Cessna 402C

Service difficulty reports · 1,782

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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 13505276875DCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.Jun 3, 2006 · N6875D · Cessna 402C · AC Power Distribution SystemSDR 13505361376GCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.May 31, 2006 · N1376G · Cessna 402C · AC Power Distribution SystemSDR 1350532763EAMaster Switch · inoperativeCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH.May 28, 2006 · N763EA · Cessna 402C · Navigation SystemSDR IWV2006F00000Channel · crackedDURING COMPLIANCE WITH AD 2005-12-13 BY INSTALLATION OF SPAR MOD KIT SK402-47B IT WAS DISCOVERED THAT THE LT NACELLE OB ENGINE SUPPORT BEAM CHANNEL PN 56541111 HAD A 1.75 INCH CRACK RUNNING LONGITUDINALLY ON THE IB RADIUS. THE AREA OF THE CRACK IS IN A LOCATMay 1, 2006 · N18VV · Cessna 402C · Nacelle/Pylon, Main FrameSDR 1350527514Circuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH, MFG DATE CODE 0527.Apr 24, 2006 · N514NC · Cessna 402C · DC Power Distribution SystemSDR 1350522770CACircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP, MX CHANGED CIRCUIT BREAKER SWITCH MFG DATE CODE 0552.Apr 6, 2006 · N770CA · Cessna 402C · Electrical Power System WiringSDR 13505272714BCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH MFG DATE CODE 0527.Mar 30, 2006 · N2714B · Cessna 402C · Electrical Power SystemSDR 2006FA0000417Packing · out of position#1 CYLINDER EXHAUST PUSHROD HOUSING PACKING BLEW OUT. SUSPECT POSSIBLE CRANKCASE PRESSURIZATION. PACKING HAD SMALL CUT MOST LIKELY FROM INSTALLATION HOWEVER THAT SOULD NOT HAVE ALLOWED IT TO BLOW OUT.Mar 29, 2006 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR 13504421361GCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER SWITCH INOP, MX CHANGED CIRCUIT BREAKER SWITCH MFG DATE CODE 0442.Mar 23, 2006 · N1361G · Cessna 402C · Electrical Power SystemSDR CA060112007Intercostal · damagedPILOTS OUTBOARD INTERCOSTAL RUDDER PEDAL MOUNT REPAIRED DUE TO SEVERAL SMALL CRACKS.Jan 1, 2006 · Cessna 402C · Fuselage Main, Attach FittingsSDR AU510001608Line · crackedLINE LOCATED IN RT WING ROOT CRACKED. LIMITED INFORMATION PROVIDED.Dec 12, 2005 · Cessna 402C · Aircraft Fuel Distribution SystemSDR AU510001594Line · worn(AUS) RT ENGINE FUEL SUPPLY LINE LOCATED BETWEEN FUEL BOWL AND NACELLE CHAFED THROUGH ON WING STRUCTURE LIGHTENING HOLE. FUEL LEAKING INTO WING. (CASA NR 510001594)Dec 12, 2005 · Cessna 402C · Engine Fuel DistributionSDR GNB2006F00002Distributor Gear · strippedENROUTE LT ENGINE BEGAN TO RUN ROUGH, LANDED. RUN UP FOUND LT ENGINE MAGNETO ROUGH AND EXCESSIVE DROP. (SW01200603302) (K)Dec 7, 2005 · N57PB · Cessna 402C · Magneto/DistributorSDR GNB2006F00000Distributor Gear · strippedENROUTE, RAN ROUGH, LANDED. RUNUP FOUND RT MAGNETO ROUGH AND EXCESSIVE DROP. (SW01200603304) (K)Dec 6, 2005 · N4643N · Cessna 402C · Magneto/DistributorSDR GNB2006F00001Distributor Gear · strippedPRE TAKEOFF RUNUP CHECKED GOOD. PULLED ONTO RUNWAY, APPLIED POWER, RT ENGINE BEGAN TO RUN ROUGH. ABORTED TAKEOFF. MAINTENANCE DISCOVERED 10-15 TEETH STRIPPED ON DISTRIBUTOR GEAR. VERY COLD TEMP, PROBABLE CAUSE. (SW01200603303) (K)Dec 5, 2005 · N747WS · Cessna 402C · Magneto/DistributorSDR HYI2006F00007Uplock Switch · failedCREW REPORTED RT MAIN GEAR DID NOT FULLY RETRACT WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE RT UPLOCK MICROSWITCH, GEAR SWING CHECKS OK. AIRCRAFT RELEASED FOR SERVICE. (K)Dec 2, 2005 · N618CA · Cessna 402C · Landing Gear Position and WarningSDR HYI2006F00006Uplock Switch · failedCREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE ATTEMPTED TO REMOVE AND REPLACE THE RT UPLOCK MICROSWITCH, 2 SWITCHES FAILED (BAD FROM STOCK) BEFORE INSTALLING A SERVICEABLE UNIT, GEAR SWING CHECKS, OK. AIRCRAFT RELEASDec 2, 2005 · N618CA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYI2006F00004Uplock Switch · failedCREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE RT UPLOCK SWITCH, GEAR SWING CHECKS OK. AIRCRAFT RELEASED FOR SERVICE. (K)Dec 2, 2005 · N618CA · Cessna 402C · Landing Gear Position and WarningSDR HYI2006F00003Uplock Switch · failedCREW REPORTED LT MAIN GEAR DID NOT FULLY RETRACT WITH HEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE LT UPLOCK MICROSWITCH, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K)Dec 2, 2005 · N2615G · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYI2006F00002Uplock Switch · failedCREW REPORTED GEAR UNSAFE LIGHT REMAINTED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE LT UPLOCK MICROSWITCH, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K)Dec 2, 2005 · N2615G · Cessna 402C · Landing Gear Position and WarningSDR HYI2006F00001Uplock Switch · failedCREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE ATTEMPTED TO REMOVE AND REPLACE THE LT HAND UP LOCK MICROSWITCH, 3 SWITCHES FAILED (BAD FROM STOCK) BEFORE INSTALLING A SERVICABLE UNIT, GEAR SWING CHECKS, OK. AIRCRAFT RDec 2, 2005 · N2615G · Cessna 402C · Landing Gear Position and WarningSDR HYI2006F00000Uplock Switch · failedCREW REPORTED GEAR UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE IN UP POSITION, MAINTENANCE REMOVED AND REPLACED THE LT UP LOCK MICROSWITCH, GEAR SWING CHECKS, OK. AIRCRAFT RELEASED FOR SERVICE. (K)Dec 2, 2005 · N2615G · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA051006Axle · crackedON ROLLOUT AFTER LANDING CREW ENCOUNTERED WHAT WAS THOUGHT TO BE A FLAT TIRE. MAINTENANCE PERSONNEL FOUND THAT THE RIGHT MAIN LANDING GEAR AXLE WAS CRACKED AT THE INNER BEARING AREA.Oct 6, 2005 · N1376 · Cessna 402C · Nose/Tail Landing Gear Strut/AxleSDR 08222005Bolt · shearedPROPELLER FAILED TO TURN ON START. CRANKSHAFT LARGE ATTACH BOLTS SHEARED AND GEAR DISLODGED FROM CRANKSHAFT. ENGINE REMOVED AND REPLACED.Aug 22, 2005 · N6875D · Cessna 402C · Engine (Reciprocating)SDR HYI2005F00006Bolt · shearedLT PROPELLER FAILED TO TURN ON START, MAINTENANCE FOUND CRANKSHAFT LARGE ATTACH BOLTS SHEARED AND GEAR DISLODGED FROM CRANKSHAFT. MAINTENANCE REMOVED AND REPLACED THE ENGINE AND RETURNED THE AIRCRAFT TO SERVICE. (NE01200505271) (K)Aug 18, 2005 · N6875D · Cessna 402C · Reciprocating Engine Power SectionSDR HYI2005F00005Connecting Rod · unserviceableAT 3000 FT, ON APPROACH, LT ENGINE BEGAN TO RUN ROUGH, PILOT PERFORMED FLOW CHECK, ALL ENGINE INSTRUMENTS APPEARED NORMAL, BOOST PUMPS TO LOW AS A PRECAUTIONARY. LT ENGINE CONTINUED TO RUN ROUGHER THEN SHUTDOWN, PILOT FEATHERED LT PROPELLER, LANDED WITHOUT INCAug 18, 2005 · N764EA · Cessna 402C · Reciprocating Engine Power SectionSDR 2005FA0001115Tube · splitEIGHT MILES NORTH EAST OF KFLL, PILOT NOTICED A HYDRAULIC SMELL IN THE COCKPIT DURING CLIMB-OUT. THERE WERE NO ABNORMALITIES NOTED. PILOT DECLARED AN EMERGENCY AT KPMP. PILOT LANDED AIRCRAFT AT KPMP WITHOUT INCIDENT. POST FLIGHT REVEALED HYDRAULIC SITE TUBJul 27, 2005 · N78FC · Cessna 402C · Hydraulic Reservoir, MainSDR GNB2005F00005Control Cable · wornWEAR FROM BLENDING DUE TO SOFTER MATERIAL USED IN NEW STYLE CABLE.Jun 28, 2005 · N3292M · Cessna 402C · Aileron Control SystemSDR 2005FA0000895Arm · damagedFOUND THAT THE FLOAT VALVE ARM WAS HITTING THE RETAINER HUB WHEN THE VALVE WAS FULLY ENGAGED. IT WOULD APPEAR THAT THE ARM COULD SUFFER ENOUGH DAMAGE TO SEVER THE ARM FROM THE FLOAT BASE AND THAT WOULD ALLOW THE FLOAT VALVE CLOSE AND SHUT THE FLOW OF FUEL OFFJun 17, 2005 · N145RC · Cessna 402C · Fuel Control/Reciprocating EnginesSDR GNB2005F00004Valve · warpedWARPED VALUE. (K)Jun 8, 2005 · N494BC · Cessna 402C · Exhaust TurbochargerSDR GNB2005F00006Control Cable · wornCABLE BLENDED AT PULLEY. PROBABLE CAUSE, SOFTER NEW STYLE STAINLESS STEEL CABLE MATERIAL. SERVICE LIFE IS ONLY FRACTIONS OF OLD STYLE STEEL CABLES. (K)May 25, 2005 · N305AT · Cessna 402C · Flight Control SystemSDR 04052005Uplock Switch · inoperativeAIRCRAFT HAD THE HYDRAULIC LIGHT REMAIN ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE WAS UNABLE TO DUPLICATE, THE LT DOWNLOCK SWITCH WAS RESEALED AND LUBRICATED, FLIGHT CHECK UNSATISFACTORY, STILL UNABLE TO DUPLICATE ON GROUND, REPLACED NOSE UPLOCK SWITCH ANApr 5, 2005 · N548GA · Cessna 402C · Landing Gear Position and WarningSDR GNB2005F00002Cable · frayedDURING INSPECTION, FOUND RT NOSE STEERING CABLE BLENDED AND FRAYED AT PULLEY. NEW MFG CABLES (STANLESS STEEL) LAST ONLY FRACTION OF TIME AS OLD STYLE CABLES. HAS BECOME MUCH MORE COMMON OCCURRANCE. (K)Apr 3, 2005 · N3292M · Cessna 402C · Landing Gear Steering SystemSDR GNB2005F00001Bolt · shearedRT ENGINE WOULD NOT TURN OVER. REMOVED RT STARTER ADAPTER. FOUND LARGE CRANKSHAFT GEAR NOT ATTACHED. FOUND ALL 6 ATTACH BOLTS SHEARED BUT CONNECTED TOGETHER WITH SAFETY WIRE. (SW01200503998) (K)Apr 3, 2005 · N402SA · Cessna 402C · Reciprocating Engine Power SectionSDR HYI2005F00004Seat · brokenPILOT REPORTED FIXED BACK DOUBLE PASSENGER SEAT BROKEN. MAINTENANCE FOUND SEAT SEPARATED FROM PEDASTAL. REMOVED AND REPLACED SEAT AND SENT BACK TO ORIGINAL MFG FOR REPAIR. SEAT WAS INSTALLED UNDER AVIATION FABRICATOR STC SA2716CE. (K)Mar 7, 2005 · N2611X · Cessna 402C · Passenger Compartment EquipmentSDR HYI2005F00003Beam · crackedDURING ENGINE NACELLE INSPECTION, FOUND 1.5 INCH CRACK ON TOP REAR RADIUS OF CROSSOVER BEAM. REMOVED BEAN AND INSTALLED NEW BEAM IAW MFG MM. (NE01200502852) (K)Feb 16, 2005 · N406GA · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYI2005F00002Bolt · shearedUPON ENGINE START, AFTER SEVERAL ROTATIONS, PROP STOPPED AND WOULD NOT TURN. MECHANIC FOUND CRANKSHAFT LARGE GEAR ATTACH BOLTS SHEARED AND GEAR DISLODGED FROM CRANKSHAFT. MECHANIC REMOVED AND REPLACED ENGINE AND RETURNED AIRCRAFT TO SERVICE. (NE01200502601)Jan 31, 2005 · N26514 · Cessna 402C · Main Landing GearSDR N3B2005F00000Connecting Rod · looseIT APPEARS FOR SURE THAT NUT ON CONNECTING ROD CAP, LOOSEN. BOLT HEAD SHEARED OFF. ENGINE STOPPED RUNNING SOOP AFTERWARD. (BOLT NR 629340) (K)Jan 10, 2005 · N775RC · Cessna 402C · Reciprocating Engine Power SectionSDR HYI2005F00001Relay · stuckAIRCRAFT LOST ELECTRICAL POWER SHORTLY AFTER TAKEOFF. AIRCRAFT LANDED W/O INCIDENT. MECHANIC FOUND RT STRAT RELAY STUCK ON. REMOVED AND REPLACED LT AND RT RELAYS, RT STARTER. AIRCRAFT IS EQUIPPED WITH STAART WARNING LIGHT SYSTEM. MX DETERMINED THAT THE SYJan 3, 2005 · N812AN · Cessna 402C · Engine StarterSDR GNB2005F00000Line · crackedCRACKED PRESSURE LINE AT THE BEND. (SW01200502449) (K)Oct 18, 2004 · N402MQ · Cessna 402C · Standard Practices/StructuresSDR GNB2004F00000Line · crackedPILOT PRE-FLIGHT, HYDRAULIC RESERVOIR LOW. MAINTENANCE PRESSURE CHECKED SYSTEM, FOUND NR 6 PRESSURE LINE CRACKED AT BEND RADIUS.Aug 25, 2004 · N26156 · Cessna 402C · Hydraulic System, MainSDR HYI2005F00000Circuit Breaker · failedON SHORT FINAL, CREW REPORTED SMELL OF SMOKE, TO REDUCE LOAD ALL LIGHTS WERE TURNED OFF, SMELL DISSIPATED. MECHANIC FOUND ANTI COLLISION WIRING DAMAGED NEAR C/B PANEL AND CIRCUIT BREAKER FAILED. REPAIRED WIRING, REPLACED BREAKER AND RETURNED AIRCRAFT TO SERVAug 23, 2004 · N2615G · Cessna 402C · Light System WiringSDR 2004F00274Wire · failedON SHORT FINAL, CREW REPORTED ODOR OF SMOKE, TO REDUCE LOAD ALL LIGHTS WERE TURNED OFF. ODOR DISSIPATED. MAINTENANCE FOUND ANTI COLLISION WIRING DAMAGED NEAR C/B PANEL ON CIRCUIT BREAKER FAILED. REPAIRED WIRING REPLACED BREAKER AND RETURNED AIRCRAFT TO SERVICEAug 23, 2004 · N2615G · Cessna 402C · Light System WiringSDR GNB2004F00001Bearing · destroyedDURING THE FIRST INITIAL 500 HOUR MAGNETO INSPECTION ON A FACTORY ENGINE. MAINTENANCE DISCOVERED AN ODD LOOKING LUBE ON BOTH MAGNETOS AND INSUFFICIENT AMOUNT IN WELL. THE LT MAGNETO BEARING LOOKED OK, HOWEVER, THE RT MAGNETO BEARING WAS UNUSABLE AND METAL TJul 28, 2004 · N402SA · Cessna 402C · Magneto/DistributorSDR RSH2004F00000Barrel · crackedDURING ROUTINE INSPECTION OF LANDING GEAR A CRACK WAS FOUND ON LT LANDING GEAR ANCHOR LUG UPPER TORQUE LINK AND TRUNION ASSY.Jul 8, 2004 · N220RS · Cessna 402C · Main Landing GearSDR CA040604011Shaft · broken(CAN) VACUUM PUMP SHEAR SHAFT, BROKE AFTER INSTALLED. REPLACED PUMP BY OTHER SOURCE.May 27, 2004 · Cessna 402C · Vacuum Distribution SystemSDR CA040604010Shaft · sheared(CAN) VACUUM PUMP SHEAR SHAFT BROKE ON START.May 27, 2004 · Cessna 402C · Vacuum Distribution SystemSDR HYI2004F00002Gear · failedUPON START, RT ENGINE FAILED TO TURN. MECHANIC FOUND PROP COULD NOT BE TURNED BY HAND EITHER. LATER INSPECTION FOUND CRANKSHAFT LARGE GEAR MISSING TEETH, AND STARTER ADAPTER MISSING TEETH ON DRIVE GEAR. MECHANIC TO REMOVE AND REPLACE ENGINE.Apr 19, 2004 · N26514 · Cessna 402C · Reciprocating Engine Power SectionSDR HYI2004F00001Relay · overheatedPILOT ATTEMPTED START OF LEFT ENGINE, ENGINE DID NOT TURN. MECHANIC FOUND START RELAY OVERHEATED AND DISCOLORED REMOVE AND REPLACED RELAY AND STARTER AS A PRECAUTION AIRCRAFT RELEASED BACK TO SERVICE.Apr 19, 2004 · N106CA · Cessna 402C · Engine CrankingSDR X6PA200400003Bulkhead · crackedBOTTOM CENTER OF BULKHEAD FOUND CRACKED AT THE REAR TIE DOWN HOOK ATTACH POINT. CRACK APPEARS TO ORIGINATE FROM OLD REPAIR.Mar 25, 2004 · N350RC · Cessna 402C · Fuselage Main, Bulkhead
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