CS 27.1325 Static
pressure systems
ED Decision 2003/15/RM
(a) Each instrument with static air case connections must be vented so that the influence of rotorcraft speed, the opening and closing of windows, airflow variation, and moisture or other foreign matter does not seriously affect its accuracy.
(b) Each static pressure port must be designed and located in such a manner that the correlation between air pressure in the static pressure system and true ambient atmospheric static pressure is not altered when the rotorcraft encounters icing conditions. An anti-icing means or an alternate source of static pressure may be used in showing compliance with this requirement. If the reading of the altimeter, when on the alternate static pressure system, differs from the reading of the altimeter when on the primary static system by more than 15 m (50 feet), a correction card must be provided for the alternate static system.
(c) Except as provided in sub-paragraph (d), if the static pressure system incorporates both a primary and an alternate static pressure source, the means for selecting one or the other source must be designed so that:
(1) When either source is selected, the other is blocked off, and
(2) Both sources cannot be blocked off simultaneously.
(d) For unpressurised rotorcraft, sub-paragraph (c)(1) does not apply if it can be demonstrated that the static pressure system calibration, when either static pressure source is selected is not changed by the other static pressure source being open or blocked.
Rotorcraft static pressure systems must ensure accurate instrument readings, unaffected by speed, airflow, or icing. Alternate static sources require correction cards if altitude differs significantly. Systems with primary/alternate sources must prevent simultaneous blockage, unless demonstrated otherwise for unpressurized rotorcraft, ensuring calibration is maintained.
* Summary by Aviation.Bot - Always consult the original document for the most accurate information.
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