Skip to content

CHI02LA063

2002-01-13 · Mattoon, Illinois, United States · None · 1 aircraft · Status: Completed

Airport MTO

Current FAA registration · N4217S

Make / Model
BEECH V35B
Year of manufacture
1977 · 25 years old at event
Seats / Engines
6 seats · 1 engine
Last airworthiness date
19761119
ADS-B equipped
Yes — Mode-S A502B4

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

A loss of engine power for undetermined reasons. Factor to the accident was the unsuitable rough/uneven terrain encountered during the forced landing.

Factual narrative

On January 13, 2002, at 1115 central standard time, a Beech V35B, N4217S, piloted by a private pilot, sustained substantial damage during a forced landing near the Coles County Memorial Airport (MTO), Mattoon, Illinois. Visual meteorological conditions prevailed at the time of the accident. The flight was operating under the provisions of 14 CFR Part 91 without a flight plan. The pilot and his single passenger reported no injuries. The flight departed at 1100 and had the intended destination of Rantoul, Illinois. According to the pilot's written statement, he had departed MTO, climbed to 3,000 feet above mean sea level, throttled back to 23 inches of manifold pressure and 2,300 rpm, and set the fuel flow rate to 14 gallons per hour. The pilot reported that approximately 4 - 5 miles northeast of MTO the engine rpm began to fluctuate between 1,800 and 1,900 rpm. The pilot stated he decided to turn back to MTO and entered the traffic pattern for runway 24. The pilot reported he lowered the landing gear while on downwind leg. The pilot stated that after he turned onto the base leg the engine began to lose power. The pilot reported he turned on the electric fuel pump and "worked throttle" with no change in engine performance. The pilot stated he turned onto the final approach for runway 24 and "Engine occasional sputter but seemed quieter. [Manifold] pressure, rpm just dropping, airspeed and altitude dropping quickly." The airplane landed approximately 1/4 mile short of runway 24. An inspector with the Federal Aviation Administration performed the post-accident examination of the airplane. The engine was subjected to an operational test while still attached to the airframe and original fuel system. The engine started without hesitation and ran at varying power ranges without any anomalies. During a forced landing the airplane landed short of the runway resulting in substantial damage. Approximately 4 - 5 miles northeast of the departure airport the engine began to fluctuate between 1,800 - 1,900 rpm. The pilot elected to turn back to the departure airport and enter the traffic pattern for runway 24. The pilot reported he lowered the landing gear while on downwind leg. The pilot stated the engine began to lose significant power while on base leg and he turned on the electric fuel pump and "worked throttle" with no change in engine performance. The pilot stated he turned onto the final approach for runway 24 and "Engine occasional sputter but seemed quieter. [Manifold] pressure, rpm just dropping, airspeed and altitude dropping quickly." The airplane landed approximately 1/4 mile short of runway 24. The engine was subjected to an operational test while still attached to the airframe and original fuel system. The engine started without hesitation and ran at varying power ranges without any anomalies. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2002_CHI02LA063.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.