BS 2S 97:1964
Specification for aircraft material - 21/2 per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 6 in)

Standard No.

BS 2S 97:1964

Release Date

1964

Published By

British Standards Institution (BSI)

Status

Withdraw

Replace By

BS 2S 97:1964+A3:2015

Latest

BS 2S 97:1964+A3:2015

Scope

BRITISH STANDARD SPECIFICATION FOR AIRCRAFT MATERIAL 5/2 PER CENT NICKEL-CHROMIUM-MOLYBDENUM STEEL 1. Inspection and testing procedure. 2. Process of manufacture. 3. Chemical composition. 4. Surface dressing. 5. Condition. 6. Final heat treatment. 7. Mechanical properties.

BS 2S 97:1964 history

• 1964 BS 2S 97:1964+A3:2015 Specification 2½ per cent nickel-chromium-molybdenum steel. (1000/1160 MPa: limiting ruling section 150 mm)
• 1964 BS 2S 97:1964 Specification for aircraft material - 21/2 per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 6 in)