Section 171.313 14 CFR Ch. I (1-1-19 Edition) and Auxiliary Data C. Auxiliary Data A contents are specified below, Auxiliary Data B contents are reserved for future use, and Auxiliary Data C contents are reserved for national use. The address codes of the auxiliary data words shall be as shown in Table 8b. (2) Organization and timing. The organization and timing of digital auxiliary data must be as specified in Table 7b. Data containing digital information must be transmitted with the least significant bit first. Alphanumeric data characters must be encoded in accordance with the 7-unit code character set as defined by the American National Standard Code for Information Interchange (ASCII). An even parity bit is added to each character. Alphanumeric data must be transmitted in the order in which they are to be read. The serial transmission of a character must be with the lower order bit transmitted first and the parity bit transmitted last. The timing for alphanumeric auxiliary data must be as shown in Table 7c. (3) Auxiliary Data A content: The data items specified in Table 8c are defined as follows: (i) Approach azimuth antenna offset shall represent the minimum distance between the Approach Azimuth antenna phase center and the vertical plane containing the runway centerline. (ii) Approach azimuth to MLS datum point distance shall represent the minimum distance between the Approach Azimuth antenna phase center and the vertical plane perpendicular to the centerline which contains the MLS datum point. (iii) Approach azimuth alignment with runway centerline shall represent the minimum angle between the approach azimuth antenna zero-degree guidance plane and the runway certerline. (iv) Approach azimuth antenna coordinate system shall represent the coordinate system (planar or conical) of the angle data transmitted by the approach azimuth antenna. (v) Approach elevation antenna offset shall represent the minimum distance between the elevation antenna phase center and the vertical plane containing the runway centerline. (vi) MLS datum point to threshold distance shall represent the distance measured along the runway centerline from the MLS datum point to the runway threshold. (vii) Approach elevation antenna height shall represent the height of the elevation antenna phase center relative to the height of the MLS datum point. (viii) DME offset shall represent the minimum distance between the DME antenna phase center and the vertical plane containing the runway centerline. (ix) DME to MLS datum point distance shall represent the minimum distance between the DME antenna phase center and the vertical plane perpendicular to the centerline which contains the MLS datum point. (x) Back azimuth antenna offset shall represent the minimum distance between the back azimuth antenna phase center and the vertical plane containing the runway centerline. (xi) Back azimuth to MLS datum point distance shall represent the minimum distance between the Back Azimuth antenna and the vertical plane perpendicular to the centerline which contains the MLS datum point. (xii) Back azimuth antenna alignment with runway centerline shall represent the minimum angle between the back azimuth antenna zero-degree guidance plane and the runway centerline. Section 171.313 Azimuth performance requirements. This section prescribes the performance requirements for the azimuth equipment of the MLS as follows: (a) Approach azimuth coverage requirements. The approach azimuth equipment must provide guidance information in at least the following volume of space (see Figure 9): TABLE 8b - AUXILIARY DATA WORD ADDRESS CODES No. 1. 2. 3. 4. 5. 6. 7. 8. I13 I14 0 0 0 0 0 0 0 0 I15 0 0 0 0 0 0 0 0 I16 0 0 0 0 0 0 0 1 I17 0 0 0 1 1 1 1 0 I18 0 1 1 0 0 1 1 0 I19 1 0 1 0 1 0 1 0 864 VerDate Sep<11>2014 08:20 May 17, 2019 Jkt 247048 PO 00000 Frm 00874 Fmt 8010 Sfmt 8010 Y:\SGML\247048.XXX 247048 I20 1 1 0 1 0 0 1 1 1 0 1 1 0 1 0 0