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Atlas / NTSB / WPR21LA052

NTSB CAROL · Event

Event WPR21LA052

2020-11-11 Fallbrook, California, United States Airport · L18 Minor 1 aircraft Status: Completed

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 ↗.