CS 25.941 Inlet, engine, and exhaust compatibility
ED
Decision 2007/010/R
For
aeroplanes using variable inlet or exhaust system geometry, or both –
(a) The system comprised of the inlet, engine
(including thrust augmentation systems, if incorporated), and exhaust must be
shown to function properly under all operating conditions for which approval
is sought, including all engine rotating speeds and power settings, and engine
inlet and exhaust configurations;
(b) The dynamic effects of the operation of
these (including consideration of probable malfunctions) upon the aerodynamic
control of the aeroplane may not result in any condition that would require
exceptional skill, alertness, or strength on the part of the pilot to avoid
exceeding an operational or structural limitation of the aeroplane; and
(c) In showing compliance with sub-paragraph
(b) of this paragraph, the pilot strength required may not exceed the limits
set forth in CS 25.143(d) subject to the conditions set forth in
sub-paragraphs (e) and (f) of CS 25.143.
[Amdt
25/3]
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