{"data":{"id":"us/14-cfr-171.311","jurisdiction":"us","citation":"14 CFR 171.311","heading":"Signal format requirements.","body":"The signals radiated by the MLS must conform to the signal format in which angle guidance functions and data functions are transmitted sequentially on the same C-band frequency. Each function is identified by a unique digital code which initializes the airborne receiver for proper processing. The signal format must meet the following minimum requirements:\n(a) Frequency assignment. The ground components (except DME/Marker Beacon) must operate on a single frequency assignment or channel, using time division multiplexing. These components must be capable of operating on any one of the 200 channels spaced 300 KHz apart with center frequencies from 5031.0 MHz to 5090.7 MHz and with channel numbering as shown in Table 1a. The operating radio frequencies of all ground components must not vary by more than ±10 KHz from the assigned frequency. Any one transmitter frequency must not vary more than ±50 Hz in any one second period. The MLS angle/data and DME equipment must operate on one of the paired channels as shown in Table 1b.\nTable 1a—Frequency Channel Plan\nChannel No. Frequency (MHz)\n500 5031.0\n501 5031.3\n502 5031.6\n503 5031.9\n504 5032.2\n505 5032.5\n506 5032.8\n507 5033.1\n508 5033.4\n509 5033.7\n510 5034.0\n511 5034.3\n* * * * *\n598 5060.4\n599 5060.7\n600 5061.0\n601 5061.3\n* * * * *\n698 5090.4\n699 5090.7\nTable 1b—Channels\nChannel pairing DME parameters\nDME No. VHF freq. MHz MLS angle freq. MHz MLS Ch. No. Interrogation Reply\nFreq. MHz Pulse codes Freq. MHz Pulse codes µs\nDME/N µs DME/P Mode\nIA µs FA µs\n* 1X 1025 12 962 12\n** 1Y 1025 36 1088 30\n* 2X 1026 12 963 12\n** 2Y 1026 36 1089 30\n* 3X 1027 12 964 12\n** 3Y 1027 36 1090 30\n* 4X 1028 12 965 12\n** 4Y 1028 36 1091 30\n* 5X 1029 12 966 12\n** 5Y 1029 36 1092 30\n* 6X 1030 12 967 12\n** 6Y 1030 36 1093 30\n* 7X 1031 12 968 12\n** 7Y 1031 36 1094 30\n* 8X 1032 12 969 12\n** 8Y 1032 36 1095 30\n* 9X 1033 12 970 12\n** 9Y 1033 36 1096 30\n* 10X 1034 12 971 12\n** 10Y 1034 36 1097 30\n* 11X 1035 12 972 12\n** 11Y 1035 36 1098 30\n* 12X 1036 12 973 12\n** 12Y 1036 36 1099 30\n* 13X 1037 12 974 12\n** 13Y 1037 36 1100 30\n* 14X 1038 12 975 12\n** 14Y 1038 36 1101 30\n* 15X 1039 12 976 12\n** 15Y 1039 36 1102 30\n* 16X 1040 12 977 12\n** 16Y 1040 36 1103 30\n▽17X 108.00 1041 12 978 12\n17Y 108.05 5043.0 540 1041 36 36 42 1104 30\n17Z 5043.3 541 1041 21 27 1104 15\n18X 108.10 5031.0 500 1042 12 12 18 979 12\n18W 5031.3 501 1042 24 30 979 24\n18Y 108.15 5043.6 542 1042 36 36 42 1105 30\n18Z 5043.9 543 1042 21 27 1105 15\n19X 108.20 1043 12 980 12\n19Y 108.25 5044.2 544 1043 36 36 42 1106 30\n19Z 5044.5 545 1043 21 27 1106 15\n20X 108.30 5031.6 502 1044 12 12 18 981 12\n20W 5031.9 503 1044 24 30 981 24\n20Y 108.35 5044.8 546 1044 36 36 42 1107 30\n20Z 5045.1 547 1044 21 27 1107 15\n21X 108.40 1045 12 982 12\n21Y 108.45 5045.4 548 1045 36 36 42 1108 30\n21Z 5045.7 549 1045 21 27 1108 15\n22X 108.50 5032.2 504 1046 12 12 18 983 12\n22W 5032.5 505 1046 24 30 983 24\n22Y 108.55 5046.0 550 1046 36 36 42 1109 30\n22Z 5046.3 551 1046 21 27 1109 15\n23X 108.60 1047 12 984 12\n23Y 108.65 5046.6 552 1047 36 36 42 1110 30\n23Z 5046.9 553 1047 21 27 1110 15\n24X 108.70 5032.8 506 1048 12 12 18 985 12\n24W 5033.1 507 1048 24 30 985 24\n24Y 108.75 5047.2 554 1048 36 36 42 1111 30\n24Z 5047.5 555 1048 21 27 1111 15\n25X 108.80 1049 12 986 12\n25Y 108.85 5047.8 556 1049 36 36 42 1112 30\n25Z 5048.1 557 1049 21 27 1112 15\n26X 108.90 5033.4 508 1050 12 12 18 987 12\n26W 5033.7 509 1050 24 30 987 24\n26Y 108.95 5048.4 558 1050 36 36 42 1113 30\n26Z 5048.7 559 1050 21 27 1113 15\n27X 109.00 1051 12 988 12\n27Y 109.05 5049.0 560 1051 36 36 42 1114 30\n27Z 5049.3 561 1051 21 27 1114 15\n28X 109.10 5034.0 510 1052 12 12 18 989 12\n28W 5034.3 511 1052 24 30 989 24\n28Y 109.15 5049.6 562 1052 36 36 42 1115 30\n28Z 5049.9 563 1052 21 27 1115 15\n29X 109.20 1053 12 990 12\n29Y 109.25 5050.2 564 1053 36 36 42 1116 30\n29Z 5050.5 565 1043 21 27 1116 15\n30X 109.30 5034.6 512 1054 12 12 18 991 12\n30W 5034.9 513 1054 24 30 991 24\n30Y 109.35 5050.8 566 1054 36 36 42 1117 30\n30Z 5051.1 567 1054 21 27 1117 15\n31X 109.40 1055 12 992 12\n31Y 109.45 5051.4 568 1055 36 36 42 1118 30\n31Z 5051.7 569 1055 21 27 1118 15\n32X 109.50 5035.2 514 1056 12 12 18 993 12\n32W 5035.5 515 1056 24 30 993 24\n32Y 109.55 5052.0 570 1056 36 36 42 1119 30\n32Z 5052.3 571 1056 21 27 1119 15\n33X 109.60 1057 12 994 12\n33Y 109.65 5052.6 572 1057 36 36 42 1120 30\n33Z 5052.9 573 1057 21 27 1120 15\n34X 109.70 5035.8 516 1058 12 12 18 995 12\n34W 5036.1 517 1058 24 30 995 24\n34Y 109.75 5053.2 574 1058 36 36 42 1121 30\n34Z 5053.5 575 1058 21 27 1121 15\n35X 109.80 1059 12 996 12\n35Y 109.85 5053.8 576 1059 36 36 42 1122 30\n35Z 5054.1 577 1059 21 27 1122 15\n36X 109.90 5036.4 518 1060 12 12 18 997 12\n36W 5036.7 519 1060 24 30 997 24\n36Y 109.95 5054.4 578 1060 36 36 42 1123 30\n36Z 5054.7 579 1060 21 27 1123 15\n37X 110.00 1061 12 998 12\n37Y 110.05 5055.0 580 1061 36 36 42 1124 30\n37Z 5055.3 581 1061 21 27 1124 15\n38X 110.10 5037.0 520 1062 12 12 18 999 12\n38W 5037.3 521 1062 24 30 999 24\n38Y 110.15 5055.6 582 1062 36 36 42 1125 30\n38Z 5055.9 583 1062 21 27 1125 15\n39X 110.20 1063 12 1000 12\n39Y 110.25 5056.2 584 1063 36 36 42 1126 30\n39Z 5056.5 585 1063 21 27 1126 15\n40X 110.30 5037.6 522 1064 12 12 18 1001 12\n40W 5037.9 523 1064 24 30 1001 24\n40Y 110.35 5056.8 586 1064 36 36 42 1127 30\n40Z 5057.1 587 1064 21 27 1127 15\n41X 110.40 1065 12 1002 12\n41Y 110.45 5057.4 588 1065 36 36 42 1128 30\n41Z 5057.7 589 1065 21 27 1128 15\n42X 110.50 5038.2 524 1066 12 12 18 1003 12\n42W 5038.5 525 1066 24 30 1003 24\n42Y 110.55 5058.0 590 1066 36 36 42 1129 30\n42Z 5058.3 591 1066 21 27 1129 15\n43X 110.60 1067 12 1004 12\n43Y 110.65 5058.6 592 1067 36 36 42 1130 30\n43Z 5058.9 593 1067 21 27 1130 15\n44X 110.70 5038.8 526 1068 12 12 18 1005 12\n44W 5039.1 527 1068 24 30 1005 24\n44Y 110.75 5059.2 594 1068 36 36 42 1131 30\n44Z 5059.5 595 1068 21 27 1131 15\n45X 110.80 1069 12 1006 12\n45Y 110.85 5059.8 596 1069 36 36 42 1132 30\n45Z 5060.1 597 1069 21 27 1132 15\n46X 110.90 5039.4 528 1070 12 12 18 1007 12\n46W 5039.7 529 1070 24 30 1007 24\n46Y 110.95 5060.4 598 1070 36 36 42 1133 30\n46Z 5060.7 599 1070 21 27 1133 15\n47X 111.00 1071 12 1008 12\n47Y 111.05 5061.0 600 1071 36 36 42 1134 30\n47Z 5061.3 601 1071 21 27 1134 15\n48X 111.10 5040.0 530 1072 12 12 18 1009 12\n48W 5040.3 531 1072 24 30 1009 24\n48Y 111.15 5061.6 602 1072 36 36 42 1135 30\n48Z 5061.9 603 1072 21 27 1135 15\n49X 111.20 1073 12 1010 12\n49Y 111.25 5062.2 604 1073 36 36 42 1136 30\n49Z 5062.5 605 1073 21 27 1136 15\n50X 111.30 5040.6 532 1074 12 12 18 1011 12\n50W 5040.9 533 1074 24 30 1011 24\n50Y 111.35 5062.8 606 1074 36 36 42 1137 30\n50Z 5063.1 607 1074 21 27 1137 15\n51X 111.40 1075 12 1012 12\n51Y 111.45 5063.4 608 1075 36 36 42 1138 30\n51Z 5063.7 609 1075 21 27 1138 15\n52X 111.50 5041.2 534 1076 12 12 18 1013 12\n52W 5041.5 535 1076 24 30 1013 24\n52Y 111.55 5064.0 610 1076 36 36 42 1139 30\n52Z 5064.3 611 1076 21 27 1139 15\n53X 111.60 1077 12 1014 12\n53Y 111.65 5064.6 612 1077 36 36 42 1140 30\n53Z 5064.9 613 1077 21 27 1140 15\n54X 111.70 5041.8 536 1078 12 12 18 1015 12\n54W 5042.1 537 1078 24 30 1015 24\n54Y 111.75 5065.2 614 1078 36 36 42 1141 30\n54Z 5065.5 615 1078 21 27 1141 15\n55X 111.80 1079 12 1016 12\n55Y 111.85 5065.8 616 1079 36 36 42 1142 30\n55Z 5066.1 617 1079 21 27 1142 15\n56X 111.90 5042.4 538 1080 12 12 18 1017 12\n56W 5042.7 539 1080 24 30 1017 24\n56Y 111.95 5066.4 618 1080 36 36 42 1143 30\n56Z 5066.7 619 1080 21 27 1143 15\n57X 112.00 1081 12 1018 12\n57Y 112.05 1081 36 1144 30\n58X 112.10 1082 12 1019 12\n58Y 112.15 1082 36 1145 30\n59X 112.20 1083 12 1020 12\n59Y 122.25 1083 36 1146 30\n** 60X 1084 12 1021 12\n** 60Y 1084 36 1147 30\n** 61X 1085 12 1022 12\n** 61Y 1085 36 1148 30\n** 62X 1086 12 1023 12\n** 62Y 1086 36 1149 30\n** 63X 1037 12 1024 12\n** 63Y 1087 36 1150 30\n** 64X 1088 12 1151 12\n** 64Y 1088 36 1025 30\n** 65X 1089 12 1152 12\n** 65Y 1089 36 1026 30\n** 66X 1090 12 1153 12\n** 66Y 1090 36 1027 30\n** 67X 1091 12 1154 12\n** 67Y 1091 36 1028 30\n** 68X 1092 12 1155 12\n** 68Y 1092 36 1029 30\n** 69X 1093 12 1156 12\n** 69Y 1093 36 1030 30\n70X 112.30 1094 12 1157 12\n** 70Y 112.35 1094 36 1031 30\n71X 112.40 1095 12 1158 12\n** 71Y 112.45 1095 36 1032 30\n72X 112.50 1096 12 1159 12\n** 72Y 112.55 1096 36 1033 30\n73X 112.60 1097 12 1160 12\n** 73Y 112.65 1097 36 1034 30\n74X 112.70 1098 12 1161 12\n** 74Y 112.75 1098 36 1035 30\n75X 112.80 1099 12 1162 12\n** 75Y 112.85 1099 36 1036 30\n76X 112.90 1100 12 1163 12\n** 76Y 112.95 1100 36 1037 30\n77X 113.00 1101 12 1164 12\n** 77Y 113.05 1101 36 1038 30\n78X 113.10 1102 12 1165 12\n** 78Y 113.15 1102 36 1039 30\n79X 113.20 1103 12 1166 12\n** 79Y 113.25 1103 36 1040 30\n80X 113.30 1104 12 1167 12\n80Y 113.35 5067.0 620 1104 36 36 42 1041 30\n80Z 5067.3 621 1104 21 27 1041 15\n81X 113.40 1105 12 1168 12\n81Y 113.45 5067.6 622 1105 36 36 42 1042 30\n81Z 5067.9 623 1005 21 27 1042 15\n82X 113.50 1106 12 1169 12\n82Y 113.55 5068.2 624 1106 36 36 42 1043 30\n82Z 5068.5 625 1106 21 27 1043 15\n83X 113.60 1107 12 1170 12\n83Y 113.65 5068.8 626 1107 36 36 42 1044 30\n83Z 5069.1 627 1107 21 27 1044 15\n84X 113.70 1108 12 1171 12\n84Y 113.75 5069.4 628 1108 36 36 42 1045 30\n84Z 6069.7 629 1108 21 27 1045 15\n85X 113.80 1109 12 1172 12\n85Y 113.85 5070.0 630 1109 36 36 42 1046 30\n85Z 5070.3 631 1109 21 27 1046 15\n86X 113.90 1110 12 1173 12\n86Y 113.95 5070.6 632 1110 36 36 42 1047 30\n86Z 5070.9 633 1110 21 27 1047 15\n87X 114.00 1111 12 1174 12\n87Y 114.05 5071.2 634 1111 36 36 42 1048 30\n87Z 5071.5 635 1111 21 27 1048 15\n88X 114.10 1112 12 1175 12\n88Y 114.15 5071.8 636 1112 36 36 42 1049 30\n88Z 5072.1 637 1112 21 27 1049 15\n89X 114.20 1113 12 1176 12\n89Y 114.25 5072.4 638 1113 36 36 42 1050 30\n89Z 5072.7 639 1113 21 27 1050 15\n90X 114.30 1114 12 1177 12\n90Y 114.35 5073.0 640 1114 36 36 42 1051 30\n90Z 5073.3 641 1114 21 27 1051 15\n91X 114.40 1115 12 1178 12\n91Y 114.45 5073.6 642 1115 36 36 42 1052 30\n91Z 5073.9 643 1115 21 27 1052 15\n92X 114.50 1116 12 1179 12\n92Y 114.55 5074.2 644 1116 36 36 42 1053 30\n92Z 5074.5 645 1116 21 27 1053 15\n93X 114.60 1117 12 1180 12\n93Y 114.65 5074.8 646 1117 36 36 42 1054 30\n93Z 5075.1 647 1117 21 27 1054 15\n94X 114.70 1118 12 1181 12\n94Y 114.75 5075.4 648 1118 36 36 42 1055 30\n94Z 5075.7 649 1118 21 27 1055 15\n95X 114.80 1119 12 1182 12\n95Y 114.85 5076.0 650 1119 36 36 42 1056 30\n95Z 5076.3 651 1119 21 27 1056 15\n96X 114.90 1120 12 1183 12\n96Y 114.95 5076.6 652 1120 36 36 42 1057 30\n96Z 5076.9 653 1120 21 27 1057 15\n97X 115.00 1121 12 1184 12\n97Y 115.05 5077.2 654 1121 36 36 42 1058 30\n97Z 5077.5 655 1121 21 27 1058 15\n98X 115.10 1122 12 1185 12\n98Y 115.15 5077.8 656 1122 36 36 42 1059 30\n98Z 5078.1 657 1122 21 27 1059 15\n99X 115.20 1123 12 1186 12\n99Y 115.25 5078.4 658 1123 36 36 42 1060 30\n99Z 5078.7 659 1123 21 27 1060 15\n100X 115.30 1124 12 1187 12\n100Y 115.35 5079.0 660 1124 36 36 42 1061 30\n100Z 5079.3 661 1124 21 27 1061 15\n101X 115.40 1125 12 1188 12\n101Y 115.45 5079.6 662 1125 36 36 42 1062 30\n101Z 5079.9 663 1125 21 27 1062 15\n102X 115.50 1126 12 1189 12\n102Y 115.55 5080.2 664 1126 36 36 42 1063 30\n102Z 5080.5 665 1126 21 27 1063 15\n103X 115.60 1127 12 1190 12\n103Y 115.65 5080.B 666 1127 36 36 42 1064 30\n103Z 5081.1 667 1127 21 27 1064 19\n104X 115.70 1128 12 1191 12\n104Y 115.75 5081.4 668 1128 36 36 42 1065 30\n104Z 5081.7 669 1128 21 27 1065 19\n105X 115.80 1129 12 1192 12\n105Y 115.85 5082.0 670 1129 36 36 42 1066 30\n105Z 5082.3 671 1129 21 27 1066 15\n106X 115.90 1130 12 1193 12\n106Y 115.95 5082.6 672 1130 36 36 42 1067 30\n106Z 5082.9 673 1130 21 27 1067 15\n107X 116.00 1131 12 1194 12\n107Y 116.05 5083.2 674 1131 36 36 42 1068 30\n107Z 5083.5 675 1131 21 27 1068 15\n108X 116.10 508 1132 12 1195 12\n108Y 116.15 5083.8 676 1132 36 36 42 1069 30\n108Z 5084.1 677 1132 21 27 1069 15\n109X 116.20 1133 12 1196 12\n109Y 116.25 5084.4 678 1133 36 36 42 1070 30\n109Z 5084.7 679 1133 21 27 1070 15\n110X 116.30 1134 12 1197 12\n110Y 116.35 5085.0 680 1134 36 36 42 1071 30\n110Z 5085.3 681 1134 21 27 1071 15\n111X 116.40 1135 12 1198 12\n111Y 116.45 5086.6 682 1135 36 36 42 1072 30\n111Z 5085.9 683 1135 21 27 1072 15\n112X 116.50 1136 12 1199 12\n112Y 116.55 5086.2 684 1136 36 36 42 1073 30\n112Z 5086.5 685 1136 21 27 1073 15\n113X 116.60 1137 12 1200 12\n113Y 116.65 5086.8 686 1137 36 36 42 1074 30\n113Z 5087.1 687 1137 21 27 1074 15\n114X 116.70 1138 12 1201 12\n114Y 116.75 5087.4 688 1138 36 36 42 1075 30\n114Z 5087.7 689 1138 21 27 1075 15\n115X 116.80 1139 12 1202 12\n115Y 116.85 5088.0 690 1139 36 36 42 1076 30\n115Z 5088.3 691 1139 21 27 1076 15\n116X 116.90 1140 12 1203 12\n116Y 116.95 5088.6 692 1140 36 36 42 1077 30\n116Z 5088.9 693 1140 21 27 1077 15\n117X 117.00 1141 12 1204 12\n117Y 117.05 5089.2 694 1141 36 36 42 1078 30\n117Z 5089.5 695 1141 21 27 1078 15\n118X 117.10 1142 12 12.5 12\n118Y 117.15 5089.8 696 1142 36 36 42 1079 30\n118Z 5090.1 697 1142 21 27 1079 12\n119X 117.20 1143 12 1206 12\n119Y 117.25 5090.4 698 1143 36 36 42 1080 30\n119Z 5090.7 699 1143 21 27 1080 15\n120X 117.30 1144 12 1207 12\n120Y 117.35 1144 36 1081 30\n121X 117.40 1145 12 1208 12\n121Y 117.45 1145 36 1082 30\n122X 117.50 1146 12 1209 12\n122Y 117.55 1146 36 1083 30\n123X 117.60 1147 12 1210 12\n123Y 117.65 1147 36 1084 30\n124X 117.70 1148 12 1211 12\n** 124Y 117.75 1148 36 1085 30\n125X 117.80 1149 12 1212 12\n** 125Y 117.85 1149 36 1086 30\n126X 117.90 1150 12 1213 12\n** 126Y 117.95 1150 36 1087 30\nNotes:\n* These channels are reserved exclusively for national allotments.\n** These channels may be used for national allotment on a secondary basis. The primary reason for reserving these channels is to provide protection for the secondary Surveillance Radar (SSR) system.\n▽ 108.0 MHz is not scheduled for assignment to ILS service. The associated DME operating channel No. 17X may be assigned to the emergency service.\n(b) Polarization. (1) The radio frequency emissions from all ground equipment must be nominally vertically polarized. Any horizontally polarized radio frequency emission component from the ground equipment must not have incorrectly coded angle information such that the limits specified in paragraphs (b) (2) and (3) of this section are exceeded.\n(2) Rotation of the receiving antenna thirty degrees from the vertically polarized position must not cause the path following error to exceed the allowed error at that location.\n(c) Modulation requirements. Each function transmitter must be capable of DPSK and continuous wave (CW) modulations of the RF carrier which have the following characteristics.\n(1) DPSK. The DPSK signal must have the following characteristics:\nbit rate 15.625 KHz\nbit length 64 microseconds\nlogic “0” no phase transition\nlogic “1” phase transition\nphase transition less than 10 microseconds\nphase tolerance ±10 degrees\nThe phase shall advance (or retard) monotonically throughout the transition region. Amplitude modulation during the phase transition period shall not be used.\n(2) CW. The CW pulse transmissions and the CW angle transmissions as may be required in the signal format of any function must have characteristics such that the requirements of paragraph (d) of this section are met.\n(d) Radio frequency signal spectrum. The transmitted signal must be such that during the transmission time, the mean power density above a height of 600 meters (2000 feet) does not exceed −100.5 dBW/m 2 for angle guidance and −95.5 dBW/m 2 for data, as measured in a 150 KHz bandwidth centered at a frequency of 840 KHz or more from the assigned frequency.\n(e) Synchronization. Synchronization between the azimuth and elevation components is required and, in split-site configurations, would normally be accomplished by landline interconnections. Synchronization monitoring must be provided to preclude function overlap.\n(f) Transmission rates. Angle guidance and data signals must be transmitted at the following average repetition rates:\nFunction Average data rate (Hertz)\nApproach Azimuth 13 ±0.5\nHigh Rate Approach Azimuth 1 39 ±1.5\nApproach Elevation 39 ±1.5\nBack Azimuth 6.5 ±0.25\nBasic Data (2)\nAuxiliary Data (3)\n1 The higher rate is recommended for azimuth scanning antennas with beamwidths greater than two degrees. It should be noted that the time available in the signal format for additional functions is limited when the higher rate is used.\n2 Refer to Table 8a.\n3 Refer to Table 8c.\n(g) Transmission sequences. Sequences of angle transmissions which will generate the required repetition rates are shown in Figures 2 and 3.\n(h) TDM cycle. The time periods between angle transmission sequences must be varied so that exact repetitions do not occur within periods of less than 0.5 second in order to protect against synchronous interference. One such combination of sequences is shown in Figure 4 which forms a full multiplex cycle. Data may be transmitted during suitable open times within or between the sequences.\n(i) Function Formats (General). Each angle function must contain the following elements: a preamble; sector signals; and a TO and FRO angle scan organized as shown in Figure 5a. Each data function must contain a preamble and a data transmission period organized as shown in Figure 5b.\n(1) Preamble format. The transmitted angle and date functions must use the preamble format shown in Figure 6. This format consists of a carrier acquisition period of unmodulated CW transmission followed by a receiver synchronization code and a function identification code. The preamble timing must be in accordance with Table 2.\n(i) Digital codes. The coding used in the preamble for receiver synchronization is a Barker code logic 11101. The time of the last phase transition midpoint in the code shall be the receiver reference time (see Table 2). The function identification codes must be as shown in Table 3. The last two bits (I11 and I12) of the code are parity bits obeying the equations:\nI6 + I7 + I8 + I9 + I10 + I11 = Even\nI6 + I8 + I10 + I12 = Even\n(ii) Data modulation. The digital code portions of the preamble must be DPSK modulated in accordance with § 171.311(c)(1) and must be transmitted throughout the function coverage volume.\n(2) Angle function formats. The timing of the angle transmissions must be in accordance with Tables 4a, 4b, and 5. The actual timing of the TO and FRO scans must be as required to meet the accuracy requirements of §§ 171.313 and 171.317.\n(i) Preamble. Must be in accordance with requirements of § 171.311(i)(1).\nTable 2—Preamble Timing 1\nEvent Event time slot begins at—\n15.625 kHz clock pulse (number) Time (milliseconds)\nCarrier acquisition:\n(CW transmission) 0 0\nReceiver reference time code:\nI1 = 1 13 0.832\nI2 = 1 14 0.896\nI3 = 1 15 0.960\nI4 = 0 16 1.024\nI5 = 1 17 2 1.088\nFunction identification:\nI6 18 1.152\nI7 19 1.216\nI8 20 1.280\nI9 21 1.344\nI10 (see table 1) 22 1.408\nI11 23 1.472\nI12 24 1.536\nEND PREAMBLE 25 1.600\n1 Applies to all functions transmitted.\n2 Reference time for receiver synchronization for all function timing.\nTable 3—Function Identification Codes\nFunction Code\nI6 I7 I8 I9 I10 I11 I12\nApproach azimuth 0 0 1 1 0 0 1\nHigh rate approach azimuth 0 0 1 0 1 0 0\nApproach elevation 1 1 0 0 0 0 1\nBack azimuth 1 0 0 1 0 0 1\nBasic data 1 0 1 0 1 0 0 0\nBasic data 2 0 1 1 1 1 0 0\nBasic data 3 1 0 1 0 0 0 0\nBasic data 4 1 0 0 0 1 0 0\nBasic data 5 1 1 0 1 1 0 0\nDasic data 6 0 0 0 1 1 0 1\nAuxiliary data A 1 1 1 0 0 1 0\nAuxiliary data B 1 0 1 0 1 1 1\nAuxiliary data C 1 1 1 1 0 0 0\n(ii) Sector signals. In all azimuth formats, sector signals must be transmitted to provide Morse Code identification, airborne antenna selection, and system test signals. These signals are not required in the elevation formats. In addition, if the signal from an installed ground component results in a valid indication in an area where no valid guidance should exist, OCI signals must be radiated as provided for in the signal format (see Tables 4a, 4b, and 5). The sector signals are defined as follows:\n(A) Morse Code. DPSK transmissions that will permit Morse Code facility identification in the aircraft by a four letter code starting with the letter “M” must be included in all azimuth functions. They must be transmitted and repeated at approximately equal intervals, not less than six times per minute, during which time the ground subsystem is available for operational use. When the transmissions of the ground subsystem are not available, the identification signal must be suppressed. The audible tone in the aircraft is started by setting the Morse Code bit to logic “1” and stopped by a logic “0” (see Tables 4a and 4b). The identification code characteristics must conform to the following: the dot must be between 0.13 and 0.16 second in duration, and the dash between 0.39 and 0.48 second. The duration between dots and/or dashes must be one dot plus or minus 10%. The duration between characters (letters) must not be less than three dots. When back azimuth is provided, the code shall be transmitted by the approach azimuth and back azimuth within plus or minus 0.08 seconds.\n(B) Airborne antenna selection. A signal for airborne antenna selection shall be transmitted as a “zero” DPSK signal lasting for a six-bit period (see Tables 4a and 4b).\nTable 4a—Approach Azimuth Function timing\nEvent Event time slot begins at—\n15.625 kHz clock pulse (number) Time (milliseconds)\nPreamble 0 0\nMorse code 25 1.600\nAntenna select 26 1.664\nRear OCI 32 2.048\nLeft OCI 34 2.176\nRight OCI 36 2.304\nTo test 38 2.432\nTo scan 1 40 2.560\nPause 8.760\nMidscan point 9.060\nFRO scan 1 9.360\nFRO test 15.560\nEnd Function (Airborne) 15.688\nEnd guard time; end function (ground) 15.900\nAA1 The actual commencement and completion of the TO and the FRO scan transmissions are dependent on the amount of proportional guidance provided. The time slots provided shall accommodate a maximum scan of plus or minus 62.0 degrees. Scan timing shall be compatible with accuracy requirements.\nTable 4b—High Rate Approach Azimuth and Back Azimuth Function Timing\nEvent Event time slot begins at—\n15.625 kHz clock pulse (number) Time (milliseconds)\nPreamble 0 0\nMorse Code 25 1.600\nAntenna select 26 1.664\nRear OCI 32 2.048\nLeft OCI 34 2.176\nRight OCI 36 2.304\nTo test 38 2.432\nTo scan 1 40 2.560\nPause 6.760\nMidscan point 7.060\nFRO scan 1 7.360\nFRO test pulse 11.560\nEnd function (airborne) 11.688\nEnd guard time; end function (ground) 11.900\n1 The actual commencement and completion of the TO and the FRO scan transmissions are dependent on the amount of proportional guidance provided. The time slots provided will accommodate a maximum scan of plus or minus 42.0 degrees. Scan timing shall be compatible with accuracy requirements.\n(C) OCI. Where OCI pulses are used, they must be: (1) greater than any guidance signal in the OCI sector; (2) at least 5 dB less than the level of the scanning beam within the proportional guidance sector; and (3) for azimuth functions with clearance signals, at least 5 dB less than the level of the left (right) clearance pulses within the left (right) clearance sector.\nTable 5—Approach Elevation Function Timing\nEvent Event time slot begins at:\n15.625 kHz clock pluse (number) Time (milliseconds)\nPreamble 0 0\nProcessor pause 25 1.600\nOCI 27 1.728\nTo scan 1 29 1.856\nPause 3.406\nMidscan point 3.606\nFRO scan 1 3.806\nEnd function (airborne) 5.356\nEnd guard time; end function (ground) 5.600\n1 The actual commencement and completion of the TO and FRO scan transmissions are dependent upon the amount of proportional guidance provided. The time slots provided will accommodate a maximum scan of −1.5 degrees to + 29.5 degrees. Scan timing shall be compatible with accuracy requirements.\nThe duration of each pulse measured at the half amplitude point shall be at least 100 microseconds, and the rise and fall times shall be less then 10 microseconds. It shall be permissible to sequentially transmit two pulses in each out-of-coverage indication time slot. Where pulse pairs are used, the duration of each pulse shall be at least 50 microseconds, and the rise and fall times shall be less then 10 microseconds. The transmission of out-of-coverage indication pulses radiated from antennas with overlapping coverage patterns shall be separated by at least 10 microseconds.\nNote:\nIf desired, two pulses may be sequentially transmitted in each OCI time slot. Where pulse pairs are used, the duration of each pulse must be 45 (±5) microseconds and the rise and fall times must be less than 10 microseconds.\n(D) System test. Time slots are provided in Tables 4a and 4b to allow radiation of TO and FRO test pulses. However, radiation of these pulses is not required since the characteristics of these pulses have not yet been standardized.\n(iii) Angle encoding. The encoding must be as follows:\n(A) General. Azimuth and elevation angles are encoded by scanning a narrow beam between the limits of the proportional coverage sector first in one direction (the TO scan) and then in the opposite direction (the FRO scan). Angular information must be encoded by the amount of time separation between the beam centers of the TO and FRO scanning beam pulses. The TO and FRO transmissions must be symmetrically disposed about the midscan point listed in Tables 4a, 4b, 5, and 7. The midscan point and the center of the time interval between the TO and FRO scan transmissions must coincide with a tolerance of ±10 microseconds. Angular coding must be linear with angle and properly decoded using the formula:\nwhere:\nθ = Receiver angle in degrees.\nV = Scan velocity in degrees per microsecond.\nT0 = Time separation in microseconds between TO and FRO beam centers corresponding to zero degrees.\nt = Time separation in microseconds between TO and FRO beam centers.\nThe timing requirements are listed in Table 6 and illustrated in Figure 7.\n(B) Azimuth angle encoding. Each guidance angle transmitted must consist of a clockwise TO scan followed by a counterclockwise FRO scan as viewed from above the antenna. For approach azimuth functions, increasing angle values must be in the direction of the TO scan; for the back azimuth function, increasing angle values must be in the direction of the FRO scan. The antenna has a narrow beam in the plane of the scan direction and a broad beam in the orthogonal plane which fills the vertical coverage.\n(C) Elevation angle encoding. The radiation from elevation equipment must produce a beam which scans from the horizon up to the highest elevation angle and then scans back down to the horizon. The antenna has a narrow beam in the plane of the scan direction and a broad beam in the orthogonal plane which fills the horizontal coverage. Elevation angles are defined from the horizontal plane containing the antenna phase center; positive angles are above the horizontal and zero angle is along the horizontal.\n(iv) Clearance guidance. The timing of the clearance pulses must be in accordance with Figure 8. For azimuth elements with proportional coverage of less than ±40 degrees (±20 degrees for back azimuth), clearance guidance information must be provided by transmitting pulses in a TO and FRO format adjacent to the stop/start times of the scanning beam signal. The fly-right clearance pulses must represent positive angles and the fly-left clearance pulses must represent negative angles. The duration of each clearance pulse must be 50 microseconds with a tolerance of ±5 microseconds. The transmitter switching time between the clearance pulses and the scanning beam transmissions must not exceed 10 microseconds. The rise time at the edge of each clearance pulse must be less than 10 microseconds. Within the fly-right clearance guidance section, the fly-right clearance guidance signal shall exceed scanning beam antenna sidelobes and other guidance and OCI signals by at least 5 dB; within the fly-left clearance guidance sector, the fly left clearance guidance signal shall exceed scanning beam antenna sidelobes and all other guidance and OCI signals by at least 5 dB; within the proportional guidance sector, the clearance guidance signals shall be at least 5dB below the proportional guidance signal. Optionally, clearance guidance may be provided by scanning throughout the approach guidance sector. For angles outside the approach azimuth proportional coverage limits as set in Basic Data Word One (Basic Data Word 5 for back azimuth), proper decode and display of clearance guidance must occur to the limits of the guidance region. Where used, clearance pulses shall be transmitted adjacent to the scanning beam signals at the edges of proportional coverage as shown in Figure 8. The proportional coverage boundary shall be established at one beamwidth inside the scan start/stop angles, such that the transition between scanning beam and clearance signals occurs outside the proportional coverage sector. When clearance pulses are provided in conjunction with a narrow beamwidth (e.g., one degree) scanning antenna, the scanning beam antenna shall radiate for 15 microseconds while stationary at the scan start/stop angles.\n(3) Data function format. Basic data words provide equipment characteristics and certain siting information. Basic data words must be transmitted from an antenna located at the approach azimuth or back azimuth site which provides coverage throughout the appropriate sector. Data function timing must be in accordance with Table 7a.\nTable 6—Angle Scan Timing Constants\nFunction Max value of t (usec) To (usec) V(deg/usec) Tm (usec) Pause time (usec) Tt (usec)\nApproach azimuth 13,000 6,800 0.02 7,972 600 13,128\nHigh rate approach azimuth 9,000 4,800 0.02 5,972 600 9,128\nApproach elevation 3,500 3,350 0.02 2,518 400 N/A\nBack azimuth 9,000 4,800 −0.02 5,972 600 9,128\nTable 7a—Basic Data Function Timing\nEvent Event time slot begins at: 1\n15.625 kHz clock pulse (number) Time (milliseconds)\nPreamble 0 0\nData transmission (bits I13-I30) 25 1.600\nParity transmission (bits I31-I32) 43 2.752\nEnd function (airborne) 45 2.880\nEnd guard time: end function (ground) 3.100\n1 The previous event time slot ends at this time.\nTable 7b—Auxiliary Data Function Timing—(Digital)\nEvent Event time slot begins at:\n15.625 kHz clock pulse (number) Time (milliseconds)\nPreamble 0 0\nAddress transmission (bits I13-I20) 25 1.600\nData transmission: (bits I21-I69) 33 2.112\nParity transmission (bits I70-I76) 82 5.248\nEnd function (airborne) 89 5.696\nEnd guard time; end function (ground) 5.900\nTable 7c—Auxiliary Data Function Timing—(Alphanumeric)\nEvent Event time slot begins at:\n15.615 kHz clock pulse (number) Time (milliseconds)\nPreamble 0 0\nAddress transmission (bits I13-I20) 25 1.600\nData transmission: (bits I21-I76 33 2.112\nEnd function (airborne) 89 5.696\nEnd guard time; (end function ground) 5.900\n(i) Preamble. Must be in accordance with requirements of § 171.311(i)(1).\n(ii) Data transmissions. Basic data must be transmitted using DPSK modulation. The content and repetition rate of each basic data word must be in accordance with Table 8a. For data containing digital information, binary number 1 must represent the lower range limit with increments in binary steps to the upper range limit shown in Table 8a. Data containing digital information shall be transmitted with the least significant bit first.\n(j) Basic Data word requirements. Basic Data shall consist of the items specified in Table 8a. Basic Data word contents shall be defined as follows:\n(1) Approach azimuth to threshold distance shall represent the minimum distance between the Approach Azimuth antenna phase center and the vertical plane perpendicular to the centerline which contains the landing threshold.\n(2) Approach azimuth proportional coverage limit shall represent the limit of the sector in which proportional approach azimuth guidance is transmitted.\n(3) Clearance signal type shall represent the type of clearance when used. Pulse clearance is that which is in accordance with § 171.311 (i) (2) (iv). Scanning Beam (SB) clearance indicates that the proportional guidance sector is limited by the proportional coverage limits set in basic data.\nTable 8a—Basic Data Words\nData bit # Data item definition LSB value Data bit value\nBasic Data Word No. 1\n1 Preamble N/A 1\n2 1\n3 1\n4 0\n5 1\n6 0\n7 1\n8 0\n9 1\n10 0\n11 0\n12 0\n13 Approach azimuth to threshold distance (Om−630m) 100m 100m\n14 200m\n15 400m\n16 800m\n17 1600m\n18 3200m\n19 Approach azimuth proportional coverage limit (negative limit) (0° to −62°) 2° −2°\n20 −4°\n21 −8°\n22 −16°\n23 −32°\n24 Approach azimuth proportional coverage limit (positive limit) (0° to + 62°) 2° 2°\n25 4°\n26 8°\n27 16°\n28 32°\n29 Clearance signal type N/A 0 = pulse; 1 = SB\n30 Spare Transmit zero\n31 Parity: (13 + 14 + 15. . . + 30 + 31 = odd) N/A N/A\n32 Parity: (14 + 16 + 18. . . + 30 + 32 = odd) N/A N/A\nNote 1: Transmit throughout the Approach Azimuth guidance sector at intervals of 1.0 seconds or less.\nNote 2: The all zero state of the data field represents the lower limit of the absolute value of the coded parameter unless otherwise noted.\nBasic Data Word No. 2\n1 Preamble N/A 1\n2 1\n3 1\n4 0\n5 1\n6 0\n7 1\n8 1\n9 1\n10 1\n11 0\n12 0\n13 Minimum glide path (2.0° to 14.7°) 0.1° 0.1°\n14 0.2°\n15 0.4°\n16 0.8°\n17 1.6°\n18 3.2°\n19 6.4°\n20 Back azimuth status see note 4\n21 DME status see note 6\n22\n23 Approach azimuth status see note 4\n24 Approach azimuth status see note 4\n25 Spare Transmit zero\n26 ......do Do.\n27 ......do Do.\n28 ......do Do.\n29 ......do Do.\n30 ......do Do.\n31 Parity: (13 + 14 + 15. . . + 30 + 31) = odd) N/A N/A\n32 Parity: (14 + 16 + 18. . . + 30 + 32 = odd) N/A N/A\nNote 1: Transmit throughout the Approach Azimuth guidance sector at intervals of 0.16 seconds or less.\nNote 2: The all zero state of the data field represents the lower limit of the absolute range of the coded parameter unless otherwise noted.\nBasic Data Word No. 3\n1 Preamble N/A 1\n2 1\n3 1\n4 0\n5 1\n6 1\n7 0\n8 1\n9 0\n10 0\n11 0\n12 0\n13 Approach azimuth beamwidth (0.5°−4.0°) See note 7 0.5° 0.5°\n14 1.0°\n15 2.0°\n16 Approach elevation beamwidth (0.5° to 2.5°) See note 7 0.5° 0.5°\n17 1.0°\n18 Note: values greater than 2.5° are invalid 2.0°\n19 DME distance (Om to 6387.5m 12.5m 12.5m\n20 25.0m\n21 50.0m\n22 100.0m\n23 200.0m\n24 400.0m\n25 800.0m\n26 1600.0m\n27 3200.0m\n28 Spare Transmit zero\n29 ......do Do.\n30 ......do Do.\n31 Parity: (13 + 14 + 15. . . + 30 + 31 = odd)\n32 Parity: (14 + 16 + 18. . . + 30 + 32 = odd) N/A N/A\nNote 1: Transmit throughout the Approach Azimuth guidance sector at intervals of 1.0 seconds or less.\nNote 2: The all zero state of the data field represents the lower limit of the absolute range of the coded parameter unless otherwise noted.\nBasic Data Word No. 4\n1 Preamble N/A 1\n2 1\n3 1\n4 0\n5 1\n6 1\n7 0\n8 0\n9 0\n10 1\n11 0\n12 0\n13 Approach azimuth magnetic orientation (0° to 359°) 1° 1°\n14 2°\n15 4°\n16 8°\n17 16°\n18 32°\n19 64°\n20 128°\n21 256°\n22 Back azimuth magnetic orientation (0° to 359°) 1° 1°\n23 2°\n24 4°\n25 8°\n26 16°\n27 32°\n28 64°\n29 128°\n30 256°\n31 Parity: (13 + 14 + 15. . . + 30 + 31 = odd) N/A N/A\n32 Parity: (14 + 16 + 18. . . + 30 + 32 = odd) N/A N/A\nNote 1: Transmit at intervals of 1.0 second or less throughout the Approach Azimuth guidance sector, except when Back Azimuth guidance is provided. See Note 8.\nNote 2: The all zero state of the data field represents the lower limit of the absolute range of the coded parameter unless otherwise noted.\nBasic Data Word No. 5\n1 Preamble N/A 1\n2 1\n3 1\n4 0\n5 1\n6 1\n7 1\n8 0\n9 1\n10 1\n11 0\n12 0\n13 Back azimuth proportional coverage negative limit (0° to −42°) 2° −2°\n14 −4°\n15 −8°\n16 −16°\n17 −32°\n18 Back azimuth proportional coverage positive limit (0° to + 42°) 2° 2°\n19 4°\n20 8°\n21 16°\n22 32°\n23 Back azimuth beamwidth (0.5° to 4.0°) See note 7 0.5° 0.5°\n24 1.0°\n25 2.0°\n26 Back azimuth status See Note 10\n27 ......do Do.\n28 ......do Do.\n29 ......do Do.\n30 ......do Do.\n31 Parity: (13 + 14 + 15. . . + 30 + 31 = odd) N/A N/A\n32 Parity: (14 + 16 + 18. . . + 30 + 32 = odd) N/A N/A\nNote 1: Transmit only when Back Azimuth guidance is provided. See note 9.\nNote 2: The all zero state of the data filed represents the lower limit of the absolute range of the coded parameter unless otherwise noted.\nBasic Data Word No. 6\n1 Preamble N/A 1\n2 1\n3 1\n4 0\n5 1\n6 0\n7 0\n8 0\n9 1\n10 1\n11 0\n12 1\n(13- 30) MLS ground equipment identification (Note 3)\n13 Character 2 N/A B1\n14 B2\n15 B3\n16 B4\n17 B5\n18 B6\n19 Character 3 N/A B1\n20 B2\n21 B3\n22 B4\n23 B5\n24 B6\n25 Character 4 N/A B1\n26 B2\n27 B3\n28 B4\n29 B5\n30 B6\n31 Parity: (13 + 14 + 15. . . + 30 + 31 = odd) N/A N/A\n32 Parity: (14 + 16 + 18. . . + 30 + 32 = odd) N/A N/A\nNote 1: Transmit at intervals of 1.0 second or less throughout the Approach Azimuth guidance sector, except when Back Azimuth guidance is provided. See note 8.\nNote 3: Characters are encoded using the International Alphabet Number 5, (IA-5):\nNote 4: Coding for status bit:\n0 = Function not radiated, or radiated in test mode (not reliable for navigation).\n1 = Function radiated in normal mode (for Back Azimuth, this also indicates that a Back Azimuth transmission follows).\nNote 5: Date items which are not applicable to a particular ground equipment shall be transmitted as all zeros.\nNote 6: Coding for status bits:\nI21 I22\n0 0 DME transponder inoperative or not available.\n1 0 Only IA mode or DME/N available.\n0 0 FA mode, Standard 1, available.\n1 1 FA mode, Standard 2, available.\nNote 7: The value coded shall be the actual beamwidth (as defined in § 171.311 (j)(9) rounded to the nearest 0.5 degree.\nNote 8: When back Azimuth guidance is provided, Data Words 4 and 6 shall be transmitted at intervals of 1.33 seconds or less throughout the Approach Azimuth coverage and 4 seconds or less throughout the Back Azimuth coverage.\nNote 9: When Back Azimuth guidance is provided, Data Word 5 shall be transmitted at an interval of 1.33 seconds or less throughout the Back Azimuth coverage sector and 4 seconds or less throughout the Approach Azimuth coverage sector.\nNote 10: Coding for status bit:\n0 = Function not radiated, or radiated in test mode (not reliable for navigation).\n1 = Function radiated in normal mode.\n(4) Minimum glidepath the lowest angle of descent along the zero degree azimuth that is consistent with published approach procedures and obstacle clearance criteria.\n(5) Back azimuth status shall represent the operational status of the Back Azimuth equipment.\n(6) DME status shall represent the operational status of the DME equipment.\n(7) Approach azimuth status shall represent the operational status of the approach azimuth equipment.\n(8) Approach elevation status shall represent the operational status of the approach elevation equipment.\n(9) Beamwidth the width of the scanning beam main lobe measured at the −3 dB points and defined in angular units on the antenna boresight, in the horizontal plane for the azimuth function and in the vertical plane for the elevation function.\n(10) DME distance shall represent the minimum distance between the DME antenna phase center and the vertical plane perpendicular to the runway centerline which contains the MLS datum point.\n(11) Approach azimuth magnetic orientation shall represent the angle measured in the horizontal plane clockwise from Magnetic North to the zero-degree angle guidance radial originating from the approach azimuth antenna phase center. The vertex of the measured angle shall be at the approach azimuth antenna phase center.\nNote:\nFor example, this data item would be encoded 090 for an approach azimuth antenna serving runway 27 (assuming the magnetic heading is 270 degrees) when sited such that the zero degree radial is parallel to centerline.\n(12) Back azimuth magnetic orientation shall represent the angle measured in the horizontal plane clockwise from Magnetic North to the zero-degree angle guidance radial originating from the Back Azimuth antenna. The vertex of the measured angle shall be at the Back Azimuth antenna phase center.\nNote:\nFor example, this data item would be encoded 270 for a Back Azimuth Antenna serving runway 27 (assuming the magnetic heading is 270 degrees) when sited such that the zero degree radial is parallel to centerline.\n(13) Back azimuth proportional coverage limit shall represent the limit of the sector in which proportional back azimuth guidance is transmitted.\n(14) MLS ground equipment identification shall represent the last three characters of the system identification specified in § 171.311(i)(2). The characters shall be encoded in accordance with International Alphabet No. 5 (IA-5) using bits b1 through b6.\nNote:\nBit b7 of this code may be reconstructed in the airborne receiver by taking the complement of bit b6.\n(k) Residual radiation. The residual radiation of a transmitter associated with an MLS function during time intervals when it should not be transmitting shall not adversely affect the reception of any other function. The residual radiation of an MLS function at times when another function is radiating shall be at least 70 dB below the level provided when transmitting.\n(l) Symmetrical scanning. The TO and FRO scan transmissions shall be symmetrically disposed about the mid-scan point listed in Tables 4a, 4b and 5. The mid-scan point and the center of the time interval between the TO and FRO scan shall coincide with a tolerance of plus or minus 10 microseconds.\n(m) Auxiliary data—(1) Addresses. Three function identification codes are reserved to indicate transmission of Auxiliary Data A, Auxiliary Data B, 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.\n(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.\n(3) Auxiliary Data A content: The data items specified in Table 8c are defined as follows:\n(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.\n(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.\n(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.\n(iv) Approach azimuth antenna coordinate system shall represent the coordinate system (planar or conical) of the angle data transmitted by the approach azimuth antenna.\n(v) Approach elevation antenna offset shall represent the minimum distance between the elevation antenna phase center and the vertical plane containing the runway centerline.\n(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.\n(vii) Approach elevation antenna height shall represent the height of the elevation antenna phase center relative to the height of the MLS datum point.\n(viii) DME offset shall represent the minimum distance between the DME antenna phase center and the vertical plane containing the runway centerline.\n(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.\n(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.\n(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.\n(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.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER J—NAVIGATIONAL FACILITIES","PART 171—NON-FEDERAL NAVIGATION FACILITIES","Subpart J—Microwave Landing System (MLS)"],"source_url":"https://www.ecfr.gov/api/versioner/v1/full/2026-08-25/title-14.xml","current_through":"2026-08-25","vintage":"","retrieved_at":"2026-08-27T02:24:20Z","sha256":"98e672bcacdce11564b52d385e658cbf821fcf9f66a8618584b20ba7c4655ba7","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-171.309","next":"us/14-cfr-171.313"},"notice":"GroundRules: Original legal text. Not legal advice."}