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BS 7S 80:2002

Current
Current

The latest, up-to-date edition.

High chromium-nickel corrosion resisting steel forging stock, bars, forgings and parts (880 to 1080 MPa: limiting ruling section 100 mm)
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

03-05-2004

Publisher

British Standards Institution

Committees responsible
Foreword
1 Scope
2 Normative reference
3 Technical requirements
Annex A (informative)
Bibliography

Defines the characteristics of a high chromium-nickel corrosion resisting steel, supplied in the form of: forging stock, designation S 80A: forgings, designation S 80C: bar, designation S 80E, black bars, designation S 80B and bright bars, designation S 80D.

This British Standard specifies the characteristics of a high chromium-nickel corrosion resisting steel, supplied in the following forms, and as parts, for aerospace applications.

  1. Forging stock: softened, designation S 80A.
  2. Forgings: De 100 mm, hardened and tempered, designation S 80C.
  3. Bar: softened, designation S 80E.
  4. Black bars: De 100 mm, hardened and tempered, designation S 80B.
  5. Bright bars: De 100 mm, hardened and tempered, designation S 80D.

Committee
ACE/61/-/15
DevelopmentNote
Supersedes BS 6S80(1990) and 00/709810 DC (07/2002) Reviewed and confirmed by BSI, December 2012. (11/2012)
DocumentType
Standard
Pages
10
PublisherName
British Standards Institution
Status
Current
Supersedes

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BS SP119 & SP120(1957) : 1957 HIGH TENSILE STEEL FORK JOINTS (UNIFIED THREADS) - FOR AIRCRAFT
11/30251779 DC : 0 BS 6SP 4:2000+A3 - PINS HEADED, PLAIN SHANK, DRILLED, STEEL ALLOY AND CORROSION RESISTING STEEL WITH A STRENGTH CLASS 880/1080 MPA
BS 2SP 7:1943 Specification for aircraft material. Fork joints (high tensile type) (for sizes No. 4 B.A. to ¾ inch B.S.F. inclusive)
BS 4A114(1999) : 1999 SPECIFICATION FOR CORROSION-RESISTING STEEL, MUSHROOM-HEADED, SLOTTED-DRIVE, BOLTS, STRENGTH CLASS 880 MPA
SBAC TS 220 : 1 TECHNICAL SPECIFICATION FOR UNION NUTS, SELF-LOCKING (UNIFIED THREADS) - HIGH TEMPERATURE NICKEL ALLOY INCONEL 718 CLASSIFICATION R[M] >= 1270 MPA (185000 LBF/IN[2]) @ T[A]/+705 DEGREES C
10/30212959 DC : 0 BS A 400 - SPECIFICATION FOR CORROSION-RESISTING STEEL NUTS, PLAIN AND SLOTTED (UNIFIED HEXAGONS AND UNIFIED THREADS) FOR SHEAR BOLTS FOR AIRCRAFT
BS 4A104(2002) : 2002 AEROSPACE SERIES - SPECIFICATION FOR CORROSION-RESISTING STEEL BOLTS (UNIFIED HEXAGONS AND UNIFIED THREADS), STRENGTH CLASS 880 MPA, FOR AIRCRAFT
15/30281806 DC : 0 BS A 401 TO A 420 - AEROSPACE SERIES - SPECIFICATION FOR SCREWS, PAN AND 100 DEGREES COUNTERSUNK HEAD, HEXALOBULAR DRIVE RECESS (UNIFIED THREADS BELOW 1/4 INCH), VARIOUS MATERIALS
BS 3A117(1962) : 1962 AEROSPACE SERIES - BOLTS, PAN HEAD, SLOTTED DRIVE, UNIFIED THREADS, CORROSION RESISTING STEEL, STRENGTH CLASS 880 MPA, FOR AIRCRAFT - SPECIFICATION
15/30266106 DC : 0 BS 3A 117:1962+A2 - SPECIFICATION FOR CORROSION-RESISTING STEEL PAN HEAD BOLTS (UNIFIEDTHREADS) FOR AIRCRAFT
BS 3A125 TO 3A[...](1981) : 1981 AEROSPACE SERIES - SPECIFICATION FOR STIFFNUTS (UNIFIED THREADS) FOR AIRCRAFT
BS 3A 174:2012 100° Countersunk head, D-slot recess, corrosion-resisting steel bolts (Unified threads), Strength Class 880 MPa, for aircraft
BS A 401-420:2015 Specification for screws, pan and 100° countersunk head, hexalobular drive recess (unified threads below ¼ inch) in various materials

BS 5555:1993 Specification for SI units and recommendations for the use of their multiples and of certain other units
PREN 4500-001 : 200P2 AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 001: GENERAL RULES
BS 5S 100:1993 Procedure for inspection, testing and acceptance of wrought steels (other than plate, sheet, strip and tube)
PREN 4500-005 : 200P2 AEROSPACE SERIES - METALLIC MATERIALS - RULES FOR DRAFTING AND PRESENTATION OF MATERIAL STANDARDS - PART 005: SPECIFIC RULES FOR STEELS

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