Standard: RTCA DO-227

MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR LITHIUM BATTERIES

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Scope:

Contains both requirements and general guidelines regarding the design, testing, application, handling, storage, and disposal of lithium cells and batteries. It provides designers, manufacturers, and users of equipment installed in aircraft with information on the performance characteristics and operating and environmental limitations of lithium cells and batteries powering such equipment. Two categories of maximum cell and battery sizes are identified. Category I: Solid-cathode cells that contain less than 0.15 grams of lithium or lithium alloy, and batteries that use not more than four such cells. Category II: Liquid-cathode cells that contain less than 0.15 grams of lithium or lithium alloy, or batteries comprised of these cells. Cells that contain 0.15 to not more than 5 grams of lithium or lithium alloy. Batteries that contain not more than 25 grams lithium or lithium alloy. Cells containing more than 5 grams of lithium or lithium alloy, or batteries that contain more than 25 grams of lithium or lithium alloy are beyond the scope of this document. FAA Technical Standard Order (TSO) – C97 references this document.

Organization: RTCA, Inc.
Document Number: rtca do-227
Publish Date: 1995-01-01
Page Count: 91
Change Type: COMPLETE REVISION
Available Languages: EN
DOD Adopted: NO
ANSI Approved: NO
Most Recent Revision: YES
Current Version: YES
Status: Active

Standards That Reference This Standard

Showing 10 of 12.

EASA TOR RMT.0561
EASA NPA 2015-02
FAA 80 FR 30753
FAA 80 FR 31451
FAA 73 FR 70257
FAA 80 FR 49298
FAA 80 FR 77696
FAA 81 FR 23573
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