VT35 is an active CAAC type-certification project in certification-basis definition and continued flight-test/design work. The CAAC approvals held by the separate EH216-S model do not apply to VT35.
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VT35
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Distributed lift propulsion and autonomous flight-control architecture; detailed certification-level redundancy evidence is not yet public.
Battery, control and cabin overlays communicate system context only; exact internal placement is not asserted.
Exact inverter installation, pack geometry, structural internals and certification-level electrical partitioning are omitted.