Transformer rectifier units for aircraft -- Part 001 -- Technical specification
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Aerospace Series Transformer Rectifier Units for Aircraft Part 001: Technical Specification
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Aerospace Series Bolts, Normal Hexagonal Head, Close Tolerance Normal Shank, Short Thread, in Titanium Alloy, Aluminium IVD Coated Classification : 1 100 MPa (at Ambient Temperature)/425 Degrees C
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Aerospace Series Bolts, Normal Hexagonal Head, Close Tolerance Normal Shank, Short Thread, in Titanium Alloy, Aluminium IVD Coated Classification : 1 100 MPa (at Ambient Temperature) / 425 Degrees C
Document status: [ Revised ]
Aerospace series Screws, 100° countersunk normal head, offset cruciform recess, close tolerance shank, short thread, in titanium alloy, aluminium IVD coated Classification: 1 100 MPa (at ambient temperature) / 425 °C
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Aerospace series Screws, pan head, six lobe recess, coarse tolerance shank, medium length thread, in alloy steel, cadmium plated Classification: 1 100 MPa (at ambient temperature) / 235 °C
Document status: [ Revised ]
Aerospace series — Screw, pan head, hexalobular recess, coarse tolerance shank, medium length thread, in alloy steel, cadmium plated — Classification: 1 100 MPa (at ambient temperature) / 235 °C
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Aerospace series — Screw, pan head, offset cruciform recess, threaded to head, in corrosion resisting steel, passivated, metric — Classification: 490 MPa (at ambient temperature)/425 °C
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Aerospace Series Screws, Pan Head, Offset Cruciform Recess, Threaded to Head, in Corrosion Resisting Steel, Passivated Classification : 490 MPa (at Ambient Temperature)/425 Degrees C
Document status: [ Revised ]
Screws, pan head, slotted, threaded to head, in corrosion resisting steel, passivated - Classification: 490 MPa (at ambient temperature)/425 deg C
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