N288CA

COSTRUZIONI AERONAUTICHE TECNA P2012 TRAVELLER · 2019 · Valid Registration

Registered owner: HYANNIS AIR SERVICE INC, 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

Accident · 2002-04-12 Unresolved
Piper PA-28-181 Fatal injuryoperator not yet resolved
Source: NTSB case NYC02FA082

Maintenance disclosures

J · 2026-04-11 Matched by certificate designator
ATA 2430

PILOT REPORTED LEFT AND RIGHT ALTERNATOR FAILURES IN FLIGHT. MAINTENANCE INSPECTED AND FOUND FOUND BOTH ALTERNATOR BELTS TO HAVE FAILED. LEFT AND RIGHT ALTERNATOR BELTS WERE REPLACED WITH NO FURTHER DEFECTS NOTED.

Source: SDR HYIA20260424002 · FAA SDRS
R J · 2026-02-26 Matched by certificate designator
ATA 8530

PILOT REPORTED RIGHT ENGINE HIGH EGT DURING CRUISE FLIGHT. MAINTENANCE INSPECTED AND FOUND THE NR 4 EXHAUST VALVE CHIPPED NEAR VALVE SEAT. THE CYLINDER WAS REPLACED WITH NO FURTHER DEFECTS NOTED.

Source: SDR HYIA20260327007 · FAA SDRS
O · 2024-09-26 Matched by certificate designator
ATA 3497

PILOT REPORTED STALL HEAT CASS MESSAGE DOES NOT TURN OFF WHEN SWITCH IS TURNED ON. MAINTENANCE INSPECTED AND FOUND STALL HEATER SWITCH PINS SHORTED/ARCED. REMOVED AND REPLACED SWITCH, CONNECTOR AND PINS AS REQUIRED WITH NO FURTHER DEFECTS FOUND

Source: SDR HYIA20241003002 · FAA SDRS
F · 2023-06-30 Matched by certificate designator
ATA 2731

PILOT REPORTED PITCH TRIM ONLY GOES NOSE DOWN, WILL NOT GO NOSE UP. MAINTENANCE INSPECTED PITCH TRIM SYSTEM, VERIFIED PITCH TRIM CABLE TENSIONS PER TECNAM SERVICE LETTER SIL-2021-05 TENSIONS ARE 27 LBS, VERIFIED HORIZONTAL TRIM TAB TRAVEL CHECK IAW TECNAM JOB CARD NO. 1257 ED.1 REV. 0 NO ADJUSTMENT NEED AT THIS TIME. OPERATED PITCH TRIM VERIFIED FULL TRAVEL ON BOTH COPILOT AND PILOT SIDE COCKPIT INDICATION GOOD, NO DEFECTS NOTED.

Source: SDR HYIA20230707002 · FAA SDRS
O · 2020-05-28 Matched by certificate designator
ATA 5320

THE NLG ATTACH STRUCTURE WAS FOUND TO BE DAMAGED DURING AN INSPECTION INITIATED DUE TO SIMILAR FINDINGS ON OTHER COMPANY AIRCRAFT. THE DAMAGE IS LOCATED AT FWD MOST FUSELAGE BULKHEAD, LWR CENTER SECTION, IN THE AREA CORRESPONDING TO THE NLG MOUNTS. THE STRUCTURE AFT OF NLG BULKHEAD WAS INSPECTED WITH THE FOLLOWING DEFECTS NOTED: 1)THE FWD SECTIONS OF FLOORBOARD SUPPORTS AS THEY ARE RIVETED TO FORWARD-MOST FUSELAGE BULKHEAD ARE CRACKED. THE OEM HAS BEEN NOTIFIED AND A FLEETWIDE INSPECTION HAS BEEN ISSUED FOR ALL COMPANY AIRCRAFT.

Source: SDR HYIA20200528001 · FAA SDRS