N9379K

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

STINSON 108-2 No injuries Part 91operator not named in the NTSB record
Source: NTSB case SEA79FTA12

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.

4 reports on file, 2017-07-20 – 2018-04-03.

OTHER · 2018-04-03 Unresolved
ATA 6330

Part: FITTING — CRACKED (MGB) · airframe 2,690 hrs · 5,730 cycles

CRACKED MGB SUPPORT FITTING. COUNTER TORQUE CROSSBEAM FITTING PLATE WAS FOUND CRACKED.

Source: SDR 2018FA0000130
OTHER · 2018-04-03 Unresolved
ATA 3400

Part: BRACKET — FAILED (FLUX VALVE) · airframe 2,254 hrs · 5,734 cycles

PILOT CONDUCTING A POST FLIGHT WALK-AROUND FOUND THE FLUX COMPENSATOR HANGING UNDERNEATH THE AFT CENTER PORTION OF THE TAILBOOM. FLUX VALVE MOUNT BRACKET RING HAD FAILED.

Source: SDR EIBA2018040300123
OTHER · 2018-04-03 Unresolved
ATA 6330

Part: SUPPORT FITTING — CRACKED (MAIN GEARBOX) · airframe 2,690 hrs · 5,730 cycles

CRACKED MGB SUPPORT FITTING. WHILE COMPLETING LEONARDO SB 119-087 LEFT HAND COUNTER TORQUE CROSSBEAM FITTING PLATE WAS FOUND CRACKED.

Source: SDR 2018FA0000129
PARTIAL RPM/PWR LOSS · 2017-07-20 Matched by certificate designator
ATA 7321

Part: FUEL CONTROL — SURGES (ENGINE) · airframe 2,234 hrs · 4,982 cycles

ENGINE TORQUE AND N1 FROM 3-5% DURING APPROACH IN A HOVER AND AFTER TOUCH DOWN.

Source: SDR 2017F00127