Casualties unknown

Engine Failure During Climb-Out Leads to Forced Landing After Helicoid Insert Cross-Threading (N6858P)

Lincoln Park, NJ, US

On November 26, 2005, a Piper PA-24-180 (registration N6858P) was involved in an aviation accident near Lincoln Park, NJ. Investigators recorded the probable cause as: The improper installation of the helicoil by the non-certificated mechanic, and the inadequate inspection of the installation by the certificated mechanic. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-10Data APIEditorial standards

During climb-out, pilot felt engine imbalance and misfire, then backfire and total power loss. Forced landing resulted in tree impact and substantial damage. Investigation found cross-threaded helicoil in cylinder head with metal particles.

Incident

During the climb-out from the departure airport, the pilot noticed that the engine felt off balance and began to misfire. The pilot initiated a return to the airport, but shortly thereafter the engine backfired and lost all power. The pilot then performed a forced landing, during which the airplane impacted trees and sustained substantial damage.

Examination

Post-accident examination of the engine revealed that a helicoil insert was cross-threaded in the number 3 cylinder head. Additionally, metallic particles were found adhered to the cylinder head and the top of the piston.

Maintenance Background

Thirteen days before the accident, the pilot had reported difficulty clearing one of the spark plugs and subsequently removed the number 3 cylinder bottom spark plug. A mechanic then cleaned the spark plug hole, assured that no steel particles remained in the cylinder, replaced the helicoil, installed a new spark plug, and ran the engine. The mechanic who performed the helicoil installation was non-certificated, and at the time of the work, no certificated mechanic was present.

According to Textron Lycoming Service Instruction No. 1043A, if a spark plug helicoil insert replacement is performed with the cylinder assembled on the engine, "some provision must be made for preventing the aluminum shavings from entering the combustion chamber."

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20051210X01961. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.