N108SD

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

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, 2002-06-03 – 2013-03-08.

OTHER · 2013-03-08 Unresolved
ATA 2822

Part: PUMP — FAILED (FUEL BOOST) · airframe 7,962 hrs · 7,950 cycles

INSTALLED FOUR O/H FUEL BOOST PUMPS, IN SAME POSITION. EACH BOOST PUMP WOULD OPERATE WHEN INITIALLY POWERED UP, THEN FAIL TO OPERATE ON SUBSEQUENT ATTEMPTS. INSTALLATION OF FIFTH OVER HAULED UNIT OPS CHECKED NORMAL WITH NO SUBSEQUENT FAILURES.

Source: SDR COZR20130311003
OTHER · 2003-02-05 Matched by certificate designator
ATA 7920

Part: HOSE — CHAFED (ENGINE)

THIS HOSE DETERIORATES RAPIDLY DUE TO THE FACT THAT THE HOSE IS A CORRUGATED TUBE HOUSED IN A STEEL BRAID THAT CHAFES THE TUBE CAUSING CHAFE DAMAGE TO THE HOSE AND SUBSEQUENT OIL LEAK. THIS HOSE SHOULD BE REDESIGNED TO EXTEND RELIABILITY. THE HOSES LAST ABOUT 2 YEARS, 1,000 HOURS.

Source: SDR 53075
OTHER · 2002-06-03 Unresolved
ATA 6220

Part: HEAD — DAMAGED (MAIN ROTOR)

DURING INSPECTION, DAMAGE WAS NOTED ON TAIR ROTOR CROSSHEAD PITCH CHANGE ARMS CAUSED BY CONTACT WITH THE P/C LINKS.

Source: SDR JBZ2002F00000