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Empennage

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are mounted to the rear of the fuselage. This is the simplest configuration that performs all three aspects of the function of a tail: trim, stability, and control. Around 60% of current aircraft designs — and about 80% ever — incorporate this type of tail. Examples are found on aircraft of every
922:(fins). In this position, the tail surfaces interact constructively with the wingtip vortices and, with careful design, can significantly reduce drag to improve efficiency, without adding unduly to the structural loads on the wing. 500: – The horizontal stabiliser is mounted on top of the fin, creating a "T" shape when viewed from the front. T-tails keep the stabilisers out of the engine wake, and give better pitch control. T-tails have a good 258:
that controls changes in pitch, the up-and-down motion of the aircraft's nose. In some aircraft the horizontal stabilizer and elevator are one unit, and to control pitch the entire unit moves as one. This is known as a
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An outboard tail is split in two, with each half mounted on a short boom just behind and outboard of each wing tip. It comprises outboard horizontal stabilizers (OHS) and may or may not include additional boom-mounted
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may be fitted lower down where it will be in free air when the aircraft is stalled. A T-tail must be stronger, and therefore heavier than a conventional tail. T-tails also tend to have a larger
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when viewed from the front. Cruciform tails are often used to keep the horizontal stabilisers out of the engine wake, while avoiding many of the disadvantages of a
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into which the stabiliser may be hinged at its spar and adjustably jacked a few degrees in incidence either up or down. Usually controlled by a cockpit crank.
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featured an "X" tail, which was reinforced and fitted with a wheel on each surface so that the craft could sit on its tail and take off and land vertically.
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designs. Here, the tail surfaces are set at diagonal angles, with each surface contributing to both pitch and yaw. The control surfaces, sometimes called
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Benjamin Darrenougue; "Aircraft Configurations With Outboard Horizontal Stabilizers" (Final year project report), Queens University Belfast, 14 May 2004.
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on the rudder to reduce the pilot effort required to keep the aircraft straight in situations of asymmetrical thrust, such as single engine operations.
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Some aircraft are fitted with a tail assembly that is hinged to pivot in two axes forward of the fin and stabiliser, in an arrangement referred to as a
282:, used to control yaw, which is movement of the fuselage right to left motion of the nose of the aircraft. The rear section of the vertical fin is the 341:
on the rear of the elevators or rudder which act to change the aerodynamic load on the surface. Usually controlled by a cockpit wheel or crank.
2027: 795:, act differentially to provide yaw control (in place of the rudder) and act together to provide pitch control (in place of the elevator). 633:
A twin boom has two fuselages or booms, with a vertical stabiliser on each, and a horizontal stabiliser between them. Examples include the
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In spite of effective control surfaces, many early aircraft that lacked a stabilising empennage were virtually unflyable. Even so-called "
318:(ELT) are often located in the empennage, because the aft of the aircraft provides better protection for these in most aircraft crashes. 1982: 1927: 1792: 1149: 2047: 1403: 1368: 1262: 1242: 1200: 1107: 1078: 807: 362:
used to trim some elevators and stabilators as well as increased control force feel. Usually controlled by a cockpit wheel or crank.
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stability. In some aircraft with swept wings, the airfoil section or angle of incidence may change radically towards the tip.
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an arrow". Most aircraft feature an empennage incorporating vertical and horizontal stabilising surfaces which stabilise the
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Chronik Eines Flugzeugwerkes 1932-1945. B&V – Blohm & Voss Hamburg – HFB Hamburger Flugzeugbau
504:, and are more efficient on low speed aircraft. However, the T-tail has several disadvantages. It is more likely to enter a 330:
devices are provided to eliminate the need for the pilot to maintain constant pressure on the elevator or rudder controls.
837: 315: 131:, is a structure at the rear of an aircraft that provides stability during flight, in a way similar to the feathers on an 2361: 2300: 2141: 1396: 733: 355:
trim system which uses a spring to provide an adjustable preload in the controls. Usually controlled by a cockpit lever.
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Kurt W. Muller; "Analysis of a Semi-Tailless Aircraft Design" (Master's thesis), Naval Postgraduate School, US, 2002.
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used to move the main control surface, as well as act as a trim tab. Usually controlled by a cockpit wheel or crank.
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tested the proposed control system in 1944 and, following several design proposals, an order was received for the
476: – The horizontal stabilisers are placed midway up the vertical stabiliser, giving the appearance of a 2208: 2052: 2002: 1119: 634: 1992: 1545: 1475: 609:, consists of two small vertical stabilisers on either side of the horizontal stabiliser. Examples include the 288:, a movable aerofoil that is used to turn the aircraft's nose right or left. When used in combination with the 2037: 2320: 2295: 2057: 1962: 1852: 1822: 1797: 1663: 1628: 814:
spacecraft. A V-tail may also have a smaller radar signature. Other aircraft featuring a V-tail include the
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to which these are attached. On an airliner this would be all the flying and control surfaces behind the
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Aircraft empennage designs may be classified broadly according to the fin and tailplane configurations.
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The tailplane comprises the tail-mounted fixed horizontal stabiliser and movable elevator. Besides its
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A V-tail can be lighter than a conventional tail in some situations and produce less drag, as on the
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The overall shapes of individual tail surfaces (tailplane planforms, fin profiles) are similar to
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Location of tailplane – mounted high, mid or low on the fuselage, fin or tail booms.
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Location of fins – on the fuselage (over or under), tailplane, tail booms or wings
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and is used to provide pitch stability. The rear section of the tailplane is called the
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Structurally, the empennage consists of the entire tail assembly, including the
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arrangement). A "tailless" type usually still has a vertical stabilising fin (
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The fin comprises the fixed vertical stabiliser and rudder. Besides its
176:). Heavier-than-air aircraft without any kind of empennage (such as the 1972: 1623: 1605: 1530: 289: 284: 181: 1708: 1678: 1585: 1560: 1490: 1034: 1029: 1002: 941:
just weeks before the war ended. The outboard tail reappeared on the
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Fixed stabiliser and movable elevator surfaces, or a single combined
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An alternative to the fin-and-tailplane approach is provided by the
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The most successful tailless configuration has been the tailless
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General Aviation Aircraft Design: Applied Methods and Procedures
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size and role, from general aviation types like the ubiquitous
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The configuration was first developed during World War II by
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whose trailing edge provide pitch stability, and rearwards
97: 822:. A slight modification to the V-tail can be found on the 115: 112: 106: 68: 1346:
Zdenek Titz and Jaroslav Zazvonil; "Kauba's Dwarfs",
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SpaceShipOne at the US National Air and Space Museum
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Aviation Supplies & Academics, 1997. 100: 94: 71: 62: 1124:"ATA Airline Handbook Chapter 5: How Aircraft Fly" 1013:which has a canard foreplane but no vertical fin. 27:Tail section of an aircraft containing stabilizers 1009:adopted the "tailless" description for the novel 460:to the largest airliners ever flown, such as the 208:The major components of an airplane's empennage. 1291:Aircraft Design: A Systems Engineering Approach 1255:Dictionary of Aeronautical Terms, third edition 1071:Dictionary of Aeronautical Terms, third edition 589:Number of fins – usually one or two. 180:) are rare, and generally use specially shaped 440:Some locations have been given special names: 296:, the essential feature of aircraft movement. 1404: 1285: 1283: 993:foreplane (nor does it have a second wing in 8: 1187: 1185: 1183: 1181: 1179: 1177: 1175: 596:Twin fins may be mounted at various points: 140: 1210: 1208: 1411: 1397: 1389: 1094: 1092: 1090: 1088: 1086: 1226: 1224: 242:The front (usually fixed) section of the 1065: 1063: 1061: 1059: 1057: 1055: 1051: 1363:(in German). Motor Buch Verlag, 1979 1317:Flight Testing of Fixed Wing Aircraft 1218:, p. 26. Thompson Publications, 1980. 1156:. Oxford Dictionaries. Archived from 276:has a fixed front section called the 172:" usually have a tail fin (usually a 7: 707:Unusual fin configurations include: 724: – examples include the 1235:Flight Training Manual 4th Edition 1020:, especially for combat aircraft. 989: – either tailplane or 840:uses an inverted V-tail as do the 373:Multi-engined aircraft often have 292:, the result is a banking turn, a 25: 1191:Aviation Publishers Co. Limited, 1098:Aviation Publishers Co. Limited, 808:Northrop Grumman RQ-4 Global Hawk 892: 883: 874: 766: 757: 695: 686: 677: 558: 549: 540: 531: 90: 52: 1195:, p. 14 (27th revised edition) 1102:, p. 10 (27th revised edition) 870: 753: 673: 527: 434:General Dynamics F-111 Aardvark 2321:In-flight entertainment system 2018:Horizontal situation indicator 1306:, Elsevier Science 2013, p.483 943:Scaled Composites SpaceShipOne 663:or on the wing tips as on the 1: 316:emergency locator transmitter 2301:Environmental control system 734:Northrop Grumman E-2 Hawkeye 605:A twin tail, also called an 135:. The term derives from the 1348:Flying Review International 816:Beechcraft Model 35 Bonanza 414:Configuration – 2378: 1978:Course deviation indicator 1669:Electro-hydraulic actuator 1334:November 23, 2022, at the 1154:Oxford Dictionaries Online 956: 585:, it is characterised by: 574: 410:, it is characterised by: 399: 2209:Conventional landing gear 1120:Air Transport Association 635:Northrop P-61 Black Widow 192:to provide the necessary 1993:Flight management system 714: – as on the 333:The trim device may be: 2296:Emergency oxygen system 2058:Turn and slip indicator 1853:Leading-edge droop flap 1823:Drag-reducing aerospike 1798:Adaptive compliant wing 1793:Active Aeroelastic Wing 1350:, Nov 1965, pp.169-172. 1001:) and control surface ( 516:. Examples include the 484:. Examples include the 274:vertical tail structure 2336:Passenger service unit 2137:Self-sealing fuel tank 2033:Multi-function display 1275:Introduction to Flight 1011:X-36 research aircraft 974: 939:Blohm & Voss P 215 914: 726:Lockheed Constellation 716:McDonnell Douglas X-36 643:de Havilland Sea Vixen 522:McDonnell Douglas DC-9 453:horizontal stabilisers 308:cockpit voice recorder 267:full-flying stabiliser 239: 226:rear pressure bulkhead 209: 141: 43: 2316:Ice protection system 2234:Tricycle landing gear 2224:Landing gear extender 1441:Aft pressure bulkhead 1289:Mohammad H. Sadraey, 1122:(November 10, 2011). 987:horizontal stabiliser 966: 912: 346:adjustable stabiliser 248:horizontal stabiliser 234: 207: 161:, as well as housing 123:), also known as the 35: 2281:Auxiliary power unit 1689:Flight control modes 1315:Ralph D. Kimberlin, 1302:Snorri Gudmundsson, 1130:on November 10, 2011 920:vertical stabilizers 611:Antonov An-225 Mriya 432:or "-flying tail". ( 312:flight data recorder 236:Yaw, pitch, and roll 220:and the part of the 36:The empennage of an 2362:Aircraft components 2260:Escape crew capsule 2167:War emergency power 2038:Pitot–static system 1883:Variable-sweep wing 1591:Vertical stabilizer 1359:Pohlmann, Hermann. 1319:, AIAA 2003, p.380. 1293:, Wiley 2013, p.289 1273:Anderson, John D., 1214:Reichmann, Helmet: 999:vertical stabiliser 929:and George Haag at 744:North American X-15 577:Vertical stabilizer 514:radar cross section 490:Douglas A-4 Skyhawk 449:vertical stabiliser 381:Tail configurations 279:vertical stabiliser 254:, and is a movable 174:vertical stabiliser 1968:Attitude indicator 1948:Airspeed indicator 1943:Aircraft periscope 1193:From the Ground Up 1100:From the Ground Up 975: 915: 683:Tailplane mounted 659:midwing as on the 447: – The 240: 210: 44: 2349: 2348: 2276:Aircraft lavatory 2013:Heading indicator 1958:Annunciator panel 1938:Air data computer 1848:Leading-edge cuff 1216:Flying Sailplanes 979:tailless aircraft 959:Tailless aircraft 953:Tailless aircraft 902: 901: 856:LearAvia Lear Fan 776: 775: 732:(three), and the 705: 704: 665:Handley Page Manx 568: 567: 564:Flying tailplane 537:Fuselage mounted 445:Conventional tail 326:In some aircraft 170:tailless aircraft 16:(Redirected from 2369: 2331:Navigation light 2311:Hydraulic system 2286:Bleed air system 2214:Drogue parachute 1888:Vortex generator 1506:Interplane strut 1413: 1406: 1399: 1390: 1383: 1378: 1372: 1357: 1351: 1344: 1338: 1326: 1320: 1313: 1307: 1300: 1294: 1287: 1278: 1277:, 5th ed, p. 517 1271: 1265: 1251: 1245: 1231:Transport Canada 1228: 1219: 1212: 1203: 1189: 1170: 1169: 1167: 1165: 1160:on July 22, 2012 1146: 1140: 1139: 1137: 1135: 1126:. Archived from 1116: 1110: 1096: 1081: 1067: 931:Blohm & Voss 896: 889:Inverted V-tail 887: 878: 871: 834:Inverted V tail: 830:called a Y-tail. 779:V, Y and X tails 770: 761: 754: 699: 690: 681: 674: 562: 553: 544: 535: 528: 294:coordinated turn 163:control surfaces 144: 122: 121: 118: 117: 114: 111: 108: 105: 102: 99: 96: 87: 86: 83: 82: 79: 76: 73: 70: 67: 64: 61: 58: 21: 2377: 2376: 2372: 2371: 2370: 2368: 2367: 2366: 2352: 2351: 2350: 2345: 2341:Ram air turbine 2306:Flight recorder 2264: 2243: 2176: 2157:Thrust reversal 2081: 2072: 2043:Radar altimeter 2008:Head-up display 1918: 1907: 1803:Anti-shock body 1785: 1773: 1634:Artificial feel 1616:Flight controls 1610: 1476:Fabric covering 1426: 1422:components and 1417: 1387: 1386: 1379: 1375: 1358: 1354: 1345: 1341: 1336:Wayback Machine 1327: 1323: 1314: 1310: 1301: 1297: 1288: 1281: 1272: 1268: 1252: 1248: 1229: 1222: 1213: 1206: 1190: 1173: 1163: 1161: 1148: 1147: 1143: 1133: 1131: 1118: 1117: 1113: 1097: 1084: 1068: 1053: 1048: 1026: 961: 955: 935:Skoda-Kauba SL6 907: 897: 888: 879: 781: 771: 762: 700: 692:Twin tail boom 691: 682: 579: 573: 563: 554: 545: 536: 518:Gloster Javelin 486:Hawker Sea Hawk 404: 398: 383: 324: 306:The aircraft's 238:in an aircraft. 202: 151:flight dynamics 137:French language 93: 89: 55: 51: 28: 23: 22: 15: 12: 11: 5: 2375: 2373: 2365: 2364: 2354: 2353: 2347: 2346: 2344: 2343: 2338: 2333: 2328: 2326:Landing lights 2323: 2318: 2313: 2308: 2303: 2298: 2293: 2288: 2283: 2278: 2272: 2270: 2266: 2265: 2263: 2262: 2257: 2251: 2249: 2248:Escape systems 2245: 2244: 2242: 2241: 2236: 2231: 2226: 2221: 2216: 2211: 2206: 2201: 2196: 2190: 2188: 2186:arresting gear 2178: 2177: 2175: 2174: 2169: 2164: 2159: 2154: 2149: 2144: 2142:Splitter plate 2139: 2134: 2129: 2124: 2119: 2114: 2109: 2104: 2099: 2094: 2088: 2086: 2074: 2073: 2071: 2070: 2065: 2060: 2055: 2050: 2045: 2040: 2035: 2030: 2025: 2020: 2015: 2010: 2005: 2000: 1995: 1990: 1985: 1980: 1975: 1970: 1965: 1960: 1955: 1950: 1945: 1940: 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774: 773: 764: 752: 751: 748:Dornier Do 335 737: 730:Bellanca 14-13 719: 703: 702: 693: 684: 672: 671: 654: 647:Sadler Vampire 639:P-38 Lightning 626: 619:Avro Lancaster 594: 593: 590: 575:Main article: 572: 569: 566: 565: 556: 547: 538: 526: 525: 493: 473:Cruciform tail 469: 438: 437: 426: 423: 400:Main article: 397: 394: 390:wing planforms 382: 379: 371: 370: 363: 360:anti-servo tab 356: 349: 342: 323: 320: 246:is called the 201: 198: 41:Boeing 747-200 26: 24: 14: 13: 10: 9: 6: 4: 3: 2: 2374: 2363: 2360: 2359: 2357: 2342: 2339: 2337: 2334: 2332: 2329: 2327: 2324: 2322: 2319: 2317: 2314: 2312: 2309: 2307: 2304: 2302: 2299: 2297: 2294: 2292: 2289: 2287: 2284: 2282: 2279: 2277: 2274: 2273: 2271: 2269:Other systems 2267: 2261: 2258: 2256: 2255:Ejection seat 2253: 2252: 2250: 2246: 2240: 2237: 2235: 2232: 2230: 2227: 2225: 2222: 2220: 2217: 2215: 2212: 2210: 2207: 2205: 2202: 2200: 2199:Arrestor hook 2197: 2195: 2194:Aircraft tire 2192: 2191: 2189: 2187: 2183: 2179: 2173: 2170: 2168: 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1745: 1742: 1740: 1737: 1735: 1732: 1730: 1727: 1725: 1722: 1720: 1717: 1715: 1714:Rudder pedals 1712: 1710: 1707: 1705: 1702: 1700: 1697: 1695: 1692: 1690: 1687: 1685: 1682: 1680: 1677: 1675: 1672: 1670: 1667: 1665: 1662: 1660: 1657: 1655: 1652: 1650: 1647: 1645: 1642: 1640: 1637: 1635: 1632: 1630: 1627: 1625: 1622: 1621: 1619: 1617: 1613: 1607: 1604: 1602: 1599: 1597: 1594: 1592: 1589: 1587: 1584: 1582: 1579: 1577: 1574: 1572: 1571:Trailing edge 1569: 1567: 1564: 1562: 1559: 1557: 1554: 1552: 1551:Stressed skin 1549: 1547: 1544: 1542: 1539: 1537: 1534: 1532: 1529: 1527: 1524: 1522: 1519: 1517: 1514: 1512: 1509: 1507: 1504: 1502: 1499: 1497: 1494: 1492: 1489: 1487: 1484: 1482: 1479: 1477: 1474: 1472: 1469: 1467: 1464: 1462: 1459: 1457: 1454: 1452: 1449: 1447: 1444: 1442: 1439: 1438: 1436: 1433: 1429: 1425: 1421: 1414: 1409: 1407: 1402: 1400: 1395: 1394: 1391: 1382: 1377: 1374: 1370: 1369:3-87943-624-X 1366: 1362: 1356: 1353: 1349: 1343: 1340: 1337: 1333: 1330: 1325: 1322: 1318: 1312: 1309: 1305: 1299: 1296: 1292: 1286: 1284: 1280: 1276: 1270: 1267: 1264: 1263:1-56027-287-2 1260: 1256: 1253:Crane, Dale: 1250: 1247: 1244: 1243:0-7715-5115-0 1240: 1236: 1232: 1227: 1225: 1221: 1217: 1211: 1209: 1205: 1202: 1201:0-9690054-9-0 1198: 1194: 1188: 1186: 1184: 1182: 1180: 1178: 1176: 1172: 1159: 1155: 1151: 1145: 1142: 1129: 1125: 1121: 1115: 1112: 1109: 1108:0-9690054-9-0 1105: 1101: 1095: 1093: 1091: 1089: 1087: 1083: 1080: 1079:1-56027-287-2 1076: 1072: 1069:Crane, Dale: 1066: 1064: 1062: 1060: 1058: 1056: 1052: 1045: 1041: 1038: 1036: 1033: 1031: 1028: 1027: 1023: 1021: 1019: 1014: 1012: 1008: 1005:). However, 1004: 1000: 996: 992: 988: 984: 980: 973: 972: 965: 960: 952: 950: 948: 944: 940: 936: 932: 928: 923: 921: 911: 905:Outboard tail 904: 895: 891: 886: 882: 877: 873: 872: 866: 862: 859: 857: 853: 850: 847: 843: 839: 836:The unmanned 835: 832: 829: 825: 821: 817: 813: 809: 805: 801: 798: 797: 796: 794: 790: 786: 778: 769: 765: 760: 756: 755: 749: 745: 741: 738: 735: 731: 727: 723: 722:Multiple fins 720: 717: 713: 710: 709: 708: 701:Wing mounted 698: 694: 689: 685: 680: 676: 675: 670: 669:Rutan Long-EZ 666: 662: 658: 655: 652: 651:Edgley Optica 648: 644: 640: 636: 632: 631: 627: 624: 620: 616: 615:B-25 Mitchell 612: 608: 604: 603: 599: 598: 597: 591: 588: 587: 586: 584: 578: 570: 561: 557: 552: 548: 543: 539: 534: 530: 529: 523: 519: 515: 511: 507: 503: 499: 498: 494: 491: 487: 483: 479: 475: 474: 470: 467: 463: 459: 454: 450: 446: 443: 442: 441: 435: 431: 427: 424: 421: 417: 413: 412: 411: 409: 403: 395: 393: 391: 386: 380: 378: 376: 368: 364: 361: 357: 354: 350: 347: 343: 340: 336: 335: 334: 331: 329: 321: 319: 317: 313: 309: 304: 302: 297: 295: 291: 287: 286: 281: 280: 275: 270: 268: 264: 263: 257: 253: 249: 245: 237: 233: 229: 227: 223: 219: 215: 206: 199: 197: 195: 191: 188:, often with 187: 183: 179: 175: 171: 166: 164: 160: 156: 152: 148: 145:which means " 143: 138: 134: 130: 129:tail assembly 126: 120: 85: 49: 42: 39: 34: 30: 19: 18:Tail assembly 2291:Deicing boot 2219:Landing gear 2162:Townend ring 2152:Thrust lever 2127:NACA cowling 2092:Autothrottle 2084:fuel systems 2082:devices and 1873:Stall strips 1843:Krueger flap 1813:Channel wing 1759:Wing warping 1749:Stick shaker 1744:Stick pusher 1664:Dual control 1649:Centre stick 1516:Leading edge 1486:Flying wires 1470: 1446:Cabane strut 1376: 1360: 1355: 1347: 1342: 1324: 1316: 1311: 1303: 1298: 1290: 1274: 1269: 1254: 1249: 1234: 1215: 1192: 1162:. Retrieved 1158:the original 1153: 1144: 1132:. Retrieved 1128:the original 1114: 1099: 1070: 1015: 982: 978: 976: 970: 947:SpaceShipTwo 945:in 2003 and 927:Richard Vogt 924: 916: 865:Lockheed XFV 860: 851: 833: 828:Monnett Moni 799: 793:ruddervators 782: 772:Ventral fin 763:Triple fins 739: 721: 711: 706: 657:Wing mounted 656: 628: 623:ERCO Ercoupe 606: 600: 595: 580: 509: 495: 471: 444: 439: 405: 387: 384: 372: 332: 325: 305: 301:movable tail 300: 298: 293: 283: 277: 271: 266: 260: 247: 241: 211: 178:Northrop B-2 167: 128: 124: 47: 45: 29: 2239:Tundra tire 2122:Intake ramp 2053:Transponder 1838:Gurney flap 1779:Aerodynamic 1694:Fly-by-wire 1576:Triple tail 1150:"Empennage" 1040:Tail-sitter 740:Ventral fin 661:F7U Cutlass 502:glide ratio 466:Blériot VII 462:Airbus A380 186:swept wings 2229:Oleo strut 2117:Inlet cone 2112:Gascolator 2078:Propulsion 2068:Yaw string 2063:Variometer 1919:instrument 1898:Wing fence 1833:Gouge flap 1808:Blown flap 1764:Yaw damper 1739:Stabilator 1724:Side-stick 1659:Dive brake 1546:Stabilizer 1521:Lift strut 1511:Jury strut 1046:References 820:Davis DA-2 546:Cruciform 506:deep stall 458:Cessna 172 430:stabilator 396:Tailplanes 262:stabilator 147:to feather 2204:Autobrake 2132:NACA duct 2107:Fuel tank 2097:Drop tank 2080:controls, 1963:Astrodome 1953:Altimeter 1818:Dog-tooth 1783:high-lift 1734:Spoileron 1719:Servo tab 1699:Gust lock 1654:Deceleron 1639:Autopilot 1596:Wing root 1581:Twin tail 1566:Tailplane 1501:Hardpoint 1471:Empennage 1434:structure 983:tail-less 949:in 2010. 806:trainer, 728:(three), 630:Twin boom 602:Twin tail 402:tailplane 375:trim tabs 367:servo tab 244:tailplane 218:tailplane 200:Structure 48:empennage 38:Atlas Air 2356:Category 2172:Wet wing 2147:Throttle 1893:Vortilon 1754:Trim tab 1684:Flaperon 1674:Elevator 1629:Airbrake 1601:Wing tip 1526:Longeron 1496:Fuselage 1432:Airframe 1420:Aircraft 1332:Archived 1164:March 5, 1134:March 5, 1024:See also 846:Mini-IMP 838:Predator 810:RPV and 510:tail-let 468:of 1907. 416:tailless 408:planform 339:trim tab 290:ailerons 256:aerofoil 252:elevator 222:fuselage 190:dihedral 182:airfoils 142:empenner 2182:Landing 1973:Compass 1921:systems 1913:Avionic 1903:Winglet 1786:devices 1729:Spoiler 1624:Aileron 1606:Wingbox 1531:Nacelle 1481:Fairing 1424:systems 981:(often 971:Swallow 898:X-tail 880:V-tail 861:X tail: 800:V tail: 736:(four). 583:profile 555:T-tail 214:tailfin 1917:flight 1878:Strake 1709:Rudder 1679:Elevon 1644:Canard 1586:V-tail 1561:T-tail 1491:Former 1451:Canopy 1367:  1261:  1241:  1199:  1106:  1077:  1035:S-duct 1030:Trijet 1003:rudder 995:tandem 991:canard 969:DH108 933:. The 852:Y tail 842:Lazair 818:, and 789:X-tail 785:V-tail 712:No fin 649:, and 621:, and 607:H-tail 497:T-tail 482:T-tail 420:canard 353:bungee 285:rudder 216:, the 2102:FADEC 1988:EICAS 1863:Slats 1704:HOTAS 1556:Strut 1018:delta 824:Waiex 478:cross 159:pitch 139:verb 133:arrow 2184:and 2048:TCAS 2028:ISIS 1983:EFIS 1928:ACAS 1915:and 1868:Slot 1828:Flap 1781:and 1769:Yoke 1541:Spar 1466:Dope 1365:ISBN 1259:ISBN 1239:ISBN 1197:ISBN 1166:2013 1136:2013 1104:ISBN 1075:ISBN 1007:NASA 967:The 863:The 844:and 826:and 812:X-37 787:and 746:and 667:and 571:Fins 520:and 488:and 451:and 328:trim 322:Trim 314:and 272:The 157:and 125:tail 46:The 2023:INS 2003:GPS 1858:LEX 1536:Rib 418:or 358:an 344:an 265:or 194:yaw 155:yaw 153:of 127:or 88:or 2358:: 1282:^ 1233:: 1223:^ 1207:^ 1174:^ 1152:. 1085:^ 1054:^ 977:A 750:). 645:, 641:, 637:, 617:, 613:, 392:. 365:a 351:a 337:a 310:, 269:. 228:. 165:. 116:dʒ 78:ɑː 60:ɑː 1412:e 1405:t 1398:v 1371:. 1168:. 1138:. 848:. 653:. 625:. 524:. 492:. 436:) 422:. 119:/ 113:ɪ 110:n 107:ɪ 104:p 101:m 98:ɛ 95:ˈ 92:/ 84:/ 81:ʒ 75:n 72:ˈ 69:ɪ 66:p 63:m 57:ˌ 54:/ 50:( 20:)

Index

Tail assembly

Atlas Air
Boeing 747-200
/ˌɑːmpɪˈnɑːʒ/
/ˈɛmpɪnɪ/
arrow
French language
to feather
flight dynamics
yaw
pitch
control surfaces
tailless aircraft
vertical stabiliser
Northrop B-2
airfoils
swept wings
dihedral
yaw

tailfin
tailplane
fuselage
rear pressure bulkhead

Yaw, pitch, and roll
tailplane
elevator
aerofoil

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