Loomis XENON 4 N912XV

Summary

On 17 April 2017 at about 18:41 local time, a Loomis XENON 4 registered N912XV was involved in an accident near Knoxville, Iowa, United States. 2 people were on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

17 April 2017 at 18:41

Classification

Accident

Location

Knoxville, Iowa, United States

Nearest airport

Knoxville Municipal (OXV)

Coordinates

41.3264, -93.0925

Aircraft

Loomis XENON 4

Registration

N912XV

Category

Gyrocraft

Year built

2016

Engines

1

Operator

Not recorded

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Knoxville → Knoxville

Aircraft damage

Substantial

Weather

VMC

Light

Day

NTSB number

CEN17LA156

Nobody was injured.

A partial loss of engine power for reasons that could not be determined based on the available information. Contributing to the accident was the failure of the owners to obtain proper materials regarding the operation and maintenance of the engine.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The sport pilot reported that the takeoff in the experimental, amateur-built gyroplane was normal; however, while continuing to climb through 500 ft above ground level, the aircraft stopped climbing and started to descend. The pilot-rated passenger reported hearing a decrease in engine power, but the engine continued to operate. The pilot started to turn back to the airport, then chose to land in a field. He saw a powerline and he turned sharply; the gyroplane hit the powerline then fell and impacted the side of a ditch. The gyroplane kit manufacturer installed a turbocharged, 135-hp Rotax 912 ULST that was modified from the 100-hp Rotax 912 ULS engine. During a postaccident examination, the engine started without hesitation and was run at idle power, but only for a brief time, since the propeller was broken. The brother of the accident pilot, who was a co-owner of the aircraft, reported that the engine had a history of not developing full power. He stated that the engine would develop about 3,500 rpm instead of developing full power at 5,200 to 5,300 rpm. On numerous occasions, he adjusted the manifold pressure probe by trial and error to get the engine to develop full power. The engine would operate properly, then the problem would reoccur, and he would repeat the process. The gyroplane had operated successfully for 7.9 hours since the last time the engine had not produced full power until the time of the accident. The owners reported that they did not understand the operation of the turbocharged engine or its associated components, and that the kit manufacturer did not provide operating manuals that explained the operation of the gyroplane or its turbocharged engine.

Quoted verbatim from the NTSB record.