N247GS

Service difficulty reports · 22

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 = 'N247GS' 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 HYIA20240828001Fitting · crackedWHILE PERFORMING THE LIGHTED BORESCOPE PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02 R2 TO SATISFY AD2017-10-19, A CRACK WAS IDENTIFIED ON THE OUTBOARD SIDE OF THE LEFT-HAND OUTBOARD FITTING. THIS CRACK MEASURES .152 IN LENGTH AND IS CONSISTENT WITH OTHERS FOUNDJul 11, 2024 · N247GS · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20210305001Ignition Unit · meltedTHE PILOT REPORTED THAT DURING A TURN ONTO THE RUNWAY THE AIRCRAFT THE WING DROPPED AND THE AIRCRAFT WOULD NOT ROLL. THE RIGHT TIRE WAS FOUND TO BE LEANING AGAINST THE STRUT. MAINTENANCE INSPECTED AND FOUND THE RIGHT AXLE TO BE CRACKED. REMOVED AND REPLACED THMar 3, 2021 · N247GS · Cessna 402C · Heating SystemSDR HYIA2020040627001Static Line · distortedPILOT REPORTED BURNING ODOR IN THE CABIN. UPON INSPECTION, MAINTENANCE FOUND STATIC LINE DISTORTED. TROUBLESHOT HEATER, AND FOUND OPERATIONAL. INSPECTED BAY AREA, HEATER DUCTS, COMBUSTION BLOWER, FUEL PUMP, THERMOSTAT, AIRFLOW SWITCH, HEATER SWITCH AND WIRINMar 27, 2020 · N247GS · Cessna 402C · Pitot/Static SystemSDR HYIA20200326001Static Line · out of adjustPILOT REPORTED BURNING ODOR IN THE CABIN. UPON INSPECTION, MAINTENANCE FOUND STATIC LINE IN FRONT OF THE RIGHT FORWARD VENT. THE LINE WOULD BECOME PLIABLE WITH HEAT BUT WAS UNDAMAGED. REPOSITIONED LINE, INSPECTED BAY AND NO FURTHER DEFECTS NOTED.Mar 25, 2020 · N247GS · Cessna 402C · Pitot/Static SystemSDR HYIA20200227002Cylinder · brokenPILOT REPORTED ROUGH RUNNING RIGHT ENGINE ON CLIMB OUT. MAINTENANCE INSPECTED AND FOUND THE NUMBER 6 CYLINDER EXHAUST VALVE TO BE BROKEN AND THE NUMBER 4 CYLINDER DAMAGED. REPLACED BOTH CYLINDERS AND RELEASED TO SERVICE.Feb 22, 2020 · N247GS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA2020022700002Cylinder · low pressurePILOT REPORTED ROUGH RUNNING RIGHT ENGINE ON CLIMB OUT. MAINTENANCE INSPECTED AND FOUND THE NUMBER 6 CYLINDER EXHAUST VALVE TO BE BROKEN AND THE NUMBER 4 CYLINDER DAMAGED. REPLACED BOTH CYLINDERS AND RELEASED TO SERVICE.Feb 22, 2020 · N247GS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20200106001Rib · crackedDURING MAINTENANCE A CRACK WAS VISUALLY DISCOVERED ON THE RIGHT HAND CLOSEOUT RIB (P/N: 5122115-56) AT R.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE. THE CRACK TRAVELJan 3, 2020 · N247GS · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20161109206Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 6, 2016 · N247GS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161109205Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 6, 2016 · N247GS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160812065Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE CRACKED AND DISPLAYS EVIDENCE OF HEAT DAMAGE.Aug 6, 2016 · N247GS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160812064Exhaust Valve · crackedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE CRACKED AND DISPLAYS EVIDENCE OF HEAT DAMAGE.Aug 6, 2016 · N247GS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160712001Lifter · corrodedDURING OTHER UNSCHEDULED MAINTENANCE AND INSPECTION OF ENGINE HYDRAULIC LIFTER ON THE RIGHT ENGINE, THE NR 4 CYLINDER WAS FOUND PITTED. MAINTENANCE REPLACED THE LIFTER IAW MM 72-40-09Jul 2, 2016 · N247GS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA201608003019Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Jul 1, 2016 · N247GS · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA2015022002Nut · crackedDURING INSPECTION FOUND ENG THROUGH BOLT NUT PN 652541 CRACKED ON THE NR 3 CYLINDER, CAUSING THE BOLT TO BACK OUT. NEW THROUGH BOLT NUTS ARE USED AT EACH OVERHAUL.Feb 19, 2015 · N247GS · Cessna 402C · Reciprocating Engine Power SectionSDR HYIA20150220003Nut · crackedDURING INSPECTION FOUND ENGINE THROUGH BOLT NUT CRACKED ON THE NR 3 CYLINDER, CAUSING THROUGH BOLT TO BACK OUT.Feb 19, 2015 · N247GS · Cessna 402C · Engine (Reciprocating)SDR HYIA20150220002Nut · crackedDURING INSPECTION FOUND ENG THROUGH BOLT NUT PN 652541 CRACKED ON THE NR 3 CYLINDER, CAUSING THROUGH BOLT TO BACK OUT.Feb 19, 2015 · N247GS · Cessna 402C · Reciprocating Engine Power SectionSDR HYIA20140623001Axle · crackedWHILE TURNING TO LINE UP WITH RUNWAY CENTERLINE, DIFFICULT TO TURN ACFT RT. ACFT ONLY TURNED TO THE LT. INSPECTION OF LT MLG FOUND WHEEL ASSEMBLY LEANED AGAINST LG. FURTHER INSPECTION FOUND LG AXLE TO BE CRACKED.Jun 17, 2014 · N247GS · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA20140415044Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, OEM PN 5142002-5, WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDUREApr 5, 2011 · N247GS · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415003Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 19, 2011 · N247GS · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA247GSAVIONICSRadio · malfunctionedON DESCENT, CREW REPORTED BOTH COMMMUNICATION RADIOS FAILED TO TRANSMIT OR RECEIVE. EMERGENCY WAS DECLARED, LANDING WAS UNEVENTFUL. MX INSPECTED ACFT, ALL SYS CHECKED NORMAL. COULD NOT DUPLICATE COMMUNICATION FAILURE. ACFT RELEASED BACK TO SERVICE.May 27, 2010 · N247GS · Cessna 402C · Communications SystemSDR HYIA1352471Bulkhead · corrodedBULKHEAD LOCATED ON THE RIGHT FUSELAGE WALL JUST AFT OF FIRST OFFICERS SIDE WINDOW AT FUSELAGE STATION 154.5 FOUND TO BE CORRODED BEYOND MANUFACTURERS LIMITS. REMOVED CORRODED AREA AND SPLICED IN NEW BULK HEAD.Oct 22, 2007 · N247GS · Cessna 402C · Fuselage Main, BulkheadSDR 1350522N247GSCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.Aug 19, 2006 · N247GS · Cessna 402C · Electrical Power System
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