The Code of Federal Regulations of the United States of America: Having General Applicability and Legal Effect in Force June 1, 1938, Volume 4U.S. Government Printing Office, 1939 |
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Page 114
... loads . 04.22 Control surface loads . 04.23 Control system loads . 04.24 Ground loads . 04.25 Water loads . 04.26 Special loading conditions . 04.27 Multiplying factors of safety . 04.3 Proof of structure . 04.30 General . 04.31 Proof ...
... loads . 04.22 Control surface loads . 04.23 Control system loads . 04.24 Ground loads . 04.25 Water loads . 04.26 Special loading conditions . 04.27 Multiplying factors of safety . 04.3 Proof of structure . 04.30 General . 04.31 Proof ...
Page 115
... load factor incre- ment , Condition I. " Balancing " distribution - hori- zontal tail . " Maneuvering " tail load distri- bution . " Damping " tail load distribution . Aileron load distribution . Elevator control force limits . Aileron ...
... load factor incre- ment , Condition I. " Balancing " distribution - hori- zontal tail . " Maneuvering " tail load distri- bution . " Damping " tail load distribution . Aileron load distribution . Elevator control force limits . Aileron ...
Page 118
... loads and shall demonstrate the ability of the structure to develop the required factors of safety with respect to these loads either by analytical methods satisfactory to the Secretary or by reference to authenticated test data , or by ...
... loads and shall demonstrate the ability of the structure to develop the required factors of safety with respect to these loads either by analytical methods satisfactory to the Secretary or by reference to authenticated test data , or by ...
Page 122
... load factors and design level speed , V. ( See §§ 04.111 , 04.211 . ) 04.106 Design wing loading , W / S . The design weight ( § 04.101 ) divided by the design wing area ( § 04.104 ) . 04.107 Design power loading , W / P . The design ...
... load factors and design level speed , V. ( See §§ 04.111 , 04.211 . ) 04.106 Design wing loading , W / S . The design weight ( § 04.101 ) divided by the design wing area ( § 04.104 ) . 04.107 Design power loading , W / P . The design ...
Page 123
... load to the design weight . When the load in question represents the net external load acting on the airplane in a given direction , n represents the acceleration factor in that direction . 04.120 Limit load . A load ( or load factor ...
... load to the design weight . When the load in question represents the net external load acting on the airplane in a given direction , n represents the acceleration factor in that direction . 04.120 Limit load . A load ( or load factor ...
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