No fatalities

Throttle Stuck After Power Reduction Leads to Runway Excursion (N44438)

Newport, NH, US

On July 24, 1998, a Piper PA-28-151 (registration N44438) was involved in an aviation accident near Newport, NH. No fatalities were reported. Investigators recorded the probable cause as: The seizure of the throttle shaft, due to the overhaul facilities' failure to insure all metal fragments had been removed from the carburetor before inserting the throttle shaft after reaming the throttle shaft bushings. 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 2026-07-04Data APIEditorial standards
Aircraft registered N44438
Aircraft registered N44438. Photo: Georges Seguin ( Okki ) / CC BY-SA 3.0, via Wikimedia Commons

A pilot diverted after the throttle became stuck during descent. Unable to stop on landing, the airplane exited the runway and came to rest on a hill. Post-accident examination revealed a galled throttle shaft and improper bushing reaming.

Accident Sequence

After departing and climbing to a cruise altitude of 6,500 feet above mean sea level, the pilot reduced power to descend below a cloud layer. Following the power reduction, the throttle became stuck. Unable to move the throttle, the pilot diverted to an alternate airport. With the engine still running, the airplane touched down on the runway, but the pilot was unable to stop. The airplane exited the departure end of the runway, traveled 75 feet, and came to rest on top of a hill.

Pilot Actions

During the landing, the pilot believed the throttle was in the idle position. After the accident, he realized it was slightly open.

Post-Accident Examination

Examination of the carburetor, which had 12 hours since overhaul, revealed that the throttle shaft could not be rotated by hand. A punch and hammer were required to remove the shaft. The shaft was galled where it rested on the bushings. Both ends of the original shaft (part number CF 13-1521) measured .3105 of an inch in diameter. A new shaft supplied by the overhaul facility measured .3104 of an inch in diameter at both ends.

Under the supervision of the NTSB Investigator, the original throttle bushings were reamed with the original router. Then the new throttle shaft was inserted, and it rotated freely. The old shaft was then inserted but was difficult to rotate. After removing the old throttle shaft, the bushings were reamed using a new router the company had bought after the accident. Again, the old shaft was inserted, and this time it rotated freely. The butterfly valve was then installed, and the throttle shaft continued to rotate without difficulty.

Frequently asked questions

What happened in the 24 Jul 1998 Piper PA-28-151 accident near Newport, NH?

A pilot diverted after the throttle became stuck during descent. Unable to stop on landing, the airplane exited the runway and came to rest on a hill. Post-accident examination revealed a galled throttle shaft and improper bushing reaming.

Were there any fatalities in the 24 Jul 1998 Piper PA-28-151 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 24 Jul 1998 involved a Piper PA-28-151, registration N44438, at Newport, NH.

What was the probable cause of the accident?

The seizure of the throttle shaft, due to the overhaul facilities' failure to insure all metal fragments had been removed from the carburetor before inserting the throttle shaft after reaming the throttle shaft bushings.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X10686. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.