N414PG

CESSNA 414A · 1982 · Fixed-wing multi-engine · 2 engines · 8 seats · Valid Registration

Registered owner: 89 GALILEO AVIATION LLC, FL (owner ≠ operator)

Operators of this aircraft

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

No operator established for this aircraft.

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

3 reports on file, 2002-07-11 – 2004-04-23.

PARTIAL RPM/PWR LOSS · 2004-04-23 Unresolved
ATA 8530

Part: CYLINDER HEAD — SEPARATED (ENGINE) · airframe 3,927 hrs

DURING POWER REDUCTION FROM TAKE-OFF POWER TO CLIMB POWER, A (POP) WAS HEARD AND ONE OF THE ENGINES BEGAN RUNNING ROUGH. THERE WAS NO INSTRUMENT/GAGE INDICATION AS TO WHICH ENGINE. AIRCRAFT LANDED WITH OUT INCIDENT. POST FLIGHT EXAMINATION FOUND NR 1 ENGINE, NR 6 CYLINDER HEAD HAD SEPARATED.

Source: SDR BHA05RS
OTHER · 2004-04-08 Unresolved
ATA 5341

Part: ATTACH FITTING — CORRODED (RT WING) · airframe 3,914 hrs

IN COMPLYING WITH SUPPLEMENTAL INSPECTION 57-10-20, FOUND THE RT WING LOWER SPAR ATTACH FITTING HAD SIGNIFICANT CORROSION IN SOME OF THE FITTING MOUNTING HOLES. THE FITTING WAS REPLACED. NO FURTHERDEFECTS WERE NOTED.

Source: SDR BHA04RS
INFLIGHT SEPARATION · 2002-07-11 Matched by certificate designator
ATA 8530

Part: CYLINDER HEAD — CRACKED (LT ENGINE)

CYLINDER HEAD SEPERATED FROM BARREL DURING CLIMB OUT. ENGINE FEATHERED AND AIRCRAFT LANDED SAFTELY. CYLINDER HEAD CRACKED ABOVE THREADED AREA TO BARREL.

Source: SDR 2002F00758