Usaf Flight Manual f16

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Flight Manual USAF F16

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Usaf Flight Manual f16

  1. 1. T.O.1F-16A-l FLIGHT MANUAL PUBNR USAF/EPAF SERIES AIRCRAFT 036802 F-16A/B BLOCKS 10 AND 15 /J.q:'~:-, j " ~ . ,," ( ,._,., '. ( / ,.., .'., ,.~ ", ,.,f'" -., r •••..•• --- " ~ LOCKHEED MARTIN CORPORATION ; 14 "'. .... ----..'--..... ') ,~ "--. L ... .. . F33657-75-C-0310 F42620-01-D-0058 COMPL. TIM CHG: .' .. ,'" -,' ," ~.,·i ,-",._- . ", l. --------- ------------------------~ IF-16A-l-0001X Commanders are responsible for bringing this publication to the attention of all Air Force personnel cleared for operation of subject aircraft. Published under authority of the Secretary of the Air Force. 14 AUGUST 1995 CHANGE 14 15 AUGUST 2003
  2. 2. 10. 1 F- 16A- 1 DISTRIBUTION STATEMENT Distribution is authorized to Department of Defense (DOD) components only (Direct Military Support). Other requests for this document shall be referred to OO-ALCIYPVT, 6080 Gum Ln., Hill AFB, UT 84056-5825. EXPORT CONTROL NOTICE WARNING: This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C. Sec. 2751 et seq) or the Export Administration Act of 1979 as amended (Title 50, U.S.C. app. 2401 et seq). Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of AFI 61-204. HANDLING AND DESTRUCTION NOTICE For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document. SUPPLEMENTAL NOTICE This manual is incomplete without T.O. 1F-16A-1-1, T.O. 1F-16A-1-3 (Block 10), or T.O. 1F-16A-1-4 (Block 15 and l@]). For RNLAF, when operating with the Orpheus Reconnaissance System, this manual is incomplete without T.O. NE1F-16A-1. SUPERSEDURE NOTICE See Technical Order Index, T.O. 0-1-CD-1, CAT-1-4, for current status of Flight Manuals, Safety Supplements, Operational Supplements, and Flight Crew Checklists. This manual supersedes T.O. 1F-16A-1SS-421. T-2 Change 14
  3. 3. T. O. 1F- 16A- 1 Reproduction for nonmilitary use of the information or illustrations contained in this publication is not permitted. The policy for military use reproduction is established for the Army in AR380-5, for the Navy and Marine Corps in OPNAVINST 5510.1B, and for the Air Force in Air Force Instruction 31-401. 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 DESTROY SUPERSEDED PAGES.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 .. Change ... Change ... Change ... Change .. . o '" 14 Aug . 1 ... 25 Mar . 2 .... 10 Feb . 3 .... 15 Sep 4 .... 2 Mar Change Change Change Change Change 95 96 97 97 98 ... . ... . ... . ... . .. ,. Change Change Change Change Change 5 , .... 4 Jan 99 6 '" 15 May 99 7 , .. 15 Mar 00 8 ' ... 15 Dec 00 9 ... Not Issued ... 10 ... Not Issued .... 11 .... 15 Jul 02 .. , 12... 15 Nov 02 . .. 13 .... 15 Apr 03 ... 14... 15 Aug 03 TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 584, CONSISTING OF THE FOLLOWING: Page No. * Change No. Title T-2 ............... ' A ............... .. B C .................... . D .................... . a .................... . b Blank .............. . i ..................... . ii ..... , ........ , ...... , III . . . . . , . . . . . . . . . . . . . . . iv ..... , .............. . vi ..... , ........ , ..... . vii .... , ........ , ..... . viii .... , .............. . ix ... ,., ........ , x ................... .. Xl . . . . . . . . . . . . . . , . . . . . , .... , ........ , ..... .... , .............. ................... ................... ................... ................... o 13 13 13 12 o v ............. ' " xii xiii xiv xv xvi 1-1 14 14 14 14 14 14 14 . , . . , . 1-2 ................... . 1-3 .. , ................ . 1-4 ................. , . 1-4.1 ................. . 1-4.2 Blank .......... , 1-5 .................. . 1-6 ..... " ......... " .' 1-6.1 ................ . 1-6.2 Blank ........... . 1-7 ................... , 1-8 ................... , 1-9 .. 12 ]2 12 12 13 8 8 8 8 * Change Page No. 1-10 1-11 1-12 1-13 1-14 1-15 1-16 1-17 1-18 1-19 1-20 1-21 No. o o o o o o o o 1-22 .................. . 1 1-23 1-24 1-25 1-26 1-27 1-28 1-29 1-30 1-31 1 ............... , .... . ........... '" ... . ............... , .. ................. . ............... , .. ...... , ........ , .. ............... , .. ............... , .. 12 1-32 .... , . , ........ , . , o 1-33 ... , ............. . 1-34 ................. , 1-35 ...... , ......... . 1-36 ................. , ] -37 ................. . 1-38 ...... , .......... , 1-39 ...... , ........ , . , ] -40 ...... , .... , ... , ]-40.1 ............. . 1-40.2 ........... , 1-40.3 .......... , 1-40.4 .. 1-40.5 ........... , 1-40.6 .. 2 12 6 12 12 12 12 2 2 2 o o o o o o .. ... . ........ , ....... . ....... , ........ . ................. , ........ , ......... , ........ , ........ , ........ , ........ , , ................. , ........ , ........ . ........ , ......... . .................. . o o o o o o o o o o o o o o o o o o 12 12 12 12 12 12 Page No. * Change No. 1-40.7 .. 1-40.8 ............. , .. 1-40.9 .... , ........ , 1-40.10 ........... .. 1-41 ...... , ........ , 1-42 ............... , .. 1-43 ............... , .. 1-44 ................. . 1-45 ................. . 1-46 .................. . 1-47 ., " , ............. . 1-48 .................. . 1-49 .................. ' 1-50 .................. . 1-51 .... , ............. . 1-52 .. " .............. . 1-53 .. '., ............ ,. 1-54 .. " , ............. . 1-55 .... , ....... . 1-56 ........... "" 1-57 ........... ,. 1-58 .... , ....... , 1-59 .. ' 1-60 ... 1-61 ............ , 1-62 ... , ......... , 1-63 ........... , 1-64 ... 1-65. 1-66 ... , , ...... , .. 1-66.1 ....... . 1-66.2 Blank .. 1-67 .......... . 1-68 .......... . 1-69 ........... , ..... . 1-70. 1-71 ,. 12 12 12 12 12 o o 1 11 1 1 o o 2 1 o 2 o o o 12 o o 13 o o 2 o 13 o 13 13 1 o o o * Zero in this column indicates an original page. 1-14 USAF/EPAF Change 14 A
  4. 4. T.O. 1F- 16A- 1 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES. LIST OF EFFECTIVE PAGES (Cont) Page No. *Change No. 1-72 . . 0 1-73 . .. . . . . . .. . . . .. .. . . 0 1-74. . . . . . . . . . . . . . . . . . . 12 1-75................... 2 1-76. . . . . . . . . . . . . . . . . . . 0 1-77 .. .. . . . . . . . . . . . . . .. .. 12 1-78................... 13 12 1-78.1 ............. . . . . 1-78.2 Blank . . . . . . . . . . . 1 1-79 ................... , 11 1-80 ................... , 0 1-81 ................... , 0 1-82. . . . . . . . . . . . . . . . . . . 0 1-83 ....... , ........ , . . 3 0 1-84 ................ '" 1-85 ................ , .. ,. 13 1-86 ....... , ........ , . . 0 1-87 , ............... , . . 2 1-88 ................ , . . 2 1-89 , . . . . . . . . . . . . . . . . . . 2 1~90 . . . . . . . . . . . . 0 1-91 '" .......... ,. . ... 0 1-92 , .................. , 0 1-93,.... .... .......... 2 1-94 Blank ............ , 2 1-95 .................. , 3 1-96 .................. , 3 ] -97 ................... " 12 1-98 .. , ............... , 5 1-99 ........... , ..... . 2 1-100 .......... , ..... . 2 1-100.1 .......... , .... . 2 1-100.2 .............. . 12 12 1-100.3 . , ..... . 2 1-100.4 Blank .. , .... . 1-101 ... , ............. . o 1-102. . ....... , .... . o 1-103 ................. . o 1-104 ............ , .... . o 1-105 ............ , .... . o 1-106 ................. . 2 1-107 ..... , ........ , .. . 1 1-108 .......... , ...... . o 7 1-109 .............. , .. , 1-110 ................. . 7 1-111 ................. . 7 1-112 .................. . 4 1-113 .................. . 6 1-114 ................. . 6 8 1-115, ...... , ....... . 1-116 , ............... , 6 1-116.1 ... " .. , ... , .. , , 6 1-116.2 .............. , , 6 1-117 ............ . 6 1-118 .. 11 Page No. *Change No. 1-119 .. , 1-120 .............. , 1-121. . . . . . . . . . . . . . . . . . . 1-122 .............. , ... 1-123 ....... , .......... 1-124. . . . . . . . . . . . . . . . . . 1-125 ....... , ........... 1-126. . . . . . . . . . . . . . . . . . . 1-127 ....... , . . . . . . . . . . 1-128 ....... , ........ ,. 1-129. . . . . . . . . . . . . . . . . . 1-130, . . . . . . . . . . . . . . . . . 1-131 ................ , . 1-132. . . . . . . . . . . . . . . . . . 0 0 0 1 3 0 1 0 7 13 13 0 0 0 1-133, ........ , . . . . . . . . 0 1-134 ......... , ........ 0 1-135 .................. , 0 1-136 ......... , . . . . . . . . 0 1-137 . . . . . . . . . . . . . . . . . . 0 1-138. . . . . . . . . . . . . . . . . . 0 1-139 .. , ............... 5 1-140. . . . . . . . . . . . . . . . . . 12 1-141 .. , ............... , . 0 1-142 .. , ............... ,.12 1-143 .................. " 13 1-144 ........... , ...... , . 0 1-145 ........... , . . . . . . 0 1-146. . . . . . . . . . . . . . . . . . 0 1-147 .... , ............ . o 1-148 ............ , .... . o 12 1-149 ............ , .. , .. 1-150 .... , ............ . o 1-151 ............. , ... . 12 Change 14 *Change No. 1-172... 1-173., ................. 1-174., ................. 1-175 ... , .. .. ........... 1-176 ............ , . . . . . . 1-177 ... , . . .. .. .. . .... .. 1-178 ............ , ..... 1-179.................. 1-180 ... , .............. 1-181 ............ , ....... 1-182. . . . . . . . . . . . . . . . . . 1-183 ................. , . 1-184 ................ '" 1-184.1 . . . . . . . . . . . . . . . . .. 1-184.2 ............ , . . . 1-185 ............. , 1-186 .............. , ... 1-187 .............. , ... 1-188 ..... , ............ , 1-189 .............. , ... '. 1-190 .................. ,. 1-191. . . . . . . . . . . . . . . . . . . . 1-192. . . . . . . . . . . . . . .. . . .. 1-193 ................ , . 1-194. . . . . . . . . . . . . . . . . . 1-195. . . . . . . . . . . . . . . . . . 1-196 ....... , . . . . . . . . . . 1-197 . . . . . . . . . . . . . . . . . . 1-198 ................. . 1-199 ................. . 1-200 ................. . 1-201, ........ , ... , ... . 1-202 ......... , ....... . 0 0 0 0 2 0 0 0 12 0 12 12 0 12 12 12 0 0 0 0 12 0 13 12 13 12 12 13 4 o o o o 1-152 ...... , .......... . 3 1-202.1 ....... , ....... . 12 1-152.1 ........ , ...... . 1-152.2 Blank ......... . 1-153 ...... , .......... . 1-154 ...... , .......... , 1-155 ...... , . , ...... . 1-156 ...... , ........ , . 1-157 ................. , 1-158 ............... , . , 1-159 ................. . 1-160 ............... , .. 1-161 ................. . 1-162 ........ , ....... . 1-163 ........ . 1-164 ........ , ... , ... . 1-165 ................. , 1-166. , ............... , 1-167. , .............. . 1-168 .......... , ..... . 1-169 .......... , ..... . 1-170 ....... , .. , ...... , 1-171 .. 13 2 1-202.2 ....... ' ....... . 1-202.3 ....... , .. , .... . 1-202.4 ....... , ....... . 1-203 ............. , ... . 1-204 ................. . 1-205 ........... , ..... . 1-206 .. , .............. . 1-207 .. , .............. . 1-208 ........... , ..... . 1-209 .. , .............. . 1-210 ............. , ... . 1-211 .... , ........ , ... . 1-212 .... , ........ , ... . 1-213 .... , ........ , . , .. 1-214 .... , .. . 1-215 ................. . 1-216 ................. . 1-217 ............... , .. 1-218 ............... ,. 1-219 .............. . 1-220 Blank .. 12 12 12 12 o o 3 11 o o 3 o 12 3 11 11 o o o o o * Zero in this column indicates an original page. B Page No. 12 12 12 5 o 2 o 7 1 7 13 o o o 12 o o
  5. 5. T.O. 1 F-16A-l INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES. LIST OF EFFECTIVE PAGES (Cont) Page No. *Change No. 2-1 . . 11 2-2 . . . . . . . . . . . . . . . . . . . . 11 2-2.1 . . . . . . . . . . . . . . . . . . 5 2-2.2 Blank ...... . . . . . . 5 2-3 . . . . . . . . . . . . . . . . . . . . 13 2-4 . . . . . . . . . . . . . . . . . . . . 12 2-5 . . . . . . . . . . . . . . . . . . . . 12 2-6 . . . . . . . . . . . . . . 12 2-7 .................... 11 2-8 . . . . . . . . . . . . . . . . . . . . 13 11 2-9 . . . . . . . . . . . . . . . . . . . . 2-10 . . . . . . . . . . . . . . . . . . . 14 14 2-11 . . . . . . . . . . . . . . . . . . . 0 2-12 . . . . . . . . . . . . . . . . . . . 2-13 .................. . 2-14 . . . . . . . . . . . . . . . . . . . 4 0 2-15 . . . . . . . . . . . . . . . . . . . 2-16 . . . . . . . . . . . . . . . . . . . 12 2-17 .................. . 2-18 . . . . . . . . . . . . . . . . . . . 12 8 2-18.1 ............. 2-18.2 Blank. . . . . . . . . . 8 2 2-19 . . . . . . . . . . . . . . . . . . . 2-20 . . . . . . . . . . . . . . . . . . . 5 11 2-20.1 .................. 2-20.2 Blank. . . . . . . . . . . 11 2-21 ................... 11 2-22 . . . . . . . . . . . . . . . . . . . 13 2-23 . . . . . . . . . . . . . . . . . . . 13 2-24.. ... .... .. .. ...... 2 2-25 . . . . . . . . . . . . . . . . . . . .. 12 2-26.. .. . .. .. .. .. 11 2-27 . . . . . . . . . . . . . . . . . . . 12 2-28 . . . . . . . . . . . . 13 2-28.1 ................ 13 2-28.2 Blank. . . . . . . . . . . 7 11 2-29 . . . . . . . . . . . . . . . . . . 2-30 ................. . 11 2-31 .................. . o 2-32 .................. . 2 o 2-33 .................. . 2-34 .................. . o 2-35 .............. " .. . o 7 2-36 ................. . 7 2-37 ......... " 7 2-38 ................. . 2-38.1 ................ . 13 2-38.2 Blank .......... . 11 13 2-39 .................. . 2-40 .... . 13 8 2-41 .......... . 2-42 ......... " o 2-43 .......... . o 2-44 .................. . o 3-1 ... 13 Page No. 3-2 .. 3-3 ................... . 3-4 ................... . 3-5 ................... . 3-6 ................... . 3-7 ................. . 3-8 ................... . 3-9 .......... '" ...... . 3-10 ................. . 3-11 .................. . 3-12 ..... " ... " ...... . 3-13 ......... '" ...... . 3-14 .................. . 3-15 .................. . 3-16 ..... " ........... . 3-17 .................. . 3-18 .................. . 3-19 .................. . 3-20 ................ " . 3-21 .................. . 3-22 ..... " ........... . 3-23 .................. . 3-24 ..... " ........... . 3-25 .................. . 3-26 ......... '" ...... . 3-27 .................. . 3-28 ..... " .. , ...... . 3-28.1 .............. . 3-28.2 Blank ........ . 3-29 ............... . 3-30 .................. . 3-31 .................. . 3-3? ..... " ........... . 3-33 ................. . 3-34 ..... " .......... . 3-35 ...... . 3-36 ... . 3-36.1 .... . 3-36.2 Blank .. 3-37 ..... . 3-38 ........... . 3-38.1 ......... . 3-38.2 Blank .......... . 3-39 .......... " .. '" .. 3-40 ..... '" .......... . 3-40.1 ................ . 3-40.2 Blank .......... . 3-41 .................. . 3-42 .................. . 3-43 .......... " ...... . 3-44 .......... " ...... . 3-45 ......... , ........ . 3-46 ................. . 3-47 ................. . 3-48 .. . *Change No. 12 3 12 o 2 o o 12 3 3 o 12 5 5 o 2 3 o 12 13 o o 8 o 12 14 13 8 6 7 7 5 o 3 8 7 7 6 6 14 13 13 11 1 13 13 13 13 1 8 o o 11 11 5 Page No. *Change No. 3-49 .. . 3-50 .................... , 3-50.1 ................. 3-50.2 Blank. . . . . . . . . . . 3-51 . . . . . . . . . . . . . . . . . . . 3-52 . . . . . . . . . . . . . . . . . . . . 3-53 ...... , . .... ....... 3-54.................... 3-55 . . . . . . . . . . . . . . . . . . . 3-56. . . . . . . . . . . . . . . . . . . 3-56.1 .,. . . . . . . . . . . . . . . 3-56.2 Blank . . . . . . . . . . . 3-57 . . . . . . . . . . . . . . . . . . . 3-58. . . . . . . . . . . . . . . . . . . 3-59. . . . . . . . . . . . . . . . . . . 3-60. . . . . . . . . . . . . . . . . . . 3-61 . . . . . . . . . . . . . . . . . 3-62. . . . . . . . . . . . . . . . . . . 3-63. . . . . . . . . . . . . . . 3-64 ...... " ...... , ... . 3-65 . . . . . . . . . . . . . . . . . . . 3-66..... ............ 3-67 . . . . . . . . . . . . . . . . . . . . 3-68...... .............. 3-69. . . . . . . . . . . . . . . . . . . 3-70. . . . . . . . . . . . . . . . . . . 3-71 .................. . 3-72 . . . . . . . . . . . . . . . . . . . 3-73. .. . . . ............. 3-74 . . . . . . . . . . . . . . . . . . . 3-75................... 3-76............... 3-77 . . . . . . . . . . . . . . . 3-78. .. ... .. ... .... .. .. 3-79.... . . ........ " 3-80. . . . . . . . . . . . . . . . . . . 3-81 .................. . 3-82 .............. , .. " 3-83 .................. . 3-84 ............ . 3--35 ............ . 3-86 ... . 3-87 .. , ... '" ., .. 3-88 ............ . 3-89 ............ . 3-90 .. . 3-90.1 .......... . 3-90.2 ................ . 3-91 .............. , 3-92 ............ . 3-93 .......... . 3-94 .. 3-95 ... ' ...... . 3-96 .. 3-97 .. 13 8 7 0 0 12 3 0 7 7 7 7 8 11 11 3 6 13 7 8 8 1 4 8 4 1 1 1 1 1 1 4 13 13 4 o 8 2 11 12 14 13 14 14 14 7 8 8 5 4 8 4 * Zero in this column indicates an original page. Change 14 C
  6. 6. 10. 1F- 16A- 1 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES. LIST OF EFFECTIVE PAGES (Cont) Page No. 3-98 .. 3-99 .............. , ... . 3-100 ................ . 3-101 ................. . 3-102 ................ . 3-]03 ................. . 3-104 ........... . 3-104.1 ......... . 3-104.2 Blank ... . 3-105 ........... . 3-106 ................. . :1-107 ............. . :3-108 ......... . 3-109 ........ . 3-110 ........... . 3-111 ............. . 3-112 ............. . 3-113 ... , ......... . 3-114 ........... . 3-115 ............. . 3 0 116 ........... . 3-117 .......... . 3-118 ........... . ~3-119 .......... . :3-120 ... , ............ . 3-121 ................. . 3-122 ................. . 3-123 ................. . 3-124 ................. . 3-125 ................. . 3-126 ............... . 3-127 ............ . 3-128 .. . :3-129 ... . 3-130. 3-131 ... ;:3-132 ... . 3-132.1 ............ . 3-132.2 Blank ...... . 3-13:3.. . .......... . 3-134 .............. , 3-135 ................ . 3-136 ......... , . 3-137 ......... , ....... . 3-138 ................. . 3-139 ................ . 3-140 ......... , ...... . 3-140.1 ....... , ...... . 3-140.2 .............. . 3-141 .... . 3-142 ... . 3-143 .. . 3-144 .. . 3-145 .. . 3-146 .. . *Change No. 1 1 1 8 8 13 8 13 o 5 o o o o 5 11 11 :3 12 7 Page No. 4-1 4-2 Blank ............. . 5-1 ................... . 5-2 ................... . 5-3 . . . .......... . 5-4..... . ....... . 5-4.1 ................. . 5-4.2 Blank ........... . 5-5 ................... . 5-6 ................... . 5-7 ........... . 5-8 .................. . 5-9 ................... . 5-10 ................... . 5-11 .................. . 5-12 .......... , ...... . 5-12.1 ................ . 5-12.2 ........ , ....... . 5-13 ............... '" . 5-14 .................. . 6-1 ................... . 6-2 ., ................ . 2 2 6-3 ., 6-4 .. 6-5 ., ................ . o 6-6 .................. . 2 6-7 ........... . 6-8 ... . 6-9 ... . 6-10 .. . 6-11 ........... . 6-12 ................. . 6-13 ................. . 6-]4 .. . 6-15 ................ . 6-16 Blank ......... . 7-1 ................. . 7-2 .. 7-3 .. 7-4 .' 7-5 ., ... 7-6 .. 7-7 .. 11 13 12 o 11 11 11 11 11 4 4 4 4 3 4 7 8 8 11 11 11 11 6 7 8 *Change No. 7-8 ................. . 8-1 8-2 8-3 8-4 8-5 8-6 .................. . .................. . .. .' .. . ............ . ............. . 8-7 ............. . 8-8 .. . 8-9 .. 8-10 .... 8-11 .. o o 3 8 11 11 8 2 o o 13 8 1 o o 8 11 8 13 3 8 o o o 3 o 4 4 4 4 4 4 8 8 8 8 12 13 1 o 8 8 8 13 13 13 1:3 1:3 13 13 13 13 1:3 13 * Zero in this column indicates an original page. o Change 14 Page No. *Change No. 13 13 13 13 13 13 13 13 8-20.. . .... .. ....... .. . 13 8-21 . . . . . . . . . . . . . . . . . . . 13 8-22 ..................... 13 8-23.. . .... .. ....... . . . 13 8-24 . . . . . . . . . . . . . . . . . . . 13 8-25 ................. , . 13 8-26 . . . . . . . . . . . . . . . . . . . 13 8-27 . . . . . . . . . . . . . . . . . . . 13 8-28 ............ , . .... . 13 8-29 ...... , .. .... . .... . 13 8-30 ...... , .......... , . 13 8-31 . . . . . . . . . . . . . . . . . . . 13 13 8-32 ...... , ..... , .. . .... 8-33 .................. '" 13 8-34 ............ , ... .. . 13 8-35 ...... , .. " ., ..... . 13 8-36. . . . . . . . . . . . . . . . . . . 13 8-37 . . .. . . . . . . . . . . . . . . . 13 8-38 Blank. . . . . . . . . . . . . 13 Glossary_1 ............ 13 Glossary_2 ............ 13 Glossary_3 ........... 13 Glossary_4 ........... 13 Glossary_5 ............ 13 Glossary _6 Blank .. 0 8-12 8-13 8-14 8-15 8-16 8-17 8-18 8-19 ..... . ................... ....... .. ....... ... ................... ........... ..... .. .. ................... .. ....... .......... ...................
  7. 7. TO. 1F- 16A-l FLIGHT MANUAL, SAFETY SUPPLEMENT, AND OPERATIONAL SUPPLEMENT STATUS This supplement status page is based on information available as of 15 August 2003. It is not an official status page. Flight Manual Basic Date Change No. and Date T.O. IF-16A-l 14 Aug 1995 14 Supplemental Flight Manuals Basic Date Change No. and Date T.O. IF-16A-l-1 28 Nov 1994 10 15 Feb 2003 T.O.IF-16A-I-3 15 Nov 1999 6 15 Jun 2003 T.O. IF-16A-I-4 15 Nov 1999 6 15 Jun 2003 Flight Crew Checklist Basic Date Change No. and Date T.O.IF-16A-ICL-l 7 Mar 1994 14 15 Aug 2003 15 Aug 2003 INCORPORATED SAFETY AND OPERATIONAL SUPPLEMENTS T.O. Number Date IF-16A-lSS-421 03 Jul 03 Flight Manual Sections Affected Short Title Nozzle Failure Logic II, III OUTSTANDING SAFETY AND OPERATIONAL SUPPLEMENTS T.O. Number Date Short Title Flight Manual Sections Affected None uI.'· .,/ .:~ Change 14 a/(b blank)
  8. 8. T.O. 1F-16A- 1 TABLE OF CONTENTS SECTION I Description and Operation 1-1 SECTION II Normal Procedures 2-1 SECTION III Emergency Procedures 3-1 SECTION IV Crew Duties 4-1 SECTION V Operating Limitations 5-1 SECTION V Operating Limitations (Stores) - Block 10 T.O. IF-16A-I-3 Operating Limitations (Stores) - Block 15 T.O. IF-16A-I-4 SECTIONV and~ SECTION VI Flight Characteristics 6-1 SECTION VII Adverse Weather Operation 7-1 SECTION VIII Air Refueling Procedures 8-1 GLOSSARY Standard and Nonstandard Abbreviations APPENDIX A Performance Data - FI00-PW-200 T.O.IF-16A-l-l APPENDIXB (Not Applicable) T.O. IF-16A-l-l APPENDIXC Performance Data - FI00-PW-220 or FI00-PW-220E T.O. IF-16A-l-l Glossary 1 Change 13
  9. 9. T.O. 1F-16A-l BEFORE YOU TAKE OFF, READ THIS! 1 F-16X-1--0002X@ SCOPE 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 experience 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 instructions under most conditions. Multiple emergencies, adverse weather, terrain, etc., may require modification of the procedures. This manual must be used with one or more of the following manuals to obtain information necessary for safe and efficient operation: T.O. IF-16A-l-l Supplemental Flight Manual, F-16AIB Aircraft T.O. IF-16A-5-2 T.O. IF-16A-6CF-l T.O. IF-16A-25-1 T.O. IF-16A-25-10 T.O. IF-16A-34-1-1 T.O.I-IM-44-1FD T.O. IF-16A-34-1-3 T.O. IF-16A-1-3 Supplemental Flight Manual, F-16AIB Aircraft (Block 10) T.O. IF-16A-34-1-4 T.O. IF-16A-1-4 Supplemental Flight Manual, F-16AIB Aircraft (Block 15 and T.O.IF-16A-39 ~) II Change 13 T.O. l-lC-l Loading Data Acceptance and FUllctional Check Flight Procedures Manual, F-16AIB Aircraft Nuclear Weapons Delivery Manual (SECRET) (Title Unclassified) Aircrew Practice Bomb Delivery Procedures Avionics and Nonnuclear Weapons Delivery Flight Manual Combat Weapons Delivery Software (CWDS) Avionics and Nonnuclear Weapons Delivery Flight Manual ~ Avionics and Nonnuclear Weapons Delivery Flight Manual M Aircraft Battle Damage Repair Basic Flight Crew Air Refueling Procedures I
  10. 10. T. O. 1F- 16A- 1 • PERMISSIBLE 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. HOW TO BE ASSURED OF HAVING LATEST DATA I Refer to T.O. 0-I-CD-l, CAT-I-4 for a listing of all current flight manuals, safety supplements, operational supplements, 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 attacood to formal safety and operational supplements. Clear all discrepancies before flight. instructions in the supplement. Vhen lengthy additions are required, the formal supplement provides one-sided 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., 3-48.1) are inserted in proper numerical sequence and may be printed on both sides. SAFETY SUPPLEMENTS Information involving safety is promptly forwarded in a safety supplement. Urgent information is published in interim safety supplements and transmitted by electronic message. Formal supplements are mailed. The supplement title block and status page (published with formal supplements only) should be checked to determine the effect of this supplement on this manual and other outstanding supplements. ARRANGEMENT I OPERATIONAL SUPPLEMENTS 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 modifications. For details of equipment modification, see the individual equipment illustration. Information involving changes to operating procedures 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. SUPPLEMENT INFORMATION AND GUIDELINES HOW TO GET PERSONAL COPIES Supplements are safety or operational and are indicated -ISS or -IS, respectively. Supplements are issued as interim electronic messages or formal printed copies. All interim supplements are assigned odd numbers, such as -ISS-195. When an interim supplement is formalized, it will be assigned the next following even number, such as -ISS-196. 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 Each pilot is entitled to a personal copy of the flight manual, safety supplements, operational supplements, and a checklist. The required quantities should be ordered before needed to assure their timely receipt. Check with the publication distribution officer whose job is to fulfill T.O. requests. Basically, the required quantities must be ordered from the appropriate T.O. Index. T.O. 00-5-1 and T.O. 00-5-2 give detailed information for properly ordering these publications. 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 available for use with the manual. They are obtained through local purchase procedures and are listed in the Federal Supply Schedule (FSC Group 75, Office Change 13 iii
  11. 11. T.O. 1F-16A-1 Supplies, Part n. Check with supply personnel for assistance in procuring these items. CHANGE SYMBOL I The change symbol, as illustrated by the black line in the margin of this paragraph, indicates changes made to the current issue. WARNINGS, CAUTIONS, AND NOTES The following definitions apply to Warnings, Cautions, and Notes found throughout the manual. I WARNING I Operating procedures, techniques, etc., which could result in personal injury or loss of life if not carefully followed. PILOT'S RESPONSIBILITY - TO LET US KNOW Every effort is made to keep the flight manual current. Review conferences with operating personnel and a constant review of safety investigation and flight test reports assure inclusion of the latest data in the manual. Comments, corrections, and questions 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 11-215 through command headquarters to OO-ALCI YPVT, 6080 Gum Lane, Hill AFB, UT 84056-5825. PUBLICATION DATE 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 - F-16A and F-16B aircraft Operating procedures, techniques, etc., which could result in damage to equipment ifnot carefully followed. ~ F -16A aircraft [ID F-16B aircraft NOTE rnfl F -16B aircraft, forward cockpit ~ F -16B aircraft, rear cockpit ~ Air Defense ~ Belgium USE OF WORDS SHALL, WILL, SHOULD, AND MAY ~ Denmark 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. ~ Netherlands ~ Norway [g§] USAF ~ USAFIUSN An operating procedure, technique, etc., which is considered essential to emphasize. USE OF WORDS AS DESIRED AND AS REQUIRED ENGINE DESIGNATION CODES As desired allows pilot preference in switch/control positioning. As required indicates those actions which vary based on mission requirements. AIRSPEED REFERENCES All references to airspeed quoted in knots refer to indicated airspeed. iv Change 12 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 - Any engine I PW200 I FIOO-PW-200 I PW2201 FIOO-PW-220 or F100-PW-220E •
  12. 12. IO.lF-16A-l HAVE QUICK RADIO DESIGNATION CODES System and/or component effectivity for a particular HAVE QUICK radio version is denoted by a HAVE QUICK radio code enclosed in a box located in the text or on an illustration. The symbols and designations are as follows: No code HAVE QUICK II or HAVE QUICK II PHASE II I HQ II HAVE QUICK II I HQ 11.2 I tHAVE QUICK II PHASE II BLOCK DESIGNATION CODES/SERIAL NUMBER/ TAIL NUMBER CROSS-REFERENCE 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 illustrations.
  13. 13. T. O. 1F- 16A- 1 AIRCRAFT MODIFICATION/RETROFIT INFORMATION This list includes the applicable T.O.IECP effectivities. It is not an official status page. Refer to T.O. 0-1-1-4 for the complete listing of TCTO's. Throughout this manual, black TV screen symbols containing white numerals (D) are used to distinguish information related to aircraft which are modified by TV CODE/ T.O.NO. 1F-16-1751 SHORT TITLE Integration of Pressure Breathing for G (PBG) (ECP 1677) a specific T.O.IECP. 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 0 indicates that the information is only applicable to aircraft not modified by a specific T.O.IECP. EFFECTIVITY RETROFIT PRODUCTION ~ NA ~ All ~ ~ All NA ~ NA rrrn NA INQ] NA I Summary: • Retrofit authorized • Est start date - In work • Installs a new oxygen system which provides pressure breathing for g (PBG). @) 1F-16-1791 RLG Capability (ECP 1707A) ~ NA ~ TBD ~ TBD INQ] All ~ All ~All ~ Complete ~ NA INQ] NA I ~All ~ Complete MAll 1M All Summary: • Retrofit - As required • Est start date - In work • The INS gimbal INU is interchangeable with the ring laser gyro (RLG) INU. The only cockpit indications that a RLG INU is installed are the shorter alignment times, greater accuracy, and different memory addresses. VI Change 12
  14. 14. 10. 1 F- 16A-l TVCODEI T.O. NO. NA EFFECTIVITY PRODUCTION RETROFIT SHORT TITLE Early Provisions for Improved Capability (ECP 0350) ~ F-16A 80-0541 and on; F-16B 80-635 and on NA ~ F-16A 80-35471 NA FA-56 and on; F-16B 80-35881 FB-13 and on ~ F-16A 80-3596 and on; F-16B 80-3612 and on NA [N;J F-16A 78-0258 and on; F-16B 80-3649 and on M F-16A 78-0300 and on; F-16B 80-3689 and on I8Nl All NA NA I Summary: • Retrofit NA • Multinational Staged Improvement Plan (MSIP) installs improved avionics and provides for CARA, AMRAAM, and LANTIRN. BE1F-16-6007 NE1F-16-6001 N01F-16-6003 Incorporate Increased Area Horizontal Tail (ECP 0425) (~mJ M ECP 4003) ~ F-16A 80-0541 NA and on; F-16B 80-635 and on ~ F-16A 80-35471 FA-56 and on; F-16B 80-3588/ FB-13 and on [Q§ F-16A 80-3596 and on; F-16B 80-3612 and on I8Nl All ~ F-16A 78-0116/FA-01 thru 80-3546/FA-55; F-16B 78-0162/FB-01 thru 78-0173/FB-12 NA I ~ Complete M Complete Summary: • • • ~ mJ I!iQl Retrofit authorized Est start date - In work Increased horizontal tail area to reduce rotation speed, increase departure resistance, and make aircraft less susceptible to deep stall in the event of a departure. Change 12 VII
  15. 15. T. O. 1F- 16A- 1 TV CODE/ T.O.NO. ® 1F-16-1977 SHORT TITLE Improved Switch Guard for Fuel Master Switch (ECP 2120) EFFECTIVITY PRODUCTION RETROFIT All NA Summary: • Retrofit authorized • Est start date - In work • Rescission date - TBD • Modification replaces existing in-line switch guard with a side guard configuration. ff) 1F-16-1958 Z2 Software Provides F100-PW-220E Engine With PFL Capability (OCP 20007) ~ NA ~ All ~ NA ~ IQ§ NA ml All [N;] NA [N;] All rrn [NQ] NA Complete Complete Summary: • Retrofit authorized • Est start date - In work • Modification adds Pilot Fault List reporting capability to aircraft equipped with F100-PW-220E engine. ~ [!J§] F-16A 78-0001 thru 80-0540; F -16B All ~NA rn;J All [Q§ F-16A 78-0174 thru 78-0203; F-16B All [N;] NA Modify WOW Switch for Interruption of ChafflFlare Dispense System (ECP 1212) ~NA IQ§ NA 1F-16-1404 BE1F-16-6004 ~ F-16A 78-0212 thru 78-0257; F-16B All !NQ] NA I [fill Complete Summary: ~ All • Retrofit authorized • Est start date - In Work • Rescission date - Jul 01 • ~ Rescission date - TBD • Incorporate an NLG WOW safety mechanism to prevent inadvertent chaffi'flare dispensing on the ground. VIII Change 12
  16. 16. T.O. 1F-16A- 1 TVCODEI T.O.NO. ® IF-16-1404 EFFECTIVITY PRODUCTION RETROFIT SHORT TITLE ~NA Modify WOW Switch for Interruption of ChaffIFlare Dispense System (ECP 1212) ~ F-16A 80-0541 and on; F-16B NA ~NA ~NA ~NA [Qg] F-16A 80-3596 and on; F-16B NA ~NA ~ F -16A 78-0258 and on: ~NA Irm F-16B NA Complete I Summary: ~ All • Retrofit authorized • Est start date - In Work • Incorporate a right MLG WOW safety mechanism to prevent inadvertent chaff/flare dispensing on the ground. ~ ~ Provide Cockpit Indication of Probe Heater Malfunction (ECP 1193) ~ 1m ~ NA F-16A 87-0004 and on; F-16B 86-0197 and on All F-16A 78-0001 thru 83-1117; F -16B 78-0077 thru 83-1173 ~ IF-16-1365 Complete ~ F-16A 78-0174 thru 80-3611; F -16B 78-0204 thru 80-3615 Complete Complete ~ ~ I Summary: • Retrofit authorized • Est start date - In Work • Modification installs probe heat monitoring system and PROBE HEAT caution light to provide cockpit indication of possible probe heater failure or malfunction. 00 2J-F100(l)-594 2J-F1 00(II)-649 Redesigned 3rd Stage Fan and New 4th Stage Compressor Blades NA All F100-PW-200 Engines Summary: • • • • Retrofit - TBD Est start date - TBD Rescission date - TBD Modification reduces potential for 4th stage compressor blade failure. Completion of TCTO's removes the 600 KCAS limitation. Change 12 ix
  17. 17. T.O. 1F-16A-l TVCODEI T.O.NO. (FI) 2J-FIOO-930 SHORT TITLE Incorporation of Arctic Trim to PW200 Engines EFFECTIVITY PRODUCTION RETROFIT NA All FIOO-PW-200 Engines Summary: • • • Retrofit authorized Start date - Jun 98 Modification retrims engines to reduce occurrences of AB initiation stalls during takeoff. 00 IF-16-2170 Modification of the Ejection Mode Selector Valve Console (ECP 2362) NA All F-16B Summary: • • • ~ Retrofit authorized Start date - Feb 99 Modification enlarges the hole in the console to allow the EJECTION MODE SEL handle to seat properly in the NORM position. 5El-2-15-510 Incorporation of EDU 2.4.0. OFP to PW220 Engines NA All FIOO-PW-220 Engines Summary: • Retrofit authorized • Start date - Feb 98 • Modification installs EDU 2.4.0. OFP software for FIOO-PW-220 engines. Mter incorporation of EDU 2.4.0A OFP (TCTO 5El-2-15-5110), ~ actions are not required. 00 IF-16-2077 Installation of Improved Antiskid Braking System NA ~ All ~ All (OCP 5003B) Summary: • • • ~ Retrofit authorized Start date - Jan 99 Modification incorporates an improved Brake Control/Anti-skid Assembly to replace the current Brake Control and Antiskid Control Boxes. IF-16-2348 Summary: • • • • x Replacement of Cabin Low Pressure Switch NA ~ ~ NA All [g] All INEI All INOI All Retrofit authorized Start date - Mar 02 Rescission date - TBD Modification replaces the cabin low pressure switch, lowering CABIN PRESS caution light illumination from 27,000 to 22,500 feet. Change 13
  18. 18. 10. 1F-16A-l Block Designation Codes/Serio' Number/Tail Number Cross-Reference BLOCK 10 Serial and Tall Numbers Same for ~[A] **78-0001## **78-0002## **78-0003# **78-0005 **78-0007# **78-0008 **78-0010# **78-0011# **78-0013## **78-0015 **78-0017# **78-0019# **78-0020# **78-0021## *78-0022# *78-0024# *78-0025## *78-0026 *78-0027## *78-0038# *78-0039## *78-0040## *78-0042## *78-0043## *78-0044 *78-0047# *78-0049# *78-0050## *78-0051# *78-0052## *78-0053## *78-0054# *78-0056 *78-0057## *78-0058# *78-0059## *78-0060# *78-0061 *78-0062 *78-0063# *78-0064# *78-0065## *78-0066## *78-0068# *78-0069 *78-0070# *78-0073# *78-0074## *78-0076# *79-0290## *79-0294# *79-0296 *79-0300# *79-0303 *79-0306# *79-0307 *79-0308# *79-0309## *79-0310# *79-0311# *79-0312# *79-0314# *79-0317# *79-0322# *79-0324 *79-0326 *79-0327 *79-0329# *79-0330 *79-0331# 79-0332 79-0334 79-0335## 79-0336# 79-0337## 79-0340## 79-0341# 79-0342# 79-0344 79-0345# 79-0346# 79-0348# 79-0349## 79-0351## 79-0352 79-0353# 79-0354# 79-0355# 79-0357 79-0359# 79-0360 79-0362 79-0363# 79-0364 79-0365# 79-0366## 79-0368 79-0370 79-0371 79-0373## 79-0375 79-0376# 79-0380## 79-0381# 79-0382## 79-0383# 79-0384# 79-0387## 79-0388## 79-0389 79-0393# 79-0394## 79-0395# 79-0396# 79-0399## 79-0401## 79-0402## 79-0403## 79-0404 79-0405# 79-0406## 79-0407## 79-0408 79-0409# 80-0474# 80-0475# 80-0476# 80-0479# 80-0480# 80-0481 80-0482# 80-0483# 80-0485# 80-0487# 80-0488## 80-0489# 80-0492 80-0493# 80-0494# 80-0495 80-0496# 80-0497# 80-0498# 80-0499 80-0500# 80-0504 80-0505 80-0506# 80-0507# 80-0508# 80-0509# 80-0510# 80-0511 80-0512# 80-0513# 80-0515# 80-0518# 80-0519# 80-0520# 80-0521# 80-0522 80-0523# 80-0524 80-0525# 80-0526 80-0527 80-0528# 80-0529# 80-0530# 80-0531# 80-0533# 80-0535## 80-0537# 80-0538# 80-0539# 80-0540# ~OO **78-0077# **78-0079# **78-0080 **78-0081 **78-0082 **78-0083 **78-0084 **78-0085 **78-0087 **78-0088 **RETROFITrED FROM BLOCK 1 *RETROFITrED FROM BLOCK 5 #STORAGE **78-0089 **78-0090## **78-0091 **78-0094 **78-0096 **78-0097## **78-0098 *78-0099# *78-0100 *78-0101 *78-0102 *78-0103# *78-0104# *78-0107# *79-0411 *79-0412 *79-0413## *79-0414 *79-0415# *79-0417 *79-0418# 79-0420 79-0421 79-0422 79-0426# 79-0427 79-0428 79-0429 79-0430 79-0431 79-0432 80-0623# 80-0625# 80-0628 80-0629# 80-0630 80-0631 80-0633 80-0634 ~[AJ Serial Number/ Tall Number **78-0 116/FA-O1# **78-0117/FA-02# **78-0118/FA-03# ## INACTIVE Change 8 xi
  19. 19. T. o. 1F- 16A- 1 Block Designation Codes/Serial Number/Tail Number Cross-Reference **78-0 119/FA-04# **78-0 120/FA-05# **78-0 124/FA-09# **78-0125/FA-10# **78-0131/FA-16# **78-0 132/FA-17# *78-0 133/FA-18# *78-0 134/FA-19# *78-0 135/FA-20# *78-0 136/FA-21# *78-0 137/FA-22# *78-0 138/FA-23 # *78-0 140IFA-25# 78-0 141/FA-26# 78-0 142/FA-27# 78-0 143IFA-28# 78-0 145/FA-30# 78-0 146IFA-31# 78-0 147/FA-32# 78-0 149/FA-34 78-0151/FA-36# 78-0 152/FA-37# 78-0 153/FA-38# 78-0 155/FA-40# 78-0 158/FA-43 # 78-0 159/FA-44# 78-0 160/FA-45 # 78-0 161/FA-46# 80-3538/FA-47 80-3539/FA-48 80-3540/FA-49# 80-3541/FA-50# 80-35421FA-51# 80-3544/FA-53 80-3546/FA-55 ~oo Serial Number/ Tall Number **78-0162IFB-01 **78-0 163/FB-02 **78-0 164IFB-03# **78-0 165/FB-04 **78-0166IFB-05 *78-0 168/FB-07 *78-0 169/FB-08 *78-017 01FB-09 *78-0 171/FB-10 78-0173/FB-12 ~oo **78-0 1741E-174 **78-01761E-176 *78-01771E-177 *78-01781E-178 *78-0 1801E-180 *78-0181/E-181 *78-0 1821E-182 *78-0 1831E-183 *78-0 1841E-184 *78-0 1871E-187 *78-0 1881E-188 78-0 1891E-189 78-01901E-190 78-0191/E-191 78-01921E-192 78-0 1931E-193 78-0 1941E-194 78-0 1951E-195 78-0 1961E-196 78-0 1971E-197 78-01981E-198 78-01991E-199 78-02001E-200 78-0202lE-202 78-02031E-203 ~oo **78-0204IET-204 *78-0206IET-206 *78-0207IET-207 *78-0208IET-208 78-0210IET-210 80-0626IET-626 ~oo **78-0212/J-212 **78-0213/J-213 **78-0214/J-214 **78-0215/J-215 **78-0218/J-218 **78-0219/J-219 **78-0220/J-220 **78-0221/J-221 **78-0222/J-222 **78-0223/J-223 *78-0226/J-226 *78-0228/J -228 *78-0229/J-229 *78-0230/J-230 *78-0231/J-231 *78-0232/J-232 *78-0234/J-234 *78-0235/J-235 *78-0236/J-236 78-0238/J-238 78-0239/J-239 78-0240/J-240 78-0241/J-241 78-0242/J-242 78-0243/J -243 78-0245/J-245 78-0246/J-246 78-0247/J-247 78-0248/J-248 78-0249/J-249 78-0250/J-250 78-0251/J-251 78-0253/J-253 78-0254/J -254 78-0255/J-255 78-0256/J-256 78-0257/J-257 ~oo **78-0259/J-259 **78-0260/J-260 **78-0261/J-261 **78-0262/J-262 **78-0263/J-263 **78-0264/J-264 *78-0265/J-265 *78-0266/J -266 78-0267/J-267 78-0268/J-268 78-0269/J-269 78-0270/J-270 MOO **78-0272/272 **78-0273/273 *78-0275/275 *78-02761276 *78-0277/277 *78-0279/279 *78-0281/281 *78-0282/282 *78-0284/284 78-0285/285 78-02861286 78-02881288 78-02891289 78-0291/291 78-0292/292 78-0293/293 78-0295/295 78-0297/297 78-0298/298 78-0299/299 MOO ** 78-0302/302 *78-0304/304 78-0305/305 78-0306/306 BLOCK 15 Serial and Tall Numbers Same for ~OO ***80-0541# ***80-0542# ***80-0543# ***80-0545# ***80-0548# ***80-0549# ***80-0550 80-0551# ***80-0552# ***80-0553# ***80-0554 ***80-0556# 80-0557 ***80-0558 ***80-0559 **RETROFITTED FROM BLOCK 1 *RETROFITrED FROM BLOCK 5 #STORAGE ***AIR DEFENSE FIGHTER xii Change 8 ***80-0560# ***80-0561# ***80-0562# ***80-0563 ***80-0565 ***80-0567# ***80-0568# ***80-0569# ***80-0570# ***80-0571# ***80-0572# 80-0573## ***80-0575 ***80-0576# ***80-0577# ***80-0578 ***80-0579# ***80-0580# ***80-0581 ***80-0583# 80-0584 ***80-0587# ***80-0588# ***80-0589 ***80-0591# ***80-0593# ***80-0594 ***80-0596 ***80-0598# ***80-0601 ***80-0602 ***80-0603 ***80-0604 ***80-0605 ***80-0607# ***80-0608 80-0609 ***80-0611# ***80-0612 ***80-0613# ##INACTIVE f
  20. 20. T.O. 1F-16A-l Block Designation Codes/Serial Number/Tail Number Cross-Reference ***80-0614# ***80-0615 ***80-0616 ***80-0619# ***80-0620# ***80-0621# ***80-0622 81-0663 ***81-0665 ***81-0666 81-0667 ***81-0668 ***81-0669# 81-0670 ***81-0673 ***81-0674 ***81-0675 81-0676 81-0677 81-0678 81-0679 ***81-0680 ***81-0681 ***81-0682# 81-0683 ***81-0685 ***81-0686# 81-0687 81-0688# ***81-0690# ***81-0691# ***81-0693 ***81-0694# ***81-0695 ***81-0696# ***81-0698# ***81-0699 ***81-0700# ***81-0701# ***81-0702# ***81-0703 ***81-0705# ***81-0707# ***81-0708# ***81-0709 ***81-0710# ***81-0711# ***81-0712 ***81-0713# ***81-0715# ***81-0716# ***81-0718# ***81-0719# ***81-0720# ***81-0721## ***81-0722# ***81-0723 ***81-0725# ***81-0726# ***81-0727# ***81-0728# ***81-0729# ***81-0731 ***81-0732 ***81-0733# ***81-0734# ***81-0735# ***81-0736# ***81-0737# ***81-0738# ***81-0739# ***81-0740# ***81-0741# ***81-0742# ***81-0743# ***81-0744# ***81-0746# ***81-0748# ***81-0749# ***81-0751 ***81-0752# ***81-0753# ***81-0754# ***81-0755 ***81-0756# ***81-0757 ***81-0759 ***81-0760# ***81-0761 ***81-0762# ***81-0763 ***81-0764# ***81-0765# ***81-0767# ***81-0768# ***81-0769# ***81-0771# ***81-0772 ***81-0773 ***81-0774 ***81-0775 ***81-0776 ***81-0777 ***81-0778 ***81-0780# ***81-0781# ***81-0782 ***81-0783 ***81-0784# ***81-0785 ***81-0786 ***81-0787 81-0788 ***81-0789 81-0790 ***81-0791 81-0792# ***81-0793 81-0794# ***81-0795 81-0796 ***81-0797 ***81-0799 81-0800# ***81-0801 81-0802 ***81-0803 81-0804 ***81-0805 81-0806 ***81-0807 ***81-0809# 81-0810 ***81-0811# 82-0900 ***82-0901 82-0902 ***82-0903 82-0904 ***82-0905 82-0906 ***82-0907 82-0908 ***82-0910 82-0911 ***82-0913 82-0914 *** AIR DEFENSE FIGHTER *RETROFITTED FROM BLOCK 5 ***82-0915# ***82-0916# ***82-0917# 82-0918# ***82-0919 ***82-0921 82-0922 ***82-0923# 82-0924 ***82-0926 82-0928 ***82-0929 ***82-0930 82-0931 ***82-0932 82-0933 ***82-0935 82-0936 82-0938 82-0941 ***82-0942# 82-0944# ***82-0945# 82-0946 ***82-0947# 82-0948# 82-0949 ***82-0950 ***82-0951 82-0952# ***82-0953 ***82-0955 ***82-0956 82-0957 ***82-0958# ***82-0960# ***82-0961 82-0962# ***82-0963# 82-0964 ***82-0966# ***82-0967 82-0968# ***82-0969# 82-0970 ***82-0972 ***82-0973# ***82-0974# 82-0975# #STORAGE 82-0976 82-0977# ***82-0978# ***82-0979 82-0980 ***82-0981 82-0982# ***82-0983 ***82-0984 82-0986# ***82-0987 82-0988# ***82-0989 82-0991 ***82-0992 82-0993 ***82-0995 82-0996 ***82-0997 82-0999# ***82-1000 ***82-1001 82-1002# 82-1004# ***82-1005 ***82-1006 82-1007# ***82-1008 82-1009 ***82-1010# ***82-1012 82-1013 ***82-1014 ***82-1016# 82-1017# ***82-1019 82-1020 ***82-1021 82-1022# ***82-1023 82-1025 83-1066# 83-1068# ##INACTIVE Change 8 xiii
  21. 21. T.O. 1 F-16A-l Block Designation Codes/Serial Number/Tail Number Cross-Reference 83-1069# 83-1072# 83-1073# 83-1076# 83-1077# 83-1079 83-1080# 83-1081# 83-1083# 83-1084# 83-1085 83-1087 83-1088# 83-1090# 83-1091 83-1092# 83-1093 83-1094# 83-1095 83-1096# 83-1097 83-1098 83-1099 83-1100 83-1101# 83-1103 83-1104# 83-1105 83-1106 83-1108 83-1109 83-1110 83-1111 83-1112# 83-1113# 83-1114 ~[ID 80-0635 ***80-0636 ***80-0637 80-0638 ***81-0812 81-0813# 81-0815 81-0816 ***81-0817 ***81-0818 ***81-0819 ***81-0820 81-0821 81-0822# ***82-1026 ***82-1027 ***82-1031 ***82-1032# ***82-1033 ***82-1034 ***82-1035 ***82-1036 ***82-1039 ***82-1041 82-1043 ***82-1046 82-1047 ***82-1049 83-1166 83-1167# 83-1168# 83-1169 83-1170 83-1171# 83-1172 ~OO Change 8 87-0047IFA-103 87-0048/FA-104 87-0050/FA-106 87 -005l1FA-107 87-0052/FA-108 87-0053IFA-109 Serial Number/ Tall Number 80-3547/FA-56 80-3548/FA-57 80-3549/FA-58 80-3551/FA-60 80-3552/FA-61 80-3556IFA-65 80-3557/FA-66 80-3558/FA-67 80-3559/FA-68 80-3560IFA-69 80-3561/FA-70 80-3562/FA-71 80-35631FA-72 80-3564/FA-73 80-3565/FA-74 80-35661FA-7 5 80-3567IFA-76 80-3568IFA-77 *** AIR DEFENSE FIGHTER xiv 80-3569/FA-78 80-35721FA-81 80-3573/FA-82 80-3574/FA-83 80-3575/FA-84 80-3577/FA-86 80-3578/FA-87 80-3579/FA-88 80-3580/FA-89 80-3581/FA-90 80-35821FA-91 80-3583/FA-92 80-3584/FA-93 80-3585/FA-94 80-3586/FA-95 80-3587/FA-96 86-0073/FA-97 86-0074/FA-98 86-0075/FA-99 86-0076/FA-100 86-0077/FA-101 87-0046/FA-102 87-0054/FA-110 87-0055IFA-111 87-0056IFA-112 88-0039/FA-114 88-0040/FA-115 88-0041/FA-116 88-0042IFA-117 88-0043/FA-118 88-0044/FA-119 88-0045/FA-120 88-0046/FA-121 88-004 71FA-122 89-000 1/FA-123 89-0002/FA-124 89-00031FA-125 89-00041FA-126 89-0005/FA-127 89-00061FA-128 89-00071FA-129 89-00081FA-130 89-00091FA-131 #STORAGE 89-0010/FA-132 89-001l1FA-133 90-0025/FA-134 90-0026/FA-135 90-0027/FA-136 ~[ID 80-3589/FB-14 80-3590/FB-15 80-3592/FB-17 80-3593/FB-18 80-3594/FB-19 80-3595/FB-20 87 -000 lIFB-21 88-00 171E-0 17 88-00 181E-0 18 ~[ID 80-3612IET-612 80-3613IET-613 80-3614IET-614 80-3615IET-615 86-0 1971ET-197 86-0 1981ET-198 86-0 1991ET-199 87 -0022IET-022 [fOOOO 88-0048IFB-22 88-0049/FB-23 89-00 12/FB-24 ~OO 80-35961E-596 80-35971E-597 80-35981E-598 80-35991E-599 80-36001E-600 80-360 lIE-60 1 80-36021E-602 80-36031E-603 80-36041E-604 80-36051E-605 80-3606/E-606 80-3607/E-607 80-36081E-608 80-3609/E-609 80-3610/E-610 80-361l1E-611 82-10 ll1E-O 11 82-1024/E-024 83-10701E-070 83-107 41E-07 4 83-10751E-075 83-11071E-107 87-00041E-004 87 -OO05/E-005 87 -OO061E-006 87 -OO071E-007 87 -00081E-008 88-00 161E-0 16 80-3616/J-616 80-3617/J-617 80-3619/J -619 80-3620/J -620 80-3622/J -622 80-3623/J-623 80-3624/J -624 80-3627/J-627 80-3628/J -628 80-3630/J-630 80-3631/J -631 80-3632/J -632 80-3633/J-633 80-3635/J-635 80-3636/J-636 80-3637/J-637 80-3638/J -638 80-3640/J -640 80-3641/J-641 80-3642/J-642 80-3643/J -643 80-3644/J-644 80-3646/J -646 80-3647/J-647 80-3648/J -648 81-0864/J -864 81-08661J -866
  22. 22. T. O. 1F- 16A- 1 Block Designation Codes/Serial Number/Tail Number Cross-Reference 81-0867/J-867 81-0868/J-868 81-0869/J-869 81-0870/J-870 81-08711J-871 81-0872/J-872 81-0873/J-873 81-087 4/J-87 4 81-0875/J-875 81-0876/J-876 81-0877/J-877 81-0878/J-878 81-0879/J-879 81-0881/J-881 83-1192/J-192 83-1193/J-193 83-1194/J-194 83-1196/J-196 83-1197/J-197 83-1198/J-198 83-1199/J -199 83-1201/J-201 83-1202/J-202 83-1203/J-203 83-1204/J-204 83-1205/J-205 83-1206/J-206 83-1207 /J-207 84-1360/J-360 84-1362/J-362 84-1363/J-363 84-1364/J-364 84-1365/J-365 84-1366/J-366 84-1367/J-367 85-0135/J-135 85-0 136/J-136 85-0137/J-137 85-0138/J-138 85-0139/J-139 85-0140/J-140 85-0141/J-141 85-0142/J-142 85-0143/J-143 85-0144/J-144 85-0145/J-145 85-0146/J-146 86-0055/J-055 86-0057/J-057 86-0058/J-058 86-0060/J -060 86-0061/J-061 86-0062/J-062 86-0063/J -063 87-0508/J-508 87 -0509/J-509 87-0510/J-510 87-0511/J-511 87-0512/J-512 87-0513/J-513 87-0514/J-514 87-0515/J-515 87-0516/J-516 88-0001/J-001 88-0002/J -002 88-0003/J -003 88-0004/J-004 88-0005/J-005 88-0006/J -006 88-0008/J -008 88-0009/J -009 88-0010/J-010 88-0011/J-011 89-0013/J-013 89-00 14/J-014 89-0015/J-015 89-0016/J-016 89-0017/J-017 89-0018/J-018 89-0019/J-019 89-0020/J-020 89-00211J-021 ~[ID 80-3649/J -649 80-3650/J-650 80-3651/J-651 80-3652/J-652 80-3653/J-653 80-3654/J-654 80-3655/J-655 80-3656/J-656 80-3657/J-657 81-0882/J-882 81-0884/J-884 81-0885/J-885 83-1208/J-208 83-1209/J-209 83-1210/J-210 83-1211/J-211 84-1368/J-368 84-1369/J-369 86-0064/J-064 86-0065/J -065 87 -0066/J -066 87-0067/J-067 87 -0068/J -068 MOO 80-3658/658 80-3659/659 80-3660/660 80-36611661 80-3662/662 80-3663/663 80-3664/664 80-3665/665 80-3666/666 80-3667/667 80-3668/668 80-3669/669 80-3670/670 80-36711671 80-3672/672 80-3673/673 80-3674/674 80-3675/675 80-3677/677 80-3678/678 80-3680/680 80-36811681 80-3682/682 80-3683/683 80-3686/686 80-3687/687 80-3688/688 87 -07121712 ~OO 90-0942/900942 90-0943/900943 90-0944/900944 90-0945/900945 90-0946/900946 90-0947/900947 92-0404/920404 92-0405/405 92-0406/406 92-0407/407 92-0408/920408 92-0409/920409 92-0410/920410 ~[ID 90-0948/948 90-0949/949 90-0950/950 90-0951/951 90-0952/952 92-0452/452 92-0453/453 92-0454/454 92-0455/455 92-0456/456 92-0457/457 92-0458/920458 92-0459/920459 92-0460/920460 92-04611920461 MrnJ 80-3689/689 80-3690/690 80-3691/691 80-3692/692 80-3693/693 87-07111711 Change 12 xv
  23. 23. 10. 1 F- 16A- 1 F-1 Ei Fighting Falcon A B 1 F-16A-1-0003X @ xvi
  24. 24. 10. 1F- 16A- 1 SECTION I DESCRIPTION AND OPERATION TABLE OF CONTENTS Page The Aircraft . . . . . . . . . . . . . . . . . . . . . Aircraft General Arrangement Aircraft General Data ........... Aircraft Gross Weight (NC GW) . Cockpit Arrangement. . Engine IPW200 I .. . . . . . . . . . . . . . . . . . . . . . Engine General Description IPW200 I Engine Fuel System I PW200 I .......... Unified Fuel Control (UFC) I PW200 I Electronic Engine Control (EEC) 1-6 1-6 1-6 1-6 1-6.1 1-42 1-42 1-42 1-42 I PW200 I . . . . . . . . . . . . . . . . . . . . . . . . . 1-42 Backup Fuel Control (BUC) System I PW200 I .. . . . . . . . . . . . . . . . . . . . . . . Main Fuel Pump IPW200 I ..... Afterburner (AB) Fuel Pump IPW200 I ........................ Compressor Inlet Variable Vanes (CIVV's) I PW200 I . . . . . . . . . . . . . . . Rear Compressor Variable Vanes (RCVV's) IPW200 I ............ Compressor Bleed Air I PW200 I .. Pressurization and Dump Valve IPW200 I .................... _ Exhaust Nozzle IPW200 I . . . . . . . . . . . . . . . . Convergent Exhaust Nozzle Control (CENC) I PW200 I ................ Engine Oil System IPW200 I . . . . . . Engine Anti-Ice System I PW200 I ..... Engine ANTI ICE Switch I PW200 I .... Engine and Accessory Drive Gearboxes IPW200 I ........................... Engine Alternator I PW200 I ...... Engine Ignition System IPW200 I Jet Fuel Starter (JFS) I PW200 I • . . ENG & JET START Control Panel I PW200 I ............ JFS Switch [8] mEl IPW200 I ..... JFS RUN Light [8] mEl IPW200 I JFS Operation I PW200 I ....... Engine Controls and Indicators IPW200 I ........................ EEC BUC Switch [8] mEl I PW200 I EEC Caution Light IPW200 I . . . . . BUC Caution Light IPW200 I . . STARTING FUEL Switch [8] mEl I PW200 I ...........•.......•.• _ MAX POWER Switch I PW200 I . . . RPM Indicator I PW200 I ............. NOZ POS Indicator I PW200 I . . . . . . . . . FTIT Indicator I PW200 I ............. FUEL FLOW Indicator I PW200 I OIL Pressure Indicator IPW200 I .. HYD/OIL PRESS Warning Light I PW200 I . . . . . . . . . . . . . . . . . . . . . . . ENGINE Warning Light I PW200 I . . REDUCED IDLE THRUST (RIT) Switch IPW200 I ................ Throttle I PW200 I ............... Engine Operating Characteristics 1-44 1-44 IPW200 I ....................... Ground Operation I PW200 I . . . . 1-44 AB Operation in Flight IPW200 I BUC Operation I PW200 I ............. Engine I PW2201 ... . . . . . . . . . . . . . . . . . . . . . . . Engine General Description I PW2201 .... Engine Fuel System I PW220 I .......... Engine Control System I PW220 I . . . . . . . . Main Fuel Control (MFC) I PW2201 ... Afterburner (AB) Fuel Control 1-44 1-44 1-44 1-44 1-45 1-45 1-45 1-45 1-45 1-45 1-45 1-45 1-46 1-46 1-46 1-47 1-47 1-47 1-47 1-50 1-50 1-50 1-50 1-50 1-50 1-50 1-50 1-50 1-50 1-51 1-51 1-51 1-51 1-51 Non-AB Operation in Flight I PW200 I . . . . . . . . . . . . . • • . . . . . . 1-51 1-53 1-53 1-54 1-54 1-54 1-54 1-54 PW2201 . . . . . . . . . . . . . . . . . . . . . . . 1-54 Digital Electronic Engine Control (DEEC) I PW2201 ............... Secondary Engine Control (SEC) 1-56 I I PW2201 . . . . . . . . . . . . . . . . . . . . . . . . . Main Fuel Pump I PW2201 ........... Afterburner (AB) Fuel Pump I PW2201 . . . . . . . . . . . . . . . . . . . . . . Compressor Inlet Variable Vane (CIVV) Controll PW2201 ....... Rear Compressor Variable Vanes (RCVV's) I PW2201 ............. _ Compressor Bleed Air I PW2201 ... Pressurization and Dump Valve I PW2201 . . . . . . . . . . . . . . . . . . . . . Exhaust Nozzle I PW2201 . . . . . . . . . . . . . . . . Convergent Exhaust Nozzle Control (CENC) I PW2201 ................. Light-Off Detector (LO D) I PW220 I Engine Diagnostic Unit (EDU) I PW2201 ................... Engine Oil System I PW2201 . . Change 2 1-56 1-56 1-56 1-56 1-56 1-56 1-57 1-57 1-57 1-57 1-57 1-57 1-1
  25. 25. T.O. 1 F-16A-l EnbTine Anti-Ice System I PW220 I Engine ANTI ICE Switch I PW2201 .... Engine and Accessory Drive Gearboxes I PW2201 ......................... . Engine Alternator I PW2201 ..... . Engine Ignition System I PW220 I . Jet Fuel Starter (JFS) I PW2201 .. ENG & JET START Control Panel I PW2201 ........... . JFS Switch [8J mEl I PW2201 .... . JFS RUN Light [8J I PW2201 . JFS Operation I PW2201 ....... . Engine Controls and Indicators I PW2201 ................... . ENG CONT Switch I PW2201 ...... . AB RESET Switch [8J I PW220 I .... . ENGINE FAULT Caution Light~, rID em em I PW2201 .......................... . 1-57 1-58 1-58 1-58 1-58 1-59 1-59 1-59 1-59 1-59 1-60 1-60 1-60 1-60 ENGINE FAULT Caution Light LESS ~, LESS f1) I PW2201 ... . SEC Caution Light I PW2201 ......... . MAX POWER Switch[8J mEl I PW2201 .. RPM Indicator I PW2201 ............ . NOZ POS Indicator I PW2201 .. FTIT Indicator I PW2201 ........ . FUEL FLOW Indicator I PW220 I . OIL Pressure Indicator I PW2201 .. HYD/OIL PRESS Warning Light I PW2201 ....................... . ENGINE Warning Light I PW2201 .. REDUCED IDLE THRUST (RIT) Switch I PW2201 .............. . Throttle I PW220 I .............. . Engine Operating Characteristics I PW2201 ...................... . Ground Operations I PW2201 .. Non-AB Operation in Flight I PW2201 .................... . AB Operation in Flight I PW2201 . SEC Operation I PW2201 ........ . Fire and Overheat Detection System FIRE & OHEAT DETECT Test Button [A] mEl ............ . 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 TRAP FUEL Warning LESS ~ 1-2 Change 12 1-60 1-60 1-60 1-60 1-60 1-60 1-63 1-63 1-63 1-63 1-63 1-63 1-63 1-63 1-63 1-65 1-65 1-67 1-67 1-67 1-67 1-67 1-69 1-69 1-69 1-78 1-78 1-78 1-78.1 FUEL HOT Caution Light ...... . Fuel Tank Explosion Suppression System ..................... . Refueling System ... . Ground Refueling ......... . Air Refueling (AR) System .... . NVS AIR DISC MSL STEP Button ................ . Air Refueling (AR) Status Indicator ................. . Environmental Control System (ECS) Electrical Failures . Air-Conditioning .. _ Pressurization .............. . AIR SOURCE Knob [8J mEl " TEMP Knob [8J rntJ ...... . DEFOG Lever [8J mEl ....... . EQUIP HOT Caution Light ..... , . Cockpit Pressure Altimeter [8J mEl . CABIN PRESS Caution Light ... , , Anti-G System .. - - - ...... Electrical System .......... . Main AC Power System ......... . Overcurrent Protection Units Emergency AC Power System . DC Power System [BQ] ........ DC Power System LESS ~ . FLCS Power Supply ....... . External Power Provisions ..... . Electrical System Controls and Indicators ................ , . _ Electrical Power Distribution . Normal Operation .. Hydraulic System ..................... HYD PRESS Indicators and Warning Light ........................... . HYD PRESS Indicators ........... . HYD/OIL PRESS Warning Light ... . Emergency Power Unit (EPU) ....... . EPU Controls and Indicators . , ... . EPU Ground Safety Switch , ....... . EPU Switch .............. - - - - - - - - EPU Run Light .. . HYDRAZN Light . AIR Light ............ . EPU/GEN Test Switch ........ . EPU FUEL Quantity Indicator [8J mEl ................ . Hydrazine Leak Detector .. EPU Fired Indicator ... EPU Operation ........ . Landing Gear (LG) System ... . Main Landing Gear (MLG) .. Nose Landing Gear (NLG) . 1-79 1-79 1-79 1-79 1-79 1-80 1-80 1-80 1-80 1-80 1-80 1-80 1-83 1-84 1-84 1-85 1-85 1-85 1-85 1-85 1-85 1-85 1-85 1-86 1-86 1-90 1-90 1-90 1-90 1-101 1-101 1-101 1-101 1-101 1-104 1-104 1-104 1-106 1-106 1-106 1-106 1-106 1-106 1-106 1-106 1-107 1-107 1-107
  26. 26. 10. 1 F- 16A- 1 Landing Gear Controls and Indicators .. Landing Gear Handle ....... . Landing Gear Handle Down Permission Button ...... . DN LOCK REL Button . ALT GEAR Handle LG Warning Horn ........ _ HORN SILENCER Button .... . T.O.ILAND CONFIG Warning Light ..................... WHEELS Down Lights ..... Landing Gear Weight-on-Wheels (WOW) Switches ............ . Landing Gear Operation ........ . Nosewheel Steering (NWS) System .. NWS Controls and Indicators ........ . NWS NR DISC MSL STEP Button .. NWS Light .............. . NWS FAIL Caution Light ........ . Nosewheel Steering (NWS) System [ID . Wheel Brake System .. Toe Brake System .......... . Spin Down Braking System ... . Brakes Channel Switch lID rnfJ .. Parking Brake ~ ~ ........ . Antiskid System ........... . ANTI-SKID Switch lID mIl .. . ANTI SKID Caution Light .. Speedbrake System .......... . SPD BRK Switch ................ . SPEED BRAKE Position Indicator Drag Chute System m1 ~ ........ . DRAG CHUTE Switch m1 ~ .. Arrestment System. HOOK Switch ....... . HOOK Caution Light . Wing Flap System ................ _ Leading Edge Flaps (LEF's) .......... . LE FLAPS Switch ................ . LE FLAPS Caution Light .. Trailing Edge Flaps (TEF's) (Flaperons) ............ . ALT FLAPS Switch ..... . Flight Control System (FLCS) FLCS Limiters ....... . AOAlG Limiter ... . Roll Rate Limiter ........ . Rudder Authority Limiter Yaw Rate Limiter . FLCS Gains .... Cruise Gains . < < < < < , •••• •••••••••• 1-107 1-107 1-107 1-107 1-107 1-109 1-109 1-109 1-109 1-109 1-109 1-113 1-113 1-113 1-113 1-113 1-113 1-113 1-113 1-114 1-114 1-114 1-114 1-115 1-118 1-118 1-118 1-118 1-118 1-118 1-120 1-120 1-120 1-120 1-120 1-120 1-120 1-120 1-120 1-121 1-121 1-121 1-121 1-121 1-121 1-127 1-127 Takeoff and Landing Gains 1-127 Standby Gains .......... 1-127 FLCS Data Recorder ~ mEl . 1-127 Gun Compensation. . . . . . . . . . . . 1-127 Flight Control System (FLCS) Controls ................. 1-127 Stick .......... _ 1-127 Rudder Pedals. . . . . . . . . . . . . . . 1-130 1-130 MANUAL TRIM Panel ~ illf] ...... MANUAL PITCH Override (MPO) Switch ........................ 1-130 STORES CONFIG Switch lID illf] . 1-130 1-130 Low Speed Warning Tone. . .. . .. . . . FLIGHT CONTROL Panel (FLCP) ~ ~ ............................ 1-130 FLCS Warning, Caution, and Indicator Lights ............................ 1-130 T.O.ILAND CONFIG Warning Light. . . . . . . . . . . . . . . . . . . . . . . 1-130 FLT CONT SYS Caution Light. . 1-130 DUAL FC FAIL Warning Light . 1-130 Trim .............. " . .. . . . . . . . .. . .. 1-132 1-133 Autopilot ............. _ 1-133 Autopilot Operation . . _ Stick Steering .... 1-133 AOA System .................. 1-138 AOA Indicator . . 1-138 AOA Indexer ....... 1-138 HUD AOA Display. . 1-138 1-139 Air Data System. . . . . . . . . . .. ........... 1-139 Air Data Probes ................... 1-139 AOA Transmitters ...... . 1-139 Total Temperature Probe . 1-139 Static Pressure Ports ... 1-139 Probe Heat Monitor ~ ., .......... . 1-139 PROBE HEAT Switch. . . . .. . ..... . 1-139 Air Data Converter (ADC) . 1-141 ADC Caution Light ............... . Central Air Data Computer (CADC) .... . 1-141 1-141 CADC Caution Light .............. . 1-141 Warning, Caution, and Indicator Lights .. 1-141 Voice Message System (VMS) ........ . 1-143 VOICE MESSAGE Switch rru rn£l ... . 1-143 MASTER CAUTION Light ......... . 1-143 Caution Light Panel ................. . 1-152 MAL & IND LTS Test Button .. 1-152 Pilot Fault List (PFL) ... 1-152.1 Lighting System ..... . Exterior Lighting .......... , 1-152.1 1-152.1 Anticollision Strobe Light , 1-152.1 PositionIFormation Lights .. _ 1-152.1 Air Refueling Lights ...... - ... . < •• _ < Change 6 1-3
  27. 27. 10.lF-16A-1 Vertical Tail-Mounted Floodlight (illj ......... . 1-152.1 Landing and Taxi Lights ... . 1-154 Identification (ID) Light ~ ...... . 1-154 Identification (ID) Light ~ M ~ .. 1-154 Interior Lighting ................... . 1-154 PRIMARY CONSOLES Knob . 1-155 PRIMARY INST PNL Knob ... . 1-155 NAV/FREQ DISP Knob ~ ~ .. . 1-155 FREQ DISP Knob ~ ........ . 1-155 MAL & IND LTS Switch .. . 1-155 FLOOD INST PNL Knob .. . 1-156 FLOOD CONSOLES Knob . 1-156 Utility Light ...... . 1-156 Cockpit Spotlights . 1-157 Escape System ...... . 1-157 Canopy ....................... . 1-157 Canopy Controls and Indicators .... - 1-157 MANUAL CANOPY CONTROL Handcrank ................. _ 1-157 Canopy Handle ~ ~ . 1-157 Canopy Jettison ......... , ........ . 1-157 Ejection Seat ............... . 1-157 Ejection Seat Controls and Indicators .............. ______ _ 1-163 Ejection Handle .................. . 1-163 SHOULDER HARNESS Knob ..... 1-163 EMERGENCY MANUAL CHUTE Handle ...................... . 1-163 Ejection Safety Lever ............. . 1-163 SEAT NOT ARMED Caution Light .. 1-163 SEAT ADJ Switch ................. ' 1-163 Shoulder Harness StrapsfParachute Risers ......................... . 1-163 Inertia Reel Straps . 1-163 Lapbelt .......................... . 1-163 Survival Kit ........................ . 1-163 RADIO BEACON Switch ~ ~ ~ ~~ ......................... . 1-163 Emergency Oxygen ............... . 1-164 Ejection Seat Operation ............. . 1-164 Ejection Mode Envelopes . 1-164 Ejection Sequence Times ...... . 1-164 Canopy Jettison/Seat Ejection .. 1-164 Ejection Seat Performance .1-164 Oxygen System .......... . 1-173 Liquid Oxygen System ...... . 1-173 Pressure Breathing for G (PBG) 1-173 Oxygen System Controls and Indicators ................ . 1-173 Oxygen Duration ....... . 1-173 Emergency Oxygen System . 1-173 Oxygen System Schematic 1-173 m ................ . 1-4 Change 12 1-180 1-180 1-180 1-180 1-180 1-180 Communications System . Antenna Locations ............... . Have Quick (HQ) System LESS ~ . Single Word of Day (WOD) ... . Single WOD Transfer ......... . Multiple Word of Day (MWOD) . Automatic MVOD Loading I HQ 11.2 I 1-182 1-182 1-182 1-182 1-182 ...............•.... Time-of-Day (TOD) Transmission . Time-of-Day (TOD) Reception .. Net Number ..................... , Antijamming (AJ) Mode Operation HAVE QUICK (HQ) UHF Radio LESS ~ .......... . UHF Radio Control Panel Function Knob ..... - - - l1ode Knob I HQ I I I ... . Mode Knob I HQ I I . 2 I .. CHAN Knob ............. . Manual Frequency Knobs A-3-2-T Knob I HQ II I .. _ A-3-2 Knob I HQ 11.2 I .. VOL Knob .......... . SQUELCH Switch. . . . . . TONE Button I HQ II I . . . . . CHAN Display I HQ II. 2 I . Frequency/Status Display I HQ I I . 2 I •.••••.•.•..•. 1-182 1-182 1-183 1-183 1-183 1-183 1-184 1-184 1-184 1-184 1-184 1-184 1-184 •• STATUS Button I HQ 11.2 I • ,. T-TONE Switch I HQ 11.2 I ........... TEST DISPLAY Button I HQ 11.2 I ... ZERO Switch I HQ II. 2 I ........... " FILL Connector I HQ 11.2 I . ,. UHF RADIO ~ ............ , ,. UHF Radio Control Panel . ,. Function Knob . __ ... __ .. _ __.. . ........... Mode Knob..... CHAN Knob...... .... .. .. " Manual Frequency Knobs . VOL Knob....... . . . . . . . . SQUELCH Switch. , TONE Button ............... UHF ANT SEL Switch~ ~ . VHF Radio .................... VHF Radio Control Panel. . Function Knob ........ Preset CHAN Knob. Mode Knob. . . . . . . . . . . . . . . Manual Frequency Knobs . VOL Knob ............ SQ DIS TONE Switch. . . . LOAD Button crfj ~ ~ . . . . . WB MEM LOAD Switch [Illi] . 1-184 1-184.1 1-184.1 1-184.1 1-184.1 1-184.1 1-184.1 1-184.1 1-184.1 1-184.1 1-184.1 1-185 1-185 1-185 1-185 1-185 1-185 1-185 1-186 1-186 1-186 1-187 1-187 1-187 1-187 1-187
  28. 28. 10. 1 F- 16A- 1 HF Radio I@l [A] . . . . . . . . . . . . . . . . . HF Radio Control Panel ~ ~ .,.... OFF VOL Control Knob ............ OFF SQL Control Knob .............. USB AM LSB Select Switch .......... Preset Channel Select Knob . 1-187 1-187 1-188 1-188 1-188 1-188 CHAN Display ......... . Frequency Select Switches .. 1-188 1-188 FREQ Display ..... . LOAD TEST Switch .. 1-188 1-188 PRE Tune Light . 1-188 Change 12 1-4.1/(1-4.2 blank)
  29. 29. 10. 1F- 16A- 1 XMIT Light ..... . 1-188 1-188 MAN Tune Light .. UNTUNED Light .......... . 1-188 Built-In Test (BIT) Function ..... . 1-189 Radio Channel/Frequency Indicator (RCFI) ....................... .. 1-189 COMM Control Panel ~ rnfJ .. . 1-189 HOT MIC CIPHER Switch . 1-189 INRCOM/SV Knob .......... . 1-190 THREAT Tone Knob . .. 1-190 MSL Tone Knob .......... . 1-190 Master Zeroize Switch ~ rnfJ ., 1-190 Secure Voice System LESS IBNI ....... . 1-190 1-190 Secure Voice Control Panel ~ POWER Switch ............... . 1-190 ZEROIZE Switch 1-190 DELAY Switch . 1-191 FILL Switch .... 1-191 MODE Switch ........ . 1-191 1-191 PLAIN Cipher Switch. " . Inertial Navigation Set (INS) ........... . 1-191 Tactical Air Navigation (TACAN) System . 1-192 1-192 TACAN Control Panel ............... . TACAN Function Knob .. . 1-192 VOL Knob ........ . 1-192 1-192 XIY Channel Ring '" Units Channel Knob .............. . 1-192 Hundreds-Tens Channel Knob 1-192 1-192 CHANNEL Display .' ..... 1-192 TEST Pushbutton .. 1-193 TEST Light ................. . Instrument Landing System (lLS) 1-193 ILS Control Panel ....... . 1-193 ILS Frequency Knobs . 1-193 1-193 ILS PWR Switch .. 1-193 ILS VOL Ring .................... . MRK BCN Light .................. . 1-193 IFF System ........................... . 1-194 IFF Advisory Function ............... . 1-194 IFF Control Panel ..................... . 1-194 1-194 Mode 4 CODE Knob ~ ........... . Mode 4 CODE Knob LESS ~ . 1-194 REPLY Light IBNI ............ , .... . 1-194 1-195 REPLY Light LESS ~ ............ . TEST Light ...................... . 1-195 IFF MASTER Knob ..... . 1-195 RAD TEST MON Switch . 1-195 1-195 IFF IDENT Switch .... '" ....... . 1-195 Mode TEST Switches . 1-196 Code Wheels ....... . 1-196 MODE 4 SwitchM ...... . 1-196 MODE 4 Switch LESS IBNI .... . 1-196 MODE 4 Monitor Switch ~ .. em .. MODE 4 Monitor Switch LESS ~ .. IFF ANT SEL Switch ~ rn.El ..... . IFF IDENT Button ....... . IFF Caution Light AIFF System ~ ..... Transponder ~ Interrogator!BQ] .......... . IFF Advisory Function [@] AIFF Control Panel!BQ] .... Mode 4 CODE Knob !BQ] M-4REPLYLight~ .... AIFF MASTER Knob !BQ] M-4 Switch!BQ] ........... . Mode 4 Monitor Switch !BQ] M-l Switch!BQ] M-2 Switch!BQ] ... M-3/A Switch [@] M-C Switch ~ ................ . IFF ANT SEL Switch !BQ] ~ rnfJ . IFF IDENT Button ~ ........ . IFF Caution Light ~ .. INSTR MODE Select Panel .... INSTR HDG Knob ~ rn£l . INSTR MODE Knob ........ . Navigation Aids and Display .. Instrument Modes . . ..... . Flight Instruments .. Altimeter ............... . AirspeedlMach Indicator ......... . Standby Attitude Indicator (SAl) . Vertical Velocity Indicator (VVI) .. Magnetic Compass .............. , Attitude Director Indicator (ADI) ..... . Horizontal Situation Indicator (HSI) .. Clock ..................... . Standard Flight Data Recorder (SFDR) [BQ] ................. . F-16B Aircraft ............ . Engine Controls IPW200 I .. Throttle IPW200 I ~ ....... . BUC Switch IPW200 I ~ .. . Engine Controls I PW2201 .. . Throttle I PW220 I ~ ........... . ENG CONT Switch I PW2201 ~ Fuel System .................... . Fuel Control Panel [ID!J Speedbrake System ..... . SPD BRK Switch [ID!] .... . Drag Chute System [N;] IBQ] ......... . DRAG CHUTE Switch [frn ~ ~ Landing Gear (LG) System ........ . DN LOCK REL Button [ID!J Change 12 1-196 1-196 1-196 1-196 1-196 1-196 1-197 1-197 1-197 1-198 1-198 1-198 1-198 1-198 1-198 1-198 1-198 1-198 1-199 1-199 1-199 1-200 1-200 1-200 1-200 1-200 1-207 1-207 1-207 1-207 1-209 1-209 1-209 1-209 1-209 1-209 1-212 1-212 1-212 1-212 1-212 1-212 1-212 1-212 1-212 1-212 1-212 1-212 1-212 1-213 1-213 1 -5
  30. 30. lO. 1 F- 16A-1 Flight Control System Stick Control Operation ........ . STICK CONTROL Switch rnfJ .. Stick Indicator ~ ........... . Stick OVRD Lights [ID .. Escape System rnJ ................... . EJECTION MODE SEL Handle~ . Communications System [ID .......... . INSTR MODE Select Panel [ID .. Flight Instruments ~ . - ..... Accelerometer ~ ........ . RadarlElectro-Optical (REO) Display~ ................. . Stores Management Subsystem (SMS)~ .................. _ Fire Control Radar (FCR) ~ .. Throttle and Stick Switches/ Controls ~ .............. . ARMT CONSENT Switch ~ . Servicing Diagram 1-213 1-213 1-213 1-213 1-213 1-213 1-213 1-214 1-214 1-214 1-214 1-214 1-214 1-214 1-214 1-214 1-214 THE AIRCRAFT The F -16A is a single-engine, single-seat, multirole tactical fighter with full air-to-air and air-to-surface combat capabilities. The F-16B is a two-seat (tandem) version and performs the secondary role of a trainer. The fuselage is characterized by a large bubble canopy, forebody strakes, and an under fuselage 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 fly-by-wire system. The fire control system includes a fire control radar with search and tracking capability, a radar electro-optical (REO) display, and a head-up display (RUD). A stores management system (SMS) presents a control panel and visual display for inventory, control, and release of all stores. Basic armament includes a fuselage-mounted multibarrel 20 mm gun and an air-to-air missile on each wingtip. Additional stores of various types can be carried on pylons mounted under the wings and on the fuselage centerline. 1-6 Change 2 AIRCRAFT GENERAL ARRANGEMENT Refer to figure 1-1 for general arrangement and overall view of the aircraft. AIRCRAFT GENERAL DATA Refer to figure 1-2. The aircraft approximate dimensions are: • Span - including missile fins 32 feet 10 inches • Length - including nose probe 49 feet 6 inches • Height - top of vertical tail 16 feet 8.5 inches • Height - top of canopy 9 feet 4 inches • Tread • Wheelbase = 7 feet 9 inches 13 feet 2 inches Refer to TURNING RADIUS AND GROUND CLEARANCE, Section II. AIRCRAFT GROSS WEIGHT (A/C GW) [.B] IPW200 I Block 10 The GW of the aircraft including pilot, oil, two tip AIM -9 missiles, and a full load of 20 mm ammunition is approximately 17,500 pounds and with full internal JP-8 fuel 24,800 pounds. I PW2201 Aircraft is approximately 100 pounds heavier. [ID IPW200 I Block 10 The GW of the aircraft including two pilots, oil, two tip AIM-9 missiles, and a full load of 20 mm ammunition is approximately 18,300 pounds and with full internal JP-8 fuel 24,400 pounds. I PW2201 Aircraft is approximately 100 pounds heavier. ~ I PW200 I Block 15 The GW of the aircraft including pilot, oil, two tip AIM-9 missiles, and a full load of 20 mm ammunition is approximately 17,900 pounds and with full internal JP-8 fuel 25,200 pounds. I PW2201 Aircraft is approximately 100 pounds heavier. [ID IPW200 I Block 15 The GW of the aircraft including two pilots, oil, two tip AIM-9 missiles, and a full load of 20 mm ammunition is approximately 18,700 pounds and with full internal JP-8 fuel 24,800 pounds. I PW2201 Aircraft is approximately 100 pounds heavier.
  31. 31. T. O. 1F- 16A- 1 These GW's are approximate and shall not be used for computing aircraft performance. For maximum GW limitations, refer to Section V, OPERATING LIMITATIONS. For detailed information, refer to T.O. IF-16A-l-l, Part 1. COCKPIT ARRANGEMENT Refer to figure 1-3. The cockpit arrangement 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. Change 2 1-6.1 /(1-6.2 blank)
  32. 32. General Arrangement (Typical) 11 26 15 27 ~28 ~30 31 32 ~-~ rn For antenna locations, refer to ANTENNA LOCATIONS, this section. 33 _ ')c 34 47 64 1_ 20 3. 4. 5. 6. 7. R 90 10. 11> 12. 13. 14. 15. 16. 17. ~~~17 35 Air Data IPitot) Probe 59 57 Nose Radome 1 R LEF Drive Unit AOA Probe 19. Hydraulic Reservoir AOA Transmitter 20. AR Slipway Forward Electronic Equipment Bay 21. FLCS Accumulators Cockpit Pressure Regulator 22. Anticollision Strobe Light Power Supply Cockpit Pressure Safety Valve 23. Vertical Tail Attachment Fittings Head--Up Display (HUD) 24. Vertical Tail Instrument Panel 25. BLOCK 15 Vertical Tail-Mounted Floodlight Canopy (Movable) 26. Anticollision Strobe Light Ejection Seat 27. Rudder 28. Position Light Canopy IFixed) 29. Rudder ISA AIM--9 Missile Missile Launcher 30. [N£] INOI Drag Chute Fairing AR and Formation Light 31. Turbofan Engine Position/Formation Light 32. Speed brake Static Discharger 33. Speedbrake Actuator 34. 35. 36. 37. 38. 39. 40. 41. 42. 43. 44. 45. 46. 47. 48. 49. 50. 51. ChaffIFlare Dispenser Horizontal Tail ISA 52. Horizontal Tail 53. Formation Light 54. Flaperon ISA 55. Hook 56. Flaperon 57. Wing Structural Box 58. Fixed Trailing Edge Panel 59. Asymmetry Brake 60. LEF Rotary Actuator 61. LEF Torque Shaft 62. 63. LEF Wing Attachment Fittings 64. MLG 65. MLG Door LEF Angle Drive Gearbox 44 43 Air-Conditioning Package M61A1 20MM Gun Ammunition Drum EPU Nitrogen Bottle Gun Port NLG Door BLOCK 10 Total Temperature Probe Position Light NLG Engine Air Inlet Left Console Throttle Strake Lower Equipment Compartment IAOland IOEllNOlrn ID Light 1F-16A-1-1004X® :-I 9 -;n ...... ~ ~ I ........ Figure 1-1.
  33. 33. 10. 1 F-16A-l General Data m (Typical) MISSILE LAUNCHER OUTBOARD STORES LOCATIONS 18 FT 6 IN. ,.....,...._- -_.1 ...... SPEEDBRAKE HINGE 49 FT 6 IN. ----------------------OVERALL LENGTH--------------------~ 1o+-~~47.50 r 15.35 1 1 95.0 101.0 1 1 16 FT 8.5 IN. OVERALL HEIGHT ~-......-49.81 NOTE: Dimensions are in inches unless specified otherwise. 1F-16A-1-1 005-1 X® Figure 1-2. (Sheet 1) 1-8
  34. 34. 10. 1F- 16A- 1 WINGS Area ...................•... 300 Sq Ft Span ......•...........•... 30 Ft Aspect Ratio ............... 3.0 Taper Ratio ................ 0.2275 Sweep (LE) ................ 40 0 Dihedral ................... 0 0 Airfoil ...................•. NACA 64A204 Incidence ..•....•...•..•.•. 0 0 Twist At BL 54.0 ............. 0 0 At BL 180.0 ............ 3 0 Flaperon Area ............. 31.32 Sq Ft LEF Area .................. 36.71 Sq Ft HORIZONTAL TAILS Area ...................... 63.70 Sq Ft Aspect Ratio ............... 2.114 Taper Ratio ................ 0.390 (Theo) Sweep (LE) ................ 40 0 Dihedral ................... -10 0 Airfoil At Root ................. 6% Biconvex At Tip .................. 3.5% Biconvex VERTICAL TAIL Area ...................... 54.75 Sq Ft Aspect Ratio ............... 1.294 Taper Ratio •........•..•.•. 0.437 Sweep (LE) ................ 47.5 0 Airfoil At Root. ................ 5.3% Biconvex At Tip .................. 3.0% Biconvex Rudder Area ....•........•. 11.65 Sq Ft VENTRAL FIN (EACH) Area ....................... 8.03 Sq Ft Span ....................... 23.356 In. Theo (27.5 In. Actual) Aspect Ratio ............... 0.472 (Theo) Taper Ratio ................. 0.760 (Theo) Sweep (LE) ................. 30 0 Dihedral (Cant) .............. 15 0 Outboard Airfoil At Root ..........•...... 3.886% Modified Wedge At Tip ................... Constant 0.03R SPEEDBRAKES Area (4 Element Clamshell) .. 14.26 Sq Ft (3.565 Sq Ft Ea) LANDING GEAR (LG) Main Gear (MLG) Tire Size ................. 25.5 x 8-14 20 Ply Tire Size ................. 25.5 x 8-14 18 Ply Stroke ............•..••.. 10.5 In. Static Rolling Radius ..... 11.0 In. Nose Gear (NLG) Tire Size ................ 18 x 5.7-8 18 Ply Tire Size ................ 18 x 5.5 14 Ply Stroke .................. 10.0 In. Static Rolling Radius ..... 7.5 In. I I ENGINE F100-PW-200/220 Thrust ..........•........ 25,000 Lb Class Engine Compressor Face Diameter ..•••.... 34.8 In. Engine Length ........... 191.16 In. 32 FT 10 IN. 14-----0VERALL SPAN W/MISSILES----~ 1+---- 31 FT OVERALL SPAN W/O MISSILES ---~ 1F-16A-1-1 005-2X ® Figure 1-2. (Sheet 2) 1-9
  35. 35. T.O. 1 F-16A-1 General Data LESS GD (Typical) MISSILE LAUNCHER OUTBOARD STORES LOCATIONS 24.05 t I f I _--=__ I 18 FT 0.34 IN. SPEEDBRAKE HINGE 49 FT 6 IN. ~--------------------OVERALL LENGTH--------------------~ t+----t~ 47.50 15.35 r 1 95.0 101.0 j j 16 FT 8.5 IN. OVERALL HEIGHT STATIC GROUND LINE t+---~-49.81 NOTE: Dimensions are in inches unless specified otherwise. 1 F-16A-1-1 006-1 X ® Figure 1-2. (Sheet 3) 1-10
  36. 36. T.0.1F-16A-1 WINGS Area .. _________ .. __ . ___ .. _. 300 Sq Ft Span __ ... ____ . _. ____ .. _. _. 30 Ft Aspect Ratio ..... _... _. _... 3.0 Taper Ratio ................ 0.2275 Sweep /LE) .....•.......... 40 0 Dihedral ................... 0 0 Airfoil ..................... NACA 64A204 Incidence ..•............... 0 0 Twist At BL 54.0 ............. 0 0 At BL 180.0 ............ 3 0 Flaperon Area •............ 31.32 Sq Ft LEF Area .................. 36.71 Sq Ft HORIZONTAL TAILS Area ...................... 49.0 Sq Ft Aspect Ratio ............... 2.598 Taper Ratio ................ 0.3 (Theo) Sweep (LE) ................ 40 0 Dihedral ................... -10 0 Airfoil At Root. ................ 6% Biconvex At Tip ...........•...•.. 3.5% Biconvex VERTICAL TAIL Area ...................... 54.75 Sq Ft Aspect Ratio ............... 1.294 Taper Ratio .•.....•........ 0.437 Sweep (LE) ................ 47.5 0 Airfoil At Root .•..•............ 5.3% Biconvex At Tip .................. 3.0% Biconvex Rudder Area ............... 11.65 Sq Ft VENTRAL FIN (EACH) Area ....................... 8.03 Sq Ft Span ....................... 23.356 In. Theo /27.5 In. Actual) Aspect Ratio ............... 0.472 (Theo) Taper Ratio ................. 0.760 (Theo) Sweep (LE) ................. 30 0 Dihedral (Cant) .......•...... 15 0 Outboard Airfoil At Root ................. 3.886% Modified Wedge At Tip ................... Constant 0.03R SPEEDBRAKES Area (4 Element Clamshell) .. 14.26 Sq Ft (3.565 Sq Ft Ea) LANDING GEAR (LG) Main Gear (MLG) Tire Size ................. 25.5 x 8-14 20 Ply Tire Size ................. 25.5 x 8-14 18 Ply Stroke ................... 10.5 In. Static Rolling Radius ..•.. 11.0 In. Nose Gear (NLG) Tire Size ................ 18 x 5.7-8 18 Ply Tire Size ................ 18 x 5.5 14 Ply Stroke ....•......•....•. 10.0 In. Static Rolling Radius ..... 7.5 In. I I ENGINE F100-PW-200 Thrust ...•.•.•.••••.••••. 25,000 Lb Class Engine Compressor Face Diameter .••...... 34.8 In. Engine Length ........... 191.16 In. 32 FT 10 IN. 14-----0VERALL SPAN W/MISSILES-------+t 14---- 31 FT OVERALL SPAN WIO MISSILES ---~ 1F-16A-1-1006-2X® Figure 1-2. (Sheet 4) 1- 11
  37. 37. 10. 1 F- 16A-l Cockpit Arrangement ~ IBFI (Typical) Block to FOR DETAILS OF OXYGEN REGULATOR PANEL DIFFERENCES, SEE THE INDIVIDUAL EQUIPMENT ILLUSTRATION. RIGHT AUXILIARY CONSOLE STICK LEFT CONSOLE RIGHT CONSOLE LOCATED ON SHELF BEHIND SEAT. 1 F-16A-1-1007X@ Figure 1-3. (Sheet 1) 1-12
  38. 38. T.O. 1F-16A- 1 Cockpit Arrangement [8J IBFI (Typical) Block 10 LEFT CONSOLE 20 / / ) 2 19 3 4 5 11 25 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. RADAR Control Panel UHF Radio Control Panel FC/NAV Panel TACAN Control Panel MANUAL TRIM Panel AVTR Control Panel ECM Pod Control Panel G-Suit Hose Connection ANTI G TEST Button TEST Switch Panel DEFOG Lever FLIGHT CONTROL Panel Fuel Controi Panel CANOPY JETTISON T-Handle COMM Control Panel EPU Control Panel ELEC Control Panel Throttle FRICTION Control ENG & JET START Control Panel MANUAL PITCH Override Switch CHAFF/FLARE Dispense Button Throttle REDUCED IDLE THRUST Switch Stowage I SF I STICK CONTROL Switch 1F-16A-1-1008X® Figure 1-3. (Sheet 2) 1- 13
  39. 39. T.O. 1 F-16A-1 Cockpit Arrangement LEFT AUXILIARY CONSOLE 20 ~ I BF I (Typical) Block to RIGHT AUXILIARY CONSOLE 1 23 L_-h 4 ""r ~ ~~.~~ l71G~· ~I 19 18 16 l I :~~kd 14 11 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 9 8 5 EMER STORES JETTISON Button (Covered) WHEELS Down Lights (Green) HOOK Switch (Lever Lock) ANTI-SKID Switch LANDING TAXI Lights Switch DN LOCK REL Button LG Handle Down Permission Button LG Handle Warning Light (Red) LG Handle IFF Control Panel THREAT WARNING AUX (DIM) Knob THREAT WARNING AUX Controls and Indicators ALT GEAR Reset Button ALT GEAR Handle SPEED BRAKE Position Indicator LE FLAP POSITION Indicator (Deactivated) STORES CON FIG Switch HORN SILENCER Button GND JETT ENABLE Switch (Lever Lock) BRAKES Channel Switch 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. Figure 1-3. (Sheet 3) 1-14 Magnetic Compass Clock OXY FLOW Indicator System A HYD PRESS Indicator System B HYD PRESS Indicator EPU FUEL Quantity Indicator Cockpit Pressure Altimeter LIQUID OXYGEN Quantity Indicator Caution Light Panel FUEL QTY SEL Knob EXT FUEL TRANS Switch IF-16A-1-1009X®
  40. 40. T. O. 1F- 16A- 1 Cockpit Arrangement ~ IBFI (Typical) Block 10 INSTRUMENT PANEL L;]~~ • t:] ~ ~ c c~~~~~~~c=~~ OO~ 2 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. 26. 27. 28. 29. 30. HUD Combiner Glass Television Sensor AR Status/NWS Indicator HUD Control Panel Standby Attitude Indicator FUEL FLOW Indicator DUAL FC FAIL Warning Light (Red) HYD/OIL PRESS Warning Light IRed) CANOPY Warning Light (Red) ENGINE Warning Light (Red) Radio Channel/Frequency Indicator Vertical Velocity Indicator OIL Pressure Indicator RPM Indicator NOZ pas Indicator FTIT Indicator FUEL Quantity Indicator Altimeter 31. MRK BCN Light 32. Attitude Director Indicator 33. Horizontal Situation Indicator 34. Radar/EO Display Rudder PEDAL ADJ Knob 35. AOA Indicator 36. INSTR MODE Select Panel 37. Airspeed/Mach Indicator 38. Stores Control Panel 39. Autopilot ROLL Switch 40. Autopilot PITCH Switch 41. AUTOPILOT Switch 42. MASTER ARM Switch [A] ALT REL Button SMS PWR Switch [QID ~ mJ IFF IDENT Button; ~ [NQ] Drag Chute Switch TO/LDG CONFIG Warning Light (Red) ALT LOW and ENG FIRE Warning Lights (Red) THREAT WARNING Controls and Indicators MASTER CAUTION Light (Amber) THREAT WARNING Azimuth Indicator Spotlight AOA Indexer ~ OVRD Light 42 28 1 F-16A-l-l 010X® Figure 1-3. (Sheet 4) 1-15
  41. 41. 10. 1 F- 16A- 1 Cockpit Arrangement [AJ IBFI (Typical) Block 10 RIGHT CONSOLE 20 16 7 6 ~ 8 13 12 9 11 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. ILS Control Panel NUCLEAR CONSENT Switch (Guarded) VHF Radio Control Panel RDR ALT Switch Interior LIGHTING Control Panel ECS Control Panel Secure Voice Panel ENGINE ANTI ICE Switch ANT SEL Panel Utility Light OXYGEN REGULATOR Panel Data Transfer Unit CHAFF/FLARE Control Panel Stowage Oxygen/Communications Hookup EXT LIGHTING Control Panel VOICE MESSAGE Switch, MASTER ZEROIZE Switch Stick ~ TAKE CONTR Panel rn::EJ NWS Control Button/ Indicator (Green) LOCATED ON SHELF 22. Chaff/Flare Programmer BEHIND SEAT. 23. SEAT ADJ Switch 1F-1SA-1-1011X@ Figure 1-3. (Sheet 5) 1-16
  42. 42. T. O. 1F- 16A- 1 Cockpit A~ IBRI (T~. rangement .,plcal) Block 1.0 INSTRUMENT PANEL "'" RIGHT CONSOLE 1 F-16A-1-1 012X@ Figure 1-3• l eet 6) /Sh 1-17
  43. 43. 10. 1F-16A- 1 Cockpit Arrangement IBRI (Typical) Block 10 LEFT CONSOLE -TAKECONTfU..- t--r===~---irnJl ~ ~ ~9~~BOB : 'U' 1 ~'I'C ~11'C~11'C(ifff j CF F PWR I LS ~® [@f@ ® VOL 11 d:J 12 7 13 6 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 5 RADIO SEL Panel ILS Control Panel TACAN Control Panel UHF Radio Control Panel G-Suit Hose Connection ANTI G TEST Button MAL & IND LTS Test Button CANOPY JEniSON T-Handle ENG CONT Switch MANUAL PITCH Override Switch Throttle FUEL MASTER Switch Stowage 1 F-16A-1-1013X® Figure 1-3. (Sheet 7) 1-18
  44. 44. T.O. 1F- 16A- 1 Cockpit Arrangement IBRI (Typical) LEFT AUXILIARY CONSOLE Block 10 RIGHT AUXILIARY CONSOLE UP AOC flTaM SYS fWD fUEllilW AIT FUEl lOW CAOC ANTI-$(~ (@) I WOOl I NWSfAll - HYD PRESS A B O'/EIIOT OXYlilW AYI)Ij(S EQUI'HOT Noo.EM 5[AT NOT ARMED RADAR AlT STO<IES [NQNE 'AlA.T @) @ lEFlAPS ElECI't$ 1 CA8IN~SS 5[C COlrflC j EJECTION MODE SEL NORM I SOLO / 1 2 3 rttlrtlJ 15~ I 16 /~ • 1~ --{j!l] lLI 17 5 14 12 OJ I6lITJ I LJo~: 8 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. EMER 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 THREAT WARNING AUX (DIM) Knob THREAT WARNING AUX Controls and Indicators SPEED BRAKE Position Indicator ALT FLAPS Switch (Lever Lockl HORN SILENCER Button GND JETT ENABLE Switch (Lever Lock' LE FLAP POSITION Indicator (Deactivated: [NID [NQJ DRAG CHUTE Switch 5 1. 2. 3. 4. 5. 6. Clock OXY FLOW Indicator System B HYD PRESS Indicator System A HYD PRESS Indicator EJECTION MODE SEL Handle Caution Light Panel 1 F-16A-l-1 0 14X@ Figure 1-3. (Sheet 8) 1-19
  45. 45. T.O. 1F·16A·l Cockpit Arrangement IBRI (Typical) Block 10 INSTRUMENT PANEL 1. MASTER CAUTION Light (Amber) 2. AR Status/NWS Indicator 3. Radar/EO Display 4. DUAL FC FAIL Warning Light (Red) 6. HYD/OIL PRESS Warning Light (Red) 6. CANOPY Warning Light (Red) 7. ENGINE Warning Light (Redl 8. Standby Attitude Indicator 9. FUEL FLOW Indicator 10. Vertical Velocity Indicator 11. Radio Channel/Frequency Indicator 12. RPM Indicator 13. OIL Pressure Indicator 14. NOZ POS Indicator 15. FUEL Quantity Indicator 16. FTIT Indicator 17. Altimeter 18. MRK BeN Light 19. Attitude Director Indicator 20. Horizontal Situation Indicator 21. AOA Indicator 22. INSTR MODE Select Panel 23. Rudder PEDAL ADJ Knob 24. Airspeed/Mach Indicator 25. Reduced Idle Thrust Indicator 26. Stores Control Panel 27. IFF IDENT Button 28. ARMT CONSENT Switch (Guarded) 29. Accelerometer 30. 31. 32. 33. 34. 35. 36. 37. 38. 39. Stick Indicator OVRD Light VIDEO SEL Switch THREAT WARNING Controls & Indicators THREAT WARNING Azimuth Indicator Spotlight TO/LOG CONFIG Warning Light (Red) ALT LOW and ENG FIRE Warning Light (Red) AOA Indexer Handgrip , F-' 6A-' -1 01 5X ~ Figure 1-3. (Sheet 9) , .20
  46. 46. T. o. 1F- 16A-1 Cockpit Arrangement BRI (Typical) Block 10 RIGHT CONSOLE SUIT PRESS @ (n --PRlMARY-lHD.ES O~ 9 7 m PNl O~ fREQ DISP O~ 6 1. 2. 3. 4. 6. 6. 7. 8. 9. SUIT PRESS Switch (Nonfunctional) Interior LIGHTING Control Panel OXYGEN REGULATOR Panel Utility Light Oxygen/Communications Hookup Stowage NWS Control Button/lndicator (Green) Stick SEAT ADJ Switch 1F-16A-1-1016xe Figuree 1-3. (Sheet 10) 1-21
  47. 47. T. O. 1F- 16A- 1 Cockpit Arrangement~~ [AJ ~ (Typical) FOR DETAILS OF OXYGEN REGULATOR PANEL OR IpW200i ENGINE DIFFERENCES, SEE THE INDIVIDUAL EQUIPMENT ILLUSTRATION. INSTRUMENT PANEL RIGHT AUXILIARY CONSOLE LEFT AUXILIARY CONSOLE RIGHT - - - - . 4 CONSOLE LEFT CONSOLE LOCATED ON SHELF BEHIND SEAT, Figuree 1-3. (Sheet 11) 1-22 Change 1 1F-1SA-1-10"xe
  48. 48. T. O. 1F- 16A- 1 Cockpit Arrangement [AJIBFI (Typical) Block 15 LEFT CONSOLE 14 15 ---+l"i-+! 11 24 9 8 25 1. 2. 3. 4. 6. 6. 7. 8. 9. 10. 11. 12. 13. 14. 16. 16. 17. 18. 19. 20. 21. 22. 23. 24. 26. RADAR Control Panel UHF Radio Control Panel FC/NAV Panel TACAN Control Panel MANUAL TRIM Panel AVTR Control Panel ECM Pod Control Panel G-Suit Hose Connection ANTI G TEST Button TEST Switch Panel DEFOG Lever FLIGHT CONTROL Panel Fuel Control Panel CANOPY JETTISON T-Handle COMM Control Panel EPU Control Panel ELEC Control Panel Throttle FRICTION Control ENG & JET START Control Panel MANUAL PITCH Override Switch CHAFF/FLARE Dispense Button Throttle REDUCED IDLE THRUST Switch Stowage (If] STICK CONTROL Switch IFF ~ 1F-18A-1-101aX<il Figure 1-3. (Sheet 12) Change 1 1-23
  49. 49. T.O. 1F-16A-1 Cockpit Arrangement LEFT AUXILIARY CONSOLE 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 00 IBF I (Typical) Block 15 RIGHT AUXILIARY CONSOLE EMER STORES JETTISON Button (Covered) WHEELS Down lights (Green) HOOK Switch (lever lock) ANTI-SKID Switch LANDING TAXI Lights Switch ON lOCK REl Button lG Handle Down Permission Button lG Handle Warning Light (Red) lG Handle IFF Control Panel THREAT WARNING AUX (DIM) Knob THREAT WARNING AUX Controls and Indicators AlT GEAR Reset Button AlT GEAR Handle SPEED BRAKE Position Indicator STORES CON FIG Switch HORN SilENCER Button GND JETT ENABLE Switch (lever lock) BRAKES Channel Switch 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. Magnetic Compass Clock OXY FLOW Indicator System A HYD PRESS Indicator System B HYD PRESS Indicator EPU FUEL Quantity Indicator Cockpit Pressure Altimeter LIQUID OXYGEN Quantity Indicator Caution light Panel FUEL QTY SEl Knob EXT FUEL TRANS Switch 1F-18A-1-1019X. Figure 1-3. (Sheet 13) 1-24
  50. 50. T.O. 1F-16A- 1 Cockpit Arrangement [AJ IBF I (Typical) Block 15 INSTRUMENT PANEL L;](@[@] IfflOENT co LJ!ERNI/ 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. 26. 27. 28. 29. HUD Combiner Glass Television Sensor AR Status/NWS Indicator HUD Control Panel Standby Attitude Indicator 36 FUEL FLOW Indicator 32 DUAL FC FAIL Warning Light (Red) 31 I HYD/OIL PRESS Warning Light (Red) CANOPY Warning Light (Red) 29~_ RDR ALT LOW Warning Light (Red) ENGINE Warning Light (Red) Radio Channel/Frequency Indicator Vertical Velocity Indicator 26 OIL Pressure Indicator RPM Indicator 30. [8J ALT REL Button NOZ POS Indicator 31. LASER ARM Switch FTIT Indicator 32. ~~~ IFF IDENT Button; MJ~ DRAG CHUTE Switch FUEL Quantity Indicator AOA Indicator 33. Stores Control Panel INSTR MODE Select Panel 34. Threat Warning Azimuth Indicator Airspeed/Mach Indicator 35. THREAT WARNING Controls and Indicators 36. ENG FIRE Warning Light (Red) Attitude Director Indicator Horizontal Situation Indicator 37. T.O./LAND CON FIG Warning Light (Red) 38. MASTER CAUTION Light (Amber) Altimeter Radar/EO Display 39. Spotlight 40. AOA Indexer Autopilot PITCH Switch Autopilot ROLL Switch 41. MRK BCN Light 42. Rudder PEDAL ADJ Knob AUTOPILOT Switch MASTER ARM Switch 43. ~ OVRD Light 1 27~J." 33 ~,30 28 1F-16A-1-1020X® Figure 1-3. (Sheet 14) 1-25
  51. 51. T. O. 1F- 16A- 1 Cockpit Arrangement [8J IBF I (Typical) Block 15 RIGHT CONSOLE 4 24 6 17 18 7 16 ~ 25~ 13 8 10 12 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. ILS Control Panel VHF Radio Control Panel NUCLEAR CONSENT Switch (Guarded) SUIT PRESS Switch (Nonfunctional) Interior LIGHTING Control Panel SNSR PWR Control Panel ECS Control Panel ENGINE ANTI ICE Switch Utility Light ANT SEL Panel OXYGEN REGULATOR Panel Data Transfer Unit CHAFF/FLARE Control Panel Stowage Oxygen/Communications Hookup AVIONICS POWER Panel EXT LIGHTING Control Panel Secure Voice Control Panel VOICE MESSAGE Switch MASTER ZEROIZE Switch Stick [AJ Chaff/Flare Programmer SEAT ADJ Switch ~ VHF Control Button/ Indicator 25. ~ TAKE CONTR Panel 26. [[8 NWS Control Button/Indicator (Green) LOCATED ON SHELF BEHIND SEAT. 1I~e:::........:~.-=...J 1F-1SA-1-1021X@ Figure 1-3. (Sheet 15) 1-26
  52. 52. T. O. 1F- 16A- 1 Cockpit Arrangement IBRI (Typical) Block 15 . . . - - LEFT AUXILIARY CONSOLE RIGHT - - . - I AUXILIARY I-~~~:;-l CONSOLE ~~,[~~tQ"f"W'Ul,.1 "0 '. STICK LEFT CONSOLE RIGHT CONSOLE FOR DETAILS OF OXYGEN REGULATOR PANEL OR IpW2001 ENGINE DIFFERENCES, SEE THE INDIVIDUAL EQUIPMENT ILLUSTRATION. 1F-16A-1-1022X@ Figure 1-3. (Sheet 16) 1-27
  53. 53. T.O. 1 F- 16A-l Cockpit Arrangement IBRI (Typical) Block 15 LEFT CONSOLE m - - TAKE CD'JTROL-VHF TACAN ILS OOD MS, OC OfT PWR ® ,~'ERCOM THREAT O~O~ID I LS VOl ® [108.IOJ CHAN~[l (~l ~Q~ ~~ eM r . 1 AlAT/R ID CHAN I , I ® '/~A/AR[C orf U 0 11 U 11 2 3 12 4 s-H 7 13 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. RADIO SEL Panel ILS Control Panel TACAN Control Panel UHF Radio Control Panel G-Suit Hose Connection ANTI G TEST Button MAL & IND LTS Test Button CANOPY JETTISON T-Handle ENG CONT Switch MANUAL PITCH Override Switch Throttle FUEL MASTER Switch Stowage <ZI-- C!l 1F-16A-1-1023X@ Figure 1-3. (Sheet 17) 1-28
  54. 54. T.O. 1F- 16A- 1 Cockpit Arrangement LEFT AUXILIARY CONSOLE 9EMERSTGRES JETTISOli IBRI (Typical) Block 15 RIGHT AUXILIARY CONSOLE ~ ~P e 0 U ~ ~En° ~ . L UP S GNO JETT ENABLE ~ Off FLT CONT SYS ADC FWD FUEL LOW AFT fUEL LOW LE fLAPS OVERHEAT CAOC ENelNE fAULT ELEC SYS SEC fUEL HOT SEAT NOT ARWEO AVIONICS ATf NOT ENGAGED RAOAR ALT EQUIP HOT ANTI SKID OXY FLOW HOOK Iff NWS fAIL CABIN PRESS OXY LOW ECM NUCLEAR STORES CONFIG PROBE HEAT ~ (@) ~ - HYD PRESS A B @ @ EJECTION MODE SEL NORM i SOLO / 1 2 3 rt-};ill 15~JII 4 II ~. 16 14-r, f- II ~o1B 5 6 7 8 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. EMER STORES JETTISON Button (Covered) WHEELS Down Lights (Green) HOOK Switch (Lever Lock) DN LOCK REL Button LG Handle Down Permission Button LG Handle LG Handle Warning Light (Red) ALT GEAR Handle ALT GEAR Reset Button THREAT WARNING AUX (DIM) Knob THREAT WARNING AUX Controls and Indicators SPEED BRAKE Position Indicator HORN SILENCER Button ALT FLAPS Switch (Lever Lock) GND JETT ENABLE Switch (Lever Lock) ~ DRAG CHUTE Switch M 1. 2. 3. 4. 5. 6. 7. Clock FUEL Quantity Indicator OXY FLOW Indicator System B HYD PRESS Indicator System A HYD PRESS Indicator EJECTION MODE SEL Handle Caution Light Panel 1 F-16A-1-1 024X@ Figure 1-3. (Sheet 18) 1-29
  55. 55. 10. 1 F-16A-l Cockpit Arrangement IBRI (Typical) Block 15 INSTRUMENT PANEL 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. 26. 27. 28. 29. 30. 31. 32. MASTER CAUTION Light (Amber) AR Status/NWS Indicator Radar/EO Display DUAL FC FAIL Warning Light (Red) HYD/OIL PRESS Warning Light (Red) CANOPY Warning Light (Red) RDR ALT LOW Warning Light (Red) Standby Attitude Indicator ENGINE Warning Light (Red) FUEL FLOW Indicator OIL Pressure Indicator MRK BCN Light NOZ POS Indicator FTIT Indicator RPM Indicator AOA Indicator Vertical Velocity Indicator Attitude Director Indicator Horizontal Situation Indicator Altimeter Airspeed/Mach Indicator Accelerometer Radio Channel/Frequency Indicator INSTR MODE Select Panel ARMT CONSENT Switch (Guarded) IFF IDENT Button Reduced Idle Thrust Indicator Stick Indicator OVRD Light THREAT WARNING Controls & Indicators Threat Warning Azimuth Indicator Stores Control Panel 33. 34. 35. 36. 37. 38. 39. Spotlight VIDEO SEL Switch ENG FIRE Warning Light (Red) T.O.ILAND CONFIG Warning light (Red) ADA Indexer Rudder PEDAL ADJ Knob Handgrip 1F-16A-1-1025X® Figure 1-3. (Sheet 19) 1-30
  56. 56. 10. 1F-16A- 1 Cockpit Arrangement IBRI (Typical) Block 15 RIGHT CONSOLE 9 3 8 : - - PRIMARY - - ~ cnro.ES INST PNL : FREQ DISP I~ O~ ~~ O~ ~ ! G H T -FLOOD - Q ~~ ~ r® @ tJAL& '~ (Jffl}llllT ® CD ICD I I ~D~ 6 ~rE MrD Sw . 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. SUIT PRESS Switch (Nonfunctional) VHF Radio Control Panel Interior LIGHTING Control Panel DSPL POWER Switch OXYGEN REGULATOR Panel Utility Light Oxygen/Communications Hookup Stowage NWS Control Button/Indicator (Green) Stick SEAT ADJ Switch B Cff OXYC£N REGULATOR 0 flOW ["['B NCO" ~ ~ • . .llIml~lllllmlmIIMIII 1F-16A-1-1026X® Figure 1-3. (Sheet 20) 1-31

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