-00-0001.Jun 17, 1997 · N237YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM946Flap · crackedDURING ROUTINE A .375 INCH CRACK WAS FOUND ON THE 'DOVETAIL'. REPAIRED IAW SRM AND AMWA T.O 1900 27 00 0001. (M)May 28, 1997 · N237YV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX2778Flap · crackedDURING ROUTINE MAINTENANCE, A CRACK WAS FOUND ON RT INBOARD FLAP. REPAIRED IAW SRM AND AMW TO.Apr 23, 1997 · N237YV · Beech 1900D · Trailing Edge Flaps
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