NTSB CAROL · Event
Event GAA18CA377
Registry · N963CG
FAA Aircraft Registry record.
Make / Model
JONKER SAILPLANES (PTY) LTD JS1-C
Year of manufacture
2014 · 4 years old at event
Engine
NONE NONE
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20150226
ADS-B equipped
Yes — Mode-S AD6784
Registrant of record
GILLESPIE CHARLES P
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s inability to maintain altitude and his delayed decision to deploy the powered-glider’s engine, which necessitated an off-airport landing.
Factual narrative
The powered-glider pilot reported that, during the return flight to the airport, after an informal glider competition, about 10,000 to 11,000 ft over mountainous terrain, he was unable to find lift, the glider descended to 9,000 ft, and he started the sustainer engine. He added that, after the glider climbed back to the initial altitude, he shut the sustainer engine off, stowed it, and continued to the destination airport. He reported that, about 4 miles from the airport, the glider began a sink rate of about 1,000 ft per minute. He attempted to restart the engine but was unsuccessful in the limited time. He selected a field for an off airport landing, the glider touched down, but the ground was slightly uneven, which resulted in the right wing dragging. The glider veered 20° to the right before coming to rest. The glider sustained substantial damage to the horizontal stabilizer and elevator. The pilot reported that there were no preaccident mechanical failures or malfunctions with the glider that would have precluded normal operation. An automated weather observation station, elevation 7,950 ft, located about 14 miles east-southeast of the accident location, reported the wind was 270° at 10 knots, gusting to 15 knots, temperature 79° F, and dew point 9° F. The calculated density altitude was 10,300 ft. The powered-glider pilot reported that, during the return flight to the airport after an informal glider competition, about 10,000 to 11,000 ft over mountainous terrain, he was unable to find lift, the glider descended to 9,000 ft, and he started the sustainer engine. He added that, after the glider climbed back to the initial altitude, he shut the sustainer engine off, stowed it, and continued to the destination airport. He reported that, about 4 miles from the airport, the glider began to sink about 1,000 ft per minute. He attempted to restart the engine but was unsuccessful in the limited time available. He chose a field for an off-airport landing, the glider touched down, but the ground was slightly uneven, which resulted in the right wing dragging. The glider veered 20° to the right before coming to rest. The glider sustained substantial damage to the horizontal stabilizer and elevator. The pilot reported that there were no preaccident mechanical failures or malfunctions with the glider that would have precluded normal operation. An automated weather observation station at an elevation of 7,950 ft, located about 14 miles east-southeast of the accident location, reported wind from 270° at 10 knots, gusting to 15 knots; temperature 79°F; and dew point 9F. The calculated density altitude was 10,300 ft. 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 Environmental issues-Conditions/weather/phenomena-Temp/humidity/pressure-Thermal lifting-Effect on operation - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Attain/maintain not possible - C
- C Environmental issues-Physical environment-Terrain-Sloped/uneven terrain-Effect on operation - C
Verbatim from NTSB's published report. Source file
NTSB_2018_GAA18CA377.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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