Specification for aircraft material. ´40´ carbon steel bright bars for machining (45-55 tonf/sq in: limiting ruling section 1 inch) (primarily intended for the manufacture of nuts).

UNGÜLTIG herausgegeben am 31.1.1964

Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 21/2 inches).

UNGÜLTIG herausgegeben am 8.6.1964

Specification for aircraft material. ´40´ carbon steel bright bars for machining (55-65 tonf/sq in: limiting ruling section 3/4 inch) (primarily intended for the manufacture of machined bolts).

UNGÜLTIG herausgegeben am 31.1.1964

Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 11/8 inch).

UNGÜLTIG herausgegeben am 31.1.1964

Specification for aircraft material. 11/2 per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 21/2 in).

UNGÜLTIG herausgegeben am 31.1.1964

Specification for aircraft material. 21/2 per cent nickel-chromium-molybdenum steel (oil hardening) (100 tonf/sq in: limiting ruling section 21/2 in).

UNGÜLTIG herausgegeben am 31.1.1964

Specification for aircraft material. 12 per cent chromium corrosion-resisting steel (free machining) (45/55 tonf/sq in: limiting ruling section 6 in).

UNGÜLTIG herausgegeben am 31.1.1964

Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) billets, bars, forgings and parts (1130-1330 MPa).

UNGÜLTIG herausgegeben am 31.8.1976

Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel (precipitation hardening) billets, bars, forgings and parts (1270-1470 MPa).

UNGÜLTIG herausgegeben am 31.8.1976

Inspection and testing procedure for steel sheet and strip.

UNGÜLTIG herausgegeben am 12.8.1969