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 HYIA20140415018Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 28, 2011 · N1055 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415017Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 28, 2011 · N68752 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415016Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 28, 2011 · N2649Z · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415015Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 28, 2011 · N6875D · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415014Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 28, 2011 · N812AN · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415013Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 27, 2011 · N818AN · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415012Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 27, 2011 · N991AA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415011Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 27, 2011 · N67786 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415010Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 27, 2011 · N401TJ · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415009Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 27, 2011 · N6879R · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA375RLFTGRWire · brokenCREW REPORTED, ON APPROACH TO LAND, LANDING GEAR WAS EXTENDED BUT LT MAIN GEAR DOWN AND LOCK LIGHT FAILED TO ILLUMINATE. LAMP PRESS TO TEST OK. GEAR WARNING HORN DID NOT SOUND FOR THROTTLE OR FLAP TEST. ALTERNATE GEAR EXTENSION WAS PERFORMED PER "GEAR WILL NOJan 25, 2011 · N375R · Cessna 402C · Landing Gear System WiringSDR HYIA20140415008Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 21, 2011 · N4652N · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415007Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRAC 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OUJan 21, 2011 · N494BC · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415006Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 21, 2011 · N1361G · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415005Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 21, 2011 · N300SN · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA548GARTGRUplock Hook · wornCREW REPORTED, AFTER TAKEOFF, UPON GEAR RETRACTION, GREEN DOWNLOCK LIGHTS EXTINGUISHED, HYD PRESSURE LIGHT REMAINED ILLUMINATED ALONG WITH RED GEAR UNSAFE LIGHT. LANDING GEAR CONTINUED TO CYCLE IN AND OUT OF THE WHEEL WELLS. AFTER LEVELING AT 1000 FT, EMERGENCJan 21, 2011 · N548GA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415004Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 19, 2011 · N660CA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415003Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 19, 2011 · N247GS · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415002Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OJan 19, 2011 · N375R · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415001Drag 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 WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE Jan 19, 2011 · N524CA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA6879RHTRIgnition Unit · shortedCREW REPORTED, CABIN HEATER INOPERATIVE DURING FLIGHT. 20 MINUTES PRIOR TO REACHING FINAL DESTINATION, CREW REPORTED ODOR OF SOMETHING MELTING OR SMOLDERING. HEATER WAS TURNED OFF, AND HEATER FUEL SOURCE WAS TURNED OFF ALSO. AFTER A FEW MINUTES, ODOR WENT AWAJan 3, 2011 · N6879R · Cessna 402C · Heating SystemSDR HYIA548GAHTRLimit Switch · shortedCREW REPORTED, WHILE IN CRUISE, SMOKE APPEARED IN THE CABIN, ALONG WITH A ELECTRICAL ODOR. EMERGENCY WAS DECLARED, AFTER WHICH ALL ELECTRICAL EQUIPMENT WAS TURNED OFF. FUEL SUPPLY TO HEATER WAS ALSO SHUT OFF. AFTER SEVERAL MINUTES, THE SMOKE AND ODOR DISSIPATEDec 24, 2010 · N548GA · Cessna 402C · Heating SystemSDR HYIA121PBLFTENGConnecting Rod · brokenCREW REPORTED, CLIMBING THROUGH 6300' MSL, LT ENGINE BEGAN TO SHUDDER AND RUN ROUGH, EGT WENT TO ZERO, AND OIL PRESSURE BEGAN DROPPING. SMOKE AND OIL STARTED COMING FROM TOP OF THE ENGINE COWL. CREW SECURED ENGINE AND RETURNED TO BLOCK. LANDING WAS UNEVENTFDec 23, 2010 · N121PB · Cessna 402C · Reciprocating Engine Power SectionSDR HYIA6879RDEICEDeice System · malfunctionedCREW REPORTED, AT CRUISE ALTITUDE, ACFT BEGAN ENCOUNTERING ICING CONDITIONS. WING AND STABILIZER DEICE BOOTS FAILED TO REMOVE ICE. CREW REPORTED SURFACE DEICE SYS AS INOPERATIVE ALTHOUGH SYS HAD CHECKED NORMAL EARLIER IN THE DAY. SEVERAL ATTEMPTS AT CHANGING Dec 13, 2010 · N6879R · Cessna 402C · Airfoil Anti/De-ice SystemSDR CA101213003Cylinder · cracked(CAN) 3 CRACKED CYLINDERS AT SAME TIME. NR 1 CYLINDER HAD A CRACK BETWEEN COOLING FINS. NR 3 CYLINDER CRACKED FROM TOP OF COOLING FIN TO CYLINDER WALL. NR 5 CYLINDER WAS CRACKED 2/3RDS THE WAY AROUND THE CYLINDER HEAD (CAUSING POWER LOSS) NR 1 CYLINDER S/N526-Dec 8, 2010 · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA494BCRTENGFuel Control · out of adjustCREW REPORTED, WHILE PERFORMING "IN RANGE" CHECKLIST, RT ENGINE QUIT. CREW PERFORMED ENGINE FAILURE CHECKLIST, AND WHEN AUXILARY FUEL PUMP WAS TURNED ON HIGH POSITION, ENGINE POWER WAS RESTORED. EMERGENCY WAS DECLARED, AND CREW ELECTED TO DIVERT BECAUSE OF BETDec 7, 2010 · N494BC · Cessna 402C · Fuel Controlling SystemSDR HYIA409BKCBNHTSwitch · shortedCREW REPORTED, ON DESCENT, NOTICED AN ODOR AND SAW SMOKE COMING FROM CABIN HEAT SWITCH. EMERGENCY WAS DECLARED, DEACTIVATED ALL ELECTRICAL SYS AND SMOKE STOPPED. TURNED ON SELECTIVE ELECTRICAL EQUIPMENT ON TO FINISH APPROACH, LANDING WAS UNEVENTFUL. MX FOUNDDec 1, 2010 · N409BK · Cessna 402C · Heating SystemSDR HYIA26514AP1128Computer · shortedCREW REPORTED, ON FINAL APPROACH, A SMALL PUFF OF SMOKE CAME FROM THE NAV/COM PANEL. CREW ACCOMPLISHED SMOKE IN COCKPIT CHECKLIST, SMOKE QUICKLY SUBSIDED AND NO FURTHER SIGNS OF THE PROBLEM EXISTED. ADVISED THE TOWER, AND LANDED WITHOUT INCIDENT. MX INSPECTNov 28, 2010 · N26514 · Cessna 402C · Autopilot ComputerSDR HYIA69SC1124Switch · burnedCREW REPORTED ODOR IN COCKPIT. INTIALLY SUSPECTED HEATER, BUT ODOR REMAINED AFTER HEATER WAS TURNED OFF. CREW NOTICED SMOKE COMING FROM INSTRUMENT PANEL LIGHTING SWITCH. TURNED OFF SWITCH, SMOKE STOPPED, LANDED WITHOUT INCIDENT. MX R & R INSTRUMENT PANEL DINov 24, 2010 · N69SC · Cessna 402C · Instrument PanelSDR HYIA6879RRTENGExhaust Valve · failedCREW REPORTED, DURING INITIAL CLIMB OUT, EXPERIENCED PARTIAL POWER LOSS ON RT ENG, CONSISTENT WITH LOSS OF TURBOCHARGER. CONTINUED CLIMB OUT AT FULL POWER TO CRUISE SETTING AT 7000 FT WHILE DECLARING AN EMERGENCY AND REQUESTING DIVERSION. EXPERIENCED OIL LEAKNov 17, 2010 · N6879R · Cessna 402C · Reciprocating Engine Power SectionSDR HYIA781RHENG1115Pump · faultyCREW REPORTED, AFTER LEVELING OFF IN CRUISE, RT ENGINE FUEL FLOW STARTED TO FLUCTUATE SLIGHTLY. AFTER ABOUT 30 SECONDS, FUEL FLOW FLUCTUATION INCREASED IN LARGER INCREMENTS, THEN WENT TO ZERO. AT THIS POINT THE ENGINE QUIT. AUXILIARY PUMP WAS TURNED ON HIGH ANov 14, 2010 · N781EA · Cessna 402C · Engine Fuel PumpSDR HYIA818ANMAP1105Line · brokenCREW REPORTED, AFTER LEVELING AT 4000 FT, IN CRUISE CONFIGURATION, POWER WAS REDUCED TO 26" OF MANIFOLD PRESSURE. LT ENGINE WENT TO TO 26" OF MANIFOLD PRESSURE, BUT RT ENGINE REMAINED AT 29". CREW ELECTED TO DIVERT, WHERE AN EMERGENCY WAS DECLARED. LANDINGNov 5, 2010 · N818AN · Cessna 402C · Manifold Pressure (MP) IndicatingSDR HYIA6813J1024Resistor · burnedCREW REPORTED, IN CRUISE, STRONG ELECTRIAL SMELL IN COCKPIT. CREW DIVERTED. MX INSPECTED ACFT, R & R OVERHEATED CABIN HEATER FAN HIGH - LOW RESISTOR. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE.Oct 24, 2010 · N6813J · Cessna 402C · Air Conditioning System WiringSDR HYIA160PBKI525Hsi · failedCREW REPORTED, IN CRUISE CONFIGURATION, SMOKE WAS NOTICED BEHIND THE GLASS OF THE HORIZONTAL SITUATION INDICATOR. SMOKE WAS CONTAINED INSIDE THE INDICATOR, BUT THE CABIN DID HAVE AN ACRID BURNING ODOR. UNIT CIRCUIT BREAKER WAS PULLED WHICH STOPPED THE SMOKE.Sep 30, 2010 · N160PB · Cessna 402C · Directional Gyro and Indicating SystemSDR HYIA68752RBRK810Master Cylinder · underservicedCREW REPORTED, RT BRAKE FAILED ON TAXI WHICH LEAD TO AFT PROCEEDING INTO GRASS OFF TAXIWAY. MX INSPECTED ACFT BRAKING SYS, SERVICED RT MASTER CYLINDER. ACFT RELEASED BACK TO SERVICE.Aug 25, 2010 · N68752 · Cessna 402C · Master Cylinder/Brake ValveSDR HYIA67886LFTTQLNKBolt · missingCREW REPORTED, ON TOUCHDOWN, LT MAIN GEAR BRAKE APPEARED TO LOCK UP. DIRECTIONAL CONTROL PARTIALLY MAINTANED, BUT DID VEER OFF RUN WAY ON TO GRASS APRON. MX INSPECTED LT MAIN GEAR AND FOUND TORQUE LINK CTR PIVOT BOLT AND ASSOCIATED HARDWARE MISSING. R & R LT Aug 25, 2010 · N67886 · Cessna 402C · Main Landing Gear Attach SectionSDR HYIA494BCKG102Gyro · failedCREW REPORTED HSI FAILED (FROZEN) DURING CLIMB IN HEAVY RAIN AND MODERATE TURBULENCE. EMERGENCY DECLARED, DIVERTED. LANDING WAS UNEVENTFUL. MX FOUND REMOTE GRYO CIRCUIT BREAKER POPPED. R & R REMOTE GYRO. ACFT RELEASED BACK TO SERVICE.Aug 25, 2010 · N494BC · Cessna 402C · Directional Gyro and Indicating SystemSDR HYIA69SCRXL802Axle · crackedUPON TAXING INTO POSITION TO HOLD FOR TAKEOFF,CREW REPORTED EXPERIENCING TAXIING/ BRAKING DIFFICULTIES. MX FOUND RT MAIN GEAR LOWER BARREL AND AXLE ASSY CRACKED. MX R & R RT MAIN GEAR LOWER BARREL AND AXLE ASSY. ACFT RETURNED TO SERVICE.Aug 2, 2010 · N69SC · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA402VNRTRUNNBarrel · unserviceableCREW REPORTED, RT MAIN GEAR SHEARED OFF ON LANDING ROLL. MX FOUND RT MAIN GEAR UPPER BARREL AND TRUNNION ASSY SHEARED JUST BELOW MLG ACTUATOR ATTACH POINT. MX IS IN THE PROCESS OF REPLACING RT MLG ASSY, RT ENGINE, RT PROPELLER, RT SIDE INBD AND OTBD FLAP PANEJul 27, 2010 · N402VN · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA747LFTGEARDownlock Switch · out of adjustON APPROACH, CREW REPORTED LT MAIN GEAR DOWN AND LOCK INDICATOR FAILED TO ILLUMINATE. COMPLIED WITH EMERGENCY GEAR EXTENSION,STILL NO DOWN LOCK INDICATION, DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED LEFT MAIN GEAR DOWN LOCK SWITCH. COMJul 22, 2010 · N747WS · Cessna 402C · Landing Gear Position and WarningSDR HYIA812RAXLEAxle · fracturedON TAKEOFF ROLL, ACFT STARTED TO TURN SHARPLY TO THE RT, ABORTED TAKEOFF. MX FOUND RT MAIN GEAR AXLE BROKEN AT LOWER HALF. MX R & R LOWER BARREL AND AXLE ASSY AND RETURNED ACFT BACK TO SERVICE.Jul 22, 2010 · N812AN · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA618CARHAXLEAxle · brokenON TAKEOFF ROLL, CREW EXPERIENCED A YAW WHICH CAUSED THE TAKEOFF TO BE DISCONTINUED AT LOW SPEED. CREW TAXIED BACK TO THE RAMP. MX FOUND RT MAIN GEAR AXLE ASSY BROKEN AT LOWER HALF. MX R & R AXLE ASSY, AND RETURNED THE ACFT BACK TO SERVICE.Jun 18, 2010 · N618CA · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA36911RHAXLEAxle · crackedON TAXI, CREW REPORTED LOAD "POP" FROM RT GEAR, ACFT BECAME DIFFICULT TO TAXI. MX FOUND RT MAIN GEAR AXLE ASSY CRACKED AT LOWER HALF. R & R AXLE ASSY. RELEASED ACFT BACK TO SERVICE.Jun 18, 2010 · N36911 · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA83PB615GEARLanding Gear · malfunctionedON GEAR RETRACTION, 3 GREEN DOWN AND LOCK LIGHTS EXTINGUISHED, HYD PRESSURE LIGHT EXTINGUISHED, BUT GEAR UNLOCK LIGHT REMAINED ILLUMINATED. AFTER SEVERAL ATTEMPTS TO RETRACT THE GEAR, CONDITION REMAINED THE SAME. GROUND PERSONNEL CONFIRMED THAT THE LT MAIN GEAJun 15, 2010 · N83PB · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA247GSAVIONICSRadio · malfunctionedON DESCENT, CREW REPORTED BOTH COMMMUNICATION RADIOS FAILED TO TRANSMIT OR RECEIVE. EMERGENCY WAS DECLARED, LANDING WAS UNEVENTFUL. MX INSPECTED ACFT, ALL SYS CHECKED NORMAL. COULD NOT DUPLICATE COMMUNICATION FAILURE. ACFT RELEASED BACK TO SERVICE.May 27, 2010 · N247GS · Cessna 402C · Communications SystemSDR HYIA660CADB2Drag Brace · brokenDURING LANDING ROLLOUT, NOSE GEAR COLLAPSED. ALL INDICATIONS WERE NORMAL. MX FOUND NOSE GEAR DRAG BRACE BROKEN AT ACTUATOR ATTACH POINT. MX PERFORMED TEMPORARY REPAIRS, REPLACED PROPELLERS, FERRIED ACFT BOS FOR PERMENANT REPAIRS.May 22, 2010 · N660CA · Cessna 402C · Nose/Tail Landing GearSDR HYIA660CADRAGBRACDrag Brace · brokenDURING LANDING ROLLOUT, NOSE GEAR COLLAPSED. ALL INDICATIONS WERE NORMAL. MX FOUND NOSE GEAR DRAG BRACE BROKEN AT ACTUATOR ATTACH POINT. MX PERFORMED TEMPORARY REPAIRS, REPLACED PROPELLERS, FERRIED ACFT BOS FOR PERMENANT REPAIRS.May 22, 2010 · N660CA · Cessna 402C · Nose/Tail Landing GearSDR HYIA764EA52010Control Cable · brokenON FINAL DECENT, CREW REPORTED FLAP MALFUNCTION ( SPLIT FLAPS ). PILOT DECLARED AN EMERGENCY, LANDING WAS UNEVENTFUL. MX FOUND (1) OF (2) FLAP EXTEND CABLES BROKEN. MX R & R BOTH EXTEND AND RETRACT CABLES.May 20, 2010 · N764EA · Cessna 402C · Trailing Edge Flap Control SystemSDR HYIA20100512001Unknown · odorCREW REPORTED, ON CLIMB OUT, CABIN BECAME FILLED WITH SULFURIC / ELECTRICAL BURNING ODOR. CREW ELECTED TO REMAIN IN PATTERN AND RETURNED TO BASE, LANDING WITHOUT INCIDENT. PILOT REPORTED THAT ODOR MAY HAVE EMINATED FROM REAR OF ACFT. MX INSPECTED ACFT. COULD May 12, 2010 · N618CA · Cessna 402C · Air Distribution SystemSDR C0Q2010F00000Downlock Switch · failedAIRFRAME: UPON LANDING, THE RT MLG COLLAPSED WITH ALL 3 GREEN LIGHTS ON. DOWNLOCK SWITCH FAILED.Apr 29, 2010 · N2614L · Cessna 402C · Landing Gear Position and Warning
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