AFS-640

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AFS-640 ( afs-640 )

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9/27/01 AC 43.13-1B CHG 1 data should provide a true picture of the status of the electrical system. New or additional electrical devices should not be installed in an aircraft, nor the capacity changed of any power source, until the status of the electrical system in the aircraft has been determined accurately and found not to adversely affect the integrity of the electrical system. 11-37. JUNCTION BOX CONSTRUC- TION. Replacement junction boxes should be fabricated using the same material as the origi- nal or from a fire-resistant, nonabsorbent mate- rial, such as aluminum, or an acceptable plastic material. Where fire-proofing is necessary, a stainless steel junction box is recommended. Rigid construction will prevent “oil-canning” of the box sides that could result in internal short circuits. In all cases, drain holes should be provided in the lowest portion of the box. Cases of electrical power equipment must be insulated from metallic structure to avoid ground fault related fires. (See para- graph 11-7.) a. Internal Arrangement. The junction box arrangement should permit easy access to any installed items of equipment, terminals, and wires. Where marginal clearances are un- avoidable, an insulating material should be in- serted between current carrying parts and any grounded surface. It is not good practice to mount equipment on the covers or doors of junction boxes, since inspection for internal clearance is impossible when the door or cover is in the closed position. b. Installation. Junction boxes should be securely mounted to the aircraft structure in such a manner that the contents are readily ac- cessible for inspection. When possible, the open side should face downward or at an angle so that loose metallic objects, such as washers or nuts, will tend to fall out of the junction box rather than wedge between terminals. c. Wiring. Junction box layouts should take into consideration the necessity for ade- quate wiring space and possible future addi- tions. Electrical wire bundles should be laced or clamped inside the box so that cables do not touch other components, prevent ready access, or obscure markings or labels. Cables at en- trance openings should be protected against chafing by using grommets or other suitable means. 11-38.11-46. [RESERVED.] Par 11-38 Page 11-13 (and 11-14)

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