BS 2S 98:1964
Specification for aircraft material - 21/2 per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)

Standard No.

BS 2S 98:1964

Release Date

1964

Published By

British Standards Institution (BSI)

Status

Be replaced 2014-12

Replace By

BS 3S 98:2014

Latest

BS 3S 98:2014

Scope

BRITISH STANDARD SPECIFICATION FOR AIRCRAFT MATERIAL 5/2 PER CENT NICKEL-CHROMIUM-MOLYBDENUM STEEL (HIGH CARBON) 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 98:1964 history

• 2014 BS 3S 98:2014 Specification for 2.5% nickel-chromium-molybdenum (high carbon) steel billets, bars, forging and parts (1 160 - 1 310 MPa: limiting ruling section 155 mm)
• 1964 BS 2S 98:1964 Specification for aircraft material - 21/2 per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)