Source: http://www.law.cornell.edu/cfr/text/14/23/subpart-C
Timestamp: 2013-05-21 19:30:23
Document Index: 481751293

Matched Legal Cases: ['art 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23', '§ 23']

14 CFR 23, Subpart C - Structure | Title 14 - Aeronautics and Space | Code of Federal Regulations | LII / Legal Information Institute
CFR › Title 14 › Chapter I › Subchapter C › Part 23 › Subpart C	prev | next
14 CFR 23, Subpart C - Structure
§ 23.301 — Loads.
§ 23.302 — Canard or tandem wing configurations.
§ 23.303 — Factor of safety.
§ 23.305 — Strength and deformation.
§ 23.307 — Proof of structure.
§ 23.321 — General.
§ 23.331 — Symmetrical flight conditions.
§ 23.333 — Flight envelope.
§ 23.335 — Design airspeeds.
§ 23.337 — Limit maneuvering load factors.
§ 23.341 — Gust loads factors.
§ 23.343 — Design fuel loads.
§ 23.345 — High lift devices.
§ 23.347 — Unsymmetrical flight conditions.
§ 23.349 — Rolling conditions.
§ 23.351 — Yawing conditions.
§ 23.361 — Engine torque.
§ 23.363 — Side load on engine mount.
§ 23.365 — Pressurized cabin loads.
§ 23.367 — Unsymmetrical loads due to engine failure.
§ 23.369 — Rear lift truss.
§ 23.371 — Gyroscopic and aerodynamic loads.
§ 23.373 — Speed control devices.
§ 23.391 — Control surface loads.
§ 23.393 — Loads parallel to hinge line.
§ 23.395 — Control system loads.
§ 23.397 — Limit control forces and -torques.
§ 23.399 — Dual control system.
§ 23.405 — Secondary control system.
§ 23.407 — Trim tab effects.
§ 23.409 — Tabs.
§ 23.415 — Ground gust conditions.
— Horizontal Stabilizing and Balancing Surfaces
§ 23.421 — Balancing loads.
§ 23.423 — Maneuvering loads.
§ 23.425 — Gust loads.
§ 23.427 — Unsymmetrical loads.
— Vertical Surfaces
§ 23.441 — Maneuvering loads.
§ 23.443 — Gust loads.
§ 23.445 — Outboard fins or winglets.
— Ailerons and Special Devices
§ 23.455 — Ailerons.
§ 23.459 — Special devices.
§ 23.471 — General.
§ 23.473 — Ground load conditions and assumptions.
§ 23.477 — Landing gear arrangement.
§ 23.479 — Level landing conditions.
§ 23.481 — Tail down landing conditions.
§ 23.483 — One-wheel landing conditions.
§ 23.485 — Side load conditions.
§ 23.493 — Braked roll conditions.
§ 23.497 — Supplementary conditions for tail wheels.
§ 23.499 — Supplementary conditions for nose wheels.
§ 23.505 — Supplementary conditions for skiplanes.
§ 23.507 — Jacking loads.
§ 23.509 — Towing loads.
§ 23.511 — Ground load; unsymmetrical loads on multiple-wheel units.
§ 23.521 — Water load conditions.
§ 23.523 — Design weights and center of gravity positions.
§ 23.525 — Application of loads.
§ 23.527 — Hull and main float load factors.
§ 23.529 — Hull and main float landing conditions.
§ 23.531 — Hull and main float takeoff condition.
§ 23.533 — Hull and main float bottom pressures.
§ 23.535 — Auxiliary float loads.
§ 23.537 — Seawing loads.
§ 23.561 — General.
§ 23.562 — Emergency landing dynamic conditions.
§ 23.571 — Metallic pressurized cabin structures.
§ 23.572 — Metallic wing, empennage, and associated structures.
§ 23.573 — Damage tolerance and fatigue evaluation of structure.
§ 23.574 — Metallic damage tolerance and fatigue evaluation of commuter category airplanes.
§ 23.575 — Inspections and other procedures.