N402HG

CESSNA 402C · 1985 · Valid Registration

Registered owner: HYANNIS AIR SERVICE INC DBA, MA (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
HYANNIS AIR SERVICE INC. (HYIA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

B · 2020-09-02 Matched by certificate designator
ATA 2121

THE PILOT REPORTED THAT DURING FLIGHT A BURNING SMELL WAS NOTED. MAINTENANCE INSPECTED AND FOUND THE AV COOLING FAN CB HAD TRIPPED. REMOVED AND REPLACED THE AV COOLING FAN WITH NO FURTHER DEFECTS NOTED.

Source: SDR HYIA20200904001 · FAA SDRS
F · 2019-01-25 Matched by certificate designator
ATA 2721

PILOT REPORTED THE RUDDER TRIM BOUND UP DURING FLIGHT AND RETURNED BASE WITH NO INCIDENT. MAINTENANCE INSPECTED RUDDER TRIM CONTROL SYSTEM AND FOUND A TRIM TAB CABLE PULLEY AT FS 255 NOT ROTATING, MX CLEANED AND LUBRICATED CABLE PULLEY AT FS 255. THE RUDDER TRIM ACTUATOR WILL ALSO BE REPLACED AS A PRECAUTIONARY MEASURE.

Source: SDR HYIA20190129001 · FAA SDRS
O · 2016-11-02 Matched by certificate designator
ATA 8530

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

Source: SDR HYIA20161109197 · FAA SDRS
O · 2016-10-14 Matched by certificate designator
ATA 8530

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

Source: SDR HYIA20161108180 · FAA SDRS
O · 2016-10-13 Matched by certificate designator
ATA 8530

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

Source: SDR HYIA20161108179 · FAA SDRS
O · 2013-12-11 Matched by certificate designator
ATA 3260

LANDING GEAR WOULD NOT RETRACT, RETURN TO BLOCK. FOUND LG SQUAT SWITCH TO BE OUT OF ADJUSTMENT. .

Source: SDR HYIA20131216001 · FAA SDRS
O · 2013-05-10 Matched by certificate designator
ATA 8530

RIGHT ENGINE BEGAN TO VIBRATE ON SHORT FINAL. FOUND BROKEN INNER AND OUTER EXHAUST VALVE SPRINGS AND BROKEN INTAKE VALVE INNER SPRING ON THE NR 5 CYLINDER. PULLED ROCKER BOX COVERS AND FOUND THE INNER INTAKE AND EXHAUST VALVE SPRINGS BROKEN ON 11 OF 12 CYLINDERS. CYLINDER, TISN71.2BCA, HAD ACCULATED 8.3 HRS SINCE NEW.

Source: SDR 2013FA0000302 · FAA SDRS