N656BN - 2018 WILLIAM E MCCLAIN CH750 CRUZER - Complete Aircraft History & Registry Information

Quick Facts & Current Owner

Current Owner
MCCLAIN WILLIAM E
Location
ACWORTH, Georgia
Registration Status
Active until 02-28-2021
Serial Number
C75-10639
Last Seen on Market
Never Listed
Last Seen Airborne
No Recent Activity
Last FAA Action Date
February 2018
Owned Since
February 2018
Location of N656BN in ACWORTH, Georgia

About the WILLIAM E MCCLAIN CH750 CRUZER

The Zenith Aircraft Company STOL CH701 is a versatile and robust light-sport aircraft that has gained recognition in the general aviation community for its Short Takeoff and Landing (STOL) capabilities. Designed by aeronautical engineer Chris Heintz, the CH701 was introduced to the market in 1986 as part of Zenith Aircraft Company's mission to offer efficient, user-friendly, and affordable aircraft to aviation enthusiasts and private pilots worldwide.

The motivation for the production of the STOL CH701 stemmed from the need for an aircraft that could operate efficiently in rugged and remote areas, with limited runway facilities. STOL capabilities are critical for operations in backcountry, bush flying, and agricultural aviation, where runways are often short and unprepared. The CH701 fits perfectly into this niche, boasting a design that allows it to take off and land in minimal distances, thanks to features such as full-span leading-edge slats, large flaperons, and a high-lift wing with vortex generators.

Key Features and Capabilities

One of the key benefits of the Zenith CH701 is its versatility and adaptability. The aircraft is available in both kit form and ready-to-fly configurations, making it a popular choice for homebuilders and DIY enthusiasts. The construction of the CH701 is straightforward, requiring minimal tools and mechanical knowledge, thereby democratizing access to aviation, which aligns with Zenith’s broader vision of creating accessible aircraft.

The CH701’s robust all-metal construction and simplicity contribute to its reliability and ease of maintenance. It is powered by a variety of engines, typically in the 80-110 horsepower range, with the Rotax 912 being a popular choice due to its efficiency and reliability.

Market Position and Use Cases

Throughout its production history, the Zenith CH701 has been praised for its ruggedness, reliability, and STOL performance. It remains a favored choice among bush pilots, hobbyists, and those in need of a reliable and versatile aircraft for short-field operations. The aircraft's enduring popularity is a testament to its innovative design and the continued demand for accessible, high-performance STOL aircraft.



Flight History and Activity for N656BN

No flight activity has been observed for this aircraft since 2022.

This could indicate the aircraft is in storage, undergoing maintenance, or operating in areas without flight tracking coverage.

Maintenance and Safety Records

Safety Record Summary

  • 1 accident/incident report(s) on file

Accident and Incident Reports

September 10, 2020 - Boaz, Alabama

Damage Level
Substantial
Description
On the day of the accident, the non-instrument-rated pilot was flying a "test run" for a multi-stop cross-country flight that he planned to conduct a few days later. Before the flight, he topped off the fuel tanks in the airplane. During the flight, the pilot sent a text message to a family member stating that he was on his way back to the departure airport. Radar and automatic dependent surveillance-broadcast data during the return portion of the flight showed that the pilot was flying at an altitude between about 2,500 and 5,400 ft mean sea level (msl). Before radar contact was lost, the airplane had descended through 2,325 ft msl (about 1,400 feet above the ground [agl]), and its groundspeed had slowed from about 70 to about 40 knots. Its descent rate was about 500 ft per minute. The airplane subsequently impacted trees and terrain in a heavily wooded area. The accident site was approximately in line with the airplane’s previously recorded ground track, about 1.7 nautical miles ahead of the last radar-recorded position. Examination of the accident site and wreckage revealed that there was no discernable wreckage path horizontally through the trees and that the airplane impacted the ground in a nose-down attitude of about 45°. The relatively intact condition of the wreckage and lack of wreckage path suggested that the airplane was in a low energy state with little forward velocity when it impacted the trees. The wreckage examination also showed that adequate fuel remained onboard and that the engine displayed no evidence of any preimpact malfunction or failure that would have precluded normal operation. The pilot had obtained a weather briefing during the evening before the accident flight. No instrument flight rules conditions or other restrictions to visibility were forecast. Graphical forecasts for aviation indicated few to scattered clouds at 3,500 to 4,500 ft msl about the time of the accident. The weather forecasts that the accident pilot received reflected the weather conditions during the flight, and the weather information was issued in sufficient time for the accident pilot to be aware of the expected conditions. The low and mid-level troughs in the area helped to induce cloud cover near the accident site. Automated weather observing system information from multiple reporting stations indicated that the lowest cloud ceiling was about 2,000 ft agl with cloud layers through 4,000 ft agl. Pilot reports indicated cloud ceilings as low as 1,600 ft agl around the time of the accident. Weather satellite information and pilot reports also indicated that the cloud tops were between 4,500 and 6,000 ft msl. Thus, when the pilot remained below 2,000 ft agl, the flight would have been in visual meteorological conditions (VMC). However, when the pilot operated the airplane between 2,700 and 6,000 ft msl, the flight would have encountered instrument meteorological conditions at times. The airplane’s varying altitudes (between about 2,500 and 5,400 ft msl) were likely the result of the pilot trying to remain in VMC. Autopsy results showed that the pilot had some atherosclerosis of one coronary artery identified. Because no evidence showed that an acute cardiac event occurred during the flight, the pilot’s cardiovascular medical condition was not likely a factor in the accident. A low level of ethanol and N-propanol were detected in the pilot’s blood; however, the ethanol was likely from sources other than ingestion and was not a factor in the accident. Given all of the available information, it is likely that at some point during the return leg of the flight, the pilot encountered clouds and was attempting to remain clear of them based on the observed weather conditions and the airplane’s flight path. Shortly before the accident occurred the airplane was descending and slowing. The low energy state of the wreckage suggest that the pilot may have stalled the airplane while at an altitude too low to recover, which resulted in the subsequent collision with trees and terrain.

Complete History Timeline

⚠️

Sep 2020

Accident/Incident

Accident with substantial damage




📋

Feb 2018

Registration

Registered to MCCLAIN WILLIAM E in ACWORTH, GA




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Frequently Asked Questions

Who owns N656BN?

N656BN is currently registered to MCCLAIN WILLIAM E in ACWORTH, Georgia.

What type of aircraft is N656BN?

N656BN is a 2018 WILLIAM E MCCLAIN CH750 CRUZER with serial number C75-10639.

Has N656BN been in any accidents?

Yes, N656BN has 1 accident/incident report(s) on file with the FAA/NTSB.