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 HYIA201205170001Spar · damagedDURING A SCHEDULED MX EVENT, IT WAS NOTED THAT THE RT SPAR STRAP HAD PREVIOUSLY SUSTAINED DAMAGE. UPON NOTING THIS DISCREPANCY, A WO WAS SUBMITTED TO MRO FOR REMOVAL AND REPLACEMENT OF THE RT SPAR STRAP. THE ACFT IS GROUNDED AWAITING THE REQUIRED REPAIRS.May 16, 2012 · N120PC · Cessna 402C · Wing SparSDR HYIA20120516001Spar · crackedON SCHEDULED INSPECTION, DISCOVERED AFT SPAR WEB FLANGE CRACKED UNDER CENTER FLOORBOARDS AT FS 186.15. OPENMay 16, 2012 · N67786 · Cessna 402C · Fuselage Main, FrameSDR HYIA5112FUELODORB-Nut · loosePILOT REPORTED A FUEL ODOR IN THE COCKPIT. ODOR WAS FOUND TO BE CAUSED BY A LEAKING B-NUT ON THE HEATER FUEL PUMP. B-NUT WAS THEN SECURED, AND THE AREA WAS CHECKED WITH NO LEAKS.May 11, 2012 · N514NC · Cessna 402C · Heating SystemSDR HYIA2012F00084O-Ring · leakingPILOT REPORTED A FUEL ODOR IN CABIN. ON INSPECTION, FOUND RT SIDE FUEL FILTER BOWL WAS LEAKING. FURTHER EXAMINATION SHOWED THIS TO BE CAUSED BY A BROKEN O-RING WITHIN THE FUEL BOWL. O-RING REPLACED, AND THE UNIT OPERATIONALLY AND LEAK CHECKED GOOD.May 7, 2012 · N2651S · Cessna 402C · Aircraft Fuel Distribution SystemSDR HYIA2012043002Spar Cap · fracturedDURING ROUTINE MX, A FRACTURE WAS FOUND IN 1 OF OUR ACFT LOCATED AT THE, RT WING AFT LOWER SPAR CAP, INBD FLAP WELL, AND ADJACENT TO LWR BELL CRANK SUPPORT AT WING STA 113.69.Apr 30, 2012 · N36911 · Cessna 402C · Wing SparSDR HYIA20140414012Drag 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 & AApr 27, 2012 · N83PB · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414011Drag 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 & AApr 20, 2012 · N810BW · Cessna 402C · Landing Gear Retraction/Extension SystemSDR 2012FA0000234Propeller · malfunctionedPILOT REPORTED THAT THE RT PROPELLER WENT TO FEATHER UNCOMMANDED ON TAKEOFF ROLL. UPON ARRIVAL BY MX, THE ENGINE WAS INSPECTED WITH NO DEFECTS NOTED. AS A PRECAUTION, R & R RIGHT PROP GOVERNOR. GROUND RAN LT AND RT ENGINES WITH ALL PARAMETERS OPERATIONALLY Apr 17, 2012 · N375R · Cessna 402C · Propeller Feathering/ReversingSDR HYIA201203198521Indication Sys · inaccurateDURING CRUISE, LEFT ENGINE STARTED TO LOOSE POWER. PILOT NOTICED LT FUEL FLOW LOWER THAN 70 LBS MIN AND DECREASING. PILOT SWITCHED THE LT AUX FUEL PUMP TO HIGH AND ENGINE RAN NORMAL. AFTER 30 SECONDS, THE FUEL FLOW STARTED TO DECREASE AGAIN. THE ENGINE BECMar 19, 2012 · N120PC · Cessna 402C · Fuel Indicating SystemSDR HYIA2012030251853Switch · failedNOSE GEAR COLLAPSED ON LANDING. NLG ACTUATOR WAS REMOVED AND TESTED IN A CONTROLLED ENVIRONMENT. WHEN THE ACTUATOR WAS COLD SOAKED, THE SWITCH FAILED TO ACTIVATE PROPERLY GIVING A FALSE INDICATION THAT THE GEAR WAS DOWN AND LOCKED. DUE TO THE GEAR FAILURE, Mar 2, 2012 · N2649Z · Cessna 402C · Landing Gear ActuatorSDR HYIA20140414010Drag 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 & AFeb 28, 2012 · N5826C · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA2012021339811Switch · arcedHEATER FAILED IN FLIGHT. ACFT DIVERTED, DUE TO ODOR OF ELECTRICAL BURNING AND SMALL AMOUNT OF SMOKE IN THE COCKPIT AREA. MX FOUND THE CYCLING SWITCH POINTS ON THE HEATER WERE ARCHING. R & R THE HEATER AND CYCLING POINTS TO CLEAR DISCREPANCY.Feb 13, 2012 · N2611X · Cessna 402C · Heating SystemSDR HYIA20140415076Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWJan 19, 2012 · N402VN · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414009Drag 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 & AJan 16, 2012 · N747WS · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415075Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWDec 8, 2011 · N2714M · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415074Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWNov 17, 2011 · N6875D · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415073Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWOct 10, 2011 · N2714B · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20111003001Trim System · misriggedPILOT WHO WAS ACTING AS INSTRUCTOR FOR THIS TRAINING FLIGHT REPORTED THAT WHILE LEVELING OFF, THE FO NOTED THAT THE ELEVATOR TRIM SEEMED TO BE WORKING BACKWARDS. WHEN THE FO TRIMMED FOR NOSE DOWN, THE NOSE PITCHED UP. THE CAPTAIN TOOK THE CONTROLS AND VERIFIEDOct 3, 2011 · N88833 · Cessna 402C · Elevator Tab Control SystemSDR HYIA20140415072Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWSep 21, 2011 · N258PB · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA3249MSMOKEDimmer · failedPILOT REPORTED THAT DURING NIGHT TRAINING FLIGHT, THE ODOR OF SMOKE WAS NOTED IN THE CABIN. NOTED SMOKE COMING FROM OVERHEAD LIGHTS. PILOT PERFORMED "CABIN ELECTRICAL FIRE OR SMOKE" MEMORY ITEMS, CONTACTED ATC, AND LANDED WITHOUT INCIDENT. UPON INSPECTION, THSep 21, 2011 · N3249M · Cessna 402C · Passenger Compartment LightingSDR HYIA20110902001Relay · failedPILOT REPORTED THAT WHILE TAXIING OUT TO RUNWAY 8, NOTICED A FAINT SMELL IN THE CABIN. THEY INITIALLY THOUGHT IT WAS COMING FROM OUTSIDE THE ACFT. THEY THEN REALIZED THE SMELL WAS FROM INSIDE THE CABIN WHEN THEY NOTICED SMOKE COMING FROM BEHIND A PANEL TO THESep 2, 2011 · N26514 · Cessna 402C · AC Power Distribution SystemSDR HYIA402VNSMOKEDimmer · failedTHE PILOT REPORTED THAT ON APPROACH, THEY TURNED ON THE INSTRUMENT PANEL LIGHTS. SHORTLY AFTER TURNING THE PANEL LIGHTS ON, THEY SMELLED AN ELECTRICAL BURNING SMELL AND NOTICED A SMALL AMOUNT OF SMOKE COMING OUT OF THE RT RHEOSTAT. THEY IMMEDIATELY TURNED THE Aug 25, 2011 · N402VN · Cessna 402C · Instrument PanelSDR GNB2011F00001Web · crackedCRACKS FOUND FOR/AFT AREA PREVIOUSLY ADDRESSED IN MEB 84-12. REPAIR CONDUCTED IAW 8110-3 FAA APPROVED DATA, REF 135415A(14).Aug 24, 2011 · N57PB · Cessna 402C · Aircraft StructuresSDR HYIA1361GHSIHsi · failedPPILOT REPORTED THAT DURING CLIMB OUT AT ABOUT 500 FEET, HSI FAILED AND FROZE ON THE RUNWAY HEADING. PILOT DECLARED AN EMERGENCY AND RETURNED TO LAND. MX R & R HSI.Aug 15, 2011 · N1361G · Cessna 402C · Navigation SystemSDR HYIA20140415071Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWAug 12, 2011 · N26632 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415070Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWAug 11, 2011 · N747WS · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414008Drag 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 & AAug 11, 2011 · N4652N · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414007Drag 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 & AAug 11, 2011 · N6813J · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140414006Drag 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 & AAug 11, 2011 · N494BC · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415069Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWJul 29, 2011 · N68391 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415068Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE 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 OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OUTLJul 29, 2011 · N68391 · Cessna 402C · Main Landing GearSDR HYIA201404150068Drag Brace · crackedDURING SCHEDULED INSPECTION, NLG DRAG BRACE WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT DURING A DYE PENETRANT INSPECTION. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OUTLINEJul 19, 2011 · N812AN · Cessna 402C · Main Landing GearSDR HYIA7037ERTXLAxle · crackedPILOT REPORTED, ON COMPLETION OF FLIGHT 1033, WHILE PARKING AIRCRAFT, RIGHT MAIN GEAR LOCKED UP. MAINTENANCE INSPECTED AIRCRAFT, FOUND RIGHT MAIN LANDING GEAR AXLE CRACKED. MAINTENANCE REMOVED AND REPLACED LOWER BARREL AND AXLE ASSEMBLY. AIRCRAFT RELEASED BJul 15, 2011 · N7037E · Cessna 402C · Main Landing Gear Strut/Axle/TruckSDR HYIA20140415067Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWJul 14, 2011 · N618CA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR 2011FA0000459Cylinder · crackedDISCOVERED 3 CRACKED CYLINDERS, PN AEC631397 (F),S/N 54389-23,54589-12,54678-09. CRACKS IN CYLINDERS ARE LOCATED AT THE 17TH FIN ABOUT 3 INCHES UP FROM THE UPPER SURFACE ON THE INTAKE PORT FLANGE. ONE OF THE SIGNS OF THESE CRACKS IS A FUEL STAIN ON THE INTAKJul 14, 2011 · N402S · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20140415066Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWJul 13, 2011 · N120PC · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA02Nut · crackedRIGHT ENGINE NR 1 CYLINDER NUMBER ONE HOLD DOWN NUT CRACK.Jul 11, 2011 · N812AN · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20140415065Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWJul 8, 2011 · N6813J · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIANut · crackedRIGHT ENGINE NR 3 CYLINDER HAS ONE CRACKED HOLD DOWN NUT.Jun 24, 2011 · N69SC · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA01Nut · crackedTHE NR 3 CYLINDER OF THE RIGHT ENGINE HAD A CRACKED HOLD DOWN NUT.Jun 23, 2011 · N494BC · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA991AANOSEUplock Switch · failedCREW REPORTED DURING CRUISE FLIGHT, GEAR UNLOCK LIGHT ILLUMINATED. GEAR WAS CYCLED ONCE WITH SAME INDICATION. GEAR WAS SELCTED DOWN, THREE GREEN DOWN AND LOCK LIGHTS ILLUMINATED BUT GEAR UNLOCK LIGHT REMAINED ILLUMINATED. AIRCRFT RETURNED TO KBOS WHERE MAINJun 23, 2011 · N991AA · Cessna 402C · Landing Gear Position and WarningSDR HYIA20140415064Drag 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 WITHIN ALLOWABLE LIMIT OF MEB91-11R1. THIS UNIT HAS BEEN REPAIRED IAWJun 20, 2011 · N991AA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415063Drag 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 Jun 9, 2011 · N68752 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415062Drag 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 Jun 6, 2011 · N67886 · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415061Drag 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 May 31, 2011 · N781EA · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415060Drag 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 May 27, 2011 · N409BK · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415059Drag 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 PROCEDUREMay 27, 2011 · N2649Z · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415058Drag 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 PROCEDUREMay 16, 2011 · N3292M · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415057Drag 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 PROCEDUREMay 16, 2011 · N160PB · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20140415056Drag 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 PROCEDUREMay 16, 2011 · N769EA · Cessna 402C · Landing Gear Retraction/Extension System
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