Light
Dark
System
Log In
Loading...
Compare / EASA/
Incorporated Amendments
/
Compare & Highlight Differences
CS 29.723 Shock absorption tests
Available versions for ERULES-1963177438-5622
ED Decision 2003/16/RM
found in: CS-29 Amdt 10 - Large Rotercraft (Jan 2023)
From
CS-29 Amdt 12 - La... (Mar 2026)
CS-29 Amdt 11 - La... (Feb 2023)
CS-29 Amdt 10 - La... (Jan 2023)
From section
To
CS-29 Amdt 12 - La... (Mar 2026)
CS-29 Amdt 11 - La... (Feb 2023)
CS-29 Amdt 10 - La... (Jan 2023)
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
CS 29.723 Shock absorption tests ED Decision 2003/16/RM The landing inertia load factor and the reserve energy absorption capacity of the landing gear must be substantiated by the tests prescribed in [CS 29.725](#_DxCrossRefBm1513259428) and [29.727](#_DxCrossRefBm1513259427), respectively. These tests must be conducted on the complete rotorcraft or on units consisting of wheel, tyre, and shock absorber in their proper relation.
CS 29.723 Shock absorption tests ED Decision 2003/16/RM The landing inertia load factor and the reserve energy absorption capacity of the landing gear must be substantiated by the tests prescribed in [CS 29.725](#_DxCrossRefBm1178331821) and [29.727](#_DxCrossRefBm1178331820), respectively. These tests must be conducted on the complete rotorcraft or on units consisting of wheel, tyre, and shock absorber in their proper relation.
#### CS 29.723 Shock absorption tests *ED Decision 2003/16/RM* The landing inertia load factor and the reserve energy absorption capacity of the landing gear must be substantiated by the tests prescribed in [CS 29.725](#_DxCrossRefBm1685772286) and [29.727](#_DxCrossRefBm1685772285), respectively. These tests must be conducted on the complete rotorcraft or on units consisting of wheel, tyre, and shock absorber in their proper relation.