NTSB CAROL · Event
Event ERA13CA283
Registry · N7057H
FAA Aircraft Registry record.
Make / Model
PIPER J3C-65
Seats / Engines
2 seats · 1 engine
ADS-B equipped
Yes — Mode-S A96A76
Registrant of record
CALVERT JARED C
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s inadequate planning which resulted in an encounter with settling with power and descent into terrain during takeoff.
Factual narrative
The pilot was attempting to reposition the helicopter from an off-airport site in advance of an approaching storm. Following an uneventful preflight inspection and engine start, the pilot climbed the helicopter into a hover and turned toward his intended departure path. He then pushed the cyclic control forward and increased the collective pitch in order to clear some approaching trees. The pilot then realized that “appropriate power” was not available, and turned right in order to avoid the trees. The helicopter subsequently settled with power and impacted the brush below, resulting in substantial damage to the airframe. The pilot reported that there were no pre-impact mechanical malfunctions or failures of the helicopter, nor were any discovered during a postaccident examination of the airframe and engine conducted by a Federal Aviation Administration Inspector. The pilot additionally stated that the accident could have been prevented with “better situational awareness.” The pilot was attempting to reposition the helicopter from an off-airport site in advance of an approaching storm. Following an uneventful preflight inspection and engine start, the pilot climbed the helicopter into a hover and turned toward his intended departure path. He then pushed the cyclic control forward and increased the collective pitch in order to clear some approaching trees. The pilot then realized that “appropriate power” was not available, and turned right in order to avoid the trees. The helicopter subsequently settled with power and impacted the brush below, resulting in substantial damage to the airframe. The pilot reported that there were no pre-impact mechanical malfunctions or failures of the helicopter, nor were any discovered during a postaccident examination of the airframe and engine. The pilot additionally stated that the accident could have been prevented with “better situational awareness.” Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2013_ERA13CA283.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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