14 C.F.R. Subpart C—Strength Requirements
Title 14 - Aeronautics and Space
Strength requirements are specified in terms of limit loads, that are the maximum load to be expected in service, and ultimate loads, that are limit loads multiplied by prescribed factors of safety. Unless otherwise specified, all prescribed loads are limit loads. In determining limit load, the limit flight load factor must be at least 1.4. (a) Except as specified in paragraphs (b) and (c) of this section, the factor of safety is 1.5. (b) A factor of safety of at least five must be used in envelope design. A reduced factor of safety of at least two may be used if it is shown that the selected factor will preclude failure due to creep or instantaneous rupture from lack of rip stoppers. The selected factor must be applied to the more critical of the maximum operating pressure or envelope stress. (c) A factor of safety of at least five must be used in the design of all fibrous or non-metallic parts of the rigging and related attachments of the envelope to basket, trapeze, or other means provided for carrying occupants. The primary attachments of the envelope to the basket, trapeze, or other means provided for carrying occupants must be designed so that failure is extremely remote or so that any single failure will not jeopardize safety of flight. (d) In applying factors of safety, the effect of temperature, and other operating characteristics, or both, that may affect strength of the balloon must be accounted for. (e) For design purposes, an occupant weight of at least 170 pounds must be assumed. [Doc. No. 1437, 29 FR 8258, July 1, 1964, as amended by Amdt. 31–2, 30 FR 3377, Mar. 13, 1965] (a) The structure must be able to support limit loads without detrimental effect. (b) The structure must be substantiated by test to be able to withstand the ultimate loads for at least three seconds without failure. For the envelope, a test of a representative part is acceptable, if the part tested is large enough to include critical seams, joints, and load attachment points and members. (c) An ultimate free-fall drop test must be made of the basket, trapeze, or other place provided for occupants. The test must be made at design maximum weight on a horizontal surface, with the basket, trapeze, or other means provided for carrying occupants, striking the surface at angles of 0, 15, and 30 degrees. The weight may be distributed to simulate actual conditions. There must be no distortion or failure that is likely to cause serious injury to the occupants. A drop test height of 36 inches, or a drop test height that produces, upon impact, a velocity equal to the maximum vertical velocity determined in accordance with §31.19, whichever is higher, must be used. [Doc. No. 1437, 29 FR 8258, July 1, 1964, as amended by Amdt. 31–4, 45 FR 60179, Sept. 11, 1980]
Title 14: Aeronautics and Space
PART 31—AIRWORTHINESS STANDARDS: MANNED FREE BALLOONS
Subpart C—Strength Requirements
§ 31.21 Loads.
§ 31.23 Flight load factor.
§ 31.25 Factor of safety.
§ 31.27 Strength.
