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"

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 8PCR20171031001Bolt · shearedENGINE DISASSEMBLED FOR OVERHAUL. CRANKSHAFT CLUSTER GEAR BOLTS (6 EACH) SHEARED. NEW PART NUMBER LARGE GEAR (P/N 656991) AND BOLTS (P/N 656990) WERE IN PLACE IAW LATEST SERVICE BULLETINS. LACK OF FRETTING SIGNATURES ON CRANKSHAFT GEARS AND ATTACHING BOLTS Oct 31, 2017 · N258PB · Cessna 402C · Reciprocating Engine Power SectionSDR HYIA20171031001Cylinder · damagedDURING CLIMB OUT OF STT THE CREW REPORTED A DECREASE RT ENGINE MANIFOLD PRESSURE. SUBSEQUENT INCREASE IN RT THROTTLE LEVER DID NOT INCREASE MANIFOLD PRESSURE THOUGH MANIFOLD PRESSURE STABILIZED AT 26". THE FLIGHT WAS CONTINUED. RT ENGINE OIL TEMPERATURE BEGOct 28, 2017 · N26514 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20171027001Resistor · burnedDURING APPROACH, THE CAPTAINS OVERHEAD LIGHT SWITCH WAS ACTUATED AND THE LIGHT DID NOT ILLUMINATED. THE CREW SUBSEQUENTLY ACTUATED THE COPILOT'S OVERHEAD LIGHT SWITCH WHICH ILLUMINATED AND WAS ACCOMPANIED BY AN ODOR OF SMOKE. THE CAPTAIN SHUTDOWN ALL ELECTROct 23, 2017 · N2714M · Cessna 402C · Light System WiringSDR 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 HYIA20170921002Spar Cap · corrodedCORROSION WAS DISCOVERED ON THE AFT LOWER OUTBOARD SPAR CAP. CORROSION WAS FOUND AT RWS 107.21 TO 111.781 ON THE BOTTOM OF THE HORIZONTAL LEG OF THE CAP. DEEPER THAN THE ALLOWABLE LIMITS IAW MEB 91-11 R1, SECTION 3, ITEM B. THE SPAR CAP WAS REPLACED.Sep 16, 2017 · N406GA · Cessna 402C · Wing SparSDR HYIA20171030001Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED AT THE RT MLG ACTUATOR ATTACH FITTING RWS 88.62. THE CRACK ORIGINATED AT A LOCK FASTENER AND EXTENDED DOWN APPROXIMATED .60 INCH AND UPWARD THROUGH THE UPPER RADIUS OF PART APPROXIMATELY .70 INCH. THE UPPESep 14, 2017 · N69SC · Cessna 402C · Wing, Landing Gear Attach FittingsSDR HYIA09212017001Rib · crackedDURING A ROUTINE INSPECTION, A CRACK WAS IDENTIFIED IN THE RT CLOSE OUT RIB. THE CRACK WAS FOUND FROM THE FORWARD ROW OF LOCK FASTENERS IN THE AFT TRUNNION SUPPORT TO THE AFT SIGNAL CONDITIONER MOUNTING UPRIGHT. THE CRACKED MEASURED OUT TO 2.60 INCHES IN LSep 13, 2017 · N406GA · Cessna 402C · Wing Main, Frame StructureSDR HYIA09092017001Rotor Coil · damagedCREW REPORTED ENGINE ROUGHNESS IN FLIGHT AT POWER REDUCTION FOR CRUISE AND MIXTURE FULL RICH. THE ACFT LANDED SAFELY AT ITS INTENDED DESTINATION WITH NO ISSUE. INSPECTION DISCOVERED LOW DIFFERENTIAL COMPRESSION CHECK RESULT AT CYLINDER NR 4 OF THE LT ENGINESep 7, 2017 · N740CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA09052017001Spar Cap · corrodedCORROSION WAS DISCOVERED IN TWO PLACES INSIDE THE FUEL TANK, ON THE FORWARD VERTICAL LEG OF THE RT AFT OUTBOARD SPAR CAP. ONE OF THE AREAS OF CORROSION WAS AT WS 219.2 TO WS 229.71. THE OTHER AREA OF CORROSION WAS AT WS 208.7 TO WS 215.7. BOTH AREAS OF CORROSep 5, 2017 · N67786 · Cessna 402C · Wing SparSDR HYIA09012017001Spar Cap · corrodedWHILE CONDUCTING OTHER MAINTENANCE, CORROSION WAS DISCOVERED IN TWO PLACES INSIDE THE FUEL TANK, ON THE FORWARD RADIUS OF THE LH AFT OUTBOARD SPAR CAP (P/N 5122041-21.) THE FIRST AREA WAS FOUND AT W.S. 228.71 TO W.S. 225.71. THE SECOND AREA WAS DISCOVERED AT WSep 1, 2017 · N67786 · Cessna 402C · Wing SparSDR HYIA20170829001Resistor · burnedIN CRUISE FLIGHT, CREW RECOGNIZED SMOKE FROM DC BUSS PANEL. THE CREW REPORTED NO CIRCUIT BREAKERS OR SWITCH BREAKERS WERE TRIPPED. DURING ISOLATION OF ELECTRICAL SYSTEMS, NO MORE SMOKE WAS NOTED. THE CREW ELECTED TO DIVERT TO KSLK AS A PRECAUTION AND LANDEDAug 25, 2017 · N2714B · Cessna 402C · Air Distribution FanSDR HYIA20170826001Cylinder · damagedCREW REPORTED A STRONG VIBRATION FROM RT ENGINE AS MIXTURE WAS REDUCED BELOW 100 PPH. THE CREW ENRICHED THE MIXTURE AND ELECTED TO DIVERT TO KHYA AS A PRECAUTION. INSPECTION DISCOVERED LOW DIFFERENTIAL COMPRESSION, 0 PSI/80PSI, AT CYLINDER POSITION NUMBER 1Aug 23, 2017 · N740CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR 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 HYIA20170819001Rib · crackedDURING INSPECTION, A CRACK WAS FOUND EMANATING FROM AN AFT TRUNNION SUPPORT FASTENER HOLE ON THE RT CLOSE OUT RIB (P/N 5122155-56.) THE CRACK MEASURED 2.5 INCHES IN LENGTH. UPON REMOVAL OF THE RIB, ALL OF THE AFT TRUNNION SUPPORT FASTENER HOLES WERE FOUND ELOAug 19, 2017 · N161TA · Cessna 402C · Wing, Rib/BulkheadSDR HYIA08242017001Spar Cap · corrodedWHILE REPAIRING A FUEL LEAK, CORROSION WAS DISCOVERED IN TWO PLACES INSIDE THE FUEL TANK, ON THE FORWARD RADIUS OF THE RT AFT OUTBOARD SPAR CAP. THE FIRST AREA OF CORROSION WAS DISCOVERED AT WS 208.1 AND WAS 1 INCH IN LENGTH. THE SECOND AREA WAS LOCATED AT WAug 15, 2017 · N771EA · Cessna 402C · Wing SparSDR HYIA20170719003Rib · crackedDURING A ROUTINE INSPECTION, SIX CRACKS WERE FOUND IN THE LT CLOSE OUT RIB (P/N 5122155-55.) THESE CRACKS WERE LOCATED AT EACH OF THE SIX VERTICAL ATTACHING HOLES OF THE FORWARD ROW OF THE AFT TRUNNION SUPPORT. EACH CRACK IS TWO INCHES IN LENGTH. UPON REMOVAJul 19, 2017 · N402VN · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20170719002Rib · crackedDURING A ROUTINE INSPECTION, A CRACK (.250 IN LENGTH) WAS FOUND IN THE RT CLOSE OUT RIB (P/N 5122155-56.) THIS CRACK WAS FOUND IN THE FORWARD LOWER MOST HOLE OF THE FORWARD TRUNNION SUPPORT. UPON REMOVAL, ALL FASTENERS HOLES WERE FOUND TO BE WITHIN TOLERANCE Jul 19, 2017 · N402VN · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20170719001Rib · crackedDURING A ROUTINE INSPECTION, TWO CRACKS WERE FOUND EMANATING FROM A FWD TRUNNION SUPPORT FASTENER HOLE ON THE RT CLOSE OUT RIB (P/N 5122155-56.) THE CRACKS MEASURED .250 IN LENGTH. UPON REMOVAL OF THE CLOSE-OUT RIB, IT WAS DETERMINED THE AFT ROW OF FASTENER Jul 19, 2017 · N83PB · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20170718001Indicator · faultyPILOT REPORTED SMELL OF SMOKE IN COCKPIT UPON ACTIVATION OF WEATHER RADAR. MAINTENANCE INSPECTED AND DETERMINED TO BE DUE TO FAULTY INDICATOR. SYSTEM WAS PLACED ON MEL.Jul 15, 2017 · N740CA · Cessna 402C · Weather Radar SystemSDR HYIA20170712002Indicator · failedPILOT REPORTED BURNING SMELL FROM WEATHER RADAR WHEN TURNED ON. MAINTENANCE INSPECTED AND FOUND THE SOURCE TO BE A FAULTY INDICATOR. THE SYSTEM WAS PLACED OM MEL UNTIL SCHEDULED MAINTENANCE VISIT.Jul 11, 2017 · N406GA · Cessna 402C · Weather Radar SystemSDR HYIA20170712001Exhaust Valve · brokenPILOT REPORTED RIGHT ENGINE ROUGH AND VIBRATION IN FLIGHT. UPON INSPECTION MX DISCOVERED THE NR 4 EXHAUST VALVE TO BE BROKEN.Jul 10, 2017 · N256CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20170705004Rib · crackedDURING A ROUTINE INSPECTION, A CRACK WAS IDENTIFIED IN THE RT CLOSEOUT RIB AT RWS 106.79. ON REMOVAL, IT WAS NOTED THAT THE FASTENER HOLE WHERE THE CRACK STARTED FROM WAS NO LONGER IN TOLERANCE FOR THE LOCK FASTENER THAT WAS PREVIOUSLY INSTALLED THERE.Jul 5, 2017 · N258PB · Cessna 402C · Wing, Rib/BulkheadSDR HYIA20170705003Attach Bracket · crackedWHILE PREFORMING MAINTENANCE, A CRACK WAS DISCOVERED IN THE RT MAIN ACTUATOR ATTACH BRACKET.Jul 5, 2017 · N67886 · Cessna 402C · Wing, Attach FittingsSDR HYIA20170705002Fitting · crackedWHILE PREPPING THE LOWER NACELLE SKIN FOR SID 57-10-16 NDT INSPECTION, A CRACK WAS IDENTIFIED IN THE RT INBOARD NACELLE FITTING.Jul 5, 2017 · N771EA · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170705001Fitting · crackedWHILE PREPPING THE LOWER NACELLE SKIN FOR SID 57-10-16 NDT INSPECTION, TWO CRACKS WERE IDENTIFIED IN THE LT OUTBOARD NACELLE FITTING.Jul 5, 2017 · N6813J · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170706001Connecting Rod · bentPILOT REPORTED LEFT ENGINE RAN ROUGH DURING CLIMB AND THEN LATER ON GROUND AT IDLE. UPON INSPECTION, THE CONNECTING ROD ON THE NR 5 CYLINDER WAS FOUND TO BE BENT. THE ENGINE WAS REPLACED.Jun 30, 2017 · N818AN · Cessna 402C · Reciprocating Engine Power SectionSDR HYIA20170614001Circuit Breaker · failedPILOT REPORTED THE AVIONICS SWITCH BREAKER TRIPPED IN FLIGHT. MAINTENANCE REMOVED A REPLACED THE AVIONICS BUSS CIRCUIT BREAKER AND OPERATIONALLY CHECKED OK WITH NO FURTHER ISSUES.Jun 12, 2017 · N57PB · Cessna 402C · AC Power Distribution SystemSDR HYIA20170602001Cable · brokenPILOT REPORTED ON LOWERING THE FLAPS AFTER THE FIFTEEN DEGREE POINT, HEARD A LOUD SNAP/BANG AND THE PLANE ABRUPTLY ROLLED TO THE RIGHT FOR A SPLIT SECOND BUT THEN STRAIGHTENED OUT. LANDED AS SOON AS POSSIBLE. MAINTENANCE INSPECTED AND FOUND THAT THE UPPER RT FMay 31, 2017 · N68391 · Cessna 402C · Trailing Edge Flap Control SystemSDR HYIA20170530001Fuel Line · damagedPILOT REPORTED BURNING SMELL IN CABIN, WITH THE ODOR SEEMING TO BE ASSOCIATED WITH THE HEATER. FOUND THE HEATER FUEL LINE DAMAGED. REPLACED THE FUEL LINE.May 29, 2017 · N524CA · Cessna 402C · Heating SystemSDR HYIA20170828016Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .123 IN LENGTH.May 25, 2017 · N26632 · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170828011Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE LT OUTBOARD FITTING. THE CRACK AS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .102 IN LENGTH.May 19, 2017 · N810BW · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170821001Rib · crackedDURING A ROUTINE INSPECTION, A CRACK WAS LOCATED AT RIB RT WS. 106.79. THE CRACK WAS 1.5 INCHES IN LENGTH, REPLACED THE RIB IAW MM.May 9, 2017 · N514NC · Cessna 402C · Wing StructureSDR HYIA20170512001Pump · leakingPILOT REPORTED FUEL SMELL IN CABIN WITH HEATER RUNNING. UPON INSPECTION, MAINTENANCE DETERMINED TO BE FROM LEAKING HEATER FUEL PUMP THAT WAS DRAINING FROM HEATER VENT LINE. REPLACED FUEL PUMP WITH NO FURTHER DEFECTS NOTED.May 9, 2017 · N2615G · Cessna 402C · Heating SystemSDR HYIA20170510001Exhaust Valve · brokenPILOT REPORTED LEFT ENGINE RUNNING ROUGH IN CRUISE. MAINTENANCE INSPECTED AND FOUND THE NUMBER TWO CYLINDER EXHAUST VALVE BROKEN AND PUSHROD BENT. ENGINE HAS BEEN REMOVED FOR TEARDOWN ANALYSIS; FURTHER DETAIL WILL BE PROVIDED UPON RECEIPT OF TEARDOWN REPORT.May 6, 2017 · N5826C · 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 HYIA20170503002Unknown · odorPILOT REPORTED A BURNING ODOR IN THE CABIN WITH THE HEATER ON, AFTER LANDING NOTICED CABIN VENT FAN CIRCUIT BREAKER TRIPPED. OPENMay 2, 2017 · N68391 · Cessna 402C · Air Distribution SystemSDR HYIA20170503001Cylinder · brokenPILOT REPORTED SHUDDERING AND VIBRATION FROM LEFT ENGINE. UPON INSPECTION MAINTENANCE FOUND THE CYLINDER ROTOCOIL BROKEN. CYLINDER WAS REPLACED, ADDITIONAL DETAILS TO BE CONVEYED UPON TEARDOWN ANALYSIS.Apr 28, 2017 · N6813J · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20170428001Spar Cap · crackedDURING ROUTINE INSPECTION, A CRACK WAS FOUND IN THE RIGHT HAND SIDE LOWER FORWARD CARRY THROUGH SPAR CAP; IN THE VICINITY OF THE LOWER WING ATTACH FITTING (B.L. 47.25). THE CRACK EXTENDS THROUGH THE BULK SECTION OF THE SPAR CAP. CORRECTIVE ACTION WILL BE TO INApr 24, 2017 · N7037E · Cessna 402C · Fuselage Main, StructureSDR HYIA20170828009Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .098 IN LENGTH.Apr 14, 2017 · N494BC · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170403001Exhaust Valve · crackedPILOT REPORTED A VIBRATION FROM THE RIGHT ENGINE, 30-40 SECONDS INTO FLIGHT. MAINTENANCE INSPECTED AND FOUND THE RIGHT ENGINE NR 6 CYLINDER TO HAVE LOW COMPRESSION AND THE EXHAUST VALVE SHOWING SIGNS OF CRACKING. REPLACED THE CYLINDER AND OPS CHECKED GOOD.Mar 31, 2017 · N890CA · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20170331001Terminal · loosePILOT REPORTED SMOKE IN COCKPIT IN VICINITY OF FLAP INDICATOR/HANDLE. MAINTENANCE INSPECTED AND FOUND FLAP INDICATOR POST LIGHT TERMINAL LOOSE AND ARCHING; RE-SECURED FLAP INDICATOR POST LIGHT AND REPLACED HEAT SINK ASSEMBLY.Mar 29, 2017 · N300SN · Cessna 402C · Flight Compartment LightingSDR HYIA20170828008Fitting · crackedDURING A ROUTINE INSPECTION, THREE CRACKS WERE FOUND ON THE LT OUTBOARD NACELLE FITTING. THESE CRACKS WERE DISCOVERED ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACKS MEASURED .088, .097, AND .155 IN LENGTH.Mar 28, 2017 · N494BC · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170828002Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT INBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK IS APPROXIMATELY 1.208 INCHES IN LENGTH. OPENMar 8, 2017 · N36911 · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20170828001Fitting · crackedWHILE CONDUCTING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT INBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS APPROXIMATELY 1.208 INCHES IN LENGTH.Mar 8, 2017 · N36911 · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170308001Switch · intermittentPILOT REPORTED NOSE GEAR COLLAPSED ON LANDING. INITIAL INSPECTION AND TESTING INDICATES A FAULTY ACTUATOR SWITCH FALSELY INDICATED GEAR WAS DOWN AND LOCKED.Mar 6, 2017 · N2649Z · Cessna 402C · Landing Gear Position and WarningSDR HYIA20170307001Master Switch · odorPILOT REPORTED BURNING RUBBER SMELL IN MAIN CABIN, MAINTENANCE INSPECTED AND REPLACED THE AVIONICS MASTER SWITCH DUE TO SUSPECTED INTERNAL FAILURE (SUSPECTED DUE TO ODOR- NON REPAIRABLE PART).Mar 4, 2017 · N26514 · Cessna 402C · AC Power Distribution SystemSDR HYIA20170828006Fitting · crackedDURING A ROUTINE INSPECTION, TWO CRACKS WERE FOUND IN THE RT OUTBOARD NACELLE FITTING. THERE WAS ONE CRACK IN THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS .108 IN LENGTH. THE OTHER CRACK WAS DISCOVERED ON THE OUTBOARD SIDE OMar 3, 2017 · N2714M · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170828005Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS FOUND ON THE LT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS MEASURED AT .191 IN LENGTH.Mar 3, 2017 · N2714M · Cessna 402C · Nacelle/Pylon, Attach FittingsSDR HYIA20170828013Fitting · crackedDURING A SID 57-10-16 NDT INSPECTION, FOUR CRACKS WERE FOUND IN THE LT OUTBOARD FITTING. TWO OF THESE CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THEY MEASURED .143 AND .129 IN LENGTH. THE OTHER TWO CRACKS WERE FOUND OFeb 20, 2017 · N88833 · Cessna 402C · Nacelle/Pylon, Attach Fittings
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