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Extra resources for AIM FAR 2008: Aeronautical Information Manual federal Aviation Regulations

Sample text

LORAN’S FUTURE. S. will continue to operate the LORAN system in the short term. During this time, the FAA LORAN evaluation program, being conducted with the support of a team comprising government, academia, and industry, will identify and assess LORAN’s potential contributions to required navigation services for the National Airspace System (NAS), and support decisions regarding continued operation of the system. If the government concludes LORAN should not be kept as part of the mix of federally provided radio navigation systems, it will give the users of LORAN reasonable notice so that they Para.

The VHF/ DF receiver display indicates the magnetic direction of the aircraft from the ground station each time the aircraft transmits. d. DF equipment is of particular value in locating lost aircraft and in helping to identify aircraft on radar. REFERENCE—AIM, DIRECTION FINDING INSTRUMENT APPROACH PROCEDURE, PARAGRAPH 6-2-3. 1-1-17. INERTIAL REFERENCE UNIT (IRU), INERTIAL NAVIGATION SYSTEM (INS), AND ATTITUDE HEADING REFERENCE SYSTEM (AHRS) a. IRU’s are self-contained systems comprised of gyros and accelerometers that provide aircraft attitude (pitch, roll, and heading), position, and velocity information in response to signals resulting from inertial effects on system components.

The azimuth station transmits MLS angle and data on one of 200 channels within the frequency range of 5031 to 5091 MHz. 2. The equipment is normally located about 1,000 feet beyond the stop end of the runway, but there is considerable flexibility in selecting sites. For example, for heliport operations the azimuth transmitter can be collocated with the elevation transmitter. 3. The azimuth coverage extends: (See FIG 1-1-8). (a) Laterally, at least 40 degrees on either side of the runway centerline in a standard configuration.

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