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PAGE INTENTIONALLY LEFT BLANK AMA Validity : S / N 1 - 9999 34 00 00Page 2 (BA) FEB 00 FLIGHT ENVIRONMENT DATA DESCRIPTION AND OPERATION 1. GENERAL This section describes the systems or instruments which sense the environmental conditions. The installation is composed of : - the air data systems, - the outside air temperature system. 2. DESCRIPTION A. Air data systems - refer to 34-11-00 This section describes the instruments which operate using static and / or dynamic data. B. Outside air temperature - refer to 34-13-00 This system indicates the outside air temperature. AAAA Validity : S / N 1 - 9999 34-10 00 (BA) FEB Page 1 00 PAGE INTENTIONALLY LEFT BLANK AAAA Validity : S / N 1 - 9999 34 10-00Page 2 olto FEB 00 AIR DATA SYSTEMS DESCRIPTION AND OPERATION 1. GENERAL (Figures 1 and 1A) The air data chapter deals with the ambient air pressure systems and the instruments operating with the static and dynamic pressures. The system is composed of : - an airspeed or true airspeed indicator No. 1, - an additional airspeed or true airspeed indicator No. 2 (option), - a vertical speed indicator No. 1, - an additional vertical speed indicator No. 2 (option), - an altimeter No. 1 or, . an altimeter No. 1 with an altitude reporter (option) or, . an encoding altimeter (option), - an additional altimeter No. 2 (option), - an additional altimeter No. 3 (option), Pre-MOD. 151 - a pitot tube, - or a heated pitot tube (option), Post-MOD. 151 - a heated pitot tube, All - an additional heated pitot tube No. 2 (option). • For the description of the pitot heating system, refer to 30-30-00. Option Pre-MOD. 151, Standard Post-MOD. 151 - an alternate static source valve. The installation uses an air data system composed of a static pressure system and a total (dynamic) pressure system. The two static ports are located on the L.H. and R.H. sides of aft fuselage. ACAB Validity : S / N 823 - 849, 888, 948 - 9999 34 11-00Page 1 (BE) JUN 04 Instruments Air data systems - Schematic |