Aerospace series — Unmanned Aircraft Systems — Part 003: Geo-awareness requirements
€68.25
Aerospace series — Cables, electrical, for general purpose — Operating temperatures between -65 °C and 260 °C — Part 012: DZ family, single UV laser printable for use in low pressure atmosphere — Product standard
This document specifies the characteristics of UV laser printable electrical wires DZ family for use in the on board:— 115 VAC (phase to neutral) or 200 VAC (phase to phase) electrical network of aircraft;— 230 VAC (phase to neutral) or 400 VAC (phase to phase) electrical network of aircraft and particularly use in non-pressurized areas.This cable family is used at operating temperature between -65 °C and 260 °C. These cables are demonstrated to be arc resistant for both networks (115 VAC and 230 VAC).
Steel FE-PM44 - hardened and tempered - Bar for machining - De = 150 mm
€25.79
Steel FE-PL1501 (30CrMo12) - Air melted - Hardened and tempered - Bar - De = 40 mm - 1 050 MPa = Rm = 1 250 MPa
€30.19
Aerospace series — Lockwire, drawn — Corrosion resisting steel
Aerospace series — Cable outlet accessories for circular and rectangular electrical and optical connectors — Part 003: Grommet nut, style A — Product standard
€82.40
Aerospace series — Cable outlet accessories for circular and rectangular electrical and optical connectors — Part 004: Cable outlet, style A, straight, unsealed with clamp strain relief — Product standard
€84.00
Aerospace series — Cable outlet accessories for circular and rectangular electrical and optical connectors — Part 005: Cable outlet, style A, 90°, unsealed with clamp strain relief — Product standard
This document specifies the general characteristics, conditions for qualification, acceptance and quality assurance for a fibre optic cable with a bend-insensitive, 50 µm/125 µm Graded Index fibre core, 1,8 mm outside diameter for non pull-proof contact designs.
Aerospace series — Unmanned Aircraft Systems — Part 004: Lighting requirements
This document will provide means of compliance to cover lighting related requirements for Part 2 to 4 of the Annex to the Commission Delegated Regulation (EU) 2019/945 on unmanned aircraft and on third country UAS operators.The purpose is to be able to verify that an UA is equipped with lights:— for the controllability of the UA (the effectiveness of those light is not part of the lighting requirement but is covered by the controllability requirement; therefore its verification is covered by the clause addressing the controllability requirement of EN 4709-001);— that ensure conspicuity of the aircraft at night, the design of the light shall allow a person on the ground to distinguish a UA from a manned aircraft.This document addresses:— definition of types, technical requirements, and technical parameters of UA lights (e.g., position of lights for different UA categories, intensity for different operation modes);— definition of purpose, test procedures, requirements, and compliance rules to evaluate UA lights.
Rod ends, with self-aligning double row ball bearings and threaded shank in steel - Dimensions and loads - Inch series
€52.83
This document specifies the requirements relating to:Steel X4CrNiMo16-5-1 (1.4418)Air meltedHardened and temperedForgingsDe = 200 mm900 MPa = Rm = 1 050 MPafor aerospace applications.NOTE Other common designations:AIR: Z 8 CND 17-04.Only the chemical composition of this document are considered.
Aluminium alloy AL-P7175- T73 - Hand and die forgings - a = 125 mm
