|
DIN EN 6101 |
(DRAFT) Aerospace series - Rivet, 100° medium flush head, close tolerance - Inch series |
|
DIN 65338 |
Aerospace; hexagon bolts, close tolerance, with short-length MJ thread, shoulder, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
|
DIN EN 6038 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of the compression strength after impact |
|
DIN EN 6062 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; flatwise tensile test of composite sandwich panel |
|
DIN EN 6069 |
(DRAFT) Aerospace series - Rivet, 100° reduced flush head, close tolerance - Inch series |
|
DIN EN 2093 |
Aerospace series; aluminium alloy AL-P7009-T74; hand forgings 20 mm ≤ a ≤ 150 mm; German version EN 2093:1992 |
|
DIN EN 2563 |
Aerospace series - Carbon fibre reinforced plastics - Unidirectional laminates; determination of apparent interlaminar shear strength; German version EN 2563:1997 |
|
DIN EN 3358 |
(DRAFT) Aerospace series - Steel FE-PM1503 (X3CrNiMoAl 13-8-2), vacuum induction melted and consumable electrode remelted, solution treated and precipitation treated - Bar for machining a or D ≤ 150 mm, Rm ≥ 1400 MPa |
|
DIN 65191 |
Aerospace - Inserts for composite materials with MJ thread, threaded part floating and screw-locking, corrosion-resisting steel |
|
DIN 65202 |
Aerospace series - Elastomeric O-rings - Dimensions |
|
DIN 65258 |
Aerospace; rivets, 100° countersunk head, aluminium and aluminium alloys; metric series |
|
DIN 65270 |
Aerospace; nuts, hexagon, slotted/castellated, with MJ thread self-locking, corrosion-resisting steel; classification: 1100 MPa/120 °C |
|
DIN 65350-1 |
Aerospace; riveting; assembly accessibility of riveting tools for solid rivets |
|
DIN 65526 |
Aerospace - Hexagon bolts, close tolerance, with short-length MJ thread, titanium alloy - Nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
|
DIN 65536-2 |
Aerospace; inserts, helical coil threads, screw-locking, copper alloy; assembly and special tools |
|
DIN EN 2395 |
Aerospace series - Aluminium alloy AL-P2014A-T4 or T42 - Sheet and strip - 0,4 mm ≤ a ≤ 6 mm; German and English version EN 2395:2005 |
|
DIN EN 2850 |
(DRAFT) Aerospace series - Carbon fibre thermosetting resin unidirectional laminates - Compression test parallel to fibre direction |
|
DIN EN 3141 |
Aerospace series - Rivets, solid, universal head, in head resisting nickel base alloy NI-P11, cadmium plated, inch based series; German version EN 3141:1996 |
|
DIN EN 3475-512 |
Aerospace series - Cables, electrical, aircraft use; Test methods - Part 512: Flexure endurance; German and English version EN 3475-512:2002 |
|
DIN EN 6035 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of notched and unnotched tensile strength |
|
DIN EN 6037 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of bearing strength |
|
DIN EN 6072 |
(DRAFT) Aerospace series - Metallic materials - Test methods; constant amplitude fatigue testing |
|
DIN EN 9102 |
(DRAFT) Aerospace series - Quality systems - First article inspection |
|
DIN ISO 9152 |
Aerospace - Bolts, with MJ threads, in titanium alloys, strength class 1100 MPa - Procurement specification (ISO 9152:1998) |
|
DIN 65118-1 |
Aerospace; welded metallic component parts; indications on drawings |
|
DIN 65209 |
Aerospace series - Washers, countersunk |
|
DIN 65220 |
Aerospace - Gang channel nut assembly, with self-locking nuts, with MJ thread, nut spacing fixed or optional, channel in aluminium; Classification: 1100 MPa/120 °C |
|
DIN 65236 |
Aerospace; steel, nickel- and cobalt-alloy wire; technical specification |
|
DIN 65238 |
Aerospace - Anchor nuts with MJ thread, deep counterbore, self-locking, non-floating, corner, steel; Classification: 1100 MPa/235 °C |
|
DIN 65265 |
Aerospace - Screws, hexagon bolts with MJ thread, threaded approximately to head, titanium alloy - Nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
|
DIN 65285 |
Aerospace; countersunk head screws, with ribbed TORQ-SET (ACR) recess and MJ thread, short thread length, corrosion-resisting steel, nominal tensile strength 1100 MPa, for temperatures up to 425 °C |
|
DIN 65298 |
Aerospace; universal joints, needle bearing supported, long-time lubricated, for rotary shafts; single joints; connection dimensions, loads, masses |
|
DIN 65299 |
Aerospace; universal joints, needle bearing supported, long-time lubricated, for rotary shafts; double joints; connection dimensions, loads masses |
|
DIN 65306 |
Aerospace; inserts for composite materials, with clearance hole, corrosion resisting steel |
|
DIN 65349 |
Aerospace - Testing of locking torques for nuts and related threaded parts, with metric screw thread - Test methods |
|
DIN 65350-2 |
Aerospace; riveting; assembly accessibility of riveting tools for blind rivets |
|
DIN 65350-3 |
Aerospace; riveting; assembly accessibility of riveting tools for threaded blind rivets |
|
DIN 65350-4 |
Aerospace; riveting; assembly accessibility of riveting tools for close tolerance rivets |
|
DIN 65382 |
Aerospace; reinforcement fibres for plastics; tensile test of impregnated yarn test specimens |
|
DIN 65389 |
Aerospace - Cold-rolled steel sheet - Dimensions, masses |
|
DIN 65397 |
Aerospace - Thread inserts, with MJ thread, locked, screw-locking, corrosion-resisting steel; Classification: 1100 MPa/315 °C/425 °C |
|
DIN 65435 |
Aerospace; sleeves for fasteners; technical specification |
|
DIN 65438 |
Aerospace; bihexagonal head bolts, close tolerance, with MJ-thread, short thread length, in titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
|
DIN 65451 |
Aerospace - Thread inserts, with MJ thread, locked, screw-locking, steel; Classification: 900 MPa/1100 MPa/235 °C |
|
DIN 65455 |
Aerospace; seamless tubes in steel, nickel and titanium alloys; ultrasonic inspection |
|
DIN 65471 |
Aerospace; filler metals for welding titanium and titanium alloys; filler rods and filler wires; dimensions, masses |
|
DIN 65486 |
Aerospace; fasteners for structural application; rotary fasteners, mechanical properties; rotary fastener, assembly, pressure-tight |
|
DIN 65489 |
Aerospace; fasteners for structural and non-structural applications; rotary fasteners; countersunk washer |
|
DIN 65492 |
Aerospace; fasteners for structural application; rotary fasteners; receptacle |
|
DIN 65493 |
Aerospace; fasteners for structural application; rotary fasteners; receptacle, pressure-tight |
|
DIN 65494-101 |
Aerospace; rivet design values, static load, for protruding head rivet joints, single shear; rivet material 3.1124, metric series |
|
DIN 65517 |
Aerospace - Cheese head bolts, close tolerance, with bihexagon socket and MJ thread, short thread, titanium alloy, nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
|
DIN 65536-1 |
Aerospace; inserts, helical coil threads, screw-locking, copper alloy; class: 1100 MPa/425 °C |
|
DIN 65549 |
Aerospace; rivets, close tolerance with 130° flush head, metric series, titanium alloy |
|
DIN 65578 |
Aerospace; quick-release pins in corrosion-resisting steel, single locked, with pull or push release mechanism |
|
DIN 9020-2 |
Aerospace; mass breakdown for aircraft heavier than air; main mass groups and terms of mass; definitions |
|
DIN 9088 |
Aerospace series - Storage life of rubber products |
|
DIN EN 2002-001 |
Aerospace series - Metallic materials - Test methods - Part 1: Tensile testing at ambient temperature; German and English version EN 2002-001:2005 |
|
DIN EN 2066 |
Aerospace series - Extruded section in aluminium alloys - General tolerances; German and English version EN 2066:2001 |
|
DIN EN 2079 |
Aerospace series - Bearings, precision ball, with flange, in corrosion resisting steel, for instruments and equipment - Dimensions and loads; German version EN 2079:1995 |
|
DIN EN 2089 |
Aerospace series; aluminium alloy AL-P2014A-T6 or T62; sheet and strip; 0,4 mm ≤ a ≤ 6 mm; German version EN 2089:1994 |
|
DIN EN 2243-4 |
Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 4: Metal-honeycomb core flatwise tensile test; German and English version EN 2243-4:2005 |
|
DIN EN 2259 |
Aerospace series - Silicone rubber (VMQ) - Hardness 50 IRHD; German version EN 2259:1995 |
|
DIN EN 2559 |
Aerospace series - Carbon fibre preimpregnates - Determination of the resin and fibre content and the mass of fibre per unit area; German version EN 2559:1997 |
|
DIN EN 2591-214 |
Aerospace series - Elements of electrical and optical connection - Test methods - Part 214: Lightning strike, current and voltage pulse; German and English version EN 2591-214:2005 |
|
DIN EN 2743 |
Aerospace series - Fibre reinforced plastics - Standard procedures for conditioning prior to testing unaged materials; German and English version EN 2743:2001 |
|
DIN EN 2815 |
(DRAFT) Aerospace series - Steel FE-PM1802 (X5CrNiCu15-5) consumable electrode remelted, solution treated and precipitation treated - Bar for machining, a or D ≤ 200 mm, Rm ≥ 965 MPa |
|
DIN EN 2823 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Determination of the effect of exposure to humid atmosphere on physical and mechanical characteristics |
|
DIN EN 2910 |
Aerospace series - Shank nuts, self-locking, in heat resisting steel FE-PA92HT (A286) - Classification: 1100 MPa (at ambient temperature)/650 °C; German version EN 2910:1994 |
|
DIN EN 2952 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH2601 - Solution treated and cold worked; bar for forged fasteners D ≤ 50 mm, 1270 MPa ≤ Rm ≤ 1550 MPa |
|
DIN EN 3044 |
Aerospance series - Installation holes for inserts, screw thread, helical coil, self-locking - Design standard; German version EN 3044:1998 |
|
DIN EN 3352 |
(DRAFT) Aerospace series - Titanium alloy TI-C64001 - Investment casting, hot isostatic pressed, a < 50 mm, Rm ≥ 880 MPa |
|
DIN EN 3512 |
(DRAFT) Aerospace series - Steel FE-PL1801 (100Cr6), vacuum induction melted and consumable electrode remelted, hardened and tempered - Hollow bars for the manufacturer of bearings 3,5 mm ≤ a ≤ 55 mm |
|
DIN EN 3529 |
(DRAFT) Aerospace series - Steel FE-PM2701 (X2NiCoMo18-8-5), vacuum induction melted and vacuum arc remelted, solution treated and precipitation treated - Forgings a or D ≤ 150 mm, 1750 MPa ≤ Rm ≤ 2000 MPa |
|
DIN EN 3612 |
Aerospace series - Undercuts for splines - Design standard; German version EN 3612:1996 |
|
DIN EN 3960 |
Aerospace series - Gold base alloy AU-B40001 (AuNi18) - Filler metal for brazing, powder or paste; German version EN 3960:2001 |
|
DIN EN 6031 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of in-plane shear properties (±45° tensile test) |
|
DIN EN 6032 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Test method; determination of the glass transition temperatures |
|
DIN EN 6034 |
(DRAFT) Aerospace series - Carbon fibre reinforced plastics - Test method; determination of interlaminar fracture toughness energy; mode II, GIIC |
|
DIN EN 6043 |
(DRAFT) Aerospace series - Thermosetting resin systems - Test method; determination of gel time and viscosity |
|
DIN EN 6059-304 |
(DRAFT) Aerospace series - Electrical cables, installation, protection sleeves; test methods - Part 304: Flammability |
|
DIN EN 9100 |
Aerospace series - Quality management systems - Requirements (based on ISO 9001:2000) and quality system; Model for quality assurance in design, development, production, installation and servicing (based on ISO 9001:1994); German and English version EN 9100:2003 |
|
DIN ISO 10583 |
Aerospace fluid systems - Test methods for tube/fitting assemblies (ISO 10583:1993) |
|
DIN 29505 |
Aerospace; components of fibre reinforced plastics; indications in drawings and parts lists |
|
DIN 29543 |
Aerospace; seamless internal pressure tubes in wrought aluminium alloys; technical specification; inactive for new design |
|
DIN 29547 |
Aerospace; seamless structural tubes in wrought aluminium alloys; technical specification; inactive for new design |
|
DIN 29548-1 |
Aerospace; offsettings with wedge |
|
DIN 29548-2 |
Aerospace; offsettings without wedge |
|
DIN 29548-3 |
Aerospace; offsettings; directions for design and examples |
|
DIN 29576-1 |
Aerospace; aircraft electrical systems; characteristics; inactive for new design |
|
DIN 29576-2 |
Aerospace; aircraft electrical systems; testing of electrical cables installed in aircraft |
|
DIN 29594 |
Aerospace; aluminium alloy collars, metric series |
|
DIN 29638-2 |
Aerospace; press nuts, self-locking; directions for design and installation |
|
DIN 29639-2 |
Aerospace; press nuts, self-locking, floating; directions for design and installation |
|
DIN 29657 |
Aerospace; seamless structural tubes in steel and nickel alloys; technical specification |
|
DIN 29782 |
Aerospace; wire thread inserts; free running or screw-locking; technical specification |
|
DIN 29831 |
Aerospace; vented nickel-cadmium storage batteries, 24 V 40 Ah |
|
DIN 29850 |
Aerospace; heat treatment of wrought aluminium alloys |
|
DIN 29878 |
Aerospace - Resistance welded metal component parts - Technical specification |
|
DIN 29880 |
Aerospace; polycarbonate (PC) semi-finished products and moulded parts; technical specification |
|
DIN 29895 |
Aerospace; alternative materials for fasteners |
|
DIN 29895-2 |
Aerospace; alternative materials for fasteners; solid rivets |
|
DIN 29970 |
Aerospace - Honeycomb cores of polyamide paper, phenolic resin coated - Technical specification |
|
DIN 29972 |
Aerospace; rigid cellular materials; sheet; technical specification |
|
DIN 45643-1 |
Measurement and assessment of aircraft noise; quantities and parameters |
|
DIN 45643-2 |
Measurement and assessment of aircraft noise; aircraft noise monitoring systems within the meaning of article 19a of the Luftverkehrsgesetz (Civil Aviation Law) |
|
DIN 45643-3 |
Measurement and assessment of aircraft noise; determination of rating level of aircraft noise exposure |
|
DIN 65033 |
Aerospace; aluminium- and magnesium-alloy forgings; technical specification |
|
DIN 65038-1 |
Aerospace; steel, nickel- and cobalt-alloy bars; technical specification |
|
DIN 65052 |
Aerospace; pulleys for control cables; technical specification |
|
DIN 65053 |
Aerospace; control cable fittings; technical specification; inactive for new design |
|
DIN 65055 |
Aerospace; threaded control cable ends and turnbarrels; technical specification; inactive for new design |
|
DIN 65064 |
Aerospace - Potting compounds for care and edge filling for sandwich structures - Technical specification |
|
DIN 65074 |
Aerospace - Adhesive films and primers for structural assemblies - Technical specification |
|
DIN 65084 |
Aerospace; heat treatment of wrought titanium and titanium alloys |
|
DIN 65153 |
Aerospace - Acceptance testing of plasma arc welding equipment |
|
DIN 65155 |
Aerospace; steel rivets, close tolerance, with protruding head, shank tolerance 0 to -0,02 mm, metric series |
|
DIN 65156 |
Aerospace; close tolerance steel rivets with 100° flush head, shank tolerance 0 to - 0,02 mm, metric series |
|
DIN 65157 |
Aerospace; steel collars, metric series |
|
DIN 65170 |
Aerospace - Brazed and high-temperature brazed metallic components - Technical specifications |
|
DIN 65174 |
Aerospace; round bars of titanium and titanium alloys; dimensions, masses |
|
DIN 65179 |
Aerospace; countersunk head bolts, close tolerance, with internal offset cruciform ribbed drive and MJ thread, short thread length, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
|
DIN 65185-1 |
Aerospace; fasteners; rotary fasteners for structural and non-structural applications; technical specification |
|
DIN 65187 |
Aerospace; inserts for composite materials, with clearance hole, aluminium alloy |
|
DIN 65188 |
Aerospace; inserts for composite materials, with MJ thread, closed type, light weight, screw-locking, aluminium alloy |
|
DIN 65189 |
Aerospace; inserts for composite materials, with MJ thread, open type, screw-locking, aluminium alloy |
|
DIN 65190 |
Aerospace; inserts for composite materials, with MJ thread, closed type, screw-locking, aluminium alloy |
|
DIN 65194 |
Aerospace; sealing plugs for electrical circular connectors |
|
DIN 65197 |
Aerospace; titanium alloy round bars and wire for screw stock; dimensions, masses |
|
DIN 65203 |
Aerospace series - Elastomeric O-rings - Technical specification |
|
DIN 65207 |
Aerospace; tolerances for wrougth aluminium alloy folded profiles (sections) |
|
DIN 65209 |
(DRAFT) Aerospace series - Washers, countersunk |
|
DIN 65237 |
Aerospace - Spherical plain bearings, steel on steel - Technical specification; inactive for new design |
|
DIN 65239 |
Aerospace - Anchor nuts with MJ thread, deep counterbore, self-locking, non-floating, corner, corrosion-resisting steel, classification: 1100 MPa/315 °C/425 °C |
|
DIN 65240 |
Aerospace - Anchor nuts with MJ thread, deep counterbore, self-locking, floating, two lug, steel; Classification: 1100 MPa/235 °C |
|
DIN 65242 |
Aerospace - Anchor nuts with MJ-thread, deep counterbore, self-locking, floating, two lug, corrosion-resisting steel, classification: 1100 MPa/315 °C/425 °C |
|
DIN 65243 |
Aerospace - Anchor nuts with MJ thread, deep counterbore, self-locking, floating, single lug, steel; Classification: 1100 MPa/235 °C |
|
DIN 65244 |
Aerospace - Anchor nuts with MJ thread, deep counterbore, self-locking, floating, single lug, corrosion-resisting steel, classification: 1100 MPa/315 °C/425 °C |
|
DIN 65247 |
Aerospace; nuts, hexagon, slotted/castellated, thin, with MJ thread, corrosion-resisting steel, class: 1100 MPa/425 °C |
|
DIN 65250 |
Aerospace; seamless internal pressure tubes in titanium and titanium alloys; dimensions, masses |
|
DIN 65252 |
Aerospace series - Cellular elastomeric materials, open and closed cells - Semi-finished products and moulded parts; technical specification |
|
DIN 65259 |
Aerospace; rivets, 100° countersunk head, reduced, aluminium and aluminium alloys; metric series |
|
DIN 65260 |
Aerospace; rivets, universal head, aluminium and aluminium alloys; metric series |
|
DIN 65262-1 |
Aerospace - Sealing compounds - Part 1: Polysulphide polymer base; technical specification |
|
DIN 65262-2 |
Aerospace series - Sealing compounds - Part 2: Vinylidene fluoride and hexafluoropropylene base; technical specification |
|
DIN 65262-3 |
Aerospace series - Sealing compounds - Part 3: Silcone-rubber base; technical specification |
|
DIN 65267 |
Aerospace; screws, hexagon, with MJ thread, threaded approximately to head, steel, nominal tensile strength 900 MPa, for temperatures up to 235 °C |
|
DIN 65269 |
Aerospace; countersunk head screws, close tolerance, with ribbed TORQ-SET (ACR) recess and MJ thread, short thread length, steel, nominal tensile strength 900 MPa, for temperatures up to 235 °C |
|
DIN 65271 |
Aerospace series - Elastomeric semi-finished products and parts - Technical specification |
|
DIN 65281 |
Aerospace series - Nuts, hexagon, thin, with MJ thread, corrosion-resisting steel, classification: 1100 MPa/315 °C/425 °C |
|
DIN 65284 |
Aerospace; countersunk head screws, with ribbed TORQ-SET (ACR) recess and MJ thread, fully threaded, corrosion-resisting steel, nominal tensile strength 1100 MPa, for temperatures up to 425 °C |
|
DIN 65286 |
Aerospace; countersunk head screws, with ribbed TORQ-SET (ACR) recess and MJ thread, short thread length, steel; nominal tensile strength 900 MPa, for temperatures up to 235 °c |
|
DIN 65289 |
Aerospace; countersunk head screws, with ribbed TORQ-SET (ACR) recess and MJ thread, short thread length, titanium alloy, nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
|
DIN 65300 |
Aerospace; universal joints, needle bearing supported, long-time lubricated, for rotary shafts; technical specification |
|
DIN 65307 |
Aerospace; inserts for composite materials, with MJ thread, closed type, light weight, screw-locking, corrosion-resisting steel |
|
DIN 65313 |
Aerospace; pan head bolts with ribbed TORQ-SET (ACR) recess and MJ thread; fully threaded, corrosion-resisting steel; nominal tensile strength 1100 MPa, for temperatures up to 425 °C |
|
DIN 65314 |
Aerospace - Countersunk head bolts, close tolerance, with internal offset cruciform ribbed drive and MJ thread, short thread length, steel - Nominale tensile strength 1100 MPa, for temperatures up to 235 °C |
|
DIN 65316 |
Aerospace; countersunk head bolts, close tolerance, with internal offset cruciform ribbed drive and MJ thread, short thread length, corrosion-resisting steel; nominal tensile strength 1100 MPa, for temperatures up to 425 °C |
|
DIN 65317 |
Aerospace; countersunk head screws with ribbed TORQ-SET (ACR) recess and MJ thread, short thread length, steel; nominal tensile strength 1100 MPa, for temperatures up to 235 °C |
|
DIN 65318 |
Aerospace; pan head bolts with ribbed TORQ-SET (ACR) recess and short-length MJ-thread, steel; nominal tensile strength 110 MPa, for temperatures up to 235 °C |
|
DIN 65319 |
Aerospace; pan head bolts, close tolerance, with ribbed TORQ-SET (ACR) recess and short-length MJ thread, corrosion-resisting steel; nominal tensile strength 1100 MPa, for temperatures up to 425 °C |
|
DIN 65320 |
Aerospace; pan head bolts, close tolerance, with internal offset cruciform ribbed drive recess and short-length MJ thread, steel; nominal tensile strength 1100 MPa, for temperatures up to 235 °C |
|
DIN 65321 |
Aerospace; acrylic sheets, panes and moulded parts; technical specification |
|
DIN 65324 |
Aerospace; pan head bolts, close tolerance, with internal offset cruciform ribbed drive recess and short-length MJ thread, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
|
DIN 65330 |
Aerospace; hexagon bolts, with MJ thread, short thread, steel; nominal tensile strength 1100 MPa, for temperatures up to 235 °C |
|
DIN 65339 |
Aerospace - Hexagon bolts, close tolerance, with short-length MJ thread, corrosion-resisting steel - Nominal tensile strength 1100 MPa, for temperatures up to 425 °C |
|
DIN 65342 |
Aerospace series - Anchor nuts with MJ thread, deep counterbore, self-locking, two lug, reduced, corrosion-resisting steel, classification: 1100 MPa/315 °C/425 °C |
|
DIN 65343 |
Aerospace - Anchor nuts with MJ thread, deep counterbore, self-locking, two lug, reduced, steel; Classification: 1100 MPa/235 °C |
|
DIN 65344 |
Aerospace - Anchor nuts with MJ-thread, deep counterbore, self-locking, two lug, corrosion-resisting steel, classification: 1100 MPa/315 °C/425 °C |
|
DIN 65345 |
Aerospace; anchor nuts with MJ thread, deep counterbore, self-locking, two lug, steel; classification: 1100 MPa/235 °C |
|
DIN 65347 |
Aerospace - Anchor nuts with MJ thread, deep counterbore, self-locking, single lug, steel; Classification: 1100 MPa/235 °C |
|
DIN 65348 |
Aerospace; seamles internal pressure tubes in titanium alloys; technical specification |
|
DIN 65355 |
Aerospace; collars, metric series, wrought aluminium alloy |
|
DIN 65356-1 |
Aerospace; aromatic polyamide (aramid); high tenacity aramid filament yarns; dimensions, masses |
|
DIN 65356-2 |
Aerospace; aromatic polyamide (aramid); high tenacity aramid filament yarns; technical specification |
|
DIN 65363 |
Aerospace; lock washers for flight control rods |
|
DIN 65364 |
Aerospace; single fork ends for adjustable control rods |
|
DIN 65365 |
Aerospace; double fork ends for adjustable control rods |
|
DIN 65373 |
Aerospace; polyamide (PA) semi-finished products and moulded parts; technical specification |
|
DIN 65374 |
Aerospace; polytetrafluoroethylene (PTFE) semi-finished products and moulded parts; technical specification |
|
DIN 65385 |
Aerospace; hydraulic fluid power; filter elements; reporting of test data |
|
DIN 65390 |
Aerospace; hot-rolled steel sheet and plate; dimensions, masses |
|
DIN 65391 |
Aerospace - Press nuts with MJ thread, self-locking, corrosion-resisting steel; Classification: 1100 MPa/315 °C/425 °C |
|
DIN 65392 |
Aerospace - Press nuts with MJ thread, self-locking, floating, steel; Classification: 1100 MPa/235 °C |
|
DIN 65393 |
Aerospace - Thread inserts with MJ thread, ring locked, screw-locking, steel; Classification: 900 MPa/1100 MPa/1250 MPa/1550 MPa/235 °C |
|
DIN 65394 |
Aerospace - Thread inserts, with MJ thread, ring locked, screw-locking, corrosion-resisting steel; Classification: 900 MPa/1100 MPa/1250 MPa/1550 MPa/315 °C/425 °C |
|
DIN 65395 |
Aerospace; studs with MJ thread, ring locked, steel; nominal tensile strength 900 MPa, for temperatures up to 235 °C |
|
DIN 65396 |
Aerospace; studs with MJ thread, ring locked, corrosion resisting steel, nominal tensile strength 1250 Mpa, for temperatures up to 425 °C |
|
DIN 65398 |
Aerospace - Thread inserts, with MJ thread, locked, screw-locking, corrosion-resisting steel; Classification: 900 MPa/1100 MPa/315 °C |
|
DIN 65426-2 |
Aerospace; aromatic polyamide (aramid); woven filament fabric prepreg from high-modulus filament yarn and epoxy resin; technical specification |
|
DIN 65428 |
Aerospace; sleeves; wall thickness 0,25 mm, for fasteners with protruding head |
|
DIN 65429 |
Aerospace - Sleeves, wall thickness 0,5 mm, for fasteners with protruding head |
|
DIN 65430 |
Aerospace - Sleeves, wall thickness 0,25 mm, for fasteners with countersunk head |
|
DIN 65431 |
Aerospace - Sleeves, wall thickness 0,5 mm, for fasteners with countersunk head |
|
DIN 65433 |
Aerospace - Sleeves, wall thickness 0,25 mm, for fasteners with reduced countersunk head |
|
DIN 65434 |
Aerospace; sleeves; wall thickness 0,5 mm, for fasteners with reduced countersunk head |
|
DIN 65436 |
Aerospace; standard quality (STQ) and disc quality (DQ) of titanium and titanium alloys; requirements and tests |
|
DIN 65442 |
Aerospace; bihexagonal head bolts, close tolerance, with medium-length MJ thread, corrosion resisting nickel alloy; nominal tensile strength 1550 MPa, for temperatures up to 315 °C |
|
DIN 65444 |
Aerospace; rivets, 100° countersunk head, nickel alloy, metric series |
|
DIN 65445 |
Aerospace; rivets, 100° reduced countersunk head, metric series, nickel alloys |
|
DIN 65446 |
Aerospace; rivets, universal head, nickel alloys, metric series |
|
DIN 65448 |
Aerospace; structural adhesives; wedge test |
|
DIN 65454 |
Aerospace; hinges, extruded, in aluminium and corrosion-restisting steel; half-hinges and hinges in manufacturing lengths; light series |
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DIN 65456 |
Aerospace; washers for flight control rods, with hole for bonding |
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DIN 65457 |
Aerospace; thimbles, formed from steel; dimensions, masses |
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DIN 65464 |
Aerospace; studs with MJ thread, ring locked, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
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DIN 65470 |
Aerospace; filler metals for welding metallic materials; technical specification |
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DIN 65477 |
Aerospace - Press nuts, with MJ thread, closed type, self-locking, corrosion-resisting steel; Classification: 1100 MPa/315 °C/425 °C |
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DIN 65485 |
Aerospace; fasteners for structural application; rotary fastener, mechanical properties; rotary fastener, assembly |
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DIN 65487 |
Aerospace; fasteners for structural application; rotary fasteners; stud with countersunk head |
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DIN 65488 |
Aerospace; fasteners for structural application; rotary fasteners; installation dimensions |
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DIN 65494-102 |
Aerospace; rivet design values, static load, for protruding head rivet joints, single shear; rivet material 3.1324, metric series |
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DIN 65494-103 |
Aerospace; rivet design values, static load, for protruding head rivet joints, single shear; rivet material 3.3354, metric series |
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DIN 65494-105 |
Aerospace; rivet design values, static load, for protruding head rivet joints, single shear; rivet material 2.4360, metric series |
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DIN 65494-301 |
Aerospace; rivet design values, static load, for protruding head rivet joints, double shear; rivet material 3.1124, metric series |
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DIN 65494-302 |
Aerospace; rivet design values, static load, for protruding head rivet joints, double shear; rivet material 3.1324, metric series |
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DIN 65494-303 |
Aerospace; rivet design values, static load, for protruding head rivet joints, double shear; rivet material 3.3354, metric series |
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DIN 65494-305 |
Aerospace; rivet design values, static load, for protruding head rivet joints, double shear; rivet material 2.4360, metric series |
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DIN 65495-101 |
Aerospace; rivet design values, static load, for flush head rivet joints, single shear; rivet material 3.1124, metric series |
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DIN 65495-102 |
Aerospace; rivet design values, static load, for flush head rivet joints, single shear; rivet material 3.1324, metric series |
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DIN 65495-105 |
Aerospace; rivet design values, static load, flush head rivet joints, single shear; rivet material 2.4360, metric series |
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DIN 65495-201 |
Aerospace; rivet design values, static load, for flush head rivet joints, single shear, dimpled, rivet material 3.1124, metric series |
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DIN 65495-202 |
Aerospace; rivet design values, static load, for flush head rivet joints, single shear, dimpled, rivet material 3.1324, metric series |
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DIN 65495-205 |
Aerospace; rivet design values, static load, for flush head rivet joints, single shear, dimpled, rivet material 2.4360, metric series |
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DIN 65495-301 |
Aerospace; rivet design values, static load, for flush heat rivet joints, double shear; rivet material 3.1124, metric series |
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DIN 65495-302 |
Aerospace; rivet design values, static load, for flush heat rivet joints, double shear; rivet material 3.1324, metric series |
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DIN 65495-401 |
Aerospace; rivet design values, static load, for flush head rivet joints, double shear, dimpled, rivet material 3.1124, metric series |
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DIN 65495-402 |
Aerospace; rivet design values, static load, for flush head rivet joints, double shear, dimpled, rivet material 3.1324, metric series |
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DIN 65498 |
Aerospace; polyetherimide (PEI) semi-finished products and moulded parts; technical specification |
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DIN 65501 |
Aerospace - Shims for anchor nuts with MJ-thread |
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DIN 65503 |
Aerospace - Anchor nuts, with MJ thread, self-locking, pressure tight, two lug, steel; Classification: 900 MPa, fuel resistant from -55 °C to 120 °C |
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DIN 65504 |
Aerospace - Anchor nuts, with MJ thread, self-locking, pressure tight, two lug, corrosion-resisting steel, fuel resistant from -55 °C to 120 °C |
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DIN 65505 |
Aerospace - Anchor nuts, with MJ-thread, self-locking, pressure tight, two lug, steel; Classification: 900 MPa, air resistant from -55 °C to 230 °C |
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DIN 65506 |
Aerospace series - Anchor nuts with MJ thread, self-locking, pressure tight, two lug, corrosion-resisting steel, air resistant, from -55 °C to 230 °C |
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DIN 65525 |
Aerospace; bolts, hexagon, close tolerance, with MJ-thread, short thread, steel, nominal tensile strength 1100 MPa, for temperatures up to 235 °C |
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DIN 65528 |
Aerospace series - Nuts, bihexagonal with flange and MJ-thread, deep counterbore, self-locking, steel, class: 1550 MPa/1800 MPa/235 °C |
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DIN 65529 |
Aerospace series - Nuts, bihexagonal with flange and MJ-thread, deep counterbore, self-locking, steel, class: 1250 MPa/235 °C |
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DIN 65531 |
Aerospace series - Nuts, bihexagonal with flange and MJ-thread, deep counterbore, self-locking, corrosion-resisting, steel, class: 1250 MPa/315 °C/425 °C |
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DIN 65533 |
Aerospace; bolts, screws and nuts; allocation of materials and surface treatments; recommended selection |
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DIN 65534 |
Aerospace; nuts, hexagon, with MJ-thread, corrosion resisting steel; classification: 1100 MPa/650 °C |
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DIN 65537 |
Aerospace; cheese head bolts with bihexagon socket and MJ thread, short thread, nickel alloy; nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C |
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DIN 65538 |
Aerospace; cheese head bolts, close tolerance, with bihexagon socket and MJ thread, short thread, nickel alloy; nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C |
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DIN 65541 |
Aerospace; pan head bolts with ribbed TORQ-SET (ACR) recess and MJ thread; fully threaded, nickel alloy; nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C |
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DIN 65542 |
Aerospace; countersunk head screws, close tolerance, with ribbed TORQ-SET (ACR) recess and MJ thread, short thread length, nickel alloy, nominal tensile strength 1250 MPa, for temperatures up to 315 °C/425 °C |
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DIN 65546 |
Aerospace series - Nuts, bihexagonal with flange and MJ-thread, deep counterbore, self-locking, corrosion-resisting steel, class: 1100 MPa/315 °C/425 °C |
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DIN 65547 |
Aerospace; rivets, close tolerance, with protruding head, metric series, titanium alloy |
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DIN 65548 |
Aerospace; rivets, close tolerance with 100° flush head, metric series, titanium alloy |
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DIN 65550 |
Aerospace; flanged collars, metric series, titanium |
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DIN 65551 |
Aerospace; blind rivets with 100° reduced countersunk head, metric series, corrosion-resisting steel, with mandrel |
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DIN 65552 |
Aerospace; blind rivets with 100° countersunk head, corrosion-resisting steel, with mandrel, metric series |
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DIN 65553 |
Aerospace - Shims, without hole, for anchor nuts with MJ thread; Not to be used for new designs |
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DIN 65554 |
Aerospace; pan head bolts with ribbed TORQ-SET (ACR) recess and short-length MJ thread, corrosion-resisting steel, nominal tensile strength 1100 MPa, for temperatures up to 425 °C |
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DIN 65555 |
Aerospace; hexagon bolts with short-length MJ thread, corrosion-resisting steel; nominal tensile strength 1100 MPa, for temperatures up to 425 °C |
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DIN 65557 |
Aerospace; pan head screws with ribbed TORQ-SET (ACR) recess and MJ thread, fully threaded, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
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DIN 65558 |
Aerospace; countersunk head screws, with ribbed TORQ-SET (ACR) recess and MJ thread, fully threaded, titanium alloy; nominal tensile strength 1100 MPa, for temperatures up to 315 °C |
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DIN 65570 |
Aerospace; heat treatment facilities; general requirements |
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DIN 65574 |
Aerospace; nameplates; directions for design |
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DIN 65576 |
Aerospace; quick-release pins in corrosion-resisting steel, single locked, with self-retaining cam lever release mechanism |
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DIN 65581 |
Aerospace; titanium-alloy close-tolerance rivets and pure-titanium collars, metric series; technical specification |
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DIN 65582 |
Aerospace; heat treatment of aluminium- and magnesium-alloy castings |
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DIN 9003-5 |
Aerospace; bending of light metal sheet and strip; dimensions, limit deviations and compensation values |
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DIN 9003-6 |
Aerospace; bending of sheet and strip; stop-drill holes, corner configurations |
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DIN 9020-3 |
Aerospace; mass breakdown for aircraft heavier than air; group mass statement |
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DIN 9020-3 Beiblatt 1 |
Aerospace; mass breakdown for aircraft heavier than air; group mass statement; condensed version |
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DIN 9020-4 |
Aerospace; mass breakdown for aircraft heavier than air; detail mass statement |
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DIN 9020-5 |
Aerospace; mass breakdown for aircraft heavier than air; dimensional and construction data |
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DIN EN 12312-20 |
Aircraft ground support equipment - Specific requirements - Part 20: Electrical ground power units |
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DIN EN 14099 |
Aerospace - Space product assurance - Measurement of the peel and pull-off strength of coatings and finishes with pressure-sensitive tapes; German and English version EN 14099:2001 |
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DIN EN 14607-2 |
Space engineering - Mechanical - Part 2: Structural; English version EN 14607-2:2004 |
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DIN EN 14777 |
Space engineering - Multipaction design and test; English version EN 14777:2004 |
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DIN EN 1915-2 |
Aircraft ground support equipment - General requirements - Part 2: Stability and strength requirements, calculations and test methods; English version of DIN EN 1915-2 |
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DIN EN 2002-002 |
Aerospace series - Metallic materials - Test methods - Part 2: Tensile testing at elevated temperature; German and English version EN 2002-002:2005 |
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DIN EN 2003-10 |
(DRAFT) Aerospace series - Titanium and titanium alloys; test methods - Part 10: Sampling for determination of hydrogen content |
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DIN EN 2003-7 |
(DRAFT) Aerospace series - Steel; test methods - Part 7: Macrographic test |
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DIN EN 2003-8 |
(DRAFT) Aerospace series - Test methods for metallic materials; ultrasonic inspection of billets, bars, plates and forgings - Part 8: Acceptance criteria |
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DIN EN 2043 |
(DRAFT) Aerospace series - Metallic materials - General requirements for semi-finished product qualification (excluding forgings and castings) |
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DIN EN 2076-1/A1 |
Aerospace series; aluminium and magnesium alloy ingots and castings; technical specification; part 1: general requirements; German version EN 2076-1/A1:1993; amendment 1 |
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DIN EN 2122 |
Aerospace series - Washers, flat, in aluminium alloy, anodized or chromated; German version EN 2122:1996 |
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DIN EN 2138 |
Aerospace series - Washers, flat, in steel, cadmium plated; German version EN 2138:1999 |
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DIN EN 2145 |
Aerospace series - Rivets, solid, universal head, in aluminium alloy 2117, anodized or chromated, inch based series; German version EN 2145:1994 |
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DIN EN 2157-1 |
Aerospace series; steel; forging stock and forgings; technical specifications; part 1: general requirements; German version EN 2157-1:1993 |
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DIN EN 2187 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH1301 (NiCr19Co18Mo4Ti3Al3), solution treated and precipitation treated - Hand and die forgings, De ≤ 200 mm, Rm ≥ 1300 MPa |
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DIN EN 2240-002 |
(DRAFT) Aerospace series - Lamps incandescent - Part 002: Main characteristics |
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DIN EN 2240-016 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 016: Lamp, code 305; product standard |
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DIN EN 2240-031 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 031: Lamp, code 356; product standard |
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DIN EN 2240-035 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 035: Lamp, code 387; product standard |
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DIN EN 2240-040 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 040: Lamp, code 680; product standard |
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DIN EN 2240-050 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 050: Lamp, code 1064; product standard |
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DIN EN 2240-053 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 053: Lamp, code 1308; product standard |
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DIN EN 2240-082 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 082: Lamp, code 7079; product standard |
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DIN EN 2240-093 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 093: Lamp, code 7839; product standard |
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DIN EN 2240-096 |
(DRAFT) Aerospace series - Lamps, incandescent - Part 096: Lamp, code 72601-6; product standard |
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DIN EN 2243-6 |
Aerospace series - Non-metallic materials - Structural adhesives - Test method - Part 6: Determination of shear stress and shear strain; German and English version EN 2243-6:2005 |
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DIN EN 2266-004 |
(DRAFT) Aerospace series - Cables, electrical, for general purpose; operating temperatures between -55 °C and 200 °C - Part 004: CO2 laser printable; product standard |
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DIN EN 2267-005 |
Aerospace series - Cables, electrical, for general purpose - Operating temperatures between -55 °C and 260 °C - Part 005: UV laser printable - Product standard; German and English version EN 2267-005:2006 |
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DIN EN 2267-010 |
Aerospace series - Cables, electrical, for general purpose - Operating temperatures between -55 °C and 260 °C - Part 010: DR family, single UV laser printable - Product standard; German and English version EN 2267-010:2005 |
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DIN EN 2338 |
Aerospace series - Sheets, hot rolled in titanium and titanium alloys - Thickness 0,8 mm ≤ a ≤ 6 mm; Dimensions; German and English version EN 2338:2001 |
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DIN EN 2349-413 |
(DRAFT) Aerospace series - Requirements and test procedures for relays and contactors - Part 413: Vibration, sinusoidal and random |
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DIN EN 2403 |
(DRAFT) Aerospace series - Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3) vacuum melted, solution treated and precipitation treated - Precision casting, a or D ≤ 50 mm |
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DIN EN 2475 |
(DRAFT) Aerospace series - Steel FE-PL2106 (30CrNiMo8), air melted, hardened and tempered - Bar for machining De ≤ 100 mm, 1100 MPa ≤ Rm ≤ 1300 MPa |