|
BSI-2S-135
|
1977
|
Per Cent Carbon- Chromium Steel Billets, Bars, Forgings and Parts (Limiting Ruling Section 25 mm) (R
|
|
BSI-2S-136
|
1977
|
Per Cent Carbon- Chromium Steel (Vacuum Arc Remelted) Billets, Bars, Forgings and Parts (Limiting Ru
|
|
BSI-2S-137
|
1976
|
High Chromium-Nickel Corrosion-Resisting Steel Bright Bars (Free Machining) (880-1080 MPa; Limiting
|
|
BSI-2S-140
|
1976
|
Amd 2 2 1/2 Per Cent Nickel- Chromium-Molybdenum Steel Billets, Bars, Forgings and Parts (1080-1280
|
|
BSI-2S-142
|
1977
|
Amd 1 1 Per Cent Chromium- Molybdenum Steel Billets, Bars, Forgings and Parts (900-1100 MPa: Limitin
|
|
BSI-2S143
|
1976
|
Amd 4 Chromium-Nickel-Copper-Molybdenum Corrosion- Resisting Steel (Precipitation Hardening) Billets
|
|
BSI-2S-143
|
1386
|
Amd 3 Chromium-Nickel-Copper- Molybdenum Corrosion- Resisting Steel (Precipitation Hardening) Billet
|
|
BSI-2S-146
|
1976
|
Amd 1 4 Per Cent Nickel- Chromium-Molybdenum Air-Hardening Steel (Vacuum Arc Remelted) Billets, Bars
|
|
BSI-2S-147
|
1386
|
Amd 1 0.5 Per Cent Nickel- Chromium-Molybdenum Steel Bars for the Manufacture of Forged Bolts and Fo
|
|
BSI-2S-149
|
1386
|
Amd 1 1.75 Per Cent Nickel- Chromium-Molybdenum Steel Bars for the Manufacture of Forged Bolts and F
|
|
BSI-2S-513
|
1970
|
Spring Steel Strip (Replaces BS S 513: 1956)
|
|
BSI-2SP-1
|
1927
|
Amd 4 Shackles (Replaces BS SP 1: 1916)
|
|
BSI-2SP-105
|
1955
|
Amd 3 Swaged Cable-End Assemblies (UNF Threads) for Preformed Steel Wire Rope (W.9) for Aircraft (Re
|
|
BSI-2SP-106
|
1955
|
Amd 3 Swaged Cable-End Assemblies (UNF Threads) for Preformed Non- Corrodible Steel Wire Rope (W.11)
|
|
BSI-2SP-142-143
|
1973
|
Solid Rivets with 100 Degree Countersunk Truncated Radiused Head Made from L 86 (Sp 142) and L 37 (S
|
|
BSI-2SP-148-150
|
1979
|
Unified Aluminium Alloy Washers (Replaces BS SP 148-50: 1970)
|
|
BSI-2SP-151-153
|
1979
|
Unified Alloy Steel Washers (Replaces BS SP 151-53: 1970)
|
|
BSI-2SP-154-156
|
1979
|
Unified Corrosion- Resistant Steel Washers (Replaces BS SP 154-56: 1970)
|
|
BSI-2SP-157-163
|
1973
|
Amd 2 Solid Rivets with Universal Head Made from L 86 (SP 157 and SP 163), L 58 (SP 160 and SP 161),
|
|
BSI-2SP-47
|
1957
|
Single Coil Spring Washers for Aircraft (Replaces BS SP 47: 1952)
|
|
BSI-2SP-7
|
1943
|
Fork Joints (High Tensile Type) (Replaces BS SP 7: 1929)
|
|
BSI-2SP-77-80
|
1973
|
Snap Head Aluminium and Aluminium Alloy Rivets for Aircraft (Replaces BS SP 77 to SP 80: 1958)
|
|
BSI-2SP-81-82
|
1973
|
Snap Head High Nickel- Copper Alloy Rivets for Aircraft (Replaces BS SP 81 and SP 82: 1958)
|
|
BSI-2SP-83-85
|
1973
|
Mushroom Head Aluminium Alloy Rivets for Aircraft (Replaces BS SP 83 to SP 85: 1958)
|
|
BSI-2SP-87-88
|
1973
|
Degree Countersunk Head High Nickel-Copper Alloy Rivets for Aircraft
|
|
BSI-2SP-91-92
|
1973
|
Amd 3 Carbon Steel Worm Drive Clamps for Aircraft (Replaces BS SP 91 and SP 92: 1962)
|
|
BSI-2SP-93
|
1974
|
Amd 1 Elastomeric Grommets (Acrylonitrile- Butadiene) for Aerospace Use (Replaces BS SP 93: 1962)
|
|
BSI-2SP-95
|
1974
|
Amd 1 Elastomeric Grommets (Polychloroprene) for Aerospace Use (AMD 3515) February 27, 1981 (Replace
|
|
BSI-2SP-96
|
1982
|
Internal Retaining Rings (Imperial Sizes) (Replaces BS SP 96: 1968)
|
|
BSI-2T-66
|
1386
|
Amd 1 18/10 Chromium-Nickel Corrosion-Resisting Steel Tube (Niobium Stabilized: 550 MPa) (Weldable)
|
|
BSI-2T-68
|
1980
|
Cold Drawn 18/10 Chromium-Nickel Corrosion-Resisting Steel Tube (Niobium Stabilized: 800 N/Square mm
|
|
BSI-2TA-1
|
1974
|
Amd 3 Sheet and Strip of Commercially Pure Titanium - (Tensile Strength 290-420 MPa) AMD 10738; Apri
|
|
BSI-2TA-10
|
1974
|
Amd 2 Sheet of Titanium- Aluminium-Vanadium Alloy (Tensile Strength 960-1270 MPa) (Replaces BS TA 10
|
|
BSI-2TA-100
|
1973
|
Amd 5 Procedure for Inspection and Testing of Wrought Titanium and Titanium Alloys AMD 10739; June 2
|
|
BSI-2TA-11
|
1974
|
Bar and Section for Machining of Titanium- Aluminium-Vanadium Alloy (Tensile Strength 900 1160 MPa)
|
|
BSI-2TA-12
|
1974
|
Forging Stock of Titanium-Aluminium- Vanadium Alloy (Tensile Strength 900-1160 MPa Limiting Ruling S
|
|
BSI-2TA-13
|
1974
|
Forgings of Titanium- Aluminum-Vanadium Alloy (Tensile Strength 900-1160 MPa) (Limiting Ruling Secti
|
|
BSI-2TA-2
|
1973
|
Amd 3 Sheet and Strip of Commercially Pure Titanium - (Tensile Strength 390-540 N/mm2) AMD 10740; Ap
|
|
BSI-2TA-21
|
1973
|
Amd 2 Sheet and Strip of Titanium-Copper Alloy (Tensile Strength 540- 770 N/Square mm) (Replaces BS
|
|
BSI-2TA-28
|
1974
|
Amd 3 Forging Stock and Wire of Titanium-Aluminium- Vanadium Alloy (Tensile Strength 1100-1300 MPa)
|
|
BSI-2TA-6
|
1973
|
Amd 3 Specification for Sheet and Strip of Commercially Pure Titanium - (Tensile Strength 570-730 n/
|
|
BSI-2TA-7
|
1973
|
Bars and Sections for Machining of Commercially Pure Titanium (Tensile Strength 540-740 N/ Square mm
|
|
BSI-2V-35
|
1966
|
Plywood for Aeronautical Purposes (Replaces BS V 35: 1947)
|
|
BSI-2V-37
|
1968
|
Sitka Spruce as Finished Timber (Replaces BS V 37: 1952)
|
|
BSI-2W-11
|
1967
|
Preformed Corrosion- Resisting Steel Wire Rope (Replaces BS W 11: 1946)
|
|
BSI-2W-12
|
1989
|
Preformed Zinc Coated Carbon Steel Wire Rope (Metric And Inch Series) (Replaces BS W 12: 1968 and BS
|
|
BSI-2X-26
|
2001
|
Doping and Finishing Schemes for Fabric Covered Aircraft (S)
|
|
BSI-2X-27
|
1991
|
Cellulose Finishing Scheme for Aerospace Purposes (Replaces BS X 27: 1966 and BS X 30: 1966)
|
|
BSI-2X-32
|
1998
|
Pretreatment Etch Primer for Aerospace Purposes Supersedes X 32: 1991; (S)
|
|
BSI-2X-33
|
1998
|
Two Component Epoxy Primer for Aerospace Purposes Supersedes X 33: 1991; (S)
|
