Loss of Control in Flight · NTSB CEN16FA122

REMOS ACFT GMBH FLUGZEUGBAU REMOS GX — Española, NM

2 fatal Low-time pilot
DateMarch 11, 2016
LocationEspañola, NM
AircraftREMOS ACFT GMBH FLUGZEUGBAU REMOS GX
Purpose of flightPersonal
ConditionsDay · Visual Meteorological Cond
Phase / occurrenceUncontrolled descent Collision with terr/obj (non-CFIT)
Pilot age46
Pilot total time133 hrs · Low time
Time in type127 hrs
Fatalities2

Probable cause

The pilot's failure to maintain adequate airspeed while operating in the airport traffic pattern, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall at a low altitude.

NTSB findings

  • Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
  • Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Angle of attack-Not attained/maintained - C

What happened

The private pilot was conducting a personal flight in the airport traffic pattern. A witness reported seeing the single-engine airplane enter left traffic for runway 16 and land. The airplane then made a second takeoff and continued to make left turns. The witness reported that, while airplane was turning from the crosswind leg to the downwind leg, he heard a reduction in engine power and saw the airplane descend toward the ground. Another witness reported that he heard the airplane takeoff from the airport and then saw the airplane make a left turn. He stated that, while the airplane was in the left turn, it pitched nose-down and descended toward the ground. The witness also noted that the airplane's engine sounded normal during the flight.

A postaccident examination established that the airplane had impacted the ground in a nose-low attitude and was destroyed by impact and postimpact fire damage. The examination did not reveal any anomalies that would have precluded normal operation of the airplane during the flight. Based on the witness descriptions and the impact geometry, it is likely that the pilot did not maintain adequate airspeed during the left turn, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall at a low altitude.

An editorial "what led to it / how to avoid it" analysis for this accident is generated separately and will appear here.

View the official NTSB docket →