The complete common-error interface passes

All 19 controls pass: twelve known-answer affine systems and seven rejection controls. The future ranges agree with the independent calculation under exact and noisy training constraints, at zero/nonzero centers and on each coordinate axis. Both common-error blocks must have the correct binding. Every physical and all 15 auxiliary coordinates remain, including unidentified directions.

This qualifies the supplied 42-column interface. It does not by itself establish a narrower native prediction or actual aircraft coverage. The native candidate has separately passed its 24 controls. The next complete orientation comparison tests their combined usefulness on the same inputs and physical bounds as the earlier runs.

No native evaluations, original recordings, observed fits or protected ESA outcomes were used. The 53-stretch numerical result is unchanged.

Sealed results · Frozen scope · Native prerequisite · Roadmap.