FAR23.441:Maneuveringloads. . . . . . . . . . . . . . . . . 280 FAR23.443:Gustloads. .................... 281 FAR23.445:Outboard.ns[orwinglets.] . . . . . . . . . . . 282
30.6AileronsandSpecialDevices . . . . . . . . . . . . . . . . . . 283
FAR23.455:Ailerons.. . . . . . . . . . . . . . . . . . . . . . 283 FAR23.457:[Removed.] .................... 283 FAR23.459:Specialdevices. .................. 283
30.7GroundLoads ........................... 283
FAR23.471:General. ...................... 283 FAR 23.473 : Ground load conditions and assumptions. . . . 283 FAR 23.477 : Landing gear arrangement. . . . . . . . . . . . 284 FAR23.479:Levellanding conditions. . . . . . . . . . . . . . 284 FAR 23.481 : Tail down landing conditions. . . . . . . . . . . 285 FAR 23.483 : One-wheel landing conditions. . . . . . . . . . . 285 FAR23.485:Sideload conditions. . . . . . . . . . . . . . . . 285 FAR23.493:Braked roll conditions. . . . . . . . . . . . . . . 286 FAR 23.497 : Supplementary conditions for tail wheels. . . . 286 FAR 23.499 : Supplementary conditions for nose wheels. . . . 286 FAR 23.505 : Supplementary conditions for skiplanes. . . . . 287 FAR23.507:[Jackingloads.] .................. 287 FAR23.509:[Towingloads.] .................. 287 FAR23.511 :[Groundload; unsymmetricalloads on multiple-wheel units.] ...................... 288
30.8WaterLoads ............................ 289
FAR23.521:Waterload conditions. . . . . . . . . . . . . . . 289 FAR23.523:[Designweightsand centerofgravitypositions.] 289 FAR23.525:[Applicationofloads.] . . . . . . . . . . . . . . 289 FAR23.527:[Hull and main.oatloadfactors.] . . . . . . . . 290 FAR23.529:[Hull and main.oatlanding conditions.] . . . . 290 FAR23.531:[Hull and main.oattakeo.condition.] . . . . . 291 FAR23.533:[Hull and main.oatbottompressures.] . . . . . 291 FAR23.535:[Auxiliary.oatloads.] . . . . . . . . . . . . . . 293 FAR23.537:[Seawingloads.] . . . . . . . . . . . . . . . . . . 294
30.9EmergencyLandingConditions . . . . . . . . . . . . . . . . . 295
FAR23.561:General. ...................... 295 FAR 23.562 : Emergency landing dynamic conditions. . . . . 296
30.10FatigueEvaluation. . . . . . . . . . . . . . . . . . . . . . . . . 298
FAR23.571:[Metallicpressurized cabinstructures.] . . . . . 298 FAR23.572:[Metallic] wing, empennage, and associated struc-
tures. .......................... 299 FAR23.573:Damage tolerance andfatigue evaluation of struc-
ture.. . . . . . . . . . . . . . . . . . . . . . . . . . . 299 FAR23.574:[Metallicdamagetolerance andfatigue evalua-
tion of commuter category airplanes.] . . . . . . . . 301 FAR23.575:[Inspectionsand otherprocedures.] . . . . . . . 301
′
Elodie Roux. Septembre 2003
Subpart C : Structure
30.1 General
FAR 23.301 : Loads.
(a)
Strength requirements are speci.edin terms oflimitloads(the maximumloadsto be expected in service) and ultimate loads (limit loads multiplied by prescribed factors of safety).Unless otherwiseprovided,prescribedloads arelimitloads.
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本文链接地址:FAA规章 美国联邦航空规章 Federal Aviation Regulations 1(141)