Characteristics of aircraft electrical supplies
€115.40
Aerospace series — Heat-resisting nickel base alloy NiCr20Co3Fe3 — Rm = 650 MPa — Sheets and strips, cold rolled — 0,25 mm < a = 3 mm
€68.25
STEEL FE-PM42 - Rm >= 1350 MPa - BARS - De
€15.10
This document specifies the characteristics of screws, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated.Classification: 1 100 MPa1/315 °C2.
€115.50
Heat resisting nickel base alloy NI-P100-HT - Solution treated and precipitation treated - Sheets and strips - a
€30.19
Aerospace series — Cables, electrical, for general purpose — Operating temperatures between -65 °C and 260 °C — Part 011: DZA family, single and multicore assembly for use in low pressure atmosphere — Product standard
Aerospace series — Passivation of corrosion resisting steels and decontamination of nickel or cobalt base alloys
€84.00
Aerospace series — Elements of electrical and optical connection — Test methods — Part 508: Measurement of thickness of coating on contacts
€47.25
Aerospace series — Elements of electrical and optical connection — Test methods — Part 509: Adhesion of coating on contacts
Steel FE-PL78 - 1760 = Rm = 2000 MPa - Bar - De = 75 mm
Steel FE-PL56 - hardened and tempered - 1250 = Rm = 1400 MPa - Bar - De = 70 mm
€25.79
This document specifies the characteristics of electrical wires DZA 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).
Aerospace series — Nut, hexagonal, self-locking, with counterbore and captive washer, in steel, cadmium plated, MoS2 lubricated — Classification: 1 100 MPa (at ambient temperature)/235 °C
The purpose of this ASD-STAN Technical Report is to complement the DOA Guidance Material ASD-STAN TR 9250:2023 Aerospace series — Test organizations — General requirements for test process and capabilities applicable to the qualification of test organizations performing tests necessary to demonstrate compliance with the applicable type-certification basis, ETSO and environmental protection requirements (i.e. certification tests). This DOA Guidance Material shall be used in conjunction with ASD-STAN TR 9250:2023.It provides a means of compliance to EASA Part 21 DOA applicable requirements and/or military equivalent applicable requirements (e. g.: EMAR 21) in:— identifying the relevant DOA requirements;— identifying necessary capabilities and providing guidance for assessment and surveillance;— describing the whole test process from test specification to retention of test data;— addressing the DOA requirements for each step of the process.The requirements of the present ASD-STAN Technical Report should be cascaded to the test organization by the design organization depending on the level of involvement of the test organization.Each clause and subclause of this ASD-STAN Technical Report refers to, and complements when necessary, the corresponding paragraph of ASD-STAN TR 9250:2023.NOTE The definition of design organization is given in Clause 3 of ASD-STAN TR 9250:2023.
Aerospace series — Hexavalent chromium free chemical conversion process of magnesium and magnesium alloys
