N4013Z

Substantial
Minor

AYRES S/N: R3S-002

Accident Details

Date
Wednesday, October 15, 2003
NTSB Number
FTW04LA009
Location
Midland, TX
Event ID
20031017X01765
Coordinates
31.942499, -102.201667
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A loss of engine power due to a ruptured oil line. A contributing factor was the lack of suitable terrain available for the forced landing.

Aircraft Information

Registration
N4013Z
Make
AYRES
Serial Number
R3S-002
Year Built
1979
Model / ICAO

Registered Owner (Historical)

Name
MURPHREE FLYING SERVICE INC
Address
625 STATE HIGHWAY 70 N
Status
Deregistered
City
ROTAN
State / Zip Code
TX 79546-6917
Country
United States

Analysis

On October 15, 2003, at 1608 central daylight time, an Ayres S2R-R3S single-engine, tailwheel-equipped airplane, N4013Z, sustained substantial damage when it impacted terrain during a forced landing following a loss of engine power near Midland, Texas. The airplane was registered to and operated by Murphree Flying Service, Inc., of Rotan, Texas. The commercial pilot, sole occupant of the airplane, sustained minor injuries. Visual metrological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 137 aerial application flight. The local flight originated from Big Spring Mc Mahon-Wrinkle Airport, near Big Spring, Texas, approximately 1538.

According to the 31,000-hour pilot, after completing the first pass of the aerial application on a field, his forward visibility was suddenly obstructed by oil covering the windscreen, followed by a loss of engine power. The pilot attempted to gain altitude, turned to the left (northerly direction), and initiated a forced landing. During the forced landing, the airplane's tailwheel struck a concrete culvert as the airplane crossed a 4-lane roadway. Subsequently, the airplane impacted a telephone pole, a railroad embankment, flipped over, and came to rest inverted.

Examination of the turbine powered airplane by an FAA inspector, who responded to the accident site, revealed the main wing spar was bent, and the engine was separated from the airframe. Further investigation of the engine components revealed that a high-pressure steel-braided oil line, which connected the nose engine case to the oil cooler, had ruptured. The rupture occurred approximately 6 to 8 inches from the oil cooler.

At the time of the accident, the aircraft had a total airframe time of 2,869.5 hours. The most recent annual inspection of the aircraft was completed on December 15, 2002, with approximately 1,903.6 hours total time on the airframe.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW04LA009