CS 23.2525 System power generation, storage, and distribution

ASTM F44 F3264 Standard Specification for Normal Category Aeroplanes Certification

9.6 System Power Generation, Storage, and Distribution F3061/F3061M-24a Standard Specification for Systems and Equipment in Small Aircraft F3231/F3231M-24 Standard Specification for Electrical Systems for Aircraft with Combustion Engine Electrical Power Generation F2490-20 Standard Guide for Aircraft Electrical Load and Power Source Capacity Analysis F3233/F3233M-23b Standard Specification for Flight and Navigation Instrumentation in Aircraft F3117/F3117M-24a Standard Specification for Crew Interface in Aircraft F3120/F3120M-20 Standard Specification for Ice Protection for General Aviation Aircraft

Remarks ASTM F44 published standards for showing compliance for electrical systems that are installed on aeroplanes with electric or hybrid-electric propulsion systems. EASA has not yet accepted F3316-19; 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]

CS-23 Amdt 4

23.1303 Flight and navigation instruments

23.1331(b), (c) Instruments using a power source

23.1351(a), (b), (c) Electrical Systems – General

23.1353 Storage battery design and installation

23.1357 Circuit protective devices

Remarks At variance with CS 23.1357(b) and (d), EASA does not accept a protective device for a circuit essential to flight safety in designs applications after the date of entry into force of the AMC & GM to CS-23 Issue 4; automatic fuses or circuit breakers should be used instead.

CS-VLA Amdt 1 VLA 1303 Flight and navigation instruments VLA 1331 Instruments using a power supply VLA 1351 Electrical Systems – General VLA 1353 Storage battery design and installation VLA 1357 Circuit protective devices

Remarks At variance with CS-VLA 1357(b) and (d), EASA does not accept a protective device for a circuit essential to flight safety in designs applications after the date of entry into force of the AMC & GM to CS-23 Issue 4; automatic fuses or circuit breakers should be used instead.