# N1361G: 1980 Cessna 402C, registration cancelled 2020-05-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 22, 2020 - Status when cancelled: Valid registration - Airframe: [Cessna 402C](https://openairdocs.org/model/cessna-402c) (registry code 207590R) - Engine: [Continental TSIO-520 series](https://openairdocs.org/engine/continental-tsio-520-series) (registry code 17040) - Data sheets: [TCDS A7CE](https://openairdocs.org/tcds/A7CE), [TCDS E8CE](https://openairdocs.org/tcds/E8CE) (OpenAirDocs) - Serial number: 402C0270 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: March 12, 1980 - Certificate issued: January 5, 1996 - Last registry action: April 12, 2019 - Mode S code: A093FD - Owner when cancelled: [Hyannis Air Service Inc](https://openairdocs.org/faa-owner/HYANNIS%20AIR%20SERVICE%20INC) - Location: [Hyannis, MA](https://openairdocs.org/faa-place/MA/Hyannis) - Owner type: Corporation - Owner's area on the map: 41.6612° N, 70.2932° W: Placed by OpenAirDocs at the center of ZIP code 02601, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N1361G - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1361G - Page: https://openairdocs.org/deregistered/N1361G-2020-05-22 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Cessna 402C: https://openairdocs.org/model/cessna-402c.md ## Service difficulty reports (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HYIA20190123001](https://openairdocs.org/sdr/HYIA20190123001), Jan 23, 2019: SPAR CAP. CRACKED. DURING 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 CURREN - [SDR HYIA20180605001](https://openairdocs.org/sdr/HYIA20180605001), Jun 1, 2018: SPAR CAP. CORRODED. CORROSION 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 ARE - [SDR HYIA20171109001](https://openairdocs.org/sdr/HYIA20171109001), Nov 2, 2017: FITTING. CORRODED. DURING A ROUTINE VISUAL INSPECTION OF THE WING ATTACH FITTINGS, CORROSION WAS DISCOVERED ON THE LEFT OUTBOARD FORWARD, AFT SIDE WING ATTACH FITTING. THE FITTING - [SDR HYIA20161109208](https://openairdocs.org/sdr/HYIA20161109208), Nov 7, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160803027](https://openairdocs.org/sdr/HYIA20160803027), Jul 4, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA03252015002](https://openairdocs.org/sdr/HYIA03252015002), Mar 21, 2015: BEAM. CRACKED. THE 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 W - [SDR HYIA03252015001](https://openairdocs.org/sdr/HYIA03252015001), Mar 21, 2015: BEAM. CRACKED. THE 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 W - [SDR HYIA20141217002](https://openairdocs.org/sdr/HYIA20141217002), Dec 16, 2014: DOOR. UNSECURE. RIGHT 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 - [SDR HYIA20130621001](https://openairdocs.org/sdr/HYIA20130621001), Jun 17, 2013: BEAM. CRACKED. DURING ROUTINE INSPECTION, DAMAGE WAS NOTED AT LT NACELLE CROSSOVER BEAM INCLUDING A CRACK EXTENDING FROM OTBD EXHAUST HANGAR BRACKET HOLE LOCATIONS. - [SDR HYIA20130611104](https://openairdocs.org/sdr/HYIA20130611104), May 27, 2013: BOLT. FAILED. CREW 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 RETUR - [SDR HYIA20140414040](https://openairdocs.org/sdr/HYIA20140414040), Dec 19, 2012: DRAG BRACE. CRACKED. AT 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. - [SDR HYIA20121203002](https://openairdocs.org/sdr/HYIA20121203002), Dec 1, 2012: BEAM. CRACKED. DURING 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 I - [SDR HYIA20121126003](https://openairdocs.org/sdr/HYIA20121126003), Nov 24, 2012: BEAM. CORRODED. SEVERE CORROSION WAS DISCOVERED BETWEEN RT NACELLE OTBD ENGINE BEAM AND LOWER NACELLE SKIN. RIGHT NACELLE OTBD BEAM HAT CHANNEL WHICH IS SANDWICHED BETWEEN BEAM - [SDR HYIA20120910001](https://openairdocs.org/sdr/HYIA20120910001), Sep 10, 2012: SPAR. DAMAGED. DURING A REGULARLY SCHEDULED MX, DAMAGE WAS DISCOVERED TO THE AFT CARRY THROUGH SPAR, CENTER SECTION UPPER CAP AND CORRESPONDING WEB FLANGES. THIS DAMAGED APPEA - [SDR HYIA20120708002](https://openairdocs.org/sdr/HYIA20120708002), Jul 8, 2012: HSI. INOPERATIVE. SHORTLY 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 LANDIN - [SDR HYIA1361GHSI](https://openairdocs.org/sdr/HYIA1361GHSI), Aug 15, 2011: HSI. FAILED. PPILOT 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 - [SDR HYIA20140415006](https://openairdocs.org/sdr/HYIA20140415006), Jan 21, 2011: DRAG BRACE. CRACKED. AT 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 PENETRAN - [SDR HYIA1361G AVMSTR](https://openairdocs.org/sdr/HYIA1361G%20AVMSTR), Jan 7, 2010: MASTER SWITCH. UNSERVICEABLE. PREFLIGHT, CREW REPORTED AVIONICS MASTER SWITCH INOPERATIVE. MX R & R CIRCUIT BREAKER SWITCH. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE. - [SDR HYIA1361G](https://openairdocs.org/sdr/HYIA1361G), Mar 24, 2009: MASTER SWITCH. FAILED. CREW REPORTED BURNING ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED AVIONICS MASTER SWITCH. - [SDR 1350603N1361G](https://openairdocs.org/sdr/1350603N1361G), Aug 8, 2006: CIRCUIT BREAKER. DEFECTIVE. CREW REPORTED AVIONICS MASTER INOP. MX CHANGED CIRCUIT BREAKER SWITCH. - [SDR 13504421361G](https://openairdocs.org/sdr/13504421361G), Mar 23, 2006: CIRCUIT BREAKER. DEFECTIVE. CREW REPORTED AVIONICS MASTER SWITCH INOP, MX CHANGED CIRCUIT BREAKER SWITCH MFG DATE CODE 0442. - [SDR 20001012SH030](https://openairdocs.org/sdr/20001012SH030), Sep 4, 2000: TUBE. RUSTED. REMOVED RIGHT ELEVATOR FROM AIRCRAFT TO REPLACE HINGE BEARINGS. CLEANED INSIDE TUBE AND NOTICED 3 RUSTED HOLES THROUGH TUBE. REPLACED TUBE WITH NEW AND LUBED IN ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20090218001389I](https://openairdocs.org/incident/20090218001389I), Feb 18, 2009: Cessna 402C (N1361G), Vieques, Puerto Rico, Minor damage. (-23) During landing at tjvq the left propeller contacted the runway approximately 1,200 to 1,300 feet down runway 09 causing 28 strike marks extending… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.