N548GA

Service difficulty reports · 23

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 = 'N548GA' 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 HYIA20251027001Fitting · corrodedDURING MAINTENANCE A SMALL AREA OF SURFACE CORROSION WAS VISUALLY IDENTIFIED ON THE TOP FACE OF THE VERTICAL LEG OF THE 0822550-43 WING ATTACH FITTING (LT LOWER AFT). THIS CORROSION MEASURES APPROXIMATELY 1.5 INCHES LONG, BY .125 INCHES WIDE WITH AN APPROXIMATOct 24, 2025 · N548GA · Cessna 402C · Wing, Attach FittingsSDR HYIA20251013001Beam · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE INBOARD FACE OF THE RIGHT INBD ENGINE BEAM IN THE AREA OF THE VERTICAL ATTACH CHANNELS FOR THE CROSSOVER BEAM. THIS CRACK WAS DISCOVERED AFTER CHANGING THE CROSSOVER BEAM VERTICAL ATTACH BRACKET P/N: 5654107-15 Oct 9, 2025 · N548GA · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20230425001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE OUTBOARD LEG OF THE RIGHT HAND INBOARD NACELLE FITTING, (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .250 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXApr 23, 2024 · N548GA · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20240131001Fitting · crackedWHILE PERFORMING THE LIGHTED BORESCOPE PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02 R2 TO SATISFY AS2017-10-19, A CRACK WAS IDENTIFIED ON THE OUTBOARD SIDE OF THE RIGHT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES .0799 IN LENGTH AND ITS LOCATION IS CONSIJan 29, 2024 · N548GA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20210603001Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB (P/N: 5122115-55) AT L.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 AND TRAVELS FORWARD AN APPRJun 1, 2021 · N548GA · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20190226001Crossbeam · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CROSSOVER BEAM (P/N: 5654104-11). THIS CRACK IS IN THE AREA OF THE EXHAUST MOUNT FOR THE INBOARD EXHAUST ELBOW (APPROXIMATELY LEFT WING STATION: 87.44) THE CRACK MEASURES APPROXIMATELY 1.964 INCHES IN Feb 25, 2019 · N548GA · Cessna 402C · Nacelle/Pylon StructureSDR HYIA20171017002Beam · crackedWHILE PREFORMING OTHER MAINTENANCE, A CRACK WAS DISCOVERED IN THE AFT OUTBOARD SIDE OF THE RT INBOARD ENGINE BEAM. THE FASTENER HOLE WAS OUT OF TOLERANCE FOR THE PRESCRIBED FASTENER. THE BEAM WAS REPLACED.Oct 9, 2017 · N548GA · Cessna 402C · Engine Mount SectionSDR HYIA20171017001Fitting · crackedWHILE CONDUCTING SID 57-10-16 INSPECTION, TWO CRACKS WERE DISCOVERED ON THE OUTBOARD SIDE OF THE INBOARD FITTING, JUST FORWARD OF THE SPAR STRAP. THE FITTING WAS REPLACED.Oct 9, 2017 · N548GA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170822002Exhaust Valve · damagedCREW REPORTED 'INTERMITTENT ENGINE MISFIRE IN FLIGHT. NO PRECAUTIONARY ACTIONS WERE TAKEN BY THE CREW AND THE ACFT LANDED SAFELY AT ITS INTENDED DESTINATION WITH NO ISSUES. INSPECTION DISCOVERED LOW DIFFERENTIAL COMPRESSION CHECK RESULT AT CYLINDER NR 5 FOR Aug 19, 2017 · N548GA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20170828010Fitting · crackedDURING A SID 57-10-16 INSPECTION, A CRACK WAS DISCOVERED IN THE LT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .145 IN LENGTH.May 4, 2017 · N548GA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170221001Pump · leakingTHE PILOT REPORTED HEATER FAILED IN FLIGHT, MAY WORK ON THE GROUND. ADDITIONALLY INDICATED AN ODOR OF GAS ON CLIMB OUT. MAINTENANCE INSPECTED THE HEATER AND FOUND THE HEATER FUEL PUMP LEAKING. REMOVED AND REPLACED THE HEATER FUEL PUMP. AFTER CONDUCTING AN OPFeb 20, 2017 · N548GA · Cessna 402C · Heating SystemSDR HYIA20151203003Pump · defectivePILOT REPORTED FUEL SMELL WITH HEATER RUNNING IN FLIGHT. R & R THE HEATER FUEL PUMP & HEATER FUEL LINE. OPERATIONAL CHECKED GOOD.Nov 26, 2015 · N548GA · Cessna 402C · Heating SystemSDR HYIA20151124001Unknown · odorPILOT REPORTED STRONG FUEL SMELL IN CABIN WITH HEATER ON. INSPECTED HEATER FUEL LINES WITH NO LEAKS NOTED. AS PRECAUTION, CLEANED HEATER SPARK PLUG & FUEL NOZZLE. OPERATIONALLY CHECKED GOOD.Nov 18, 2015 · N548GA · Cessna 402C · Air Distribution SystemSDR HYIA20140414038Drag 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 29, 2012 · N548GA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415047Drag 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 Apr 12, 2011 · N548GA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA548GARTGRUplock Hook · wornCREW REPORTED, AFTER TAKEOFF, UPON GEAR RETRACTION, GREEN DOWNLOCK LIGHTS EXTINGUISHED, HYD PRESSURE LIGHT REMAINED ILLUMINATED ALONG WITH RED GEAR UNSAFE LIGHT. LANDING GEAR CONTINUED TO CYCLE IN AND OUT OF THE WHEEL WELLS. AFTER LEVELING AT 1000 FT, EMERGENCJan 21, 2011 · N548GA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA548GAHTRLimit Switch · shortedCREW REPORTED, WHILE IN CRUISE, SMOKE APPEARED IN THE CABIN, ALONG WITH A ELECTRICAL ODOR. EMERGENCY WAS DECLARED, AFTER WHICH ALL ELECTRICAL EQUIPMENT WAS TURNED OFF. FUEL SUPPLY TO HEATER WAS ALSO SHUT OFF. AFTER SEVERAL MINUTES, THE SMOKE AND ODOR DISSIPATEDec 24, 2010 · N548GA · Cessna 402C · Heating SystemSDR HYIA548GALENGEngine · unserviceableCREW REPORTED LT ENGINE POWER LOSS ENROUTE. ENGINE WAS SECURED AND PROPELLER FEATHERED. CREW ELECTED TO DIVERT TO HYA WHERE AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND 3 INCH DIAMETER HOLE IN RIGHT CRANKCASE HALF. MAINTENSep 17, 2009 · N548GA · Cessna 402C · Engine (Reciprocating)SDR 04052005Uplock Switch · inoperativeAIRCRAFT HAD THE HYDRAULIC LIGHT REMAIN ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE WAS UNABLE TO DUPLICATE, THE LT DOWNLOCK SWITCH WAS RESEALED AND LUBRICATED, FLIGHT CHECK UNSATISFACTORY, STILL UNABLE TO DUPLICATE ON GROUND, REPLACED NOSE UPLOCK SWITCH ANApr 5, 2005 · N548GA · Cessna 402C · Landing Gear Position and WarningSDR HYI2003F00004Pin · shearedTACHOMETER INOPERATIVE, RT DRIVE GEAR DOWEL PIN BROKE ON OIL PUMP GEAR. REMOVED OIL PUMP HOUSING COVER, REPLACED DRIVE PIN AND REINSTALLED COVER.Mar 27, 2003 · N548GA · Cessna 402C · Reciprocating Engine Oil SystemSDR HYI2001F00012Master Switch · failedON PREFLIGHT INSPECTION, AVIONICS MASTER SWITCH FAILED. MAINTENANCE REPLACED SWITCH AND RETURNED AIRCRAFT TO SERVICE.Nov 19, 2001 · N548GA · Cessna 402C · DC Power Distribution SystemSDR 20001205SH009Pin · brokenDURING FLIGHT, UPPER CABIN DOOR OPENED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FORWARD LATCH PIN BROKEN AT BELLCRANK ATTACH POINT. REPLACED LATCH PIN AND ASSIST SPRINGS AND RELEASED THE AIRCRAFT BACK TO SERVICE. (X)Nov 3, 2000 · N548GA · Cessna 402C · Passenger/Crew DoorsSDR 20000907SH038Bearing · destroyedPILOT REPORTED LOSS OF POWER ON TAKEOFF. MAINTENANCE FOUND PROPELLER GOVERNOR LEAKING OIL AND CONFIRMED POWER LOSS. CHANGED GOVERNOR AND RETURNED AIRCRAFT TO SERVICE. TEAR DOWN OF GOVERNOR REVEALED INTERNAL FAILURE CAUSED BY BEARING FAILURE. (X)May 12, 2000 · N548GA · Cessna 402C · Propeller Governor
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