SUBPART B — PISTON ENGINES: DESIGN AND CONSTRUCTION
Engines (CS-E) · CS-E
CS-E 210 Failure Analysis
(See AMC E 210) (a) A Failure analysis of the Engine, including the control system for a typical installation must be made to establish that no single…
AMC E 210 Failure Analysis
The Failure analysis would normally include investigation of those Engine components that could affect the functioning and integrity of the major…
CS-E 230 De-Icing and Anti-Icing Precautions
The design of the Engine induction system must be such as to minimise the risk of ice formation adversely affecting the functioning of the Engine and, if…
CS-E 240 Ignition
All spark-ignition Engines shall comply with the following: The Engine shall be equipped either with:
CS-E 250 Fuel System
Each fuel specification to be approved, including any additive, and the associated limitations in flow, temperature and pressure that ensure proper…
CS-E 260 Engine Cooling System
The design and construction of the Engine cooling system must ensure adequate cooling in all normal operating conditions within the flight envelope.
CS-E 270 Lubrication System
It shall not be possible for oil to drain into the Engine when it is not running, in such quantities as to introduce a risk of ‘hydraulicing’ or in any…
CS-E 290 Hand Turning
It must be possible to rotate the crankshaft in controlled slow motion.
Consolidated from the EASA Easy Access Rules (revision 7 Dec 2023, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.
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