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21.A.90C Stand-alone changes to the Instructions for Continued Airworthiness
Available versions for ERULES-1963177438-18952
Regulation (EU) 2021/699
found in: Initial Airworthiness and Environmental Protection (748/2012) Part-21 Part-21L (Jul 2024)
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21.A.90C Stand-alone changes to the Instructions for Continued Airworthiness Regulation (EU) 2021/699 (a) Stand-alone changes to the instructions for continued airworthiness are changes that are not directly prepared as a result of a change to the type design or repair design. (b) Stand-alone changes to the instructions for continued airworthiness can only be made by the holder of the design approval for which those instructions have been established. (c) Points [21.A.91](#_DxCrossRefBm1649096897) to [21.A.109](#_DxCrossRefBm1649097032) shall not apply to stand-alone changes to the instructions for continued airworthiness that: 1. do not affect the airworthiness limitations section of the instructions for continued airworthiness, and 2. do not require the design approval holder to perform any additional demonstration of compliance with the certification basis. (d) Stand-alone changes to the instructions for continued airworthiness referred to in point (c) shall be approved by the design approval holder under procedures agreed with the Agency.
#### 21.A.90C Stand-alone changes to the Instructions for Continued Airworthiness *Regulation (EU) 2021/699* (a) Stand-alone changes to the instructions for continued airworthiness are changes that are not directly prepared as a result of a change to the type design or repair design. (b) Stand-alone changes to the instructions for continued airworthiness can only be made by the holder of the design approval for which those instructions have been established. (c) Points [21.A.91](#_DxCrossRefBm485230388) to [21.A.109](#_DxCrossRefBm485230523) shall not apply to stand-alone changes to the instructions for continued airworthiness that: 1. do not affect the airworthiness limitations section of the instructions for continued airworthiness, and 2. do not require the design approval holder to perform any additional demonstration of compliance with the certification basis. (d) Stand-alone changes to the instructions for continued airworthiness referred to in point (c) shall be approved by the design approval holder under procedures agreed with the Agency.