ASD-STAN prEN 2388
ALUMINIUM ALLOY 2024- T351 -- TUBES FOR STRUCTURES 0,6 mm <or= a <or=12,5 mm -- AEROSPACE SERIESData Sheet by ASD-STAN Standardization, 09/01/1981
ALUMINIUM ALLOY 2024- T351 -- TUBES FOR STRUCTURES 0,6 mm <or= a <or=12,5 mm -- AEROSPACE SERIESData Sheet by ASD-STAN Standardization, 09/01/1981
HEAT RESISTING NICKEL BASE ALLOY NI-P91-HT - ANNEALED - BARS -- AEROSPACE SERIESData Sheet by ASD-STAN Standardization, 05/01/1980
Metallic materials - Test methods - Part 16: Non-destructive testing - Penetrant testingData Sheet by ASD-STAN Standardization, 01/31/2000
Aerospace series - Chloroprene rubber (CR) Heat resistance - Hardness 50 IRHDData Sheet by ASD-STAN Standardization, 07/31/2011
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 412: Humidity resistanceData Sheet by ASD-STAN Standardization, 02/01/2020
Nuts, bihexagonal, self-locking, with counterbore, in heat resisting nickel base alloy, passivated, MoS2 lubricated - Classification : 1 550 MPa (at ambient
Steel FE-PL56 - hardened and tempered - 1250 <or= Rm <or= 1400 MPa - Forging - De <or= 70 mmData Sheet by
Burning behaviour of non metallic materials under the influence of radiating heat and flames - Determination of smoke density and gas components
Heat resisting nickel base alloy (Ni-P101HT) - cold worked and solution treated - Bar for machining for fasteners 3 <or= D <or=
Polycarbonat sheet -- Technical specificationData Sheet by ASD-STAN Standardization, 07/31/2001
Aerospace series - Steel X12CrNiMoV12-3 (1.4938) - Air melted and consumable electrode remelted - Hardened and tempered - Bars - De <
Aerospace series - Cables, optical 125 micrometers diameter cladding - Part 301: Tight structure 50/125 micrometers GI, fibre nominal 1,8mm, outside diameter