Cessna 402C

Service difficulty reports · 1,781

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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 aircraft_model_key = '402C'
  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 HYIA20261022001Beam · crackedDURING SCHEDULED ENGINE BEAM REPLACEMENT, UPON REMOVAL OF ENGINE BEAM A CRACK WAS VISUALLY IDENTIFIED ON THE INBOARD FACE OF THE ENGINE BEAM. THIS CRACK IS EMANATING FROM A FASTENER LOCATION COMMON TO THE INBOARD VERTICAL CROSS OVER BEAM UPRIGHT (OEM: 5654107-Oct 20, 2026 · N160PB · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20261001001Beam · crackedDURING HIGH TIME ENGINE BEAM REPLACEMENT, UPON REMOVAL OF ENGINE BEAM A CRACK WAS VISUALLY IDENTIFIED ON THE INBOARD FACE OF THE RH INBOARD ENGINE BEAM. THIS CRACK IS EMANATING FROM A FASTENER LOCATION COMMON TO THE INBOARD VERTICAL CROSS OVER BEAM UPRIGHT (OESep 30, 2026 · N290CA · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20260923002Fitting · corrodedDURING SCHEDULED WING FITTING INSPECTION, A SMALL AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND FORWARD UPPER WING ATTACH FITTING. THIS CORROSION MEASURES APPROXIMATELY .500 INCHES LONG, .125 INCHES WIDE, AND .020 INCHES DEEP ON THE TOP FACE OF THSep 21, 2026 · N3249M · Cessna 402C · Wing, Attach FittingsSDR HYIA20260827001Fitting · crackedDURING MAINTENANCE, A CRACK WAS IDENTIFIED ON THE INBD LEG OF THE RT INBD NACELLE FITTING, THIS CRACK MEASURES APPROXIMATELY .144 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN MEL-54-02R2 TO SATISFY AD2017-10-0Aug 25, 2026 · N678JG · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20260818001Switch · faultyPILOT REPORTED THE LANDING GEAR EXTENDED BY ITSELF WITH GEAR HANDLE IN UP POSITION. MAINTENANCE INSPECTED LANDING GEAR SELECTOR SWITCH, NO DEFECTS FOUND. THE SWITCH WAS REPLACED AS A PRECAUTION, WITH NO FURTHER DEFECTS NOTED.Aug 16, 2026 · N6813J · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20260811001Beam · crackedDURING SCHEDULED INSPECTION A CRACK WAS VISUALLY IDENTIFIED ON THE LEFT HAND CROSSOVER BEAM (OEM: 5654104-11) FORWARD FACE. THIS CRACK MEASURES APPROXIMATELY 1.375 INCHES LONG AND IS CONSISTENT WITH OTHER CRACKS VISUALLY IDENTIFIED ON THESE BEAMS IN THE PAST. Aug 4, 2026 · N810BW · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20260731001Fitting · crackedDURING SCHEDULED WING FITTING INSPECTION 2 CRACKS WERE VISUALLY IDENTIFIED IN THE LOWER RADIUS OF THE RIGHT SIDE LOWER AFT WING ATTACH FITTING (OEM: 0822550-44). THE INBOARD CRACK MEASURES APPROXIMATELY 2.750 INCHES LONG AND THE OUTBOARD CRACK MEASURES APPROXIJul 28, 2026 · N375R · Cessna 402C · Wing, Attach FittingsSDR HYIA20260731002Pump · obstructedCREW REPORTED LEFT HAND ENGINE VIBRATION AND SLIGHT SURGING, ALL ENGINE INDICATIONS REPORTED NORMAL. CREW PERFORMED MAG CHECK (NORMAL) AND TURNED THE LEFT AUXILIARY PUMP OFF, THEN TO HIGH AND STILL HAD THE VIBRATION, SLIGHT SURGING AND DROPPING RPM. CREW DECIDJul 13, 2026 · N2649Z · Cessna 402C · Fuel Boost PumpSDR HYIA20260422001Beam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY DISCOVERED ON THE INBOARD FACE OF THE RIGHT HAND INBOARD 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 BRACKETApr 21, 2026 · N4630N · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20260327001Crossbeam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND CROSSOVER BEAM. THIS CRACK IS LOCATED ON THE AFT FACE OF THE BEAM, COMMON TO THE TOP OUTBOARD BOLT HOLE FOR THE TURBOCHARGER SUPPORT BRACKET. THIS CRACK MEASURES APPROXIMATELY .875 INCHES LONMar 26, 2026 · N3249M · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20260313001Crossbeam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE AFT SIDE OF THE LEFT NACELLE CROSSOVER BEAM (P/N: 5654104-11). THIS CRACK MEASURES APPROXIMATELY 1.25 INCHES IN LENGTH, AND BEGINS AT THE TOP INBOARD TURBO BRACKET MOUNTING HOLE ON THE AFT FACE OF THE BMar 12, 2026 · N2651S · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20251113001Blade · crackedDURING DISASSEMBLY FOR SCHEDULED OVERHAUL A CRACK WAS IDENTIFIED AT A SINGLE BLADE ROOT. MULTIPLE BEARING RACES WERE FOUND TO BE CORRODED AND FAILED.Nov 12, 2025 · N223PB · Cessna 402C · Propeller Blade SectionSDR HYIA20251107002Crossbeam · chafedDURING MAINTENANCE CHAFING DAMAGE WAS VISUALLY IDENTIFIED ON THE FORWARD FACE OF THE LH CROSSOVER BEAM (OEM: 5654104-11). THIS CHAFE MEASURES APPROXIMATELY .700 LONG, .500 WIDE, WITH A DEPTH OF APPROXIMATELY .011. THIS BEAM HAS BEEN REPLACED.Nov 5, 2025 · N26156 · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20251107001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE LEFT HAND INBOARD NACELLE FITTING. (P/N: 5292029-21) THIS CRACK MEASURES APPROXIMATELY .100 INCHES LONG ON THE INBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKS FNov 5, 2025 · N26156 · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20251107004Pump · leakingPILOT REPORTED A FUEL SMELL IN THE CABIN. MAINTENANCE INSPECTED AND FOUND THE HEATER FUEL PUMP LEAKING. THE FUEL PUMP WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Oct 31, 2025 · N890CA · Cessna 402C · Heating SystemSDR 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 HYIA20251010001Switch · shortedPILOT REPORTED THE AUXILIARY CABIN FAN SWITCH FELT HOT WITH A BURNING SMELL AND NOTED SPARKS. COMPANY MAINTENANCE INSPECTED AND FOUND A BURNT WIRE TERMINAL. THE TERMINAL WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Oct 8, 2025 · N223PB · Cessna 402C · Air Conditioning System WiringSDR HYIA20250829001Fitting · crackedDURING LIGHTED BORESCOPE INSPECTION (TEXTRON MEL54-02R3) TO SATISFY THE REQUIREMENT OF AD 2017-10-09, A CRACK WAS IDENTIFIED ON THE OUTBOARD SIDE OF THE LEFT HAND INBOARD NACELLE FITTING ( OEM: 5292029-21). THIS CRACK MEASURES APPROXIMATELY .287 INCHES LONG ANAug 27, 2025 · N678JG · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20250725002Rib · 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 AND TRAVELS FORWAJul 23, 2025 · N205CA · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20250725001Fitting · crackedDURING SCHEDULED NONDESTRUCTIVE TESTING AS NOTED IN CESSNA SUPPLEMENTAL INSPECTION DOCUMENT (SID) 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT HAND INBOARD NACELLE FITTING (OEM P/N: 5292029-30) THIS CRACK MEASURES APPROXIMATELY .104 INCHES LONG ON THE LOWER OJul 23, 2025 · N2611X · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20250627002Rib · crackedDURING SCHEDULED INSPECTION, A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND CLOSEOUT RIB LOCATED AT RWS 106.79. THIS CRACK IS LOCATED IN THE FORWARD VERTICAL ROW OF FASTENERS COMMON TO THE AFT TRUNNION SUPPORT. IT TRAVELS IN AN UP AND DOWN DIRECTION BETWEENJun 25, 2025 · N196CA · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20250627001Crossbeam · crackedDURING INSPECTION A CRACK WAS VISUALLY NOTED ON THE LEFT HAND CROSSOVER BEAM (OEM 5654104-11). THIS CRACK IS LOCATED ON THE AFT FACE OF THE BEAM AT APPROXIMATE LWS 81.62. THE CRACK IS APPROXIMATELY .500 INCHES LONG AND .250 INCHES DOWN FROM THE TOP EDGE OF THJun 24, 2025 · N494BC · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20250522002Rib · crackedDURING SCHEDULED MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT UPPER OUTBOARD RIB CAP COMMON TO THE CLOSEOUT RIB LOCATED AT RWS 106.79 (OEM: 5122115-12). THIS CRACK WAS IDENTIFIED IN THE RADIUS OF THE CAP TRAVELING FORWARD AND AFT, AND MEASURES APPRMay 20, 2025 · N290CA · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20250522001Fitting · crackedDURING SCHEDULED NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS NOTED ON THE RIGHT HAND OUTBOARD NACELLE FITTING P/N: 5292029-32. THE CRACK MEASURES .125 INCHES LONG AND IS CONSISTENT WITH OTHERS FOUND USING THE LIGHTED BORESCOPE INSPECTION TECHNIQUE (TEMay 20, 2025 · N290CA · Cessna 402C · Nacelle/Pylon StructureSDR HYIA20250515001Wire · shortedPILOT REPORTED LEFT ENGINE CYLINDER TEMP INDICATIONS WERE IN THE RED ON TAXI OUT. MAINTENANCE INSPECTED AND FOUND THE POSITIVE WIRE TO THE ALTERNATOR SHORTED INTO THE ADEL CLAMP AT THE CROSSOVER BEAM. THIS CAUSED DAMAGE TO THE SURROUNDING WIRE HARNESS AND HOSEMay 12, 2025 · N494BC · Cessna 402C · Electrical Power System WiringSDR HYIA20250506002Fitting · corrodedDURING SCHEDULED MAINTENANCE A SMALL AREA OF SURFACE CORROSION WAS VISUALLY IDENTIFIED ON THE RIGHT WING LOWER AFT WING FITTING. (OEM PN: 0822550-44). THIS CORROSION MEASURES APPROX. .375" LONG WITH A MAX DEPTH OF APPROX. .030" AND IS CONSISTENT WITH OTHER CORMay 1, 2025 · N747WS · Cessna 402C · Wing, Attach FittingsSDR HYIA20250506001Door Frame · corrodedDURING MAINTENANCE, CORROSION DAMAGE WAS NOTED UNDERNEATH THE STRIKER PLATE FOR THE UPPER CLAMSHELL DOOR PIN ENGAGEMENT HOLE LOCATED ON THE MAIN CABIN DOOR POST. (F.S. 213.6) THE DEPTH OF THIS CORROSION IN GREATER THAN 25% OF THE THICKNESS OF THE DOOR POST ANDMay 1, 2025 · N747WS · Cessna 402C · Fuselage Main, StructureSDR HYIA20250407001Display · failedPILOT REPORTED A BURNING SMELL AFTER TAKE-OFF. MAINTENANCE INSPECTED AND FOUND THE WEATHER RADAR DISPLAY TO BE AT FAULT. THE DISPLAY WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Mar 31, 2025 · N751CA · Cessna 402C · Weather Radar SystemSDR HYIA20250331002Fan · failedPILOT REPORTED BURNING ELECTRICAL SMELL AFTER TAKE OFF. MAINTENANCE INSPECTED AND FOUND THE INSTRUMENT FAN HARD TO TURN. MAINTENANCE REPLACED THE FAN WITH NO FURTHER DEFECTS NOTED.Mar 30, 2025 · N751CA · Cessna 402C · Air Distribution FanSDR HYIA20250314001Fitting · crackedWHILE PERFORMING LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R3 TO SATISFY AD2017-10-09, A CRACK WAS VISUALLY IDENTIFIED ON THE INBOARD AND OUTBOARD VERTICAL LEGS OF THE LEFT HAND OUTBOARD NACELLE FITTING. THE OUTBOARD CRACK MEASURESMar 12, 2025 · N677CA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20250203001Transistor · burnedPILOT REPORTED A BURNING SMELL IN THE CABIN AFTER TURNING ON INSTRUMENT LIGHTS. MAINTENANCE INSPECTED AND FOUND CO PILOT DIMMING CONTROLLER RESISTOR R1 AND HEAT SINK TRANSISTOR ASSY #7 TRANSISTOR BURNT. REMOVED AND REPLACED RESISTOR AND HEAT SINK ASSY WITH NO Jan 31, 2025 · N2611X · Cessna 402C · Flight Compartment LightingSDR HYIA20250131001Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE FORWARD FACE OF THE FWD LH UPPER FUSELAGE ATTACH FITTING PN: 0811350-9. THIS CORROSION MEASURES APPROXIMATELY .700 WIDE, AND .400 TALL, WITH AN APPROXIMATE DEPTH OF .025 AND IS CONSISTENT WIJan 30, 2025 · N26156 · Cessna 402C · Fuselage Main, Attach FittingsSDR 3BCA202501250023Sight Tube · leakingPILOT WRITE-UP REF: LP 10164, "LANDING GEAR UNLOCK LIGHT (RED) AND HYD PRESS LIGHT ON. THICK SMOKE IN CABIN SMELLED LIKE HYD FLUID." PILOT DECLARED EMERGENCY AND RETURN TO BFI SAFELY. UPON EXAMINATION FOUND PN: 5117007-12 (TUBE-SIGHT HYDRAULIC SYSTEM) SURFACE Jan 9, 2025 · N818AN · Cessna 402C · Hydraulic System, MainSDR 2024FA0000985Manifold · failedTHIS IS THE 2ND AIRCRAFT I DID HAVE THE SAME PROBLEM WITH (FIRST ONE WAS N9873F CESSNA 402-0303 MORE THAN 10 YEARS AGO). THE VACUUM MANIFOLD (PARKER AIRBORNE DIV. P#1H5-9 S#10AT) FAILED DUE TO WEAK RIVET HEADS, IN ONE INSTANCE TOTAL FAILURE OF BOTH VACUUM SYSTDec 30, 2024 · N540NE · Cessna 402C · Vacuum Distribution SystemSDR HYIA20241230001Fitting · corrodedDURING SCHEDULED AGING AIRCRAFT INSPECTION TO SATISFY THE REQUIREMENTS OF FAR 135.422 (AGING AIRCRAFT INSPECTION AND RECORDS REVIEW), A SMALL AREA OF CORROSION WAS IDENTIFIED ON THE RIGHT HAND UPPER AFT WING FITTING. (OEM: 0822550-46) THIS CORROSION MEASURES ADec 27, 2024 · N678JG · Cessna 402C · Wing, Attach FittingsSDR HYIA20241220001Fitting · corrodedDURING SCHEDULED MAINTENANCE A SMALL AREA OF SURFACE CORROSION WAS VISUALLY IDENTIFIED ON THE RIGHT WING UPPER AFT WING FITTING. (OEM PN: 0822550-46). THIS CORROSION MEASURES APPROX. 1.25" LONG WITH A MAX DEPTH OF APPROX. .009" AND IS CONSISTENT WITH OTHER CORDec 19, 2024 · N3249M · Cessna 402C · Wing, Attach FittingsSDR HYIA20241213002Circuit Breaker · failedPILOT REPORTED PLASTIC BURNING SMELL IN CABIN SMELLS FROM LEFT C/B PANEL. MAINTENANCE INSPECTED AND FOUND THE STROBE LIGHT SWITCH INOP. THE SWITCH WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Dec 12, 2024 · N2611X · Cessna 402C · Electrical Power SystemSDR HYIA20241205002Display · failedPILOT REPORTED BURNING SMELL INTERMITTENTLY AFTER TAKE-OFF. MAINTENANCE INSPECTED AND DETERMINED WEATHER RADAR DISPLAY TO BE AT FAULT. THE DISPLAY WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Nov 21, 2024 · N385CA · Cessna 402C · Weather Radar SystemSDR HYIA20241121001Fitting · crackedDURING LIGHTED BORESCOPE INSPECTION (TEXTRON MEL54-02R3) TO SATISFY THE REQUIREMENT OF AD 2017-10-09, A CRACK WAS IDENTIFIED ON THE OUTBOARD SIDE OF THE RIGHT HAND INBOARD NACELLE FITTING ( OEM: 5292029-22). THIS CRACK MEASURES APPROXIMATELY .620 INCHES LONG ANov 20, 2024 · N106CA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20241106001Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE AFT FACE OF THE LEFT HAND UPPER FUSELAGE ATTACH FITTING (OEM PN: 0811350-9). THIS CORROSION MEASURES APPROXIMATELY .400 INCHES LONG .150 WIDE, AND HAS AN APPROXIMATE DEPTH OF .015. THIS CORRNov 5, 2024 · N6879R · Cessna 402C · Wing, Attach FittingsSDR HYIA20241018001Fitting · corrodedDURING MAINTENANCE 3 SPOTS OF CORROSION WERE VISUALLY IDENTIFIED ON THE OUTBOARD LEFT UPPER AFT WING FITTING (OEM PN: 0822550-45). ALL THREE SPOTS ARE LOCATED ON THE LOWER SURFACE OF THE HORIZONTAL FLANGE OF THIS FITTING, AND ARE CONSISTENT WITH OTHER CORROSIOOct 18, 2024 · N514NC · Cessna 402C · Wing, Attach FittingsSDR 2024FA0000751Impulse Coupling · failedIMPULSE COUPLING FAILURE CAUSED RT MAGNETO TO BE INOPERATIVE AND METAL CONTAMINATION OF ENGINE.Oct 3, 2024 · Cessna 402C · Magneto/DistributorSDR HYIA20240911001Beam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE AFT SIDE OF THE LEFT NACELLE CROSSOVER BEAM (P/N: 5654104-11). THIS CRACK MEASURES APPROXIMATELY 1.316 INCHES IN LENGTH, AND BEGINS AT THE TOP INBOARD TURBO BRACKET MOUNTING HOLE ON THE AFT FACE OF THE Sep 10, 2024 · N663AA · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20240830001Switch · failedPILOT REPORTED STRONG BURNING SMELL IN COCKPIT. NOTICED PROP DE-ICE GAUGE WAS ON BUT THE SWITCH WAS OFF. CYCLED SWITCH BREAKER. DE-ICE GAUGE TURNED OFF, BUT SWITCH REMAINED LOOSE. THEY PULLED C/B'S AS PRECAUTION. MAINTENANCE TROUBLESHOT TO BAD SWITCH. BYPASSEDAug 29, 2024 · N2611X · Cessna 402C · Propeller/Rotor Anti-Ice/De-Ice SystemSDR HYIA20240827003Spar · crackedDURING MAINTENANCE A .187 INCH CRACK WAS VISUALLY IDENTIFIED ON THE LEFT HAND SIDE OF THE FORWARD CARRY THROUGH SPAR, ON THE FORWARD WEB, IN THE AREA OF THE SPAR WEB CUT OUT LOCATED AT LBL 32.55. THIS CRACK IS CONSISTENT WITH OTHER CRACKS VISUALLY IDENTIFIED IAug 26, 2024 · N890CA · Cessna 402C · Fuselage Main, StructureSDR HYIA20240828002Fitting · 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 .130 AND IS CONSISTENT WITH OTHER FOUND USING THISJul 17, 2024 · N3249M · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20240718005Axle · crackedDURING SCHEDULED NDT INSPECTION A CRACK WAS FOUND ON THE RIGHT MAIN LANDING GEAR AXLE. THE LOWER LEG AND AXLE WERE REPLACED WITH NO FURTHER DEFECTS NOTED.Jul 16, 2024 · N26156 · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA20240718004Axle · crackedDURING SCHEDULED NDT INSPECTION A CRACK WAS FOUND ON THE RIGHT MAIN LANDING GEAR AXLE. THE LOWER LEG AND AXLE WERE REPLACED WITH NO FURTHER DEFECTS NOTED.Jul 16, 2024 · N57PB · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA20240718003Axle · crackedDURING SCHEDULED NDT INSPECTION A CRACK WAS FOUND ON THE LEFT MAIN LANDING GEAR AXLE. THE LOWER LEG AND AXLE WERE REPLACED WITH NO FURTHER DEFECTS NOTED.Jul 16, 2024 · N57PB · Cessna 402C · Main Landing Gear Strut/Axle/Truck
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