Cessna 402C

Service difficulty reports · 1,782

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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"

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SDR HYIA20221114001Attach Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND UPPER AFT OUTBOARD FORWARD WING ATTACH FITTING (P/N: 0822550-45). IT IS LOCATED ON THE BOTTOM FACE OF THE UPPER HORIZONTAL LEG OF THE FITTING AND MEASURES APPROXIMATELY .674 INCHESNov 10, 2022 · N524CA · Cessna 402C · Wing, Attach FittingsSDR HYIA20221101002Axle · brokenRIGHT MAIN GEAR AXLE FAILED ON LANDING/TAXI TO GATE. MAINTENANCE IS REPLACING LOWER BARREL & AXLE.Nov 3, 2022 · N1055 · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA20221005001Igniter · burnedTHE PILOT REPORTED AN ELECTRICAL SMELL IN THE COCKPIT DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND THE HEATER IGNITION SYSTEM BURNT. THIS WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Oct 4, 2022 · N524CA · Cessna 402C · Heating SystemSDR HYIA20220909002Door 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 ANDSep 8, 2022 · N26156 · Cessna 402C · Fuselage Main, StructureSDR HYIA20220909001Rib · elongatedDURING MAINTENANCE, SEVERAL WORKING FASTENERS WERE NOTED ON THE RIGHT HAND CLOSE OUT RIB OF N26156 AT R.W.S. 106.79. THESE FASTENERS ARE COMMON TO THE AFT TRUNNION SUPPORT PLATE. THESE WORKING FASTENERS RESULTED IN ELONGATION OF THE HOLES THROUGH THE RIB BEYONSep 8, 2022 · N26156 · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20220713001Strap · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE RH SPAR STRAP. (SK 402-47B). THIS CORROSION MEASURES APPROXIMATELY 1.182 INCHES LONG, .815 INCHES WIDE, AND .050 INCHES DEEP LOCATED AT APPROXIMATE RWS 125.54. THIS STRAP WILL BE REMOVED ANJul 12, 2022 · N751CA · Cessna 402C · Fuselage Main, StructureSDR HYIA20220701002Fitting · 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 .129 IN LENGTH, AND IT'S LOCATION IS CONSISTENT WIJul 1, 2022 · N120PC · Cessna 402C · Fuselage Main, StructureSDR HYIA20220701001Fitting · crackedWHILE PERFORMING A RECURRENT NDT INSPECTION (HFEC) TO SATISFY THE REQUIREMENTS OF TEXTRON 57-10-16, A CRACK WAS FOUND ON THE INBOARD SIDE OF THE RIGHT HAND OUTBOARD NACELLE FITTING. THIS CRACK WAS MEASURED AT .055 IN LENGTH. THIS CRACK IS CONSISTENT WITH OTHJul 1, 2022 · N26156 · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20220511002Rib · crackedWHILE PERFORMING OTHER MAINTENANCE, A CRACK WAS DISCOVERED IN THE LEFT CLOSE OUT RIB. THIS CRACK EXTENDS VERTICALLY THROUGH TWO FASTENERS HOLES IN THE FIRST ROW OF ATTACH HI-LOKS BETWEEN THE AFT TRUNNION SUPPORT AND THE CLOSE OUT RIB. THE CRACK EXTENDS BETWEMay 11, 2022 · N83PB · Cessna 402C · Fuselage Main, StructureSDR HYIA20220511001Spar Cap · corrodedWHILE PERFORMING OTHER MAINTENANCE, CORROSION WAS IDENTIFIED ON THE LEFT HAND AFT LOWER OUTBOARD SPAR CAP (P/N 5122041-23) AT WING STATION 222.0 TO 229.71. THE DEEPEST AREA OF CORROSION WAS MEASURED AT .033. THIS SPAR CAP WAS REPLACED WITH A FACTORY NEW PARMay 11, 2022 · N83PB · Cessna 402C · Fuselage Main, StructureSDR HYIA20220405001Rib · crackedWHILE PERFORMING THE SID 57-10-25 INSPECTION, THREE CRACKS WHERE IDENTIFIED IN THE RIGHT CLOSE-OUT RIB (P/N 5122155-56.) THESE CRACKS WERE FOUND ON THE FORWARD ROW OF AT THE REAR TRUNNION PLATE ATTACH POINT. THERE ARE 6 HI-LOK HOLES ALIGNED VERTICALLY IN THMay 5, 2022 · N36911 · Cessna 402C · Wing StructureSDR HYIA20220413001Trunnion · crackedRIGHT MAIN LANDING GEAR TRUNNION UPPER TORQUE LINK TAB BROKE ON LANDINGApr 9, 2022 · N258PB · Cessna 402C · Fuselage, Landing Gear Attach FittingsSDR HYIA20220329001Fitting · crackedWHILE PERFORMING A RECURRENT NDT INSPECTION (HFEC) TO SATISFY THE REQUIREMENTS OF TEXTRON 57-10-16, A CRACK WAS FOUND ON THE RIGHT HAND INBOARD NACELLE FITTING. THIS CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING AND MEASURES .150 IN LENGTH. THIS CRACK Mar 28, 2022 · N6875D · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20220316001Propeller · crackedPILOT REPORTED THE LEFT PROPELLER CONTROL WAS UNRESPONSIVE AT CLIMB OUT AND PERFORMED AN AIR RETURN. COMPANY MAINTENANCE INSPECTED THE LEFT PROPELLER AND FOUND CRACKS IN THE PROPELLER HUB AT ALL 3 BLADE SOCKET LOCATIONS. AT BLADE 1 LOCATION THE CRACK IS APPRMar 15, 2022 · N740CA · Cessna 402C · Propeller Hub SectionSDR HYIA20220216001Fitting · crackedWHILE PERFORMING THE LIGHTED BOROSCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R2 TO SATISFY AD2017-10-19, A CRACK WAS IDENTIFIED ON THE OUTBOARD RADIUS OR THE LEFT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES APPROXIMATELY .119 INCHES LONGFeb 8, 2022 · N223PB · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20211217001Fuel Line · defectiveTHE PILOT REPORTED A FUEL SMELL IN THE CABIN WITH THE HEATER OFF. MAINTENANCE INSPECTED AND FOUND A DEFECT IN THE HEATER FUEL LINE. THIS WAS REPLACED FROM THE HEATER FUEL PUMP TO THE FIREWALL WITH NO FURTHER DEFECTS NOTED.Dec 13, 2021 · N6765T · Cessna 402C · Fuel StorageSDR HYIA20211130001O-Ring · defectiveTHE PILOT REPORTED A FUEL SMELL IN THE CABIN WITH THE HEATER ON. MAINTENANCE INSPECTED AND FOUND THE HEATER FUEL FILTER LEAKING. THE FUEL HEATER O-RING WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Nov 24, 2021 · N67909 · Cessna 402C · Heating SystemSDR HYIA20211022001Selector · faultyTHE PILOT REPORTED THE RIGHT ENGINE FUEL FLOW BEGAN FLUCTUATING IN FLIGHT, WITH THE ENGINE SURGING. THE PILOT ELECTED TO SHUT DOWN THE ENGINE, RESULTING IN A SINGLE-ENGINE LANDING. MAINTENANCE INSPECTED AND FOUND THE FUEL SELECTOR TO BE FAULTY. TROUBLESHOOTINGOct 17, 2021 · N406GA · Cessna 402C · Engine Fuel and ControlSDR HYIA20210924001Beam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND OUTBOARD ENGINE BEAM (P/N: 5654109-8) IN THE AREA UNDERNEATH THE FORWARD ENGINE MOUNT DOUBLER. THIS CRACK TRAVELS LEFT TO RIGHT ACROSS THE TOP FACE OF THE BEAM AND PARTIALLY DOWN THE OUTBOARDSep 24, 2021 · N290CA · Cessna 402C · Nacelle/Pylon StructureSDR HYIA20210903001Spar Cap · crackedA CRACK WAS IDENTIFIED AT THE RT SIDE OF LWR FWD CARRYTHROUGH SPAR CAP AT FASTENER LOCATION IN FWD ROW WHILE PERFORMING NDT PROCEDURE AS AMOC FOR AD2018-03-03R1. THE CRACK WAS CONFIRMED BY BOLT HOLE EDDY CURRENT AFTER THE FASTENER WAS REMOVED. THE WING JOINTSep 1, 2021 · N106CA · Cessna 402C · Wing SparSDR HYIA20210827001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT HAND INBOARD NACELLE FITTING. (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .123 INCHES LONG ON THE OUTBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKSAug 27, 2021 · N6875D · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20210823001Engine · making metalTHE PILOT REPORTED THE LEFT ENGINE HAD A LOSS OF POWER IN AND THE OIL PRESSURE FELL TO ZERO. MAINTENANCE INSPECTED AND FOUND METAL PARTICLES IN THE OIL FILTER. AN ENGINE HAS BEEN ORDERED TO REPLACE THIS ENGINE. FURTHER DETAILS ARE TO BE PROVIDED UPON ENGINE Aug 19, 2021 · N6879R · Cessna 402C · Engine (Reciprocating)SDR HYIA20210820001Blower · inoperativeTHE PILOT REPORTED SMOKE IN THE CABIN DURING CRUISE WHILE THE HEATER WAS ON. MAINTENANCE INSPECTED, FOUND THE HEATER BLOWER INOPERABLE, AND REPLACED IT WITH NO FURTHER DEFECTS NOTED.Aug 16, 2021 · N88833 · Cessna 402C · Heating SystemSDR HYIA20210817001Attach Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND UPPER FORWARD WING ATTACH FITTING. IT IS LOCATED ON THE BOTTOM FACE OF THE UPPER HORIZONTAL LEG OF THE FITTING AND MEASURES APPROXIMATELY .555 INCHES LONG, .300 INCHES WIDE, AND .0Aug 16, 2021 · N494BC · Cessna 402C · Wing, Attach FittingsSDR HYIA20210811001Attach Fitting · corrodedDURING SCHEDULED MAINTENANCE, A SPOT OF INTERGRANULAR CORROSION WAS VISUALLY IDENTIFIED ON THE RIGHT HAND, UPPER, WING ATTACH FITTING. IT MEASURES APPROXIMATELY .520 INCHES LONG, .064 INCHES DEEP, AND .221 INCHES WIDE. IT IS LOCATED ON THE BOTTOM EDGE OF THE VAug 10, 2021 · N747WS · Cessna 402C · Wing, Fuselage Attach FittingsSDR HYIA20210714001Attach Fitting · crackedDURING A 402-22 VISUAL WING ATTACHMENT FITTING INSPECTION, CORROSION WAS NOTED ON THE AFT VERTICAL PORTION OF THE LEFT HAND LOWER INBOARD WING ATTACH FITTING, JUST BEFORE THE AREA WHERE THE FITTING MOUNTS IN THE SPAR CAP. UPON REMOVAL OF THE FITTING, A LARGERJul 14, 2021 · N525RH · Cessna 402C · Fuselage, Wing Attach FittingsSDR HYIA20210712002Rib · 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 APPRJul 5, 2021 · N678JG · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20210712001Strap · corrodedDURING SID 57-10-16 INSPECTION, 3 AREAS OF CORROSION WERE IDENTIFIED ON THE RIGHT SPAR STRAP OF N402VN. THESE AREAS ARE LOCATED ON THE OUTBOARD END OF THE STRAP BETWEEN APPROXIMATE WING STATIONS, 145.87-155.62, AND ARE BEYOND LIMITS FOR REPAIR AS OUTLINED IN SJul 1, 2021 · N402VN · Cessna 402C · Wing Main, Frame StructureSDR HYIA20210625001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT SIDE OF THE RIGHT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES APPROXIMATELY .097 LONG AND IS CONSISTENT WITH OTHER CRACKS FOUND USING THE LIGHTED BORESCOPE INSPECTION TEJun 25, 2021 · N36911 · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20210611003Strap · corrodedDURING MAINTENANCE, INTERGRANULAR CORROSION WAS VISUALLY DISCOVERED ON THE RIGHT HAND SPAR STRAP OF N26514 AS PART OF SK402-47B (P/N: 5292029-2). THIS CORROSION IS LOCATED AT APPROXIMATE RIGHT WING STATION 106.79 NEAR THE OUTBOARD ENGINE BEAM NACELLE FITTING, Jun 10, 2021 · N26514 · Cessna 402C · Wing SparSDR HYIA20210611001Spring · brokenDURING APPROACH THE NOSE LANDING GEAR WOULD NOT EXTEND. AIRCRAFT LANDED WITH NOSE GEAR RETRACTED. NO INJURIES. INSPECTION FOUND THE NOSE GEAR DOOR RETURN SPRING TO BE BROKEN, WHICH CAUSED THE NOSE GEAR DOOR RETRACT BELLCRANK TO BECOME OUT POSITION JAMMING THE Jun 6, 2021 · N4630N · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20210604001Tube · out of positionTHE PILOT REPORTED A CHEMICAL SMELL COMING FROM THE HEATER IN FLIGHT. MAINTENANCE INSPECTED AND FOUND SCAT TUBING OBSTRUCTING HEATER THERMOSTAT ARM. REPOSITIONED AND SECURED SCAT TUBING WITH NO FURTHER DEFECTS NOTED.Jun 1, 2021 · N903CA · Cessna 402C · Heating SystemSDR 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 HYIA20210611002Line · crackedNOSE GEAR LIGHT DID NOT ILLUMINATE ON EXTENSION, AIRCRAFT LANDED WITH GEAR UNLOCKED, GEAR COLLAPSED ON LANDING. NO INJURIES. INSPECTED AIRCRAFT AND FOUND HYDRAULIC PRESSURE LINE IN RIGHT WING CRACKED AND BLOWDOWN BOTTLE DID NOT DISCHARGE.May 28, 2021 · N494BC · Cessna 402C · Hydraulic System, MainSDR HYIA20210525002Cylinder · damagedTHE PILOT REPORTED ENGINE SURGING AND MANIFOLD PRESSURE DROP IN FLIGHT, AND THEN SHUT DOWN ENGINE IN-FLIGHT ACCORDING TO THE QRH. DURING THE INITIAL INSPECTION, FOUND SHINY PARTICLES IN THE OIL FILTER, AND SPARK PLUG DAMAGED, AND PARTICLES IN THE PROPELLER GOMay 20, 2021 · N68391 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20210525001Master Cylinder · faultedTHE PILOT A LOSS OF PRESSURE ON THE RIGHT BRAKE DURING PARKING. MAINTENANCE INSPECTED AND FOUND THE RIGHT MASTER CYLINDER TO BE AT FAULT. REPLACED THE MASTER CYLINDER HOSE, AND RESEALED THE MASTER CYLINDER. PERFORMED BLAKE BLEEDING PROCEDURES WITH NO FURTHER May 19, 2021 · N67886 · Cessna 402C · Master Cylinder/Brake ValveSDR HYIA20210512001Crossbeam · crackedDURING INSPECTION A CRACK WAS VISUALLY DISCOVERED ON THE INBOARD END OF THE LOWER CHANNEL OF THE RIGHT HAND CROSSOVER BEAM. THIS CRACK IS IN THE AREA OF THE MOUNTING HOLES FOR THE INBOARD EXHAUST ELBOW CLAMP BRACKET, AND MEASURES APPROXIMATELY 2 INCHES LONG ANMay 11, 2021 · N514NC · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20210513001Torque Tube · brokenWHEN ACTUATING THE RUDDER PEDAL WHILE MANEUVERING INTO A PARKING SPACE, THE PILOT REPORTED THAT THE RIGHT RUDDER PEDAL HAD BROKEN OFF THE TORQUE TUBE. MAINTENANCE INSPECTED AND FOUND IT BROKEN OFF AT THE WELD. THIS WAS REPLACED BY MAINTENANCE WITH NO FURTHERMay 5, 2021 · N375R · Cessna 402C · Rudder Control SystemSDR HYIA20210503001Unknown · odorTHE PILOT REPORTED A FUEL SMELL IN THE COCKPIT IN FLIGHT AND TAXI. MAINTENANCE INSPECTED THE HEATER FUEL LINES, HEATER PUMP, ENGINE FUEL LINES, HEATER FILTER AND BOOST PUMPS FOR LEAKS, WITH NO DEFECTS NOTED. AN ENGINE AND HEATER OPS CHECK WERE PERFORMED, ANDMay 2, 2021 · N890CA · Cessna 402C · Air Distribution SystemSDR HYIA20210503002Brake Caliper · inoperativeTHE PILOT A LOSS OF PRESSURE ON THE RIGHT BRAKE ON LANDING. MAINTENANCE INSPECTED AND FOUND THE RIGHT CALIPER TO BE AT FAULT. REMOVED AND REPLACED THE RIGHT CALIPER AND PERFORMED BLAKE BLEEDING PROCEDURES. NO FURTHER DEFECTS NOTED.Apr 27, 2021 · N677 · Cessna 402C · Landing Gear Brake SystemSDR HYIA20210421001Spring · brokenTHE PILOT REPORTED THE UPPER PASSENGER DOOR OPENING IN FLIGHT. THE FLIGHT WAS THEN DIVERTED TO KHYA, WHERE MAINTENANCE INSPECTED AND FOUND THE EXTERIOR DOOR HANDLE SPRING BROKEN. THE EXTERIOR HANDLE WAS REMOVED AND REPLACED WITH NO FURTHER DEFECTS NOTED.Apr 18, 2021 · N121PB · Cessna 402C · Passenger/Crew DoorsSDR HYIA20210416001Fuel Line · crackedTHE PILOT REPORTED A FUEL SMELL WHEN THE HEATER WAS ON IN FLIGHT. MAINTENACE INSPECTED AND FOUND THE FUEL LINE AT THE FUEL NOZZLE CRACKED. THE LINE WAS REPAIRED AND REINSTALLED WITH NO FURTHER DEFECTS NOTED.Apr 14, 2021 · N466CA · Cessna 402C · Heating SystemSDR HYIA20210407002Attach Fitting · corrodedDURING MAINTENANCE 2 SPOTS OF CORROSION WERE IDENTIFIED ON THE BOTTOM SURFACE OF THE UPPER HORIZONTAL LEG OF THE 0822550-46 WING ATTACH FITTING (RH UPPER AFT FITTING, FORWARD SPAR). THE FIRST SPOT MEASURES APPROXIMATELY .514 INCHES LONG, .330 INCHES WIDE, WITHApr 7, 2021 · N406GA · Cessna 402C · Horizontal Stabilizer StructureSDR HYIA20210407001Fitting · 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 .095 INCHES LONG ON THE OUTBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKS Apr 7, 2021 · N406GA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20210407003Ignition Unit · brokenTHE PILOT REPORTED A BURNING SMELL DURING CRUISE. MAINTENANCE INSPECTED AND FOUND THE SMELL TO BE COMING FROM THE HEATER IGNITION UNIT. THE COMPONENT WAS REMOVED AND REPLACED WITH NO FURTHER DEFECTS NOTED.Apr 1, 2021 · N499CA · Cessna 402C · Heating SystemSDR HYIA20210311002Wire · chafedTHE PILOT REPORTED A BURNING SMELL AFTER THE AUTOPILOT CB POPPED DURING FLIGHT. MAINTENANCE INSPECTED AND FOUND CHAFFED WIRING AT THE PTT SWITCH. THE WIRES WERE REPAIRED WITH NO FURTHER DEFECTS NOTED.Mar 9, 2021 · N740CA · Cessna 402C · Auto Flight System WiringSDR HYIA20211310001Heater · odorTHE PILOT REPORTED A BURNING SMELL IN THE CABIN IN FLIGHT WITH THE HEATER TURNED ON. MAINTENANCE INSPECTED AND REPLACED THE HEATER ASSEMBLY WITH NO FURTHER DEFECTS NOTED.Mar 9, 2021 · N466CA · Cessna 402C · Cabin Cooling SystemSDR 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 HYIA20210222001Fitting · 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 .145 INCHES LONG ON THE INBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACKS FFeb 22, 2021 · N763EA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20210219001Heater · odorTHE PILOT REPORTED A BURNING SMELL IN THE CABIN IN FLIGHT WITH THE HEATER TURNED ON. MAINTENANCE INSPECTED AND REPLACED THE HEATER ASSEMBLY WITH NO FURTHER DEFECTS NOTED.Feb 16, 2021 · N4630N · Cessna 402C · Heating System
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