|
DIN EN 3065 |
Aerospace series - Installation holes for self-locking, serrated shank nuts; design Standard; German version EN 3065:1996 |
|
DIN EN 3071 |
(DRAFT) Aerospace series - Straight bending of sheets and strips in aluminium and aluminium alloys - Dimensioning methods and calculations of developed lengths |
|
DIN EN 3077 |
(DRAFT) Aerospace series - Clamps worm drive - Technical specification |
|
DIN EN 3078 |
(DRAFT) Aerospace series - P, Q and saddle clamps with rubber cushion - Technical specification |
|
DIN EN 3079 |
(DRAFT) Aerospace series - Pipe coupling 8°30′ up to 28000 kPa - Adaptors; metric series; technical specifiations |
|
DIN EN 3080 |
(DRAFT) Aerospace series - Pipe coupling 8°30′ in titanium alloy, tees, reduced branch with thrust wire nut |
|
DIN EN 3081 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Ferrules, welded with dynamic beam seal end, for repair; German version EN 3081:2001 |
|
DIN EN 3082 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, bulkhead welded end, for repair; German and English version EN 3082:2001 + AC:2003 |
|
DIN EN 3083 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, bulkhead, long welded end, for repair; German and English version EN 3083:2001 + AC:2003 |
|
DIN EN 3084 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, welded end threaded for repair; German and English version EN 3084:2001 + AC:2003 |
|
DIN EN 3086 |
(DRAFT) Aerospace series - hose assemblies - Designation limited to 15 digits |
|
DIN EN 3094 |
(DRAFT) Aerospace series - Sealants - Test method; determination of application time |
|
DIN EN 3095 |
(DRAFT) Aerospace series - Sealants - Test method - Determination of extended assembly time |
|
DIN EN 3096 |
(DRAFT) Aerospace series - Sealants - Test method; determination of tack-free time |
|
DIN EN 3101 |
(DRAFT) Aerospace series - Non-metallic materials - Sealants; test methods; determination of resistance to thermal rupture |
|
DIN EN 3102 |
(DRAFT) Aerospace series - Sealants - Test methods; Determination of low-temperature flexibility |
|
DIN EN 3112 |
Aerospace series - Bolts, normal hexagonal head, threaded to head, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C; German version EN 3112:1995 |
|
DIN EN 3114-001 |
Aerospace series - Test method - Microstructure of (a + ss) titanium alloy wrought products - Part 001: General requirements; German and English version EN 3114-001:2006 |
|
DIN EN 3114-002 |
Aerospace series - Test method - Microstructure of (a + ß) titanium alloy wrought products - Part 002: Microstructure of bars, sections, forging stock and forgings; German and English version EN 3114-002:2007 |
|
DIN EN 3114-003 |
Aerospace series - Test method - Microstructure of (a + ss) titanium alloy wrought products - Part 003: Microstructure of plate; German and English version EN 3114-003:2006 |
|
DIN EN 3114-004 |
Aerospace series - Test method - Microstructure of (a + ss) titanium alloy wrought products - Part 004: Microstructure of sheet for superplastic forming; German and English version EN 3114-004:2006 |
|
DIN EN 3114-2 |
(DRAFT) Aerospace series - Test method - Microstructure of (α + β) titanium alloy wrought products - Part 2: Microstructure of bars, sections, forging stock and forgings |
|
DIN EN 3115 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7050 - Wire for rivets D ≤ 10 mm |
|
DIN EN 3119 |
(DRAFT) Aerospace series - Titanium alloy TI-P46001 - Not heat treated, grade 2 forging stock for solution treated and aged forgings a or D ≤ 360 mm |
|
DIN EN 3120 |
(DRAFT) Aerospace series - Titanium alloy TI-P64003, cold worked and stress relieved - Seamless tube for pressure systems 4 mm ≤D≤ 51 mm, 690 MPa ≤Rm≤ 1030 MPa |
|
DIN EN 3135 |
Aerospace series - Rivets, solid, universal head, in corrosion resisting steel FE-PA11, passivated, inch based series; German version EN 3135:1996 |
|
DIN EN 3137 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head with dome, in corrosion resisting steel FE-PA11, passivated |
|
DIN EN 3138 |
Aerospace series - Rivets, solid, 100° countersunk normal head with dome, in corrosion resisting steel FE-PA2601, passivated, inch based series; German version EN 3138:2001 |
|
DIN EN 3139 |
Aerospace series - Rivets, solid, 100° countersunk normal head, in corrosion resisting steel FE-PA11, passivated, inch based series; German version EN 3139:2001 |
|
DIN EN 3140 |
Aerospace series - Rivets, solid, 100° countersunk normal head, in corrosion resisting steel FE-PA2601, passivated, inch based series; German version EN 3140:2001 |
|
DIN EN 3142 |
Aerospace series - Rivets, solid, universal head, in heat resisting nickel base alloy NI-P11, inch based series; German version EN 3142:1996 |
|
DIN EN 3143 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk normal head, in nickel base alloy NI-P11, cadmium plated; inch based series |
|
DIN EN 3144 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk normal head, in nickel base alloy NI-P11; inch based series |
|
DIN EN 3145 |
Aerospace series - Round bars, hot rolled in steel - Normal tolerances; Diameter 6 mm ≤ D ≤ 250 mm; Dimensions; German and English version EN 3145:2001 |
|
DIN EN 3146 |
Aerospace series - Round bars, hot rolled, in steel, close tolerances, diameter 6 mm≤D≤250 mm - Dimensions; German and English version EN 3146:2001 |
|
DIN EN 3149 |
Aerospace series - Shank nuts - Installation holes, 60° swage, flanges - Design standard; German version EN 3149:1996 |
|
DIN EN 3151 |
Aerospace series - Dowels, plain, in heat resisting nickel base alloy NI-P100HT (Inconel 718); German version EN 3151:1995 |
|
DIN EN 3152 |
Aerospace series - Nuts, self-locking, MJ threads, in heat resisting steel FE-PA2601 (A286), silver plated or uncoated - Classification: 1100 MPa (at ambient temperature)/425 °C - Technical specification; German and English version EN 3152:2004 |
|
DIN EN 3155-001 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 001: Technical specification |
|
DIN EN 3155-002 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 002: List and utilization of contacts |
|
DIN EN 3155-003 |
Aerospace series - Electrical contacts used in elements of connection - Part 003: Contacts, electrical, female, type A, crimp, class S - Product standard; German and English version EN 3155-003:2005 |
|
DIN EN 3155-004 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 004: Contacts, electrical, male, type A, crimp, class T; product standard |
|
DIN EN 3155-005 |
Aerospace series - Electrical contacts used in elements of connection - Part 005: Contacts, electrical, female, type A, crimp, class T - Product standard; German and English version EN 3155-005:2006 |
|
DIN EN 3155-005 Berichtigung 1 |
Aerospace series - Electrical contacts used in elements of connection - Part 005: Contacts, electrical, female, type A, crimp, class T - Product standard; German and English version EN 3155-005:2006, Corrigenda to DIN EN 3155-005:2006-10; German and English version EN 3155-005:2006/AC:2006 |
|
DIN EN 3155-008 |
Aerospace series - Electrical contacts used in elements of connection - Part 008: Contacts, electrical, male, type A, crimp, class S - Product standard; German and English version EN 3155-008:2005 |
|
DIN EN 3155-009 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 009: Contacts, electrical, female, type A, crimp, class S; product standard |
|
DIN EN 3155-012 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 012: Contacts, electrical, triaxial, size 8, male, type D, solder, class R; product standard |
|
DIN EN 3155-013 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 013: Contacts, electrical, triaxial, size 8, female, type D, solder, class R; product standard |
|
DIN EN 3155-014 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 014: Contacts, electrical, male, type A, crimp, class S; product standard |
|
DIN EN 3155-015 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 015: Contacts, electrical, female, type A, crimp, class S; product standard |
|
DIN EN 3155-016 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 016: Contacts, electrical, male, type A, crimp, class S; product standard |
|
DIN EN 3155-017 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 017: Contacts, electrical, relay base, female, type A, crimp, class P; product standard |
|
DIN EN 3155-018 |
Aerospace series - Electrical contacts used in elements of connection - Part 018: Contacts, electrical, male, type A, crimp, class S - Product standard; German and English version EN 3155-018:2005 |
|
DIN EN 3155-019 |
Aerospace series - Electrical contacts used in elements of connection - Part 019: Contacts, electrical, female, type A, crimp, class S - Product standard; German and English version EN 3155-019:2005 |
|
DIN EN 3155-022 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 022: Contacts, electrical rectangular, male, type A, crimp, class R; product standard |
|
DIN EN 3155-023 |
Aerospace series - Electrical contacts used in elements of connection - Part 023: Contacts, electrical rectangular, female, type A, crimp, class R - Product standard; German and English version EN 3155-023:2006 |
|
DIN EN 3155-026 |
Aerospace series - Electrical contacts used in elements of connection - Part 026: Contacts, electrical, male, type A, crimp, class R - Product standard; German and English version EN 3155-026:2006 |
|
DIN EN 3155-027 |
Aerospace series - Electrical contacts used in elements of connection - Part 027: Contacts, electrical, female, type A, crimp, class R - Product standard; German and English version EN 3155-027:2006 |
|
DIN EN 3155-028 |
Aerospace series - Electrical contacts used in elements of connection - Part 028: Contacts, electrical, coaxial, shielded, size 16, male, type D, crimp, class R - Product standard; German and English version EN 3155-028:2006 |
|
DIN EN 3155-042 |
Aerospace series - Electrical contacts used in elements of connection - Part 042: Contacts, electrical, triaxial, size 08, male 042, type D, solder, class P - Product standard; German and English version EN 3155-042:2006 |
|
DIN EN 3155-043 |
Aerospace series - Electrical contacts used in elements of connection - Part 043: Contacts, electrical, triaxial, size 08, female 043, type D, solder, class P - Product standard; German and English version EN 3155-043:2006 |
|
DIN EN 3155-044 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 044: Contacts, electrical, male 044, type A, double crimping, class T; product standard |
|
DIN EN 3155-045 |
Aerospace series - Electrical contacts used in elements of connection - Part 045: Contacts, electrical, female, type A, double crimping, class T - Product standard; German and English version EN 3155-045:2006 |
|
DIN EN 3155-046 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 046: Contacts, electrical, male, type A, double crimping, class S; product standard |
|
DIN EN 3155-047 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 047: Contacts, electrical, female, type A, double crimping, class S; product standard |
|
DIN EN 3155-052 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 052: Contacts, electrical, male 052, type A, crimp, class S, product standard |
|
DIN EN 3155-053 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 053: Contacts, electrical, female 053, type A, crimp, class S, product standard |
|
DIN EN 3155-054 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 054: Contacts, electrical, male, thermocouple NiAl, type C, crimp, class T; Product standard |
|
DIN EN 3155-055 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 055: Contacts, electrical, female, thermocouple NiAl, type C, crimp, class T; Product standard |
|
DIN EN 3155-056 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 056: Contacts, electrical, male, thermocouple NiCr, type C, crimp, class T; Product standard |
|
DIN EN 3155-057 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 057: Contacts, electrical, female, thermocouple NiCr, type C, crimp, class T; Product standard |
|
DIN EN 3155-058 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 058: Contacts, electrical, coaxial, size 16, male, type D, solder, class R; Product standard |
|
DIN EN 3155-059 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 059: Contacts, electrical, coaxial, size 16, female, type D, solder, class R; Product standard |
|
DIN EN 3155-060 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 060: Contacts, electrical, coaxial, size 12, male, type D, solder, class R; Product standard |
|
DIN EN 3155-061 |
(DRAFT) Aerospace series - Electrical contacts used in elements of connection - Part 061: Contacts, electrical, coaxial, size 12, female, type D, solder, class R; Product standard |
|
DIN EN 3160 |
(DRAFT) Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Bar, a or D ≤ 200 mm, Rm ≥ 1310 MPa |
|
DIN EN 3162 |
(DRAFT) Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Sheet and strip, a ≤ 6 mm, Rm ≥ 930 MPa |
|
DIN EN 3163 |
(DRAFT) Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, softened - Forging stock, a or D ≤ 300 mm |
|
DIN EN 3196 |
Aerospace series - Nuts, hexagonal, self-locking, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 1100 MPa (at ambient temperature)/425 °C; German version EN 3196:1994 |
|
DIN EN 3197 |
(DRAFT) Aerospace series; installation of aircraft electrical and optical interconnection systems |
|
DIN EN 3199 |
(DRAFT) Aerospace series - Lead-acid batteries for aircraft - Technical specification |
|
DIN EN 3202 |
Aerospace series - Holes and traps for T-head bolts - Design standard; German version EN 3202:1995 |
|
DIN EN 3212 |
Aerospace series - Paints and varnishes - Corrosion test by alternate immersion in a buffered sodium chloride solution; German version EN 3212:1995 |
|
DIN EN 3218-001 |
Aerospace series - Connectors, rectangular, with metallic shells and screw-locking - Part 001: Technical specification; German and English version EN 3218-001:2006 |
|
DIN EN 3218-002 |
Aerospace series - Connectors, rectangular, with metallic shells and screw-locking - Part 002: Specification of performance and contact arrangements; German and English version EN 3218-002:2006 |
|
DIN EN 3218-005 |
Aerospace series - Connectors, rectangular, with metallic shells and screw-locking - Part 005: Plug with non-removable size 22 solder contacts - Product standard; German and English version EN 3218-005:2006 |
|
DIN EN 3218-006 |
Aerospace series - Connectors, rectangular, with metallic shells and screw-locking - Part 006: Receptacle with non-removable size 22 solder contacts - Product standard; German and English version EN 3218-006:2006 |
|
DIN EN 3218-007 |
Aerospace series - Connectors, rectangular, with metallic shells and screw-locking - Part 007: Plug with rear-removable size 20 crimp contacts - Product standard; German and English version EN 3218-007:2006 |
|
DIN EN 3218-008 |
Aerospace series - Connectors, rectangular, with metallic shells and screw-locking - Part 008: Receptacle with rear-removable size 20 crimp contacts - Product standard; German and English version EN 3218-008:2006 |
|
DIN EN 3218-009 |
Aerospace series - Connectors, rectangular, with metallic shells and screws-locking - Part 009: Protective covers for EN 3218-005 and EN 3218-007 connectors - Product standard; German and English version EN 3218-009:2006 |
|
DIN EN 3218-010 |
Aerospace series - Connectors, rectangular, with metallic shells and screws-locking - Part 010: Protective covers for EN 3218-006 and EN 3218-008 connectors - Product standard; German and English version EN 3218-010:2006 |
|
DIN EN 3218-011 |
Aerospace series - Connectors, rectangular, with metallic shells and screws-locking - Part 011: Tool, insert extraction for EN 3218-005 to EN 3218-008 connectors - Product standard; German and English version EN 3218-011:2006 |
|
DIN EN 3220 |
(DRAFT) Aerospace series; heat resisting nickel base alloy (Ni-P101 HT); cold worked and softened; bar and wire for continuous forging or extrusion for fasteners 3 ≤ D ≤ 30 mm |
|
DIN EN 3225-1 |
(DRAFT) Aerospace series; heat resisting alloys produced from atomized powder, powder, compacted forging stock and and parts; technical specification; part 1: general requirements |
|
DIN EN 3225-2 |
(DRAFT) Aerospace series; heat resisting alloys produced from atomized powder, powder, compacted forging stock and and parts; technical specification; part 2: atomized powder |
|
DIN EN 3225-3 |
(DRAFT) Aerospace series; heat resisting alloys produced from atomized powder, powder, compacted forging stock and and parts; technical specification; part 3: hot compacted forging stock |
|
DIN EN 3225-4 |
(DRAFT) Aerospace series; heat resisting alloys produced from atomized powder, powder, compacted forging stock and and parts; technical specification; part 4: pre-production and production parts |
|
DIN EN 3226 |
(DRAFT) Aerospace series; nuts, hexagon, plain, normal height, normal across flats, in steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 3229 |
(DRAFT) Aerospace series; nuts, hexagon, plain, reduced height, normal across flats, in steel, cadmium plated, left hand thread; classification: 900 MPa (at ambient temperature)/235 °C |
|
DIN EN 3230 |
Aerospace series - Nuts, hexagon, slotted/castellated, reduced height, normal across flats, in steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C; German version EN 3230:2001 |
|
DIN EN 3235-1 |
(DRAFT) Aerospace series; heat resisting alloys; wrought products; technical specification; part 1: general requirements |
|
DIN EN 3235-2 |
(DRAFT) Aerospace series; heat resisting alloys; wrought products; technical specification; part 2: plate, sheet and strip |
|
DIN EN 3235-3 |
(DRAFT) Aerospace series; heat resisting alloys; wrought products; technical specification; part 3: bar and section |
|
DIN EN 3235-4 |
(DRAFT) Aerospace series; heat resisting alloys; wrought products; technical specification; part 4: seamless tube |
|
DIN EN 3235-5 |
(DRAFT) Aerospace series; heat resisting alloys; wrought products; technical specification; part 5: wire |
|
DIN EN 3236 |
Aerospace series - Inserts, thin wall, self-locking, short, in heat resisting nickel base alloy NI-P100HT (Inconel 718) - Silver plated internal thread; German version EN 3236:1998 |
|
DIN EN 3237 |
Aerospace series - Inserts, thin wall, self-locking, long, in heat resisting nickel base alloy NI-P100 HT (Inconel 718) - Silver plated internal thread; German version EN 3237:1998 |
|
DIN EN 3239 |
Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-P101HT (Waspaloy), silver plated thread - Classification: 1210 MPa (at ambient temperature)/650 °C; German version EN 3239:1995 |
|
DIN EN 3240 |
(DRAFT) Aerospace series; nuts, self-locking, clip, in heat resisting steel FE-PA92HT (A286) uncoated, classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 3241 |
(DRAFT) Aerospace series; nuts, self-locking, clip, in heat resisting steel FE-PA92HT (A286), silver coated, classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 3243 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Ferrule welded, with dynamic beam seal end; German version EN 3243:2001 |
|
DIN EN 3244 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, double ended; German version EN 3244:2001 |
|
DIN EN 3245 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, reducer; German version EN 3245:2001 |
|
DIN EN 3246 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, bulkhead; German version EN 3246:2001 |
|
DIN EN 3247 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, bulkhead, welded end; German version EN 3247:2001 |
|
DIN EN 3248 |
Aerospace series - Pipe coupling 8°30' in titanium alloy - Adapters, reduced pipe end, with locking ring; German and English version EN 3248:2001 |
|
DIN EN 3264 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Thrust wire nuts; German version EN 3264:2001 |
|
DIN EN 3266 |
Aerospace series - Pipe coupling in titanium alloy - Bulkhead nut; German version EN 3266:2001 |
|
DIN EN 3267 |
Aerospace series - Washers, bulkhead, in titanium alloy; German version EN 3267:2001 |
|
DIN EN 3268 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Pressure plug; German version EN 3268:2001 |
|
DIN EN 3269 |
Aerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, blind, with dynamic beam seal end; German and English version EN 3269:2001 |
|
DIN EN 3270 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Blanking plugs with lockring; German and English version EN 3270:2001 + AC:2003 |
|
DIN EN 3272 |
Aerospace series - Pipe coupling 8°30' - Dynamic beam seal end for ferrule, welded - Geometric configuration; German and English version EN 3272:2001 |
|
DIN EN 3273 |
Aerospace series - Pipe coupling 8°30′ - Dynamic beam seal end for elbows, tees and crosses - Geometric configuration; German and English version EN 3273:2001 |
|
DIN EN 3274 |
Aerospace series - Pipe coupling 8°30′ - Threaded; Geometric configuration; German version EN 3274:2001 |
|
DIN EN 3275 |
Aerospace series - Pipe coupling 8°30′ up to 28000 kPa - Dynamic beam seal; Metric series; Technical specification; German and English version EN 3275:2002 |
|
DIN EN 3280/A1 |
(DRAFT) Aerospace series - Bearings, airframe rolling, rigid or self-aligning - Technical specification; Amendment A1 |
|
DIN EN 3281 |
Aerospace series; bearings, airframe rolling - Rigid single row ball bearings in steel - Diameter series 8 and 9; dimensions and loads; German version EN 3281:1994 |
|
DIN EN 3282 |
Aerospace series; bearings, airframe rolling - Rigid single row ball bearings in steel, cadmium plated - Diameter series 8 and 9; dimensions and loads; German version EN 3282:1994 |
|
DIN EN 3283 |
Aerospace series; bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel - Diameter series 8 and 9; dimensions and loads; German version EN 3283:1994 |
|
DIN EN 3286 |
Aerospace series; bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel - Diameter series 0 and 2; normal clearance category; dimensions and loads; German version EN 3286:1994 |
|
DIN EN 3287 |
Aerospace series; bearings, airframe rolling - Double row self-aligning ball bearings in steel - Diameter series 2; dimensions and load; German version EN 3287:1994 |
|
DIN EN 3288 |
Aerospace series; bearings, airframe rolling - Double row self-aligning ball bearings in steel, cadmium plated - Diameter series 2; dimensions and loads; German version EN 3288:1994 |
|
DIN EN 3290 |
Aerospace series; bearings, airframe rolling - Single row self-aligning roller bearings in steel - Diameter series 3 and 4; dimensions and loads; German version EN 3290:1994 |
|
DIN EN 3291 |
Aerospace series; bearings, airframe rolling - Single row self-aligning roller bearings in steel, cadmium plated - Diameter series 3 and 4; dimensions and loads; German version EN 3291:1994 |
|
DIN EN 3292 |
Aerospace series; bearings, airframe rolling - Single row self-aligning roller bearings in corrosion resisting steel - Diameter series 3 and 4; dimensions and loads; German version EN 3292:1994 |
|
DIN EN 3295 |
(DRAFT) Aerospace series; shaft-nuts, self-locking, in FE-PA92HT (A286), silver plated |
|
DIN EN 3295/A1 |
(DRAFT) Aerospace series - Shaft-nuts, self-locking, in FE-PA92HT (A286), silver plated; Amendment A1 |
|
DIN EN 3297 |
Aerospace series - Inserts, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-P100HT (Inconel 718) - Technical specification; German version EN 3297:1998 |
|
DIN EN 3298 |
Aerospace series - Inserts, thin wall, self-locking - Installation and removal procedure; German version EN 3298:1998 |
|
DIN EN 3299 |
(DRAFT) Aerospace series - Shaft-nuts and threaded rings, self-locking, right- or left-hand MJ threads, in heat resisting steel FE-PA2601 (A286), silver plated - Technical specification |
|
DIN EN 3303 |
Aerospace series - Screws, cap head, hexagon socket, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1100 MPa (at ambient temperature)/235 °C; German version EN 3303:1997 |
|
DIN EN 3304 |
Aerospace series - Screws, 100° countersunk reduced head, offset cruciform recess, close tolerance shank, short thread, in titanium alloy, MoS2 lubricated, classification: 1100 MPa (at ambient temperature)/315 °C; German version EN 3304:1996 |
|
DIN EN 3305 |
Aerospace series - Screws, 100° countersunk head, offset cruciform recess, close tolerance shank, short thread, in alloy steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C; German version EN 3305:1996 |
|
DIN EN 3306 |
Aerospace series - Screws, 100° countersunk normal head, offset cruciform recess, threaded to head, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C; German version EN 3306:1996 |
|
DIN EN 3307 |
Aerospace series - Screws, pan head, offset cruciform recess, threaded to head, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C; German version EN 3307:1996 |
|
DIN EN 3308 |
Aerospace series - Screws, normal hexagonal head, threaded to head, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C; German version EN 3308:1996 |
|
DIN EN 3310 |
(DRAFT) Aerospace series - Titanium alloy TI-P64001 - Not heat treated, grade 2 forging stock for annealed forgings a or D ≤ 360 mm |
|
DIN EN 3311 |
(DRAFT) Aerospace series - Titanium alloy TI-P64001, annealed - Bar for machining D ≤ 150 mm |
|
DIN EN 3312 |
(DRAFT) Aerospace series - Titanium alloy TI-P64001 - Grade 2, annealed, forgings D e ≤ 150 mm |
|
DIN EN 3313 |
(DRAFT) Aerospace series - Titanium alloy TI-P64001 - Not heat treated, grade 2 forging stock for solution treated and aged forgings a or D ≤ 360 mm |
|
DIN EN 3314 |
(DRAFT) Aerospace series - Titanium alloy TI-P64001, solution treated and aged; bar for machining D ≤ 75 mm |
|
DIN EN 3315 |
(DRAFT) Aerospace series - Titanium alloy TI-P64001, solution treated and aged - Forgings De ≤ 75 mm |
|
DIN EN 3318 |
(DRAFT) Aerospace series - Titanium alloy TI-P64002 - Not heat treated, grade 2 forging stock for annealed forgings a or D ≤ 360 mm |
|
DIN EN 3319 |
(DRAFT) Aerospace series - Titanium alloy TI-P64002, annealed; bar for machining D ≤ 80 mm |
|
DIN EN 3320 |
(DRAFT) Aerospace series - Titanium alloy TI-P64002 - Grade 2, annealed, forgings De ≤ 150 mm |
|
DIN EN 3321 |
(DRAFT) Aerospace series - Titanium alloy TI-P65001, as forged - Grade 1 forging stock, for solution treated and aged forgings a or D≤ 360 mm |
|
DIN EN 3322 |
(DRAFT) Aerospace series - Titanium alloy TI-P65001, solution treated and aged - Grade 1-forgings De ≤ 75 mm |
|
DIN EN 3332 |
Aerospace series - Aluminium alloy AL-P7475-T762 - Clad sheet and strip - 1,0 mm ≤ a ≤ 6 mm; German and English version EN 3332:2005 |
|
DIN EN 3333 |
Aerospace series - Aluminium alloy AL-P7475-T762 - Sheet and strip - 0,6 mm ≤ a ≤ 6 mm; German and English version EN 3333:2005 |
|
DIN EN 3336 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7150-T651 - Plate, 6 mm < a ≤ 40 mm |
|
DIN EN 3338 |
Aerospace series - Aluminium alloy AL-P7050-T74511 - Extruded bar and section - a or D ≤ 150 mm with peripheral coarse grain control; German and English version EN 3338:2005 |
|
DIN EN 3339 |
Aerospace series - Aluminium alloy AL-P7010-T76 - Die forgings - a = 200 mm; German and English version EN 3339:2006 |
|
DIN EN 3341 |
Aerospace series - Aluminium alloy AL-P6061-T4 or T42 - Sheet and strip - 0,4 mm ≤ a ≤ 6 mm; German and English version EN 3341:2005 |
|
DIN EN 3342 |
Aerospace series - Aluminium alloy AL-P6061-T4 or T42 - Drawn or extruded bar and section - a or D ≤ 150 mm; German and English version EN 3342:2005 |
|
DIN EN 3344 |
Aerospace series - Aluminium alloy AL-P7050-T76511 - Extruded bar and section - a or D ≤ 150 mm with peripheral coarse grain control; German and English version EN 3344:2005 |
|
DIN EN 3346 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2014A-T3 - Drawn tube for structural applications; 0,6 mm ≤ a ≤ 12,5 mm |
|
DIN EN 3347 |
Aerospace series - Aluminium alloy AL-P2024-T8511 - Extruded bar and section - a or D ≤ 150 mm with peripheral coarse grain control; German and English version EN 3347:2005 |
|
DIN EN 3351 |
(DRAFT) Aerospace series - Titanium alloy TI-P63001 - Grade 2, solution treated and aged, forgings De ≤ 150 mm |
|
DIN EN 3354 |
(DRAFT) Aerospace series - Titanium alloy TI-P64001, annealed - Sheet for superplastic forming a ≤ 6 mm |
|
DIN EN 3355 |
(DRAFT) Aerospace series - Titanium alloy TI-P64001, annealed - Extruded section, De ≤ 150 mm, 900 MPa ≤ Rm 1160 MPa |
|
DIN EN 3356 |
(DRAFT) Aerospace series - Titanium alloy TI-P46001 - Grade 2, solution treated and aged, forgings De ≤ 100 mm |
|
DIN EN 3359 |
(DRAFT) Aerospace series - Steel FE-PM1503 (X3CrNiMoAl 13-8-2), vacuum induction melted and consumable electrode remelted, softened - Forging stocks a or D ≤ 300 mm |
|
DIN EN 3361 |
(DRAFT) Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) consumable electrode remelted, solution treated and precipitation treated - Sheet and strip a ≤ 6 mm, 1070 MPa ≤ Rm ≤ 1220 MPa |
|
DIN EN 3364 |
(DRAFT) Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) consumable electrode remelted, softened - Forging stock a or D ≤ 300 mm |
|
DIN EN 3365 |
(DRAFT) Aerospace series - Steel FE-PM3901 (X15CrNi17-3) air melted, softened - Forging stocks a or D ≤ 300 mm |
|
DIN EN 3369 |
(DRAFT) Aerospace series; rivets, solid, universal head, in aluminium alloy 7050, anodized or chromated, inch based series |
|
DIN EN 3370 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head with dome, in aluminium alloy 7050, anodized or chromated; inch based series |
|
DIN EN 3373-001 |
(DRAFT) Aerospace series - Terminal lugs and in-line splices for crimping on electric conductors - Part 001: Technical specification |
|
DIN EN 3373-012 |
Aerospace series - Terminal lugs and in-line splices for crimping on electric conductors - Part 012: In-line splices, insulated and sealed, for crimping on copper conductors, temperature up to 150 °C - Product standard; German and English version EN 3373-012:2005 |
|
DIN EN 3373-013 |
Aerospace series - Terminal lugs and in-line splices for crimping on electric conductors - Part 013: In-line splices, insulated and moisture resistant, for crimping on copper conductors, temperature up to 260°C - Product standard; German and English version EN 3373-013:2005 |
|
DIN EN 3377 |
Aerospace series - Nuts, hexagonal, self-locking, in heat resisting steel FE-PA92HT (A286) - Classification: 1100 MPa (at ambient temperature)/425 °C; German version EN 3377:1996 |
|
DIN EN 3378 |
(DRAFT) Aerospace series - Titanium TI-P99002, annealed - Wire for rivet 1,6 mm ≤ D ≤ 10 mm |
|
DIN EN 3379 |
Aerospace series - Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), for increased height nuts - Classification: 1210 MPa (at ambient temperature)/730 °C; German version EN 3379:1996 |
|
DIN EN 3381 |
Aerospace series - Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in titanium, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C; German version EN 3381:1996 |
|
DIN EN 3384 |
(DRAFT) Aerospace series; rings retaining, external, axial mounting, steel, phosphated |
|
DIN EN 3385 |
(DRAFT) Aerospace series; rings retaining, external, axial mounting, steel, vacuum cadmium plated |
|
DIN EN 3395 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head with dom, in aluminium alloy 2017A; metric series |
|
DIN EN 3396 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head with dom, in aluminium alloy 5056A; metric series |
|
DIN EN 3397 |
(DRAFT) Aerospace series; rivets, solid, universal head, in aluminium alloy 7050; metric series |
|
DIN EN 3398 |
(DRAFT) Aerospace series; rivets, solid, universal head, in aluminium alloy 7050, anodized or chromated, metric series |
|
DIN EN 3399 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head, in aluminium alloy 5056A; metric series |
|
DIN EN 3400 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head, in aluminium alloy 5056A, anodized or chromated; metric series |
|
DIN EN 3401 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head, in aluminium alloy 7050; metric series |
|
DIN EN 3403 |
(DRAFT) Aerospace series; rivets, solid, universal head, in aluminium alloy 5056A; metric series |
|
DIN EN 3405 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head with dome, in aluminium alloy 7050, anodized or chromated; metric series |
|
DIN EN 3408 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head in aluminium alloy 2017A; metric series |
|
DIN EN 3409 |
(DRAFT) Aerospace series; rivets, solid, universal head, in aluminium 1050A, metric series |
|
DIN EN 3410 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head, in aluminium 1050A; metric series |
|
DIN EN 3411 |
(DRAFT) Aerospace series; rivets, solid, universal head, in aluminium alloy 2017A; metric series |
|
DIN EN 3412 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head with dome, in aluminium alloy 5056A, anodized or chromated; metric series |
|
DIN EN 3413 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head with dome, in aluminium alloy 7050; metric series |
|
DIN EN 3414 |
(DRAFT) Aerospace series - Rivets, solid, universal head, in corrosion resisting steel FE-PA92HT, passivated - Metric series |
|
DIN EN 3415 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk normal head, in corrosion resisting steel FE-PA92HT, passivated - Metric series |
|
DIN EN 3416 |
(DRAFT) Aerospace series; rivets, solid, universal head, in nickel base alloy NI-P11, cadmium plated; metric series |
|
DIN EN 3417 |
(DRAFT) Aerospace series; rivets, solid, universal head, in nickel base alloy NI-P11; metric series |
|
DIN EN 3418 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head, in nickel base alloy NI-P11, cadmium plated; metric series |
|
DIN EN 3419 |
(DRAFT) Aerospace series; rivets, solid, 100° normal countersunk head, in nickel base alloy NI-P11; metric series |
|
DIN EN 3420 |
(DRAFT) Aerospace series - Rivets, solid, universal head, in corrosion resisting steel FE-PA11, passivated - Metric series |
|
DIN EN 3421 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk normal head, in corrosion resisting steel FE-PA11, passivated - Metric series |
|
DIN EN 3422 |
(DRAFT) Aerospace series - Rivets, solid, universal head, in titanium TI-PO2, anodized - Metric series |
|
DIN EN 3424 |
(DRAFT) Aerospace series; rivets, solid, universal head, in titanium alloy Ti 45,5 Cb; metric series |
|
DIN EN 3425 |
(DRAFT) Aerospace series; groove dimensions for axial mounting internal type retaining rings |
|
DIN EN 3425 |
Aerospace series - Groove dimensions for axial mounting internal type retaining rings; German and English version EN 3425:2006 |
|
DIN EN 3426 |
(DRAFT) Aerospace series; groove dimensions for axial mounting external type retaining rings |
|
DIN EN 3426 |
Aerospace series - Groove dimensions for axial mounting external type retaining rings; German and English version EN 3426:2006 |
|
DIN EN 3427 |
(DRAFT) Aerospace series; groove dimensions for radial mounting retaining rings |
|
DIN EN 3427 |
Aerospace series - Groove dimensions for radial mounting retaining rings; German and English version EN 3427:2006 |
|
DIN EN 3431 |
(DRAFT) Aerospace series - Nuts, hexagonal, self-locking, with counterbore and captive washer, in heat resisting steel, silver plated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 3434 |
(DRAFT) Aerospace series - Nuts, hexagon, slotted/castellated, self-locking, in steel, cadmium plated, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/235 °C |
|
DIN EN 3435 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, floating, two lug, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 3436 |
(DRAFT) Aerospace series - Lead-acid batteries for aircraft of format A type - Product standard |
|
DIN EN 3437 |
(DRAFT) Aerospace series - Lead-acid batteries for aircraft of format B type - Product standard |
|
DIN EN 3438 |
(DRAFT) Aerospace series - Lead-acid batteries for aircraft of format C type - Product standard |
|
DIN EN 3439 |
(DRAFT) Aerospace series - Lead-acid batteries for aircraft of format D type - Product standard |
|
DIN EN 3441 |
(DRAFT) Aerospace series; titanium TI-P99001; annealed, sheet and strip, hot rolled, a ≤ 6 mm, 290 MPa ≤ Rm ≤ 420 MPa |
|
DIN EN 3442 |
(DRAFT) Aerospace series; titanium TI-P99002; annealed, sheet and strip, hot rolled, a ≤ 6 mm, 390 MPa ≤ Rm ≤ 540 MPa |
|
DIN EN 3444 |
(DRAFT) Aerospace series - Bolts, large hexagon head, close tolerance normal shank, medium length thread, in heat resisting nickel base alloy, passivated - Classification: 1250 MPa (at ambient temperature)/650 °C |
|
DIN EN 3446 |
Aerospace series - Bearings, precision ball, without flange, in corrosion resisting steel, for instruments and equipment - Dimensions and loads; German version EN 3446:1995 |
|
DIN EN 3451 |
(DRAFT) Aerospace series - Titanium TI-P99002 - Not heat treated, grade 2 forging stock for annealed forgings a or D ≤ 300 mm |
|
DIN EN 3452 |
(DRAFT) Aerospace series - Titanium TI-P99002 - Grade 2, annealed, forgings De ≤ 150 mm |
|
DIN EN 3453 |
(DRAFT) Aerospace series - Titanium TI-P99003 - Not heat treated, grade 2 forging stock for annealed forgings a or D ≤ 300 mm |
|
DIN EN 3454 |
(DRAFT) Aerospace series - Titanium alloy TI-P19001 - Not heat treated, grade 2 forging stock for annealed forgings a or D ≤ 300 mm |
|
DIN EN 3455 |
(DRAFT) Aerospace series - Titanium alloy TI-P19001 - Not heat treated, grade 2 forging stock for solution treated and aged forgings a or D ≤ 300 mm |
|
DIN EN 3456 |
(DRAFT) Aerospace series; titanium alloy TI-P64001; annealed, sheet and strip, hot rolled, a ≤ 6 mm |
|
DIN EN 3459 |
(DRAFT) Aerospace series - Titanium alloy TI-P63001, solution treated and aged - Plates 6 mm |
|
DIN EN 3460 |
(DRAFT) Aerospace series - Titanium TI-P99002, annealed - Bar for machining a or D ≤ 150 mm, Rm ≥ 390 MPa |
|
DIN EN 3461 |
(DRAFT) Aerospace series - Titanium alloy TI-P99003, annealed - Bar for machining D ≤ 150 mm, 540 MPa ≤ Rm ≤ 740 MPa |
|
DIN EN 3462 |
(DRAFT) Aerospace series - Titanium alloy TI-P19001, annealed - Bar for machining D ≤ 150 mm |
|
DIN EN 3463 |
(DRAFT) Aerospace series - Titanium alloy TI-P19001, solution treated and aged; bar for machining D ≤ 75 mm |
|
DIN EN 3465 |
(DRAFT) Aerospace series - Titanium alloy TI-P63001 - Not heat treated, grade 2 forging stock for solution treated and aged forgings a or D ≤ 360 mm |
|
DIN EN 3466 |
(DRAFT) Aerospace series - Titanium alloy TI-P63001, solution treated and aged; bar for machining D ≤ 150 mm |
|
DIN EN 3467 |
(DRAFT) Aerospace series - Titanium alloy TI-C64001, not heat treated - Remelting stock, D e ≤ 300 mm |
|
DIN EN 3469 |
(DRAFT) Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) consumable electrode remelted, solution treated and precipitation treated - Forgings a or D ≤ 200 mm, Rm ≥ 1310 MPa |
|
DIN EN 3470 |
(DRAFT) Aerospace series - Steel FE-PM1503 (X3CrNiMoAL 13-8-2), vacuum induction melded and consumable electrode remelded, solution treated and precipitation treated - Hand and die forgings, a oder D ≤ 150 mm, 1200 MPa ≤ Rm ≤ 1400 MPa |
|
DIN EN 3474 |
Aerospace series - Aluminium alloy AL-P2024-T81 - Sheet and strip - 0,25 mm ≤ a ≤ 6 mm; German and English version EN 3474:2005 |
|
DIN EN 3475-100 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 100: General; German version EN 3475-100:2002 |
|
DIN EN 3475-201 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 201: Visual examination; German version EN 3475-201:2002 |
|
DIN EN 3475-202 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 202: Mass; German version EN 3475-202:2002 |
|
DIN EN 3475-203 |
Aerospace series - Cables, electrical, aircraft use - Test methods - Part 203: Dimensions; German and English version EN 3475-203:2006 |
|
DIN EN 3475-301 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 301: Electrical resistance per unit length; German version EN 3475-301:2002 |
|
DIN EN 3475-302 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 302: Voltage proof test; German version EN 3475-302:2002 |
|
DIN EN 3475-303 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 303: Insulation resistance; German version EN 3475-303:2002 |
|
DIN EN 3475-304 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 304: Surface resistance; German version EN 3475-304:2002 |
|
DIN EN 3475-305 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 305: Overload resistance; German version EN 3475-305:2002 |
|
DIN EN 3475-307 |
Aerospace series - Cables, electrical, aircraft use - Test methods - Part 307: Corona extinction voltage; German and English version EN 3475-307:2005 |
|
DIN EN 3475-401 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 401: Accelerated ageing; German version EN 3475-401:2002 |
|
DIN EN 3475-402 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 402: Shrinkage and delamination; German version EN 3475-402:2002 |
|
DIN EN 3475-403 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 403: Delamination and blocking; German version EN 3475-403:2002 |
|
DIN EN 3475-404 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 404: Thermal shock; German version EN 3475-404:2002 |
|
DIN EN 3475-405 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 405: Bending at ambient temperature; German version EN 3475-405:2002 |
|
DIN EN 3475-406 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 406: Cold bend test; German version EN 3475-406:2002 |
|
DIN EN 3475-407 |
Aerospace series - Cable, electrical, aircraft use - Test methods - Part 407: Flammability; German and English version EN 3475-407:2005 |
|
DIN EN 3475-408 |
Aerospace series - Cables, electrical, aircraft use - Test methods - Part 408: Fire resistance; German and English version EN 3475-408:2005 |
|
DIN EN 3475-409 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 409: Air-excluded ageing; German version EN 3475-409:2002 |
|
DIN EN 3475-410 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 410: Thermal endurance; German version EN 3475-410:2002 |
|
DIN EN 3475-411 |
Aerospace series - Cables, electrical, aircraft use - Test methods - Part 411: Resistance to fluids; German and English version EN 3475-411:2005 |
|
DIN EN 3475-412 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 412: Humidity resistance; German and English version EN 3475-412:2002 |
|
DIN EN 3475-413 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 413: Wrap back test; German and English version EN 3475-413:2002 |
|
DIN EN 3475-415 |
Aerospace series - Cables, electrical, aircraft use - Test methods - Part 415: Rapid change of temperature; German and English version EN 3475-415:2005 |
|
DIN EN 3475-416 |
Aerospace series - Cables, electrical, aircraft use - Test methods - Part 416: Thermal stability; German and English version EN 3475-416:2005 |
|
DIN EN 3475-501 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 501: Dynamic cut-through; German version EN 3475-501:2002 |
|
DIN EN 3475-502 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 502: Notch propagation; German version EN 3475-502:2002 |
|
DIN EN 3475-503 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 503: Scrape abrasion; German version EN 3475-503:2002 |
|
DIN EN 3475-504 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 504: Torsion; German version EN 3475-504:2002 |
|
DIN EN 3475-505 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 505: Tensile test on conductors and strands; German version EN 3475-505:2002 |
|
DIN EN 3475-506 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 506: Plating continuits; German version EN 3475-506:2002 |
|
DIN EN 3475-507 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 507: Adherence of plating; German version EN 3475-507:2002 |
|
DIN EN 3475-508 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 508: Plating thickness; German and English version EN 3475-508:2002 |
|
DIN EN 3475-509 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 509: Solderability; German and English version EN 3475-509:2002 |
|
DIN EN 3475-510 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 510: Tensile strength and elongation of extruded insulation, sheath and jacket material; German and English version EN 3475-510:2002 |
|
DIN EN 3475-511 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 511: Cable-to-cable abrasion; German and English version EN 3475-511:2002 |
|
DIN EN 3475-513 |
Aerospace series - Cables, electrical, aircraft use - Test methods - Part 513: Deformation resistance (Installation with plastic cable ties); German and English version EN 3475-513:2005 |
|
DIN EN 3475-603 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 603: Resistance to wet arc tracking; German and English version EN 3475-603:2002 |
|
DIN EN 3475-604 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 604: Resistance to dry arc propagation; German and English version EN 3475-604:2002 |
|
DIN EN 3475-605 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 605: Wet short circuit test; German and English version EN 3475-605:2002 |
|
DIN EN 3475-701 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 701: Strippabilitiy and adherence of insulation to the conductor; German version EN 3475-701:2002 |
|
DIN EN 3475-702 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 702: Screen pushback capability; German version EN 3475-702:2002 |
|
DIN EN 3475-703 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 703: Permanence of manufacturer's marking; German version EN 3475-703:2002 |
|
DIN EN 3475-704 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 704: Flexibility; German and English version EN 3475-704:2002 |
|
DIN EN 3475-705 |
Aerospace series - Cables, electrical, aircraft use - Test methods - Part 705: Contrast measurement; German and English version EN 3475-705:2005 |
|
DIN EN 3475-706 |
Aerospace series - Cables, electrical, aircraft use - Test methods - Part 706: Laser markability; German and English version EN 3475-706:2005 |
|
DIN EN 3475-801 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 801: Capacitance per unit length; German and English version EN 3475-801:2002 |
|
DIN EN 3475-802 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 802: Capacitance unbalance; German and English version EN 3475-802:2002 |
|
DIN EN 3475-803 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 803: Capacitance variation; German and English version EN 3475-803:2002 |
|
DIN EN 3475-804 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 804: Velocity of propagation; German and English version EN 3475-804:2002 |
|
DIN EN 3475-805 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 805: Characteristic impedance; German and English version EN 3475-805:2002 |
|
DIN EN 3475-806 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 806: Attenuation; German and English version EN 3475-806:2002 |
|
DIN EN 3475-807 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 807: Transfer impedance; German and English version EN 3475-807:2002 |
|
DIN EN 3475-808 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 808: Cross-talk; German and English version EN 3475-808:2002 |