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Atlas / NTSB / SEA07LA017

NTSB CAROL · Event

Event SEA07LA017

2006-11-14 Caldwell, Idaho, United States Airport · EUL None 1 aircraft Status: Completed

Registry · N2390T

FAA Aircraft Registry record.

Make / Model

PIPER PA-28-140

Engine

LYCOMING 0-320 SERIES (180 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

19710921

ADS-B equipped

Yes — Mode-S A22C59

Registrant of record

KESSLER DEREK D

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's inadequate in-flight planning by failing to refuel while en route which resulted in fuel exhaustion and loss of engine power while on approach to the airport. Rough/uneven terrain was a factor.

Factual narrative

On November 14, 2006, at 1300 mountain standard time (MST), a Piper PA-28-140, N2390T, sustained substantial damage following a loss of engine power and subsequent forced landing during approach to Caldwell Industrial Airport, (KEUL) Caldwell, Idaho. The airplane was operated as a visual flight rules (VFR) cross-country flight under the provisions of Title 14, CFR Part 91, when the accident occurred. The commercial pilot and passenger were not injured. Visual meteorological conditions prevailed, and a VFR flight plan was in effect. The flight originated about 0855 MST from Tonopah, Nevada, (KTPH), and was en route (approximately 335 nautical miles) to Caldwell, Idaho. During a telephone conversation with the National Transportation Safety Board investigator-in-charge on November 14, the pilot reported that the engine lost power due to fuel exhaustion while on short final to the flight planned destination airport. The pilot stated that after losing power he initiated a forced landing to an open field approximately 1/4 mile short of runway 30. The airplane encountered rough/uneven terrain during the landing sequence and sustained substantial damage to the wing assembly. This was the aircraft's second flight after being topped off with fuel. The first flight commenced on November 13, however, due to deteriorating weather conditions the pilot returned to Tonopah approximately 45 minutes after departure. The aircraft was not refueled prior to the second (accident) flight. The pilot reported the flight took longer than expected due to higher than forecasted headwinds. The pilot reported the engine lost power due to fuel exhaustion while on short final to the destination airport. The accident occurred during the final leg of a 335 nautical mile VFR cross-country flight. The pilot stated that after losing power he initiated a forced landing to an open field approximately 1/4 mile short of the runway. The airplane encountered rough/uneven terrain during the landing sequence and sustained substantial damage to the wing assembly. The accident flight was the aircraft's second flight after being topped off with fuel. The first flight commenced on November 13, however, due to deteriorating weather conditions the pilot returned to the departure airport approximately 45 minutes after departure. The aircraft was not refueled prior to the accident flight. The pilot reported the flight took longer than expected due to higher than forecasted headwinds. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2006_SEA07LA017.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.