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3.1 This specification provides designers and manufacturers of electric propulsion for light sport aircraft design references and criteria to use in designing and manufacturing EPUs. 3.2 Declaration of compliance is based on testing and documentation during the design, ground testing and flight...
4.1 Personnel utilizing reference radiographs to this standard shall be qualified to perform radiographic interpretation in accordance with a nationally or internationally recognized NDT personnel qualification practice or standard and certified by the employer or certifying agency, as applicable....
4.1 Personnel utilizing reference radiographs to this standard shall be qualified to perform radiographic interpretation in accordance with a nationally or internationally recognized NDT personnel qualification practice or standard and certified by the employer or certifying agency, as applicable....
This European Standard specifies the characteristics of electrical wires AZA family for use in the on board: - 115 V (phase to neutral) or 200 V (phase to phase) electrical network of aircraft. - 230 V (phase to neutral) or 400 V (phase to phase) electrical network of...
This European Standard specifies the characteristics of electrical wires AZ family for use in the on board: - 115 V (phase to neutral) or 200 V (phase to phase) electrical network of aircraft. - 230 V (phase to neutral) or 400 V (phase to phase) electrical network of...
This Standard specifies: • Requirements for the following crimping wire connections intended for high reliability electrical connections for use on spacecraft and associated equipment operating under high vacuum, thermal cycling and launch vibration: - removable contacts, single...
This document specifies the characteristics of UV laser printable electrical lightweight wires DR family for use in the on-board up to 115 V (phase to neutral) or 200 V (phase to phase) AC and 28 Vdc and electrical systems of aircraft at operating temperatures between - 65 °C...
This Standard specifies: • Requirements for the following crimping wire terminations intended for high reliability electrical connections for use on customer spacecraft and associated equipment operating under high vacuum, thermal cycling and launch vibration: • removable contacts,...
4.1 Design-The design procedures defined in this practice are intended to provide acceptable guidance in the original design of electrical systems. 4.2 Alteration-The alteration procedures defined in this practice are intended to provide acceptable guidance for modification of general...
4.1 This practice is intended to be used as a standard wiring practice for aircraft when not contrary to standards published by the aircraft original equipment manufacturer (OEM) or regulations. This practice is intended to be used for maintenance and preventive maintenance of electrical...
5.1 Concepts-This guide summarizes the equipment, field procedures, and data processing methods used to interpret geologic conditions, and to identify and provide locations of geologic anomalies and man-made objects with the GPR method. The GPR uses high-frequency EM waves (from 10 to 3000 MHz) to...
This standard specifies a method of verifying that the locking wire holes in an element of connection are of sufficient strength to meet normal usage. It shall be used together with ISO 2100-100.
Definition-This practice defines acceptable practices and processes for the design, alteration, and certification of electric systems and installations in general aviation aircraft. This practice does not change or create any additional regulatory requirements nor does it authorize changes in or...
This standard specifies a method of assessing the mechanical strength of crimped wire terminations for electrical contacts. It shall be used together with ISO 2100-100.
This European Standard specifies the characteristics of electrical lightweight wires DRA family for use in the on-board 115 V (phase to neutral) or 200 V (phase to phase) AC electrical systems of aircraft at operating temperatures between - 65 °C and 260 °C. These cables are...
This European Standard specifies a method of testing the fire resistance of wire harnesses protected with fire resistant sleeve for aerospace application.
This Standard specifies requirements for preparing and assembling parts to be joined by wire wrapping, as well as the selection, calibration, use and certification of wire wrapping tools. The covered wirewrapped connections are illustrated in Figure 1-1. This type of connection is...
This European Standard specifies methods of measuring the strippability and adherence of the insulation to a conductor of a finished cable. When a particular method is not specified in the detail product specification, method A shall be used. Method B is recommended for wires insulated with...
