BSI - Electronics and Aerospace - Historical Collection
This collection contains documents from the following standards organization(s): British Standards Institution
| BSI BS S 151 | EN-Chromium-nickel-molybdenum-vanadium heat-resisting steel billets bars forgings and parts - (930-1130 MPa: limiting ruling section 150 mm) - (Cr 12 Ni 2.5 Mo 1.7 V 0.3) | |
| BSI BS S 151 | EN-Chromium-Nickel- Molybdenum-Vanadium Heat-Resisting Steel Billets Bars Forgings and Parts (930-1130 MPa: Limiting Ruling Section 150 mm) (Cr 12 Ni 2.5 Mo 1.7 V 0.3)-Amd 1; | |
| BSI BS S 152 | EN-Specification for Chromium-cobalt- molybdenum- vanadium-niobium heat-resisting steel billets bars forgings and parts (consumable electrode remelted) (1 000 - 1 140 MPa) (Cr 10.5 Co 6 Mo 0.8 V 0.2 Nb | |
| BSI BS S 152 | EN-Chromium-Cobalt- Molybdenum-Vanadium- Niobium Heat-Resisting Steel Billets Bars Forgings and Parts (Consumable Electrode Remelted)(1000-1140 MPa) (Cr 10.5 Co 6 Mo 0.8 V 0.2 Nb 0.3)-Amd 1; | |
| BSI BS S 162 | EN-18 Percent Nickel- Cobalt-Molybdenum Maraging Steel for Forging Stock Forgings Bars and Parts (1800 MPa: Double Vacuum Melted) (AMD 6373) July 31 1991-Amd 1; | |
| BSI BS S 164 | EN-1 % Chromium-Molybdenum Steel Billets Bars Forgings and Parts. (1 150 to 1 300 MPa: Limiting Ruling Section 16 mm) (Suitable for Welding)-Superseding DTD 5082; | |
| BSI BS S 201 | EN-Patented Cold Drawn Carbon Steel Wire and Springs (High Duty Unground Wire)-AMD 531: June 1970 | |
| BSI BS S 201 | EN-Patented cold drawn carbon steel wire and springs (High duty unground wire)-AMD 531: June 1970; Superseding Ministry of Technology Specification D.T.D 215A; Superseded by BS 2S 201:2004 | |
| BSI BS S 202 | EN-Specification for Patented cold drawn carbon steel wire and springs - (High duty ground wire)-AMD 530: June 1970 | |
| BSI BS S 203 | EN-Carbon Steel Wire and Springs (High Duty Unground Wire; Hardened and Tempered) | |
| BSI BS S 204 | EN-Specification for Chromium-vanadium steel wire and springs - (High duty ground wire - hardened and tempered) | |
| BSI BS S 205 | EN-Specification for Austenitic chromium-nickel steel wire and springs | |
| BSI BS S 524 | EN-Specification for cold-rolled 18/10 chromium-nickel corrosion-resisting steel sheet and strip (titanium stabilized: 80 hbar)-Supersedes in part BS S 520; AMD 5559: July 1987; | |
| BSI BS S 525 | EN-Specification for cold-rolled 18/10 chromium-nickel corrosion-resisting steel sheet and strip (niobium stabilized: 80 hbar)-AMD 5560: July 1987; Supersedes in part BS S 520; | |
| BSI BS S 526 | EN-Specification for softened 18/10 chromium-nickel corrosion-resisting steel sheet and strip (titanium stabilized: 54 hbar)-AMD 4254: April 1983; Supersedes in part BS S 521; | |
| BSI BS S 527 | EN-Specification for softened 18/10 chromium-nickel corrosion-resisting steel sheet and strip (niobium stabilized: 54 hbar)-AMD 4255: April 1983; Supersedes in part BS S 521; | |
| BSI BS S 528 | EN-23/14 Chromium-Nickel Heat-Resisting Steel Sheet and Strip (Titanium Stabilized: 54 Hbar) (Elevated Temperature Properties Not Verified)-Replaces BS S 521: 1956; | |
| BSI BS S 529 | EN-23/14 Chromium-Nickel Heat-Resisting Steel Sheet and Strip (Niobium Stabilized: 54 Hbar) Elevated Temperature Properties Not Verified)-Replaces BS S 521: 1956; | |
| BSI BS S 530 | EN-Specification for 24/17 chromium-nickel heat-resisting steel sheet and strip (titanium stabilized: 54 hbar) (elevated temperature properties not verified)-Supersedes in part BS S 523; | |
| BSI BS S 531 | EN-24/17 Chromium-Nickel Heat-Resisting Steel Sheet and Strip (Niobium Stabilized: 54 Hbar) (Elevated Temperature Properties Not Verified)-Replaces BS S 523: 1956; | |
| BSI BS S 532 | EN-Specification for chromium-nickel-copper-molybdenum corrosion-resisting steel sheet and strip (precipitation hardening: 98/118 hbar)-AMD 4256: April 1983; | |
| BSI BS S 534 | EN-Specification for chromium-molybdenum steel sheet and strip (88/108 hbar) (suitable for welding)-Supersedes BS S 518; | |
| BSI BS S 535 | EN-Specification for chromium-molybdenum steel sheet and strip (115/130 hbar) (suitable for welding)-Supersedes BS S 519; | |
| BSI BS S 536 | EN-Specification for low carbon 18/10 chromium-nickel corrosion-resisting steel sheet and strip (50 hbar) | |
| BSI BS S 537 | EN-Specification for low carbon 17/12 chromium-nickel-molybdenum corrosion-resisting steel sheet and strip (50 hbar) | |
| BSI BS S 537 | EN-Low Carbon 17/12 Chromium-Nickel- Molybdenum Corrosion- Resisting Steel Sheet and Strip (50 Hbar) | |
| BSI BS S 538 | EN-Chromium-Cobalt- Molybdenum-Vanadium Heat-Resisting Steel Sheet and Strip (930- 1130 MPa: Maximum Thickness 6 mm) (Cr 12 Co 2.5 Mo 1.7 V 0.3) | |
| BSI BS SP 107-112 | EN-Tab Washers for Unified Hexagons for Aircraft-Amd 2; | |
| BSI BS SP 114 | EN-Eye Bolts (Unified Threads) for Aircraft (AMD 3350) July 31 1980-Amd 3; | |
| BSI BS SP 114 | EN-Specification for Eye bolts (unified threads) for aircraft-AMD 4081: February 1961; AMD 1800: August 1975; AMD 3350: July 1980; AMD NO 4: January 2008 | |
| BSI BS SP 118 | EN-Tie Rods (Unified Threads) for Aircraft-Amd 1; | |
| BSI BS SP 119-120 | EN-High Tensile Steel Fork Joints-Amd 1; | |
| BSI BS SP 121 | EN-Collars for Shear Pins for Aircraft | |
| BSI BS SP 128-133 | EN-Wood Screws for Aircraft-AMD 2013: June 30 1976; Supersedes BS SP 61 to 64: 1955 | |
| BSI BS SP 141 | EN-Design and Performance Requirements for Toggle Type Panel Fasteners | |
| BSI BS SP 164 | EN-Specification for Design and Performance Requirements for Turnlock Stud-Type Panel Fasteners (Metric Series) | |
| BSI BS SP 33-39 | EN-Turnbarrels Tension Rods and Swaged Cable- End Connections for Aircraft-AMD 2399:February 1956; AMD 4086:February 1961; AMD 2753:November 1978 | |
| BSI BS SP 41-46 | EN-Tab Washers for Aircraft-Amd 2; | |
| BSI BS SP 49-50 | EN-Ball Ends for Swaging on Cable for Aircraft | |
| BSI BS SP 51-52 | EN-Identification Tags for Swaged Cable-End Assemblies for Aircraft-Amd 2; | |
| BSI BS SP 53 | EN-Swaged Cable-End Assemblies (B.A. and B.S.F. Threads) for Preformed Steel Wire Rope for Aircraft-Amd 3; | |
| BSI BS SP 54 | EN-Swaged Cable-End Assemblies (B.A. and B.S.F. Threads) for Preformed Non-Corrodible Steel Wire Rope-Amd 4; | |
| BSI BS SP 57 & 58 | EN-Rivet Burrs for Aircraft (AMD 4700) March 29 1985-Amd 1; | |
| BSI BS SP 59-60 | EN-Spring Catches for Aeronautical Purposes | |
| BSI BS SP 61-64 | EN-British Standard Specifications for Wood Screws for Aircraft | |
| BSI BS SP 66-67 | EN-Cable Thimbles for Aircraft-PD 2578: September 6 1956 | |
| BSI BS SP 76 | EN-Snap Head Steel Rivets for Aircraft | |
| BSI BS SP 86 | EN-100 Degree Countersunk Head Steel Rivets for Aircraft-PD 4087: February 15 1961; AMD 473: March 15 1970 | |
| BSI BS SP 90 | EN-Corrosion-Resisting Steel Split Cotter Pins for Aircraft-AMD 5378: October 1964; AMD 484: April 1970; AMD 642: November 1970 | |
| BSI BS SP 94 | EN-Bronze Oil-Retaining Bushes and Thrust Washers for Aircraft-Amd 1; | |
| BSI BS T 72 & 73 | EN-18/10 Chromium-Nickel Corrosion-Resisting Steel Tube for Hydraulic Purposes (Niobium/ Titanium Stabilized: 550 MPa) | |
| BSI BS TA 38 | EN-Bar for Machining of Titanium-Aluminium- Molybdenum-Tin-Silicon- Carbon Alloy (Tensile Strength 1250-1420 N/Square mm) (Limiting Ruling Section 25 mm) | |
| BSI BS TA 39 | EN-Forging Stock of Titanium-Aluminium- Molybdenum-Tin-Silicon- Carbon Alloy (Tensile Strength 1250-1420 N/ Square mm) (Limiting Ruling Section 25 mm) | |
| BSI BS TA 40 | EN-Bars for Machining of Titanium-Aluminium- Molybdenum-Tin-Silicon- Carbon Alloy (Tensile Strength 1205-1375 N/ Square mm) (Limiting Ruling Section over 25 mm up to and Including 75 mm) | |
| BSI BS TA 41 | EN-Forging Stock of Titanium-Aluminium- Molybdenum-Tin-Silicon- Carbon Alloy (Tensile Strength 1205-1375 N/ Square mm) (Limiting Ruling Section over 25 mm up to and Including 75 mm) | |
| BSI BS TA 42 | EN-Forgings of Titanium- Aluminium-Molybdenum- Tin-Silicon-Carbon Alloy (Tensile Strength 1205- 1375 N/Square mm) (Limiting Ruling Section over 25 mm up to and Including 75 mm) | |
| BSI BS TA 45 | EN-Bar and Section for Machining of Titanium- Aluminium-Molybdenum- Tin-Silicon Alloy (Tensile Strength 1100- 1280 N/Square mm) (Limiting Ruling Section 25 mm)-Amd 1; | |
| BSI BS TA 46 | EN-Bar and Section for Machining of Titanium- Aluminium-Molybdenum- Tin-Silicon Alloy (Tensile Strength 1050- 1220 N/Square mm) (Limiting Ruling Section over 25 mm up to and Including 100 mm)-Amd 1; | |
| BSI BS TA 47 | EN-Forging Stock of Titanium-Aluminium- Molybdenum-Tin-Silicon Alloy (Tensile Strength 1050-1220 N/Square mm) (Limiting Ruling Section 100 mm)-Amd 1; | |
| BSI BS TA 48 | EN-Forgings of Titanium- Aluminium-Molybdenum- Tin-Silicon Alloy (Tensile Strength 1050- 1200 N/Square mm) (Limiting Ruling Section 100 mm)-Amd 1; | |
| BSI BS TA 49 | EN-Bar and Section for Machining of Titanium- Aluminium-Molybdenum- Tin-Silicon Alloy (Tensile Strength 1000 1200 N/Square mm) (Limiting Ruling Section over 100 mm up to and Including 150 mm)-Amd 1; | |
| BSI BS TA 50 | EN-Forging Stock of Titanium-Aluminium- Molybdenum-Tin-Silicon Alloy (Tensile Strength 1000-1200 N/ Square mm (Limiting Ruling Section over 100 mm up to and Including 150 mm)-Amd 1; | |
| BSI BS TA 51 | EN-Forgings of Titanium- Aluminium-Molybdenum- Tin-Silicon Alloy (Tensile Strength 1000- 1200 N/Square mm) (Limiting Ruling Section over 100 mm Up to and Including 150 mm)-Amd 1; | |
| BSI BS TA 52 | EN-Sheet and Strip of Titanium-Copper Alloy (Tensile Strength 690- 920 N/Square mm)-Amd 2; | |
| BSI BS TA 56 | EN-Plate of Titanium- Aluminium-Vanadium Alloy (Tensile Strength 895-1150 MPa) (Maximum Thickness 100 mm)-AMD 3756: September 1981 | |
| BSI BS TA 57 | EN-Plate of Titanium- Aluminium-Molybdenum- Tin-Silicon (Tensile Strength 1030-1220 MPa) (Maximum Thickness 65 mm)-Amd 1; | |
| BSI BS TA 58 | EN-Plate of Titanium- Copper Alloy (Tensile Strength 520-640 MPa) (Maximum Thickness 10 mm) (AMD 5464) April 30 1987-Amd 2; | |
| BSI BS TA 59 | EN-Sheet amd Strip of Titanium-Aluminium-Vanadium Alloy (Tensile Strength 920 MPa to 1180 MPa)-Amd 2; | |
| BSI BS X 26 | EN-Doping and Finishing Schemes for Fabric Covered Aircraft | |
| BSI BS X 27 | EN-Cellulose Finishing Scheme for Aeronautical Purposes | |
| BSI BS X 28 | EN-Matt Synthetic Finishing Scheme for Aeronautical Purposes | |
| BSI BS X 29 | EN-High Gloss Finishing Scheme for Aeronautical Purposes | |
| BSI BS X 30 | EN-Light-Weight Aluminium Finishing Scheme (Cellulose Base) for Aeronautical Purposes | |
| BSI BS X 31 | EN-Low Temperature Stoving Scheme for Aeronautical Purposes | |
| BSI BS X 32 | EN-Specification for Pretreatment primer for aerospace purposes | |
| BSI BS X 33 | EN-Two Component Epoxy Primer for Aerospace Purposes-AMD 7164: May 1 1992 | |
| BSI BS X 33 | EN-Two Component Epoxy Primer for Aerospace Purposes | |
| BSI BS X 34 | EN-Specification for Air Drying Two Component Polyurethane Finish for Aerospace Purposes | |
| BSI BS X 34 | EN-Specification for Air Drying Two Component Polyurethane Finish for Aerospace Purposes-AMD 7518: January 15 1993 |