Heat Flux Density 116 kW/m2 ± 10 kW/m2
Note: For materials this is considered to be equivalent to the capability of withstanding a fire at least as well as steel or titanium in dimensions appropriate for the purposes for which they are used.
(b)
‘Fire-resistant’ with respect to materials, components and equipment means the capability to withstand the application of heat by a flame, as defined for ‘Fireproof’, for a period of 5 minutes without any failure that would create a hazard to the aircraft.
Note: For materials this may be considered to be equivalent to the capability of withstanding a fire at least as well as aluminium alloy in dimensions appropriate for the purposes for which they are used.
(c)
Delete ‘Standard Flame’ and the definition on page 1–9 for JAR–1.
JOINT AVIATION REQUIREMENTS 12 December 1997
JAR–1
AMENDMENT 1/97/1
The requirements and other material contained in this Orange Paper Amendment 1/97/1 have been accepted by the Joint Aviation Authorities Committee for inclusion in JAR–1 and become effective on the date printed on these sheets.
Amendment 1/97/1 consists of the following:–
NPA 1–8
Editorial corrections
This Amendment 1/97/1 will be incorporated into Change 6 to JAR–1 at a future date.
Each of the pages of this Amendment has been given a number prefixed by ‘(OP)’, denoting ‘Orange Paper’. The orange pages should be inserted between the text pages of JAR–1 in the positions indicated below, but the pages in JAR–1 bearing the corresponding numbers should not be removed.
The orange pages to be inserted into JAR–1 (at Change 5) are:–
Section 1
(OP) P–4/1–1 between pages P–4/1–1
(OP) 1–2/1–3 between pages 1–2/1–3
(OP) 1–4/1–5 between pages 1–4/1–5
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