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 HYIA20210208001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE INBOARD LEG OF THE RIGHT HAND INBOARD NACELLE FITTING, (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .157 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTFeb 8, 2021 · N771EA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20210202001Fitting · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND LOWER FUSELAGE ATTACH FITTING (P/N: 0811350-10) ON N763EA. THIS CORROSION MEASURES APPROXIMATELY .390 INCHES TALL, .429 WIDE, AND HAS A MAXIMUM DEPTH OF .056. IT IS LOCATED ON THEFeb 2, 2021 · N763EA · Cessna 402C · Fuselage, Wing Attach FittingsSDR HYIA20201201001Pump · failedTHE PILOT REPORTED A BURNING SMELL IN THE CABIN INFLIGHT WITH THE HEATER TURNED ON AND DISSIPATED WHEN THE HEATER WAS TURNED OFF. MAINTENANCE INSPECTED AND FOUND THE FUEL PUMP DRIVE BROKEN AND REPLACED THE HEATER FUEL PUMP WITH NO FURTHER DEFECTS NOTED.Nov 30, 2020 · N26156 · Cessna 402C · Heating SystemSDR HYIA20201124001Fitting · crackedWHILE PERFORMING INITIAL NDT INSPECTION (HFEC) TO SATISFY THE REQUIREMENTS OF TEXTRON SID 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 .175 IN LENGTH. THIS CRACKNov 24, 2020 · N375R · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20201125001Attach Fitting · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE RIGHT HAND LOWER FUSELAGE ATTACH FITTING (P/N: 0811350-10) ON N663AA. THIS CORROSION MEASURES APPROXIMATELY .623 INCHES TALL, .252 WIDE, AND HAS A MAXIMUM DEPTH OF .034 AND IS LOCATED ON TNov 23, 2020 · N663AA · Cessna 402C · Fuselage Main, Attach FittingsSDR HYIA20201124002Axle · crackedTHE PILOT REPORTED THAT AFTER LANDING, THE AXLE BROKE WHILE EXITING THE RUNWAY. MAINTENANCE INSPECTED AND FOUND THE RIGHT AXLE TO BE CRACKED. REMOVED AND REPLACED THE RIGHT LOWER BARREL AND AXLE ASSEMBLY. NO FURTHER DEFECTS NOTED.Nov 23, 2020 · N26632 · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA20201124003Connector · burnedTHE PILOT REPORTED A BURNING PLASTIC SMELL IN THE CABIN IN FLIGHT. IT WAS NOTED THAT THE SMELL WAS PRESENT WITH THE HEATERS AND THE FANS TURNED OFF. MAINTENANCE INSPECTED AND FOUND A BURNED MOLEX CONNECTOR FOR THE PROPELLER DE-CE GAUGE. REMOVED AND REPLACEDNov 19, 2020 · N706CA · Cessna 402C · Ice/Rain Protection System WiringSDR HYIA20201117001Governor · malfunctionedTHE PILOT REPORTED THE LEFT PROPELLER STUCK AT 2500 RPMS AT CRUISE FLIGHT, AND WAS UNABLE TO ADJUST. MAINTENANCE INSPECTED AND FOUND AND ALL COMPONENTS TO BE SECURED AND IN GOOD CONDITION. REMOVED THE LEFT ENGINE PROPELLER GOVERNOR AS A PRECAUTION. PREFORMENov 16, 2020 · N7037E · Cessna 402C · Propeller Controlling SystemSDR HYIA20201116001Beam · crackedDURING MAINTENANCE A CRACK WAS 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 BRACKET P/N: 56Nov 12, 2020 · N991AA · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20201112001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE RIGHT HAND OUTBOARD NACELLE FITTING. (P/N: 5292029-24) THIS CRACK MEASURES APPROXIMATELY .102 INCHES LONG ON THE OUTBOARD LOWER LEG OF THE FITTING, AND IS CONSISTENT WITH OTHER CRACNov 10, 2020 · N68752 · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20201106002Axle · crackedTHE 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 REPLACEDNov 3, 2020 · N751CA · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA20201030001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE INBOARD LEG OF THE LEFT HAND OUTBOARD NACELLE FITTING, (P/N: 5292029-23). THIS CRACK MEASURES APPROXIMATELY .170 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEOct 30, 2020 · N401TJ · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20201005001Spar · crackedUPON REMOVAL OF LT WING TRAILING EDGE RIB ASSEMBLY PART NUMBER 5122053-35, A CRACK WAS IDENTIFIED AT AFT INBOARD WING SPAR ASSEMBLY. THE DAMAGE IS LOCATED AT LT WS 103.29 AND IS NOT VISIBLE WITH RIB ASSEMBLY INSTALLED. THE LT INBOARD SPAR ASSEMBLY PART NUMBEOct 1, 2020 · N810BW · Cessna 402C · Wing SparSDR HYIA20200929001Rib · crackedDURING MAINTENANCE TWO CRACKS WERE DISCOVERED ON THE RIGHT HAND CLOSEOUT RIB AT RWS 106.79 (P/N: 5122115-56). THESE CRACKS ORIGINATE FROM TWO SEPARATE HOLES COMMON TO THE FORWARD ROW OF FASTENERS ATTACHING THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE. THSep 28, 2020 · N818AN · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20200921001Packing · leakingTHE PILOT REPORTED A FUEL SMELL IN COCKPIT. MAINTENANCE INSPECTED AND FOUND THE CABIN HEATER FUEL FILTER BOWL LEAKING. REMOVED AND REPLACED THE BOWL SEAL WITH NO FURTHER DEFECTS NOTED.Sep 18, 2020 · N409BK · Cessna 402C · Aircraft Fuel Distribution SystemSDR HYIA20200918001Alternator · damagedTHE PILOT REPORTED AFTER LANDING SMOKE AND BURNING PLASTIC SMELL COMING FROM THE AREA OF THE RIGHT ENGINE. MAINTENANCE INSPECTED AND FOUND THE RIGHT ENGINE ALTERNATOR HAD AN ELECTRICAL SMELL. REMOVED AND REPLACED THE RIGHT ENGINE ALTERNATOR AND VOLTAGE REGULSep 18, 2020 · N706CA · Cessna 402C · DC Generator-AlternatorSDR HYIA20200911002Spar Cap · corrodedDURING MAINTENANCE CORROSION DAMAGE WAS IDENTIFIED ON BOTTOM FACE OF THE HORIZONTAL LEG OF THE LEFT HAND LOWER OUTBOARD SPAR CAP (P/N: 5122041-23). THIS DAMAGE IS LOCATED BETWEEN LWS 203.21 AND 212.46. AT IT'S DEEPEST THIS DAMAGE MEASURES .027 INCHES DEEP. Sep 11, 2020 · N810BW · Cessna 402C · Wing SparSDR HYIA20200911001Attach Fitting · 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 OF THE RIGHT HAND INBOARD NACELLE ATTACH FITTING (P/N: 5292029-22). THIS CRACK MEASURES APPROSep 10, 2020 · N763EA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA202009109002Volt Regulator · damagedTHE PILOT REPORTED A DUAL ALTERNATOR FAILURE AFTER TAKE-OFF. MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND VOLTAGE REGULATOR WAS DEFECTIVE. THIS WAS REPLACED AND PARELLEDED. NO FURTHER DEFECTS NOTED.Sep 8, 2020 · N890CA · Cessna 402C · AC RegulatorSDR HYIA202009109001Engine · damagedPILOT REPORTED A SIGNIFICANT DROP IN OIL PRESSURE DURING FLIGHT, AND AFTER LANDING, OIL LEAKING FROM RIGHT ENGINE. MAINTENANCE INSPECTED AND FOUND METAL PARTICLES IN THE OIL FILTER AND PROPELLER GOVERNOR SCREEN AND IS CHANGING THE RIGHT ENGINE, PROPELLER, VAPSep 6, 2020 · N18VV · Cessna 402C · Engine (Turbine/Turboprop)SDR HYIA20200904002Control Cable · brokenTHE PILOT REPORTED THAT THE RIGHT PROPELLER RAN AWAY IN FLIGHT, BUT DID NOT OVERSPEED. MAINTENANCE INSPECTED AND FOUND THAT THE PROPELLER CONTROL CABLE HAD BROKEN. REMOVED AND REPLACED RT PROPELLER CONTROL CABLE ASSEMBLY. NO FURTHER DEFECTS NOTED.Sep 2, 2020 · N401TJ · Cessna 402C · Propeller Controlling SystemSDR HYIA20200904001Fan · failedTHE PILOT REPORTED THAT DURING FLIGHT A BURNING SMELL WAS NOTED. MAINTENANCE INSPECTED AND FOUND THE AV COOLING FAN CB HAD TRIPPED. REMOVED AND REPLACED THE AV COOLING FAN WITH NO FURTHER DEFECTS NOTED.Sep 2, 2020 · N402HG · Cessna 402C · Air Distribution FanSDR HYIA2020090131001Cylinder · damagedPILOT REPORTED MAGNETO ROUGH IN FLIGHT. MAINTENANCE INSPECTED AND FOUND OIL IN THE #5 CYLINDER. UPON REMOVAL OF THE CYLINDER IT WAS FOUND TO HAVE MISSING MATERIAL AT THE VALVE INTAKE GUIDE. THE #5 CYLINDER WAS REPLACED WITH NO FURTHER DEFECTS NOTEDAug 28, 2020 · N68752 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20200824001Fitting · crackedDURING NDT INSPECTION AS NOTED IN SID 57-10-16, A CRACK WAS DISCOVERED ON THE LEFT HAND OUTBOARD NACELLE FITTING (P/N: 5292029-23). THIS CRACK MEASURES APPROXIMATELY .210 INCHES LONG ON THE OUTBOARD LOWER LEG OF THE FITTING AND IS CONSISTENT WITH OTHER CRACKSAug 24, 2020 · N160PB · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20200813001Blower · brokenINTERMITTENT BURNING ODOR (VERY MILD) DETECTABLE IN FLIGHT. INSPECTED AIRCRAFT WITH MASTER AND AVIONICS ON AND COULD NOT DUPLICATE SMELL. FOUND BLOWER TO BE INOPERABLE. REPLACED THE UNIT WITH NO FURTHER DEFECTS NOTED.Aug 12, 2020 · N677CA · Cessna 402C · Air Distribution FanSDR HYIA20200521001Adapter · brokenDURING INITIAL CLIMB APPROXIMATELY 3 MINUTES AFTER TAKEOFF THE CREW REPORTED A LT YAW MOVEMENT AND RECOGNIZED LT ENGINE MAP INDICATION DROPPING FOLLOWED BY A RAPIDLY DECREASING LT ENGINE OIL PRESSURE INDICATION. THE CREW ALSO REPORTED WHITE SMOKE STREAMING FRMay 20, 2020 · N6875D · Cessna 402C · Reciprocating Engine Oil SystemSDR HYIA20200519001Spar Cap · corrodedDURING MAINTENANCE TWO SPOTS OF CORROSION WERE VISUALLY IDENTIFIED ON THE AFT LEFT HAND VERTICAL SPAR CAP (P/N: 5131007-5) OF THE  VERTICAL STABILIZER. THESE SPOTS EXIST AT APPROXIMATE W.L 156.52 AND W.L. 167.52, AND HAVE A MAXIMUM DEPTH OF .033 INCHES. THIS DMay 19, 2020 · N409BK · Cessna 402C · Vertical Stabilizer, Spar/RibSDR HYIA20200512001Ignition Unit · burned outPILOT REPORTED A NOXIOUS SMELL DURING FLIGHT, AND NOTED THE HEATER DID NOT FEEL LIKE IT WAS PERFORMING. MAINTENANCE INSPECTED AND FOUND THE HEATER IGNITION UNIT TO BE BURNT OUT. REPLACED THE UNIT WITH NO FURTHER DEFECTS NOTED.May 8, 2020 · N3292M · Cessna 402C · Heating SystemSDR HYIA202005223004Cylinder · damagedPILOT REPORTED A STRONG VIBRATION IN FLIGHT. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINE #1 CYLINDER TO HAVE LOW COMPRESSION AND THE #3 AND #4 CYLINDERS TO HAVE DAMAGE AT THE ROTOCOIL. ALL THREE CYLINDERS WERE REPLACED WITH NO FURTHER DEFECTS NOTED.May 7, 2020 · N751CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA202005222004Cylinder · damagedPILOT REPORTED A STRONG VIBRATION IN FLIGHT. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINE #1 CYLINDER TO HAVE LOW COMPRESSION AND THE #3 AND #4 CYLINDERS TO HAVE DAMAGE AT THE ROTOCOIL. ALL THREE CYLINDERS WERE REPLACED WITH NO FURTHER DEFECTS NOTED.May 7, 2020 · N751CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA202005221004Cylinder · failedPILOT REPORTED A STRONG VIBRATION IN FLIGHT. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINE #1 CYLINDER TO HAVE LOW COMPRESSION AND THE #3 AND #4 CYLINDERS TO HAVE DAMAGE AT THE ROTOCOIL. ALL THREE CYLINDERS WERE REPLACED WITH NO FURTHER DEFECTS NOTED.May 7, 2020 · N751CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20200508003Fitting · corrodedWHILE PERFORMING LIGHTED BOROSCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R2 TO SATISFY AD2017-10-09, A SPOT OF CORROSION WAS IDENTIFIED ON THE RIGHT HAND OUTBOARD NACELLE FITTING (P/N: 5292029-24). THIS CORROSION IS LOCATED ON THE BOTTOM OF THE May 7, 2020 · N120PC · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20200521002Cylinder · low pressurePILOT REPORTED ROUGH RUNNING ENGINE. MAINTENANCE INSPECTED AND FOUND RIGHT #5 CYLINDER NO COMPRESSION. REMOVED AND REPLACED ENGINE WITH NO FURTHER DEFECT NOTED, AS WAS SCHEDULED FOR REMOVAL WITHIN 87 HOURS.May 6, 2020 · N120PC · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20200508001Connecting Rod · damagedDURING ROUTINE INSPECTION AND REPLACEMENT OF THE RIGHT ENGINE CYLINDER #3 IT WAS DISCOVERED THAT THE CONNECTING ROD BUSHING OF THE #3 CYLINDER WAS FOUND TO BE DAMAGED AND LOOSE. THE CONNECTING ROD AND CYLINDER WILL BE REPLACED.May 6, 2020 · N514NC · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20200508004Fitting · crackedWHILE PERFORMING LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXTRON MEL-54-02R2 TO SATISFY AD2017-10-09, A CRACK WAS IDENTIFIED IN THE OUTBOARD RADIUS OF THE RIGHT HAND OUTBOARD NACELLE FITTING. THIS CRACK MEASURES .300 INCHES LONG AND IS CONSISTENTMay 5, 2020 · N375R · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20200422001Bushing · migratedDURING ROUTINE INSPECTION AND REPLACEMENT OF THE RIGHT ENGINE CYLINDER #6 IT WAS DISCOVERED THAT THE CONNECTING ROD BUSHING OF THE #6 CYLINDER WAS FOUND TO BE LOOSE AND MIGRATING. THE CONNECTING ROD AND CYLINDER WILL BE REPLACED.Apr 21, 2020 · N2611X · Cessna 402C · Reciprocating Engine Power SectionSDR 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 HYIA2020031300001Beam · crackedDURING ULTRASONIC INSPECTION PERFORMED IN ACCORDANCE WITH AVENGER AEROSPACE SOLUTIONS AAS-ALS-15-002 REV C PER CAPE AIR REFERENCE 1 AMOC TO SATISFY AD2015-07-03, A CRACK WAS IDENTIFIED ON THE TOP FACE OF THE RIGHT HAND INBOARD ENGINE BEAM. THIS CRACK MEASURES Mar 11, 2020 · N903CA · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20200313001Hose · brokenPILOT REPORTED RIGHT BRAKE FAILURE. MAINTENANCE INSPECTED AND FOUND THE FLEXIBLE HOSE CONNECTED TO THE RIGHT MASTER CYLINDER BROKEN. REMOVED AND REPLACED THE FLEXIBLE HOSE, AND PREFORMED BLAKE BLEEDING PROCEDURES. NO FURTHER DEFECTS NOTED.Mar 10, 2020 · N2611X · Cessna 402C · Landing Gear Brake SystemSDR HYIA20200304001Fan · burned outPILOT REPORTED BURNING ODOR IN CABIN. UPON INSPECTION MAINTENANCE, FOUND THE CABIN FAN BURNT OUT. REMOVED AND REPLACED THE CABIN FAN WITH NO FURTHER DEFECTS NOTED.Feb 27, 2020 · N88833 · Cessna 402C · Air Distribution FanSDR HYIA20200227001Cylinder · low pressurePILOT REPORTED RIGHT ENGINE MAP FLUCTUATED IN FLIGHT. MAINTENANCE INSPECTED AND FOUND TURBOCHARGER IMPELLER HARD TO MOVE AS WELL AS LOW COMPRESSION ON THE NUMBER 4 & 6 CYLINDERS. TURBO AND CYLINDERS WERE REPLACED AND THE AIRCRAFT WAS RELEASED TO SERVICE.Feb 23, 2020 · N7037E · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA202002270001Cylinder · low pressurePILOT REPORTED RIGHT ENGINE MAP FLUCTUATED IN FLIGHT. MAINTENANCE INSPECTED AND FOUND TURBOCHARGER IMPELLER HARD TO MOVE AS WELL AS LOW COMPRESSION ON THE NUMBER 4 & 6 CYLINDERS. TURBO AND CYLINDERS WERE REPLACED AND THE AIRCRAFT WAS RELEASED TO SERVICE.Feb 23, 2020 · N7037E · Cessna 402C · Reciprocating Engine Cylinder SectionSDR 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 HYIA20200226001Heater · odorPILOT REPORTED SMELL OF EXHAUST IN CABIN, UPON INSPECTION MAINTENANCE DID NOT NOTE RESIDUAL SMELL. BELIEVED TO BE ISSUE WITH HEATER COMBUSTION CHAMBER. REMOVED AND REPLACED HEATER WITH NO FURTHER DEFECTS NOTED.Feb 21, 2020 · N764EA · Cessna 402C · Heating SystemSDR HYIA202002143001Seal · leakingPILOT NOTED FUEL SMELL IN FLIGHT, DEACTIVATED THE HEATER AND THE SMELL WENT AWAY. MAINTENANCE INSPECTED AND FOUND FAILED SHAFT SEAL ON THE HEATER FUEL PUMP. FUEL PUMP WAS REPLACED WITH NO FURTHER DEFECTS NOTED.Feb 13, 2020 · N205CA · Cessna 402C · Fuel Boost PumpSDR HYIA20200211001Attach Fitting · corrodedDURING MAINTENANCE ON N663AA, SMALL AREAS OF CORROSION WERE VISUALLY IDENTIFIED ON THE LEFT HAND LOWER STUB WING FITTING, (P/N: 0811350-10) LOCATED AT LEFT HAND B.L 54.25. THIS FITTING HAS BEEN REMOVED AND REPLACED USING FACTORY NEW PARTS.Feb 3, 2020 · N663AA · Cessna 402C · Fuselage Main, Attach FittingsSDR HYIA2020013129001Blower · inoperativeTHE PILOT NOTED A BURNING SMELL IN FLIGHT, CABIN FAN CIRCUIT BREAKER POPPED. MAINTENANCE INSPECTED AND DETERMINED TO BE HEATER FAN INOPERATIVE, SYSTEM WAS DISABLED AND PLACED ON MEL, ADDITIONAL DETAILS CAN BE PROVIDED AFTER RECEIPT OF TEARDOWN INSPECTION REPOJan 29, 2020 · N406GA · Cessna 402C · Air Distribution FanSDR HYIA202001210001Spar Cap · crackedA CRACK WAS IDENTIFIED AT THE RT SIDE OF THE LWR FWD CARRYTHROUGH SPAR CAP (AFT MOST IB FASTENER COMMON TO WING JOINT FITTING) WHILE PERFORMING NDT PROCEDURE AS AMOC FOR AD2018-03-03R1. THE CRACK WAS CONFIRMED WITH BOLT HOLE EDDY CURRENT PROCEDURE AFTER THE FJan 21, 2020 · N258PB · Cessna 402C · Wing Spar
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