haf flight manual f16

1. T.O. GR1F16CJ1FLIGHT MANUAL HAF SERIES AIRCRAFTF16C/DBLOCKS 50 AND 52+LOCKHEED MARTIN CORPORATION F3365790C2002 F4262001D0058GR1F-16C-1-0001XCommanders are responsible for bringing this publication to the attention of all Air Force personnel cleared for operation of subject aircraft.15 OCTOBER 2002 CHANGE 115 JUNE 2003

2. T.O. GR1F16CJ1DISCLOSURE STATEMENT This information is furnished on the conditions that it will not be released to another nation without the specific authorization of the Department of the Air Force of the United States; it will be used for military purposes only; the recipient will report promptly to the United States any known or suspected compromise; and the information will be provided substantially the same degree of security afforded it by the Department of Defense of the United States. Also, regardless of any other markings on the document, it will not be downgraded or declassified without the written approval of the originating US agency. Any request for this document should be referred to OOALC/YPXG, 6089 Wardleigh Road, Hill AFB, UT 840565838. SUPPLEMENTAL NOTICE This manual is incomplete without T.O. GR1F16CJ11 and T.O. GR1F16CJ12. SUPERSEDURE NOTICE See Technical Order Index, T.O. GR0171, for current status of Flight Manuals, Safety Supplements, Opera tional Supplements, and Flight Crew Checklists. This manual supersedes T.O. 11C130 and Interim Safety Supplements T.O. GR1F16CJ1SS27 and T.O. GR1F16CJ1SS29, and Interim Operational Supplement T.O. GR1F16CJ1S31.T2Change 1 3. T.O. GR1F16CJ1 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.LIST OF EFFECTIVE PAGES NOTE:Changes to the current issue are indicated by a vertical line in the outer margins of the page. Dates of issue for original and changed pages are: Original . . . 0 . . . . 15 Oct 02Change . . . . 1 . . . . 15 Jun 03TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 522, CONSISTING OF THE FOLLOWING: Page No.* Change No.Title . . . . . . . . . . . . . . . . . . . . T2 . . . . . . . . . . . . . . . . . . . . . . A ....................... B ....................... C ....................... D ....................... a ....................... b Blank . . . . . . . . . . . . . . . . . i ........................ ii . . . . . . . . . . . . . . . . . . . . . . . iii . . . . . . . . . . . . . . . . . . . . . . . iv . . . . . . . . . . . . . . . . . . . . . . . v........................ vi . . . . . . . . . . . . . . . . . . . . . . . vii . . . . . . . . . . . . . . . . . . . . . . viii . . . . . . . . . . . . . . . . . . . . . . 11 . . . . . . . . . . . . . . . . . . . . . . 12 . . . . . . . . . . . . . . . . . . . . . . 13 . . . . . . . . . . . . . . . . . . . . . . 14 . . . . . . . . . . . . . . . . . . . . . . 15 . . . . . . . . . . . . . . . . . . . . . . 16 . . . . . . . . . . . . . . . . . . . . . . 17 . . . . . . . . . . . . . . . . . . . . . . 18 . . . . . . . . . . . . . . . . . . . . . . 19 . . . . . . . . . . . . . . . . . . . . . . 110 . . . . . . . . . . . . . . . . . . . . . 111 . . . . . . . . . . . . . . . . . . . . . 112 . . . . . . . . . . . . . . . . . . . . . 113 . . . . . . . . . . . . . . . . . . . . . 114 . . . . . . . . . . . . . . . . . . . . . 115 . . . . . . . . . . . . . . . . . . . . . 116 . . . . . . . . . . . . . . . . . . . . . 117 . . . . . . . . . . . . . . . . . . . . . 118 . . . . . . . . . . . . . . . . . . . . . 119 . . . . . . . . . . . . . . . . . . . . . 120 . . . . . . . . . . . . . . . . . . . . . 121 . . . . . . . . . . . . . . . . . . . . . 122 . . . . . . . . . . . . . . . . . . . . . 123 . . . . . . . . . . . . . . . . . . . . . 124 . . . . . . . . . . . . . . . . . . . . . 125 . . . . . . . . . . . . . . . . . . . . . 126 . . . . . . . . . . . . . . . . . . . . . 127 . . . . . . . . . . . . . . . . . . . . .1 1 1 1 1 1 1 0 1 1 1 0 1 1 1 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 1 1 0 0Page No.* Change No.128 . . . . . . . . . . . . . . . . . . . . . 129 . . . . . . . . . . . . . . . . . . . . . 130 . . . . . . . . . . . . . . . . . . . . . 131 . . . . . . . . . . . . . . . . . . . . . 132 . . . . . . . . . . . . . . . . . . . . . 133 . . . . . . . . . . . . . . . . . . . . . 134 . . . . . . . . . . . . . . . . . . . . . 135 . . . . . . . . . . . . . . . . . . . . . 136 . . . . . . . . . . . . . . . . . . . . . 137 . . . . . . . . . . . . . . . . . . . . . 138 . . . . . . . . . . . . . . . . . . . . . 139 . . . . . . . . . . . . . . . . . . . . . 140 . . . . . . . . . . . . . . . . . . . . . 141 . . . . . . . . . . . . . . . . . . . . . 142 . . . . . . . . . . . . . . . . . . . . . 143 . . . . . . . . . . . . . . . . . . . . . 144 . . . . . . . . . . . . . . . . . . . . . 145 . . . . . . . . . . . . . . . . . . . . . 146 . . . . . . . . . . . . . . . . . . . . . 147 . . . . . . . . . . . . . . . . . . . . . 148 . . . . . . . . . . . . . . . . . . . . . 149 . . . . . . . . . . . . . . . . . . . . . 150 . . . . . . . . . . . . . . . . . . . . . 151 . . . . . . . . . . . . . . . . . . . . . 152 . . . . . . . . . . . . . . . . . . . . . 153 . . . . . . . . . . . . . . . . . . . . . 154 . . . . . . . . . . . . . . . . . . . . . 155 . . . . . . . . . . . . . . . . . . . . . 156 . . . . . . . . . . . . . . . . . . . . . 157 . . . . . . . . . . . . . . . . . . . . . 158 . . . . . . . . . . . . . . . . . . . . . 159 . . . . . . . . . . . . . . . . . . . . . 160 . . . . . . . . . . . . . . . . . . . . . 161 . . . . . . . . . . . . . . . . . . . . . 162 . . . . . . . . . . . . . . . . . . . . . 163 . . . . . . . . . . . . . . . . . . . . . 164 . . . . . . . . . . . . . . . . . . . . . 165 . . . . . . . . . . . . . . . . . . . . . 166 . . . . . . . . . . . . . . . . . . . . . 167 . . . . . . . . . . . . . . . . . . . . . 168 . . . . . . . . . . . . . . . . . . . . . 169 . . . . . . . . . . . . . . . . . . . . . 170 . . . . . . . . . . . . . . . . . . . . .0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1Page No.* Change No.171 . . . . . . . . . . . . . . . . . . . . . 172 . . . . . . . . . . . . . . . . . . . . . 173 . . . . . . . . . . . . . . . . . . . . . 174 . . . . . . . . . . . . . . . . . . . . . 175 . . . . . . . . . . . . . . . . . . . . . 176 . . . . . . . . . . . . . . . . . . . . . 177 . . . . . . . . . . . . . . . . . . . . . 178 . . . . . . . . . . . . . . . . . . . . . 179 . . . . . . . . . . . . . . . . . . . . . 180 . . . . . . . . . . . . . . . . . . . . . 181 . . . . . . . . . . . . . . . . . . . . . 182 . . . . . . . . . . . . . . . . . . . . . 183 . . . . . . . . . . . . . . . . . . . . . 184 . . . . . . . . . . . . . . . . . . . . . 185 . . . . . . . . . . . . . . . . . . . . . 186 . . . . . . . . . . . . . . . . . . . . . 187 . . . . . . . . . . . . . . . . . . . . . 188 . . . . . . . . . . . . . . . . . . . . . 189 . . . . . . . . . . . . . . . . . . . . . 190 . . . . . . . . . . . . . . . . . . . . . 191 . . . . . . . . . . . . . . . . . . . . . 192 . . . . . . . . . . . . . . . . . . . . . 193 . . . . . . . . . . . . . . . . . . . . . 194 . . . . . . . . . . . . . . . . . . . . . 195 . . . . . . . . . . . . . . . . . . . . . 196 . . . . . . . . . . . . . . . . . . . . . 197 . . . . . . . . . . . . . . . . . . . . . 198 . . . . . . . . . . . . . . . . . . . . . 199 . . . . . . . . . . . . . . . . . . . . . 1100 . . . . . . . . . . . . . . . . . . . . 1101 . . . . . . . . . . . . . . . . . . . . 1102 . . . . . . . . . . . . . . . . . . . . 1103 . . . . . . . . . . . . . . . . . . . . 1104 . . . . . . . . . . . . . . . . . . . . 1105 . . . . . . . . . . . . . . . . . . . . 1106 . . . . . . . . . . . . . . . . . . . . 1107 . . . . . . . . . . . . . . . . . . . . 1108 . . . . . . . . . . . . . . . . . . . . 1109 . . . . . . . . . . . . . . . . . . . . 1110 . . . . . . . . . . . . . . . . . . . . 1111 . . . . . . . . . . . . . . . . . . . . 1112 . . . . . . . . . . . . . . . . . . . . 1113 . . . . . . . . . . . . . . . . . . . .0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0* Zero in this column indicates an original page.B1 HAF Change 1A 4. T.O. GR1F16CJ1 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.LIST OF EFFECTIVE PAGES (Cont) Page No.*Change No.1114 . . . . . . . . . . . . . . . . . . . . 1115 . . . . . . . . . . . . . . . . . . . . 1116 . . . . . . . . . . . . . . . . . . . . 1117 . . . . . . . . . . . . . . . . . . . . 1118 . . . . . . . . . . . . . . . . . . . . 1119 . . . . . . . . . . . . . . . . . . . . 1120 . . . . . . . . . . . . . . . . . . . . 1121 . . . . . . . . . . . . . . . . . . . . 1122 . . . . . . . . . . . . . . . . . . . . 1123 . . . . . . . . . . . . . . . . . . . . 1124 . . . . . . . . . . . . . . . . . . . . 1125 . . . . . . . . . . . . . . . . . . . . 1126 . . . . . . . . . . . . . . . . . . . . 1127 . . . . . . . . . . . . . . . . . . . . 1128 . . . . . . . . . . . . . . . . . . . . 1129 . . . . . . . . . . . . . . . . . . . . 1130 . . . . . . . . . . . . . . . . . . . . 1131 . . . . . . . . . . . . . . . . . . . . 1132 . . . . . . . . . . . . . . . . . . . . 1133 . . . . . . . . . . . . . . . . . . . . 1134 . . . . . . . . . . . . . . . . . . . . 1135 . . . . . . . . . . . . . . . . . . . . 1136 . . . . . . . . . . . . . . . . . . . . 1137 . . . . . . . . . . . . . . . . . . . . 1138 . . . . . . . . . . . . . . . . . . . . 1139 . . . . . . . . . . . . . . . . . . . . 1140 . . . . . . . . . . . . . . . . . . . . 1141 . . . . . . . . . . . . . . . . . . . . 1142 . . . . . . . . . . . . . . . . . . . . 1143 . . . . . . . . . . . . . . . . . . . . 1144 . . . . . . . . . . . . . . . . . . . . 1145 . . . . . . . . . . . . . . . . . . . . 1146 . . . . . . . . . . . . . . . . . . . . 1147 . . . . . . . . . . . . . . . . . . . . 1148 . . . . . . . . . . . . . . . . . . . . 1149 . . . . . . . . . . . . . . . . . . . . 1150 . . . . . . . . . . . . . . . . . . . . 1151 . . . . . . . . . . . . . . . . . . . . 1152 . . . . . . . . . . . . . . . . . . . . 1153 . . . . . . . . . . . . . . . . . . . . 1154 . . . . . . . . . . . . . . . . . . . . 1155 . . . . . . . . . . . . . . . . . . . . 1156 . . . . . . . . . . . . . . . . . . . . 1157 . . . . . . . . . . . . . . . . . . . . 1158 . . . . . . . . . . . . . . . . . . . . 1159 . . . . . . . . . . . . . . . . . . . . 1160 . . . . . . . . . . . . . . . . . . . . 1161 . . . . . . . . . . . . . . . . . . . . 1162 . . . . . . . . . . . . . . . . . . . . 1163 . . . . . . . . . . . . . . . . . . . . 1164 . . . . . . . . . . . . . . . . . . . . 1165 . . . . . . . . . . . . . . . . . . . . 1166 . . . . . . . . . . . . . . . . . . . . 1167 . . . . . . . . . . . . . . . . . . . . 1168 . . . . . . . . . . . . . . . . . . . .0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0Page No.*Change No.1169 . . . . . . . . . . . . . . . . . . . . 1170 . . . . . . . . . . . . . . . . . . . . 1171 . . . . . . . . . . . . . . . . . . . . 1172 . . . . . . . . . . . . . . . . . . . . 1173 . . . . . . . . . . . . . . . . . . . . 1174 . . . . . . . . . . . . . . . . . . . . 1175 . . . . . . . . . . . . . . . . . . . . 1176 . . . . . . . . . . . . . . . . . . . . 1177 . . . . . . . . . . . . . . . . . . . . 1178 . . . . . . . . . . . . . . . . . . . . 1179 . . . . . . . . . . . . . . . . . . . . 1180 . . . . . . . . . . . . . . . . . . . . 1181 . . . . . . . . . . . . . . . . . . . . 1182 . . . . . . . . . . . . . . . . . . . . 1183 . . . . . . . . . . . . . . . . . . . . 1184 . . . . . . . . . . . . . . . . . . . . 1185 . . . . . . . . . . . . . . . . . . . . 1186 . . . . . . . . . . . . . . . . . . . . 1187 . . . . . . . . . . . . . . . . . . . . 1188 . . . . . . . . . . . . . . . . . . . . 1189 . . . . . . . . . . . . . . . . . . . . 1190 . . . . . . . . . . . . . . . . . . . . 1191 . . . . . . . . . . . . . . . . . . . . 1192 . . . . . . . . . . . . . . . . . . . . 1193 . . . . . . . . . . . . . . . . . . . . 1194 . . . . . . . . . . . . . . . . . . . . 1195 . . . . . . . . . . . . . . . . . . . . 1196 . . . . . . . . . . . . . . . . . . . . 1197 . . . . . . . . . . . . . . . . . . . . 1198 . . . . . . . . . . . . . . . . . . . . 1199 . . . . . . . . . . . . . . . . . . . . 1200 . . . . . . . . . . . . . . . . . . . . 1201 . . . . . . . . . . . . . . . . . . . . 1202 . . . . . . . . . . . . . . . . . . . . 1203 . . . . . . . . . . . . . . . . . . . . 1204 . . . . . . . . . . . . . . . . . . . . 1205 . . . . . . . . . . . . . . . . . . . . 1206 . . . . . . . . . . . . . . . . . . . . 1207 . . . . . . . . . . . . . . . . . . . . 1208 . . . . . . . . . . . . . . . . . . . . 1209 . . . . . . . . . . . . . . . . . . . . 1210 . . . . . . . . . . . . . . . . . . . . 1211 . . . . . . . . . . . . . . . . . . . . 1212 . . . . . . . . . . . . . . . . . . . . 1213 . . . . . . . . . . . . . . . . . . . . 1214 . . . . . . . . . . . . . . . . . . . . 1215 . . . . . . . . . . . . . . . . . . . . 1216 . . . . . . . . . . . . . . . . . . . . 1217 . . . . . . . . . . . . . . . . . . . . 1218 . . . . . . . . . . . . . . . . . . . . 1219 . . . . . . . . . . . . . . . . . . . . 1220 . . . . . . . . . . . . . . . . . . . . 1221 . . . . . . . . . . . . . . . . . . . . 1222 . . . . . . . . . . . . . . . . . . . . 1223 . . . . . . . . . . . . . . . . . . . .0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 1 1 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1* Zero in this column indicates an original page.BChange 1Page No.*Change No.1224 . . . . . . . . . . . . . . . . . . . . 1225 . . . . . . . . . . . . . . . . . . . . 1226 . . . . . . . . . . . . . . . . . . . . 21 . . . . . . . . . . . . . . . . . . . . . . 22 . . . . . . . . . . . . . . . . . . . . . . 23 . . . . . . . . . . . . . . . . . . . . . . 24 . . . . . . . . . . . . . . . . . . . . . . 25 . . . . . . . . . . . . . . . . . . . . . . 26 . . . . . . . . . . . . . . . . . . . . . . 27 . . . . . . . . . . . . . . . . . . . . . . 28 . . . . . . . . . . . . . . . . . . . . . . 29 . . . . . . . . . . . . . . . . . . . . . . 210 . . . . . . . . . . . . . . . . . . . . . 211 . . . . . . . . . . . . . . . . . . . . . 212 . . . . . . . . . . . . . . . . . . . . . 213 . . . . . . . . . . . . . . . . . . . . . 214 . . . . . . . . . . . . . . . . . . . . . 215 . . . . . . . . . . . . . . . . . . . . . 216 . . . . . . . . . . . . . . . . . . . . . 217 . . . . . . . . . . . . . . . . . . . . . 218 . . . . . . . . . . . . . . . . . . . . . 219 . . . . . . . . . . . . . . . . . . . . . 220 . . . . . . . . . . . . . . . . . . . . . 221 . . . . . . . . . . . . . . . . . . . . . 222 . . . . . . . . . . . . . . . . . . . . . 223 . . . . . . . . . . . . . . . . . . . . . 224 . . . . . . . . . . . . . . . . . . . . . 225 . . . . . . . . . . . . . . . . . . . . . 226 . . . . . . . . . . . . . . . . . . . . . 227 . . . . . . . . . . . . . . . . . . . . . 228 . . . . . . . . . . . . . . . . . . . . . 229 . . . . . . . . . . . . . . . . . . . . . 230 . . . . . . . . . . . . . . . . . . . . . 231 . . . . . . . . . . . . . . . . . . . . . 232 . . . . . . . . . . . . . . . . . . . . . 233 . . . . . . . . . . . . . . . . . . . . . 234 . . . . . . . . . . . . . . . . . . . . . 235 . . . . . . . . . . . . . . . . . . . . . 236 . . . . . . . . . . . . . . . . . . . . . 237 . . . . . . . . . . . . . . . . . . . . . 238 . . . . . . . . . . . . . . . . . . . . . 239 . . . . . . . . . . . . . . . . . . . . . 240 . . . . . . . . . . . . . . . . . . . . . 241 . . . . . . . . . . . . . . . . . . . . . 242 . . . . . . . . . . . . . . . . . . . . . 31 . . . . . . . . . . . . . . . . . . . . . . 32 . . . . . . . . . . . . . . . . . . . . . . 33 . . . . . . . . . . . . . . . . . . . . . . 34 . . . . . . . . . . . . . . . . . . . . . . 35 . . . . . . . . . . . . . . . . . . . . . . 36 . . . . . . . . . . . . . . . . . . . . . . 37 . . . . . . . . . . . . . . . . . . . . . . 38 . . . . . . . . . . . . . . . . . . . . . . 39 . . . . . . . . . . . . . . . . . . . . . . 310 . . . . . . . . . . . . . . . . . . . . .0 0 0 0 0 0 0 1 0 0 0 0 0 0 1 1 0 0 0 1 0 0 0 0 0 1 0 0 1 0 0 0 1 0 0 0 1 1 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 1 0 5. T.O. GR1F16CJ1 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.LIST OF EFFECTIVE PAGES (Cont) Page No.*Change No.311 . . . . . . . . . . . . . . . . . . . . . 312 . . . . . . . . . . . . . . . . . . . . . 313 . . . . . . . . . . . . . . . . . . . . . 314 . . . . . . . . . . . . . . . . . . . . . 315 . . . . . . . . . . . . . . . . . . . . . 316 . . . . . . . . . . . . . . . . . . . . . 317 . . . . . . . . . . . . . . . . . . . . . 318 . . . . . . . . . . . . . . . . . . . . . 319 . . . . . . . . . . . . . . . . . . . . . 320 . . . . . . . . . . . . . . . . . . . . . 321 . . . . . . . . . . . . . . . . . . . . . 322 . . . . . . . . . . . . . . . . . . . . . 323 . . . . . . . . . . . . . . . . . . . . . 324 . . . . . . . . . . . . . . . . . . . . . 325 . . . . . . . . . . . . . . . . . . . . . 326 . . . . . . . . . . . . . . . . . . . . . 327 . . . . . . . . . . . . . . . . . . . . . 328 . . . . . . . . . . . . . . . . . . . . . 329 . . . . . . . . . . . . . . . . . . . . . 330 . . . . . . . . . . . . . . . . . . . . . 331 . 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T.O. GR1F16CJ1 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.LIST OF EFFECTIVE PAGES (Cont) Page No.*Change No.66 . . . . . . . . . . . . . . . . . . . . . . 67 . . . . . . . . . . . . . . . . . . . . . . 68 . . . . . . . . . . . . . . . . . . . . . . 69 . . . . . . . . . . . . . . . . . . . . . . 610 . . . . . . . . . . . . . . . . . . . . . 611 . . . . . . . . . . . . . . . . . . . . . 612 . . . . . . . . . . . . . . . . . . . . . 613 . . . . . . . . . . . . . . . . . . . . . 614 . . . . . . . . . . . . . . . . . . . . . 615 . . . . . . . . . . . . . . . . . . . . . 616 . . . . . . . . . . . . . . . . . . . . . 71 . . . . . . . . . . . . . . . . . . . . . . 72 . . . . . . . . . . . . . . . . . . . . . . 73 . . . . . . . . . . . . . . . . . . . . . . 74 . . . . . . . . . . . . . . . . . . . . . . 75 . . . . . . . . . . . . . . . . . . . . . . 76 . . . . . . . . . . . . . . . . . . . . . . 77 . . . . . . . . . . . . . . . . . . . . . . 78 . . . . . . . . . . . . . . . . . . . . . . 81 Added . . . . . . . . . . . . . . . 82 Added . . . . . . . . . . . . . . . 83 Added . . . . . . . . . . . . . . . 84 Added . . . . . . . . . . . . . . . 85 Added . . . . . . . . . . . . . . . 86 Added . . . . . . . . . . . . . . . 87 Added . . . . . . . . . . . . . . . 88 Added . . . . . . . . . . . . . . . 89 Added . . . . . . . . . . . . . . . 810 Added . . . . . . . . . . . . . . 811 Added . . . . . . . . . . . . . . 812 Added . . . . . . . . . . . . . . 813 Added . . . . . . . . . . . . . . 814 Added . . . . . . . . . . . . . . 815 Added . . . . . . . . . . . . . . 816 Added . . . . . . . . . . . . . . 817 Added . . . . . . . . . . . . . . 818 Added . . . . . . . . . . . . . . 819 Added . . . . . . . . . . . . . . 820 Added . . . . . . . . . . . . . . 821 Added . . . . . . . . . . . . . . 822 Added . . . . . . . . . . . . . . 823 Added . . . . . . . . . . . . . . 824 Added . . . . . . . . . . . . . . 825 Added . . . . . . . . . . . . . . 826 Added . . . . . . . . . . . . . . 827 Added . . . . . . . . . . . . . . 828 Added . . . . . . . . . . . . . . 829 Added . . . . . . . . . . . . . . 830 Added . . . . . . . . . . . . . . 831 Added . . . . . . . . . . . . . . 832 Added . . . . . . . . . . . . . . 833 Added . . . . . . . . . . . . . . 834 Added . . . . . . . . . . . . . . 835 Added . . . . . . . . . . . . . . 836 Added . . . . . . . . . . . . . .0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1Page No.*Change No.837 Added . . . . . . . . . . . . . . 838 Blank Added . . . . . . . . Glossary 1 . . . . . . . . . . . . . . . Glossary 2 . . . . . . . . . . . . . . . Glossary 3 . . . . . . . . . . . . . . . Glossary 4 . . . . . . . . . . . . . . . Glossary 5 . . . . . . . . . . . . . . . Glossary 6 Blank . . . . . . . . .1 1 1 1 1 1 0 0* Zero in this column indicates an original page.DChange 1Page No.*Change No. 7. T.O. GR1F16CJ1 FLIGHT MANUALS, SAFETY SUPPLEMENT, AND OPERATIONAL SUPPLEMENT STATUS This supplement status page is based on information available as of 15 June 2003. It is not an official status page. Flight ManualBasic DateChange No. and DateT.O. GR1F16CJ115 Oct 20021Supplemental Flight ManualsBasic DateChange No. and DateT.O. GR1F16CJ119 Jun 1997715 Nov 2002T.O. GR1F16CJ1215 Feb 2000515 Mar 2003Flight Crew ChecklistBasic DateChange No. and DateT.O. GR1F16CJ1CL115 Oct 2002115 Jun 200315 Jun 2003INCORPORATED SAFETY AND OPERATIONAL SUPPLEMENTS Flight Manual Sections AffectedT.O. NumberDateShort TitleGR1F16CJ1SS2727 Nov 02FLCS Failure That Results In Loss Of Pitch ControlIIIGR1F16CJ1SS2929 Jan 03Max Range Speeds and FO Pattern AltitudesIIIGR1F16CJ1S3130 Apr 03Fuel Transfer Switch, Avionics Fault & ECM Lights, and EGI AlignIIOUTSTANDING SAFETY AND OPERATIONAL SUPPLEMENTS T.O. NumberDateShort TitleFlight Manual Sections AffectedNoneChange 1a/(b blank) 8. T.O. GR1F16CJ1TABLE OF CONTENTS SECTION IDescription and Operation11SECTION IINormal Procedures21SECTION IIIEmergency Procedures31SECTION IVCrew Duties41SECTION VOperating Limitations51SECTION VOperating Limitations (Stores)SECTION VIFlight Characteristics61SECTION VIIAdverse Weather Operation71SECTION VIIIAir Refueling Procedures81GLOSSARYStandard and Nonstandard AbbreviationsAPPENDIX APerformance Data-F100PW229T.O. GR1F16CJ11APPENDIX BPerformance Data-F110GE129T.O. GR1F16CJ11APPENDIX CPerformance Data-F100PW229/CFTT.O. GR1F16CJ11T.O. GR1F16CJ12Glossary 1Change 1i 9. T.O. GR1F16CJ1BEFORE YOU TAKE OFF, READ THIS!1F-16X-1-0002XT.O. GR1F16CJ6CF1SCOPE This manual contains the necessary information for safe and efficient operation of the aircraft. These instructions provide a general knowledge of the aircraft and its characteristics and specific normal and emergency operating procedures. Pilot experi ence is recognized; therefore, basic flight principles are avoided. Instructions in this manual are prepared to be understandable to the least experienced pilot who can be expected to operate the aircraft. This manual provides the best possible operating instruc tions under most conditions. Multiple emergencies, adverse weather, terrain, etc., may require modifica tion of the procedures. This manual must be used with one or more of the following manuals to obtain information necessary for safe and efficient opera tion: T.O. GR1F16CJ11Supplemental Flight Manual, F16C/D Air craftT.O. GR1F16CJ12Supplemental Flight Manual, F16C/D Air craftT.O. GR1F16CJ52Loading DataiiChange 1Acceptance and Func tional Check Flight Procedures Manual, F16C/D AircraftT.O. GR1F16CJ3411Avionics and Nonnu clear Weapons Deliv ery Flight ManualT.O. GR1F16CJ3412Nonnuclear Weapons BallisticsT.O. 11C1Basic Flight Crew Air Refueling ProceduresPERMISSIBLE OPERATIONS The flight manual takes a positive approach and normally states only what can be done. Unusual operations or configurations are prohibited unless specifically covered herein. Clearance must be obtained before any questionable operation which is not specifically permitted in this manual is attempted. 10. T.O. GR1F16CJ1 HOW TO BE ASSURED OF HAVING LATEST DATASAFETY SUPPLEMENTSRefer to T.O. GR0171 for a listing of all current flight manuals, safety supplements, operational supple ments, and checklists. Also, check the flight manual title page, the title block of each safety and operational supplement, and all status pages contained in the flight manual or attached to formal safety and operational supplements. Clear all discrepancies before flight.Information involving safety is promptly forwarded in a safety supplement. Urgent information is published in interim safety supplements and transmitted by electronic message. Formal supple ments are mailed. The supplement title block and status page (published with formal supplements only) should be checked to determine the effect of the supplement on this manual and other outstanding supplements.ARRANGEMENT The manual is divided into eight sections and three supplemental appendices. ILLUSTRATIONS Cockpit arrangement, cockpit console, and cockpit instrument panel illustrations display the delivered configuration plus the approved equipment modifica tions. For details of equipment modification, see the individual equipment illustration. SUPPLEMENT INFORMATION AND GUIDELINES Supplements are safety or operational and are indicated 1SS or 1S, respectively. Supplements are issued as interim electronic messages or formal printed copies. All interim supplements are assigned odd numbers, such as 1SS195. When an interim supplement is formalized, it is assigned the next following even number, such as 1SS196. Formal supplements not preceded by an interim supplement are also assigned even numbers. If an interim supplement is not to be formalized, a statement cancelling the next assigned even supplement number is included in the REMARKS section of the interim supplement. If a formal supplement is not preceded by an interim supplement, a statement cancelling the previous odd supplement number is included on the status page of the formal supplement. Occasionally, a supplement has dual references in the instructions; this is because the supplement applies to the present and subsequent manual. Minor text/illustration changes or deletions are given as instructions in the supplement. When lengthy additions are required, the formal supplement provides onesided insert page(s) to the flight manual and checklist. This supplement page(s) is attached to the original page(s). The original page(s) remains in the manual or checklist in case the supplement is rescinded and the page(s) is needed. Added page(s) (e.g., 348.1) are inserted in proper numerical sequence and may be printed on both sides.OPERATIONAL SUPPLEMENTS Information involving changes to operating proce dures is forwarded by operational supplements. The procedure for handling operational supplements is the same as for safety supplements. CHECKLIST The checklist contains itemized procedures without all of the amplification. Primary line items in the flight manual and checklist are identical. HOW TO GET PERSONAL COPIES Each pilot is entitled to a personal copy of the flight manual, safety supplements, operational supple ments, and a checklist. The required quantities should be ordered before needed to assure their timely receipt. Check with the publication distribu tion officer whose job is to fulfill T.O. requests. Country manuals and difference data are assigned a Country Standard T.O. (CSTO) number and indexed in the Security Assistance Program T.O. Index, T.O. GR0171. Updates, stock, store, and issue of CSTO's are a contractor supported function. Insure a system is established at each base to deliver the publications to the pilots immediately upon receipt. FLIGHT MANUAL BINDERS Looseleaf binders and sectionalized tabs are avail able for use with the manual. They are obtained through local purchase procedures and are listed in the USAF supply channels and may be ordered on the supply case through AFLC. Check with supply personnel for assistance in procuring these items. CHANGE SYMBOL The change symbol, as illustrated by the black line in the margin of this paragraph, indicates changes made to the current issue.Change 1iii 11. T.O. GR1F16CJ1 WARNINGS, CAUTIONS, AND NOTES The following definitions apply to Warnings, Cautions, and Notes found throughout the manual:regarding this manual or any phase of the flight manual program are welcomed. These should be forwarded on AF Form 847 in accordance with AFI 11215 through command headquarters to OOALC/ YPVT, 6080 Gum Lane, Hill AFB, UT 840565825. PUBLICATION DATEOperating procedures, techniques, etc., which could result in personal injury or loss of life if not carefully followed.Operating procedures, techniques, etc., which could result in damage to equipment if not carefully followed.The date appearing on the title page represents the currency of material contained herein. AIRCRAFT AND COCKPIT DESIGNATION CODES System and/or component effectivity for a particular aircraft version/cockpit is denoted by a letter code enclosed in a box located in the text or on an illustration. The symbols and designations are as follows: No code-F16C and F16D aircraftNOTECF16C aircraftAn operating procedure, technique, etc., which is considered essential to emphasize.DF16D aircraftDFF16D aircraft, forward cockpitDRF16D aircraft, rear cockpitPX IIPeace Xenia II aircraftPX IIIPeace Xenia III aircraftUSE OF WORDS SHALL, WILL, SHOULD, AND MAY The word shall or will is used to indicate a mandatory requirement. The word should is used to indicate a nonmandatory desired or preferred method of accomplishment. The word may is used to indicate an acceptable or suggested means of accomplishment. USE OF WORDS AS DESIRED AND AS REQUIRED As desired allows pilot preference in switch/control positioning. As required indicates those actions which vary based on mission requirements.ENGINE DESIGNATION CODES System and/or component effectivity for a particular engine version is denoted by an engine code enclosed in a box located in the text or on an illustration. The symbols and designations are as follows: No code-Either engine PW 229F100PW229GE 129F110GE129AIRSPEED REFERENCES All references to airspeed quoted in knots refer to indicated airspeed. PILOT'S RESPONSIBILITY-TO LET US KNOW Every effort is made to keep the flight manual current. Review conferences with operating person nel and a constant review of safety investigation and flight test reports assure inclusion of the latest data in the manual. Comments, corrections, and questionsivBLOCK DESIGNATION CODES/SERIAL NUMBER/ TAIL NUMBER CROSSREFERENCE Because of differences in configuration between aircraft and to avoid repetitious use of aircraft serial numbers, a block effectivity system is used. The block effectivities reflect the aircraft block, the aircraft serial number, and the tail number. Attrited aircraft are removed from the listing. This system is used throughout the manual, both in text and illustra tions. 12. T.O. GR1F16CJ1 AIRCRAFT MODIFICATION/RETROFIT INFORMA TION This list includes the applicable T.O./ECP effectivi ties. It is not an official status page. Refer to T.O. 014 for the complete listing of TCTO's. Throughout this manual, black TV screen symbols containing white numerals ((2)) are used to distinguish information related to aircraft which are modified by a specific TV CODE/ T.O. NO. b1q1F162121SHORT TITLE Flight Control Com puter Software Up date (ECP 2269)T.O./ECP. Information pertaining to modified aircraft is identified by an appropriate effectivity symbol. Information which is not identified by an effectivity symbol is considered common to all aircraft. Information pertaining only to unmodified aircraft has the appropriate effectivity symbol preceded by LESS. For example, LESS (4) indicates that the information is only applicable to aircraft not modified by a specific T.O./ECP. EFFECTIVITY PRODUCTION RETROFIT F16C 931055, and onF16C 931045 thru 931054F16D NAF16D AllSummary: D Db2pRetrofit authorized Modification incorporates FLCS improvements, including improved reset capability for FLCC pow er up failures and elimination of lateral accelerometer failures during gun firing.1F162170Modification of the Ejection Mode Selec tor Valve Console (ECP 2362)F16C NAF16C NAF16D 991534, and onF16D 931077 thru 931084F16C 991500, and onF16C 931045 thru 931076F16D 991534, and onF16D 931077 thru 931084Summary: D Retrofit authorized D Modification enlarges the hole in the console to allow the EJECTION MODE SEL handle to seat properly in the NORM position. b2tXX1F162077Summary: D Db6nNAInstallation of Improved Antiskid Braking System (OCP H086) (ECP 2478)Retrofit authorized Modification incorporates an improved Brake Control/Antiskid Assembly to replace the current Brake Control and Antiskid Control Boxes.Flight Control Com puter Software Up date for CFT (ECP 2495)F16C 991500, and onNAF16D 991534, Summary: and on D Retrofit NA D Modification incorporates flight control system software updates to provide increased roll rate capa bility in CAT III with CFT's and eliminate an existing prohibited maneuver.Change 1v 13. T.O. GR1F16CJ1 TV CODE/ T.O. NO. b7nTBDSHORT TITLE AVIONICS FAULT caution/ECM lights CDEEU mod (ECP 2526)EFFECTIVITY PRODUCTION RETROFIT F16C 991507, and onTBDF16D 991541, Summary: and on D Retrofit TBD D Modification to circuitry in the CDEEU which will allow the AVIONICS FAULT caution and ECM lights to illuminate in both cockpits of PX III D aircraft.viChange 1 14. T.O. GR1F16CJ1Block Designation Codes/Serial Number/Tail Number CrossReference BLOCK 50 Serial Numbers/ Tail NumbersC PX II 931045/045 931046/046 931047/047 931048/048 931049/049 931050/050 931051/051 931052/052 931053/053 931054/054 931055/055 931056/056 931057/057 931058/058 931059/059 931060/060 931061/061 931062/062 931063/063 931064/064 931065/065 931066/066 931067/067 931068/068 931069/069 931070/070 931071/071 931072/072 931073/073 931074/074 931075/075 931076/076D PX II 931077/077 931078/078 931079/079931080/080 931081/081 931082/082 931083/083 931084/084BLOCK 52+ Serial Numbers/ Tail NumbersC PX III 991500/500 991501/501 991502/502 991503/503 991504/504 991505/505 991506/506 991507/507 991508/508 991509/509 991510/510 991511/511 991512/512 991513/513 991514/514 991515/515 991516/516 991517/517 991518/518 991519/519 991520/520 991521/521 991522/522 991523/523 991524/524 991525/525 991526/526 991527/527 991528/528 991529/529 991530/530 991531/531 991532/532991533/533 018530/534 018531/535 018532/536 018533/537 018534/538 018535/539D PX III 991534/600 991535/601 991536/602 991537/603 991538/604 991539/605 991540/606 991541/607 991542/608 991543/609 991544/610 991545/611 991546/612 991547/613 991548/614 991549/615 018536/616 018537/617 018538/618 018539/619Change 1vii 15. T.O. GR1F16CJ1CDGR1F-16CJ-1-0003A37viiiChange 1 16. T.O. GR1F16CJ1SECTION I DESCRIPTION AND OPERATION TABLE OF CONTENTS The Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Aircraft General Data . . . . . . . . . . . . . . . . . . . Aircraft General Arrangement . . . . . . . . . . . Aircraft Gross Weight (A/C GW) . . . . . . . . . . Cockpit Arrangement . . . . . . . . . . . . . . . . . . . . Engine PW 229 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine General Description PW 229 . . . . . . Engine Fuel System PW 229 . . . . . . . . . . . . . Engine Control System PW 229 . . . . . . . . . . . Main Fuel Control (MFC) PW 229 . . . . . . Afterburner (AB) Fuel Control PW 229 . . . . . . . . . . . . . . . . . . . . Digital Electronic Engine Control (DEEC) PW 229 . . . . . . . . . . . . . . . . . . . . Secondary Engine Control (SEC) PW 229 . . . . . . . . . . . . . . . . . . . . . . Main Fuel Pump PW 229 . . . . . . . . . . . . . . Afterburner (AB) Fuel Pump PW 229 . . . . . . . . . . . . . . . . . . . . . . Compressor Inlet Variable Vane (CIVV) Control PW 229 . . . . . . . . . . . . . Rear Compressor Variable Vanes (RCVV's) PW 229 . . . . . . . . . . . . . . . . . . . Compressor Bleed Air PW 229 . . . . . . . . . Pressurization and Dump Valve PW 229 . . . . . . . . . . . . . . . . . . . . . . Exhaust Nozzle PW 229 . . . . . . . . . . . . . . . . . . Convergent Exhaust Nozzle Control (CENC) PW 229 . . . . . . . . . . . . . . . . . . . . LightOff Detector (LOD) PW 229 . . . . . . Engine Diagnostic Unit (EDU) PW 229 . . . . Engine Oil System PW 229 . . . . . . . . . . . . . . . FUEL/OIL HOT Caution Light PW 229 . . . . . . . . . . . . . . . . . . . . . . Engine AntiIce System PW 229 . . . . . . . . . . Engine ANTI ICE Switch PW 229 . . . . . . INLET ICING Caution Light PW 229 . . . . . . . . . . . . . . . . . . . . . . Engine and Accessory Drive Gearboxes PW 229 . . . . . . . . . . . . . . . . . . . . Engine Alternator PW 229 . . . . . . . . . . . . . . . Engine Ignition System PW 229 . . . . . . . . . .16 17 17 17 17 131 131 131 131 131 131 133 133 133 133 133 133 134 134 134 134 134 134 134 134 135 135 135 135 135 135Jet Fuel Starter (JFS) PW 229 . . . . . . . . . . . . ENG & JET START Control Panel PW 229 . . . . . . . . . . . . . . . . . . . . . . . . JFS Switch C DF PW 229 . . . . . . . . . . . . . JFS RUN Light C DF PW 229 . . . . . . . . . JFS Operation PW 229 . . . . . . . . . . . . . . . . Engine Controls and Indicators PW 229 . . . . . . . . . . . . . . . . . . . . ENG CONT Switch PW 229 . . . . . . . . . . . . AB RESET Switch C DF PW 229 . . . . . . ENGINE FAULT Caution Light PW 229 . . . . . . . . . . . . . . . . . . . . . . Pilot Fault List Display (PFLD) PW 229 . . . . . . . . . . . . . . . . . . . . SEC Caution Light PW 229 . . . . . . . . . . . . EEC Caution Light PW 229 . . . . . . . . . . . . BUC Caution Light PW 229 . . . . . . . . . . . . MAX POWER Switch C DF PW 229 . . . . RPM Indicator PW 229 . . . . . . . . . . . . . . . . NOZ POS Indicator PW 229 . . . . . . . . . . . . FTIT Indicator PW 229 . . . . . . . . . . . . . . . . FUEL FLOW Indicator PW 229 . . . . . . . . OIL Pressure Indicator PW 229 . . . . . . . . HYD/OIL PRESS Warning Light PW 229 . . . . . . . . . . . . . . . . . . . . . . ENGINE Warning Light PW 229 . . . . . . . Throttle PW 229 . . . . . . . . . . . . . . . . . . . . . . Engine Operating Characteristics PW 229 . . . . . . . . . . . . . . . . Engine General PW 229 . . . . . . . . . . . . . . . Ground Operations PW 229 . . . . . . . . . . . . NonAB Operation in Flight PW 229 . . . . . . . . . . . . . . . . . . . . . . AB Operation in Flight PW 229 . . . . . . . . SEC Operation PW 229 . . . . . . . . . . . . . . . . Engine GE 129 . . . . . . . . . . . . . . . . . . . . . . . . . . . . General Description GE 129 . . . . . . . . . . . . . Engine Fuel/Control System GE 129 . . . . . . Digital Electronic Control (DEC) GE 129 . . . . . . . . . . . . . . . . . . . . . Afterburner Fuel Control (AFC) GE 129 . . . . . . . . . . . . . . . . . . . . . . Main Engine Control (MEC) GE 129 . . . Primary (PRI) Engine Operation GE 129 . . . . . . . . . . . . . . . . . .136 136 136 136 137 137 137 139 139 139 139 139 139 139 139 139 139 139 139 139 140 140 140 140 140 140 142 142 144 144 144 144 144 144 14411 17. T.O. GR1F16CJ1 Hybrid (HYB) Engine Operation GE 129 . . . . . . . . . . . . . . . . . . Secondary Engine Control (SEC) Operation GE 129 . . . . . . . . . . . . . . . . . . Engine Fuel Boost Pump GE 129 . . . . . . . Main Fuel Pump GE 129 . . . . . . . . . . . . . . Afterburner (AB) Fuel Pump GE 129 . . . . . . . . . . . . . . . . . . . . . . Inlet Guide Vanes (IGV's) GE 129 . . . . . . Variable Stator Vanes (VSV's) GE 129 . . . . . . . . . . . . . . . . . . . . . Compressor Bleed Air GE 129 . . . . . . . . . Exhaust Nozzle GE 129 . . . . . . . . . . . . . . . . . . AB Flame Detector GE 129 . . . . . . . . . . . . . . Engine Monitoring System (EMS) GE 129 . . . . . . . . . . . . . . . . . . . . . . . . Engine Oil System GE 129 . . . . . . . . . . . . . . . FUEL/OIL HOT Caution Light GE 129 . . . . . . . . . . . . . . . . . . . . . . Engine AntiIce System GE 129 . . . . . . . . . . Engine ANTI ICE Switch GE 129 . . . . . . INLET ICING Caution Light GE 129 . . . . . . . . . . . . . . . . . . . . . . Engine and Accessory Drive Gearboxes GE 129 . . . . . . . . . . . . . . . . . . . . Engine Alternator GE 129 . . . . . . . . . . . . . . . Engine Ignition System GE 129 . . . . . . . . . . Jet Fuel Starter (JFS) GE 129 . . . . . . . . . . . . ENG & JET START Control Panel GE 129 . . . . . . . . . . . . . . . . . . . . . . . . JFS Switch C DF GE 129 . . . . . . . . . . . . . JFS RUN Light C DF GE 129 . . . . . . . . . JFS Operation GE 129 . . . . . . . . . . . . . . . . Engine Controls and Indicators GE 129 . . . . . . . . . . . . . . . . . . . . ENG CONT Switch GE 129 . . . . . . . . . . . . SEC Caution Light GE 129 . . . . . . . . . . . . EEC Caution Light GE 129 . . . . . . . . . . . . BUC Caution Light GE 129 . . . . . . . . . . . . MAX POWER Switch C DF GE 129 . . . . AB RESET Switch C DF GE 129 . . . . . . ENGINE FAULT Caution Light GE 129 . . . . . . . . . . . . . . . . . . . . . . Pilot Fault List Display (PFLD) GE 129 . . . . . . . . . . . . . . . . . . . . RPM Indicator GE 129 . . . . . . . . . . . . . . . NOZ POS Indicator GE 129 . . . . . . . . . . . . FTIT Indicator GE 129 . . . . . . . . . . . . . . . . FUEL FLOW Indicator GE 129 . . . . . . . . OIL Pressure Indicator GE 129 . . . . . . . .12146 147 147 147 147 147 147 147 147 148 148 148 148 148 149 149 149 149 149 150 150 150 151 151 151 151 153 153 153 153 153 153 153 153 153 153 153 153HYD/OIL PRESS Warning Light GE 129 . . . . . . . . . . . . . . . . . . . . . . ENGINE Warning Light GE 129 . . . . . . . Throttle GE 129 . . . . . . . . . . . . . . . . . . . . . . Engine Operating Characteristics GE 129 . . . . . . . . . . . . . . . Ground Operations GE 129 . . . . . . . . . . . . NonAB Operation in Flight GE 129 . . . . AB Operation GE 129 . . . . . . . . . . . . . . . . . Inlet Thump GE 129 . . . . . . . . . . . . . . . . . . SEC Operation GE 129 . . . . . . . . . . . . . . . . Fire and Overheat Detection System . . . . . . . . FIRE & OHEAT DETECT Test Button C DF . . . . . . . . . . . . . . . . . . . . . . . . Fuel System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel Tank System . . . . . . . . . . . . . . . . . . . . . . . Fuel Transfer System . . . . . . . . . . . . . . . . . . . . Fuel Tank Vent and Pressurization System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Fuel Supply System . . . . . . . . . . . . . . Fuel Quantity Indicating System . . . . . . . . . Reservoir Fuel Level Sensing System . . . . . Fuel Low Caution Lights . . . . . . . . . . . . . . HUD FUEL Low/Bingo Indication . . . . . . . . HUD TRP FUEL Warning . . . . . . . . . . . . . . . FUEL/OIL HOT Caution Light . . . . . . . . . . Fuel Tank Explosion Suppression System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Refueling System . . . . . . . . . . . . . . . . . . . . . . . Ground Refueling . . . . . . . . . . . . . . . . . . . . . Air Refueling (AR) System . . . . . . . . . . . . . NWS A/R DISC MSL STEP Button . . . . . . . . . . . . . . . . . . . . . . . . . . Air Refueling (AR) Status Indicator . . . . . . . . . . . . . . . . . . . . . . . . Environmental Control System (ECS) . . . . . . . Electrical Failures . . . . . . . . . . . . . . . . . . . . . . AirConditioning . . . . . . . . . . . . . . . . . . . . . . . . Pressurization . . . . . . . . . . . . . . . . . . . . . . . . . . AIR SOURCE Knob C DF . . . . . . . . . . . . . TEMP Knob C DF . . . . . . . . . . . . . . . . . . . . DEFOG Lever C DF . . . . . . . . . . . . . . . . . . EQUIP HOT Caution Light . . . . . . . . . . . . Cockpit Pressure Altimeter C DF . . . . . . CABIN PRESS Caution Light . . . . . . . . . . AntiG System . . . . . . . . . . . . . . . . . . . . . . . . . . Electrical System . . . . . . . . . . . . . . . . . . . . . . . . . . Main AC Power System . . . . . . . . . . . . . . . . . . Overcurrent Sensing Contactors . . . . . . .153 154 154 154 154 154 156 156 156 158 158 158 158 158 161 161 174 174 174 174 174 177 177 177 177 177 178 178 178 178 180 180 181 181 181 182 182 182 182 182 182 183 18. T.O. GR1F16CJ1 Standby AC Power System . . . . . . . . . . . . . . . 183 Emergency AC Power System . . . . . . . . . . . . 183 DC Power System . . . . . . . . . . . . . . . . . . . . . . . 183 FLCS Power Supply . . . . . . . . . . . . . . . . . . . . . 183 External Power Provisions . . . . . . . . . . . . . . . 186 Electrical System Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . 186 Electrical Power Distribution . . . . . . . . . . . . 186 Electrical System Normal Operation . . . . . . 186 Hydraulic System . . . . . . . . . . . . . . . . . . . . . . . . . 198 HYD PRESS Indicators and Warning Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 198 HYD PRESS Indicators . . . . . . . . . . . . . . . 198 HYD/OIL PRESS Warning Light . . . . . . . 198 Emergency Power Unit (EPU) . . . . . . . . . . . . . . 198 EPU Controls and Indicators . . . . . . . . . . . . . 199 EPU Ground Safety Switch . . . . . . . . . . . . 199 EPU Switch . . . . . . . . . . . . . . . . . . . . . . . . . . 199 EPU Run Light . . . . . . . . . . . . . . . . . . . . . . . 199 HYDRAZN Light . . . . . . . . . . . . . . . . . . . . . 199 AIR Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . 199 EPU/GEN Test Switch . . . . . . . . . . . . . . . . 199 EPU FUEL Quantity Indicator C DF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 199 Hydrazine Leak Detector . . . . . . . . . . . . . . 199 EPU Fired Indicator . . . . . . . . . . . . . . . . . 1102 EPU Operation . . . . . . . . . . . . . . . . . . . . . . . . 1102 Landing Gear (LG) System . . . . . . . . . . . . . . . . 1104 Main Landing Gear (MLG) . . . . . . . . . . . . . . 1104 Nose Landing Gear (NLG) . . . . . . . . . . . . . . 1104 Landing Gear Controls and Indicators . . . 1104 Landing Gear Handle . . . . . . . . . . . . . . . . 1104 Landing Gear Handle Down Permission Button . . . . . . . . . . . . . . . . . . . . . . . . . . . 1104 DN LOCK REL Button . . . . . . . . . . . . . . . 1104 ALT GEAR Handle . . . . . . . . . . . . . . . . . . 1106 LG Warning Horn . . . . . . . . . . . . . . . . . . . 1106 HORN SILENCER Button . . . . . . . . . . . . 1106 TO/LDG CONFIG Warning Light . . . . . 1106 WHEELS Down Lights . . . . . . . . . . . . . . . 1106 Landing Gear WeightonWheels (WOW) Switches . . . . . . . . . . . . . . . . . . . . . . . . . . 1106 Landing Gear Operation . . . . . . . . . . . . . . . . 1106 Nosewheel Steering (NWS) System . . . . . . . . . 1110 NWS Controls and Indicators . . . . . . . . . . . 1110 NWS A/R DISC MSL STEP Button . . . . 1110 NWS Light . . . . . . . . . . . . . . . . . . . . . . . . . . 1110 NWS FAIL Caution Light . . . . . . . . . . . . 1110 Nosewheel Steering (NWS) System D . . . . 1110Wheel Brake System . . . . . . . . . . . . . . . . . . . . . . Toe Brake System . . . . . . . . . . . . . . . . . . . . . . Spin Down Braking System . . . . . . . . . . . . . Brakes Channel Switch C DF . . . . . . . . . . . Parking Brake C DF . . . . . . . . . . . . . . . . . . . Antiskid System . . . . . . . . . . . . . . . . . . . . . . . ANTISKID Switch C DF . . . . . . . . . . . . ANTI SKID Caution Light . . . . . . . . . . . . Speedbrake System . . . . . . . . . . . . . . . . . . . . . . . SPD BRK Switch . . . . . . . . . . . . . . . . . . . . SPEED BRAKE Position Indicator . . . . Drag Chute System . . . . . . . . . . . . . . . . . . . . . . . DRAG CHUTE Switch . . . . . . . . . . . . . . . Arrestment System . . . . . . . . . . . . . . . . . . . . . . . HOOK Switch . . . . . . . . . . . . . . . . . . . . . . . HOOK Caution Light . . . . . . . . . . . . . . . . Wing Flap System . . . . . . . . . . . . . . . . . . . . . . . . Leading Edge Flaps (LEF's) . . . . . . . . . . . . . LE FLAPS Switch . . . . . . . . . . . . . . . . . . . FLCS LEF LOCK PFL . . . . . . . . . . . . . . . Trailing Edge Flaps (TEF's) (Flaperons) . . . . . . . . . . . . . . . . . . . . . . . . . . ALT FLAPS Switch . . . . . . . . . . . . . . . . . . Flight Control System (FLCS) . . . . . . . . . . . . . Digital Backup (DBU) . . . . . . . . . . . . . . . . FLCS Limiters . . . . . . . . . . . . . . . . . . . . . . . . . AOA/G Limiter . . . . . . . . . . . . . . . . . . . . . . Roll Rate Limiter . . . . . . . . . . . . . . . . . . . . Rudder Authority Limiter . . . . . . . . . . . . Yaw Rate Limiter . . . . . . . . . . . . . . . . . . . . FLCS Gains . . . . . . . . . . . . . . . . . . . . . . . . . . . Cruise Gains . . . . . . . . . . . . . . . . . . . . . . . . Takeoff and Landing Gains . . . . . . . . . . . Standby Gains . . . . . . . . . . . . . . . . . . . . . . FLCS Data Recorder C DF . . . . . . . . . . . . . AngleofSideslip (AOS) Feedback Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . Gun Compensation . . . . . . . . . . . . . . . . . . . . . Flight Control System (FLCS) Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . Stick . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Rudder Pedals . . . . . . . . . . . . . . . . . . . . . . . MANUAL TRIM Panel . . . . . . . . . . . . . . . MANUAL PITCH Override (MPO) Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . STORES CONFIG Switch C DF . . . . . . Low Speed Warning Tone . . . . . . . . . . . . . FLT CONTROL Panel (FLCP) C DF . .1110 1110 1111 1111 1111 1116 1117 1117 1117 1117 1117 1117 1118 1118 1118 1118 1118 1118 1118 1118 1120 1120 1120 1120 1121 1121 1121 1121 1121 1121 1127 1127 1127 1127 1127 1127 1127 1127 1130 1130 1130 1130 1130 113013 19. T.O. GR1F16CJ1 FLCS Warning, Caution, and Indicator Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FLCS Warning Light . . . . . . . . . . . . . . . . . DBU ON Warning Light . . . . . . . . . . . . . . TO/LDG CONFIG Warning Light . . . . . FLCS FAULT Caution Light . . . . . . . . . . BuiltIn Test (BIT) . . . . . . . . . . . . . . . . . . . Pilot Fault List Display (PFLD) . . . . . . . Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Autopilot Operation . . . . . . . . . . . . . . . . . . . . ADV MODE Switch . . . . . . . . . . . . . . . . . . Stick Steering . . . . . . . . . . . . . . . . . . . . . . . . . AOA System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AOA Indicator . . . . . . . . . . . . . . . . . . . . . . . AOA Indexer . . . . . . . . . . . . . . . . . . . . . . . . HUD AOA Display . . . . . . . . . . . . . . . . . . . Air Data System . . . . . . . . . . . . . . . . . . . . . . . . . . Air Data Probes . . . . . . . . . . . . . . . . . . . . . AOA Transmitters . . . . . . . . . . . . . . . . . . . Total Temperature Probe . . . . . . . . . . . . . Static Pressure Ports . . . . . . . . . . . . . . . . . Probe Heat Monitor . . . . . . . . . . . . . . . . . . PROBE HEAT Switch . . . . . . . . . . . . . . . . Pneumatic Sensor Assembly (PSA) . . . . . . Central Air Data Computer (CADC) . . . . . CADC Caution Light . . . . . . . . . . . . . . . . . Warning, Caution, and Indicator Lights . . . . Voice Message System (VMS) . . . . . . . . . . . VOICE MESSAGE Switch C DF . . . . . MASTER CAUTION Light . . . . . . . . . . . . . . Pilot Fault List Display (PFLD) . . . . . . . . . Caution Light Panel . . . . . . . . . . . . . . . . . . . . MAL & IND LTS Test Button . . . . . . . . . Lighting System . . . . . . . . . . . . . . . . . . . . . . . . . . Exterior Lighting . . . . . . . . . . . . . . . . . . . . . . Anticollision Strobe Light . . . . . . . . . . . . Position/Formation Lights . . . . . . . . . . . . Air Refueling Lights . . . . . . . . . . . . . . . . . Vertical TailMounted Floodlight . . . . . . Landing and Taxi Lights . . . . . . . . . . . . . Interior Lighting . . . . . . . . . . . . . . . . . . . . . . . PRIMARY CONSOLES Knob . . . . . . . . . PRIMARY INST PNL Knob . . . . . . . . . . . DATA ENTRY DISPLAY Knob . . . . . . . . MAL & IND LTS Switch . . . . . . . . . . . . . . FLOOD INST PNL Knob . . . . . . . . . . . . . FLOOD CONSOLES Knob . . . . . . . . . . .141130 1130 1132 1132 1132 1135 1135 1135 1135 1136 1136 1136 1137 1137 1138 1138 1138 1138 1138 1138 1138 1138 1140 1140 1140 1140 1140 1145 1146 1146 1146 1147 1147 1148 1148 1148 1148 1148 1154 1154 1154 1155 1155 1155 1155 1155 1155NVIS Switch PX III . . . . . . . . . . . . . . . . . . HandsOn Blackout (HOBO) Switch PX III . . . . . . . . . . . . . . . . . . . . . . Utility Light . . . . . . . . . . . . . . . . . . . . . . . . Cockpit Spotlights . . . . . . . . . . . . . . . . . . . Escape System . . . . . . . . . . . . . . . . . . . . . . . . . . . Canopy . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Canopy Controls and Indicators . . . . . . . . . MANUAL CANOPY CONTROL Handcrank . . . . . . . . . . . . . . . . . . . . . . . Canopy Handle C DF . . . . . . . . . . . . . . . . Canopy Jettison . . . . . . . . . . . . . . . . . . . . . . . . Ejection Seat . . . . . . . . . . . . . . . . . . . . . . . . . . Ejection Handle . . . . . . . . . . . . . . . . . . . . . SHOULDER HARNESS Knob . . . . . . . . EMERGENCY MANUAL CHUTE Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . Ejection Safety Lever . . . . . . . . . . . . . . . . SEAT NOT ARMED Caution Light . . . . SEAT ADJ Switch . . . . . . . . . . . . . . . . . . . Shoulder Harness Straps/Parachute Risers . . . . . . . . . . . . . . . . . . . . . . . . . . . . Inertia Reel Straps . . . . . . . . . . . . . . . . . . Lapbelt . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Survival Kit . . . . . . . . . . . . . . . . . . . . . . . . . RADIO BEACON Switch . . . . . . . . . . . . . Emergency Oxygen . . . . . . . . . . . . . . . . . . Ejection Seat Operation . . . . . . . . . . . . . . . . Ejection Mode Envelopes . . . . . . . . . . . . . . . Ejection Sequence Times . . . . . . . . . . . . . . . . Canopy Jettison/Seat Ejection . . . . . . . . . . . Ejection Seat Performance . . . . . . . . . . . . . . Oxygen System PX III . . . . . . . . . . . . . . . . . . . . . Onboard Oxygen Generating System (OBOGS) . . . . . . . . . . . . . . . . . . . . OBOGS Backup Oxygen Supply (BOS) . . . . . . . . . . . . . . . . . . . . . . . . OBOGS Monitor . . . . . . . . . . . . . . . . . . . . . . . Emergency Oxygen Supply (EOS) . . . . . . . OBOGS BuiltInTests (BIT's) . . . . . . . . . . . OBOGS PowerUp BIT . . . . . . . . . . . . . . . . . OBOGS Periodic BIT . . . . . . . . . . . . . . . . . . . OBOGS Manual BIT . . . . . . . . . . . . . . . . . . . OBOGS Pneumatic BIT . . . . . . . . . . . . . . . . . Pressure Breathing for G (PBG) . . . . . . . . . Oxygen System Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . Oxygen System Schematic . . . . . . . . . . . . . .1155 1157 1157 1157 1157 1157 1157 1157 1157 1161 1161 1161 1161 1161 1161 1161 1161 1161 1161 1161 1164 1164 1164 1164 1164 1164 1164 1164 1173 1173 1173 1173 1173 1173 1173 1173 1173 1174 1174 1174 1174 20. T.O. GR1F16CJ1 Oxygen System PX II . . . . . . . . . . . . . . . . . . . . . Liquid Oxygen System . . . . . . . . . . . . . . . . . . Pressure Breathing for G (PBG) . . . . . . Oxygen System Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . Oxygen Duration . . . . . . . . . . . . . . . . . . . . Emergency Oxygen System . . . . . . . . . . . . . Oxygen System Schematic . . . . . . . . . . . . . . Communications, Navigation, and IFF (CNI) Equipment . . . . . . . . . . . . . . . . . . . . . . Upfront Controls . . . . . . . . . . . . . . . . . . . . . . . DED/CNI Readouts . . . . . . . . . . . . . . . . . . . . CNI Readout/DED Page Summary . . . . IFF Control Panel C DF PX III . . . . . . . . . . C & I (Communications and IFF) Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IFF MASTER Knob . . . . . . . . . . . . . . . . . . IFF M4 CODE Switch . . . . . . . . . . . . . . . IFF MODE 4 REPLY Switch . . . . . . . . . . IFF MODE 4 MONITOR Switch . . . . . . IFF ENABLE Switch . . . . . . . . . . . . . . . . . IFF MODE 1/MODE 3 Selector Levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUX COMM Panel C DF PX II . . . . . . . . . . CNI (Communications, Navigation, and IFF) Knob . . . . . . . . . . . . . . . . . . . . IFF MASTER Knob . . . . . . . . . . . . . . . . . . M4 CODE Switch . . . . . . . . . . . . . . . . . . . IFF MODE 4 REPLY Switch . . . . . . . . . . IFF MODE 4 MONITOR Switch . . . . . . TACAN Function Switch . . . . . . . . . . . . . TACAN CHANNEL Selector Levers . . . AUDIO 1 Control Panel . . . . . . . . . . . . . . . . . COMM 1 (UHF) Power Knob . . . . . . . . . COMM 1 (UHF) Mode Knob . . . . . . . . . . COMM 2 (VHF) Power Knob . . . . . . . . . . COMM 2 (VHF) Mode Knob . . . . . . . . . . SECURE VOICE Knob . . . . . . . . . . . . . . . MSL Tone Knob . . . . . . . . . . . . . . . . . . . . . TF Tone Knob . . . . . . . . . . . . . . . . . . . . . . . THREAT Tone Knob . . . . . . . . . . . . . . . . . AUDIO 2 Control Panel . . . . . . . . . . . . . . . . . ILS Power Knob . . . . . . . . . . . . . . . . . . . . . TACAN Power Knob . . . . . . . . . . . . . . . . . INTERCOM Knob . . . . . . . . . . . . . . . . . . . HOT MIC CIPHER Switch . . . . . . . . . . . ANT SEL Panel C DF . . . . . . . . . . . . . . . . . . IFF ANT SEL Switch C DF . . . . . . . . . . UHF ANT SEL Switch C DF . . . . . . . . . Communications System . . . . . . . . . . . . . . . . . .1177 1177 1177 1177 1177 1177 1177 1182 1182 1182 1185 1185 1186 1186 1186 1186 1186 1187 1187 1187 1187 1187 1187 1188 1188 1188 1188 1188 1188 1188 1189 1189 1189 1189 1189 1189 1190 1190 1190 1190 1190 1190 1190 1191 1191Antenna Locations . . . . . . . . . . . . . . . . . . . . . Have Quick (HQ) System . . . . . . . . . . . . . . . Single Word of Day (WOD) . . . . . . . . . . . Single WOD Transfer . . . . . . . . . . . . . . . . Multiple Word of Day (MWOD) . . . . . . . Automatic MWOD Loading PX III . . . . . TimeofDay (TOD) Transmission . . . . . TimeofDay (TOD) Reception PX III . . . TimeofDay (TOD) Reception PX II . . . Net Number . . . . . . . . . . . . . . . . . . . . . . . . . Antijamming (AJ) Mode Operation . . . . Have Quick (HQ) UHF Radio . . . . . . . . . . . . Operation of the UHF Radio on Upfront Controls . . . . . . . . . . . . . . . . . . UHF Radio Backup Control Panel . . . . . Function Knob . . . . . . . . . . . . . . . . . . . . . . Mode Knob PX II . . . . . . . . . . . . . . . . . . . . Mode Knob PX III . . . . . . . . . . . . . . . . . . . . CHAN Knob . . . . . . . . . . . . . . . . . . . . . . . . . Manual Frequency Knobs . . . . . . . . . . . . A32T Knob PX II . . . . . . . . . . . . . . . . . . A32 Knob PX III . . . . . . . . . . . . . . . . . . . . VOL Knob . . . . . . . . . . . . . . . . . . . . . . . . . . SQUELCH Switch . . . . . . . . . . . . . . . . . . . TONE Button PX II . . . . . . . . . . . . . . . . . . CHAN Display PX III . . . . . . . . . . . . . . . . Frequency/Status Display PX III . . . . . . STATUS Button PX III . . . . . . . . . . . . . . . TTONE Switch PX III . . . . . . . . . . . . . . . . TEST DISPLAY Button PX III . . . . . . . . ZERO Switch PX III . . . . . . . . . . . . . . . . . . FILL Connector PX III . . . . . . . . . . . . . . . VHF Radio . . . . . . . . . . . . . . . . . . . . . . . . . . . . Operation of the VHF Radio on Upfront Controls . . . . . . . . . . . . . . . . . . Zeroize Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . Navigation Systems . . . . . . . . . . . . . . . . . . . . . . Embedded Global Positioning and Inertial Navigation Set (EGI) PX III . . . . . . . . . . . Global Positioning System (GPS) PX II . . . Inertial Navigation Set (INS) PX II . . . . . . Tactical Air Navigation (TACAN) System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Operation of the TACAN on Upfront Controls . . . . . . . . . . . . . . . . . . . . . . . . . . Terrain Following Radar (TFR) System . . . . . AIFF System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AIFF Transponder PX II . . . . . . . . . . . . . . . . AIFF Transponder PX III . . . . . . . . . . . . . . . Operation of the Transponder on Upfront Controls PX II . . . . . . . . . . . . . Operation of the Transponder on Upfront Controls PX III . . . . . . . . . . . .1191 1191 1191 1191 1191 1193 1193 1193 1193 1194 1194 1194 1194 1196 1196 1196 1196 1197 1197 1197 1197 1197 1197 1197 1197 1197 1198 1198 1198 1198 1198 1198 1198 1199 1199 1199 1200 1200 1200 1200 1200 1200 1201 1201 1201 120215 21. T.O. GR1F16CJ1 AIFF Interrogator . . . . . . . . . . . . . . . . . . . . . . Operation of the Interrogator on Upfront Controls PX II . . . . . . . . . . . . . Operation of the Interrogator on Upfront Controls PX III . . . . . . . . . . . . AIFF Controls and Indicators . . . . . . . . . . . IFF IDENT Button . . . . . . . . . . . . . . . . . . IFF (Mode 4) Caution Light . . . . . . . . . . . UHF VHF IFF Transmit Switch PX II . . . . . . . . . . . . . . . . . . . . . . Target Management Switch PX III . . . . . Instrument Landing System (ILS) . . . . . . . . . ILS Controls . . . . . . . . . . . . . . . . . . . . . . . . Operation of the ILS on Upfront Controls . . . . . . . . . . . . . . . . . . . . . . . . . . MRK BCN Light . . . . . . . . . . . . . . . . . . . . . INSTR MODE Select Panel . . . . . . . . . . . . . . . . INSTR HDG Knob C DF . . . . . . . . . . . . . INSTR MODE Knob . . . . . . . . . . . . . . . . . Navigation Aids and Display . . . . . . . . . . Instrument Modes . . . . . . . . . . . . . . . . . . . Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Airspeed/Mach Indicator . . . . . . . . . . . . . . . . Standby Attitude Indicator (SAI) . . . . . . . . Vertical Velocity Indicator (VVI) . . . . . . . . . Magnetic Compass . . . . . . . . . . . . . . . . . . . . . Attitude Director Indicator (ADI) . . . . . . . . Horizontal Situation Indicator (HSI) . . . . . Clock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Crash Survivable Flight Data Recorder (CSFDR) . . . . . . . . . . . . . . . . . . . . . F16D Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Controls DR . . . . . . . . . . . . . . . . . . . . Throttle DR . . . . . . . . . . . . . . . . . . . . . . . . . ENG CONT Switch DR . . . . . . . . . . . . . . . Fuel System . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel Control Panel DR . . . . . . . . . . . . . . . Speedbrake System . . . . . . . . . . . . . . . . . . . . SPD BRK Switch DR . . . . . . . . . . . . . . . . . Drag Chute System . . . . . . . . . . . . . . . . . . . . DRAG CHUTE Switch DR . . . . . . . . . . . . Landing Gear (LG) System . . . . . . . . . . . . . . DN LOCK REL Button DR . . . . . . . . . . . Flight Control System . . . . . . . . . . . . . . . . . . Stick Control Operation . . . . . . . . . . . . . . . . STICK CONTROL Switch DF . . . . . . . . . Stick Indicator DR . . . . . . . . . . . . . . . . . . . Stick OVRD Lights D . . . . . . . . . . . . . . . .161203 1204 1204 1204 1204 1204 1204 1205 1205 1205 1206 1206 1206 1206 1206 1206 1206 1215 1215 1216 1216 1216 1216 1216 1216 1217 1217 1219 1219 1219 1219 1219 1219 1219 1219 1219 1219 1219 1219 1219 1219 1220 1220 1220Escape System D . . . . . . . . . . . . . . . . . . . . . . EJECTION MODE SEL Handle DR . . . Communications System . . . . . . . . . . . . . . . INSTR Mode Select Panel D . . . . . . . . . . . . Flight Instruments DR . . . . . . . . . . . . . . . . . Accelerometer DR . . . . . . . . . . . . . . . . . . . . Aft Station Interface Unit (ASIU) DR PX III . . . . . . . . . . . . . . . . . . . . STICK CONTROL Switch DR PX III . . . ASIU Switch DR PX III . . . . . . . . . . . . . . . Multifunction Display (MFD) DR . . . . . . . . Throttle and Stick Switches/Controls DR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARMT CONSENT Switch DR . . . . . . . . . . . Aft Seat HUD Monitor (ASHM) DR . . . . . . Servicing Diagram . . . . . . . . . . . . . . . . . . . . .1220 1220 1221 1221 1221 1221 1221 1221 1222 1222 1222 1222 1222 1222THE AIRCRAFT The F16C is a singleengine, singleseat, multirole tactical fighter with full airtoair and airtosurface combat capabilities. The F16D is a twoseat (tandem) version and performs the secondary role of a trainer. The fuselage is characterized by a large bubble canopy, forebody strakes, and an underfuse lage engine air inlet. The wing and tail surfaces are thin and feature moderate aft sweep. The wing has automatic leading edge flaps which enhance performance over a wide speed range. Flaperons are mounted on the trailing edge of the wing and combine the functions of flaps and ailerons. The horizontal tails have a small negative dihedral and provide pitch and roll control through symmetrical/ differential deflection. The vertical tail, augmented by twin ventral fins, provides directional stability. All flight control surfaces are actuated hydraulically by two independent hydraulic systems and are directed by signals through a flybywire system. The fire control system includes a fire control radar with search and tracking capability; two multifunc tion displays (MFD's) for presentation of navigation, radar, weapons, and other information; and a headup display (HUD). Upfront controls provide a central control point for fire control, communica tions, navigation, and IFF functions. A stores management system (SMS) presents a visual display on a selected MFD for inventory, control, and release of all stores. Basic armament includes a fuselagemounted multibarrel 20 mm gun and an airtoair missile on each wingtip. Additional stores of various types can be carried on pylons mounted under the wings and on the fuselage. 22. T.O. GR1F16CJ1 AIRCRAFT GENERAL DATAAIRCRAFT GROSS WEIGHT (A/C GW)Refer to figure 11. The aircraft approximate dimensions are:The GW of the aircraft including pilot, oil, two tip AIM120 missiles, and a full load of 20 mm ammunition is approximately 21,000 pounds and with full internal JP8 fuel 28,200 pounds.DSpan-including missile fins= 32 feet 10 inchesDLength-including nose probe= 49 feet 5.2 inchesDHeight-top of vertical tail = 16 feet 10 inchesDHeight-top of canopy= 9 feet 4 inchesDTread= 7 feet 9 inchesDWheelbase= 13 feet 2 inchesRefer to TURNING RADIUS AND GROUND CLEARANCE, Section II.CThe GW of the aircraft including pilot, oil, two tip AIM120 missiles, and a full load of 20 mm ammunition is approximately 21,600 pounds and with full internal JP8 fuel 27,500 pounds. PX II DPX III D The GW of the aircraft including pilot, oil, two tip AIM120 missiles, and a full load of 20 mm ammunition is approximately 21,900 pounds and with full internal JP8 fuel 27,800 pounds. PX III CFT's add approximately 900 pounds when empty and hold approximately 3000 pounds of JP8 fuel.These GW's are approximate and shall not be used for computing aircraft performance. For maximum GW limitations, refer to Section V, OPERATING LIMITA TIONS. For detailed information, refer to T.O. GR1F16CJ11, Part I. COCKPIT ARRANGEMENTAIRCRAFT GENERAL ARRANGEMENT Refer to figure 12 for general arrangement and overall view of the aircraft.Refer to figure 13. The cockpit is conventional except for the seat, which is reclined 30 degrees, and the stick, which is mounted on the right console. The cockpit contains no circuit breakers.17 23. T.O. GR1F16CJ1General Data AIM-9 MISSILE MISSILE LAUNCHER 15.1613.32 OUTBOARD STORES LOCATIONSFLAPERON 40370-GALLON FUEL TANK37.39 69.6328.6395.82 30.63 195.5218 FT 4.2 IN. SPEEDBRAKE HINGE 29.7270.878.45135.84 190.4312.0544.42SHADED AREA REPRESENTS PX IIID AIRCRAFT49 FT 5.2 IN. OVERALL LENGTH46.8082.0515.35 29.08108.621595.0 101.019.5 16 FT 10.0 IN. OVERALL HEIGHT22.20 STATIC GROUND LINE 49.81 NOTE: Dimensions are in inches unless specified otherwise.GR1F-16CJ-1-0004-1A37Figure 11.(Sheet 1)18 24. T.O. GR1F16CJ1WINGS Area Span Aspect Ratio Taper Ratio Sweep (LE) Dihedral Airfoil Incidence Twist At BL 54.0 At BL 180.0 Flaperon Area LEF Area HORIZONTAL TAILS Area Aspect Ratio Taper Ratio Sweep (LE) Dihedral Airfoil At Root At Tip VERTICAL TAIL Area Aspect Ratio Taper Ratio Sweep (LE) Airfoil At Root At Tip Rudder Area300 Sq Ft 30 Ft 3.0 0.2275 40 0 NACA 64A204 0 0 3 31.32 Sq Ft 36.71 Sq FtVENTRAL FIN (EACH) Area Span Aspect Ratio Taper Ratio Sweep (LE) Dihedral (Cant) Airfoil At Root At Tip8.03 Sq Ft 23.356 In. Theo (27.5 In. Actual) 0.472 (Theo) 0.760 (Theo) 30 15 Outboard 3.886% Modified Wedge Constant 0.03RSPEEDBRAKES Area (4 Element Clamshell)63.70 Sq Ft 2.114 0.390 (Theo) 40 -10 6% Biconvex 3.5% Biconvex 54.75 Sq Ft 1.294 0.437 47.5 5.3% Biconvex 3.0% Biconvex 11.65 Sq FtLANDING GEAR (LG) Main Gear (MLG) Tire Size Stroke Static Rolling Radius Nose Gear (NLG) Tire Size Stroke Static Rolling Radius14.26 Sq Ft (3.565 Sq Ft Ea)27.75 x 8.75-14.5 24 Ply 10.5 In. 11.9 In. 17.9 x 6.7R8 22 Ply 10.0 In. 7.5 In.ENGINE F100PW229 Thrust Engine Compressor Face Diameter Engine Length29,000 Lb Class 34.8 In. 208 In.F110-GE-129 Thrust Engine Compressor Face Diameter Engine Length29,500 Lb Class 35.8 In. 183.76 In.32 FT 10 IN. * OVERALL SPAN W/MISSILES 31 FT OVERALL SPAN W/O MISSILES10 46.5 93.0 * Add 3 inches for AIM-120 missiles GR1F-16CJ-1-0004-2A37Figure 11.(Sheet 2)19 25. 8111182515 16 15 13 14For antenna locations, refer to ANTENNA LOCATIONS, this section.17 2723C8 59 101122 17 1819 20302128 29 3112 386 739374032 33413434 17 35 36 4217214 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16.26 24DT.O. GR1F16CJ1110General Arrangement (Typical)Air Data (Pitot) Probe Nose Radome AOA Probe AOA Transmitter Forward Electronic Equipment Bay Cockpit Pressure Regulator Cockpit Pressure Safety Valve HUD/ASHM Instrument Panel Canopy (Movable) Ejection Seat Canopy (Fixed) AIM-9 Missile Missile Launcher AR and Formation Light Position/Formation Light17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. 30. 31. 32.36362 61 60 5954 55 56 58 57Static Discharger LEF Drive Unit Hydraulic Reservoir AR Slipway FLCS Accumulators Anticollision Strobe Light Power Supply Vertical Tail Attachment Fittings Vertical Tail Vertical Tail-Mounted Floodlight Anticollision Strobe Light Rudder Position Light Drag Chute Fairing Rudder ISA Turbofan Engine SpeedbrakeFigure 12.52 5333. 34. 35. 36. 37. 38. 39. 40. 41. 42. 43. 44. 45. 46. 47. 48.514450 49 44 4847Speedbrake Actuator Chaff/Flare Dispenser Horizontal Tail ISA Horizontal Tail Formation Light Flaperon ISA Hook Flaperon Wing Structural Box Fixed Trailing Edge Panel Asymmetry Brake LEF Rotary Actuator LEF Torque Shaft LEF Wing Attachment Fittings MLG4645 44 44 4349. 50. 51. 52. 53. 54. 55. 56. 57. 58. 59. 60. 61. 62. 63.1413 16MLG Door LEF Angle Drive Gearbox Air-Conditioning Package M61A1 20MM Gun Ammunition Drum EPU Nitrogen Bottle Gun Port NLG Door Position Light NLG Engine Air Inlet Left Console Throttle Strake Lower Equipment Compartment GR1F-16CJ-1-0005X37 26. T.O. GR1F16CJ1Cockpit Arrangement C DF (Typical) PX II DFDF INSTRUMENT PANELLEFT AUXILIARY CONSOLERIGHT AUXILIARY CONSOLE STICKTHROTTLEDFLEFT CONSOLERIGHT CONSOLEDFGR1F-16CJ-1-0006A37Figure 13.(Sheet 1)111 27. T.O. GR1F16CJ1Cockpit Arrangement C DF (Typical) PX II LEFT CONSOLE23 22 241 22120418 19 1714515 16131136 7 9128DF 10 1. UHF Backup Control Panel 2. AUDIO 1 Control Panel 3. AUDIO 2 Control Panel 4. ECM Control Panel 5. AVTR Control Panel 6. EXT LIGHTING Control Panel 7. MANUAL TRIM Panel 8. G-Suit Hose Connection 9. ANTI G TEST Button 10. DF STICK CONTROL Switch 11. Stowage 12. TEST Switch Panel 13. DEFOG Lever 14. FLT CONTROL Panel 15. Fuel Control Panel 16. AUX COMM Panel 17. CANOPY JETTISON T-Handle 18. EPU Control Panel 19. ELEC Control Panel 20. Throttle FRICTION Control 21. ENG & JET START Control Panel 22. MANUAL PITCH Override Switch 23. CHAFF/FLARE Dispense Button 24. ThrottleDF GR1F-16CJ-1-0007A37Figure 13.(Sheet 2)112 28. T.O. GR1F16CJ1Cockpit Arrangement C DF (Typical) PX II LEFT AUXILIARY CONSOLERIGHT AUXILIARY CONSOLEDF18191235171616 15 1214 13 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19.471043811265 7 89EMER STORES JETTISON Button (Covered) WHEELS Down Lights (Green) HOOK Switch (Lever Lock) ANTI-SKID Switch DN LOCK REL Button LG Handle Down Permission Button LG Handle LG Handle Warning Light (Red) LANDING TAXI LIGHTS Switch CMDS Control Panel RF Transmit Panel RWR Aux Control Panel ALT GEAR Handle ALT GEAR Reset Button SPEED BRAKE Position Indicator STORES CONFIG Switch HORN SILENCER Button GND JETT ENABLE Switch (Lever Lock) BRAKES Channel Switch91. 2. 3. 4. 5. 6. 7. 8. 9. 10.10Magnetic Compass FUEL Quantity Indicator Pilot Fault List Display System A HYD PRESS Indicator System B HYD PRESS Indicator Caution Light Panel LIQUID OXYGEN Quantity Indicator EPU FUEL Quantity Indicator Cockpit Pressure Altimeter ClockGR1F-16CJ-1-0008A37Figure 13.(Sheet 3)113 29. T.O. GR1F16CJ1Cockpit Arrangement C DF (Typical) PX II INSTRUMENT PANELDF1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29.HUD Combiner Glass DF AOA Indexer AR Status/NWS Indicator 42 2 Integrated Control Panel (ICP) Standby Attitude Indicator FUEL FLOW Indicator 41 Data Entry Display 40 ENG FIRE and ENGINE Warning 39 Lights (Red) 38 36 HYD/OIL PRESS Warning Light (Red) 37 FLCS and DBU ON Warning 35 34 Lights (Red) 28 TO/LDG CONFIG Warning Light (Red) 33 32 CANOPY Warning Light (Red) 31 Right MFD 22 OIL Pressure Indicator 29 NOZ POS Indicator 30 RPM Indicator 23 30. Autopilot ROLL Switch FTIT Indicator 31. ADV MODE Switch Vertical Velocity Indicator 32. MASTER ARM Switch 21 MRK BCN Light 33. C ALT REL Button FUEL QTY SEL Panel 34. LASER ARM Switch Rudder PEDAL ADJ Knob 35. IFF IDENT Button AOA Indicator 36. DRAG CHUTE Switch INSTR MODE Select Panel 37. RWR Prime Control Panel Airspeed/Mach Indicator 38. Azimuth Display/Indicator Attitude Director Indicator 39. F-ACK Button Horizontal Situation Indicator 40. TF FAIL Warning Light (Red) Altimeter 41. MASTER CAUTION Light (Amber) Left MFD 42. ECM Light (Green), DF ECM (Green) and OVRD (Amber) Light Autopilot PITCH SwitchFigure 13.(Sheet 4)11437 6 8 91 42412 14 15 165 1327 2518 1926 2036 3410 1117DF 3932 31 3029GR1F-16CJ-1-0009A37 30. T.O. GR1F16CJ1Cockpit Arrangement C DF (Typical) PX II RIGHT CONSOLE17191 2DF 1843165615 1410 13127 9811DF1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19.SNSR PWR Control Panel HUD Control Panel Interior LIGHTING Control Panel NUCLEAR CONSENT Switch (Guarded) PLAIN Cipher Switch AIR COND Control Panel ENGINE ANTI-ICE Switch Utility Light ANT SEL Panel AVIONICS POWER Panel OXYGEN REGULATOR Panel DTU Control Panel Stowage Oxygen/Communication Hookup VOICE MESSAGE Switch ZEROIZE Switch Stick DF NWS Control Button/Indicator (Green) SEAT ADJ SwitchGR1F-16CJ-1-0010A37Figure 13.(Sheet 5)115 31. T.O. GR1F16CJ1Cockpit Arrangement DR (Typical) PX IIINSTRUMENT PANELLEFT AUXILIARY CONSOLERIGHT AUXILIARY CONSOLE STICKTHROTTLELEFT CONSOLERIGHT CONSOLEGR1F-16CJ-1-0011A37Figure 13.(Sheet 6)116 32. T.O. GR1F16CJ1Cockpit Arrangement DR (Typical) PX II LEFT CONSOLE7 9 81 2610 5 111. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11.43AUDIO 1 Control Panel AUDIO 2 Control Panel G-Suit Hose Connection ANTI G TEST Button MAL & IND LTS Test Button FUEL MASTER Switch MANUAL PITCH Override Switch ENG CONT Switch Throttle CANOPY JETTISON T-Handle StowageGR1F-16CJ-1-0012A37Figure 13.(Sheet 7)117 33. T.O. GR1F16CJ1Cockpit Arrangement DR (Typical) PX II LEFT AUXILIARY CONSOLE11524 714512 106 1911 81. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15.3RIGHT AUXILIARY CONSOLE6133 4EMER STORES JETTISON Button (Covered) WHEELS Down Lights (Green) HOOK Switch (Lever Lock) DN LOCK REL Button LG Handle Down Permission Button LG Handle Warning Light (Red) LG Handle ALT GEAR Handle ALT GEAR Reset Button Blank Panel SPEED BRAKE Position Indicator ALT FLAPS Switch (Lever Lock) HORN SILENCER Button GND JETT ENABLE Switch (Lever Lock) DRAG CHUTE SwitchFigure 13.(Sheet 8)118251. 2. 3. 4. 5. 6.Clock FUEL Quantity Indicator System B HYD PRESS Indicator System A HYD PRESS Indicator EJECTION MODE SELECT Handle Caution Light Panel GR1F-16CJ-1-0013A37 34. T.O. GR1F16CJ1Cockpit Arrangement DR (Typical) PX II INSTRUMENT PANEL1. MASTER CAUTION Light (Amber) 2. ENG FIRE and ENGINE Warning Lights (Red) 3. HYD/OIL PRESS Warning Light (Red) 4. FLCS and DBU ON Warning Lights (Red) 5. AR Status/NWS Indicator 6. TO/LDG CONFIG Warning Light (Red) 7. CANOPY Warning Light (Red) 8. Right MFD 9. VIDEO SEL Switch 10. Standby Attitude Indicator 11. FUEL FLOW Indicator 12. OIL Pressure Indicator 13. FAULT ACK Button 14. NOZ POS Indicator 15. RPM Indicator 16. FTIT Indicator 17. Pilot Fault List Display 18. Accelerometer 19. Altimeter 20. Vertical Velocity Indicator 21. Attitude Director Indicator 22. Horizontal Situation Indicator 23. MRK BCN Light 24. Rudder PEDAL ADJ Knob 25. INSTR MODE Select Panel 26. AOA Indicator 27. Airspeed/Mach Indicator 28. ARMT CONSENT Switch (Guarded)39323338 3740 4135IFF IDENT Button Data Entry Display Integrated Keyboard Panel (IKP) Stick Indicator OVRD Light (Amber) Blank Azimuth Display/Indicator Left MFD AOA Indexer TF FAIL Warning Light (Red) Handgrip ECM Light (Green) Aft Seat HUD Monitor5 8 11367 9 121028 26 2521 2213 14 1527 19 183129. 30. 31. 32. 33. 34. 35. 36. 37. 38. 39. 40. 41.4613430 292 317 20162324GR1F-16CJ-1-0014A37Figure 13.(Sheet 9)119 35. T.O. GR1F16CJ1Cockpit Arrangement DR (Typical) PX II RIGHT CONSOLE7 86 152 41. 2. 3. 4. 5. 6. 7. 8.3Interior LIGHTING Control Panel OXYGEN REGULATOR Panel Utility Light Oxygen/Communications Hookup Stowage NWS Control Button/Indicator (Green) Stick SEAT ADJ SwitchGR1F-16CJ-1-0015A37Figure 13.(Sheet 10)120 36. T.O. GR1F16CJ1Cockpit Arrangement C DF (Typical) PX III DFDFINSTRUMENT PANELLEFT AUXILIARY CONSOLERIGHT AUXILIARY CONSOLE STICKTHROTTLEDFRIGHT CONSOLE LEFT CONSOLEDFGR1F-16CJ-1-1006X37Figure 13. (Sheet 11)Change 1121 37. T.O. GR1F16CJ1Cockpit Arrangement C DF (Typical) PX III LEFT CONSOLE24 23 251 222213419 20751816 171415813101269DF 11 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25.UHF Backup Control Panel AUDIO 1 Control Panel AUDIO 2 Control Panel ECM Control Panel AVTR Control Panel EXT LIGHTING Control Panel JHMCS Connection MANUAL TRIM Panel G-Suit Hose Connection ANTI G TEST Button DF STICK CONTROL Switch Stowage TEST Switch Panel DEFOG Lever FLT CONTROL Panel Fuel Control Panel IFF Panel CANOPY JETTISON T-Handle EPU Control Panel ELEC Control Panel Throttle FRICTION Control ENG & JET START Control Panel MANUAL PITCH Override Switch CHAFF/FLARE Dispense Button Throttle GR1F-16CJ-1-1007X37Figure 13. (Sheet 12)122 38. T.O. GR1F16CJ1Cockpit Arrangement C DF (Typical) PX III LEFT AUXILIARY CONSOLERIGHT AUXILIARY CONSOLEDF18191235171616 15 1214 13 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19.471043811256 79EMER STORES JETTISON Button (Covered) WHEELS Down Lights (Green) HOOK Switch (Lever Lock) ANTI-SKID Switch DN LOCK REL Button LG Handle Down Permission Button LG Handle LG Handle Warning Light (Red) LANDING TAXI LIGHTS Switch CMDS Control Panel HMCS Panel RWR Aux Control Panel ALT GEAR Handle ALT GEAR Reset Button SPEED BRAKE Position Indicator STORES CONFIG Switch HORN SILENCER Button GND JETT ENABLE Switch (Lever Lock) BRAKES Channel Switch81. 2. 3. 4. 5. 6. 7. 8. 9.9Magnetic Compass FUEL Quantity Indicator Pilot Fault List Display System A HYD PRESS Indicator System B HYD PRESS Indicator Caution Light Panel EPU FUEL Quantity Indicator Cockpit Pressure Altimeter ClockGR1F-16CJ-1-1008X37Figure 13. (Sheet 13)123 39. T.O. GR1F16CJ1Cockpit Arrangement C DF (Typical) PX III INSTRUMENT PANELDF1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29.HUD Combiner Glass AOA Indexer AR Status/NWS Indicator Integrated Control Panel (ICP) Standby Attitude Indicator FUEL FLOW Indicator Data Entry Display ENG FIRE and ENGINE Warning 38 Lights (Red) 35 HYD/OIL PRESS Warning Light (Red) FLCS and DBU ON Warning 34 Lights (Red) TO/LDG CONFIG Warning Light (Red) CANOPY and OXY LOW Warning Lights (Red) 31 Right MFD OIL Pressure Indicator NOZ POS Indicator 30 RPM Indicator 30. Autopilot ROLL Switch FTIT Indicator 31. ADV MODE Switch Vertical Velocity Indicator 32. MASTER ARM Switch MRK BCN Light 33. LASER ARM Switch FUEL QTY SEL Panel 34. IFF IDENT Button Rudder PEDAL ADJ Knob 35. DRAG CHUTE Switch AOA Indicator 36. RWR Prime Control Panel INSTR MODE Select Panel 37. Azimuth Display/Indicator Airspeed/Mach Indicator 38. F-ACK Button Attitude Director Indicator 39. TF FAIL Warning Light (Red) Horizontal Situation Indicator 40. MASTER CAUTION Light (Amber) Altimeter 41. ECM Light (Green), DF ECM (Green) Left MFD and OVRD (Amber) Light Autopilot PITCH SwitchFigure 13. (Sheet 14)124Change 14136 33 32437 287 6 8 9140392932245 2722252326 2013 18 1910 1112 14 15 16 1721GR1F-16CJ-1-1009X37 40. T.O. GR1F16CJ1Cockpit Arrangement C DF (Typical) PX III RIGHT CONSOLE17DF 1843165615 14191 220 1013127 9 8 11DF1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20.SNSR PWR Control Panel HUD Control Panel Interior LIGHTING Control Panel NUCLEAR CONSENT Switch (Guarded) PLAIN Cipher Switch AIR COND Control Panel ENGINE ANTI-ICE Switch Utility Light ANT SEL Panel AVIONICS POWER Panel OBOGS MONITOR Panel UDTU Stowage Oxygen/Communication Hookup VOICE MESSAGE Switch ZEROIZE Switch Stick DF NWS Control Button/Indicator (Green) SEAT ADJ Switch OXYGEN Panel GR1F-16CJ-1-1010X37Figure 13. (Sheet 15)Change 1125 41. T.O. GR1F16CJ1Cockpit Arrangement DR (Typical) PX IIIINSTRUMENT PANELLEFT AUXILIARY CONSOLERIGHT AUXILIARY CONSOLE STICKTHROTTLELEFT CONSOLERIGHT CONSOLEGR1F-16CJ-1-1011X37Figure 13. (Sheet 16)126 42. T.O. GR1F16CJ1Cockpit Arrangement DR (Typical) PX III LEFT CONSOLE7 9 81 2610 5 111. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11.43AUDIO 1 Control Panel AUDIO 2 Control Panel G-Suit Hose Connection ANTI G TEST Button MAL & IND LTS Test Button FUEL MASTER Switch MANUAL PITCH Override Switch ENG CONT Switch Throttle CANOPY JETTISON T-Handle StowageGR1F-16CJ-1-1012X37Figure 13. (Sheet 17)127 43. T.O. GR1F16CJ1Cockpit Arrangement DR (Typical) PX III LEFT AUXILIARY CONSOLE11524 714512 106 1911 81. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15.3RIGHT AUXILIARY CONSOLE6133 4EMER STORES JETTISON Button (Covered) WHEELS Down Lights (Green) HOOK Switch (Lever Lock) DN LOCK REL Button LG Handle Down Permission Button LG Handle Warning Light (Red) LG Handle ALT GEAR Handle ALT GEAR Reset Button Blank Panel SPEED BRAKE Position Indicator ALT FLAPS Switch (Lever Lock) HORN SILENCER Button GND JETT ENABLE Switch (Lever Lock) DRAG CHUTE SwitchFigure 13. (Sheet 18)128251. 2. 3. 4. 5. 6.Clock FUEL Quantity Indicator System B HYD PRESS Indicator System A HYD PRESS Indicator EJECTION MODE SELECT Handle Caution Light Panel GR1F-16CJ-1-1013X37 44. T.O. GR1F16CJ1Cockpit Arrangement DR (Typical) PX III INSTRUMENT PANEL1. MASTER CAUTION Light (Amber) (NVIS) 40 41 38 2. ENG FIRE and ENGINE Warning 2 3 46 Lights (Red) 37 39 3. HYD/OIL PRESS Warning Light (Red) 1 4. FLCS and DBU ON Warning Lights (Red) 5 5. AR Status/NWS Indicator 34 6. TO/LDG CONFIG Warning Light (Red) 33 7. CANOPY and OXY LOW Warning Lights (Red) 8 8. Right MFD (NVIS) 32 36 11 10 9. VIDEO SEL Switch 35 10. Standby Attitude Indicator 27 19 18 11. FUEL FLOW Indicato

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