N75HS

CESSNA 750 · 1998 · Fixed-wing multi-engine · 2 engines · 12 seats · Valid Registration

Registered owner: PERFECT X AVIATION LLC, TX (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
CENTURY AVIATION INC (LDIA)Certificate holderMatched by certificate designator

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.

2 reports on file, 1995-02-09 – 2025-05-12.

VIBRATION/BUFFET; ELECT. POWER LOSS-50 PC · 2025-05-12 Matched by certificate designator
ATA 2421

Part: GENERATOR — DESTROYED (ZONE 400) · airframe 8,748 hrs · 6,962 cycles

DC GENERATOR BEARING FAILED CAUSING GENERATOR TO PARTIALLY DISINTEGRATE AND BECOME DETACHED FROM ITS DRIVE PAD. DURING THE FAILURE THE FIRE LOOP WAS STRUCK CAUSING IT TO FAIL, OIL WAS RELEASED FROM THE ENGINE CAUSING A LOSS OF OIL PRESSURE, AND THE HEAT FROM THE FAILURE BURNED THE AREA AND COMPONENTS ADJACENT THE GENERATOR. DEPARTED KTKI THIS MORNING TO GO TO TUPJ WITH 2 CREW AND 8 PAX. ENROUTE NEAR THE BAHAMAS GOT CASS MESSAGE THAT SAID DC.BEARING FAIL RH. THIS FOLLOWED UP ALMOST IMMEDIATELY WITH A RH GEN FAILURE. WHILE RUNNING THE APPROPRIATE CHECKLIST, WE STARTED TO FELL HEAVY VIBRATIONS COMING FROM THE RH ENGINE. THIS IN TURN GAVE US ANOTHER CASS MESSAGE THAT SAID FIRE DETEC FAIL RH ENGINE. ABOUT 2-3 MINUTES LATE WE GOT ANOTHER CASS MESSAGE THE SAID OIL PRESSURE LOW RH ENG. WE DECLARED AND EMERGENCY AT THIS TIME AND DIVERTED TO KMIA. WE ENDED UP HAVING TO SHUT THE RH ENG DOWN DUE TO LOW OIL PRESSURE. A SINGLE ENGINE LANDING WAS MADE INTO KMIA.

Source: SDR LDIA2025051400001
OTHER · 1995-02-09 Unresolved
ATA 7261

Part: OIL PUMP — FAILED (ENGINE)

THE ENGINE WAS DISASSEMBLED TO DETERMINE THE REASON FOR THE REPORTED PROBLEMS. DISASSEMBLY OF THE OIL PUMP ASSEMBLY REVEALED THE POST SB 7185 PLATE HAD BECOME WELDED TO THE SCAVENGE ELEMENT CAUSING IT TO SHEAR THE SHAFT DRIVE PIN. THIS FAILURE CAUSED FLOODING OF THE NR 4 BEARING CAVITY, ULTIMATELY RESULTING IN AN OIL FIRE AT THE NR 4 BEARING AREA.

Source: SDR 95ZZZX1146