structural limitations
Posted: Fri Nov 25, 2022 3:13 pm
Below is an excerpt from a British aviation magazine reporter's impressions of the Sonex. The comment is provocative. My familiarity with the Sonex is not sufficient to assess the validity of the information presented. Comments would be appreciated.
Pilot Magazine (Britain)
Flight test: Sonex Aircraft LLC Sonex
PUBLISHED: 17:31 11 June 2018
However, if you plan on cruising this fast it’d better be smooth, because Va and Vno (design manoeuvring speed and structural speed) are the same at 109kt IAS. In fact, the relatively light weight (even when operating at the Utility max weight) and low wing loading mean that cruising at the sort of speeds the Sonex can achieve requires a pilot to be quite circumspect if there’s any possibility of turbulence.
Pilot Magazine (Britain)
Flight test: Sonex Aircraft LLC Sonex
PUBLISHED: 17:31 11 June 2018
However, if you plan on cruising this fast it’d better be smooth, because Va and Vno (design manoeuvring speed and structural speed) are the same at 109kt IAS. In fact, the relatively light weight (even when operating at the Utility max weight) and low wing loading mean that cruising at the sort of speeds the Sonex can achieve requires a pilot to be quite circumspect if there’s any possibility of turbulence.