N2812 - 2001 Chicco Miguel E Quicksilver Sport II Aircraft Registration
SBM32001 CHICCO MIGUEL E QUICKSILVER SPORT II
Aircraft Description
N2812 is a 2001 Chicco Miguel E QUICKSILVER SPORT II, a single-engine two-cycle piston aircraft registered to Sky Knights Flight Club in Thousand Oaks, CA. This aircraft holds a experimental airworthiness certificate issued by the Federal Aviation Administration on January 25, 2010. The registration certificate was issued on September 26, 2013. The registration is set to expire on September 30, 2029. Powered by a Rotax 503 DCDI engine producing 52 horsepower, N2812 is. The aircraft's Mode S transponder code is A2D450 (hex), used for ADS-B identification and flight tracking. N2812 was last tracked by AviatorDB at coordinates 31.9727, 35.9916 on June 30, 2025. The FAA registry record for N2812 was last updated on September 2, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
Chicco Miguel E is an aircraft manufacturer with aircraft registered in the FAA database tracked by AviatorDB. AviatorDB tracks 1 Chicco Miguel E aircraft currently registered in the FAA database, including the QUICKSILVER SPORT II model.
AviatorDB has found no NTSB accident or incident reports involving N2812. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (2)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Jul 8, 2017 | WPR17FA146 | Unknown | Fatal | A partial loss of engine power for reasons that could not be determined during postaccident examination in combination with the low cruise altitude selected by the pilots, which resulted in an ocean ditching. The lack of personal flotation devices likely contributed to the drowning of one of the pilots. |
| Jun 29, 2013 | WPR13LA318 | Substantial | Serious | The partial loss of engine power while maneuvering due to the blockage of the exhaust system by broken internal engine baffles that had shifted during the flight, which resulted in a forced landing and subsequent impact with terrain. |
A partial loss of engine power for reasons that could not be determined during postaccident examination in combination with the low cruise altitude selected by the pilots, which resulted in an ocean ditching. The lack of personal flotation devices likely contributed to the drowning of one of the pilots.
The partial loss of engine power while maneuvering due to the blockage of the exhaust system by broken internal engine baffles that had shifted during the flight, which resulted in a forced landing and subsequent impact with terrain.
Additional Details
Last Known Position
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC