Casualties unknown

Pilot Reports Fuel Exhaustion During Forced Landing (N6887F)

Peyton, CO, US

On July 26, 2002, a Piper PA-24-250 (registration N6887F) was involved in an aviation accident near Peyton, CO. Investigators recorded the probable cause as: A loss of engine power due to fuel exhaustion as a result of leaking fuel caps. Contributing to the accident was the lack of suitable terrain for a forced landing. 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

A pilot reported that the airplane ran out of fuel after about 3 hours and 10 minutes of flight. A forced landing to a road resulted in the right main landing gear folding and damage to the right wing and horizontal stabilizer.

Accident Overview

According to the pilot, the fuel tanks were topped off with a total of 60 gallons of fuel before the flight. The pilot stated that he flew for approximately 3 hours and 10 minutes before the "airplane ran out of fuel." He then performed a forced landing to a road, but the road ended short of the required braking distance. To avoid hitting telephone poles, "J" boxes, and a fence, the pilot applied "heavy" left rudder. During the landing, the right main landing gear folded under the fuselage, and subsequently, the right wing and right horizontal stabilizer were bent up.

Pilot Statement

The pilot reported that the airplane was equipped with "thermos bottle" type fuel caps. He believed that fuel was being siphoned out of the tanks, possibly explaining why the fuel was exhausted earlier than expected.

Postaccident Examination

A postaccident examination of the fuel tank area, conducted by the pilot, revealed some fuel residue stains inside the fuel door. No further details on the examination were provided.

Performance Data

According to the performance section of the Pilot's Operating Handbook (POH), the fuel consumption at 19.5 inches of manifold pressure, 2,450 revolutions per minute, and 6,500 to 7,500 feet cruising altitude was approximately 13 gallons per hour. This suggests that the fuel usage during the flight was consistent with the handbook figures, but the pilot's belief of siphoning may have contributed to the fuel exhaustion.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020808X01328. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.