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CS 23.2430 Powerplant installation, energy storage and distribution systems

Normal-Category Aeroplanes (CS-23) · CS-23 · EAR revision 13 May 2026

IRImplementing rule

CS 23.2430Powerplant installation, energy storage and distribution systems

(a)Each system must:

(1)Be designed to provide independence between multiple energy storage and supply systems so that a failure of any one component in one system will not result in the loss of energy storage or supply of another system.

(2)Be designed to prevent catastrophic events due to lightning strikes taking into account direct and indirect effects for aeroplanes where the exposure to lightning is likely.

(3)Provide energy to the powerplant installation with adequate margins to ensure safe functioning under all permitted and likely operating conditions, and accounting for likely component failures.

(4)Provide the information established in CS 23.2445(g) to the flight crew and provide uninterrupted supply of that energy when the system is correctly operated, accounting for likely energy fluctuations.

(5)Provide a means to safely remove or isolate the energy stored within the system.

(6)Be designed to retain the energy under all likely operating conditions and minimise hazards to the occupants during any survivable emergency landing. For Level-4 aeroplanes, failure due to overload of the landing system must be taken into account.

(7)Prevent hazardous contamination of the energy supplied to each powerplant installation.

(b)Each storage system must:

(1)withstand the loads under likely operating conditions without failure, accounting for installation;

(2)be isolated from personnel compartments and protected from likely hazards;

(3)be designed to prevent significant loss of stored energy due to energy transfer or venting under likely operating conditions;

(4)provide energy for at least one-half hour of operation at maximum continuous power or thrust; and

(5)be capable of jettisoning energy safely if this functionality is provided.

(c)Each energy-storage-refilling or -recharging system must be designed to:

(1)prevent improper refilling or recharging;

(2)prevent contamination of the stored energy during likely operating conditions; and

(3)prevent the occurrence of any hazard to the aeroplane or to persons during refilling or recharging.

(d)Likely errors during ground handling of the aeroplane must not lead to a hazardous loss of stored energy.

IR · CS 23.2430 — CS-23 · ED Decision 2023/002/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMCAcceptable means of compliance

AMC1 23.2430Powerplant installation, energy storage and distribution systems

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ASTM F44 F3264 Standard Specification for Normal Category Aeroplanes Certification

8.7 Fuel and Energy Storage and Distribution Systems F3062/F3062M-20 Standard Specification for Aircraft Powerplant Installation F3063/F3063M-21 Standard Specification for Aircraft Fuel Storage and Delivery F3064/F3064M-21 Standard Specification for Aircraft Powerplant Control, Operation, and Indication F3066/F3066M-18 Standard Specification for Aircraft Powerplant Installation Hazard Mitigation F3114-21 Standard Specification for Structures F3397/F3397M Standard Practice for Aeroplane Turbine Fuel System Hot Weather Operations

Remarks ASTM F44 published standards for showing compliance for electric propulsion systems. EASA has not yet accepted F3239-22a; however, EASA would take into consideration applications from applicants that use this standard as the basis for the development of their means of compliance subject to agreement with EASA. [AMC & GM to CS-23: Issue 4] [AMC & GM to CS-23: Issue 5]

AMC · AMC1 23.2430 — CS-23 · ED Decision 2026/003/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMCAcceptable means of compliance

AMC2 23.2430Powerplant installation, energy storage and distribution systems

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CS-23 Amdt 4

23.951 Fuel System - General

23.953 Fuel system independence

23.954 Fuel system lightning protection

23.955 Fuel flow

23.957 Flow between interconnected tanks

23.959 Unusable fuel supply

23.961 Fuel system hot weather operation

23.963(a), (d), (e) Fuel tank: general

23.965 Fuel tank tests

23.967(a), (c), (d), (e) Fuel tank installation

23.969 Fuel tank expansion space

23.971 Fuel tank sump

23.973 Fuel tank filler connection

23.975 Fuel tank vents and carburettor vapour vents

23.977 Fuel tank outlet

23.979 Pressure fuelling systems

23.991 Fuel pumps

23.993 Fuel system lines and fittings

23.994 Fuel system components

23.997(b), (d), (e) Fuel strainer or filter

23.999 Fuel system drains

23.1001(a) through (f) Fuel jettisoning system

23.1337(a) Powerplant instruments installation

23.721 Landing gear systems - General

Remarks Provisions of AMC2 cover only fuel systems

AMC · AMC2 23.2430 — CS-23 · ED Decision 2017/025/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMCAcceptable means of compliance

AMC3 23.2430Powerplant installation, energy storage and distribution systems

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CS VLA Amdt 1 VLA.951 Fuel System - General VLA.955 Fuel flow VLA.957 Flow between interconnected tanks VLA.959 Unusable fuel supply VLA.961 Fuel system hot weather operation VLA.963 Fuel tank: general VLA.965 Fuel tank tests VLA.967 Fuel tank installation VLA.969 Fuel tank expansion space VLA.971 Fuel tank sump VLA.973 Fuel tank filler connection VLA.975 Fuel tank vents and carburettor vapour vents VLA.977 Fuel strainer or filter VLA.991 Fuel pumps VLA.993 Fuel system lines and fittings VLA.999 Fuel system drains VLA.1337 Powerplant instruments

Remarks Provisions of AMC3 cover only fuel systems

AMC · AMC3 23.2430 — CS-23 · ED Decision 2017/025/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

All rules in SUBPART E — POWERPLANT INSTALLATION

Consolidated from the EASA Easy Access Rules (revision 13 May 2026, 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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