NTSB CAROL · Event
Event WPR21LA052
Registry · N57517
FAA Aircraft Registry record.
Make / Model
BELLANCA 7GCBC
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19730625
ADS-B equipped
Yes — Mode-S A76397
Registrant of record
DU AIRCRAFT LEASING
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A partial loss of engine power for reasons that could not be determined with the available evidence.
Factual narrative
On November 11, 2020, about 0950 Pacific standard time, a Bellanca 7GCBC, N57517 sustained substantial damage when it was involved in an accident near Fallbrook, California. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that, during the initial climb, between 400 and 600 ft above ground level, the engine started to sputter, and the airplane began to lose lift. The pilot declared an emergency and executed a forced landing back to the runway. The pilot stated that the landing was hard and fast with about 1/3 of the runway remaining. The pilot was unable to stop the airplane before it ran off the runway and down a 50-ft embankment. Both wings and lift struts were substantially damaged. A postaccident engine examination revealed that the fuel in the engine gascolator was free of contaminants and contained blue-colored fuel that smelled of avgas. The spark plugs displayed normal operating signatures. The oil filter was removed and cut open to reveal no evidence of metal fragments or shavings. The engine crankshaft was rotated by hand and accessory gear and valve train continuity was established. The examination of the engine revealed no evidence of any preaccident mechanical failures or malfunctions that would have precluded normal operation. The pilot reported that, during the initial takeoff climb, between 400 and 600 ft above ground level, the engine started to sputter, and the airplane began to lose lift. The pilot declared an emergency and executed a forced landing back to the runway. The airplane landed hard and fast with about 1/3 of the runway remaining. The pilot was unable to stop the airplane before it ran off the runway and down a 50-ft embankment. A postaccident engine examination revealed no evidence of any preaccident mechanical failures or malfunctions that would have precluded normal operation. The reason for the partial loss of engine power could not be determined with the available evidence. 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).
- — Not determined-Not determined-(general)-(general)-Unknown/Not determined
Verbatim from NTSB's published report. Source file
NTSB_2020_WPR21LA052.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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