N1361G, cancelled May 22, 2020

Service difficulty reports · 22

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N1361G' AND deregistration_id = 'N1361G-2020-05-22'
  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 HYIA20190123001Spar Cap · crackedDURING MAINTENANCE A CRACK WAS VISUALLY DISCOVERED ON THE RIGHT HAND FORWARD UPPER SPAR CAP P/N: 5122031-6. THIS CRACK HAS BEEN CONFIRMED BY SURFACE EDDY CURRENT INSPECTION AND IS LOCATED IN THE FORWARD RADIUS BETWEEN THE VERTICAL AND HORIZONTAL LEGS OF THE CAJan 23, 2019 · N1361G · Cessna 402C · Wing SparSDR HYIA20180605001Spar Cap · corrodedCORROSION WAS DISCOVERED ON THE LT AFT LOWER OUTBOARD SPAR CAP WS 221.71 ON THE FORWARD SIDE OF THE CAP, INSIDE THE FUEL TANK, NEAR THE RADIUS. THE CORRODED AREA MEASURED .075 TALL, .243 IN WIDTH, AND .063 IN DEPTH. OUT OF LIMITS IAW MEB 95-11, R1, SECTION 3Jun 1, 2018 · N1361G · Cessna 402C · Wing SparSDR HYIA20171109001Fitting · corrodedDURING A ROUTINE VISUAL INSPECTION OF THE WING ATTACH FITTINGS, CORROSION WAS DISCOVERED ON THE LEFT OUTBOARD FORWARD, AFT SIDE WING ATTACH FITTING. THE FITTING WAS REMOVED AND REPLACED WITH FACTORY NEW PARTS.Nov 2, 2017 · N1361G · Cessna 402C · Wing, Attach FittingsSDR HYIA20161109208Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Nov 7, 2016 · N1361G · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA20160803027Exhaust Valve · damagedCYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.Jul 4, 2016 · N1361G · Cessna 402C · Reciprocating Engine Cylinder SectionSDR HYIA03252015002Beam · crackedTHE LT NACELLE OTBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY FROM NACELLE, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDIMar 21, 2015 · N1361G · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA03252015001Beam · crackedTHE LT NACELLE INBD ENG BEAM WAS FOUND TO BE CRACKED JUST FWD OF AFT ENG MOUNT, TRANSVERSE TO LENGTH OF BEAM, ACROSS UPPER FACE OF BEAM, DURING NDT PRESCRIBED WITHIN MEL-54-01. REMOVE BEAM ASSEMBLY FROM NACELLE, PERFORM DETAILED VISUAL INSPECTION OF SURROUNDIMar 21, 2015 · N1361G · Cessna 402C · Nacelle/Pylon Miscellaneous StructureSDR HYIA20141217002Door · unsecureRIGHT SIDE EMER DOOR OPENED AT 1000 FT AFTER DEPARTURE. INSPECTED THE EMER EXIT DOOR SYS, SECURED THE EMER EXIT DOOR, SEALED & SEATED PROPERLY IN THE DOOR FRAME. NO FURTHER DEFECTS FOUND.Dec 16, 2014 · N1361G · Cessna 402C · Emergency ExitsSDR 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 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 HYIA20140414040Drag 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 & ADec 19, 2012 · N1361G · Cessna 402C · Landing Gear Retraction/Extension SystemSDR HYIA20121203002Beam · crackedDURING A SCHEDULED MX EVENT, THE RT ENGINE ASSY WAS REMOVED FOR A SCHEDULED TIME CHANGE. UPON REMOVAL, A CRACK WAS DISCOVERED AT THE RT NACELLE CROSSOVER BEAM IN THE AREA OF TURBOCHARGER BRACKET HOLE LOCATIONS. LOCATION OF CRACK RELATIVE TO RT NACELLE CROSSOVDec 1, 2012 · N1361G · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20121126003Beam · corrodedSEVERE CORROSION WAS DISCOVERED BETWEEN RT NACELLE OTBD ENGINE BEAM AND LOWER NACELLE SKIN. RIGHT NACELLE OTBD BEAM HAT CHANNEL WHICH IS SANDWICHED BETWEEN BEAM AND LOWER NACELLE SKIN, IS SEVERELY CORRODED. REMOVED RT NACELLE OTBD ENGINE BEAM , PERFORMED DETNov 24, 2012 · N1361G · Cessna 402C · Nacelle/Pylon, Main FrameSDR HYIA20120910001Spar · damagedDURING A REGULARLY SCHEDULED MX, DAMAGE WAS DISCOVERED TO THE AFT CARRY THROUGH SPAR, CENTER SECTION UPPER CAP AND CORRESPONDING WEB FLANGES. THIS DAMAGED APPEARED TO BE CAUSED BY PREVIOUS REPAIR ATTEMPTS INCLUDING MISDRILLS TO SPAR CAP AND CRACKS IN WEB FLANSep 10, 2012 · N1361G · Cessna 402C · Fuselage Main, StructureSDR HYIA20120708002Hsi · inoperativeSHORTLY AFTER TAKEOFF, THE PILOT REPORTED THAT THEIR HSI WAS INOPERATIVE WHICH WAS ACCOMPANIED BY A SMOKE ODOR IN THE COCKPIT AND ELECTED TO RETURN FOR A LANDING. UPON INSPECTION AND CONFIRMATION BY MX, THE HSI WAS SUBSEQUENTLY REPLACED AND THE ACFT WAS RELEAJul 8, 2012 · N1361G · Cessna 402C · Directional Gyro and Indicating SystemSDR 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 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 HYIA1361G AVMSTRMaster Switch · unserviceablePREFLIGHT, CREW REPORTED AVIONICS MASTER SWITCH INOPERATIVE. MX R & R CIRCUIT BREAKER SWITCH. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE.Jan 7, 2010 · N1361G · Cessna 402C · DC Power Distribution SystemSDR HYIA1361GMaster Switch · failedCREW REPORTED BURNING ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED AVIONICS MASTER SWITCH.Mar 24, 2009 · N1361G · Cessna 402C · AC Power Distribution SystemSDR 1350603N1361GCircuit Breaker · defectiveCREW REPORTED AVIONICS MASTER INOP. MX CHANGED CIRCUIT BREAKER SWITCH.Aug 8, 2006 · N1361G · Cessna 402C · Electrical Power SystemSDR 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 20001012SH030Tube · rustedREMOVED RIGHT ELEVATOR FROM AIRCRAFT TO REPLACE HINGE BEARINGS. CLEANED INSIDE TUBE AND NOTICED 3 RUSTED HOLES THROUGH TUBE. REPLACED TUBE WITH NEW AND LUBED INSIDE TUBE. (X)Sep 4, 2000 · N1361G · Cessna 402C · Elevator Control System
Back to N1361G, cancelled May 22, 2020