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 HYIA20140422111Fuel Line · crackedPILOT REPORTED FUEL SMELL IN COCKPIT. FOUND A FUEL LINE FROM THE RT ENG FIREWALL TO THE RT FUEL BOWL LEAKING. THE LINE WAS REPLACED, OPERATIONAL & LEAK CHECK WERE PERFORMED WITH NO DEFECTS NOTED.Apr 20, 2014 · N2615G · Cessna 402C · Aircraft Fuel Distribution SystemSDR HYIA20140421109Unknown · odorPILOT REPORTED A FUEL ODOR IN THE COCKPIT. PERFORMED A FUEL PRESSURE TEST & NO DEFECTS WERE NOTED, NO ACTION TAKEN.Apr 18, 2014 · N223PB · Cessna 402C · Air Distribution SystemSDR HYIA20140421110Drain Line · looseA PAX REPORTED A FUEL SMELL IN THE CABIN AFTER TAKEOFF. TIGHTENED THE DRAIN LINE ON THE RT FUEL AUXILIARY PUMP & PERFORMED A PRESS TEST, NO DEFECTS NOTED.Apr 18, 2014 · N2615G · Cessna 402C · Aircraft Fuel Distribution SystemSDR HYIA20140421108Heater · leakingDURING A TRAINING FLIGHT THE PILOT REPORTED A FUEL SMELL IN THE COCKPIT WHEN THE HEATER WAS ON. HE SHUT OFF THE HEATER & REPORTED THE DISCREPANCY TO MX. SECURED THE B NUT AT THE HEATER FUEL NOZZLE. OPERATIONAL & LEAK CHECKS WERE PERFORMED WITH NO DISCREPANCApr 18, 2014 · N466CA · Cessna 402C · Heating SystemSDR HYIA20140412001Bearing Support · corrodedAT SCHEDULED INSPECTION, SEVERE CORROSION WAS FOUND AT LWR RUDDER HINGE BRACKET & ASSOCIATED BEARING BLOCK. CORRECTIVE ACTION WILL BE TO REMOVE AFFECTED PARTS FOR REPLACEMENT WITH NEW IAW MEB00-4 & PERFORM ADDITIONAL DETAILED INSPECTION OF SURROUNDING STRUCTUApr 10, 2014 · N258PB · Cessna 402C · Rudder Miscellaneous StructureSDR HYIA2014040400002Sensor · failedAUTOPILOT COMPUTER CIRCUIT BREAKER TRIPPED WITH A HOT ELECTRICAL ODOR IN CABIN. INSPECTED & FOUND ODOR FROM ALTITUDE SENSOR. DISCONNECTED AUTOPILOT SYS.Apr 4, 2014 · N3249M · Cessna 402C · Altitude ControllerSDR HYIA2014040100001Actuator · failedPILOT SELECTED GEAR DOWN DURING FUNCTIONAL CHECK FLIGHT, GEAR INDICATED TWO GREEN FOR LT MAIN & NLG, RED UNSAFE FOR RT MLG. PILOT CYCLED LG SEVERAL TIMES, UNSAFE CONDITION REMAINED. PERFORMED EMERGENCY EXTENSION CHECKLIST & PULLED TEE HANDLE TO BLOW MLG DOWMar 22, 2014 · N18VV · Cessna 402C · Landing Gear ActuatorSDR HYIA03142014001Spar Cap · corrodedDURING ROUTINE SCHEDULED INSPECTION, AREAS OF CORROSION WERE FOUND AT LT & RT LWR WING SPAR CAP STRAPS PREVIOUSLY INSTALLED VIA CESSNA SK402-47 ON 04/16/2003 TO SATISFY REQUIREMENT OF CESSNA MEB02-5 & AD2005-12-13. THE CORRECTIVE ACTION TO REMEDIATE CONDITIONMar 12, 2014 · N2615G · Cessna 402C · Wing SparSDR HYIA2014040400001Pedal · failedRIGHT RUDDER PEDAL ON GROUND. R & R RUDDER PEDAL.Feb 27, 2014 · N402VN · Cessna 402C · Rudder Control SystemSDR HYIA02262014002Wire · damagedSMOKE FROM WIRES LEADING TO WINDSHIELD, WHERE CONNECTS TO CONTROL PEDESTAL.Feb 22, 2014 · N5826C · Cessna 402C · Window System WiringSDR HYIA20140414061Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMENJan 29, 2014 · N2651S · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414060Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEJan 29, 2014 · N6875D · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414059Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEJan 29, 2014 · N7037E · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA01172014001Master Cylinder · contaminatedUPON LANDING IN SJU FLIGHT 4481 LT BRAKE INOPERATIVE. COMPANY MX BLED AIR FROM LT MASTER CYLINDER & RE-SERVICED MASTER CYLINDER WITH HYD FLUID IAW MANUFACTURERS SERVICE INSTRUCTIONS.Jan 13, 2014 · N2748Y · Cessna 402C · Landing Gear Brake SystemSDR HYIA20140109001Caliper · frozenLEFT BRAKE FROZEN UP ON TAXI. REPLACED LT BRAKE CALIPER & REPLACED PARKING BRAKE VLV. PURGED LT BRAKE SYS FLUID & PERFORMED BRAKE BLEEDING. PARKING BRAKE VLV PN C165007-0201, REPLACED AS A PRECAUTION.Jan 9, 2014 · N300SN · Cessna 402C · BrakeSDR HYIA20140102001Heater · faultyCABIN HEATER PRODUCES HEAVY EXHAUST SMELL & MINIMAL HEAT WHEN ON. DEFERRED CABIN HEATER FAN IAW MEL 21-01-2.Dec 30, 2013 · N300SN · Cessna 402C · Heating SystemSDR HYIA201341220001Heater Pump · leakingSTRONG SMELL OF FUEL IN COCKPIT DURING FLIGHT. R & R HEATER FUEL PUMP IAW SERVICE MANUAL, LEAK CHECKED GOOD.Dec 19, 2013 · N88833 · Cessna 402C · Heating SystemSDR HYIA20131219001Engine · failedOPERATING FLIGHT 1821 ALB TO MSS RETURNED TO ALB IMMEDIATELY AFTER TAKEOFF & LANDED SAFELY WITH 3 PAX ON BOARD. PILOT NOTED DECREASING LT ENG OIL PRESS & HEARD A LOUD BANG FROM LT ENG AFTER ROTATION. LT ENG MAGNETO SEPARATED FROM ACCESSORY DRIVE & CONNECTINGDec 19, 2013 · N409BK · Cessna 402C · Engine (Reciprocating)SDR HYIA20131216002Dimmer · malfunctionedSHUT DOWN ENGS & EVACUATED ACFT AFTER DETECTING SMOKE COMING FROM THROTTLE QUADRANT AREA DURING TAXI TO RUNWAY 08. VISUAL INSPECTION OF INSTRUMENT PANEL LIGHT DIMMER ASSEMBLY & FOUND A FAILED RESISTOR INTEGRAL TO ASSEMBLY. REMOVED AFFECTED ASSEMBLY & INSTALLDec 12, 2013 · N764EA · Cessna 402C · Flight Compartment LightingSDR HYIA20131216001Squat Switch · out of adjustLANDING GEAR WOULD NOT RETRACT, RETURN TO BLOCK. FOUND LG SQUAT SWITCH TO BE OUT OF ADJUSTMENT. .Dec 11, 2013 · N402HG · Cessna 402C · Landing Gear Position and WarningSDR HYIA20140414058Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEDec 4, 2013 · N406GA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414057Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEDec 4, 2013 · N6879R · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414056Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEDec 2, 2013 · N160PB · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414055Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEDec 2, 2013 · N747WS · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414054Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEDec 2, 2013 · N67886 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR GULA2014F00057Pump · failedLEFT ENGINE DRIVEN FUEL PUMP FAILED DURING GROUND TRIM RUN UP. UNABLE TO ADJUST FUEL FLOW FOR STABLE FLOW. FUEL FLOW WAS FLUCTUATING AT MID RANGE AND MAX POWER SETTINGS. FAILED ON MAX POWER DROPPING DOWN TO BELOW MID POWER SETTING.Oct 1, 2013 · N67887 · Cessna 402C · Engine Fuel PumpSDR HYIA20131003001Turbocharger · failedRIGHT ENGINE STEADY, LOSS OF MAP IN CRUISE WITH CORRESPONDING DECREASE IN OIL PRESSURE. ELECTED TO SHUTDOWN AND SECURE RT ENGINE IN FLIGHT AND MADE AN UNSCHEDULED LANDING. DURING INSPECTION, RT ENGINE TURBOCHARGER FOUND TO BE AT FAULT. REPLACED RT TURBOCHAOct 1, 2013 · N69SC · Cessna 402C · Exhaust TurbochargerSDR HYIA20140414052Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEAug 15, 2013 · N4630N · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414051Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEAug 14, 2013 · N88833 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414050Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEAug 14, 2013 · N6765T · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414053Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEAug 9, 2013 · N4652N · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414049Drag 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 BEYOND LIMIT ALLOWABLE. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMEAug 8, 2013 · N991AA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA08032013001Pump · faultyRT ENGINE POWER LOSS AND LOSS OF FUEL FLOW IN CRUISE POWER SETTING. PUMP FOUND FAULTY.Aug 2, 2013 · N5826C · Cessna 402C · Engine Fuel PumpSDR HYIA20130727001Light · faultyINSTRUMENT PANEL LIGHTS EXTINGUISHED AFTER TAKEOFF. F/O INSTRUMENT LIGHT CIRCUIT BREAKER TRIPPED FOLLOWED BY MOMENTARY PUFF OF SMOKE.Jul 25, 2013 · N1376G · Cessna 402C · Flight Compartment LightingSDR HYIA20130629106Starter · looseDURING TAKEOFF, THE CREW REPORTED LT ENGINE DECREASING OIL PRESSURE. THE CREW ELECTED TO FEATHER THE PROP, SHUTDOWN THE ENGINE AND RETURN TO ORIGINAL BASE. CONTRACT MX PERFORMED AN INITIAL INSP AND DETERMINED THE LEFT STARTER HAD SEPARATED FROM THE STARTER AJun 26, 2013 · N2611X · Cessna 402C · Engine StarterSDR HYIA20130621001Beam · crackedDURING ROUTINE INSPECTION, DAMAGE WAS NOTED AT LT NACELLE CROSSOVER BEAM INCLUDING A CRACK EXTENDING FROM OTBD EXHAUST HANGAR BRACKET HOLE LOCATIONS.Jun 17, 2013 · N1361G · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20136011105Spar · crackedDURING A ROUTINE SCHEDULED INSPECTION A .61 INCH CRACK WAS FOUND IN THE RT SIDE OF THE FORWARD SPAR WEB AT FS 154.50. THE DAMAGED AREA WAS REPAIRED IAW AAS-SSR-13-70, REV NC, DATED JUNE 10,2013.Jun 7, 2013 · N525RH · Cessna 402C · Fuselage Main, FrameSDR HYIA20130611102Diode · failedON TAXI, THE CREW REPORTED A BURNING ODOR IN THE COCKPIT. MX FOUND A FAILED LT ENGINE STARTER RELAY DIODE FAILED.May 31, 2013 · N106CA · Cessna 402C · Engine Starting System WiringSDR HYIA20130605100Web · crackedDURING A ROUTINE SCHEDULED INSPECTION, A .62" CRACK WAS FOUND IN THE RT SIDE OF THE FORWARD SPAR WEB AT BS 154.50. DAMAGE WAS MAPPED AND SENT TO ENGINEERING. THE DAMAGED AREA WAS REPAIRED IAW A REPAIR DEFINITION SUPPLIED AND SUBSTANTIATED BY REPORT AAS-SSR-1May 31, 2013 · N2611X · Cessna 402C · Fuselage Miscellaneous StructureSDR HYIA20130611104Bolt · failedCREW REPORTED LOSING RT ENGINE MAP AT 9000 FEET AND NOTICED OIL LEAKING FROM RT ENGINE COWL. THE RT PROP WAS FEATHERED AND RT ENGINE SHUTDOWN AND THE ACFT RETURNED TO DEPARTURE AIRFIELD. MX INSPECTED AND FOUND THE CRANKSHAFT GEAR WAS SEPARATED FROM THE CRANKMay 27, 2013 · N1361G · Cessna 402C · Engine (Reciprocating)SDR HYIA20136011103Fuel Line · chafedDURING PREFLIGHT, THE CREW REPORTED A FUEL ODOR IN THE COCKPIT. MX DETERMINED THERE WAS A FUEL LEAK OTBD OF THE NACELLE AND FOUND A CHAFED FUEL LINE AFT OF FORWARD FLOAT VALVE. BOTH DISCREPANCIES WERE REPAIRED AND LEAK CHECK ACCOMPLISHED.May 27, 2013 · N771EA · Cessna 402C · Engine Fuel DistributionSDR HYIA20140414048Drag 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 & AMay 13, 2013 · N88833 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR 2013FA0000302Valve Spring · brokenRIGHT ENGINE BEGAN TO VIBRATE ON SHORT FINAL. FOUND BROKEN INNER AND OUTER EXHAUST VALVE SPRINGS AND BROKEN INTAKE VALVE INNER SPRING ON THE NR 5 CYLINDER. PULLED ROCKER BOX COVERS AND FOUND THE INNER INTAKE AND EXHAUST VALVE SPRINGS BROKEN ON 11 OF 12 CYLINMay 10, 2013 · N402HG · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20130426001Engine · damagedFLIGHT CREW REPORTED THAT DURING CRUISE, NOTICED DECREASING MANIFOLD PRESSURE AS WELL AS DIMINISHING OIL PRESSURE ON THE RT ENGINE AT 6,000". CREW SHUTDOWN ENGINE IN FLIGHT. LANDED SAFELY AT DESTINATION AIRPORT. ON MX INSPECTION, DISCOVERED CONNECTING RODS Apr 25, 2013 · N2611X · Cessna 402C · Engine (Reciprocating)SDR HYIA20130416001Spar · damagedDURING A SCHEDULED MX EVENT, DAMAGE WAS NOTED TO THE AFT CARRY THROUGH SPAR. MULTIPLE DAMAGE POINTS WERE DISCOVERED ON THE SPAR FLOOR SUPPORT FLANGE. OPENApr 15, 2013 · N769EA · Cessna 402C · Fuselage Main, FrameSDR HYIA20130416004Beam · damagedDURING A SCHEDULED MX EVENT DAMAGE WAS NOTED TO THE LT NACELLE OTBD ENGINE BEAM RADIUS. DAMAGE WAS MAPPED AND SUBMITTED FOR ENGINEERING ASSISTANCE. REPAIRS WILL BE COMPLETED IAW REPAIR DEFINITION SUPPLIED AND SUBSTATIATED.Apr 12, 2013 · N1055 · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20130416003Spar · damagedDURING A SCHEDULED MX EVENT, DAMAGE WAS NOTED TO THE AFT CARRY THROUGH SPAR ASSY CENTER SECTION. DAMAGE INCLUDES WEB FLANGE CRACKS. OPENApr 12, 2013 · N1055 · Cessna 402C · Fuselage Main, StructureSDR HYIA20130416002Spar · damagedDURING A SCHEDULED MX EVENT, DAMAGE WAS NOTED TO THE FORWARD CARRY THROUGH SPAR ASSY IN THE CENTER SECTION. DAMAGE INCLUDES DRILL STARTS TO UPPER CAP AND CORRESPONDING WEB FLANGE CRACKS. THESE DAMAGE POINTS WERE MAPPED AND SUBMITTED FOR ENGINEERING ASSISTANCApr 12, 2013 · N1055 · Cessna 402C · Fuselage Main, StructureSDR HYIA20130327001Skin · chafedDURING A SCHEDULED MX INSPECTION, HORIZONTAL STABILIZER WAS REMOVED WHICH REVEALED DAMAGE TO THE ACFT FUSELAGE SKIN. DAMAGE APPEARS TO HAVE BEEN CAUSED BY THE L/E OF THE HORIZONTAL STABILIZER CHAFING INTO THE FUSELAGE SKIN. DAMAGED AREA RANGED FROM FS 342.24 Mar 26, 2013 · N1376G · Cessna 402C · Fuselage Main, Plate/SkinSDR HYIA20130320001Pump · malfunctionedFLIGHT CREW REPORTED THAT PRIOR TO TAKEOFF ALL INDICATIONS WERE NORMAL. SHORTLY AFTER TAKEOFF WHILE CLIMBING, THE CREW REPORTED THAT THE RT ENGINE SURGED AND THEN BEGAN TO LOSE POWER, AT WHICH POINT THE CREW NOTICED A SPIKE IN FUEL FLOW (295 PPH). CREW SHUTOFMar 18, 2013 · N660CA · Cessna 402C · Engine Fuel Pump
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