N6350X

No registry detail on file · not in current registry

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

B K · 1998-07-14 Matched by certificate designator
ATA 2820

WHILE READING THE ACFT HOUR METER, A STRONG FUEL SMELL WAS NOTICED. A FUEL STAIN WAS NOTICED UNDER THE LEFT WING STARTING AT THE INBD ENGINE NACELLE AND SEEPING DOWN THE MAIN WING SPAR TO THE INBD MAIN GEAR DOOR. CROSS-FEED FUEL LINE HAD BEEN CHAFED AFT OF THE TURBOCHARGER BY A STRINGER AND WAS LEAKING. UNFORTUNATELY, THESE LINES MAINTAIN A POSITIVE PRESSURE ON THEM WITH NO WAY TO TURN OFF THE FUEL. IT IS SUBMITTER'S RECOMMENDATION THAT CESSNA PROVIDE SOME MEANS TO ENABLE THE PILOT TO TURN OFF THE FUEL SUPPLY TO THESE FUEL LINES.

Source: SDR 98ZZZX2982 · FAA SDRS
O · 1997-05-09 Matched by certificate designator
ATA 5720

AFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH TIP TANK AFT SUPPORT BRACKETS (CESSNA P/N 08222600-29 AND -30) TO THE WING. LT SIDE ALSO CRACKED MOST OTBD RIB (CESSNA P/N 0822040-17) AND THE MOST AFT TIP TANK SUPPORT BULKHEAD (CESSNA P/N 0823400-63, SUBASSY OF 823400-109) HAD 2 CRACKS. RIGHT DID NOT REFLECT ANY DAMAGE TO STRINGER (MOST AFT POINT) OF TIP TANK, HOWEVER, LT SIDE HAD STRUCK SOLID OBJECT AT SOME POINT.

Source: SDR 97ZZZX2115 · FAA SDRS
O · 1997-05-09 Matched by certificate designator
ATA 5712

AFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH TIP TANK AFT SUPPORT BRACKETS (CESSNA P/N 08222600-29 AND -30) TO THE WING. LT SIDE ALSO CRACKED MOST OTBD RIB (CESSNA P/N 0822040-17) AND THE MOST AFT TIP TANK SUPPORT BULKHEAD (CESSNA P/N 0823400-63, SUBASSY OF 823400-109) HAD 2 CRACKS. RIGHT DID NOT REFLECT ANY DAMAGE TO STRINGER (MOST AFT POINT) OF TIP TANK, HOWEVER, LT SIDE HAD STRUCK SOLID OBJECT AT SOME POINT.

Source: SDR 97ZZZX2116 · FAA SDRS
O · 1997-05-09 Matched by certificate designator
ATA 5730

AFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH TIP TANK AFT SUPPORT BRACKETS (CESSNA P/N 08222600-29 AND -30) TO THE WING. LT SIDE ALSO CRACKED MOST OTBD RIB (CESSNA P/N 0822040-17) AND THE MOST AFT TIP TANK SUPPORT BULKHEAD (CESSNA P/N 0823400-63, SUBASSY OF 823400-109) HAD 2 CRACKS. RIGHT DID NOT REFLECT ANY DAMAGE TO STRINGER (MOST AFT POINT) OF TIP TANK, HOWEVER, LT SIDE HAD STRUCK SOLID OBJECT AT SOME POINT.

Source: SDR 97ZZZX2112 · FAA SDRS
O · 1997-05-09 Matched by certificate designator
ATA 5751

AFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH TIP TANK AFT SUPPORT BRACKETS (CESSNA P/N 08222600-29 AND -30) TO THE WING. LT SIDE ALSO CRACKED MOST OTBD RIB (CESSNA P/N 0822040-17) AND THE MOST AFT TIP TANK SUPPORT BULKHEAD (CESSNA P/N 0823400-63, SUBASSY OF 823400-109) HAD 2 CRACKS. RIGHT DID NOT REFLECT ANY DAMAGE TO STRINGER (MOST AFT POINT) OF TIP TANK, HOWEVER, LT SIDE HAD STRUCK SOLID OBJECT AT SOME POINT.

Source: SDR 97ZZZX2113 · FAA SDRS
O · 1997-05-09 Matched by certificate designator
ATA 5720

AFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH TIP TANK AFT SUPPORT BRACKETS (CESSNA P/N 08222600-29 AND -30) TO THE WING. LT SIDE ALSO CRACKED MOST OTBD RIB (CESSNA P/N 0822040-17) AND THE MOST AFT TIP TANK SUPPORT BULKHEAD (CESSNA P/N 0823400-63, SUBASSY OF 823400-109) HAD 2 CRACKS. RIGHT DID NOT REFLECT ANY DAMAGE TO STRINGER (MOST AFT POINT) OF TIP TANK, HOWEVER, LT SIDE HAD STRUCK SOLID OBJECT AT SOME POINT.

Source: SDR 97ZZZX2114 · FAA SDRS
O · 1997-05-09 Matched by certificate designator
ATA 5720

AFTER HAVING PROBLEMS WITH ANOTHER 400 SERIES ACFT, INSPECTED AFT ATTACH POINT OF TIP TANKS. DISCOVERED THE MOST AFT WING SKIN CRACKED AND HORIZ RIVETS SHEARED THAT ATTACH THE OTBD AILERON BRACKET ASSY (CESSNA P/N 521001-12) WHICH ARE SAME RIVETS THAT ATTACH TIP TANK AFT SUPPORT BRACKETS (CESSNA P/N 08222600-29 AND -30) TO THE WING. LT SIDE ALSO CRACKED MOST OTBD RIB (CESSNA P/N 0822040-17) AND THE MOST AFT TIP TANK SUPPORT BULKHEAD (CESSNA P/N 0823400-63, SUBASSY OF 823400-109) HAD 2 CRACKS. RIGHT DID NOT REFLECT ANY DAMAGE TO STRINGER (MOST AFT POINT) OF TIP TANK, HOWEVER, LT SIDE HAD STRUCK SOLID OBJECT AT SOME POINT.

Source: SDR 97ZZZX2117 · FAA SDRS
K · 1997-05-02 Matched by certificate designator
ATA 8520

DURING THE COURSE OF A NORMAL FLIGHT, PILOT NOTICED OIL LEAK ON LEFT ENGINE. AFTER FLIGHT, REMOVED ENGINE COWLING AND SAW 5 CYLINDER STUDS HAD BROKEN ON THE NR 1 CYLINDER. ON ENGINES OPERATED ON 1600 TBO'S, SUSPECT TIME IN SERVICE IS THE MAIN CAUSE FOR BREAKAGE. PLEASE NOTE: THIS IS NOT A 7TH STUD TYPE CASE, HOWEVER, IT IS A 'HEAVY' CASE.

Source: SDR 97ZZZX2068 · FAA SDRS