N171ZV, cancelled Jun 6, 2012

Service difficulty reports · 17

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 = 'N171ZV' AND deregistration_id = 'N171ZV-2012-06-06'
  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 BSAASDR0724Shutoff Valve · inoperativeDURING CLIMB THE LEFT ENVIROMENTAL FAIL LIGHT ILLUMINATED AND WOULD NOT RESET. UPON RETURN TO BOSTON THE DISCREPANCY WAS INITIALLY DEFERRED. AFTER RETURN TO BOSTON THE RT PRESSURE REGULATING SHUT OFF VALVE WAS REMOVED AND REPLACED. GROUND CHECK GOOD.Sep 16, 2007 · N171ZV · Beech 1900D · Air Distribution SystemSDR BSAASDR0714Fire Loop · false indicationRIGHT FIRE LOOP ANNUNCIATOR ILLUMINATED WHEN VECTORED TO FINAL (DESCENT) INTO BOSTON. CREW LANDED WITHOUT INCIDENT. THE RIGHT FORWARD ENGINE FIRE LOOP WAS REMOVED AND REPLACED, AND AN OPERATIONAL CHECK ON THE SYSTEM WAS PERFORMED.May 16, 2007 · N171ZV · Beech 1900D · Fire DetectionSDR BSAASDR0616Tube · blownDURING CLIMBOUT, AT 500FT AGL, LT ENVIRO FAIL LIGHT CAME ON, CREW DEACTIVATED LT BLEED SYSTEM, LIGHT STAYED ON. CREW RETURNED TO FIELD. MX FOUND & REPAIRED LEAK IN THE LT BLEED AIR EVA TUBING.Jun 24, 2006 · N171ZV · Beech 1900D · Engine Bleed Air SystemSDR BSAASDR0606Bonding Jumper · looseCREW WAS DESCENDING WHEN SMOKE WAS NOTED IN THE COCKPIT, APPROXIMATELY 15 TO 20 MNIUTES FROM DESTINATION. CREW DECLARED EMERGENCY, CONTINUED DESCENT, AND LANDED WITH NO FURTHER INCIDENTS. THE WINDSHIELD HEAT WAS TURNED ON THE TIME. A LOOSE GROUND LEAD WIRE Feb 22, 2006 · N171ZV · Beech 1900D · Windshield/Door Rain/Ice RemovalSDR 65858Transducer · fluctuatesRT OIL PRESSURE WAS FLUCTUATING FROM 60-95 PSI AIRCRAFT DIVERTED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED OIL PRESSURE TRANSDUCER AND FILTER. P/N 101-389023-5 S/N 7034-5-380Oct 15, 2004 · N171ZV · Beech 1900D · Engine Oil PressureSDR 64378Powerpack · failedWHEN MAIN LANDING GEAR HANDLE WAS DOWN SELECTED, MAIN LANDING GEAR WOULD NOT EXTEND 2 AMP CB POPPED. CREW FOLLOWED PROCEDURES MANUALLY EXTENDED LANDING GEAR. GOT 3 GOOD DOWN AND LOCKED INDICATIONS. LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED MOTOAug 29, 2004 · N171ZV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 55918Uplock Switch · malfunctionedCREW REPORTED WITH LANDING GEAR RAISED INTRANSIT LIGHTS REMAINED ILLUM. CREW DECLARED AN EMERGENCY, AND RETURNED TO FIELD WITH NO FURTHER INCIDENTS. ACFT FERRIED TO DUJ FOR MAINTENANCE. GEAR INTRANSIT LIGHT W/N EXTINGUISH WHEN UP. REMOVED AND REPLACED RT GENov 7, 2003 · N171ZV · Beech 1900D · Landing Gear Position and WarningSDR 050849Gas Generator · failedON APPROACH ON FLIGHT 5547 ARRIVING FROM PITTSBURGH PENNSYLVANIA TO WATERTOWN NEW YORK, THE LEFT ENGINE ITT EXCEEDED LIMITS. THE ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED May 20, 2003 · N171ZV · Beech 1900D · Turbine SectionSDR 050516Solenoid · stuckON FLIGHT 5534 UPON THE TAKEOFF ROLL THE RIGHT ENGINE WOULD ONLY GO TO 1550 RPM. THE CREW ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LOW PITCH SOLENOID TO BE STUCK. MAINTENANCE CLEANED AND LUBED THE SOLENOID.May 7, 2003 · N171ZV · Beech 1900D · Propeller SystemSDR 044910Truss · crackedWHILE PERFORMING AN "H" CHECK ON LT ENGINE TRUSS, MAINT FOUND A CRACK AT THE OUTBOARD COWLING ATTACH BRACKET. MAINT R & R WITH ANOTHER TRUSS. UPON RECEIPT OF OLD TRUSS, VENDOR DID A REPORT. REPORT REVEALED THAT A CRACK AT BOTH UPPER COWLING BRACKETS AND CHANov 7, 2002 · N171ZV · Beech 1900D · Engine Mount SectionSDR 98ZZZM900Skin · crackedOVERNIGHT MAINTENANCE, FOUND .5 INCH CRACK IN LHOB FLAP 29.5 INCH FROM OUTBOARD EDGE AND 15 INCH FROM TRAILING EDGE ON BOTTOM SKIN. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M)Mar 28, 1998 · N171ZV · Beech 1900D · Trailing Edge FlapsSDR 98ZZZM154Skin · crackedICT - OVERNIGHT MAINTENANCE FOUND .5 INCH CRACK IN SKIN ON LEFT OUTBOARD FLAP 26 .25 INCH FROM OUTBOARD END AND 11.75 INCH FROM TE. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)Dec 1, 1997 · N171ZV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZM1199Indicator Assy · failedFLT 5737 - ON APPROACH TO MCI FROM OMA THE RIGHT LANDING GEAR ANNUNCIATOR GREEN LIGHT DID NOT ILLUMINATE. THE LANDING GEAR WARNING HORN DID NOT SOUND AND THE GEAR HANDLE INTRANSIT LIGHTS WERE EXTINGUISHED. EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUTSep 18, 1997 · N171ZV · Beech 1900D · Landing Gear Position and WarningSDR 97ZZZX4167Flap · crackedDURING ROUTINE INSPECTION OF FLAP, A CRACK ON THE 'DOVETAIL' WAS FOUND. REPAIRED WITH DOUBLER.Jun 26, 1997 · N171ZV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX4166Flap · crackedDURING ROUTINE MAINTENANCE, THE RT INBOARD FLAP WAS FOUND TO HAVE A CRACK. REPAIRED IAW AMWA T.O. AND SRM.Jun 4, 1997 · N171ZV · Beech 1900D · Trailing Edge FlapsSDR 96ZZZX2794Blade · splitDURING ROUTINE MAINTENANCE, THE TRAILING EDGE WAS FOUND SPLIT APPROXIMATELY 2.5 INCHES. REPAIRED IAW HARTZELL MM AND FORM 8110-3.Feb 19, 1996 · N171ZV · Beech 1900D · Propeller Blade SectionSDR 96ZZZX114Gas Shock · bentWHEN CLOSING THE CARGO DOOR, THE GAS SHOCK BENT. REMOVED AND REPLACED GAS SHOCK.Oct 4, 1995 · N171ZV · Beech 1900D · Cargo/Baggage Doors
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