N186LA

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.

4 reports on file, 2013-02-26 – 2018-06-12.

OTHER · 2018-06-12 Matched by certificate designator
ATA 5311

Part: FRAME — CRACKED (BS 4640) · airframe 2,789 hrs · 6,669 cycles

DURING INSPECTION, FOUND A CRACK ON THE MAIN TRANSMISSION FRAME AT BS 4640

Source: SDR 2A6R201806124783
OTHER · 2018-06-12 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (FUSELAGE) · airframe 2,789 hrs · 6,669 cycles

DURING INSPECTION, FOUND A DENT ON THE LEFT FUSELAGE SKIN PANEL.

Source: SDR 2A6R201806124782
OTHER · 2018-06-12 Matched by certificate designator
ATA 5330

Part: SKIN — CHAFED (ENG BAY DOOR) · airframe 2,789 hrs · 6,669 cycles

DURING INSPECTION FOUND THE RIGHT UPPER BACK COWLING CHAFED ALMOST COMPLETELY THRU.

Source: SDR 2A6R201806124781
OTHER · 2013-02-26 Matched by certificate designator
ATA 6220

Part: BOLT — CRACKED (MAIN ROTOR) · airframe 1,882 hrs

DURING A 100HR ANNUAL INSPECTION, IT WAS NOTED ON THE VEMD THAT THERE WERE MAST MOMENT EXCEEDANCES TRAPPED. DURING A DIE PENETRANT INSPECTION OF THE SECONDARY BOLTS 3 OF 4 INSTALLED SECONDARY BOLTS HAD CRACKING IN THE THREADED PORTION OF THE BOLT.

Source: SDR 2013FA0000127