Pilot Debrief

AERONCA 7BCM near Eureka Springs, AR — 2018-06-14

Final reportCEN18LA223
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Date
2018-06-14
Location
Eureka Springs, AR, USA
Airport
55AR
Aircraft
AERONCA 7BCM
Registration
N9098C
Category
Airplane
Highest injury
Serious
Fatalities
0
Phase of flight
Initial climb

Probable cause

The pilot’s failure to maintain adequate airspeed following a partial loss of engine power after takeoff for undetermined reasons, which resulted in the airplane exceeding its critical angle of attack and an aerodynamic stall at a low altitude.

NTSB narrative

The pilot was conducting his first flight in the airplane that he purchased earlier the same day. The pilot stated that he did not identify any anomalies during his preflight inspection of the airplane and that the fuel tank had been topped-off before the flight. He reported that the engine started normally and that he observed no anomalies during two separate engine run-ups that he completed before takeoff. He noted that he verified full engine speed, checked proper operation of both magnetos, and cycled the carburetor heat control during both engine run-ups. The pilot reported that after an uneventful takeoff, about 200 ft above ground level, the engine suddenly lost power. The pilot stated that the engine was partially running but was unable to produce enough thrust to sustain level flight. The pilot decided to return to the airport due to heavily wooded terrain ahead of the airplane's position. The pilot stated that he rolled the airplane into a steep left turn, and about halfway through the 180° turn, the airplane entered an aerodynamic stall at a low altitude. The pilot reported that the airplane impacted terrain in a left-wing-down, nose-down attitude. The forward fuselage, outboard left wing, and both wing struts sustained substantial damage during impact. A postaccident wreckage examination did not reveal any evidence of mechanical malfunction that would have precluded normal operation of the airplane or its engine during the flight. The fuel samples collected after the accident were free of contamination. The cause of the partial loss of engine power could not be determined with the available evidence. It is likely that when the pilot turned back to the airport after the engine lost partial power, he did not maintain adequate airspeed and exceeded the airplane’s critical angle of attack, which resulted in an aerodynamic stall. A review of available maintenance documentation revealed that the airplane did not have a current annual inspection. The pilot, who also held an aviation mechanic certificate with inspector authorization, did not apply for a ferry flight permit before the flight.

Analysis

Primary failure mode
Engine power loss
First missed decision gate
Pilot could have applied for a ferry flight permit before the flight.

NTSB coding

Evidence available

  • Photos
  • 8 docket documents
View NTSB final reportView NTSB docket

Docket documents8

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