N490KM

CESSNA 414 · Valid Registration

Registered owner: RASF414 LLC, FL (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
ISLAND SEAS LLC (7ILA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

O · 2015-01-16 Matched by certificate designator
ATA 8530

WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS NR 3 LOCATION, SN64015-16, NR 5 LOCATION, SN64016-17, NR 6 LOCATION, SN 63936-02. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OTBD FROM THE HEAD/BARREL JUNCTION. ENGINES WERE MODIFIED IAW STC SE4327SW-D.

Source: SDR 7ILA2015F00000 · FAA SDRS
O · 2015-01-16 Matched by certificate designator
ATA 8530

WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS NR 3 LOCATION, SN 64015-16, NR 5 LOCATION, SN 64016-17, NR 6 LOCATION, SN 63936-02. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OTBD FROM THE HEAD/BARREL JUNCTION. ENGINES WERE MODIFIED IAW STC SE4327SW-D.

Source: SDR 7ILA2015F00001 · FAA SDRS
O · 2015-01-16 Matched by certificate designator
ATA 8530

WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS NR 3 LOCATION, SN64015-16, NR 5 LOCATION, SN64016-17, NR 6 LOCATION, SN 63936-02. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OTBD FROM THE HEAD/BARREL JUNCTION. ENGINES WERE MODIFIED IAW STC SE4327SW-D.

Source: SDR 7IL2015F00002 · FAA SDRS
O · 2015-01-16 Matched by certificate designator
ATA 8530

WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS: NR 3 LOCATION, SN60652-27, NR 5 LOCATION, SN 60652-25, NR 4 LOCATION, SN 606652-23. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OTBD FROM THE HEAD/BARREL JUNCTION. ENGINE WAS MODIFIED IAW STC SE4327SW-D. CRACKS WERE DETECTED VIA SOAP BUBBLE TEST, EXCEPT THAT NR 5 CYLINDER HAD AUDIBLE HISS DURING COMPRESSION TEST AND HOLE BURNED IN BAFFLING.

Source: SDR 7IL2015F00003 · FAA SDRS
O · 2015-01-16 Matched by certificate designator
ATA 8530

WHILE PERFORMING 100 HR INSPECTION OF AIRCRAFT, FOUND CRACKS IN CYLINDERS: NR 3 LOCATION, SN60652-27, NR 5 LOCATION, SN 60652-25, NR 4 LOCATION, SN 606652-23. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OTBD FROM THE HEAD/BARREL JUNCTION. ENGINE WAS MODIFIED IAW STC SE4327SW-D. CRACKS WERE DETECTED VIA SOAP BUBBLE TEST, EXCEPT THAT NR 5 CYLINDER HAD AUDIBLE HISS DURING COMPRESSION TEST AND HOLE BURNED IN BAFFLING.

Source: SDR 7IL2015F00004 · FAA SDRS
O · 2015-01-16 Matched by certificate designator
ATA 8530

WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND CRACKS IN CYLINDERS: NR 3 LOCATION, SN60652-27, NR 5 LOCATION, SN 60652-25, NR 4 LOCATION, SN 606652-23. CRACKS WERE FOUND IN THE HEAD CASTING ON THE INTAKE VALVE SIDE IN THE VICINITY OF FINS 15-17 AS COUNTED OTBD FROM THE HEAD/BARREL JUNCTION. ENGINE WAS MODIFIED IAW STC SE4327SW-D. CRACKS WERE DETECTED VIA SOAP BUBBLE TEST, EXCEPT THAT NR 5 CYLINDER HAD AUDIBLE HISS DURING COMPRESSION TEST AND HOLE BURNED IN BAFFLING.

Source: SDR 7IL2015F00005 · FAA SDRS
O · 2015-01-16 Matched by certificate designator
ATA 5280

WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND RT REAR INNER GEAR DOOR ATTACH BRACKETS CRACKED AT INBD BOLT HOLE. BRACKET WAS STILL SECURED BY REMAINING MOUNT TABS. SIMILAR BRACKETS ARE USED ON FWD SIDE OF GEAR DOOR AS WELL AS LT GEAR DOOR, NO DAMAGE FOUND ON OTHER BRACKETS. DAMAGE IS DUE TO ROUTINE WEAR AND TEAR.

Source: SDR 7IL2015F00006 · FAA SDRS
O · 2015-01-16 Matched by certificate designator
ATA 5280

WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND RT REAR INNER GEAR DOOR ATTACH BRACKETS CRACKED AT INBD BOLT HOLE. BRACKET WAS STILL SECURED BY REMAINING MOUNT TABS. SIMILAR BRACKETS ARE USED ON FWD SIDE OF GEAR DOOR AS WELL AS LT GEAR DOOR, NO DAMAGE FOUND ON OTHER BRACKETS. DAMAGE IS DUE TO ROUTINE WEAR AND TEAR.

Source: SDR 7IL2015F00007 · FAA SDRS
O · 2015-01-16 Matched by certificate designator
ATA 6113

WHILE PERFORMING 100 HR INSPECTION OF ACFT, FOUND SPINNER REAR BULKHEAD CRACKED. BULKHEAD SN DY-1863.

Source: SDR 7IL2015F00008 · FAA SDRS