Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D = 100 mm, Rm = 900 MPa

UNGÜLTIG herausgegeben am 1.2.2026

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D = 200 mm

UNGÜLTIG herausgegeben am 1.2.2026

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De = 100 mm, Rm = 960 MPa

UNGÜLTIG herausgegeben am 1.2.2026

Aerospace series - Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in heat resisting nickelbase alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 550 MPa (at ambient temperature) / 650°C (Endorsed by AENOR in March of 2003.)

UNGÜLTIG herausgegeben am 1.3.2005

Aerospace series - Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class:100 MPa (at ambient temperature) (Endorsed by AENOR in April of 2003.)

UNGÜLTIG herausgegeben am 1.3.2005

Aerospace series - Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated - Classification: 900 MPa (at ambient temperature)/350 °C (Endorsed by AENOR in April of 2003.)

UNGÜLTIG herausgegeben am 1.3.2005

RESILIENT FLOOR COVERINGS. DETERMINATION OF RESIDUAL INDENTATION AFTER STATIC LOADING.

UNGÜLTIG herausgegeben am 27.7.1995

PRINCIPLES OF CONSTRUCTION AND ADJUSTMENT OF VOLUMETRIC GLASSWARE

UNGÜLTIG herausgegeben am 15.8.1974

LABORATORY GLASSWARE. BURETTES. PART 1: GENERAL REQUIREMENTS.

UNGÜLTIG herausgegeben am 16.12.1991

LABORATORY GLASSWARE. BURETTES. PART 2: BURETTES FOR WHICH NO WAITING TIME IS SPECIFIED.

UNGÜLTIG herausgegeben am 19.2.1991