N155ZV, cancelled May 6, 2011

Service difficulty reports · 20

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 = 'N155ZV' AND deregistration_id = 'N155ZV-2011-05-06'
  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 AMWA1019019Spar · crackedDURING DETAIL INSPECTION, RT AFT SPAR FLANGE AT WS117.5 WAS FOUND TO BE CRACKED FROM RIVET TO EDGE OF FLANGE. MAINTENANCE OBTAINED APPROVED DATA, PERFORMED REPAIR AND CLEARED DISCREPANCY.Nov 8, 2007 · N155ZV · Beech 1900D · Wing SparSDR AMWA1001016Skin · dentedRT CENTER LEADING EDGE AT APPROXIMATELY WS 54.45 HAD BIRD STRIKE DAMAGE EXCEEDING STRUCTURAL REPAIR MANUAL LIMITS. OBTAINED APPROVED DATA, REPAIRED LEADING EDGE AND CLEARED DISCREPANCY.Nov 8, 2007 · N155ZV · Beech 1900D · Wing, Plate/SkinSDR AMWA87352Indication Sys · smokeON TAXI OUT CAPT NOTED SMOKE AND ELECTRICAL ODOR WHICH APPEARED TO BE COMING FROM CAPT'S EFIS SYSTEM. CREW DECIDED TO RETURN TO GATE WITH NO FURTHER INCIDENT. CND ON GROUND, SYSTEM OPS CHECKS NORMAL. REMOVED AND REPLACED CAPT EFIS SCREEN FOR PRECAUTIONARY MSep 11, 2007 · N155ZV · Beech 1900D · Flight Environment DataSDR AMWA15036AFrame · chafedFUSELAGE FRAME AT FS 438.25 LT HAD CHAFFING. REPAIRED IAW ACFT ENGINEERING REPORT NR 6772-2 REV 1R.Jul 10, 2007 · N155ZV · Beech 1900D · Fuselage Main, FrameSDR AMWA15036CSkin · chafedFRICTION CHAFFING CREATED WORN SEGMENTS ON THE RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE. DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW ENGINEERING REPORT NR 6772-1 REV 1R.Jul 10, 2007 · N155ZV · Beech 1900D · Wing, Plate/SkinSDR AMWA15036BSkin · chafedFRICTION CHAFFING CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE. DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW ENGINEERING REPORT NR 677201 REV 1R.Jul 10, 2007 · N155ZV · Beech 1900D · Wing, Plate/SkinSDR AMWA15036Spar · corrodedCORROSION LT AND AFT MAIN SPAR FLANGE. REPAIRED IAW ENGINEERING REPORT NR 6772-3 REV A DATED JUN 25, 2007.Jul 9, 2007 · N155ZV · Beech 1900D · Wing SparSDR AMWA81813Landing Gear · malfunctionedWHEN GEAR WAS EXTENDED FOR LANDING, THE RT MAIN GEAR DID NOT SHOW DOWN AND LOCKED. THE CREW DECLAIRED AN EMERGENCY AND FOLLOWED EMERGENCY PROCEDURES, BY PUMPING THE GEAR DOWN. THE AIRCRAFT THEN LANDED SAFELY WITH NO FURTHER INCIDENT.Jan 3, 2007 · N155ZV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 1060918030Oil System · low pressureAFTER TAKEOFF ON CLIMBOUT LEFT OIL PRESSURE ANNUNCIATOR ILLUMINATED & OIL PRESSURE WAS BELOW 60 PSI ON INDICATOR AT 3500 LB TORQUE. CREW SHUT ENGINE DOWN AND RETURNED TO FIELD WITHOUT FURTHER INCIDENT. NOTE: INFORMATION IN COMPUTER BLOCKS IS FOR GAS GENERATOSep 18, 2006 · N155ZV · Beech 1900D · Turbine Engine Oil SystemSDR 76087Trim Panel · looseAFTER ARRIVAL INTO PIT, THE CREW REPORTED THAT THE DOOR WOULD NOT OPEN FROM THE OUTSIDE. THE CREW THEN OPENED THE DOOR FROM THE INSIDE NORMALLY. MAINTENANCE RE-SECURED TRIM PIECE AND TRIM BACK.Feb 27, 2006 · N155ZV · Beech 1900D · Passenger/Crew DoorsSDR 1051229025Spar Cap · corrodedCORROSION ON LT WING MAIN SPAR FWD SPAR CAP FLANGE. FOUND DURING INSPECTIONFeb 15, 2006 · N155ZV · Beech 1900D · Wing SparSDR 1051229028ASpar Cap · corrodedBIO CORROSION ON RIGHT WING MAIN SPAR CAP FLANGE NEAR WS 124588. MAINTENANCE FOUND DURING INSPECTION.Feb 15, 2006 · N155ZV · Beech 1900D · Wing SparSDR 1051229028Spar Cap · corrodedBIO CORROSION ON LEFT WING MAIN SPAR FWD SPAR CAP FLANGE. FOUND DURING INSPECTION.Feb 15, 2006 · N155ZV · Beech 1900D · Wing SparSDR 62795Wire · damagedAFTER TAKEOFF, GEAR HANDLE WAS PLACED IN UP POSITION. LANDING GEAR INTRANSIT LIGHTS AND AURAL HORN DID NOT EXTINGUISH AIRCRAFT RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. REPAIRED BROKEN WIRES AT TB152 AND REPAIRED BAD SPLICES AT A406 PCB. Jul 5, 2004 · N155ZV · Beech 1900D · Landing Gear System WiringSDR 57841Downlock · inoperativeAFTER NORMAL EXTENSION OF LANDING GEAR RT MAIN DID NOT SHOW DOWN AND LOCK AFTER TOWER FLY BY. A/C LANDED WITH NO FURTHER INCIDENT. REPLACED RT MAIN GEAR DOWN LOCK SWITCH AND HARNESS ASSY, RIGGED SWITCHES AND PERFORMED GEAR SWINGS AS REQUIRED. OPS CK GOOD.Jan 12, 2004 · N155ZV · Beech 1900D · Landing Gear Position and WarningSDR MASA97154Actuator · failedAIRSHUTTLE 5547 - BWI-BDR - UPON DESCENT IN BDR, THE CREW SELECTED GEAR DOWN AND DID NOT GET GEAR DOWN AND LOCKED INDICATION. THE CREW DECLARED AND EMERGENCY AND LANDED IN BDR WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACTUATSep 17, 1997 · N155ZV · Beech 1900D · Landing Gear ActuatorSDR 97ZZZX3305Attach Bracket · excess wearFLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. Jul 11, 1997 · N155ZV · Beech 1900D · Trailing Edge FlapsSDR 97ZZZX3304Attach Bracket · excess wearFLEET CAMPAIGN, 'MAINTENANCE INSPECTED THE LT AND RT OTBD FLAP ATTACHMENT BRACKETS AND THE AFT ROLLER BEARING IAW RAYTHEON ACFT CO (RAC) SAFETY COMMUNIQUE NR 137 DATED MAY, 1997. FOUND ATTACHMENT BRACKETS WITH EXCESSIVE WEAR AND AFT ROLLER BEARINGS BINDING. Jul 11, 1997 · N155ZV · Beech 1900D · Trailing Edge FlapsSDR MASA97034Windshield · warpedDURING MAINTENANCE, COPILOT'S WINDSHIELD WOULD NOT HEAT WHEN LOW WAS SELECTED. T/S SYSTEM AND FOUND THE WINDSHIELD WAS FAULTY. MAINTENANCE REMOVED AND REPLACED THE RT WINDSHIELD IAW BMM, OPS CHK GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (X)Jun 2, 1997 · N155ZV · Beech 1900D · Flight Compartment WindowsSDR 95ZZZX4168Rivets · looseRIVETS LOCATED IN RT WING OUTBOARD OF NACELLE TOP SPAR AREA LOOSE CAUSING FUEL LEAK. VERY COMMON OCCURRENCE WITH APPROXIMATELY A 6-10 RIVET LENGTH ALONG TOP WING SPAR.Jun 22, 1995 · N155ZV · Beech 1900D · Wing Miscellaneous Structure
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