# N4652N: 1978 Cessna 402C, registration cancelled 2021-04-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 17, 2021 - 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: 402C0011 - Year built: 1978 - Type of aircraft: Fixed wing multi engine - Engine type: Reciprocating - Airworthiness: Standard, normal - Airworthiness date: November 28, 1978 - Certificate issued: April 14, 1998 - Last registry action: August 15, 2019 - Mode S code: A5AED9 - 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/N4652N - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=4652N - Page: https://openairdocs.org/deregistered/N4652N-2021-04-17 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 HYIA20171226001](https://openairdocs.org/sdr/HYIA20171226001), Dec 22, 2017: CYLINDER. FAILED. PILOT REPORTED RIGHT ENGINE RUNNING ROUGH. UPON INSPECTION FOUND THE RIGHT ENGINE NR 3 CYLINDER TO HAVE LOW COMPRESSION AND THE CYLINDER EXHAUST VALVE TO HAVE E - [SDR HYIA20171213001](https://openairdocs.org/sdr/HYIA20171213001), Dec 12, 2017: FITTING. CRACKED. THE RT OB NACELLE FITTING PART NUMBER 5292029-24 WAS FOUND TO BE CRACKED DURING BORESCOPE INSPECTION PRESCRIBED BY TEXTRON MULTI-ENGINE SERVICE LETTER MEL-54-02 - [SDR HYIA20161108194](https://openairdocs.org/sdr/HYIA20161108194), Oct 30, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161108193](https://openairdocs.org/sdr/HYIA20161108193), Oct 30, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION; EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20161018001](https://openairdocs.org/sdr/HYIA20161018001), Oct 16, 2016: EXHAUST PIPE. CRACKED. PILOT REPORTED ON PREFLIGHT: RIGHT ENGINE MAIN EXHAUST STACK LOOSE. UPON INSPECTION MAINTENANCE FOUND THE RIGHT OVERBOARD EXHAUST PIPE CRACKED. REPLACED OVERBOA - [SDR HYIA20160825091](https://openairdocs.org/sdr/HYIA20160825091), Aug 22, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160825090](https://openairdocs.org/sdr/HYIA20160825090), Aug 22, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160825089](https://openairdocs.org/sdr/HYIA20160825089), Aug 22, 2016: EXHAUST VALVE. DAMAGED. CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE. - [SDR HYIA20160511001](https://openairdocs.org/sdr/HYIA20160511001), May 5, 2016: UNKNOWN. ODOR. PILOT DETECTED SMELL OF BURNING RUBBER IN FIRST OFFICERS FLOORBOARD AREA. PERFORMED A DETAILED VISUAL INSPECTION ON THE FOLLOWING ACFT AREAS & COMPONENTS, MLG B - [SDR HYIA20141212001](https://openairdocs.org/sdr/HYIA20141212001), Dec 10, 2014: SEALANT. FAULTY. PILOT REPORTED SMELL OF FUEL IS CONSTANT WITHIN CABIN. MX IS IN PROCESS OF RESEALING FAULTY SEALANT IN THE WING TANKS. - [SDR HYIA20140624002](https://openairdocs.org/sdr/HYIA20140624002), Jun 23, 2014: WEB. CRACKED. DURING SCHEDULED INSPECTION, MULTIPLE WEB FLANGE CRACKS WERE FOUND AT AFT FUSELAGE CARRY THROUGH SPAR ASSEMBLY PN 5211173-2 AT CTR UPPER SECTION FWD & AFT WEBS. - [SDR HYIA20140624001](https://openairdocs.org/sdr/HYIA20140624001), Jun 23, 2014: BEAM. CRACKED. DURING VISUAL INSPECTION OF NACELLE STRUCTURE AT TURBOCHARGER REMOVAL FOR OTHER MAINTENANCE, THE RT NACELLE CROSSOVER BEAM WAS FOUND TO BE CRACKED AT TURBOCHARG - [SDR HYIA20140621001](https://openairdocs.org/sdr/HYIA20140621001), Jun 20, 2014: SPAR CAP. CORRODED. DURING SCHEDULED INSPECTION, AREAS OF EXFOLIATING CORROSION WERE FOUND AT RT WING LWR SPAR CAP STRAP OEM PN 5292029-2 PREVIOUSLY INSTALLED TO SATISFY REQUIREMEN - [SDR HYIA20140414053](https://openairdocs.org/sdr/HYIA20140414053), Aug 9, 2013: 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 HYIA20140414027](https://openairdocs.org/sdr/HYIA20140414027), Nov 7, 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 HYIA2012052200001](https://openairdocs.org/sdr/HYIA2012052200001), May 22, 2012: ENGINE. POWER LOSS. RT ENGINE LOST POWER, VIBRATED SUDDENLY. INSPECTED ENGINE, CHECKED PARAMETERS, PERFORMED COMPRESSION CHECK, ADJUSTED IDLE FUEL MIXTURE, CHECKED RT WING TANK SUM - [SDR HYIA20140414008](https://openairdocs.org/sdr/HYIA20140414008), Aug 11, 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 HYIA20140415008](https://openairdocs.org/sdr/HYIA20140415008), 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 HYIA4652NRMLG](https://openairdocs.org/sdr/HYIA4652NRMLG), Aug 31, 2009: TRUNNION. SHEARED. CREW REPORTED, RT MLG SHEERED OFF ON LANDING ROLL. MX FOUND RT MLG UPPER BARREL AND TRUNNION ASSY SHEARED JUST BELOW MLG ACTUATOR ATTACH POINT. MX REMOVED AND R - [SDR 13552N122707](https://openairdocs.org/sdr/13552N122707), Dec 26, 2007: SKIN. DEBONDED. ON TAXI IN, CREW NOTICED DEBONDING HAD TAKEN PLACE ON RT AILERON UPPER IB SKIN. THE DISPLACEMENT OF SKIN DID NOT AFFECT THE FLIGHT CHARACTERISTICS OF THE AIRCRA - [SDR 2002FA0000897](https://openairdocs.org/sdr/2002FA0000897), Jul 12, 2002: ANGLE. SEPARATED. COULD NOT MOVE AILERONS. 90 PERCENT ANGLE, USED TO PREVENT OIL CANNING, BONDED INSIDE AILERON, BROKE LOOSE AND WORKED ITS WAY DOWN TRAILING EDGE OF AILERON AND - [SDR 20000907SH039](https://openairdocs.org/sdr/20000907SH039), Aug 14, 2000: TIRE. UNSERVICEABLE. CREW REPORTED UNUSUAL NOISE ON TAXI. FOUND CHUNK OF AFT TIRE MISSING. MAINTENANCE DISPATCHED TO CHANGE TIRE. FOUND LARGE PORTION OF RECAP HAD SEPARATED FROM COR ## 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 20090831017479I](https://openairdocs.org/incident/20090831017479I), Aug 31, 2009: Cessna 402C (N4652N), Nantucket, MA, Minor damage. (-23) During roll-out, after landing, on runway 6, the right main landing gear separated at the oleo and released from the aircraft. The aircraft came to rest… ## Other aircraft with N4652N - [Cancelled 1951-10-22](https://openairdocs.org/deregistered/N4652N-1951-10-22): Cessna T-50, S/N 5681. Exported to Mexico. Owner: [Vest Aircraft And Finance Co](https://openairdocs.org/faa-owner/VEST%20AIRCRAFT%20AND%20FINANCE%20CO), [Denver, CO](https://openairdocs.org/faa-place/CO/Denver) --- 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.