N5686X

Substantial
None

Ayres Corporation S-2RS/N: 2359R

Accident Details

Date
Monday, May 31, 2004
NTSB Number
DEN04LA083
Location
Beaver, UT
Event ID
20040615X00792
Coordinates
38.380538, -112.660827
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the in-flight failure of the engine's P3 tube which resulted in the loss of engine power and the subsequent impact with terrain during a forced landing. Contributing factors include the lack of suitable terrain for a forced landing and the fence.

Aircraft Information

Registration
Make
AYRES CORPORATION
Serial Number
2359R
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
S-2RA660
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
S-2R

Registered Owner (Current)

Name
WRIGHT WAYNE M
Address
10314 AUGUSTINE HERMAN HWY
City
CHESTERTOWN
State / Zip Code
MD 21620-3236
Country
United States

Analysis

On May 31, 2004, at approximately 1215 mountain daylight time, an Ayres Corporation S-2R, N5686X, was substantially damaged when it impacted terrain during a forced landing to a field approximately 1 nautical mile north of Beaver, Utah. The commercial certificated pilot, the sole occupant on board, was not injured. Visual meteorological conditions prevailed at the time of the accident. The local aerial application flight was being conducted under the provisions of Title 14 CFR Part 137 without a flight plan. The flight originated at approximately 1120.

According to the pilot, he had finished spraying a field and was returning to Beaver Municipal Airport (U52), for another load. He said that he had half a tank of fuel remaining and the engine was producing "excellent power." A few moments later, the engine ran rough for about a second and then stopped. He did not notice anything coming out of the exhaust. The pilot tried twice to restart the engine but was unsuccessful and he attempted a forced landing to an open field. During the landing, the airplane impacted terrain and struck a fence. Both wings were displaced aft and the right main landing gear was collapsed.

A visual examination of the engine revealed a 360 degree crack around the P3 air pressure tube, causing a separation of the tube between the engine plenum and fuel control unit. The crack was approximately one-quarter inch aft of the "B" nut, which connects the P3 air pressure tube to the fuel control unit. There was a "notable" amount of carbon build-up in the area around the crack. According to a maintenance representative, failure of the tube in flight would have resulted in a "significant reduction in fuel scheduling which could result in an engine flameout." An attempt to restart the engine in flight would "likely have failed," however; an attempt would have accounted for the "notable" amount of carbon build-up around the break in the tube.

No other aircraft anomalies were noted.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN04LA083