# N762EA: Cessna 402C, registration cancelled 2023-12-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 11, 2023 - Status when cancelled: Valid registration - Airframe: [Cessna 402C](https://openairdocs.org/model/cessna-402c) (registry code 207590R) - Data sheets: [TCDS A7CE](https://openairdocs.org/tcds/A7CE) (OpenAirDocs) - Serial number: 402C0061 - Type of aircraft: Fixed wing multi engine - Airworthiness: Standard, normal - Airworthiness date: March 29, 1979 - Certificate issued: January 29, 1999 - Last registry action: August 11, 2023 - Mode S code: AA495B - 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/N762EA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=762EA - Page: https://openairdocs.org/deregistered/N762EA-2023-12-11 From the FAA registry file of November 7, 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 (16) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HYIA20160913145](https://openairdocs.org/sdr/HYIA20160913145), Sep 14, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160913144](https://openairdocs.org/sdr/HYIA20160913144), Sep 14, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160825097](https://openairdocs.org/sdr/HYIA20160825097), Aug 24, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160803050](https://openairdocs.org/sdr/HYIA20160803050), Jul 17, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION, EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160803049](https://openairdocs.org/sdr/HYIA20160803049), Jul 17, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA201410114001](https://openairdocs.org/sdr/HYIA201410114001), Nov 13, 2014: ACTUATOR. FAILED. ELEVATOR TRIM JAMMED, CREW COMPLETED FLIGHT & LANDED WITHOUT INCIDENT. R & R THE ELEVATOR TRIM TAB ACTUATOR IAW 402C MM CH 27-30-02. OPERATIONS CHECKED GOOD. - [SDR HYIA20140424112](https://openairdocs.org/sdr/HYIA20140424112), Apr 23, 2014: PUMP. LEAKING. PILOT REPORTED FUEL SMELL IN COCKPIT DURING FLIGHT. AFTER LANDING, A WALK AROUND INSPECTION REVEALED THE ODOR WAS COMING FROM THE NOSE AREA WITH VISIBLE LEAKAGE - [SDR HYIA20130118001](https://openairdocs.org/sdr/HYIA20130118001), Jan 16, 2013: TURBOCHARGER. FAILED. PILOT REPORTED A GRADUAL POWER LOSS, ACCOMPANIED BY PARTIAL ENGINE STUTTER DURING FLIGHT IN THE RT ENGINE. THE PILOT LANDED SAFELY AT PLANNED DESTINATION AIRPOR - [SDR HYIA20121225001](https://openairdocs.org/sdr/HYIA20121225001), Dec 22, 2012: CALIPER. INOPERATIVE. PILOT REPORTED THAT DURING LANDING ROLLOUT, THE ACFT PULLED TO THE LT WHEN THE BRAKES WERE APPLIED. AFTER RELEASING BRAKE PRESSURE, THE RT BRAKE WAS APPLIED BY - [SDR HYIA20121203001](https://openairdocs.org/sdr/HYIA20121203001), Nov 30, 2012: CONTROL CABLE. SEPARATED. PILOT REPORTED THAT DURING THE CLIMB, THE LT PROPELLER RPM RATE BECAME UNCONTROLLABLE. THE PILOT ELECTED TO RETURN TO THE DEPARTURE AIRPORT AND LANDED SAFELY. U - [SDR HYIA20140414001](https://openairdocs.org/sdr/HYIA20140414001), Feb 7, 2011: 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 135762010708](https://openairdocs.org/sdr/135762010708), Jan 2, 2008: ACTUATOR. FAILED. NOSE GEAR DOWN AND LOCKED INDICATOR LIGHT WAS ILLUMINATED WITH GEAR UNSAFE AND HYDRAULIC PRESSURE LIGHTS OUT. PILOT PERFORMED CHECK LIST, BLEW GEAR DOWN, AND LA - [SDR 135762112207](https://openairdocs.org/sdr/135762112207), Nov 22, 2007: SWITCH. FAILED. HEATER INOPERATIVE, SMOKE CAME FROM SWITCH. MAINTENANCE INSPECTED AND FOUND THE HEATER SWITCH TO BE BAD. MAINTENANCE REMOVED AND REPLACED SWITCH, OPERATIONALLY - [SDR 97ZZZX553](https://openairdocs.org/sdr/97ZZZX553), Jan 18, 1997: GUSSET. CRACKED. INSP OF THE PILOT SEAT SUPPORT STRUCTURE FOUND P/N 5011011-7 GUSSETT, P/N 5015019-1, AND 5015019-3 CHANNELS HAD CRACKED AND FAILED. THERE IS NO ACCESS TO P/N 50 - [SDR 97ZZZX552](https://openairdocs.org/sdr/97ZZZX552), Jan 18, 1997: CHANNEL. CRACKED. INSP OF THE PILOT SEAT SUPPORT STRUCTURE FOUND P/N 5011011-7 GUSSETT, P/N 5015019-1, AND 5015019-3 CHANNELS HAD CRACKED AND FAILED. THERE IS NO ACCESS TO P/N 50 - [SDR 97ZZZX551](https://openairdocs.org/sdr/97ZZZX551), Jan 18, 1997: CHANNEL. CRACKED. INSP OF THE PILOT SEAT SUPPORT STRUCTURE FOUND P/N 5011011-7 GUSSETT, P/N 5015019-1, AND 5015019-3 CHANNELS HAD CRACKED AND FAILED. THERE IS NO ACCESS TO P/N 50 --- 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.