# N1376G: 1980 Cessna 402C, registration cancelled 2020-05-29 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 29, 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: 402C0271 - Year built: 1980 - Type of aircraft: Fixed wing multi engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: March 14, 1980 - Certificate issued: October 24, 2018 - Last registry action: October 24, 2018 - Mode S code: A09863 - Owners when cancelled: [Hyannis Air Service Inc](https://openairdocs.org/faa-owner/HYANNIS%20AIR%20SERVICE%20INC), [Cape Air](https://openairdocs.org/faa-owner/CAPE%20AIR) - 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/N1376G - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1376G - Page: https://openairdocs.org/deregistered/N1376G-2020-05-29 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 (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HYIA20191114001](https://openairdocs.org/sdr/HYIA20191114001), Nov 14, 2019: FITTING. CORRODED. DURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE TOP FACE OF THE LOWER LEG OF THE FORWARD LEFT HAND LOWER AFT WING FITTING (P/N: 0822550-4 - [SDR HYIA20191106002](https://openairdocs.org/sdr/HYIA20191106002), Nov 6, 2019: SPAR CAP. CORRODED. DURING MAINTENANCE AN AREA OF CORROSION WAS IDENTIFIED ON THE RIGHT HAND LOWER AFT OUTBOARD SPAR CAP P/N: 5122041-24. THIS CORROSION IS LOCATED BETWEEN RIGHT WI - [SDR HYIA20190925003](https://openairdocs.org/sdr/HYIA20190925003), Sep 25, 2019: RIB. CRACKED. DURING MAINTENANCE TWO CRACKS WERE DISCOVERED ON THE RIGHT HAND CLOSEOUT RIB (P/N: 5122115-56) AT RWS 106.79. THESE CRACKS ORIGINATE FROM A COMMON HOLE IN THE F - [SDR HYIA20190925002](https://openairdocs.org/sdr/HYIA20190925002), Sep 25, 2019: RIB. CRACKED. DURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB (P/N: 5122115-55) AT LWS 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF - [SDR HYIA20171201001](https://openairdocs.org/sdr/HYIA20171201001), Nov 29, 2017: SOCKET. DETERIORATED. DURING DESCENT FOR LANDING AT SCHEDULED DESTINATION, THE LWR PANEL LIGHT RHEOSTAT WAS ACTUATED. AFTER 2-3 SECONDS A STRONG ELECTRICAL ODOR WAS NOTED. THE PANEL - [SDR HYIA20170828007](https://openairdocs.org/sdr/HYIA20170828007), Jan 9, 2017: FITTING. CRACKED. DURING A ROUTINE INSPECTION, THREE CRACKS WERE FOUND ON THE RT OUTBOARD NACELLE FITTING. TWO OF THE CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST F - [SDR HYIA20161109196](https://openairdocs.org/sdr/HYIA20161109196), Nov 2, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161108182](https://openairdocs.org/sdr/HYIA20161108182), Oct 19, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160304001](https://openairdocs.org/sdr/HYIA20160304001), Mar 2, 2016: UNKNOWN. ODOR. PILOT REPORTED HEATER SMELL. RAN HEATER FOR 30 MINUTES, COULD NOT DUPLICATE SMELL. INSPECTED HEATER IAW MM CH 21. - [SDR HYIA20141001001](https://openairdocs.org/sdr/HYIA20141001001), Sep 30, 2014: CALIPER. DEFECTIVE. ON PREFLIGHT PILOT REPORTED RT BRAKES INOPERATIVE, NO BRAKES ON THE RT SIDE. R & R THE RT BRAKE CALIPER & BRAKE PADS IAW MM 32-10-00. OPERATIONS CHECKED GOOD. - [SDR HYIA20130727001](https://openairdocs.org/sdr/HYIA20130727001), Jul 25, 2013: LIGHT. FAULTY. INSTRUMENT PANEL LIGHTS EXTINGUISHED AFTER TAKEOFF. F/O INSTRUMENT LIGHT CIRCUIT BREAKER TRIPPED FOLLOWED BY MOMENTARY PUFF OF SMOKE. - [SDR HYIA20130327001](https://openairdocs.org/sdr/HYIA20130327001), Mar 26, 2013: SKIN. CHAFED. DURING A SCHEDULED MX INSPECTION, HORIZONTAL STABILIZER WAS REMOVED WHICH REVEALED DAMAGE TO THE ACFT FUSELAGE SKIN. DAMAGE APPEARS TO HAVE BEEN CAUSED BY THE L - [SDR HYIA20140415038](https://openairdocs.org/sdr/HYIA20140415038), Mar 25, 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 PENETR - [SDR HYIA1376GLBEAM](https://openairdocs.org/sdr/HYIA1376GLBEAM), Nov 18, 2009: BEAM. CRACKED. DURING A ROUTINE SCHEDULED INSP, MX FOUND LT NACELLE INBD ENG CARRIER BEAM CRACKED. REPLACEMENT OF BEAM IN PROGRESS. - [SDR HYIA1376G](https://openairdocs.org/sdr/HYIA1376G), Feb 17, 2009: CIRCUIT BREAKER. FAILED. ON PREFLIGHT INSPECTION, CREW REPORTED AVIONIC MASTER SWITCH INOP. CONTRACT MAINTENANCE REMOVED AND REPLACED SWITCH, SYSTEM CHECKED OK. THIS CIRCUIT BREAKER IS - [SDR 13505361376G](https://openairdocs.org/sdr/13505361376G), May 31, 2006: CIRCUIT BREAKER. DEFECTIVE. CREW REPORTED AVIONICS MASTER SWITCH INOP. MX CHANGED CIRCUIT BREAKER SWITCH. - [SDR HYI2003F00006](https://openairdocs.org/sdr/HYI2003F00006), Jul 8, 2003: MASTER SWITCH. BURNED. UPON CLIMBOUT, PILOT SMELLED SMOKE, FOUND SMOKE COMING FROM AVIONICS MASTER SWITCH. PILOT NOTIFIED TOWER BEFORE SHUTTING DOWN AVIONICS SWITCH, LANDING WITHOUT I - [SDR 99ZZZX3741](https://openairdocs.org/sdr/99ZZZX3741), Sep 6, 1999: BRACKET. BROKEN. ON RT ENGINE START, PILOT NOTICED SMOKE FROM RT COWL, SHUT DOWN ENGINE PER NORMAL PROCEDURE AND EVACUATED PASSENGERS. MAINTENANCE FOUND ALTERNATOR POWER CABLE C - [SDR 99ZZZX1745](https://openairdocs.org/sdr/99ZZZX1745), Mar 31, 1999: CIRCUIT BREAKER. FAILED. AFTER LANDING IN ACK, CREW SHUT OFF ALL EXTERNAL LIGHTS EXCEPT BELLY STROBE AND NAV LIGHTS. NOTICED SMOKE COMING FROM NAV LIGHT SWITCH/BREAKER. SHUT OFF SWITCH, - [SDR 97ZZZX1227](https://openairdocs.org/sdr/97ZZZX1227), Mar 4, 1997: DIODE. BURNT. PILOT REPORTED ARCING AND SMOKE FROM ELECTRIC HEATED WINDSHIELD. ELECTRICAL CONNECTION OR LEFT SIDE OF HEATED WINDSHIELD HAS DIODE THAT MELTED AND ARCED. - [SDR 97ZZZX1046](https://openairdocs.org/sdr/97ZZZX1046), May 8, 1996: MOUNT BEAM. CRACKED. ESTIMATED CYCLES = 28,000. ESTIMATED ENGINE CHANGES = 70. LEFT ENGINE OUTBOARD BEAM FOUND CRACKED AT FORWARD MOUNT LOCATION BETWEEN NUTPLATE HOLES. ## 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 20181226022359I](https://openairdocs.org/incident/20181226022359I), Dec 26, 2018: Cessna 402C (N1376G), Provincetown, MA, Minor damage. On landing roll out the aircraft struck a deer with the nose wheel. The deer pass under the left side fuselage missing the propeller. --- 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.