Aviation Accident Summaries

Aviation Accident Summary CEN13LA571

Santa Teresa, NM, USA

Aircraft #1

N3078F

CESSNA 182J

Analysis

The pilot reported that he was making a circling descent to the airport after dropping parachutists and that he used carburetor heat during the descent. As the pilot was on the base leg of the landing pattern, close to the turn onto the final leg, the engine lost power. The pilot landed the airplane short of the runway, and the firewall buckled and the nose landing gear bent forward. The operator later functionally tested the engine and it operated normally.

Factual Information

On September 29, 2013, about 1530 mountain daylight time, a Cessna 182J, N3078F, landed short of the runway at Dona Ana County Airport (5T6), Santa Teresa, New Mexico, after the engine lost power. The pilot, the sole occupant on board, was not injured. The airplane was substantially damaged. The airplane was registered to and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a skydiving flight. Visual meteorological conditions prevailed at the time of the accident, and no flight plan had been filed. The local flight originated from 5T6 about 1505. The pilot told a Federal Aviation Administration inspector that he was returning to the airport after parachutists had exited the airplane. During the descent, he momentarily opened throttle several times to "clear" the engine. Carburetor heat was on throughout the descent. When he went to advance the throttle to level off in the traffic pattern, the engine failed to respond. The pilot immediately turned towards runway 28. The airplane landed short of the runway. Post-accident inspection revealed the firewall was buckled and the nose landing gear was bent forward. According to the operator, the engine was functionally tested and it operated normally. It was his opinion that when the pilot advanced the throttle to level off, the engine "loaded up" and failed to respond.

Probable Cause and Findings

A loss of engine power for reasons that could not be determined because no anomalies were found during the postaccident engine examination.

 

Source: NTSB Aviation Accident Database

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