N4217S

Substantial
None

Beech V35BS/N: D9968

Accident Details

Date
Sunday, January 13, 2002
NTSB Number
CHI02LA063
Location
Mattoon, IL
Event ID
20020115X00072
Coordinates
39.469581, -88.360900
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

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

Aircraft Information

Registration
Make
BEECH
Serial Number
D9968
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
V35BBE35
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
V35B

Registered Owner (Current)

Name
DELTA U 84 LLC
Address
2515 E LAKESHORE DR APT 11
City
CROWN POINT
State / Zip Code
IN 46307-7225
Country
United States

Analysis

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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI02LA063