ASD-STAN prEN 2699
Aluminium alloy (5086) – Annealed and straightened (H111) – Drawn bar – 6 <or= D <or= 50 mm
Data Sheet by ASD-STAN Standardization, 03/31/1988
NACE ASAE-ASABE B11 CGA ICC CTA
Aluminium alloy (5086) – Annealed and straightened (H111) – Drawn bar – 6 <or= D <or= 50 mm
Data Sheet by ASD-STAN Standardization, 03/31/1988
Titanium TI-P99003 – Not heat treated – Grade 2 forging stock, for annealed forgings – a or D <or= 300 mm
Data Sheet by ASD-STAN Standardization, 09/30/1995
Titanium TI-P99002 – Grade 2 – Annealed – Forgings – De <or= 150 mm
Data Sheet by ASD-STAN Standardization, 09/30/1995
Aluminium alloy AL-C27 – Solution treated and artificially aged (T6) – Structural precision castings
Data Sheet by ASD-STAN Standardization, 10/17/1988
Aerospace series – Receptacle, floating, single lug
Data Sheet by ASD-STAN Standardization, 07/31/2006
Aerospace series-Inserts, MJ threads, self-locking, with self-broaching keys, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated
Data Sheet by ASD-STAN Standardization, 06/01/2008
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) – As forged – Forging stock – a or D <or= 200 mm – 690 MPa <or= Rm <or= 880 MPa
Data Sheet by ASD-STAN Standardization, 08/30/1996
Aerospace series – Connector, electrical and optical, rectangular, modular, rectangular inserts, operating temperature 175deg C (or 125deg C) continuous – Part 133: Size 3 receptacle for rack and panel application – Product standard
Data Sheet by ASD-STAN Standardization, 09/01/2010
Steel FE-CM68 – as manufactured – reference heat treatment : solution treated – Remelting stock
Data Sheet by ASD-STAN Standardization, 03/31/1988
Nuts, anchor, self-locking, fixed, two lug, with counterbore, in heat resisting steel, silver plated – Classification : 1 100 MPa (at ambient temperature) / 425 deg C
Data Sheet by ASD-STAN Standardization, 01/31/1997
Anaerobic polymerisable compounds – Torque strength 16 Nm – Thixotropic index 8
Data Sheet by ASD-STAN Standardization, 01/31/1995
Aerospace series-Weldability and brazeability of materials in aerospace constructions-Part 006: Homogeneous assemblies of titanium alloys
Data Sheet by ASD-STAN Standardization, 07/01/2011