AC 150/5300-13

Antonov AN-10 C-IV 126 38.0 37.0 9.8 55,111 Antonov AN-12 C-IV 127 38.0 33.2 10.5 55,111 Antonov AN-124 C-VI 124 70.7 68.0 20.2 362,874 Antonov AN-14 A-II 52 22.0 11.3 4.6 3,450 Antonov AN-22 C-V 140 * 64.3 50.9 12.6 226,796 Antonov AN-24 B-III 119 29.2 23.5 8.3 21,004 Antonov AN-26 C-III 121 29.2 23.8 8.6 24,004 Antonov AN-28 A-II 88 22.0 13.0 4.9 5,602 Antonov AN-30 B-III 112 29.4 24.4 8.3 23,151 Antonov AN-72 A-III 89 * 25.8 25.8 8.2 29,937 AW.650 Argosy 220 C-III 123 35.1 26.5 8.2 42,184 AW.660 Argosy C.Mk.1 B-III 113 35.1 27.2 8.2 43,998 BAC 111-200 C-III 129 27.0 28.5 7.5 35,834 BAC 111-300 C-III 128 27.0 28.5 7.5 40,143 BAC 111-400 C-III 137 27.0 28.5 7.5 39,463 BAC 111-475 C-III 135 28.5 28.5 7.5 44,679 BAC 111-500 D-III 144 28.5 32.6 7.5 47,400 BAC/Aerospatiale Concord D-III 162 25.5 62.6 11.4 185,066 BAe 146-100 B-III 113 26.3 26.2 8.6 33,838 BAe 146-200 B-III 117 26.3 28.6 8.6 40,030 BAe 146-300 C-III 121 26.3 31.8 8.6 47,174 BAe Jetstream 31 B-II 99 15.8 14.4 5.3 6,600 Beech Airliner 1900-C B-II 120 * 16.6 17.6 4.5 7,530 Beech Airliner C99 B-I 107 14.0 13.6 4.4 5,126 Beech Baron 58 B-I 96 11.5 9.1 3.0 2,495 Beech Baron 58P B-I 101 11.5 9.1 2.8 2,812 Beech Baron 58TC B-I 101 11.5 9.1 2.8 2,812 Beech Baron B55 A-I 90 11.5 8.5 2.8 2,313 Beech Baron E55 A-I 88 11.5 8.8 2.8 2,404 Beech Bonanza A36 A-I 72 10.2 8.4 2.6 1,656 Beech Bonanza B36TC A-I 75 11.5 8.4 2.6 1,746 Beech Bonanza F33A A-I 70 10.2 8.1 2.5 1,542 Beech Bonanza V35B A-I 70 10.2 8.0 2.0 1,542 Beech Duchess 76 A-I 76 11.6 8.8 2.9 1,769 Beech Duke B60 B-I 98 11.9 10.3 3.7 3,073 AC 150/5300-13 CHG 6 9/30/00 Appendix 13 258 Aircraft Airport Reference Code Appch Speed Knots Wingspan Meters Length Meters Tail Height Meters Maximum Takeoff Kg Beech E18S A-II 87 15.1 10.7 2.9 4,218 Beech King Air B100 B-I 111 14.0 12.2 4.7 5,352 Beech King Air C90-1 B-II 100 15.3 10.8 4.3 4,377 Beech King Air F90 B-I 108 14.0 12.1 4.6 4,967 Beech Sierra 200-B24R A-I 70 10.0 7.8 2.5 1,247 Beech Skipper 77 A-I 63 9.1 7.3 2.1 760 Beech Sundowner 180-C23 A-I 68 10.0 7.8 2.5 1,111 Beech Super King Air B200 B-II 103 16.6 13.4 4.6 5,670 BN-2A Mk.3 Trislander A-II 65 16.2 13.9 4.3 4,536 Boeing 707-100 C-IV 139 39.9 44.2 12.7 116,727 Boeing 707-200 D-IV 145 39.9 44.2 12.7 116,727 Boeing 707-320 C-IV 139 43.4 46.6 12.9 141,521 Boeing 707-320B C-IV 136 44.4 46.6 12.8 152,679 Boeing 707-420 C-IV 132 43.4 46.6 12.9 141,521 Boeing 720 C-IV 133 39.9 41.5 12.6 104,009 Boeing 720B C-IV 137 39.9 41.7 12.6 106,277 Boeing 727-100 C-III 125 32.9 40.6 10.5 76,657 Boeing 727-200 C-III 138 32.9 46.7 10.6 95,028 Boeing 737-100 C-III 137 28.3 28.7 11.3 49,895 Boeing 737-200 C-III 137 28.3 30.5 11.4 52,390 Boeing 737-300 C-III 137 28.9 33.4 11.2 61,235 Boeing 737-400 C-III 139 28.9 36.5 11.2 68,039 Boeing 737-500 C-III 140 * 28.9 31.0 11.2 60,555 Boeing 747-100 D-V 152 59.6 70.7 19.6 272,155 Boeing 747-200 D-V 152 59.6 70.7 19.7 377,842 Boeing 747-300SR D-V 141 59.6 70.7 19.6 272,155 Boeing 747-400 D-V 154 64.9 70.7 19.6 394,625 Boeing 747-SP C-V 140 59.6 56.3 20.1 315,700 Boeing 757 C-IV 135 38.0 47.3 13.7 115,666 Boeing 767-200 C-IV 130 47.6 48.5 16.1 142,882 Boeing 767-300 C-IV 130 47.6 55.0 16.0 158,757 Boeing 777-200 D-V 145 60.9 63.7 18.8 286,900 Boeing 777-300 D-V 145 60.9 73.9 18.8 299,370 Boeing B-52 D-V 141 * 56.4 48.0 12.4 221,353 Boeing C97 Stratocruiser B-IV 105 43.1 33.6 11.7 66,134 Boeing E-3 C-IV 137 44.5 46.6 12.8 147,418 Boeing E-4 (747-200) D-V 152 59.6 70.7 19.7 377,842 Boeing YC-14 A-IV 89 39.3 40.1 14.7 97,976 Bristol Brittania 300/310 B-IV 117 43.4 37.9 11.4 83,915 Canadair CL-44 C-IV 123 43.4 41.7 11.7 95,254 Canadair CL-600 C-II 125 18.8 20.8 6.3 18,711 Casa C-207A Azor B-III 102 27.8 20.8 7.7 16,511 Casa C-212-200 Aviocar A-II 81 19.0 15.2 6.3 7,700 Cessna Citation I B-I 108 14.4 13.3 4.4 5,375 Cessna Citation II B-II 108 15.8 14.4 4.6 6,033 Cessna Citation III B-II 114 16.3 16.9 5.1 9,979 Cessna-150 A-I 55 10.0 7.3 2.4 726 Cessna-177 Cardinal A-I 64 10.8 8.3 2.6 1,134 Cessna-402 Businessliner B-I 95 12.1 11.0 3.5 2,858 Cessna-404 Titan B-I 92 14.1 12.0 4.0 3,810 Cessna-414 Chancellor B-I 94 13.4 11.1 3.5 3,078 Cessna-421 Golden Eagle B-I 96 12.7 11.0 3.5 3,379 9/30/00 AC 150/5300-13 CHG 6 Appendix 13 267 Aircraft Airport Reference Code Appch Speed Knots Wingspan Feet Length Feet Tail Height Feet Maximum Takeoff Lbs HS.121 Trident Super 3B D-III 146 98.0 131.2 28.3 158,000 Tupolev TU-134 D-III 144 95.2 121.5 30.0 103,600 Tupolev TU-144 E-III 178 94.8 212.6 42.2 396,000 Boeing YC-14 A-IV 89 129.0 131.7 48.3 216,000 Lockheed 1649 Constellat’n A-IV 89 150.0 116.2 23.4 160,000 Boeing C97 Stratocruiser B-IV 105 141.3 110.3 38.3 145,800 Bristol Brittania 300/310 B-IV 117 142.3 124.2 37.5 185,000 Ilyushin Il-18 B-IV 103 122.7 117.8 33.3 134,640 Ilyushin Il-76 B-IV 119 165.7 152.8 48.4 374,785 Lockheed 1049 Constellat’n B-IV 113 123.0 113.6 24.8 137,500 Lockheed 749 Constellat’n B-IV 93 123.0 95.2 22.4 107,000 MDC-DC-7 B-IV 110 127.5 112.3 31.7 143,000 Vickers Vanguard 950 B-IV 119 118.0 122.9 34.9 146,500 Aerospatiale C 160 Trans. C-IV 124 131.3 106.3 38.7 108,596 Airbus A-300-600 C-IV 135 147.1 177.5 54.7 363,763 Airbus A-300-B4 C-IV 132 147.1 175.5 55.5 330,700 Airbus A-310-300 C-IV 125 144.1 153.2 52.3 330,693 Antonov AN-10 C-IV 126 124.8 121.4 32.2 121,500 Antonov AN-12 C-IV 127 124.8 109.0 34.6 121,500 Boeing 707-100 C-IV 139 130.8 145.1 41.7 257,340 Boeing 707-320 C-IV 139 142.4 152.9 42.2 312,000 Boeing 707-320B C-IV 136 145.8 152.9 42.1 336,600 Boeing 707-420 C-IV 132 142.4 152.9 42.2 312,000 Boeing 720 C-IV 133 130.8 136.2 41.4 229,300 Boeing 720B C-IV 137 130.8 136.8 41.2 234,300 Boeing 757 C-IV 135 124.8 155.3 45.1 255,000 Boeing 767-200 C-IV 130 156.1 159.2 52.9 315,000 Boeing 767-300 C-IV 130 156.1 180.3 52.6 350,000 Boeing E-3 C-IV 137 145.9 153.0 42.0 325,000 Canadair CL-44 C-IV 123 142.3 136.8 38.4 210,000 Dassault 1150 Atlantic C-IV 130 * 122.7 104.2 37.2 100,000 Lockheed 100-20 Hercules C-IV 137 132.6 106.1 39.3 155,000 Lockheed 100-30 Hercules C-IV 129 132.6 112.7 39.2 155,000 Lockheed 1011-1 C-IV 138 155.3 177.7 55.8 430,000 Lockheed 1011-100 C-IV 140 155.3 177.7 55.8 466,000 Lockheed 1011-200 C-IV 140 155.3 177.7 55.8 466,000 Lockheed 1011-600 C-IV 140 * 142.8 141.0 53.0 264,000 Lockheed 400 C-IV 121 * 119.7 97.8 38.1 84,000 Lockheed C-141A Starlifter C-IV 129 159.9 145.0 39.3 316,600 Lockheed C-141B Starlifter C-IV 129 159.9 168.3 39.3 343,000 Marshall (Shorts) Belfast C-IV 126 158.8 136.4 47.0 230,000 MDC-DC-10-10 C-IV 136 155.3 182.3 58.4 443,000 MDC-DC-8-10 C-IV 131 142.4 150.8 43.3 276,000 MDC-DC-8-20/30/40 C-IV 133 142.4 150.8 43.3 315,000 MDC-DC-8-50 C-IV 137 142.4 150.8 43.3 325,000 MDC-DC-8-62 C-IV 124 148.4 157.5 43.4 350,000 Tupolev TU-114 C-IV 132 * 167.6 177.5 50.0 361,620 Vickers VC-10-1100 C-IV 128 146.2 158.7 39.5 312,000 Vickers VC-10-1150 C-IV 138 146.2 171.7 39.5 335,100 Boeing 707-200 D-IV 145 130.8 145.1 41.7 257,340 AC 150/5300-13 CHG 6 9/30/00 Appendix 13 268 Aircraft Airport Reference Code Appch Speed Knots Wingspan Feet Length Feet Tail Height Feet Maximum Takeoff Lbs General Dynamics 880 D-IV 155 120.0 129.3 36.0 193,500 General Dynamics 990 D-IV 156 120.0 139.2 39.5 255,000 Ilyushin Il-62 D-IV 152 141.8 174.3 40.5 363,760 Ilyushin Il-86 D-IV 141 157.7 195.3 51.8 454,150 Lockheed 1011-250 D-IV 144 155.3 177.7 55.8 496,000 Lockheed 1011-500 D-IV 144 155.3 164.2 55.8 496,000 Lockheed 1011-500 Ex. Wing D-IV 148 164.3 164.2 55.8 496,000 MDC-DC-10-30 D-IV 151 165.3 181.6 58.6 590,000 MDC-DC-10-40 D-IV 145 165.4 182.3 58.6 555,000 MDC-DC-8-61 D-IV 142 142.4 187.4 43.0 325,000 MDC-DC-8-63 D-IV 147 148.4 187.4 43.0 355,000 MDC-MD-11 D-IV 155 169.8 201.3 57.8 602,500 Rockwell B-1 D-IV 165 * 137.0 147.0 34.0 477,000 Tupolev TU-154 D-IV 145 123.3 157.2 37.4 216,050 Antonov AN-22 C-V 140 * 211.0 167.0 41.2 500,000 Boeing 747-SP C-V 140 195.7 184.8 65.8 696,000 MDC-C-133 C-V 128 179.7 157.5 48.2 300,000 Boeing 747-100 D-V 152 195.7 231.8 64.3 600,000 Boeing 747-200 D-V 152 195.7 231.8 64.7 833,000 Boeing 747-300SR D-V 141 195.7 231.8 64.3 600,000 Boeing 747-400 D-V 154 213.0 231.8 64.3 870,000 Boeing 777-200 D-V 145 199.9 209.1 18.8 286,900 Boeing 777-300 D-V 145 199.9 242.3 18.8 299,370 Boeing B-52 D-V 141 * 185.0 157.6 40.8 488,000 Boeing E-4 (747-200) D-V 152 195.7 231.8 64.7 833,000 Antonov AN-124 C-VI 124 232.0 223.0 66.2 800,000 Lockheed C-5B Galaxy C-VI 135 222.7 247.8 65.1 837,000 * Approach speeds estimated. 9/30/00 AC 150/5300-13 CHG 6 Appendix 13 273 Aircraft Airport Reference Code Appch Speed Knots Wingspan Meters Length Meters Tail Height Meters Maximum Takeoff Kg HS.121 Trident Super 3B D-III 146 29.9 40.0 8.6 71,668 Tupolev TU-134 D-III 144 29.0 37.0 9.1 46,992 Tupolev TU-144 E-III 178 28.9 64.8 12.9 179,623 Boeing YC-14 A-IV 89 39.3 40.1 14.7 97,976 Lockheed 1649 Constellat'n A-IV 89 45.7 35.4 7.1 72,575 Boeing C97 Stratocruiser B-IV 105 43.1 33.6 11.7 66,134 Bristol Brittania 300/310 B-IV 117 43.4 37.9 11.4 83,915 Ilyushin Il-18 B-IV 103 37.4 35.9 10.1 61,072 Ilyushin Il-76 B-IV 119 50.5 46.6 14.8 170,000 Lockheed 1049 Constellat'n B-IV 113 37.5 34.6 7.6 62,369 Lockheed 749 Constellat'n B-IV 93 37.5 29.0 6.8 48,534 MDC-DC-7 B-IV 110 38.9 34.2 9.7 64,864 Vickers Vanguard 950 B-IV 119 36.0 37.5 10.6 66,451 Aerospatiale C 160 Trans. C-IV 124 40.0 32.4 11.8 49,258 Airbus A-300-600 C-IV 135 44.8 54.1 16.7 165,000 Airbus A-300-B4 C-IV 132 44.8 53.5 16.9 150,003 Airbus A-310-300 C-IV 125 43.9 46.7 15.9 150,000 Antonov AN-10 C-IV 126 38.0 37.0 9.8 55,111 Antonov AN-12 C-IV 127 38.0 33.2 10.5 55,111 Boeing 707-100 C-IV 139 39.9 44.2 12.7 116,727 Boeing 707-320 C-IV 139 43.4 46.6 12.9 141,521 Boeing 707-320B C-IV 136 44.4 46.6 12.8 152,679 Boeing 707-420 C-IV 132 43.4 46.6 12.9 141,521 Boeing 720 C-IV 133 39.9 41.5 12.6 104,009 Boeing 720B C-IV 137 39.9 41.7 12.6 106,277 Boeing 757 C-IV 135 38.0 47.3 13.7 115,666 Boeing 767-200 C-IV 130 47.6 48.5 16.1 142,882 Boeing 767-300 C-IV 130 47.6 55.0 16.0 158,757 Boeing E-3 C-IV 137 44.5 46.6 12.8 147,418 Canadair CL-44 C-IV 123 43.4 41.7 11.7 95,254 Dassault 1150 Atlantic C-IV 130 * 37.4 31.8 11.3 45,359 Lockheed 100-20 Hercules C-IV 137 40.4 32.3 12.0 70,307 Lockheed 100-30 Hercules C-IV 129 40.4 34.4 11.9 70,307 Lockheed 1011-1 C-IV 138 47.3 54.2 17.0 195,045 Lockheed 1011-100 C-IV 140 47.3 54.2 17.0 211,374 Lockheed 1011-200 C-IV 140 47.3 54.2 17.0 211,374 Lockheed 1011-600 C-IV 140 * 43.5 43.0 16.2 119,748 Lockheed 400 C-IV 121 * 36.5 29.8 11.6 38,102 Lockheed C-141A Starlifter C-IV 129 48.7 44.2 12.0 143,607 Lockheed C-141B Starlifter C-IV 129 48.7 51.3 12.0 155,582 Marshall (Shorts) Belfast C-IV 126 48.4 41.6 14.3 104,326 MDC-DC-10-10 C-IV 136 47.3 55.6 17.8 200,941 MDC-DC-8-10 C-IV 131 43.4 46.0 13.2 125,191 MDC-DC-8-20/30/40 C-IV 133 43.4 46.0 13.2 142,882 MDC-DC-8-50 C-IV 137 43.4 46.0 13.2 147,418 MDC-DC-8-62 C-IV 124 45.2 48.0 13.2 158,757 Tupolev TU-114 C-IV 132 * 51.1 54.1 15.2 164,028 Vickers VC-10-1100 C-IV 128 44.6 48.4 12.0 141,521 Vickers VC-10-1150 C-IV 138 44.6 52.3 12.0 151,999 Boeing 707-200 D-IV 145 39.9 44.2 12.7 116,727 General Dynamics 880 D-IV 155 36.6 39.4 11.0 87,770 General Dynamics 990 D-IV 156 36.6 42.4 12.0 115,666 AC 150/5300-13 CHG 6 9/30/00 Appendix 13 274 Aircraft Airport Reference Code Appch Speed Knots Wingspan Meters Length Meters Tail Height Meters Maximum Takeoff Kg Ilyushin Il-62 D-IV 152 43.2 53.1 12.3 164,999 Ilyushin Il-86 D-IV 141 48.1 59.5 15.8 205,999 Lockheed 1011-250 D-IV 144 47.3 54.2 17.0 224,982 Lockheed 1011-500 D-IV 144 47.3 50.0 17.0 224,982 Lockheed 1011-500 Ex. Wing D-IV 148 50.1 50.0 17.0 224,982 MDC-DC-10-30 D-IV 151 50.4 55.4 17.9 267,619 MDC-DC-10-40 D-IV 145 50.4 55.6 17.9 251,744 MDC-DC-8-61 D-IV 142 43.4 57.1 13.1 147,418 MDC-DC-8-63 D-IV 147 45.2 57.1 13.1 161,025 MDC-MD-11 D-IV 155 51.8 61.4 17.6 273,289 Rockwell B-1 D-IV 165 * 41.8 44.8 10.4 216,364 Tupolev TU-154 D-IV 145 37.6 47.9 11.4 97,999 Antonov AN-22 C-V 140 * 64.3 50.9 12.6 226,796 Boeing 747-SP C-V 140 59.6 56.3 20.1 315,700 MDC-C-133 C-V 128 54.8 48.0 14.7 136,078 Boeing 747-100 D-V 152 59.6 70.7 19.6 272,155 Boeing 747-200 D-V 152 59.6 70.7 19.7 377,842 Boeing 747-300SR D-V 141 59.6 70.7 19.6 272,155 Boeing 747-400 D-V 154 64.9 70.7 19.6 394,625 Boeing 777-200 D-V 145 60.9 63.7 18.8 286,900 Boeing 777-300 D-V 145 60.9 73.9 18.8 299,370 Boeing B-52 D-V 141 * 56.4 48.0 12.4 221,353 Boeing E-4 (747-200) D-V 152 59.6 70.7 19.7 377,842 Antonov AN-124 C-VI 124 70.7 68.0 20.2 362,874 Lockheed C-5B Galaxy C-VI 135 67.9 75.5 19.8 379,657 * Approach speeds estimated. 12/31/2009 AC 150/5300-13 CHG 15 Appendix 14 Appendix 14. Declared Distances 1. APPLICATION. The purpose of declared distances in airport design is to provide an equivalent runway safety area (RSA), runway object free area (ROFA), or runway protection zone (RPZ) in accordance with the design standards in Chapters 2 and 3 at existing constrained airports where it is otherwise impracticable to meet standards by other means. Declared distances are also employed when there are obstructions in the runway approaches and/or departure surface that are beyond the ability of the airport owner to remove and result in a displaced runway threshold or change in the departure end of the runway (DER). a. This appendix, by treating the airplane's runway performance distances independently, provides an alternative airport design methodology by declaring distances to satisfy the airplane's takeoff run, takeoff distance, accelerate-stop distance, and landing distance requirements. The declared distances are takeoff run available (TORA), takeoff distance available (TODA), accelerate-stop distance available (ASDA), and landing distance available (LDA), which when treated independently may include clearway and stopway and may limit runway use. This alternative design methodology may affect the beginning and ending of the RSA, ROFA, RPZ, and primary surface. b. Where declared distances differ, the primary surface extends 200 feet (60 m) beyond each end of the runway or the far end of each TODA, whichever is further, to protect departures to the extent of the 14 CFR Part 77 approach surface for that runway end, i.e. 20:1, 34:1, and 50:1 originating at or beyond the end of TODA. 2. BACKGROUND. In applying declared distances in airport design, it is helpful to understand the relationship between airplane certification, aircraft operating rules, airport data, and airport design. a. Airplane certification provides the airplane's performance distances. The performance speeds, e.g., V1, takeoff decision speed, VLOF, lift-off speed, V2, takeoff safety speed, VSO, stalling speed or the minimum steady flight speed in the landing configuration, and the following distances to achieve or decelerate from these speeds are established by the manufacturer and confirmed during certification testing for varying climatological conditions, operating weights, etc. (1) Takeoff run - the distance to accelerate from brake release to lift-off, plus safety factors. (2) Takeoff distance - the distance to accelerate from brake release past lift-off to start of takeoff climb, plus safety factors. (3) Accelerate-stop distance - the distance to accelerate from brake release to V1 and then decelerate to a stop, plus safety factors. (4) Landing distance - the distance from the threshold to complete the approach, touchdown, and decelerate to a stop, plus safety factors. b. Aircraft operating rules provide a minimum acceptable level of safety by controlling the airplane maximum operating weights by limiting the airplane's performance distances as follows: (1) Takeoff run shall not exceed the length of runway. (2) Takeoff distance shall not exceed the length of runway plus clearway. (3) Accelerate-stop distance shall not exceed the length of runway plus stopway. (4) Landing distance shall not exceed the length of runway. c. Airport data provides the runway length and/or the following declared distance information for calculating maximum operating weights and/or operating capability. (1) Takeoff run available (TORA) - the length of runway declared available and suitable for satisfying takeoff run requirements. (2) Takeoff distance available (TODA) - the TORA plus the length of any remaining runway or clearway beyond the far end of the TORA available for satisfying takeoff distance requirements. The usable TODA length is controlled by obstacles present in the departure area vis-a-vis aircraft performance. As such, the usable TODA length is determined by the aircraft operator before each takeoff and requires knowledge of the location of each controlling obstacle in the departure area. Extending the usable TODA lengths requires the removal of existing objects limiting the usable TODA lengths. (3) Accelerate-stop distance available (ASDA) - the length of runway plus stopway declared available and suitable for satisfying accelerate-stop distance requirements. (4) Landing distance available (LDA) - the length of runway declared available and suitable for satisfying landing distance requirements. 3. FAA APPROVAL FOR APPLYING DECLARED DISTANCES IN AIRPORT DESIGN. The application of declared distances at a specific location requires prior FAA approval on a case-by-case basis. Approval is reflected on the FAA-approved Airport Layout Plan. 275 AC 150/5300-13 CHG 15 12/31/2009 Appendix 14 4. RUNWAY SAFETY AREA (RSA) AND RUNWAY OBJECT FREE AREA (ROFA) LENGTHS. The standard RSA length P in the following paragraphs is the length specified in tables 3-1, 3-2, and 3-3 for the RSA length beyond the runway ends. The standard ROFA length R in the following paragraphs is the length specified in tables 3-1, 3-2, and 3-3 for the ROFA length beyond the runway ends. The RSA and the ROFA shall extend for the full length of the runway plus the greater of the following lengths beyond the runway ends for takeoff and landing in both directions. a. For takeoff. (1) At the start of takeoff end of runway. The RSA and the ROFA need to extend behind the start of takeoff to continue the entrance taxiway safety area and taxiway object free area and/or provide an area for jet blast protection. The portion of runway behind the start of takeoff is unavailable and/or unsuitable for takeoff run, takeoff distance, and accelerate-stop distance computations. (2) At the far end of runway with stopway. The RSA shall extend P and the ROFA shall extend R beyond the far end of stopway. (3) At the far end of runway without stopway. The RSA shall extend P and the ROFA shall extend R beyond the far end of ASDA. The portion of runway beyond the ASDA is unavailable and/or unsuitable for accelerate-stop distance computations. b. For landing. (1) At the approach end of runway. The RSA shall extend P and the ROFA shall extend R before the threshold. The portion of runway behind the threshold is unavailable and/or unsuitable for landing distance computations. (2) At the rollout end of runway. The RSA shall extend P and the ROFA shall extend R beyond the rollout end of LDA. The portion of runway beyond the LOA is unavailable and/or unsuitable for landing distance computations. 5. RUNWAY PROTECTION ZONE (RPZ) LOCATION AND SIZE. The RPZ function may be fulfilled by the RPZ beginning at a location other than 200 feet (60 m) beyond the end of the runway. When an RPZ begins at a location other than 200 feet (60 m) beyond the end of runway, two RPZs are required, i.e, a departure RPZ and an approach RPZ. The two RPZs normally overlap. a. Approach RPZ. The approach RPZ shall begin 200 feet (60 m) before the threshold. Table 2-4 contains standard dimensions for approach RPZs. The portion of runway behind the threshold is unavailable and/or unsuitable for landing distance computations. b. Departure RPZ. The departure RPZ shall begin 200 feet (60 m) beyond the far end of TORA. The portion of runway beyond the TORA is unavailable and/or unsuitable for takeoff run computations. The standard dimensions for departure RPZs are: (1) Starting 200 feet (60 m) beyond the far end of TORA, 1,000 feet (300 m) long, 250 feet (75 m) wide, and at the far end of RPZ 450 feet (135 m) wide—for runways serving only small airplanes in Aircraft Approach Categories A and B. (2) Starting 200 feet (60 m) beyond the far end of TORA, 1,000 feet (300 m) long, 500 feet (150 m) wide, and at the far end of RPZ 700 feet (210 m) wide—for runways serving large airplanes in Aircraft Approach Categories A and B. (3) Starting 200 feet (60 m) beyond the far end of TORA, 1,700 feet (510 m) long, 500 feet (150 m) wide, and at the far end of RPZ 1,010 feet (303 m) wide—for runways serving Aircraft Approach Categories C and D. 6. CLEARWAY LOCATION. The clearway is located at the far end of TORA. The portion of runway extending into the clearway is unavailable and\or unsuitable for takeoff run and takeoff distance computations. 7. NOTIF1CATION. The clearway and stopway lengths, if provided, and declared distances (TORA, TODA, ASDA, and LDA) will be provided by the airport owner for inclusion in the Airport/Facility Directory (and in the Aeronautical Information Publication (AIP), for international airports) for each operational runway direction: a. The TORA - the length of the runway less any length of runway unavailable and/or unsuitable for takeoff run computations. See figure A14-l. b. The TODA - the TORA plus the length of any remaining runway and/or clearway beyond the far end of the TORA. See figure A14-2. c. The ASDA - the length of the runway plus the length of any stopway beyond the far end of the runway less any length of runway and/or stopway unavailable and/or unsuitable for accelerate-stop distance computations. See figure A14-3. d. The LDA - the length of the runway less any length of runway unavailable and/or unsuitable for landing distance computations. See figure A14-4. Note: When the threshold is sited for small airplanes (see appendix 2, paragraphs 5a and 5b), report LDA as “LDA for airplanes of 12,500 pounds (5 700 kg) or less maximum certificated takeoff weight.” 276 1/3/08 AC 150/5300-13 CHG 12 Appendix 16 291 Appendix 16. NEW INSTRUMENT APPROACH PROCEDURES 1. BACKGROUND. This appendix applies to the establishment of new authorized instrument approach procedures. For purposes of this appendix, an Instrument Approach Procedure (IAP) amendment or the establishment of a Global Positioning System (GPS) instrument procedure "overlaying” an existing authorized instrument procedure does not constitute a new procedure. However, a significant reduction in minima (i.e. ¼ mile reduction in visibility and/or 50 foot reduction in decision altitude or minimum descent altitude) would constitute a new procedure. a. This appendix identifies airport landing surface requirements to assist airport sponsors in their evaluation and preparation of the airport landing surface to support new instrument approach procedures. It also lists the airport data provided by the procedure sponsor that the FAA needs to conduct the airport airspace analysis specified in FAA Order 7400.2, Procedures for Handling Airspace Matters. The airport must be acceptable for IFR operations based on an Airport Airspace Analysis (AAA), under FAA Order 7400.2. b. FAA Order 8260, TERPS, reflects the contents of this appendix as the minimum airport landing surface requirements that must be met prior to the establishment of instrument approach procedures at a public use airport. This order also references other FAA requirements, such as a safety analysis to determine the need for approach lighting and other visual enhancements to mitigate the effects of a difficult approach environment. This is a consideration regardless of whether or not a reduction in approach minimums is desired. Airport sponsors are always encouraged to consider an approach lighting system to enhance the safety of an instrument procedure. In the absence of any identified benefits or safety enhancement from an approach light system, sponsors should at least consider installing lower cost visual guidance aids such as REIL or PAPI. c. The tables provided in this appendix are for planning purposes only and should be used in conjunction with the rest of the document. All pertinent requirements within this AC and other FAA documents, as well as local siting conditions, ultimately will determine the lowest minimums obtainable. 2. INTRODUCTION. To be authorized a new instrument approach procedure, the runway must have an instrument runway designation. Instrument runways are runway end specific. The runway end designation is based on the findings of an AAA study (Refer to Order 7400.2). In addition, the instrument runway designation for the desired minimums must be depicted on the FAA-approved ALP. If not depicted, a change to the ALP is required. As part of the ALP approval process, the FAA will conduct an AAA study to determine the runway's acceptability for the desired minimums. 3. ACTION. The airport landing surface must meet the standards specified in tables A16-1 A through C, for each specified runway, direction and have adequate airspace to support the instrument approach procedure. When requesting an instrument procedure, the sponsor must specify the runway direction, the desired approach minimums, whether circling approach procedures are desired, and the survey needed to support the procedure. For all obligated National Plan of Integrated Airport Systems (NPIAS) airports, the sponsor must also provide a copy of the FAA-approved ALP showing the instrument procedure(s) requested. An ALP is also recommended for all other airports. 4. DEFINITIONS. a. Precision Approach. An instrument approach procedure providing course and vertical path guidance conforming to ILS, or MLS, precision system performance standards contained in ICAO annex 10. Table A16-1A defines the requirements for ILS, LAAS, WAAS, MLS, and other precision systems. b. Approach Procedure with Vertical Guidance (APV). An instrument approach procedure providing course and vertical path guidance that does not conform to ILS or MLS system performance standards contained in ICAO annex 10, or a precision approach system that does not meet TERPS alignment criteria. Table A16-1B defines the requirements for WAAS and authorized barometric VNAV. c. Nonprecision Approach. An instrument approach procedure providing course guidance without vertical path guidance. Table A16-1C defines the requirements for VOR, NDB, LDA, GPS (TS0-129) or other authorized RNAV system. 5. AIRPORT AIRSPACE ANALYSIS SURVEYS. a. Use the standards identified in ACs 150/5300-16, 1505300-17, and 150/5300-18 to survey and compile the appropriate data to support the development of instrument procedures. b. When the runway has or is planned to have an approach that has vertical guidance (ILS, MLS or PAR, APV, LPV, RNP, TLS, LNAV/VNAV, etc.), use the Vertically Guided Airport Airspace Analysis Survey criteria in AC 150/5300-18. c. When the runway has or is planned to have an approach without vertical guidance (VOR, VOR/DME, TACAN, NDB, LNAV, LP, etc.), use the Non- Vertically Guided Airport Airspace Analysis Survey criteria in AC 150/5300-18. AC 150/5300-13 CHG 12 1/3/08 Appendix 16 292 Table A16-1A. Precision Instrument Approach Requirements. Visibility Minimums1 <3/4 statute mile < 1-statute mile Height Above Touchdown (HAT)2 200 TERPS Glidepath Qualification Surface (GQS)3 Table A2-1, Row 7, Criteria, and Appendix 2, par. 5a Clear TERPS precision "W" surfaces 4 Clear See Note 5 TERPS Paragraph 251 34:1 Clear 20:1 Clear Precision Obstacle Free Zone (POFZ) 200 x 8006 Required Not Required Airport Layout Plan7 Required Minimum Runway Length 4,200 ft (1,280 m) (Paved) Runway Markings (See AC 150/5340-1) Precision Nonprecision Holding Position Signs & Markings (See AC 150/5340-1 and AC 150/5340-18) Precision Nonprecision Runway Edge Lights8 HIRL / MIRL Parallel Taxiway 9 Required Approach Lights10 MALSR, SSALR, or ALSF Recommended Runway Design Standards; e.g., Obstacle Free Zone (OFZ) 11 < 3/4-statute mile approach visibility minimums ≥ 3/4-statute mile approach visibility minimums Threshold Siting Criteria To Be Met 12 Table A2-1, Row 9, Criteria Table A2-1, Row 8, Criteria Survey Required for Lowest Minima Vertically Guided Airport Airspace Analysis Survey 1. Visibility minimums are subject to application of FAA Order 8260.3 (TERPS) and associated orders or this table, whichever are higher. 2. The HAT indicated is for planning purposes only. Actual obtainable HAT is determined by TERPS. 3. The GQS is applicable to approach procedures providing vertical path guidance. It limits the magnitude of penetration of the obstruction clearance surfaces overlying the final approach course. The intent is to provide a descent path from DA to landing free of obstructions that could destabilize the established glidepath angle. The GQS is centered on a course from the DA point to the runway threshold. Its width is equal to the precision “W” surface at DA, and tapers uniformly to a width 100 feet from the runway edges. If the GQS is penetrated, vertical guidance instrument approach procedures (ILS/MLS/WAAS/LAAS/Baro-VNAV) are not authorized 4. The “W” surface is applicable to precision approach procedures. It is a sloping obstruction clearance surface (OCS) overlying the final approach course centerline. The surface slope varies with glidepath angle. The “W” surface must be clear to achieve lowest precision minimums. Surface slope varies with glide path angle, 102/angle; e.g., for optimum 3º glide path 34:1 surface must be clear. 5. If the W surface is penetrated, HAT and visibility will be increased as required by TERPS. 6. This is a new airport surface (see paragraph 306). 7. An ALP is only required for airports in the NPIAS; it is recommended for all others. 8. Runway edge lighting is required for night minimums. High intensity lights are required for RVR-based minimums. 9. A parallel taxiway must lead to the threshold and, with airplanes on centerline, keep the airplanes outside the OFZ. 10. To achieve lower visibility minimums based on credit for lighting, a TERPS specified approach light system is required. 11. Indicates what chart should be followed in the related chapters of this document. 12. Circling procedures to a secondary runway from the primary approach will not be authorized when the secondary runway does not meet threshold siting (reference Appendix 2), OFZ (reference paragraph 306) criteria, and TERPS Order paragraph 251 criteria. 1/3/08 AC 150/5300-13 CHG 12 Appendix 16 293 Table A16-1B. Approach Procedure With Vertical Guidance (APV-RNP) Approach Requirements Visibility Minimums1 < 3/4-statute mile < 1-statute mile 1-statute mile >1-statute mile14 Height Above Touchdown (HAT)2 250 300 350 400 TERPS Glidepath Qualification Surface (GQS)3 Table A2-1, Row 7, Criteria, and Appendix 2, par. 5a Clear TERPS Paragraph 251 34:1 clear 20:1 clear 20:1 clear, or penetrations lighted for night minimums (See AC 70/7460-1) Precision Obstacle Free Zone (POFZ) 200 x 8004 Required Recommended Airport Layout Plan5 Required Minimum Runway Length 4,200 ft (1,280 m) (Paved) 3,200 ft (975 m)6 (Paved) 3,200 ft (975 m)6,7 Runway Markings (See AC 150/5340-1) Precision Nonprecision (precision recommended) Nonprecision7 Holding Position Signs & Markings (See AC 150/5340-1 and AC 150/5340-18) Precision Nonprecision (precision recommended) Nonprecision7 Runway Edge Lights8 HIRL / MIRL MIRL/LIRL Parallel Taxiway 9 Required Recommended Approach Lights10 Required11 Recommended Runway Design Standards; e.g., Obstacle Free Zone (OFZ) 12 <3/4-statute mile approach visibility minimums ≥ 3/4-statute mile approach visibility minimums Threshold Siting Criteria To Be Met 13 Table A2-1, Row 4 and 9, Criteria Appendix 2, Table A2-1, Lines 4 and 8, Criteria Survey Required for Lowest Minima Vertically Guided Airport Airspace Analysis Survey 1. Visibility minimums are subject to the application of FAA Order 8260.3 (TERPS) and associated orders or this table, whichever is higher. 2. The HAT indicated is for planning purposes only. Actual obtainable HAT is determined by TERPS. 3. The GQS is applicable to approach procedures providing vertical path guidance. It limits the magnitude of penetration of the obstruction clearance surfaces overlying the final approach course. The intent is to provide a descent path from DA to landing free of obstructions that could destabilize the established glidepath angle. The GQS is centered on a course from the DA point to the runway threshold. Its width is equal to the precision “W” surface at DA, and tapers uniformly to a width 100 feet from the runway edges. If the GQS is penetrated, vertical guidance instrument approach procedures (ILS/MLS/WAAS/LAAS/Baro-VNAV) are not authorized 4. This is a new airport surface (see paragraph 306) 5. An ALP is only required for obligated airports in the NPIAS; it is recommended for all others. 6. Runways less than 3,200 feet are protected by 14 CFR Part 77 to a lesser extent (77.23(a)(2) is not applicable for runways less than 3,200 feet). However runways as short as 2400 feet could support an instrument approach provided the lowest HAT is based on clearing any 200-foot obstacle within the final approach segment. 7. Unpaved runways require case-by-case evaluation by regional Flight Standards personnel. 8. Runway edge lighting is required for night minimums. High intensity lights are required for RVR-based minimums. 9. A parallel taxiway must lead to the threshold and, with airplanes on centerline, keep the airplanes outside the OFZ. 10. To achieve lower visibility minimums based on credit for lighting, a TERPS specified approach light system is required. 11. ODALS, MALS, SSALS are acceptable. For LPV based minima approach lights are recommended not required. 12. Indicates what chart should be followed in the related chapters in this document. 13. Circling procedures to a secondary runway from the primary approach will not be authorized when the secondary runway does not meet threshold siting (reference Appendix 2), OFZ (reference paragraph 306) and TERPS paragraph 251 criteria. 14. For circling requirements, see Table 16-1C. AC 150/5300-13 CHG 12 1/3/08 Appendix 16 294 Table A16-1C. Nonprecision Approach Requirements Visibility Minimums1 < 3/4-statute mile < 1-statute mile 1-statute mile >1-statute mile Circling Height Above Touchdown 2 300 340 400 450 Varies TERPS Paragraph 251 34:1 clear 20:1 clear 20:1 clear or penetrations lighted for night minimums (See AC 70/7460-1) Airport Layout Plan3 Required Recommended Minimum Runway Length 4,200 ft (1,280 m) (Paved) 3,200 ft (975 m)4 (Paved) 3,200 ft (975 m)4,5 Runway Markings (See AC 150/5340-1) Precision Nonprecision5 Visual (Basic)5 Holding Position Signs & Markings (See AC 150/5340-1 and AC 150/5340-18) Precision Nonprecision Visual (Basic)5 Runway Edge Lights6 HIRL / MIRL MIRL / LIRL MIRL / LIRL (Required only for night minima) Parallel Taxiway 7 Required Recommended Approach Lights8 MALSR, SSALR, or ALSF Required Required 9 Recommended9 Not Required Runway Design Standards, e.g. Obstacle Free Zone (OFZ)10 <3/4-statute mile approach visibility minimums ≥ 3/4-statute mile approach visibility minimums Not Required Threshold Siting Criteria To Be Met 11 Table A2-1, Row 9, Criteria Table A2-1, Row 8, Criteria Table A2-1, Row 1–5, Criteria Table A2-1, Row 1–2, Criteria Survey Required for Lowest Minima Vertically Guided Airport Airspace Analysis Survey Non-Vertically Guided Airport Airspace Analysis Survey Non-Vertically Guided Airport Airspace Analysis Survey Non-Vertically Guided Airport Airspace Analysis Survey 1. Visibility minimums are subject to the application of FAA Order 8260.3 (TERPS) and associated orders or this table, whichever is higher. 2. The Height Above Touchdown (HAT) indicated is for planning purposes only. Actual obtainable HAT is determined by TERPS. 3. An ALP is only required for obligated airports in the NPIAS; it is recommended for all others. 4. Runways less than 3,200 feet are protected by 14 CFR Part 77 to a lesser extent. However runways as short as 2400 feet could support an instrument approach provided the lowest HAT is based on clearing any 200-foot obstacle within the final approach segment. 5. Unpaved runways require case-by-case evaluation by regional Flight Standards personnel. 6. Runway edge lighting is required for night minimums. High intensity lights are required for RVR-based minimums. 7. A parallel taxiway must lead to the threshold and, with airplanes on centerline, keep the airplanes outside the OFZ. 8. To achieve lower visibility minimums based on credit for lighting, a TERPS specified approach lighting system is required. 9. ODALS, MALS, SSALS, SALS are acceptable. 10. Indicates what chart should be followed in the related chapters in this document. 11. Circling procedures to a secondary runway from the primary approach will not be authorized when the secondary runway does not meet threshold siting (reference Appendix 2), OFZ (reference paragraph 306), and TERPS Order, 8260.3 paragraph 251, criteria. 1/3/08 AC 150/5300-13 CHG 12 Appendix 17 295 Appendix 17. MINIMUM DISTANCES BETWEEN CERTAIN AIRPORT FEATURES AND ANY ON-AIRPORT AGRICULTURE CROPS Table A17-1. Minimum Distances Between Certain Airport Features and Any On-Airport Agriculture Crops Distance in Feet From Runway Centerline to Crop Distance in Feet From Runway End to Crop Aircraft Approach Category and Design Group 1 Visual & > ¾ mile < ¾ mile Visual & > ¾ mile < ¾ mile Distance in Feet from Centerline of Taxiway to Crop Distance in Feet from Edge of Apron to Crop Category A & B Aircraft Group I 200 2 400 3003 600 45 40 Group II 250 400 4003 600 66 58 Group III 400 400 600 800 93 81 Group IV 400 400 1,000 1,000 130 113 Category C, D, & E Aircraft Group I 530 3 575 3 1,000 1,000 45 40 Group II 530 3 575 3 1,000 1,000 66 58 Group III 530 3 575 3 1,000 1,000 93 81 Group IV 530 3 575 3 1,000 1,000 130 113 Group V 530 3 575 3 1,000 1,000 160 138 Group VI 530 3 575 3 1,000 1,000 193 167 1. Design Groups are based on wing span or tail height, and Category depends on approach speed of the aircraft as shown below: Design Group Category Group I: Wing span up to 49 ft. Category A: Speed less than 91 knots Group II Wing span 49 ft. up to 73 ft. Category B: Speed 91 knots up to 120 knots Group III: Wing span 79 ft. up to 117 ft. Category C: Speed 121 knots up to 140 knots Group IV: Wing span 113 ft. up to 170 ft. Category D: Speed 141 knots up to 165 knots Group V: Wing span 171 ft. up to 213 ft. Category E: Speed 166 knots or more Group VI: Wing span 214 ft. up to 261 ft. 2. If the runway will only serve small airplanes (12,500 lb. and under) in Design Group I, this dimension may be reduced to 125 feet; however, this dimension should be increased where necessary to accommodate visual navigational aids that may be installed. For example, farming operations should not be allowed within 25 feet of a Precision Approach Path Indicator (PAPI) light box. 3. These dimensions reflect the Threshold Siting Surface (TSS) as defined in AC 150/5300-13, Appendix 2. The TSS cannot be penetrated by any object. Under these conditions, the TSS is more restrictive than the OFA, and the dimensions shown here are to prevent penetration of the TSS by crops and farm machinery. AC 150/5300-13 CHG 12 1/3/08 Appendix 17 296 This page intentionally left blank. 9/29/06 AC 150/5300-13 CHG 10 Appendix 18 297 Appendix 18. ACRONYMS The acronyms presented herein are intended for use with this publication only. AAA Airport Airspace Analysis AC Advisory Circular AD Airport Design AFD Airport Facility Directory ADG Airplane Design Group AIP Airport Improvement Program or Aeronautical Information Publication ALP Airport Layout Plan ALS Approach Lighting System ALSF(-1, -2) Approach Lighting System with Sequenced Flashers APV Approach Procedure with Vertical Guidance ARC Airport Reference Code ARP Airport Reference Point ASDA Accelerate-Stop Distance Available ASDE Airport Surface Detection Equipment ASR Airport Surveillance Radar ATC Air Traffic Control ATCT Airport Traffic Control Tower AWOS Automated Weather Observing System AZ Azimuth BRL Building Restriction Line CAT Category CFR Code of Federal Regulation CFW Center Field Wind CWY Clearway DA Decision Altitude DER Departure End of Runway DME Distance Measuring Equipment DXF AutoCAD Drawing Interchange file format EDS Environmental Data Service EL Elevation FBO Fixed Base Operator GPA Glidepath Angle GPS Global Positioning System GQS Glidepath Qualification Surface GS Glide Slope GVGI Generic Visual Slope Indicator HAT Height Above Touchdown HIRL High Intensity Runway Lights IFR Instrument Flight Rules IGES Initial Graphics Exchange Specification file format ILS Instrument Landing System IM Inner Marker IMC Instrument Meteorological Conditions LAAS Local Area Augmentation System LDA Landing Distance Available or Localizer Type Directional Aid LDIN Lead-In Lights LIRS Low Impact Resistant Supports LNAV Lateral Navigation LOC Localizer LPV Localizer Performance with Vertical Guidance MALS Medium Intensity Approach Lighting System MALSF Medium Intensity Approach Lighting System with Sequenced Flashers MALSR Medium Intensity Approach Lighting System with Runway Alignment Indicator Lights MIRL Medium Intensity Runway Lights MLS Microwave Landing System MM Middle Marker MSL Mean Sea Level NAVAID Navigational Aid NCDC National Climatic Data Center NDB Nondirectional Beacon NP Mon-Precision (Markings NPIAS National Plan of Integrated Airport Systems NTIS National Technical Information Service OCS Obstacle Clearance Surface ODALS Omnidirectional Approach Lighting System OEI One Engine Inoperative OFA Object Free Area OFZ Obstacle Free Zone OIS Obstacle Identification Surface OM Outer Marker NPA Non-Precision Approach P Precision (Markings) PA Precision Approach PAPI Precision Approach Path Indicator POFA Precision Object Free Area RAIL Runway Alignment Indicator Lights REIL Runway End Identifier Lights RNAV Area Navigation ROFA Runway Object Free Area RPZ Runway Protection Zone RSA Runway Safety Area RVR Runway Visual Range RW Runway SALS Short Approach Lighting System SSALR Short Simplified Approach Lighting System with Runway Alignment Indicator Lights SSALS Simplified Short Approach Lighting System SWY Stopway TCH Threshold Crossing Height TERPS FAA Order 8260.3, United States Standard for Terminal Instrument Procedures TH Threshold TL Taxilane TODA Takeoff Distance Available TORA Takeoff Run Available TSA Taxiway Safety Area TVOR Terminal Very High Frequency Omnirange TW Taxiway AC 150/5300-13 CHG 10 9/29/06 Appendix 18 298 USGS United States Geological Service V Visual (Markings) V1 Takeoff decision speed V2 Takeoff safety speed VFR Visual Flight Rules VLOF Lift-off speed VSO Stalling speed or the minimum steady flight speed in the landing configuration VNAV Vertical Navigation VOR Very High Frequency Omnirange WAAS Wide Area Augmentation System 9/29/06 AC 150/5300-13 CHG 10 Appendix 19 299 Appendix 19. INDEX Accelerate-Stop Distance Available (ASDA) definition.............................................................................2 length ..............................................................................276 Acronyms ...............................................................................297 Administration Building .........................................................118 Aeronautical Studies.............................................................6, 13 Aircraft Approach Category airplane listing ................................................................251 definition ............................................................................ 1 selection.............................................................................. 5 Aircraft Parking Area ................................... 10, 14, 15, 117, 139 Airplane Data.......................................................... 156, 165, 251 Airplane Design Group (ADG) airplane listing ................................................................251 definition.............................................................................1 selection..............................................................................5 Airport Buildings....................................................................117 Airport Design Standards Modification......................................5 Airport Elevation definition.............................................................................1 Airport Layout Plan (ALP) application ..........................................................................9 definition.............................................................................1 requirements .......................................................................5 Airport property requirements ....................................................9 Airport Reference Code (ARC) definition.............................................................................4 standards .............................................................................5 Airport Reference Point (ARP) definition ............................................................................ 1 standards......................................................................... 109 Airport Rotating Beacon .......................................................... 65 Airport Surface Detection Equipment (ASDE).........................66 Airport Surveillance Radar (ASR)............................................66 Airport survey.........................................................................122 Airport Traffic Control Tower (ATCT) ....................................65 Airport Traffic Control Tower Visibility ............................10, 35 Airspace Availability ..................................................................9 Approach Lighting System (ALS) ALSF-2 .............................................................................64 MALS ...............................................................................64 MALSF.............................................................................64 MALSR ............................................................................64 Apron for Based Airplanes .....................................................117 Aprons criteria...............................................................................10 gradient .............................................................................54 Auto Parking.....................................................................13, 123 Aviation easements.....................................................................9 Bird Hazards .......................................................................10, 13 Blast Fence criteria.......................................................................................77 definition ....................................................................................1 Bridges approach aprons................................................................70 blast protection .................................................................70 curbs .................................................................................70 height ................................................................................69 length ................................................................................69 load considerations ...........................................................69 longitudinal grades ...........................................................69 marking and lighting.........................................................69 pavement heating..............................................................70 security fences ....................................................................7 service roads .....................................................................70 siting precepts...................................................................69 width.................................................................................69 Building Plan ..........................................................................122 Building Restriction Lie (BRL) criteria...............................................................................12 definition.............................................................................1 Bypass Taxiway........................................................................34 Category (CATI) Runway ..........................................................2 Category (CATII) Runway .........................................................2 Category III (CAT III) Runway..................................................2 Center Field Wind (CFW) Installations ....................................66 Clear Zone ..................................................................................1 Clear Zone (See Runway Protection Zone) .................. 2, 13, 276 Clearway (CWY) definition.............................................................................1 standards ........................................................... 22, 139, 276 Compass Calibration Pad criteria.............................................................................111 definition.............................................................................1 Computer Program........................................ 34, 35, 88, 146, 153 Crosswind Runway............................................................. 10, 87 Crosswinds definition...........................................................................87 Declared Distances criteria..................................................................... 275, 276 definition.............................................................................2 Displaced Threshold definition ............................................................................3 siting requirements .........................................................101 Dual Parallel Taxiway ..............................................................34 Eating Facilities ......................................................................123 Electronic Deliverables...........................................................283 Entrance Taxiway .....................................................................34 Environmental Assessments ...................................................6, 9 Exit Taxiway .................................................................... 35, 142 FAA Studies of Objects ........................................................6, 13 Federal Assistance ......................................................................6 AC 150/5300-13 CHG 10 9/29/06 Appendix 19 300 Frangible NAVAID definition ............................................................................ 2 Hangars................................................................................... 118 Hazard to Air Navigation definition ............................................................................ 2 determination...................................................................... 6 presumption ........................................................................ 2 Holding Bay ............................................................................. 34 Holdline to runway...................................................... 10, 14, 15, 139 Inner-approach OFZ definition ............................................................................ 2 standards........................................................................... 22 Inner-transitional OFZ definition ............................................................................ 2 standards........................................................................... 22 Instrument Approach Procedures ........................................... 291 Instrument Landing System (1LS) glide slope .................................................................. 61, 62 localizer ...................................................................... 61, 62 marker beacons........................................................... 61, 63 Jet Blast heat effects........................................................................ 77 pressures ........................................................................... 77 velocity distances.............................................................. 77 Landing Distance Available (LDA) definition ............................................................................ 2 length.............................................................................. 276 Large Airplane definition ............................................................................ 2 Lead-in Lighting System (LDIN) ............................................. 65 Local Role .................................................................................. 6 Low Impact Resistant Supports (LIRS) definition ............................................................................ 2 Manager’s Office.................................................................... 123 Microwave Landing System (MLS) ......................................... 59 Modification of Airport Design Standards ................................. 5 Navigational Aids (NAVAIDs) clearing requirements ....................................................... 59 non-Federal....................................................................... 59 protection.................................................................... 59, 67 siting ................................................................................. 59 Nondirectional Beacon (NDB) ................................................. 63 Notice to the FAA airport development............................................................ 5 proposed construction ........................................................ 6 Object definition ............................................................................ 2 Object Clearing Criteria recommendations.............................................................. 13 standards........................................................................... 12 Object Free Area (OFA) definition ............................................................................ 2 standards ............................................................ 22, 33, 276 Obstacle Free Zone (OFZ) definition ............................................................................ 2 standards................................................................... 21, 139 Obstruction to Air Navigation definition ............................................................................ 2 presumption........................................................................ 2 survey requirement ............................................................. 9 Omindirectional Approach Lighting System (ODALS) ........... 65 Parallel Taxiway....................................................................... 33 Precision Object Free Area....................................................... 22 Property requirements ................................................................ 9 Public Restrooms.................................................................... 123 Recommendations requirement......................................................................... 1 Related Reading Material ........................................................... 3 Rescue and Firefighting Access Roads..................................... 23 Roads...................................................................................... 123 Runway (RW) definition ............................................................................ 3 gradient............................................................................. 49 length................................................................................ 21 line of sight....................................................................... 56 location ............................................................................... 9 orientation..................................................................... 9, 87 requirements for additional runways .......................... 10, 87 to aircraft parking area.................................. 10, 14, 15, 139 to helicopter touchdown pad ................................ 10, 14, 15 to holdline..................................................... 10, 14, 15, 139 to parallel runway ............................................................. 11 to parallel taxilane ................................ 10, 12, 14, 15, 139 to parallel taxiway ................................ 10, 12, 14, 15, 139 width................................................................................. 21 Runway Blast Pad definition ............................................................................ 3 drainage ............................................................................ 78 gradient ............................................................................ 54 length.......................................................................... 21, 78 marking sod lighting......................................................... 78 surface characteristics....................................................... 21 surface strength ................................................................ 78 width .................................................................. 21, 78 Runway Object Free Area background ..................................................................... 139 definition ............................................................................ 2 standards................................................................... 22, 276 Runway Obstacle Free Zone (OFZ) definition ............................................................................ 2 standards........................................................................... 21 Runway Protection Zone (RPZ) criteria............................................................... 13, 140, 276 definition ............................................................................ 3 Runway Safety Area (RSA) background ..................................................................... 139 definition ............................................................................ 3 gradient............................................................................. 54 length........................................................................ 21, 276 surface characteristics ...................................................... 21 width ................................................................................ 21 9/29/06 AC 150/5300-13 CHG 10 Appendix 19 301 Runway Shoulder definition (See Shoulder)....................................................3 drainage ............................................................................78 gradient .............................................................................54 marking and lighting.........................................................78 strength .............................................................................78 surface characteristics.......................................................21 width ...........................................................................21, 78 Runway visibility zone .............................................................56 Runway Visual Range Facilities...............................................66 Separation Standards .....................................................10, 14-16 Shoulder definition.............................................................................3 Small Airplane definition.............................................................................3 Standards applicability ........................................................................5 modification........................................................................5 requirements .......................................................................1 State Role....................................................................................6 Stopway (SWY) definition.............................................................................3 gradient .............................................................................49 location .............................................................................23 standards .........................................................................139 surface characteristics .......................................................23 width .................................................................................23 Takeoff Distance Available (TODA) definition ............................................................................1 length..............................................................................276 Takeoff Run Available (TORA) definition ............................................................................1 length..............................................................................276 Taxilane (TL) airport traffic control tower visibility ...............................35 definition ............................................................................3 dimensional standards ......................................................33 on apron edge ...................................................................35 to object...............................................................10, l6, 141 to parallel runway................................... 10, 12, 14, 15, 139 to parallel taxilane ...............................................10, l6, 141 to parallel taxiway ...............................................10, l6, 141 to parked aircraft .................................................10, l6, 141 to service and maintenance roads ........................10, l6, 141 Taxilane Object Free Area definition.............................................................................2 standards ...........................................................................33 width .........................................................................33, 141 wingtip clearance ..............................................................33 Taxiway (TW) airport traffic control tower visibility ...............................35 definition.............................................................................3 dimensional standards.......................................................33 edge safety margin......................................................34, 38 gradient .............................................................................54 intersections ......................................................................34 layout ................................................................................10 line of sight .......................................................................56 on apron edge....................................................................35 pavement filet ............................................... 34, 38, 40, 149 taxiway between parallel runways....................................35 to object .............................................................. 10, 16, 141 to parallel runway ................................... 10, 12, 14, 15, 139 to parallel taxilane ...............................................10, l6, 141 to parallel taxiway ...............................................10, l6, 141 to parked aircraft..................................................10, l6, 141 to service and maintenance roads ........................10, l6, 141 width ................................................................... 33, 38, 141 Taxiway Object Free Area definition ............................................................................2 standards...........................................................................33 width......................................................................... 33, 141 wingtip clearance..............................................................33 Taxiway Safety Area (TSA) definition ............................................................................3 gradient.............................................................................54 surface characteristics.......................................................33 width......................................................................... 33, 142 Taxiway Shoulder definition (See Shoulder)....................................................3 drainage ............................................................................78 gradient.............................................................................54 marking and lighting ........................................................78 strength.............................................................................78 surface characteristics.......................................................33 width...........................................................................33, 78 Terminal Very High Frequency Omnirange (TVOR) ..............64 Threshold (TH) definition ............................................................................3 siting requirements .........................................................101 Tiedowns ........................................................................ 117, 118 Transient Apron......................................................................117 Tunnels drainage ............................................................................70 lighting..............................................................................70 passenger and baggage......................................................70 ventilation .........................................................................70 Turnaround ...............................................................................35 Vehicle Parking ................................................................ 13, 123 Visual Runway definition.............................................................................3 Waiting Room.........................................................................122 Wildlife Hazards.................................................................10, 13 Wind Analysis ......................................................................9, 87 Wind Coverage .........................................................................87 Wingtip Clearance ............................................................ 33, 146