Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
21L.B.62 Initial oversight investigation
Available versions for ERULES-1963177438-21302
Regulation (EU) 2022/1358
found in: Initial Airworthiness and Environmental Protection (748/2012) Part-21 Part-21L (Jul 2024)
From
Initial Airworthin... (Nov 2025)
Initial Airworthin... (Jul 2024)
From section
To
Initial Airworthin... (Nov 2025)
Initial Airworthin... (Jul 2024)
To section
No visible text changes
0 removals
0 additions
View
Rich
Plain
Sync scrolling
Share
From
Show details
Hide details
To
Show details
Hide details
Version
Show side by side
21L.B.62 Initial oversight investigation Regulation (EU) 2022/1358 (a)    Upon receiving a declaration of design compliance, the Agency shall verify that the aircraft is within the scope of [Subpart C](#_DxCrossRefBm1649097830) of Section A of this Annex and that the declaration contains all the information specified in point [21L.A.43](#_DxCrossRefBm1649097270). The Agency shall acknowledge the receipt of the declaration, including the assignment of an individual declaration of design compliance reference number to the declarant for that aircraft configuration. (b)    The Agency shall conduct a physical inspection and assessment of the first article of that aircraft in the final configuration, taking into consideration the safety review carried out in accordance with point (a)(2) of point [21L.B.242](#_DxCrossRefBm1649097844). If the Agency finds evidence, in the declaration or through the physical inspection and assessment carried out in accordance with the first sentence, indicating that the aircraft could be incapable of conducting a safe flight or could be environmentally incompatible during in‑service operations, the Agency shall raise a finding in accordance with point [21L.B.21](#_DxCrossRefBm1649097779).
#### 21L.B.62 Initial oversight investigation *Regulation (EU) 2022/1358* (a) Upon receiving a declaration of design compliance, the Agency shall verify that the aircraft is within the scope of [Subpart C](#_DxCrossRefBm485231326) of Section A of this Annex and that the declaration contains all the information specified in point [21L.A.43](#_DxCrossRefBm485230761). The Agency shall acknowledge the receipt of the declaration, including the assignment of an individual declaration of design compliance reference number to the declarant for that aircraft configuration. (b) The Agency shall conduct a physical inspection and assessment of the first article of that aircraft in the final configuration, taking into consideration the safety review carried out in accordance with point (a)(2) of point [21L.B.242](#_DxCrossRefBm485231340). If the Agency finds evidence, in the declaration or through the physical inspection and assessment carried out in accordance with the first sentence, indicating that the aircraft could be incapable of conducting a safe flight or could be environmentally incompatible during in‑service operations, the Agency shall raise a finding in accordance with point [21L.B.21](#_DxCrossRefBm485231275).