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Aircraft record

N2649Z1980 Cessna 402C

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:3 NTSB accidents (substantial damage at worst, latest Nov 2022)9 ADs may apply10 service difficulty reports

Registration
Valid
expires Jul 31, 2027
Based in
Hyannis, MA
owner city / state
Engine
TSIO-520 SER · 300 hp
Cont Motor
Owners
1
since 2008
NTSB events
3
substantial, 2022
ADs may apply
9
confirm with A&P
Service reports
10
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Hyannis Air Service INC
Owner type
Corporation
City, state
Hyannis, MA
Certificate issued
Jun 11, 2008
Expires
Jul 31, 2027
Airworthiness
Standard · Normal
Airworthiness date
Aug 19, 1980

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Cessna
Model
402C
Year
1980
Serial number
402C0333
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
10
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A29184

Engine

Make and model
Cont Motor Tsio-520 Ser
Type
Reciprocating
Power
300 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2008 – nowHyannis Air Service INCHyannis, MA · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (3)

Accident · substantial damage

Nov 18, 2022 · Mashpee, MA

The airplane’s impact with a bird while enroute.

Damage
Substantial
Injuries
None
Report
ERA23LA106

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA23LA106)

Accident · substantial damage

Sep 15, 1997 · Kivalina, AK

An overstress fracture of the nose landing gear attachment. A factor associated with the accident was the rough landing area.

Damage
Substantial
Injuries
None
Report
ANC97LA150

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC97LA150)

Accident · substantial damage

Sep 8, 1997 · Buckland, AK

The failure of the pilot of the Cessna 402C, N2649Z, to maintain adequate clearance while taxiing alongside the stationary Cessna 208B, N1123R.

Damage
Substantial
Injuries
None
Report
ANC97LA145

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC97LA145)

Accident history for this model

ADs published since 1998 that may apply (9)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2017-10-09Textron Aviation Inc. AirplanesJun 7, 2017Airframe (402C)Certain serial numbers: 402C 402C0001–402C1020; 414A 414A0001–414A1212. Only with: Equipped with Cessna Multi-Engine Service Kit SK402-47 (Original Issue, Rev A, or Rev B) or nacelle fittings P/Ns 5292029-9, -10, -11, -12, -21, -22, -23, or -24.
2016-17-08Elevator Tab Control SystemSep 12, 2016Airframe (402C)
2015-07-03Nacelles/PylonsApr 24, 2015Airframe (402C)Certain serial numbers: 402C 402C0001–402C1020; 414A 414A0001–414A1212
2012-23-01WingsDec 26, 2012Airframe (402C)Only with: Model 402C modified by STC SA927NW; Model 414A modified by STC SA892NW.
2009-16-03Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating…Sep 9, 2009Engine (TSIO-520 SER)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed.
Show all 9 ADs
ADSubjectEffectiveApplies to
2005-20-25The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411…Nov 9, 2005Airframe (402C)Certain serial numbers: 401 655; 401 401-0001–401-0322; 401A 655; 401A 401A0001–401A0132; 401B 401B0001–401B0221; 402 402-0001–402-0322; …. Only with: Equipped with an avionics bus circuit breaker switch P/N CM3589-50, 593-250-101, 593-250-102, W31-X2M5A-50, or W31-X1000-50.
2005-12-13Cessna Aircraft Company Models 402C and 414A AirplanesJun 22, 2005Airframe (402C)
2000-01-16Cessna Aircraft Company 300 and 400 Series AirplanesFeb 15, 2000Airframe (402C)
98-04-28Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414…Mar 13, 1998Airframe (402C)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (10)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Fuel · pump · obstructedJul 13, 2026

    CREW REPORTED LEFT HAND ENGINE VIBRATION AND SLIGHT SURGING, ALL ENGINE INDICATIONS REPORTED NORMAL. CREW PERFORMED MAG CHECK (NORMAL) AND TURNED THE LEFT AUXILIARY PUMP OFF, THEN TO HIGH AND STILL HAD THE VIBRATION, SLIGHT SURGING AND DROPPING RPM. CREW DECIDED TO FEATHER THE ENGINE AND SHUT IT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · heater · odorMar 11, 2018

    PILOT REPORTED SMOKE SMELL IN COCKPIT. TURNED HEATER OFF AND SMELL STOPPED. MAINTENANCE INSPECTED AND AFTER TROUBLESHOOTING DETERMINED THE HEATER ASSEMBLY WAS TO BE REPLACED. REPLACED HEATER WITH NO FURTHER DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · switch · intermittentMar 6, 2017

    PILOT REPORTED NOSE GEAR COLLAPSED ON LANDING. INITIAL INSPECTION AND TESTING INDICATES A FAULTY ACTUATOR SWITCH FALSELY INDICATED GEAR WAS DOWN AND LOCKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Electrical power · alternator · defectiveNov 25, 2014

    BITTER FUME LIKE SMELL IN CABIN. INSPECTED ELEC WIRING & FOUND NO DEFECTS. SMELL WAS DETERMINED TO BE COMING FROM THE LT ALTERNATOR. R & R THE LT ALTERNATOR & RETURNED THE ACFT TO SERVICE WITH NO FURTHER DEFECT NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · drag brace · crackedNov 29, 2012

    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. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMENT DRAG BRACE HAS BEEN INSTALLED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · drag brace · crackedJul 10, 2012

    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. THIS CRACK WAS FOUND TO BE BEYOND LIMIT ALLOWABLE OF MEB91-11R1. THIS UNIT HAS BEEN SCRAPPED & A REPLACEMENT DRAG BRACE HAS BEEN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · switch · failedMar 2, 2012

    NOSE GEAR COLLAPSED ON LANDING. NLG ACTUATOR WAS REMOVED AND TESTED IN A CONTROLLED ENVIRONMENT. WHEN THE ACTUATOR WAS COLD SOAKED, THE SWITCH FAILED TO ACTIVATE PROPERLY GIVING A FALSE INDICATION THAT THE GEAR WAS DOWN AND LOCKED. DUE TO THE GEAR FAILURE, BOTH ACFT PROPELLERS STRUCK THE GROUND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · drag brace · crackedMay 27, 2011

    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 PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OUTLINED IN MEB941-11R1 & RETURNED TO…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · drag brace · crackedJan 28, 2011

    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 PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OUTLINED IN MEB941-11R1 & RETURNED TO…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · solenoid · stuckAug 5, 1999

    DURING FIGHT, PILOT REPORTED SMOKE IN THE COCKPIT AND RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. THE MAINTENANCE DEPARTMENT WAS DISPATCHED. POSSIBLE CAUSE WAS HYDRAULIC MANIFOLD SOLENOID STUCK AND CAUSED SYSTEM TO OVERHEAT CAUSING A PIN HOLE IN THE HYDRAULIC SIGHT GAUGE. THIS CAUSED THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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