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GM 21.A.33(d) Inspections and tests
Available versions for ERULES-1963177438-3684
ED Decision 2019/018/R
found in: Initial Airworthiness and Environmental Protection (748/2012) Part-21 Part-21L (Jul 2024)
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GM 21.A.33(d) Inspections and tests ED Decision 2019/018/R The applicant should inform EASA sufficiently in advance about the execution of inspections and tests that are used for compliance demonstration purposes unless EASA has explicitly excluded these inspections and tests from its involvement according to [21.B.100](#_DxCrossRefBm1649096973). Additionally, the applicant may propose to EASA to perform or witness flight or other tests of particular aspects of the product during its development and before the type design is fully defined. However, before EASA performs or witnesses any flight test, the applicant should have performed these tests already before EASA and should ensure that no features of the product preclude the safe conduct of the evaluation requested. EASA may require any such tests to be repeated once the type design is fully defined to ensure that subsequent changes have not adversely affected the conclusions from any earlier evaluation. A statement of conformity as per point [21.A.33](#_DxCrossRefBm1649096983)(c) is also required for the above tests.
##### GM 21.A.33(d) Inspections and tests *ED Decision 2019/018/R* The applicant should inform EASA sufficiently in advance about the execution of inspections and tests that are used for compliance demonstration purposes unless EASA has explicitly excluded these inspections and tests from its involvement according to [21.B.100](#_DxCrossRefBm485230464). Additionally, the applicant may propose to EASA to perform or witness flight or other tests of particular aspects of the product during its development and before the type design is fully defined. However, before EASA performs or witnesses any flight test, the applicant should have performed these tests already before EASA and should ensure that no features of the product preclude the safe conduct of the evaluation requested. EASA may require any such tests to be repeated once the type design is fully defined to ensure that subsequent changes have not adversely affected the conclusions from any earlier evaluation. A statement of conformity as per point [21.A.33](#_DxCrossRefBm485230474)(c) is also required for the above tests.