N4652N, cancelled Apr 17, 2021

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 = 'N4652N' AND deregistration_id = 'N4652N-2021-04-17'
  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 HYIA20171226001Cylinder · failedPILOT REPORTED RIGHT ENGINE RUNNING ROUGH. UPON INSPECTION FOUND THE RIGHT ENGINE NR 3 CYLINDER TO HAVE LOW COMPRESSION AND THE CYLINDER EXHAUST VALVE TO HAVE EVIDENCE OF A BURNING. THE CYLINDER WAS REPLACED.Dec 22, 2017 · N4652N · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20171213001Fitting · crackedTHE RT OB NACELLE FITTING PART NUMBER 5292029-24 WAS FOUND TO BE CRACKED DURING BORESCOPE INSPECTION PRESCRIBED BY TEXTRON MULTI-ENGINE SERVICE LETTER MEL-54-02R2 DATED MARCH 29, 2017 AS CONTINUING ACTION REQUIRED BY AD2017-10-09. THE CRACK IS FAINT BUT VDec 12, 2017 · N4652N · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20161108194Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 30, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161108193Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Oct 30, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20161018001Exhaust Pipe · crackedPILOT REPORTED ON PREFLIGHT: RIGHT ENGINE MAIN EXHAUST STACK LOOSE. UPON INSPECTION MAINTENANCE FOUND THE RIGHT OVERBOARD EXHAUST PIPE CRACKED. REPLACED OVERBOARD EXHAUST PIPE.Oct 16, 2016 · N4652N · Cessna 402C · Engine Collector/Tailpipe/NozzleSDR HYIA20160825091Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Aug 22, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160825090Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Aug 22, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160825089Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Aug 22, 2016 · N4652N · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160511001Unknown · odorPILOT DETECTED SMELL OF BURNING RUBBER IN FIRST OFFICERS FLOORBOARD AREA. PERFORMED A DETAILED VISUAL INSPECTION ON THE FOLLOWING ACFT AREAS & COMPONENTS, MLG BRAKES, MLG WHEELS ASSEMBLY, LT & RT WW, NLG WHEEL ASSEMBLY & WW, COCKPIT AREA, CONTROL PEDESTAL, BOMay 5, 2016 · N4652N · Cessna 402C · Air Distribution SystemSDR HYIA20141212001Sealant · faultyPILOT REPORTED SMELL OF FUEL IS CONSTANT WITHIN CABIN. MX IS IN PROCESS OF RESEALING FAULTY SEALANT IN THE WING TANKS.Dec 10, 2014 · N4652N · Cessna 402C · Fuel StorageSDR HYIA20140624002Web · crackedDURING SCHEDULED INSPECTION, MULTIPLE WEB FLANGE CRACKS WERE FOUND AT AFT FUSELAGE CARRY THROUGH SPAR ASSEMBLY PN 5211173-2 AT CTR UPPER SECTION FWD & AFT WEBS. THIS DAMAGE AREA DIRECTLY CORRESPONDS TO CTR CABIN FLOORBOARD AREA & IS PRONE TO DAMAGE AS PAXS & Jun 23, 2014 · N4652N · Cessna 402C · Fuselage Miscellaneous StructureSDR HYIA20140624001Beam · crackedDURING VISUAL INSPECTION OF NACELLE STRUCTURE AT TURBOCHARGER REMOVAL FOR OTHER MAINTENANCE, THE RT NACELLE CROSSOVER BEAM WAS FOUND TO BE CRACKED AT TURBOCHARGER MOUNT BRACKET ATTACH HOLE AFT SIDE OF BEAM. CORRECTIVE ACTION WILL BE TO R & R BEAM WITH NEW OEMJun 23, 2014 · N4652N · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20140621001Spar Cap · corrodedDURING SCHEDULED INSPECTION, AREAS OF EXFOLIATING CORROSION WERE FOUND AT RT WING LWR SPAR CAP STRAP OEM PN 5292029-2 PREVIOUSLY INSTALLED TO SATISFY REQUIREMENT OF AD2005-12-13 CONCURRENT WITH MEB02-5. THE CORRECTIVE ACTION WILL BE TO PERFORM A DETAILED INSPJun 20, 2014 · N4652N · Cessna 402C · Wing SparSDR HYIA20140414053Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEAug 9, 2013 · N4652N · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414027Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, 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 BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & ANov 7, 2012 · N4652N · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA2012052200001Engine · power lossRT ENGINE LOST POWER, VIBRATED SUDDENLY. INSPECTED ENGINE, CHECKED PARAMETERS, PERFORMED COMPRESSION CHECK, ADJUSTED IDLE FUEL MIXTURE, CHECKED RT WING TANK SUMP FOR WATER, PERFORMED RUN UP, COULD NOT DUPLICATE, FCF CHECKS GOOD.May 22, 2012 · N4652N · Cessna 402C · Engine (Turbine/Turboprop)SDR HYIA20140414008Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE, 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 BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & AAug 11, 2011 · N4652N · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415008Drag 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 21, 2011 · N4652N · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA4652NRMLGTrunnion · shearedCREW REPORTED, RT MLG SHEERED OFF ON LANDING ROLL. MX FOUND RT MLG UPPER BARREL AND TRUNNION ASSY SHEARED JUST BELOW MLG ACTUATOR ATTACH POINT. MX REMOVED AND REPLACED RT MLG ASSY, RT PROPELLER, RT ENG, RT SIDE INBD AND OTBD FLAP PANEL ASSEMBIES, AND RT LANAug 31, 2009 · N4652N · Cessna 402C · Fuselage, Landing Gear Attach FittingsSDR 13552N122707Skin · debondedON TAXI IN, CREW NOTICED DEBONDING HAD TAKEN PLACE ON RT AILERON UPPER IB SKIN. THE DISPLACEMENT OF SKIN DID NOT AFFECT THE FLIGHT CHARACTERISTICS OF THE AIRCRAFT AS NOTED BY THE CREW. MX REMOVED AND REPLACED AILERON, DISPENSED AILERON FOR REPAIR.Dec 26, 2007 · N4652N · Cessna 402C · AileronsSDR 2002FA0000897Angle · separatedCOULD NOT MOVE AILERONS. 90 PERCENT ANGLE, USED TO PREVENT OIL CANNING, BONDED INSIDE AILERON, BROKE LOOSE AND WORKED ITS WAY DOWN TRAILING EDGE OF AILERON AND INTO FLAP TRAILING EDGE, PREVENTING AILERONS FROM MOVING. 90 PERCENT ANGLE IS 8 INCHES LONG AND .3Jul 12, 2002 · N4652N · Cessna 402C · AileronsSDR 20000907SH039Tire · unserviceableCREW REPORTED UNUSUAL NOISE ON TAXI. FOUND CHUNK OF AFT TIRE MISSING. MAINTENANCE DISPATCHED TO CHANGE TIRE. FOUND LARGE PORTION OF RECAP HAD SEPARATED FROM CORE TIRE. MAINTENANCE REMOVED AND REPLACED TIRE AND RELEASED AIRCRAFT BACK INTO SERVICE. (X)Aug 14, 2000 · N4652N · Cessna 402C · Tire
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