|
DIN EN 3476 |
Aerospace series - Steel FE-PL1501 (30CrMo12) - Air melted - Softened - Forging stock - a or D =300 mm; German and English version EN 3476:2006 |
|
DIN EN 3477 |
(DRAFT) Aerospace series - Steel FE-PM3503 (X7CrNiMo15-7-3) - Air melted, solution treated and precipitation treated - Plate 6 mm < a ≤ 15 mm, 1310 MPa ≤ Rm ≤ 1550 MPa |
|
DIN EN 3479 |
Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) - Consumable electrode remelted - Solution treated and precipitation treated - Plate - 6 mm < a = 20 mm - 1070 MPa = Rm = 1220 MPa; German and English version EN 3479:2007 |
|
DIN EN 3490 |
Aerospace series - Steel FE-PM3901 (X15CrNi17-3) - Air melted - Hardened and tempered - Bar for machining - De = 200 mm - 900 MPa = Rm = 1100 MPa; German and English version EN 3490:2007 |
|
DIN EN 3491 |
Aerospace series - Steel FE-PM3901 (X15CrNi17-3) - Air melted - Hardened and tempered - Forgings - De = 100 mm - 900 MPa = Rm = 1100 MPa; German and English version EN 3491:2006 |
|
DIN EN 3494 |
(DRAFT) Aerospace series - Titanium alloy TI-P19001 - Grade 2, solution treated and aged, forgings De ≤ 75 mm |
|
DIN EN 3495 |
(DRAFT) Aerospace series - Titanium alloy TI-P19001 - Grade 2, annealed, forgings De ≤ 150 mm |
|
DIN EN 3496 |
(DRAFT) Aerospace series - Titanium TI-P99003 - Grade 2, annealed, forgings De ≤ 150 mm |
|
DIN EN 3497 |
(DRAFT) Aerospace series; titanium TI-P99001; annealed, sheet and strip, cold rolled, a ≤ 3 mm, 290 MPa ≤Rm ≤ 420 MPa |
|
DIN EN 3498 |
(DRAFT) Aerospace series; titanium TI-P99002; annealed, sheet and strip, cold rolled, a ≤ 3 mm, 390 MPa ≤ Rm ≤ 540 MPa |
|
DIN EN 3499 |
(DRAFT) Aerospace series; titanium TI-P99003; annealed, sheet and strip, cold rolled, a ≤ 3 mm, 570 MPa ≤ Rm ≤ 730 MPa |
|
DIN EN 3504 |
(DRAFT) Aerospace series; titanium and titanium alloys; circular tubes for fluids; close tolerances; diameter 3,2 mm ≤ D ≤ 50 mm, thickness 0,25 mm ≤ a ≤ 2 mm; dimensions |
|
DIN EN 3506 |
Aerospace series - Hot rolled sheets and plates in heat resisting alloys - Thickness 2,0 mm ≤ a ≤ 100 mm; Dimensions; German and English version EN 3506:2001 |
|
DIN EN 3510 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) solution treated and precipitation treated - Bar and section De ≤ 100 mm |
|
DIN EN 3515 |
(DRAFT) Aerospace series - Steel FE-PL8201 (41NiCrMo2), air melted, hardened and tempered - Hand and die forgings De ≤ 25 mm, 1100 MPa ≤ Rm ≤ 1300 MPa |
|
DIN EN 3516 |
(DRAFT) Aerospace series - Steel FE-PL8201 (41NiCrMo2), air melted, softened - Forging stock a or D ≤ 300 mm |
|
DIN EN 3517 |
(DRAFT) Aerospace series - Steel FE-PL2105 - Air melted; hardened and tempered; bar for machining De ≤ 150 mm, 1080 MPa ≤ Rm ≤ 1280 MPa |
|
DIN EN 3519 |
(DRAFT) Aerospace series - Steel FE-PL2105 - Air melted; hardened and tempered; bar for machining De ≤ 150 mm, 880 MPa ≤ Rm ≤ 1080 MPa |
|
DIN EN 3520 |
(DRAFT) Aerospace series - Steel FE-PL2105 - Air melted; softened; forging stock a or D ≤ 300 mm |
|
DIN EN 3523 |
Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bar for machining - De = 100 mm - 1080 MPa = Rm = 1280 MPa; German and English version EN 3523:2007 |
|
DIN EN 3524 |
Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Sheet and strip - 2 mm = a = 6 mm - 1080 MPa = Rm = 1280 MPa; German and English version EN 3524:2007 |
|
DIN EN 3525 |
Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Plate - 6 mm < a = 20 mm - 1080 MPa = Rm = 1280 MPa; German and English version EN 3525:2007 |
|
DIN EN 3526 |
Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Sheet and strip - 0,5 mm = a = 6 mm - 980 MPa = Rm = 1180 MPa; German and English version EN 3526:2007 |
|
DIN EN 3527 |
Aerospace series - Steel FE-PL1504 (33CrMoV12) - Air melted - Softened - Forging stock - a or D = 300 mm; German and English version EN 3527:2007 |
|
DIN EN 3531 |
Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Sheet and strip - a = 6 mm - 1 750 MPa = Rm = 2 000 MPa; German and English version EN 3531:2007 |
|
DIN EN 3532 |
Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Plate - 6 mm < a = 40 mm - 1 750 MPa = Rm = 2 000 MPa; German and English version EN 3532:2007 |
|
DIN EN 3536 |
(DRAFT) Aerospace series - Nuts, hexagon, self-locking, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 3537 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, fixed, two lug, with counterbore, in heat resisting steel, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 3538 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, fixed, two lug, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 3539 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, one lug, fixed, with counterbore, in heat resisting steel, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 3542 |
Aerospace series - Inserts, screw thread, helical coil, self-locking, in heat resisting nickel base alloy NI-PH2801 (Inconel X750); German version EN 3542:1998 |
|
DIN EN 3543 |
Aerospace series - Screws, 100° countersunk normal head, offset cruciform recess, close tolerance shank, short thread, in heat and corrosion resisting steel, passivated; classification: 1100 MPa (at ambient temperature)/425 °C; German version EN 3543:1997 |
|
DIN EN 3544-1 |
(DRAFT) Aerospace series - Titanium and titanium alloys; wrought products; technical specification - Part 1: General requirements |
|
DIN EN 3544-2 |
(DRAFT) Aerospace series - Titanium and titanium alloys; wrought products; technical specification - Part 2: Plate, sheet and strip |
|
DIN EN 3544-3 |
(DRAFT) Aerospace series - Titanium and titanium alloys; wrought products; technical specification - Part 3: Bar and section |
|
DIN EN 3545-001 |
Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 °C to 175 °C - Part 001: Technical specification; German and English version EN 3545-001:2005 |
|
DIN EN 3545-001/A1 |
(DRAFT) Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 °C to 175 °C - Part 001: Technical specification; Amendment A1 |
|
DIN EN 3545-002 |
Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 °C to 175 °C - Part 002: Specification of performance and contact arrangements; German and English version EN 3545-002:2005 |
|
DIN EN 3545-003 |
Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 °C to 175 °C - Part 003: Connectors with female contacts - Product standard; German and English version EN 3545-003:2005 |
|
DIN EN 3545-004 |
Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 °C to 175 °C - Part 004: Connectors with male contacts - Product standard; German and English version EN 3545-004:2005 |
|
DIN EN 3545-005 |
(DRAFT) Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 °C to 175 °C - Part 005: Female coding and attachment system for mounting on free housing (plug), product standard |
|
DIN EN 3545-006 |
(DRAFT) Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 °C to 175 °C - Part 006: Male coding and attachment system for mounting on fixed housing (receptacle), product standard |
|
DIN EN 3545-007 |
Aerospace series - Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures -55 °C to 175 °C - Part 007: Cable clamp - Product standard; German and English version EN 3545-007:2005 |
|
DIN EN 3552 |
Aerospace series - Aluminium alloy AL-P2618A-T6 or T62 - Clad sheet and strip - 0,4 mm ≤ a ≤ 6 mm; German and English version EN 3552:2005 |
|
DIN EN 3553 |
Aerospace series - Aluminium alloy AL-P2618A-T6511 - Extruded bar and section - a or D ≤ 160 mm; German and English version EN 3553:2004 |
|
DIN EN 3557 |
(DRAFT) Aerospace series - Aluminium alloy AL-P6061-T4 - Drawn tube for pressure applications, 0,6 mm ≤ a ≤ 3 mm |
|
DIN EN 3561 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Ferrules with dynamic beam seal end, welded and reduced at pipe end; German and English version EN 3561:2001 + AC:2003 |
|
DIN EN 3566 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Adaptors with lockring; German and English version EN 3566:2001 + AC:2003 |
|
DIN EN 3567-001 |
Aerospace series - In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B - Part 001: Technical specification; German and English version EN 3567-001:2001 |
|
DIN EN 3567-003 |
Aerospace series - In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B - Part 003: Single in-line couplers; Product standard; German and English version EN 3567-003:2001 |
|
DIN EN 3567-004 |
Aerospace series - In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B - Part 004: Double in-line couplers; Product standard; German and English version EN 3567-004:2001 |
|
DIN EN 3611 |
Aerospace series - Spigots - Dimensions and fit selection; design standard; German version EN 3611:1995 |
|
DIN EN 3618 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk normal head, in titanium Ti 44,5 Cb; inch based series |
|
DIN EN 3624 |
(DRAFT) Aerospace series - Polysulphide sealants, two component - Technical specification |
|
DIN EN 3626 |
(DRAFT) Aerospace series - Nuts, hexagon, self-locking, in steel, cadmium plated, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 3630 |
(DRAFT) Aerospace series; fluid fittings, flanged, straight, sealing by O-ring, for 0,8 mm thick tubes |
|
DIN EN 3631 |
(DRAFT) Aerospace series; fluid fittings, flanged 90° elbowed; sealing by O-ring, for 0,8 mm thick tubes |
|
DIN EN 3633 |
(DRAFT) Aerospace series; installation hole for fluid fittings, flanged |
|
DIN EN 3638 |
Aerospace series - Heat resisting alloy FE-PA2601(X6NiCrTiMoV26-15) - Consumable electrode remelted - Solution and precipitation treated - Sheet, strip and plate - 0,5 mm = a = 10 mm; German and English version EN 3638:2007 |
|
DIN EN 3639 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2601, softened and cold worked; wire for forged fasteners D ≤ 15 mm, 900 MPa ≤ Rm ≤ 1100 MPa |
|
DIN EN 3642 |
Aerospace series - Rivets, solid, 100° countersunk normal head, with dome, in titanium TI-PO2, anodized - Inch based series; German version EN 3642:1996 |
|
DIN EN 3643 |
Aerospace series - Rivets, solid, 100° countersunk normal head, in titanium TI-PO2, anodized - Inch based series; German version EN 3643:1996 |
|
DIN EN 3644 |
Aerospace series - Rivets, solid, universal head, in titanium TI-PO2, anodized - Inch based series; German version EN 3644:1996 |
|
DIN EN 3646-004 |
Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous - Part 004: Receptacle, jam-nut mounting - Product standard; German and English version EN 3646-004:2006 |
|
DIN EN 3646-005 |
Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous - Part 005: Receptacle, hermetic, square flange mounting - Product standard; German and English version EN 3646-005:2006 |
|
DIN EN 3646-006 |
Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous - Part 006: Receptacle, hermetic, jam-nut mounting - Product standard; German and English version EN 3646-006:2006 |
|
DIN EN 3646-007 |
Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous - Part 007: Receptacle, hermetic, round flange, welding or brazing mounting - Product standard; German and English version EN 3646-007:2006 |
|
DIN EN 3646-008 |
Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous - Part 008: Plug - Product standard; German and English version EN 3646-008:2006 |
|
DIN EN 3646-009 |
Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous - Part 009: Protective cover for receptacle - Product standard; German and English version EN 3646-009:2006 |
|
DIN EN 3646-010 |
Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous - Part 010: Protective cover for plug - Product standard; German and English version EN 3646-010:2006 |
|
DIN EN 3646-011 |
Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous - Part 011: Dummy receptacle - Product standard; German and English version EN 3646-011:2006 |
|
DIN EN 3653 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, floating, self-aligning, on lug, in steel, cadmium plated, MoS2 lubricated; classification: 900 MPa (at ambient temperature)/235 °C |
|
DIN EN 3656 |
(DRAFT) Aerospace series - Polycarbonate, self-extinguishing, low smoke emission - Characteristics |
|
DIN EN 3660-001 |
(DRAFT) Aerospace series; cable outlet accessories for circular and rectangular electrical and optical connectors; part 001: technical specification |
|
DIN EN 3660-002 |
(DRAFT) Aerospace series; cable outlet accessories for circular and rectangular electrical and optical connectors; part 002: index of product standards |
|
DIN EN 3660-003 |
(DRAFT) Aerospace series; cable outlet accessories for circular and rectangular electrical and optical connectors; part 003: grommet nut, type A, 003; product standard |
|
DIN EN 3660-004 |
(DRAFT) Aerospace series; cable outlet accessories for circular and rectangular electrical and optical connectors; part 004: cable outlet, type A, 004; straight unsealed, with clamp strain relief; product standard |
|
DIN EN 3660-005 |
(DRAFT) Aerospace series; cable outlet accessories for circular and rectangular electrical and optical connectors; part 005: cable outlet, type A, 005; 90° unsealed, with clamp strain relief; product standard |
|
DIN EN 3661-001 |
(DRAFT) Aerospace series - Circuit breakers, single-pole, temperature compensated, rated currents 20 A to 50 A - Part 001: Technical specification |
|
DIN EN 3662-001 |
(DRAFT) Aerospace series - Circuit breakers, three-pole, temperature compensated, rated currents 20 A to 50 A - Part 001: Technical specification |
|
DIN EN 3662-005 |
(DRAFT) Aerospace series - Circuit breakers, three-pole, temperature compensated, rated currents 20 A to 50 A - Part 005: With polarized signal contact and unified mounting hardware, centre-to-centre distance of terminals 21 mm; product standard |
|
DIN EN 3662-006 |
(DRAFT) Aerospace series - Circuit breakers, three-pole, temperature compensated, rated currents 20 A to 50 A - Part 006: With polarized signal contact and unified mounting hardware, bus-bar version; product standard |
|
DIN EN 3663 |
Aerospace series - Pipe coupling - O-rings in rubber NBR, 75 IRHD, Temperature range: - 55 °C to 135 °C; German and English version EN 3663:2001 + AC:2003 |
|
DIN EN 3666 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH2601 - Solution treated and cold worked; bar for forged fasteners D ≤ 50 mm, 1550 MPa ≤ Rm ≤ 1830 MPa |
|
DIN EN 3668 |
Aerospace series - Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) - Non heat treated - Forging stock - a or D = 250 mm; German and English version EN 3668:2006 |
|
DIN EN 3671 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb), non heat treated - Forging stock a or D ≤ 250 mm |
|
DIN EN 3671 |
Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Non heat treated - Forging stock - a or D = 250 mm; German and English version EN 3671:2007 |
|
DIN EN 3672 |
(DRAFT) Aerospace series; shank nuts, self-locking; in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated, for 30 ° swage; classification: 1210 MPa (at ambient temperature)/730 °C |
|
DIN EN 3676 |
Aerospace series - Inserts, thin wall, self-locking - Design standard; German version EN 3676:1998 |
|
DIN EN 3677 |
(DRAFT) Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Forgings, a or D ≤ 200 mm, Rm ≥ 1310 MPa |
|
DIN EN 3677 |
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted - Solution treated and precipitation treated - Forgings - a or D = 200 mm - Rm = 1 310 MPa; German and English version EN 3677:2007 |
|
DIN EN 3678 |
(DRAFT) Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Forgings, a or D ≤ 200 mm, Rm ≥ 930 MPa |
|
DIN EN 3678 |
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted - Solution treated and precipitation treated - Forgings - a or D = 200 mm - Rm = 930 MPa; German and English version EN 3678:2007 |
|
DIN EN 3679 |
(DRAFT) Aerospace series - Steel FE-PM3902 (X7CrNiAl17-7) air melted, solution treated and precipitation hardened - Plate, 6 mm < a ≤ 15 mm, 1240 MPa ≤ Rm ≤ 1450 MPa |
|
DIN EN 3682-001 |
(DRAFT) Aerospace series - Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperatures 150 °C continuous - Part 001: Technical specification |
|
DIN EN 3682-002 |
(DRAFT) Aerospace series - Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 °C continuous - Part 002: Specification of performance and contact arrangements |
|
DIN EN 3683 |
(DRAFT) Aerospace series - Test methods - Titanium alloy wrought products - Determination of primary α content; point count method and line intercept method |
|
DIN EN 3683 |
Aerospace series - Test methods - Titanium alloy wrought products - Determination of primary a content - Point count method and line intercept method; German and English version EN 3683:2007 |
|
DIN EN 3684 |
(DRAFT) Aerospace series - Test methods - Titanium alloy wrought products - Determination of β transus temperature; metallographic method |
|
DIN EN 3684 |
Aerospace series - Test methods - Titanium alloy wrought products - Determination of ß transus temperature - Metallographic method; German and English version EN 3684:2007 |
|
DIN EN 3688 |
Aerospace series - T-ring fillers in titanium alloy for welding pipes - 14000 kPa nominal pressure; German and English version EN 3688:2001 + AC:2003 |
|
DIN EN 3689 |
Aerospace series - T-ring fillers in titanium alloy for welding pipes - 28000 kPa nominal pressure; German and English version EN 3689:2001 + AC:2003 |
|
DIN EN 3690 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, bulkhead, long; German and English version EN 3690:2001 + AC:2003 |
|
DIN EN 3691 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, bulkhead, long, welded end; German and English version EN 3691:2001 + AC:2003 |
|
DIN EN 3696 |
Aerospace series - Washers in heat resisting steel; German and English version EN 3696:2001 |
|
DIN EN 3703 |
(DRAFT) Aerospace series - Heat release rate for materials and products under the influence of radiating heat and flames - Test method |
|
DIN EN 3708-001 |
(DRAFT) Aerospace series - Modular interconnection systems, terminal junction systems - Part 001: Technical specification |
|
DIN EN 3708-002 |
(DRAFT) Aerospace series - Modular interconnection systems, terminal junction systems - Part 002: Performance specification |
|
DIN EN 3708-003 |
(DRAFT) Aerospace series - Modular interconnection systems, terminal junction systems - Part 003: Removable feedback modules version, sealed, product standard |
|
DIN EN 3708-004 |
(DRAFT) Aerospace series - Modular interconnection systems, terminal junction systems - Part 004: Removable feedback modules version, unsealed, product standard |
|
DIN EN 3708-005 |
(DRAFT) Aerospace series - Modular interconnection systems, terminal junction systems - Part 005: Frames with accessories for feedback modules, sealed and unsealed, product standard |
|
DIN EN 3714 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, floating, two lug, with counterbore, in heat resisting steel, silver plated; classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 3716-001 |
(DRAFT) Aerospace series - Connector, single-way, with triaxial interface, for transmission of digital data - Part 001: Technical specification |
|
DIN EN 3716-001 |
Aerospace series - Connector, single-way, with triaxial interface, for transmission of digital data - Part 001: Technical specification; German and English version EN 3716-001:2006 |
|
DIN EN 3716-002 |
(DRAFT) Aerospace series - Connector, single-way, with triaxial interface, for transmission of digital data - Part 002: Conditions of use and list of product standards |
|
DIN EN 3716-002 |
Aerospace series - Connectors, single-way with triaxial interface, for transmission of digital data - Part 002: Conditions of use and list of product standards; German and English version EN 3716-002:2006 |
|
DIN EN 3716-003 |
(DRAFT) Aerospace series - Connector, single-way, with triaxial interface, for transmission of digital data - Part 003: Solder receptacle; product standard |
|
DIN EN 3716-003 |
Aerospace series - Connectors, single-way with traxial interface, for transmission of digital data - Part 003: Solder receptacle - Product standard; German and English version EN 3716-003:2006 |
|
DIN EN 3716-004 |
(DRAFT) Aerospace series - Connector, single-way, with triaxial interface, for transmission of digital data - Part 004: Solder plug; product standard |
|
DIN EN 3716-004 |
Aerospace series - Connectors, single-way with triaxial interface, for transmission of digital data - Part 004: Solder plug - Product standard; German and English version EN 3716-004:2006 |
|
DIN EN 3718 |
(DRAFT) Aerospace series - Test method for metallic materials - Ultrasonic inspection of tubes |
|
DIN EN 3719 |
Aerospace series - Aluminium or aluminium alloy conductors for electrical cables - Product standard; German and English version EN 3719:2005 |
|
DIN EN 3720 |
Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting steel FE-PA92HT (A286), MoS2 coated - Classification: 1100 MPa (at ambient temperature)/425 °C; German version EN 3720:1995 |
|
DIN EN 3721 |
Aerospace series - Nuts, bihexagonal, self-locking, deep counterbored, in heat resisting steel FE-PA92HT (A286), MoS2 coated - Classification: 1100 MPa (at ambient temperature)/425 °C; German version EN 3721:1995 |
|
DIN EN 3722 |
Aerospace series - Shank nuts, self-locking, in heat resisting steel FE-PA92HT (A286), MoS2 coated - Classification: 1100 MPa (at ambient temperature)/425 °C; German version EN 3722:1995 |
|
DIN EN 3723 |
Aerospace series - Nuts, hexagonal, self-locking, in heat resisting steel FE-PA92HT (A286), MoS2 coated - Classification: 1100 MPa (at ambient temperature)/425 °C; German version EN 3723:1996 |
|
DIN EN 3724 |
Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Strength class: 1100 MPa (at ambient temperature); German and English version EN 3724:2004 |
|
DIN EN 3725 |
Aerospace series - Screws, pan head, six lobe recess, normal shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated - Strength class: 1100 MPa (at ambient temperature); German and English version EN 3725:2004 |
|
DIN EN 3728 |
(DRAFT) Aerospace series - Shaft-nuts, self-locking - Left-hand thread, in heat resisting steel FE-PA92HT (A286), silver plated |
|
DIN EN 3729 |
(DRAFT) Aerospace series - Rings, threaded, self-locking - Left-hand thread, in heat resisting steel FE-PA92HT (A286), silver plated |
|
DIN EN 3730 |
Aerospace series - Clamps, saddle fixed and sliding version in aluminium alloy with rubber cushioning - Dimensions, masses; German and English version EN 3730:2001 |
|
DIN EN 3735 |
(DRAFT) Aerospace series - Titanium alloy TI-P65002, solution treated and aged; bar for machining D ≤ 75 mm |
|
DIN EN 3736 |
(DRAFT) Aerospace series - Titanium alloy TI-P65002 - Grade 2, solution treated and aged, forgings De ≤ 75 mm |
|
DIN EN 3737 |
(DRAFT) Aerospace series - Titanium alloy TI-P65002 - Not heat treated, grade 2 forging stock for solution treated and aged forgings a or D ≤ 360 mm |
|
DIN EN 3738 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head with dome, in titanium alloy Ti 45,5 Cb; metric series |
|
DIN EN 3739 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head, in titanium alloy Ti 45,5 Cb; metric series |
|
DIN EN 3740 |
Aerospace series - Bolts, shouldered, thin hexagonal head, close tolerance shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C; German version EN 3740:1996 |
|
DIN EN 3741 |
Aerospace series - Nuts, clip, metric - Installation holes and assembly; German and English version EN 3741:2004 |
|
DIN EN 3743 |
(DRAFT) Aerospace series; straight pins, spring type, heavy duty, in corrosion resisting spring steel, passivated |
|
DIN EN 3744 |
(DRAFT) Aerospace series; straight pins, spring type, light duty, in corrosion resisting spring steel, passivated |
|
DIN EN 3745-201 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 201: Visual examination; German and English version EN 3745-201:2002 |
|
DIN EN 3745-202 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 202: Fibre dimensions; German and English version EN 3745-202:2005 |
|
DIN EN 3745-205 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 205: Cable longitudinal dimensional stability; German and English version EN 3745-205:2002 |
|
DIN EN 3745-301 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 301: Attenuation; German and English version EN 3745-301:2002 |
|
DIN EN 3745-302 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 302: Numerical aperture; German and English version EN 3745-302:2002 |
|
DIN EN 3745-305 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 305: Immunity to ambient light coupling; German and English version EN 3745-305:2002 |
|
DIN EN 3745-401 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 401: Accelerated ageing; German and English version EN 3745-401:2005 |
|
DIN EN 3745-402 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 402: Temperature cycling; German and English version EN 3745-402:2005 |
|
DIN EN 3745-404 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 404: Thermal shock; German and English version EN 3745-404:2005 |
|
DIN EN 3745-406 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 406: Cold bend test; German and English version EN 3745-406:2005 |
|
DIN EN 3745-407 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 407: Flammability; German and English version EN 3745-407:2005 |
|
DIN EN 3745-412 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 412: Humidity resistance; German and English version EN 3745-412:2005 |
|
DIN EN 3745-501 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 501: Optical fibre proof test; German and English version EN 3745-501:2005 |
|
DIN EN 3745-502 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 502: Tensile strength for short length of optical fibres; German and English version EN 3745-502:2005 |
|
DIN EN 3745-503 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 503: Scrape abrasion; German and English version EN 3745-503:2005 |
|
DIN EN 3745-504 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 504: Micro bending test; German and English version EN 3745-504:2002 |
|
DIN EN 3745-506 |
(DRAFT) Aerospace series - Fibres and cables, optical, aircraft use; test methods - Part 506: Impact resistance |
|
DIN EN 3745-507 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 507: Cut-through; German and English version EN 3745-507:2002 |
|
DIN EN 3745-508 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 508: Torsion; German and English version EN 3745-508:2002 |
|
DIN EN 3745-509 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 509: Kink test; German and English version EN 3745-509:2002 |
|
DIN EN 3745-510 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 510: Bending test; German and English version EN 3745-510:2002 |
|
DIN EN 3745-511 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 511: Cable to cable abrasion; German and English version EN 3745-511:2002 |
|
DIN EN 3745-513 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 513: Crush resistance; German and English version EN 3745-513:2005 |
|
DIN EN 3745-701 |
Aerospace series - Fibres and cables, optical, aircraft use; Test methods - Part 701: Strippability; German and English version EN 3745-701:2002 |
|
DIN EN 3745-703 |
(DRAFT) Aerospace series - Fibres and cables, optical, aircraft use; test methods - Part 703: Durability of manufacturer's marking |
|
DIN EN 3745-703 |
Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 703: Durability of manufacturer's marking; German and English version EN 3745-703:2005 |
|
DIN EN 3746 |
Aerospace series - O-rings, in fluorosilicone rubber (FVMQ) - Hardness 80 IRHD; German and English version EN 3746:2003 |
|
DIN EN 3746 |
Aerospace series - O-rings, in fluorosilicone rubber (FVMQ) - Hardness 80 IRHD; German and English version EN 3746:2003 |
|
DIN EN 3746 |
Aerospace series - O-rings, in fluorosilicone rubber (FVMQ) - Hardness 80 IRHD; German and English version EN 3746:2003 |
|
DIN EN 3747 |
Aerospace series - O-rings, in fluorosilicone rubber (FVMQ) - Technical specification; German and English version EN 3747:2003 |
|
DIN EN 3750 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, fixed, 90° corner, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 3751 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, fixed, closed corner, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 3752 |
Aerospace series - Nuts, self-locking, MJ threads, in heat resisting steel FE-PA2601 (A286), MoS2 coated - Classification: 1100 MPa (at ambient temperature)/425 °C - Technical specification; German and English version EN 3752:2004 |
|
DIN EN 3753 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, fixed, 60° corner, with counterbore, in alloy steel, cadmium plated, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 3754 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, fixed, 60° corner, with counterbore, in heat resisting steel, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 3757 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, floating, self-aligning, two lug, in heat resisting steel, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/315 °C |
|
DIN EN 3758 |
(DRAFT) Aerospace series - Simplex high speed data transmission system |
|
DIN EN 3759 |
Aerospace series - Screws, pan head, offset cruciform recess, threaded to head, in heat and corrosion resisting steel, passivated - Classification: 1100 MPa (at ambient temperature)/425 °C; German version EN 3759:1996 |
|
DIN EN 3760 |
Aerospace series - Screws, 100° countersunk normal head, offset cruciform recess, threaded to head, in heat and corrosion resisting steel, passivated - Classification: 1100 MPa (at ambient temperature)/425 °C; German version EN 3760:1996 |
|
DIN EN 3761 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2601, softened and cold worked; bar for forged fasteners D ≤ 50 mm, 1100 MPa ≤ Rm ≤ 1300 MPa |
|
DIN EN 3762 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PA2601, softened and cold worked; wire for forged fasteners D ≤ 15 mm, 1100 MPa ≤ Rm ≤ 1300 MPa |
|
DIN EN 3763 |
(DRAFT) Aerospace series - Nuts, hexagonal, self-locking, ball seat, in heat resisting steel, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/315 °C |
|
DIN EN 3764 |
(DRAFT) Aerospace series - Washers, concave, in heat resisting steel, passivated |
|
DIN EN 3765 |
(DRAFT) Aerospace series - Electrolytic silver plating for general use - Steels, heat resisting alloys, copper and copper alloys |
|
DIN EN 3767 |
(DRAFT) Aerospace series - Rivets, blind, nut plate, 100° countersunk head, in heat resisting steel, passivated, metric series |
|
DIN EN 3768 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, one lug, fixed, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 3769 |
Aerospace series - Electrolytic polishing of corrosion resistant steels and heat resisting alloys; German version EN 3769:1997 |
|
DIN EN 3773-001 |
Aerospace series - Circuit breakers, single-pole, temperature compensated, rated currents 1 A to 25 A, switching capacity 65 In/1000 A max. - Part 001: Technical specification; German version EN 3773-001:1999 |
|
DIN EN 3773-003 |
Aerospace series - Circuit breakers, single-pole, temperature compensated, rated currents 1 A to 25 A, switching capacity 65 In/1000 A max. - Part 003: Metric thread terminals; product standard; German version EN 3773-003:1999 |
|
DIN EN 3773-004 |
Aerospace series - Circuit breakers, single-pole, temperature compensated, rated currents 1 A to 25 A, switching capacity 65 In/1000 A max. - Part 004: UNC thread terminals; product standard; German version EN 3773-004:1999 |
|
DIN EN 3774-001 |
Aerospace series - Circuit breakers, three-pole, temperature compensated, rated currents 2 A to 25 A, switching capacity 65 In - Part 001: Technical specification; German version EN 3774-001:1999 |
|
DIN EN 3774-003 |
Aerospace series - Circuit breakers, three-pole, temperature compensated, rated currents 2 A to 25 A, switching capacity 65 In - Part 003: Metric thread terminals; product standard; German version EN 3774-003:1999 |
|
DIN EN 3774-004 |
Aerospace series - Circuit breakers, three-pole, temperature compensated, rated currents 2 A to 25 A, switching capacity 65 In - Part 004: UNC thread terminals; product standard; German version EN 3774-004:1999 |
|
DIN EN 3776 |
(DRAFT) Aerospace series - Pins, quick release, two balls, single acting, single locking, |
|
DIN EN 3777 |
(DRAFT) Aerospace series - Pins, quick release, single and double acting - Technical specification |
|
DIN EN 3778 |
(DRAFT) Aerospace series - Pins, quick release, two balls, double acting, single locking, |
|
DIN EN 3779 |
(DRAFT) Aerospace series - Polycarbonate sheet - Dimensions |
|
DIN EN 3781 |
(DRAFT) Aerospace series; grooves for spiral wound retaining rings; design standard |
|
DIN EN 3782 |
(DRAFT) Aerospace series; grooves for 100° countersunk head screws; design standard |
|
DIN EN 3788 |
Aerospace series - Pipe coupling 8°30′ - Protective caps; German and English version EN 3788:2001 + AC:2003 |
|
DIN EN 3789 |
Aerospace series - Pipe coupling 8°30′ - Protective plugs with external threads; German and English version EN 3789:2001 + AC:2003 |
|
DIN EN 3790 |
Aerospace series - Pipe coupling 8°30′ - Protective caps with internal threads; German and English version EN 3790:2001 + AC:2003 |
|
DIN EN 3792 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Technical specification |
|
DIN EN 3793 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds; test method - Determination of static shear strength |
|
DIN EN 3794 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds; test method - Determination of torque strength on threaded fasteners |
|
DIN EN 3795 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds; test method - Determination of freedom from excessive cure rate |
|
DIN EN 3796 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds; test method - Determination of ability of anaerobic polymerisable compounds to set on metal surface |
|
DIN EN 3797 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 2 Nm; viscosity 125 mm2s-1 |
|
DIN EN 3798 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 2 Nm; viscosity 500 mm2s-1 |
|
DIN EN 3799 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 5 Nm - Viscosity 125 mm2s-1 |
|
DIN EN 3800 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 5 Nm; viscosity 500 mm2s-1 |
|
DIN EN 3801 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 5 Nm; thixotropic index 8 |
|
DIN EN 3802 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 10 Nm; viscosity 125 mm2s-1 |
|
DIN EN 3803 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 10 Nm; viscosity 500 mm2s-1 |
|
DIN EN 3804 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 10 Nm; thixotropic index 3,5 |
|
DIN EN 3805 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 10 Nm; thixotropic index 8 |
|
DIN EN 3806 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 16 Nm; viscosity < 50 mm2s-1 |
|
DIN EN 3807 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 16 Nm; viscosity 500 mm2s-1 |
|
DIN EN 3808 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 16 Nm; thixotropic index 8 |
|
DIN EN 3809 |
(DRAFT) Aerospce series - Anaerobic polymerisable compounds - Torque strength 19 Nm; viscosity < 50 mm2s-1 |
|
DIN EN 3810 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 19 Nm; viscosity 125 mm2s-1 |
|
DIN EN 3811 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 19 Nm; viscosity 500 mm2s-1 |
|
DIN EN 3812 |
(DRAFT) Aerospace series - Anaerobic polymerisable compounds - Torque strength 19 Nm; thixotropic index 8 |
|
DIN EN 3816 |
Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Air melted - Softened and cold rolled - Sheet and strip a = 3 mm - Rm = 800 MPa; German and English version EN 3816:2006 |
|
DIN EN 3818 |
Aerospace series - Bolts, MJ threads, in titanium alloy TI-P64001 - Strength class: 1100 MPa (at ambient temperature) - Technical specification; German and English version EN 3818:2004 |
|
DIN EN 3820 |
(DRAFT) Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 3821 |
(DRAFT) Aerospace series - Washers, chamfered, with counterbore, in heat resisting steel, passivated |
|
DIN EN 3822 |
(DRAFT) Aerospace series - Washers, flat, thick, in heat resisting steel, passivated |
|
DIN EN 3824 |
(DRAFT) Aerospace series - Clinch-nuts, blind, self-locking, with counterbore, in corrosion resisting steel, MoS2 lubricated; classification: 600 MPa (at ambient temperature)/315 °C |
|
DIN EN 3830 |
(DRAFT) Aerospace series - Electrical system - Load analysis |
|
DIN EN 3831 |
Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated; German and English version EN 3831:2004 |
|
DIN EN 3833 |
Aerospace series - Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), passivated - Classification: 1550 MPa (at ambient temperature)/ 650 °C - Technical specification; German and English version EN 3833:2004 |
|
DIN EN 3834 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, floating, two lug, incremental counterbore, in corrosion resisting steel, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/315 °C |
|
DIN EN 3835 |
(DRAFT) Aerospace series; washers, 100° dimpled, in heat resisting steel, passivated |
|
DIN EN 3838 |
(DRAFT) Aerospace series - Requirements and tests on user-applied markings on aircraft electrical cables |
|
DIN EN 3840 |
(DRAFT) Aerospace series - Paints and varnishes - Technical specification |
|
DIN EN 3841-100 |
Aerospace series - Circuit breakers - Test methods - Part 100: General; German and English version EN 3841-100:2004 |
|
DIN EN 3841-201 |
Aerospace series - Circuit breakers - Test methods - Part 201: Visual inspection; German and English version EN 3841-201:2004 |
|
DIN EN 3841-202 |
Aerospace series - Circuit breakers - Test methods - Part 202: Dimensions and masses; German and English version EN 3841-202:2004 |
|
DIN EN 3841-301 |
Aerospace series - Circuit breakers - Test methods - Part 301: Voltage drop; German and English version EN 3841-301:2004 |
|
DIN EN 3841-302 |
Aerospace series - Circuit breakers - Test methods - Part 302: Insulation resistance; German and English version EN 3841-302:2004 |
|
DIN EN 3841-303 |
Aerospace series - Circuit breakers - Test methods - Part 303: Dielectric strength; German and English version EN 3841-303:2004 |
|
DIN EN 3841-304 |
Aerospace series - Circuit breakers - Test methods - Part 304: Tripping points; German and English version EN 3841-304:2004 |
|
DIN EN 3841-305 |
Aerospace series - Circuit breakers - Test methods - Part 305: Short-circuit performance; German and English version EN 3841-305:2004 |
|
DIN EN 3841-306 |
Aerospace series - Circuit breakers - Test methods - Part 306: Service life; German and English version EN 3841-306:2004 |
|
DIN EN 3841-307 |
Aerospace series - Circuit breakers - Test methods - Part 307: Performance with a locked tripping system; German and English version EN 3841-307:2004 |
|
DIN EN 3841-401 |
Aerospace series - Circuit breakers - Test methods - Part 401: Sand and dust; German and English version EN 3841-401:2004 |
|
DIN EN 3841-402 |
Aerospace series - Circuit breakers - Test methods - Part 402: Corrosion; German and English version EN 3841-402:2004 |
|
DIN EN 3841-403 |
Aerospace series - Circuit breakers - Test methods - Part 403: Humidity; German and English version EN 3841-403:2004 |
|
DIN EN 3841-404 |
Aerospace series - Circuit breakers - Test methods - Part 404: Explosion proofness; German and English version EN 3841-404:2004 |
|
DIN EN 3841-405 |
Aerospace series - Circuit breakers - Test methods - Part 405: Fluid resistance; German and English version EN 3841-405:2004 |
|
DIN EN 3841-406 |
Aerospace series - Circuit breakers - Test methods - Part 406: Flammability; German and English version EN 3841-406:2004 |
|
DIN EN 3841-407 |
Aerospace series - Circuit breakers - Test methods - Part 407: Temperature variation; German and English version EN 3841-407:2004 |
|
DIN EN 3841-501 |
Aerospace series - Circuit breakers - Test methods - Part 501: Actuator button travel; German and English version EN 3841-501:2004 |
|
DIN EN 3841-502 |
Aerospace series - Circuit breakers - Test methods - Part 502: Operating forces; German and English version EN 3841-502:2004 |
|
DIN EN 3841-503 |
Aerospace series - Circuit breakers - Test methods - Part 503: Strength of actuating components; German and English version EN 3841-503:2004 |
|
DIN EN 3841-504 |
Aerospace series - Circuit breakers - Test methods - Part 504: Strength of mounting elements; German and English version EN 3841-504:2004 |
|
DIN EN 3841-505 |
Aerospace series - Circuit breakers - Test methods - Part 505: Strength of main terminals; German and English version EN 3841-505:2004 |
|
DIN EN 3841-506 |
Aerospace series - Circuit breakers - Test methods - Part 506: Vibration performance; German and English version EN 3841-506:2004 |
|
DIN EN 3841-507 |
Aerospace series - Circuit breakers - Test methods - Part 507: Mechanical shocks; German and English version EN 3841-507:2004 |
|
DIN EN 3841-508 |
Aerospace series - Circuit breakers - Test methods - Part 508: Centrifugal acceleration; German and English version EN 3841-508:2004 |
|
DIN EN 3841-509 |
Aerospace series - Circuit breakers - Test methods - Part 509: Insertion and extraction forces of signal contact terminals; German and English version EN 3841-509:2004 |
|
DIN EN 3841-510 |
Aerospace series - Circuit breakers - Test methods - Part 510: Strength of signal contact terminals; German and English version EN 3841-510:2004 |
|
DIN EN 3841-511 |
Aerospace series - Circuit breakers - Test methods - Part 511: Combined test: temperature, altitude and vibration; German and English version EN 3841-511:2004 |
|
DIN EN 3842 |
Aerospace series - Circular tubes for fluids in corrosion resistant steel - Diameter 3,2 mm ≤ D ≤ 100 mm, thickness 0,32 mm ≤ a ≤ 2,5 mm; Dimensions; German and English version EN 3842:2001 |
|
DIN EN 3843 |
(DRAFT) Aerospace series - Nuts, bihexagonal, self-locking, with counterbore, in heat resisting steel, passivated - Classification: 1100 MPa (at ambient temperature)/650 °C |
|
DIN EN 3844-1 |
(DRAFT) Aerospace series - Flammability of non-metallic materials - Part 1: Small burner test, vertical; determination of the vertical flame propagation |
|
DIN EN 3844-2 |
(DRAFT) Aerospace series - Flammability of non-metallic materials - Part 2: Small burner test, horizontal; determination of the horizontal flame propagation |
|
DIN EN 3844-3 |
(DRAFT) Aerospace series - Flammability of non-metallic materials - Part 3: Small burner test, 45°; determination of the resistance of material to flame and glow propagation and to flame penetration |
|
DIN EN 3847 |
(DRAFT) Aerospace series - Paints and varnishes - Determination of sedimentation rating |
|
DIN EN 3848 |
Aerospace series - Semi-finished metallic products - Methods of measuring form deviations; German and English version EN 3848:2001 |
|
DIN EN 3851 |
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Swivel nut, straight; German and English version EN 3851:2003 |
|
DIN EN 3852 |
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Straight unions, welded, threaded; German and English version EN 3852:2002 |
|
DIN EN 3853 |
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Straight unions, threaded; German and English version EN 3853:2002 |
|
DIN EN 3854 |
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Ferrules, welded; German and English version EN 3854:2002 |
|
DIN EN 3855 |
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Caps; German and English version EN 3855:2002 |
|
DIN EN 3856 |
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Swivel nuts for thrust wire; German and English version EN 3856:2002 |
|
DIN EN 3857 |
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Elbows 90°, welded; German and English version EN 3857:2002 |
|
DIN EN 3858 |
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Thrust wires in steel FE-PA 13; German and English version EN 3858:2002 |
|
DIN EN 3860 |
(DRAFT) Aerospace series; titanium alloy TI-P19001; annealed, sheet and strip, cold rolled, a ≤ 3 mm |
|
DIN EN 3867 |
(DRAFT) Aerospace series - Pipe couplings, loose flanges and seals - Flanges in titanium alloy TI-P64001 |
|
DIN EN 3867 |
Aerospace series - Pipe couplings, loose flanges and seals - Flanges in titanium alloy TI-P64001; German and English version EN 3867:2004 |
|
DIN EN 3868 |
(DRAFT) Aerospace series - Pipe couplings, loose flanges and seals - Flange connectors, welded, in titanium alloy TI-P64001 |
|
DIN EN 3868 |
Aerospace series - Pipe couplings, loose flanges and seals - Flange connectors, welded, in titanium alloy TI-P64001; German and English version EN 3868:2004 |
|
DIN EN 3869 |
Aerospace series - Pipe couplings, loose flanges and seals - Seals in fluorocarbon rubber and armature in aluminium alloy; German and English version EN 3869:2004 |
|
DIN EN 3870 |
(DRAFT) Aerospace series; titanium alloy TI-P19001; solution treated and aged, sheet and strip, hot rolled, a ≤ 6 mm |
|
DIN EN 3871 |
(DRAFT) Aerospace series; titanium alloy TI-P19001; solution treated and aged, sheet and strip, cold rolled, a ≤ 3 mm |
|
DIN EN 3872 |
Aerospace series - Aluminium alloy AL-R39002-H112 - Die forgings - a ≤ 200 mm; German and English version EN 3872:2005 |
|
DIN EN 3874 |
(DRAFT) Aerospace series - Test methods for metallic materials - Constant amplitude force-controlled low cycle fatique testing |
|
DIN EN 3875 |
(DRAFT) Aerospace series - Metallic materials - Filler metal for brazing; technical specification |
|
DIN EN 3877 |
(DRAFT) Aerospace series - Metallic materials - Test method; determination of solidus and liquidus temperatures by differential thermal analysis of braze alloys |
|
DIN EN 3878 |
(DRAFT) Aerospace series - Test method for metallic materials, braze alloys - Flexibility test |
|
DIN EN 3879 |
(DRAFT) Aerospace series - Metallic materials - Filler metal for welding; technical specification |
|
DIN EN 3880 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7075-T73 - Die forgings a ≤ 125 mm |
|
DIN EN 3881 |
(DRAFT) Aerospace series - Aluminium Alloy AL-P7075-T73 - Hand forgings a ≤ 125 mm |
|
DIN EN 3882 |
Aerospace series - Heat resisting alloy NI-WH1801 (NiCr20Co18Ti3Al2) - Filler metal for welding; German version EN 3882:2001 |
|
DIN EN 3883 |
Aerospace series - Heat resisting alloy NI-WH2301 (NiCr22Fe19Mo9Co2) - Filler metal for welding; German version EN 3883:2001 |
|
DIN EN 3884 |
Aerospace series - Heat resisting alloy NI-WH2601 (NiCr19Nb5Mo3Ti) - Filler metal for welding; German version EN 3884:2001 |
|
DIN EN 3885 |
Aerospace series - Heat resisting alloy NI-WH3601 (NiCr22Mo9Nb4) - Filler metal for welding; German version EN 3885:2001 |
|
DIN EN 3886 |
Aerospace series - Heat resisting alloy NI-WH1303 (NiCo20Cr20Mo5Ti2Al) - Filler metal for welding; German version EN 3886:2001 |