# N2714M: 1979 Cessna 402C, registration cancelled 2023-05-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 27, 2023 - 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: 402C0211 - Year built: 1979 - Type of aircraft: Fixed wing multi engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: October 29, 1979 - Certificate issued: June 22, 1998 - Last registry action: March 4, 2023 - Mode S code: A2AD23 - 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/N2714M - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=2714M - Page: https://openairdocs.org/deregistered/N2714M-2023-05-27 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 (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HYIA20171027001](https://openairdocs.org/sdr/HYIA20171027001), Oct 23, 2017: RESISTOR. BURNED. DURING APPROACH, THE CAPTAINS OVERHEAD LIGHT SWITCH WAS ACTUATED AND THE LIGHT DID NOT ILLUMINATED. THE CREW SUBSEQUENTLY ACTUATED THE COPILOT'S OVERHEAD LIGHT - [SDR HYIA20170828006](https://openairdocs.org/sdr/HYIA20170828006), Mar 3, 2017: FITTING. CRACKED. DURING A ROUTINE INSPECTION, TWO CRACKS WERE FOUND IN THE RT OUTBOARD NACELLE FITTING. THERE WAS ONE CRACK IN THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF T - [SDR HYIA20170828005](https://openairdocs.org/sdr/HYIA20170828005), Mar 3, 2017: FITTING. CRACKED. DURING A ROUTINE INSPECTION, A CRACK WAS FOUND ON THE LT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE S - [SDR HYIA20161010167](https://openairdocs.org/sdr/HYIA20161010167), Sep 29, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161010166](https://openairdocs.org/sdr/HYIA20161010166), Sep 29, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161010165](https://openairdocs.org/sdr/HYIA20161010165), Sep 29, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161010164](https://openairdocs.org/sdr/HYIA20161010164), Sep 29, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161010163](https://openairdocs.org/sdr/HYIA20161010163), Sep 29, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160818082](https://openairdocs.org/sdr/HYIA20160818082), Aug 17, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160818081](https://openairdocs.org/sdr/HYIA20160818081), Aug 17, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160818080](https://openairdocs.org/sdr/HYIA20160818080), Aug 17, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160803051](https://openairdocs.org/sdr/HYIA20160803051), Jul 20, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20150107001](https://openairdocs.org/sdr/HYIA20150107001), Jan 7, 2015: SPAR CAP. MECHANIC ERROR. UPON DISASSEMBLY OF RT NACELLE LOWER FAIRING FOR INSPECTION OF RT WING SPAR STRAP IAW SID 57-10-16, UNINTENTIONAL DRILL DAMAGE AT WING SPAR STRAP WAS FOUND BY V - [SDR HYIA20140905116](https://openairdocs.org/sdr/HYIA20140905116), Sep 1, 2014: TRANSDUCER. INACCURATE. ON INITIAL CLIMB, THE PILOT REPORTED FUEL FLOW OF 160PPH. AFTER REACHING CRUISING ALTITUDE THE FUEL FLOW WENT TO 0 & THE PILOT REPORTED TEMP POWER LOSS. THE PIL - [SDR HYIA20140414020](https://openairdocs.org/sdr/HYIA20140414020), Sep 11, 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 HYIA201205170005](https://openairdocs.org/sdr/HYIA201205170005), May 16, 2012: SPAR. DAMAGED. DURING A MX EVENT, DAMAGE WAS DISCOVERED ON THE FORWARD CARRY THROUGH SPAR ASSY. DAMAGE INCLUDES FWD LOWER SPAR WEB FLANGE CRACK AND CORRESPONDING VERTICAL STIF - [SDR HYIA20140415075](https://openairdocs.org/sdr/HYIA20140415075), Dec 8, 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 HYIA20140415043](https://openairdocs.org/sdr/HYIA20140415043), Apr 5, 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 HYIA20140415025](https://openairdocs.org/sdr/HYIA20140415025), Feb 8, 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 HYIA2714MAVMSTR](https://openairdocs.org/sdr/HYIA2714MAVMSTR), Jan 3, 2010: CIRCUIT BREAKER. UNSERVICEABLE. CREW REPORTED AVIONICS BUSS FAILURE. MX R & R CIRCUIT BREAKER SWITCH. SYS CHECKS OK. ACFT RELEASED BACK TO SERVICE. - [SDR HYIA2714M](https://openairdocs.org/sdr/HYIA2714M), Feb 7, 2009: UNKNOWN. UNKNOWN. RT ENG SURGING AT CRUISE POWER. RESHAPED LEFT NOSE BOWL DUE TO PROP CABLE ROD END CLEARANCE. - [SDR 1357141120307](https://openairdocs.org/sdr/1357141120307), Dec 3, 2007: TURBOCHARGER. FAILED. PILOT LOG READS THE FOLLOWING: LEFT ENG SMOKES ON APPROACH. MAINTENANCE INSPECTED AND FOUND TURBO TO HAVE FAILED. MAINTENANCE REMOVED AND REPLACED THE TURBO. - [SDR HYI2003F00022](https://openairdocs.org/sdr/HYI2003F00022), Sep 30, 2003: RHEOSTAT. UNSERVICEABLE. AFTER REACHING CRUISE ALTITUDE, CREW NOTICED SMOKE FROM PEDESTAL LIGHTING RHEOSTATS. DAY/NIGHT SWITCH TURNED OFF, CIRCUIT BREAKERS PULLED, SMOKE STOPPED. DIVERT - [SDR HYI2003F00011](https://openairdocs.org/sdr/HYI2003F00011), Sep 3, 2003: COMPUTER. FAILED. 5 MINUTES INTO CLIMB, CREW REPORTED SMOKE FROM AVIONICS RACK, RETURNED W/O INCIDENT. MECHANIC FOUND A/P PITCH SERVO HARNESS SHORTED, CAUSING A/P COMPUTER TO FAI - [SDR HYI2003F00014](https://openairdocs.org/sdr/HYI2003F00014), Aug 29, 2003: LINE. LOOSE. ON CLIMB OUT, AFTER FIRST POWER REDUCTION, RIGHT ENGINE COST POWER, ATTEMPTED AUX FUEL PUMP, CROSSFEED, NO HELP. SECURED ENGINE AND FEATHERED PROP. RETURNED W/O - [SDR HYI2003F00015](https://openairdocs.org/sdr/HYI2003F00015), Aug 27, 2003: PUMP. FAILED. ON CLIMB OUT, TOWER REPORTED SMOKE FROM LT ENGINE, CREW REPORTED LOSS OF POWER AFTER AUX BOOST PUMP WAS TURNED ON, ENGINE SHUT DOWN, RETURNED W/O INCIDENT. MECH ## FAA accident and incident reports (4) 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 20171023020259I](https://openairdocs.org/incident/20171023020259I), Oct 23, 2017: Cessna 402C (N2714M), Bedford, MA, Minor damage. Aircraft was on final approach to kbos to runway 04R, pilot turned on overhead light to view landing chart. Shortly after he noticed dust particles in the air… - [Incident 19900622062349I](https://openairdocs.org/incident/19900622062349I), Jun 22, 1990: Cessna 402C (N2714M), Friday Harbor, WA, Minor damage. Landed downwind. Departed off side of runway. Pilot advised he was landing wrong way. - [Incident 19821117065449I](https://openairdocs.org/incident/19821117065449I), Nov 17, 1982: Cessna 402C (N2714M), Sacramento, CA. Left engine shut down when pilot returned to gate. Excessive fuel started fire in induction system on restart. - [Incident 19811111086029I](https://openairdocs.org/incident/19811111086029I), Nov 11, 1981: Cessna 402C (N2714M), Ruth, CA, Substantial damage. Lightning strike a FL120. Bright flash, loud boom, dimmed lights. On landing found aircraft had extensive damage. ## Other aircraft with N2714M - [Cancelled 1971-07-14](https://openairdocs.org/deregistered/N2714M-1971-07-14): Piper PA-12, S/N 12-1129. Owner: [Zurcher Donald E](https://openairdocs.org/faa-owner/ZURCHER%20DONALD%20E), [Bullhead City, AZ](https://openairdocs.org/faa-place/AZ/Bullhead%20City) --- 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.