Aircraft Description
N6622G is a Cessna 150L, a single-engine reciprocating (piston) aircraft registered to Sky High Adventures LLC in Wilmington, DE. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on September 2, 1970. The registration certificate was issued on March 16, 2019. The registration is set to expire on March 31, 2029. Powered by a Cont Motor 0-200 SERIES engine producing 100 horsepower, N6622G is. The aircraft's Mode S transponder code is A8BE4C (hex), used for ADS-B identification and flight tracking. The FAA registry record for N6622G was last updated on July 22, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Cessna A150 Aerobat was a specialized aerobatic trainer variant of the popular Cessna 150, designed to democratize aerobatic instruction for civilian pilots. First flown in prototype form on September 12, 1957, it was a high-wing, single-engine monoplane that seated two occupants and featured structural reinforcements for +6/-3G aerobatic maneuvers. With a wingspan of 32 feet 9 inches and powered by a 100-horsepower Continental O-200 engine, the aircraft served flight schools worldwide from 1969 to 1977. The A150 Aerobat was manufactured by Cessna Aircraft Company of Wichita, Kansas. AviatorDB tracks 80,556 Cessna aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is C150.
AviatorDB has found no NTSB accident or incident reports involving N6622G. 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 |
|---|---|---|---|---|
| Jun 28, 2016 | CEN16LA236 | Substantial | Fatal | The pilot’s disregard of the banner-tow operator's policy regarding the maximum allowable flight duration, which resulted in a total loss of engine power due to fuel exhaustion. |
| Feb 12, 2011 | CEN11LA182 | Substantial | None | The loss of preload torque on a connecting rod nut and bolt, which precipitated a separation of the connecting rod from the engine's crankshaft and resulted in the total loss of engine power. |
The pilot’s disregard of the banner-tow operator's policy regarding the maximum allowable flight duration, which resulted in a total loss of engine power due to fuel exhaustion.
The loss of preload torque on a connecting rod nut and bolt, which precipitated a separation of the connecting rod from the engine's crankshaft and resulted in the total loss of engine power.
Additional Details
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC