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Aircraft record

N3249MCessna 402C

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19828 ADs may apply21 service difficulty reports

Registration
Valid
expires Jan 31, 2030
Based in
Hyannis, MA
owner city / state
Owners
1
since 2009
NTSB events
None
since 1982
ADs may apply
8
confirm with A&P
Service reports
21
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Hyannis Air Service INC
Owner type
Corporation
City, state
Hyannis, MA
Certificate issued
Apr 17, 2009
Expires
Jan 31, 2030
Airworthiness
Standard · Normal
Airworthiness date
May 29, 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
Serial number
402C0296
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
A380CB

Engine

Type
Reciprocating

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

Ownership history

Ownership history from FAA records
  1. 2009 – nowHyannis Air Service INCHyannis, MA · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (8)

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.
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.
Show all 8 ADs
ADSubjectEffectiveApplies to
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 (21)

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.

  • Wings · fitting · corrodedSep 21, 2026

    DURING SCHEDULED WING FITTING INSPECTION, A SMALL AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND FORWARD UPPER WING ATTACH FITTING. THIS CORROSION MEASURES APPROXIMATELY .500 INCHES LONG, .125 INCHES WIDE, AND .020 INCHES DEEP ON THE TOP FACE OF THE FITTING. THIS CORROSION IS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Nacelles and pylons · crossbeam · crackedMar 26, 2026

    DURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND CROSSOVER BEAM. THIS CRACK IS LOCATED ON THE AFT FACE OF THE BEAM, COMMON TO THE TOP OUTBOARD BOLT HOLE FOR THE TURBOCHARGER SUPPORT BRACKET. THIS CRACK MEASURES APPROXIMATELY .875 INCHES LONG TRAVELING LONGITUDINALLY ACROSS THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · fitting · corrodedDec 19, 2024

    DURING SCHEDULED MAINTENANCE A SMALL AREA OF SURFACE CORROSION WAS VISUALLY IDENTIFIED ON THE RIGHT WING UPPER AFT WING FITTING. (OEM PN: 0822550-46). THIS CORROSION MEASURES APPROX. 1.25" LONG WITH A MAX DEPTH OF APPROX. .009" AND IS CONSISTENT WITH OTHER CORROSION FOUND ON THESE FITTINGS IN THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Wings · rib · crackedSep 26, 2023

    DURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB (P/N: 5122115-55) AT L.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS FORWARD AN APPROXIMATE LENGTH OF .992 INCHES. THE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · exhaust valve · damagedAug 30, 2016

    CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · exhaust valve · damagedAug 30, 2016

    CYLINDER REMOVED DUE TO LOW COMPRESSION AT INSPECTION. EXHAUST VALVE DISPLAYS EVIDENCE OF HEAT DAMAGE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · push-pull rod · bentNov 5, 2015

    WHEN EXTENDING FLAPS 15 DEGREES, ACFT ROLLS RT UNCOMMANDED. REST OF FLAP DEPLOYMENT AFTER TRIM INITIATED FEELS NORMAL. INSPECTED & FOUND THE RT INBD & OTBD FLAP RODS BENT. R & R RIT INBD & OTBD FLAP PUSH & PULL RODS & RE-RIGGED FLAP CABLES.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · connecting rod · out of limitsOct 1, 2015

    DURING REPLACEMENT OF THE NR 2 CYLINDER, THE CONNECTING ROD BUSHING, PN 530658, HAD MOVED FROM THE CONNECTING ROD BORE IN A REARWARD DIRECTION & EXHIBITED MISSING MATERIAL FROM CONTACT WITH THE PISTON PIN BORE BOSS. THE ENG WAS COMPLETELY DISASSEMBLED FOR FURTHER EXAMINATION. INSPECTION REVEALED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · fluid · lowApr 27, 2014

    WHILE TAXIING, THE PILOT ATTEMPTED TO EXECUTE A RT TURN. THE RT BRAKE PEDAL WENT SOFT & THE ACFT STOPPED TURNING & TAXIED STRAIGHT FWD. THE PILOT CLOSED THE THROTTLE & STOPPED, BUT THE ACFTS NOSE & LT TIRE WENT INTO THE GRASS. THE ACFT COULD NOT BE MOVED WITH DIFFERENTIAL POWER SO THE PASSENGERS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Autoflight · sensor · failedApr 4, 2014

    AUTOPILOT COMPUTER CIRCUIT BREAKER TRIPPED WITH A HOT ELECTRICAL ODOR IN CABIN. INSPECTED & FOUND ODOR FROM ALTITUDE SENSOR. DISCONNECTED AUTOPILOT SYS.

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

Showing the 10 most recent of 21 reports.

Related aircraft

Show all 8 related aircraft
All 115 registered Cessna 402C aircraft

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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