# Commission Regulation (EU) No 748/2012 of 3 August 2012 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations (recast) (Text with EEA relevance), Division 21.A.65: Continuing structural integrity for aeroplane structures

Extent: E+W+S+N.I.

The holder of the type-certificate or restricted type-certificate for a large aeroplane must ensure that the continuing structural integrity programme remains valid throughout the operational life of the aeroplane, taking into account service experiences and current operations.

---
Source: https://www.legislation.gov.uk/eur/2012/748/annex/I/section/A/division/subpart+b/division/21.a.65 (the official version)
Page: https://openlegislation.uk/eu-regulation-2012-748/annex-I/section-A/division-subpart+b/division-21.a.65
Contains public sector information licensed under the Open Government Licence v3.0. Source: legislation.gov.uk, The National Archives.