Although no major problems were encountered during the initial testing phase, some minor issues with the landing gear and flight control system had to be rectified. The former problem was partly due to the tandem main landing gear being very narrow, in order to fit into the wings; the leg shortened in length and rotated as it was stowed. During one landing incident, the chain mechanism (used to shorten the gear) in the Mark 1 gear jammed, resulting in incomplete rotation. In a second incident with Arrow 202 on 11 November 1958, the flight control system commanded elevons full down at landing; the resulting reduction in weight on the gears reduced the effective tire friction, ultimately resulting in brake lockup and subsequent gear collapse. A photograph taken of the incident proved that inadvertent flight control activation had caused the accident. The only occasion when a test flight was diverted occurred on 2 February 1959, when a TCA Viscount crash-landed in Toronto, necessitating a landing at CFB Trenton.