NA 131
DIN Standards Committee Aerospace
DIN 65209 [CURRENT] references following documents:
| Document number | Edition | Title |
|---|---|---|
| DIN EN 2092 | 2006-10 | Aerospace series - Aluminium alloy AL-P7075-T6 or T62 - Clad sheet and strip - 0,4 mm ≤ a ≤ 6 mm; German and English version EN 2092:2005 More |
| DIN EN 2424 | 2008-10 | Aerospace series - Marking of aerospace products; German and English version EN 2424:2008 More |
| DIN EN 2696 | 2006-10 | Aerospace series - Aluminium alloy AL-P7075-T6 or T62 - Sheet and strip - 0,4 mm ≤ a ≤ 6 mm; German and English version EN 2696:2005 More |
| DIN ISO 2768-1 | 1991-06 | General tolerances; tolerances for linear and angular dimensions without individual tolerance indications; identical with ISO 2768-1:1989 More |
| WL 1.4544-1 | 1982-03 | Stainless austenitic chromium-nickel steel with about 0.05C-18Cr-10Ni-0.4Ti; sheets, plates and strips More |
| WL 1.4546-1 | 1982-03 | Stainless austenitic chromium-nickel steel with about 0.05C-18Cr-10Ni-0.6Nb; rods and forgings More |
| WL 1.4943-1 | 1992-08 | Aerospace; heat-resisting precipitation-hardening nickel-chromium-titanium steel with approx. 0,03 C, 25 Ni, 15 Cr, 1,8 Ti, consumable electrode remelted; sheet, plate and strip More |
| WL 1.4943-2 | 1992-08 | Aerospace; heat-resisting precipitation-hardening nickel-chromium-titanium steel with approx. 0,03 C, 25 Ni, 15 Cr, 1,8 Ti, consumable elektrode remelted; bars and forgings More |
| WL 1.4944-1 | 1982-03 | High temperature precipitation-hardening nickel-chromium-titanium steel with about 0.06C-25Ni-15Cr-2.1Ti-1.2Mo; sheets, strips and plates More |
| WL 1.7214-1 | 1992-03 | Aerospace; weldable hardened and tempered chromium-molybdenum steel with approx. 0,25C-1Cr-0,2Mo; sheet, plate and strip More |
