HEAT RESISTING NICKEL BASE ALLOY NI-P91-HT - Rp0,2 >or= 310 MPa - SHEETS AND STRIPS 0,25 mm < a <or= 3 mm

Aluminium alloy (5086) - Annealed and straightened (H111) - Drawn bar - 6 <or= D <or= 50 mmData Sheet by ASD-STAN Standardization,

Steel FE-PL75 - 1250 MPa <or= Rm <or= 1400 MPa - Forgings De <or= 40 mm - Aerospace SeriesData Sheet by ASD-STAN

Aerospace series-Lamps, incandescent-Part 094: Lamp, code 8022-Product StandardData Sheet by ASD-STAN Standardization, 10/01/1996

Test methods for transparent materials for aircraft glazing -- Part 22: Determination of thermal relaxation of stretched acrylic sheetData Sheet by ASD-STAN

Steel FE-PM37 - 900 MPa <or= Rm <or= 1100 MPa - Sheet a <or= 6 mm - Aerospace SeriesData Sheet by ASD-STAN

Aerospace series - Steel FE-PM3501 (X105CrMo17) - Hardened and tempered - Bars D < or = 150 mmData Sheet by ASD-STAN Standardization,

Glass fibre thermosetting preimpregnates - Technical specification - Part 5 : Glass fabric/phenolic resin preimpregnateData Sheet by ASD-STAN Standardization, 10/31/2001

Aluminium alloy Al-C26-T6 - Chill castingsData Sheet by ASD-STAN Standardization, 04/22/1986

Steel FE-PL61 - Carburized, hardened and tempered - Bar De <or= 40 mmData Sheet by ASD-STAN Standardization, 04/22/1986

HEAT AND CRAZING RESISTANT ACRYLIC SHEETS FOR AIRCRAFT GLAZING - TECHNICAL SPECIFICATION -- AEROSPACE SERIESData Sheet by ASD-STAN Standardization, 01/01/1982

Steel FE-PL1504 (33CrMoV12) - Air Melted - Hardened and Tempered - Forgings - De <or= 80 mm 1 200 MPa <or= Rm