|
AECMA PREN 2776 |
Aerospace Series Steel FE-P11 Rm Less Than or Equal to 340 MPa Sheet and Strip a Less Than or Equal to 2 mm-Issue P 1 |
|
AECMA PREN 2779 |
Aerospace Series Steel FE-PL56 Hardened and Tempered 1250 Less Than or Equal to Rm Less Than or Equal to 1400 MPa Bar De Less Than or Equal to 70 mm-Issue P 1 |
|
AECMA PREN 2780 |
Aerospace Series Steel FE-PL56 Hardened and Tempered 1250 Less Than or Equal to Rm Less Than or Equal to 1400 MPa Forgings De Less Than or Equal to 70 mm-Issue P 1 |
|
AECMA PREN 2781 |
Aerospace Series Non-Metallic Materials Structural Adhesives Test Methods Determination of the Primer Thickness |
|
AECMA PREN 2786 |
Aerospace Series Electrolytic Silver Plating Heat Resistant Steels and Alloys Copper and Copper Alloys |
|
AECMA PREN 2792 |
Aerospace Series Rod Ends, Adjustable Double Fork and Threaded Shank Dimensions and Loads-Issue P 1 |
|
AECMA PREN 2793 |
Aerospace Series Phosphate Treatment of Ferrous Alloys |
|
AECMA PREN 2794-001 |
Aerospace Series Circuit Breakers, Single-Pole, Temperature Compensated, Rated Currents 20 A to 50 A Part 001 : Technical Specification-Edition P 1 |
|
AECMA PREN 2794-003 |
Aerospace Series Circuit Breakers, Single-Pole, Temperature Compensated, Rated Currents 20 A to 50 A Part 003 : Metric Thread Fasteners, Distance Between Terminal Centres 19 mm Product Standard-Edition P 1 |
|
AECMA PREN 2794-004 |
Aerospace Series Circuit Breakers, Single-Pole, Temperature Compensated, Rated Currents 20 A to 50 A Part 004 : UNC Thread Fasteners, Distance Between Terminal Centres 21 mm Product Standard-Edition P 1 |
|
AECMA PREN 2795 |
Aerospace Series Fluorocarbon - Rubber (FPM) (Low Compression Set) Hardness 50 IRHD |
|
AECMA PREN 2795 |
Aerospace Series Fluorocarbon Rubber (FPM) Low Compression Set Hardness 50 IRHD-Edition P 1 |
|
AECMA PREN 2796 |
Aerospace Series Fluorocarbon - Rubber (FPM) (Low Compression Set) Hardness 60 IRHD |
|
AECMA PREN 2796 |
Aerospace Series Fluorocarbon Rubber (FPM) Low Compression Set Hardness 60 IRHD-Edition P 1 |
|
AECMA PREN 2797 |
Aerospace Series Fluorocarbon - Rubber (FPM) (Low Compression Set) Hardness 70 IRHD |
|
AECMA PREN 2797 |
Aerospace Series Fluorocarbon Rubber (FPM) Low Compression Set Hardness 70 IRHD-Edition P 1 |
|
AECMA PREN 2798 |
Aerospace Series Fluorocarbon - Rubber (FPM) (Low Compression Set) Hardness 80 IRHD |
|
AECMA PREN 2798 |
Aerospace Series Fluorocarbon Rubber (FPM) Low Compression Set Hardness 80 IRHD-Edition P 1 |
|
AECMA PREN 2799 |
Aerospace Series Fluorocarbon - Rubber (FPM) (Low Compression Set) Hardness 90 IRHD |
|
AECMA PREN 2799 |
Aerospace Series Fluorocarbon Rubber (FPM) Low Compression Set Hardness 90 IRHD-Edition P 1 |
|
AECMA PREN 2802 |
Aerospace Series Aluminium Alloy AL-P7475-T761 Sheet and Strip 0,6 mm Less Than or Equal to a Less Than or Equal to 6 mm-Edition P2 |
|
AECMA PREN 2804 |
Aerospace Series Aluminium Alloy 7075-T7651 Plate 6 Less Than a Less Than or Equal to 25 mm-Issue P 1 |
|
AECMA PREN 2804 |
Aerospace Series Aluminium Alloy AL-P7075-T7651 Plate 6mm Less Than a Less Than or Equal to 25mm-Edition P 3 |
|
AECMA PREN 2805 |
Aerospace Series Aluminium Alloy 7475-T7651 Plate 6 Less Than a Less Than or Equal to 25 mm-Issue P 1 |
|
AECMA PREN 2805 |
Aerospace Series Aluminium Alloy AL-P7475-T7651 Plate 6 mm Less Than a Less Than or Equal to 40 mm-Edition P 1 |
|
AECMA PREN 2805 |
Aerospace Series Aluminium Alloy AL-P7475-T7651 Plate 6mm Less Than a Less Than or Equal to 40mm-Edition P 3 |
|
AECMA PREN 2806 |
Aerospace Series Aluminium Alloy 2024-T42 Extruded Section 1,2 Less Than or Equal to a Less Than or Equal to 100 mm with Coarse Peripheral Grain Control-Issue P 1 |
|
AECMA PREN 2809 |
Aerospace Series Nuts, Hexagon, Slotted/Castellated, Thin Normal Across Flats, in Heat Resisting Steel Silver Plated Classification: 600 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2810 |
Aerospace Series Nuts, Hexagon, Slotted/Castellated, Reduced Height, Normal Across Flats, in Heat Resisting Steel, Passivated Classification: 900 MPa (at Ambient Temperature)/650 Degrees Celsius-Edition P 3; Supersedes Edition P 2: September 1996; Replaced by EN 2810 |
|
AECMA PREN 2812 |
Aerospace Series Stripping of Electric Cables as Defined by EN 2084, EN 2234, EN 2235, and EN 2346-Issue P 1 |
|
AECMA PREN 2812 |
Aerospace Series Stripping of Electric Cables-Edition P 2 |
|
AECMA PREN 2816 |
Aerospace Series Steel FE-PM1802 (X5CrNiCu15-5) Consumable Electrode Remelted Solution Treated and Precipitation Hardened Forgings a or D Less Than or Equal to 200 mm Rm Greater Than or Equal to 965 MPa-Edition P 2 |
|
AECMA PREN 2816 |
Aerospace Series Steel FE-PM64 Solution Annealed and Precipitation Hardened 960 Less Than or Equal to Rm Less Than or Equal to 1070 MPa Forgings De Less Than or Equal to 200 mm-Issue P 1 |
|
AECMA PREN 2817 |
Aerospace Series Steel FE-PM64 Solution Annealed and Precipitation Hardened 1070 Less Than or Equal to Rm Less Than or Equal to 1310 MPa Bar for Machining De Less Than or Equal to 200 mm-Issue P 1 |
|
AECMA PREN 2818 |
Aerospace Series Steel FE-PM1802 (X5CrNiCu15-5) Consumable Electrode Remelted Solution Treated and Precipitation Hardened Forgings a or D Less Than or Equal to 200 mm 1 070 MPa Less Than or Equal to Rm Less Than or Equal to 1 310 MPa-Edition P 2 |
|
AECMA PREN 2818 |
Aerospace Series Steel FE-PM64 Solution Annealed and Precipitation Hardened 1070 Less Than or Equal to Rm Less Than or Equal to 1310 MPa Forgings De Less Than or Equal to 200 mm-Issue P 1 |
|
AECMA PREN 2821 |
Aerospace Series Steel FE-PM1802 (X5CrNiCu15-5) Consumable Electrode Remelted Solution Treated and Precipitation Treated Bar for Machining a or D Less Than or Equal to 200 mm Rm Greater Than or Equal to 1 310 MPa-Edition P 3 |
|
AECMA PREN 2823 |
Aerospace Series Fibre Reinforced Plastics Determination of the Effect of Exposure to Humid Atmosphere on Physical and Mechanical Characteristics-Issue P 2 |
|
AECMA PREN 2823 |
Aerospace Series Fibre Reinforced Plastics Test Method for the Determination of the Effect of Exposure to Humid Atmospheres on Physical and Mechanical Characteristics |
|
AECMA PREN 2823 |
Aerospace Series Fibre Reinforced Plastics Test Method for the Determination of the Effect of Exposure to Humid Atmospheres on Physical and Mechanical Characteristics |
|
AECMA PREN 2824 |
Aerospace Series Burning Behaviour, Determination of Smoke Density and Gas Components in the Smoke of Materials Under the Influence of Radiating Heat and Flames - Test Equipment, Apparatus and Media |
|
AECMA PREN 2825 |
Aerospace Series Burning Behaviour, Determination of Smoke Density and Gas Components in the Smoke of Materials Under the Influence of Radiating Heat and Flames - Determination of Smoke Density |
|
AECMA PREN 2826 |
Aerospace Series Burning Behaviour, Determination of Smoke Density and Gas Components in the Smoke of Materials Under the Influence of Radiating Heat and Flames - Determination of Gas Components in the Smoke |
|
AECMA PREN 2828 |
Aerospace Series Adhesion Test for Metallic Coatings by Burnishing-Edition 1 |
|
AECMA PREN 2829 |
Aerospace Series Adhesion Test for Metallic Coatings by Shot Peening-Edition 1 |
|
AECMA PREN 2830 |
Aerospace Series Adhesion Test for Metallic Coatings by Shearing Action-Edition 1 |
|
AECMA PREN 2833-1 |
Aerospace Series Glass Fibre Thermosetting Preimpregnates Technical Specification Part 1 : General Requirements-Edition P 2 |
|
AECMA PREN 2833-1 |
Aerospace Series Glass Fibre Thermosetting Preimpregnates Technical Specification Part 1 : General-Edition P 1 |
|
AECMA PREN 2833-2 |
Aerospace Series Glass Fibre Thermosetting Preimpregnates Technical Specification Part 2: Glass Fabric/Epoxy Resin Preimpregnates Curing at up to 125 Degrees Celsius for Continuous Use up to 80 Degrees Celsius-Edition P 1 |
|
AECMA PREN 2833-2 |
Aerospace Series Technical Specification Glass Fibre Thermosetting Preimpregnates Part 2: Glass Fabric/Epoxy Resin Preimpregnates Curing at 125 Degrees Celsius for Continuous Use up to 80 Degrees Celsius-Issue 3 |
|
AECMA PREN 2833-3 |
Aerospace Series Glass Fibre Thermosetting Preimpregnates Techical Specification Part 3: Glass Fabric/Epoxy Resin Preimpregnate Curing at up to 180 Degrees C for Continuous Use up to 120 Degrees C-Edition P 1 |
|
AECMA PREN 2833-3 |
Aerospace Series Glass Fibre Thermosetting Preimpregnates Techical Specification Part 3: Glass Fabric/Epoxy Resin Preimpregnate Curing at up to 180 Degrees Celsius for Continuous Use up to 120 Degrees Celsius-Issue 3 |
|
AECMA PREN 2833-4 |
Aerospace Series Glass Fibre Thermosetting Preimpregnates Technical Specification Part 4: Unidirectional Glass/Epoxy Resin Preimpregnate Curing at Up to 125 Degrees C for Continuous Use Up to 80 Degress C-Edition P 1 |
|
AECMA PREN 2833-4 |
Aerospace Series Glass Fibre Thermosetting Preimpregnates Technical Specification Part 4: Unidirectional Glass/Epoxy Resin Preimpregnate Curing at up to 125 Degrees Celsius for Continuous Use up to 80 Degress Celsius-Issue 3 |
|
AECMA PREN 2833-5 |
Areospace series Glass Fibre Thermosetting Preimpregnates Technical Specification Part 5: Glass Fabric/Phenolic Resin Preimpregnate-Edition P 1 |
|
AECMA PREN 2850 |
(Faulty Standard) Aerospace Series Carbon Fibre Thermosetting Resin Unidirectional Laminates Compression Test Parallel to Fibre Direction-Edition P 2 |
|
AECMA PREN 2851 |
Aerospace Series Marking of Parts and Assemblies Indications on Drawings-Edition 1 |
|
AECMA PREN 2853 |
Aerospace Series Current Ratings for Electrical Cables with Conductor EN 2083-Edition P 1 |
|
AECMA PREN 2853 |
Aerospace Series Current Ratings for Electrical Cables with Conductor EN 2083-Revision 2 |
|
AECMA PREN 2854-002 |
Aerospace series Cables, electrical for general purpose Cross sections equal to and greater than 9 mm2 Operating temperatures between - 55 °C and 260 °C Part 002: General-Edition P 2 |
|
AECMA PREN 2854-002 |
Aerospace Series Cables, Electrical, for General Purpose Cross Sections Equal to and Greater Than 9 mm2 Operating Temperatures Between - 55 Degrees Celsius and 260 Degrees Celsius Part 002: General-Edition P 1 |
|
AECMA PREN 2854-003 |
Aerospace series Cables, electrical for general purpose Cross sections equal to and greater than 9 mm2 Operating temperatures between - 55 °C and 260 °C Part 003: Product standard-Edition P 2 |
|
AECMA PREN 2854-003 |
Aerospace Series Cables, Electrical, for General Purpose Cross Sections Equal to and Greater Than 9 mm2 Operating Temperatures Between - 55 Degrees Celsius and 260 Degrees Celsius Part 003: Product Standard-Edition P 1 |
|
AECMA PREN 2855 |
Aerospace Series Nuts, Anchor, Self-Locking, Fixed, 90 Degree Corner, Reduced Series, with Counterbore Classification: 1100 MPa/235 Degrees C-Issue P 1 |
|
AECMA PREN 2856 |
Aerospace Series Nuts, Anchor, Self-Locking, Fixed, Closed Corner, Reduced Series, with Counterbore Classification: 1100 MPa/235 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2858-1 |
Aerospace Series Titanium and Titanium Alloys Forging Stock and Forgings Technical Specification Part 1 - General Requirements-Edition 1 |
|
AECMA PREN 2858-3 |
Aerospace Series Titanium and Titanium Alloys Forging Stock and Forgings Technical Specification Part 3 - Pre-Production and Production Forgings-Edition 1 |
|
AECMA PREN 2859 |
Aerospace Series Bolts, Normal Hexagonal Head, Close Tolerance Normal Shank, Short Thread, in Alloy Steel, Cadmium Plated Classification: 1 100 MPa (at Ambient Temperature)/235 Degrees C-Edition P 2 |
|
AECMA PREN 2860-1 |
Aerospace Series Heat Resisting Alloys Forging Stock and Forgings Technical Specification Part 1 - General Requirements-Edition P 1 |
|
AECMA PREN 2860-2 |
Aerospace Series Heat Resisting Alloys Forging Stock and Forgings Technical Specification Part 2 - Forging Stock-Edition P 1 |
|
AECMA PREN 2860-3 |
Aerospace Series Heat Resisting Alloys Forging Stock and Forgings Technical Specification Part 3 - Pre-Production and Production Forgings-Edition P 1 |
|
AECMA PREN 2862 |
Aerospace Series Nuts, Anchor, Self-Locking, Fixed, 90 Degree Corner, with Counterbore, in Alloy Steel, Cadmium Plated, MoS2 Lubricated Classification : 1 100 MPa (at Ambient Temperature)/235 Degrees C-Edition P 1; Corrigendum 05/10/1993 |
|
AECMA PREN 2863 |
Aerospace Series Nuts, Anchor, Self-Locking, Fixed, 90 Degree Corner, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification : 1 100 MPa (at Ambient Temperature)/315 Degrees C-Edition P 1; Corrigendum 05/10/1993 |
|
AECMA PREN 2865 |
Aerospace Series Nuts, Anchor, Self-Locking, Floating, Two Lug, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification : 1 100 MPa (at Ambient Temperature)/315 Degrees C-Edition P 1 |
|
AECMA PREN 2865 |
Aerospace Series Nuts, Anchor, Self-Locking, Two Lug, Floating, with Counterbore, in Heat Resisting Steel, MoS2 Lubricated Classification : 1100 MPa (at Ambient Temperature)/315 Degrees C-Edition 1 |
|
AECMA PREN 2866 |
Aerospace Series Nuts, Anchor, Self-Locking, Floating, One Lug, with Counterbore, in Steel, Cadmium Plated, MoS2 Lubricated Classification : 1 110 MPa (at Ambient Temperature) / 235 Degrees C-Issue P 1 |
|
AECMA PREN 2868 |
Aerospace Series Nuts, Hexagonal, Slotted/Castellated, Normal Height, Normal Across Flats, in Heat Resisting Steel, Silver Plated Classification : 1 100 MPa (at Ambient Temperature) / 650 Degrees C-Edition P 1 |
|
AECMA PREN 2869 |
Aerospace Series Nuts, Hexagonal, Slotted/Castellated, Normal Height, Normal Across Flats, in Heat Resisting Steel, Passivated Classification : 1 100 MPa (at Ambient Temperature) / 650 Degrees C-Edition P 1 |
|
AECMA PREN 2870 |
Aerospace Series Bolts, Bihexagonal Normal Head, Close Tolerance Normal Shank,Short Thread in Titanium Alloy, Anodized, MoS2 Lubricated Classification;1100 MPa (at Ambient Temperature) /315 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2874 |
Aerospace Series Bolts, Large Bihexagonal Head, Close Tolerance Normal Shank, Medium Length Thread, in Nickel Alloy, Passivated Classification : 1 550 MPa (at Ambient Temperature) /315 Degrees C-Issue P 1 |
|
AECMA PREN 2878 |
Aerospace Series Nuts, Anchor, Self-Locking, Air Resistant, Sealing, Floating, Two Lug, With Counterbore, in Alloy Steel, Cadmium Plated, MoS2 Lubricated Classification: 900 MPa (At Ambient Temperature) / 235 Degrees C-Edition P 1 |
|
AECMA PREN 2879 |
Aerospace Series Nuts, Anchor, Self-Locking, Fuel Resistant, Sealing, Floating, Two Lug, With Counterbore, in Corrosion Resisting Steel, Passivated, MoS2 Lubricated Classification: 900 MPa (At Ambient Temperature) / 235 Degrees C-Edition P 1 |
|
AECMA PREN 2880 |
Aerospace Series Nuts, Anchor, Self-Locking, Fuel Resistant, Sealing, Floating, Two Lug, With Counterbore, in Alloy Steel, Cadmium Plated, MoS2 Lubricated Classification: 900 MPa (At Ambient Temperature) / 120 Degrees C-Edition P 1 |
|
AECMA PREN 2881 |
Aerospace Series Nuts, Anchor, Self-Locking, Fuel Resistant, Sealing, Floating, Two Lug, With Counterbore, in Corrosion Resisting Steel, Passivated, MoS2 Lubricated Classification: 900 MPa (At Ambient Temperature) / 120 Degrees C-Edition P 1 |
|
AECMA PREN 2882 |
Aerospace Series Nuts, Hexagonal, Seld-Locking, with Counterbore and Captive Washer, in Steel, Cadmium Plated, MoS2 Lubricated Classification : 1100 MPa (at Ambient Temperature)/235 Degrees C-Issue P 1 |
|
AECMA PREN 2883 |
Aerospace Series Nuts, Hexagonal, Self-Locking, with Counterbore and Captive Washer, in Heat Resisting Steel, MoS2 Lubricated Classification: 1 100 MPa (at Ambient Temperature)/315 Degrees Celsius-Edition P 1 |
|
AECMA PREN 2884 |
Aerospace Series Bolts, Pan Head, Torq-Setrm Recess, Coarse Tolerance Shank, Short Thread, in Titanium Alloy, Anodised Classification: 1100 MPa/315 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2885 |
Aerospace Series Bolts, Pan Head, Torq-Setrm Recess, Coarse Tolerance Shank, Short Thread, in Steel, Cadmium Plated Classification: 900 MPa/235 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2886 |
Aerospace Series Bolts, Pan Head, Torq-Setrm Recess, Close Tolerance Shank, Short Thread, in Steel, Cadmium Plated Classification: 900 MPa/235 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2887 |
Aerospace Series Bolts, Normal Hexagonal Head, Threaded to Head, in Corrosion Resisting Steel, Passivated Classification: 600 MPa (at Ambient Temperature)/425 Degrees C-Edition P 2 |
|
AECMA PREN 2887 |
Screws, Hexagonal Normal Head, Fully Threaded, in Corrosion Resisting Steel, Passivated Classification: 600 MPa/425 Degrees Celsius |
|
AECMA PREN 2888 |
Aerospace Series Bolts, Normal Hexagonal Head, Coarse Tolerance Normal Shank, Short Thread, in Corrosion Resisting Steel, Passivated Classification: 600 MPa (at Ambient Temperature) / 425 Degrees C-Edition 1 |
|
AECMA PREN 2888 |
Aerospace Series Bolts, Normal Hexagonal Head, Coarse Tolerance Normal Shank, Short Thread, in Corrosion Resisting Steel, Passivated Classification: 600 MPa (at Ambient Temperature) /425 Degrees C-Edition P 2 |
|
AECMA PREN 2888 |
Bolts, Hexagonal Normal Head, Coarse Tolerance Shank, Short Thread, in Corrosion Resisting Steel, Passivated Classification: 600 MPa/425 Degrees Celsius |
|
AECMA PREN 2889 |
Aerospace Series Bolts, Normal Hexagonal Head, Coarse Tolerance Normal Shank, Short Thread, in Alloy Steel, Cadmium Plated Classification: 900 MPa (at Ambient Temperature) / 235 Degrees C-Edition 1 |
|
AECMA PREN 2889 |
Aerospace Series Bolts, Normal Hexagonal Head, Coarse Tolerance Normal Shank, Short Thread, in Alloy Steel, Cadmium Plated Classification: 900 MPa (at Ambient Temperature)/235 Degrees C-Edition P 2 |
|
AECMA PREN 2894 |
Aerospace Series Nuts, Bihexagonal, Self-Locking, with counterbore, in Heat Resisting Nickel Base Alloy, Passivated, MoS2 Lubricated Classification: 1 550 MPa (at Ambient Temperature)/315 Degrees Celsius-Edition P 1 |
|
AECMA PREN 2895 |
Aerospace Series Nuts, Hexagonal, Plain, Normal Height, Normal Across Flats, in Corrosion Resisting Steel, Passivated Classification : 900 MPa (at Ambient Temperature) / 425 Degrees C-Edition P 1 |
|
AECMA PREN 2898 |
Aerospace Series Corrosion and Heat Resisting Steel Rivets Technical Specification-Issue P 1 |
|
AECMA PREN 2899 |
Aerospace Series Vulcanized Rubbers Tests on the Susceptibility to Corrosion in a Damp Atmosphere of Metals in Contact with Vulcanized Rubbers-Edition P 1 |
|
AECMA PREN 2900 |
Aerospace Series Clamps Technical Specification-Issue P 2; Inactive for New Design See PREN 3077 and PREN 3078 |
|
AECMA PREN 2902 |
Aerospace Series Clamps, Loop (<
> Type) with Rubber Cushioning in Aluminium Alloy Dimensions - Masses-Issue P 1; Inactive for New Design See PREN 4114 |
|
AECMA PREN 2903 |
Aerospace Series Clamps Worm Drive Dimensions - Masses-Issue P 2; Inactive for New Design See PREN 4234 |
|
AECMA PREN 2905 |
Aerospace Series Rubber Cushionings for Clamps Dimensions - Masses-Issue P 2; Inactive for New Design See PREN 4115 |
|
AECMA PREN 2907 |
Aerospace Series Nuts, Self Locking, Bi Hexagonal, in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification: 1100 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2908 |
Aerospace Series Nuts, Self Locking, Bi Hexagonal, Deep Counterbored, in Heat Resisting Steel FE-PA92HT (A286) Unplated Classification: 1100 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2909 |
Aerospace Series Nuts, Self Locking, Bi Hexagonal, Deep Counterbored, in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification: 1100 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2911 |
Aerospace Series Shank Nuts, Self Locking, Flange Restrained, in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification: 1100 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2915 |
Aerospace Series Steel FE-PM3801 (X5CrNiCu17-4) Consumable Electrode Remelted Solution Treated and Precipitation Treated Bar a or D Less Than or Equal to 200 mm Rm Greater Than or Equal to 965 MPa-Edition P 2; Inactive for New Design see EN 2815 |
|
AECMA PREN 2915 |
Aerospace Series Steel FE-PM65 Solution Annealed and Precipitation Hardened Rm Greater Than or Equal to 960 MPa Bar De Less Than or Equal to 200 mm-Issue P 1 |
|
AECMA PREN 2916 |
Aerospace Series Steel FE-PM3801 (X5CrNiCu17-4) Consumable Electrode Remelted Solution Treated and Precipitation Treated Forgings a or D Less Than or Equal to 200 mm Rm Greater Than or Equal to 965 MPa-Edition P 2; Inactive for New Design See EN 2816 |
|
AECMA PREN 2916 |
Aerospace Series Steel FE-PM65 Solution Annealed and Precipitation Hardened Rm Greater Than or Equal to 960 MPa Forgings De Less Than or Equal to 150 mm-Issue P 1 |
|
AECMA PREN 2917 |
Aerospace Series Steel FE-PM3801 (X5CrNiCu17-4) Consumable Electrode Remelted Solution Treated and Precipitation Treated Bar a or D Less Than or Equal to 200 mm Rm Greater Than or Equal to 1 070 MPa-Edition P 2; Inactive for New Design See EN 2817 |
|
AECMA PREN 2917 |
Aerospace Series Steel FE-PM65 Solution Annealed and Precipitation Hardened Rm Greater Than or Equal to 1070 MPa Bar De Less Than or Equal to 200 mm-Issue P 1 |
|
AECMA PREN 2918 |
Aerospace Series Steel FE-PM3801 (X5crNiCu17-4) Consumable Electrode Remelted Solution Treated and Precipitation Treated Forgings a or D Less Than or Equal to 200 mm Rm Greater Than or Equal to 1 0707 MPa-Edition P 2; Inactive for New Design See EN 2818 |
|
AECMA PREN 2918 |
Aerospace Series Steel FE-PM65 Solution Annealed and Precipitation Hardened Rm Greater Than or Equal to 1070 MPa Forgings De Less Than or Equal to 150 mm-Issue P 1 |
|
AECMA PREN 2919 |
Aerospace Series Steel FE-PL72 Carburized, Hardened and Tempered Bar De Less Than or Equal to 160 mm-Issue P 1 |
|
AECMA PREN 2920 |
Aerospace Series Steel FE-PL72 Carburized, Hardened and Tempered Forgings De less Than or Equal to 160 mm-Issue P 1 |
|
AECMA PREN 2921 |
Aerospace Series Nuts, Hexagon, Thin, Reduced Across Flats, Heat Resisting Steel, Passivated Classification : 900 MPa / 650 Degrees C |
|
AECMA PREN 2921 |
Aerospace Series Nuts, Hexagon, Thin, Reduced Across Flats, Heat Resisting Steel, Passivated Classification: 900 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2922 |
Aerospace Series Nuts, Hexagon, Plain, Reduced Height, Reduced Across Flats, in Heat Resisting Steel, Passivated, Left Hand Thread Classification : 600 MPa (at Ambient Temperature) / 650 Degrees C-Edition P 1 |
|
AECMA PREN 2922 |
Aerospace Series Nuts, Hexagon, Plain, Reduced Height, Reduced Across Flats, in Heat Resisting Steel, Passivated, Left Hand Thread Classification : 600 MPa (at Ambient Temperature) / 650 Degrees C-Edition P 2 |
|
AECMA PREN 2923 |
Aerospace Series Nuts, Hexagon, Plain, Reduced Height, Reduced Across Flats, in Heat Resisting Steel, Silver Plated Classification : 600 MPa (at Ambient Temperature) / 425 Degrees C-Edition P 1 |
|
AECMA PREN 2923 |
Aerospace Series Nuts, Hexagon, Plain, Reduced Height, Reduced Across Flats, in Heat Resisting Steel, Silver Plated Classification : 600 MPa (at Ambient Temperature) / 425 Degrees C-Edition P 2 |
|
AECMA PREN 2924 |
Aerospace Series Nuts, Hexagon, Plain, Reduced Height, Reduced Across Flats, in Heat Resisting Steel, Silver Plated, Left Hand Thread Classification : 600 MPa (at Ambient Temperature) / 425 Degrees C-Edition P 1 |
|
AECMA PREN 2924 |
Aerospace Series Nuts, Hexagon, Plain, Reduced Height, Reduced Across Flats, in Heat Resisting Steel, Silver Plated, Left Hand Thread Classification : 600 MPa (at Ambient Temperature) / 425 Degrees C-Edition P 2 |
|
AECMA PREN 2925 |
Aerospace Series Bolts with Double Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Steel FE-PA92HT (A286) Classification : 900 MPa / 650 Degrees C-Issue P 2 |
|
AECMA PREN 2926 |
Aerospace Series Bolts with Double Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Steel FE-PA92HT (A286), Silver Plated Classification : 900 MPa / 650 Degrees C-Issue P 2 |
|
AECMA PREN 2927 |
Bolts with Double Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718) Classification 1275 MPa/650 Degrees Celsius |
|
AECMA PREN 2928 |
Bolts with Double Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P100HT (Inconel 718) Silver Plated Classification 1275 MPa/650 Degrees Celsius |
|
AECMA PREN 2929 |
Aerospace Series Bolts with Double Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Classification : 1 210 MPa / 735 Degrees C-Issue P 2 |
|
AECMA PREN 2929 |
Bolts with Double Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Classification 1210 MPa/735 Degrees Celsius |
|
AECMA PREN 2930 |
Aerospace Series Bolts with Double Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy), Silver Plated Classification : 1 210 MPa / 735 Degrees C-Issue P 2 |
|
AECMA PREN 2930 |
Bolts with Double Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Silver Plated Classification 1210 MPa/735 Degrees Celsius |
|
AECMA PREN 2931 |
Aerospace Series Bolts T-head, Relieved Shank, Long Thread, in Heat Resisting Steel FE-PA92HT (A286) Unplated Classification: 900 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2932 |
Aerospace Series Bolts T-Head, Relieved Shank, Long Thread, in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification: 900 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2933 |
Aerospace Series Bolts T-Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P100HT (INCO 718) Unplated Classification: 1275 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2934 |
Aerospace Series Bolts T-Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P100HT (INCO 718) Silver Plated Classification: 1275 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2935 |
Aerospace Series Bolts T-Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Unplated Classification: 1210 MPa/730 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2936 |
Aerospace Series Bolts T-Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Silver Plated Classification 1210 MPa/730 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2937 |
Aerospace Series Screws, Hexagon Head, Thread to Head, in Heat Resisting Steel FE-PA92HT (A286) Unplated Classification: 900 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2938 |
Aerospace Series Screws, Hexagon Head, Thread to Head, in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification: 900 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2939 |
Aerospace Series Screws, 100 Degrees Countersunk Head, Torq-Setrm Recess, Thread to Head, in Heat Resisting Steel FE-PA92HT (A286) Unplated Classification: 900 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2940 |
Aerospace Series Screws, 100 Degrees Countersunk Head, Torq-Setrm Recess, Thread to Head, in Heat Resisting Steel FE-PA92HT (A286) Silver Plated Classification: 900 MPa/650 Degrees Celsius-Issue P 1 |
|
AECMA PREN 2941 |
Aerospace Series Nickel Alloy Rivets Technical Specification |
|
AECMA PREN 2945 |
Aerospace Series Assembly with Self-Locking Thread Inserts-Issue P 1 |
|
AECMA PREN 2947 |
Aerospace Series Steel FE-PA3004 (X10CrNi18-09) Air Melted not Hot Treated Wire for Springs D Less than or Equal to 2,3 mm-Edition P 1 |
|
AECMA PREN 2951 |
Aerospace Series Metallic Materials Test Method Micrographic Determination of Content of Non-Metallic Inclusions-Edition P 1 |
|
AECMA PREN 2951 |
Aerospace Series Metallic Materials Test Method Micrographic Determination of Content of Non-Metallic Inclusions-Edition P1 |
|
AECMA PREN 2957 |
Aerospace Series Method of Preparation of Forged Samples-Issue P 1 |
|
AECMA PREN 2959 |
Aerospace Series Heat Resisting Alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) Solution Treated and Cold Worked Bar for Forged Fasteners 3 mm Less Than or Equal to D Less Than or Equal to 30 mm-Edition P2 |
|
AECMA PREN 2959 |
Aerospace Series Heat Resisting Nickel Base Alloy (NI-P1O1HT) Solution Treated and Cold Worked Bar for Hot Upset Forging for Fasteners 3 Less Than or Equal to D Less Than or Equal to 30 mm-Issue P 1 |
|
AECMA PREN 2960 |
Aerospace Series Heat Resisting Nickel Base Alloy (NI-P101HT) Cold Worked and Solution Treated Bar for Machining for Fasteners 3 Less Than or Equal to D Less Than or Equal to 50 mm-Issue P 1 |
|
AECMA PREN 2961 |
Heat Resisting Nickel Base Alloy (Ni-P100HT) Cold Worked and Solution Treated Bar for Machining for Fasteners 3 Less Than or Equal to D Less Than or Equal to 50 mm |
|
AECMA PREN 2962 |
Aerospace Series Carbon Fibre Filament Yarn (Polyacrylonitrile Precursor) Technical Specification |
|
AECMA PREN 2962 |
Aerospace Series Carbon Fibre Filament Yarn (Polyacrylonitrile Precursor) Technical Specification-Edition P 1 |
|
AECMA PREN 2985 |
Aerospace Series Nickel-Cadmium Batteries of Format A Type-Edition p 1 |
|
AECMA PREN 2986 |
Aerospace Series Nickel-Cadmium Batteries of Format B Type-Edition P 1 |
|
AECMA PREN 2988 |
Aerospace Series Nickel-Cadmium Batteries of Format D Type-Edition P 1 |
|
AECMA PREN 2991 |
Aerospace Series Nickel-Cadmium Batteries of Format E Type-Edition P 1 |
|
AECMA PREN 2993 |
Aerospace Series Nickel-Cadmium Batteries of Format F Type-Edition P 1 |
|
AECMA PREN 2995-001 |
Aerospace Series Circuit Breakers, Single-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 001: Technical Specification-Edition P 1 |
|
AECMA PREN 2995-001 |
Aerospace Series Circuit Breakers, Single-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 001: Technical Specification-Edition P 2 |
|
AECMA PREN 2995-004 |
Aerospace Series Circuit Breakers, Single-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 004: With Signal Contact and Unified Mounting Hardware Centre-to-Centre Distance of Terminals 18 mm Product Standard-Edition P 1 |
|
AECMA PREN 2995-005 |
Aerospace Series Circuit Breakers, Single-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 005: With Polarized Signal Contact and Unified Mounting Hardware Centre-to-Centre Distance of Terminals 18 mm Product Standard-Edition P 1 |
|
AECMA PREN 2995-005 |
Aerospace Series Circuit Breakers, Single-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 005: With Polarized Signal Contact and Unified Mounting Hardware Centre-to-Centre Distance of Terminals 18 mm Product Standard-Edition P 2 |
|
AECMA PREN 2995-005 |
Aerospace Series Circuit Breakers, Single-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 005: With Polarized Signal Contact Product Standard-Edition P 3 |
|
AECMA PREN 2996-001 |
Aerospace Series Circuit Breakers, Three-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 001: Technical Specification-Edition P 1 |
|
AECMA PREN 2996-004 |
Aerospace Series Circuit Breakers, Three-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 004: With Signal Contact and Unified Mounting Hardware Centre-to-Centre Distance of Terminals 12,8 mm Product Standard-Edition P 1 |
|
AECMA PREN 2996-004 |
Aerospace Series Circuit Breakers, Three-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 004: With Signal Contact and Unified Mounting Hardware Centre-to-Centre Distance of Terminals 12,8 mm Product Standard-Edition P 2 |
|
AECMA PREN 2996-004 |
Aerospace Series Circuit Breakers, Three-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 004: With Signal Contact Product Standard-Edition P 3 |
|
AECMA PREN 2996-005 |
Aerospace Series Circuit Breakers, Three-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 005: With Polarized Signal Contact and Unified Mounting Hardware Centre-to-Centre Distance of Terminals 12,8 mm Product Standard-Edition P 1 |
|
AECMA PREN 2996-005 |
Aerospace Series Circuit Breakers, Three-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 005: With Polarized Signal Contact and Unified Mounting Hardware Centre-to-Centre Distance of Terminals 12,8 mm Product Standard-Edition P 2 |
|
AECMA PREN 2996-005 |
Aerospace Series Circuit Breakers, Three-Pole, Temperature Compensated, Rated Current 1 A to 25 A Part 005: With Polarized Signal Contact Product Standard-Edition P 3 |
|
AECMA PREN 2997-004 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Fire-Resistant or Non Fire-Resistant, Operating Temperatures -65 Degrees C to 175 Degrees C Continuous, 200 Degrees C Continuous, 260 Degrees C Peak Part 004: Jam-Nut Mounted Receptacle Product Standard-Edition P 2 |
|
AECMA PREN 2997-004 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Operating Temperatures 175 Degrees Celsius Continuous, 200 Degrees Celsius Continuous, 260 Degrees Celsius Peak and Fire Resistant Part 004- Jam- Nut Mounted Receptacle Product Standard-Issue P 1 |
|
AECMA PREN 2997-005 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Operating Temperatures 175 Degrees Celsius Continuous, 200 Degrees Celsius Continuous, 260 Degrees Celsius Peak and Fire Resistant Part 005- Hermetic Square Flange Receptacle Product Standard |
|
AECMA PREN 2997-006 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Fire-Resistant or Non Fire-Resistant, Operating Temperatures -65 Degrees C to 175 Degrees C Continuous, 200 Degrees C Continuous, 260 Degrees C Peak Part 006: Hermetic Jam-Nut Mounted Receptacle Product Standard-Edition P 2 |
|
AECMA PREN 2997-006 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Operating Temperatures 175 Degrees C Continuous, 200 Degrees C Continuous, 260 Degrees C Peak and Fire Resistant Part 006 - Hermetic Jam-Nut Mounted Receptacle Product Standard-Issue P 1 |
|
AECMA PREN 2997-007 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Operating Temperatures 175 Degrees Celsius Continuous, 200 Degrees Celsius Continuous, 260 Degrees Celsius Peak and Fire Resistant Part 007- Hermetic Receptacle with Round Flange Attached by Soldering or Brazing-Issue P 1 |
|
AECMA PREN 2997-008 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Operating Temperatures 175 Degrees Celsius Continuous, 200 Degrees Celsius Continuous, 260 Degrees Celsius Peak and Fire Resistant Part 008- Plug Product Standard-Issue P 1 |
|
AECMA PREN 2997-009 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Operating Temperatures 175 Degrees Celsius Continuous, 200 Degrees Celsius Continuous, 260 Degrees Celsius Peak and Fire Resistant Part 009- Flight Flank for Receptacle Product Standard-Issue P 1 |
|
AECMA PREN 2997-010 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Operating Temperatures 175 Degrees C Continuous, 200 Degrees C Continuous, 260 Degrees C Peak and Fire Resistant Part 010 - Flight Blank for Plug Product Standard-Issue P 1 |
|
AECMA PREN 2997-011 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Fire-Resistant or Non Fire-Resistant, Operating Temperatures - 65 Degrees C to 175 Degrees C Continuous, 200 Degrees C Continuous, 260 Degrees C Peak Part 011: Dummy Receptacle Product Standard-Edition P 2 |
|
AECMA PREN 2997-011 |
Aerospace Series Connectors, Electrical, Circular, Coupled by Threaded Ring, Operating Temperatures 175 Degrees C Continuous, 200 Degrees C Continuous, 260 Degrees C Peak and Fire Resistant Part 011- Dummy Receptacle Product Standard-Issue P 1 |
|
AECMA PREN 2998 |
Aerospace Series Washers Countersunk Heat Resisting Steel-Issue P 1 |
|
AECMA PREN 3001 |
Aerospace Series Tempered Float Glass Plies for Aircraft Applications Technical Specification-Edition P 1 |
|
AECMA PREN 3002 |
Aerospace Series Chromic Acid Anodizing Testing of Adhesives-Issue P 1 |
|
AECMA PREN 3003 |
Aerospace series Non-Metallic materials Structural adhesives Determination of mass per unit area of film adhesives Test method-Edition P 1 |
|
AECMA PREN 3004 |
Aerospace Series Nuts, Self Locking, in Heat Resisting Steel FE-PA92HT (A286) Classification: 1100 MPa/650 Degrees Celsius Technical Specification-Issue P 1 |
|
AECMA PREN 3005 |
Aerospace Series Nuts, Self-Locking, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Classification: 1210 MPa/730 Degrees Celsius Technical Specification-Issue P 1 |
|
AECMA PREN 3006 |
Aerospace Series Bolts, Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Steel FE-PA92HT (A286) Classification 900 MPa/650 Degrees Celsius Unplated-Issue P 1 |
|
AECMA PREN 3007 |
Aerospace Series Bolts, Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Steel FE-PA92HT (A286) Classification 900 MPa/650 Degrees Celsius Silver Plated-Issue P 1 |
|
AECMA PREN 3008 |
Aerospace Series Bolts, Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P100HT (INCO 718) Classification 1275 MPa/650 Degrees Celsius Unplated-Issue P 1 |
|
AECMA PREN 3009 |
Aerospace Series Bolts, Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P100HT (INCO 718) Classification 1275 MPa/650 Degrees Celsius Silver Plated-Issue P 1 |
|
AECMA PREN 3010 |
Aerospace Series Bolts, Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Classification 1210 MPa/730 Degrees Celsius Unplated-Issue P 1 |
|
AECMA PREN 3011 |
Aerospace Series Bolts, Hexagon Head, Relieved Shank, Long Thread, in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Classification 1210 MPa/730 Degrees Celsius Silver Plated-Issue P 1 |
|
AECMA PREN 3012 |
Aerospace Series Nuts, Self-Locking, Bihexagonal in Heat Resisting Nickel Base Alloy NI-P101HT (Waspaloy) Unplated Classification: 1210 MPa/730 Degrees Celsius-Issue P 1 |
|
AECMA PREN 3014 |
Aerospace Series Self-Locking Serrated Shank Nuts in Heat Resisting Steel FE-PA92HT Classification: 1100 MPa/650 Degrees Celsius-Edition P 2; Supersedes Issue P 1: February 1987; Replaced by EN 3014 |
|
AECMA PREN 3015 |
Aerospace Series Self-Locking Serrated Shank Nuts in Heat Resisting Steel FE-PA92HT Silver Plated Classification: 1100 MPa/650 Degrees Celsius-Edition P 2; Supersedes Issue P 1: February 1987; Replaced by EN 3015 |
|
AECMA PREN 3017 |
Aerospace Series Washers, Facing/Packing Heat Resisting Steel-Issue P 1 |
|
AECMA PREN 3018 |
Aerospace Series Heat Resisting Alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1) Consumable Electrode Remelted Cold Drawn Wire for the Manufacture of Thread Inserts D Less than or Equal to 3 mm-Edition P 1 |
|
AECMA PREN 3018 |
Aerospace Series Heat Resisting Alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1) Consumable Electrode Remelted Cold Drawn Wire for the Manufacture of Thread Inserts D Less Than or Equal to 3 mm-Edition P1 |
|
AECMA PREN 3020 |
Aerospace Series Self-Locking Plate Nuts, Floating, Two-Lug, in Heat Resisting Steel FE-PA92HT (A286), Silver Plated Classification : 1 100 MPa (at Ambient Temperature) /650 Degrees C-Issue P 2 |
|
AECMA PREN 3020 |
Self Locking Plate Nuts Floating, Two-Lug in Heat Resisting Steel FE-PA2HT (A286), Silver-Coated Classification: 1100 MPa/650 Degrees Celsius |
|
AECMA PREN 3026 |
Aerospace Series Test Method for Dry Film Lubricants Corrosion Test on Steels Specimens-Edition 1 |
|
AECMA PREN 3030 |
Aerospace Series Test Method for Dry Film Lubricants Solids Content-Edition 1 |
|
AECMA PREN 3032 |
Aerospace Series Test Method for Dry Film Lubricants Thickness Measurement-Edition 1 |
|
AECMA PREN 3033 |
Aerospace Series Nuts, Self-Locking, Hexagonal with Captive Washer, in Heat Resisting Steel FE-PA92HT (A286), Uncoated Classification : 1100 MPa/425 Degrees C-Issue P 1 |
|
AECMA PREN 3033 |
Aerospace Series Nuts, Self-Locking, Hexagonal with Captive Washer, in Heat Resisting Steel FE-PA92HT (A286), Uncoated Classification: 1100 MPa/425 Degrees Celsius-Issue P 1 |
|
AECMA PREN 3034 |
Aerospace Series Nuts, Self-Locking, Hexagonal with Captive Washer, in Heat Resisting Steel FE-PA92HT (A286), Silver Coated Classification: 1100 MPa/425 Degrees Celsius-Issue P 1 |
|
AECMA PREN 3035 |
Aerospace Series Bolts, 100 Degrees Countersunk Head, Torq-Setrm Recess, Close Tolerance Shank, Short Thread, in Steel Cadmium Plated Classification: 1100 MPa/235 Degrees Celsius-Issue P 1 |
|
AECMA PREN 3037 |
Aerospace Series Bolts, Pan Head, Torq-Setrm Recess, Close Tolerance Shank, Short Thread, in Titanium Alloy, Anodised Classification: 1100 MPa/315 Degrees Celsius-Issue P 1 |
|
AECMA PREN 3042 |
(CANCELLED) Aerospace Series Quality Assurance EN Aerospace Products Qualification Procedure-Edition 1 |
|
AECMA PREN 3042 |
(CANCELLED) Aerospace Series Quality Assurance EN Aerospace Products Qualification Procedure-Edition 2 |
|
AECMA PREN 3042/PR A1 |
Aerospace Series Quality Assurance EN Aerospace Products Approval of the Quality System of Manufacturers-Edition 1 |
|
AECMA PREN 3043 |
Aerospace Series Fasteners, Externally Threaded, in Heat Resisting Steel FE-PA92HT (A 286) Classification: 90 MPa/550 Degrees Celcius Manufacturing Method Optional Technical Specification-Issue P 2 |
|
AECMA PREN 3044 |
Aerospace Series Installation of Self-Locking Thread Inserts Design Dimensions-Issue P 1 |
|
AECMA PREN 3045 |
Aerospace Series Bearings-Airframe Rolling Rigid Single Row Ball Bearings in Steel Diameter Series 0 and 2 Reduced Clearance Category Dimensions and Loads-Issue P 1 |
|
AECMA PREN 3046 |
Aerospace Series Bearings-Airframe Rolling Rigid Single Row Ball Bearings in Steel Cadmium Plated Diameter Series 0 and 2 Reduced Clearance Category Dimensions and Loads-Issue P 1 |
|
AECMA PREN 3047 |
Aerospace Series Bearings-Airframe Rolling Rigid Single Row Ball Bearings in Corrosion Resisting Steel Diameter Series 0 and 2 Reduced Clearance Category Dimensions and Loads-Issue P 1 |
|
AECMA PREN 3048 |
Aerospace Series Bearings, Spherical Plain in Corrosion Resisting Steel with Self-Lubricating Liner, Light Series Elevated Loads at Ambient Temperature Dimensions and Loads-Issue P 1 |
|
AECMA PREN 3050 |
Aerospace Series 0-Rings in Low Compression Set Fluorocarbon Rubber Technical Specification-Issue P 1 |
|
AECMA PREN 3051 |
Substitute Materials for Bolts |
|
AECMA PREN 3052 |
Aerospace Series Bolts, Hexagonal Normal Head, Close Tolerance Normal Shank, Short Thread, in Heat and Corrosion Resisting Steel, Passivated Classification: 1100 MPa (at Ambient Temperature) / 425 Degrees C-Edition 1 |
|
AECMA PREN 3052 |
Aerospace Series Bolts, Hexagonal Normal Head, Close Tolerance Shank, Short Thread in Corrosion Resisting Steel, Passivated Classification: 1100 MPa/425 Degrees Celsius-Issue P 1 |
|
AECMA PREN 3055 |
Aerospace Series Bearings-Airframe Rolling Single Row Self-Aligning Roller Bearings in Corrosion Resisting Steel Dimensions and Loads-Issue P 1 |
|
AECMA PREN 3056 |
Aerospace Series Bearings-Airframe Rolling Rigid Two Row Ball Bearings in Steel Dimensions and Loads-Issue P 1 |
|
AECMA PREN 3057 |
Aerospace Series Bearings-Airframe Rolling Rigid Two Row Ball Bearings in Steel Cadmium Plated Dimensions and Loads-Issue P 1 |
|
AECMA PREN 3058 |
Aerospace Series Bearings-Airframe Rolling Rigid Two Row Ball Bearings in Corrosion Resisting Steel Dimensions and Loads-Issue P 1 |
|
AECMA PREN 3059 |
Aerospace Series Bearings, Airframe Rolling Rigid Single Row Ball Bearings in Steel, with Flanged Alignment Bush, Cadmium Plated Dimensions and Loads-Edition P 1 |
|
AECMA PREN 3059 |
Aerospace Series Bearings, Airframe Rolling Rigid Single Row Ball Bearings in Steel, with Flanged Alignment Housing, Cadmium Plated Dimensions and Loads-Edition P 2 |
|
AECMA PREN 3060 |
Aerospace Series Bearings, Airframe Rolling Rigid Single Row Ball Bearings in Steel, Cadmium Plated, with Flanged Alignment Bush, Cadmium Plated Dimensions and Loads |
|
AECMA PREN 3060 |
Aerospace Series Bearings, Airframe Rolling Rigid Single Row Ball Bearings in Steel, Cadmium Plated, with Flanged Alignment Housing, Cadmium Plated Dimensions and Loads-Edition P 2 |
|
AECMA PREN 3061 |
Aerospace Series Bearings, Airframe Rolling Rigid Single Row Ball Bearings in Corrosion Resisting Steel, with Flanged Alignment Bush Dimensions and Loads-Edition P 1 |
|
AECMA PREN 3064 |
Aerospace Series Self-Locking Serrated Shank Nuts Assembly Procedure-Issue P 1 |
|
AECMA PREN 3065 |
Aerospace Series Installation Holes for Self-Locking Serrated Shank Nuts Design Specifications-Issue P 1 |
|
AECMA PREN 3071 |
Aerospace Series Straight Bending of Sheets and Strips in Aluminium and Aluminium Alloys Dimensioning Methods and Calculations of Developed Lengths-Edition 1 |
|
AECMA PREN 3077 |
Aerospace Series Clamps Worm Drive Technical Specification-Edition P 1 |
|
AECMA PREN 3079 |
Aerospace Series Pipe Coupling 8 Degree 30' Up to 28 000 kPa Adaptors Metric Series Technical Specification-Edition P 1 |
|
AECMA PREN 3084 |
Aerospace Series Pipe Coupling 8 Degrees 30' in Titanium Alloy Unions, Long, Welded, for Repair-Edition P 1 |
|
AECMA PREN 3086 |
Aerospace Series Hose Assemblies Designation Limited to 15 Digits-Edition P 1 |
|
AECMA PREN 3090 |
Aerospace Series Polysulphide Sealants Test Method Determination of the Effects of Accelerated Storage |
|
AECMA PREN 3091 |
Aerospace Series Polysulphide Sealants Test Method Determination of the Effects of Long Term Storage |
|
AECMA PREN 3092 |
Aerospace Series Sealants Test Method Determination of the Non-Volatile Content |
|
AECMA PREN 3093 |
Aerospace Series Sealants Test Method Determination of Flow |
|
AECMA PREN 3094 |
Aerospace Series Sealants Test Method Determination of Application Time |
|
AECMA PREN 3094 |
Aerospace Series Sealants Test Method Determination of Application Time-Edition P 1 |
|
AECMA PREN 3095 |
Aerospace Series Sealants Test Method Determination of Extended Assembly Time-Edition P 1 |
|
AECMA PREN 3095 |
Aerospace Series Test Method for Sealants Determination of Extended Assembly Time |
|
AECMA PREN 3096 |
Aerospace Series Sealants Test Method Determination of Tack-Free Time |
|
AECMA PREN 3096 |
Aerospace Series Sealants Test Method Determination of Tack-Free Time-Edition P 1 |
|
AECMA PREN 3098 |
Aerospace Series Test Methods for Sealants Determination of the Curing Rate and Repairability After Storage in Fluids |
|
AECMA PREN 3101 |
Aerospace Series Non-Metallic Materials Sealants Test Method Determination of Resistance to Thermal Rupture-Edition P 1 |
|
AECMA PREN 3101 |
Aerospace Series Test Methods for Sealants Determination of Resistance to Thermal Rupture |
|
AECMA PREN 3102 |
Aerospace Series Sealants Test Methods Determination of Low-Temperature Flexibility |
|
AECMA PREN 3102 |
Aerospace Series Sealants Test Methods Determination of Low-Temperature Flexibility-Edition P 1 |
|
AECMA PREN 3103 |
Aerospace series test methods for sealants determination of resistance to peeling |
|
AECMA PREN 3104 |
Aerospace Series Sealants Test Methods Determination of Shear Strength |
|
AECMA PREN 3105 |
Aerospace Series Sealants Test Methods Determination of the Corrosive Effect of Sealants on Metallic Materials |
|
AECMA PREN 3106 |
Aerospace Series Sealants, Test Methods Determination of Loss of Mass and Flexibility After Fluid Immersion |
|
AECMA PREN 3110 |
Aerospace Series Sealants Method of Manufacture of Moulded Plates |
|
AECMA PREN 3112 |
Aerospace Series Bolts, Normal Hexagonal Head, Threaded to Head, in Alloy Steel, Cadmium Plated Classification: 900 MPa (at Ambient Temperature)/235 Degrees C-Edition P 2 |
|
AECMA PREN 3112 |
Screws, Hexagonal Normal Head, Fully Threaded in Steel, Cadmium Plated Classification 900 MPa/235 Degrees Celsius |
|
AECMA PREN 3113 |
Aerospace Series Screws, Hexagonal Normal Head, Fully Threaded in Titanium Alloy Anodized Classification: 900 MPa/315 Degrees Celsius-Issue P 1 |
|
AECMA PREN 3113 |
Aerospace Series Screws, Hexagonal Normal Head, Fully Threaded, in Titanium Alloy Anodized Classification: 900 MPa/315 Degrees C-Edition P 2; Withdrawn - Not Replaced |
|
AECMA PREN 3114-1 |
Aerospace Series Microstructure of (a + b) Titanium Alloy Wrought Products Part 1: General Requirements-Issue P 1 |
|
AECMA PREN 3114-2 |
Aerospace Series Microstructure (a + b) Titanium Alloy Wrought Products Part 2: Microstructure of Bars, Sections, Forging Stock and Forgings-Issue P 1 |
|
AECMA PREN 3114-3 |
Aerospace Series Microstructure of (a + b) Titanium Alloy Wrought Products Part 3: Microstructure of Plate-Issue P 1 |
|
AECMA PREN 3114-3 |
Aerospace Series Test Method Microstructure of (a + b) Titanium Alloy Wrought Products Part 3: Microstructure of Plate-Edition P 1 |
|
AECMA PREN 3114-4 |
Aerospace Series Test Method Microstructure of (a + b) Titanium Alloy Wrought Products Part 4: Microstructure of Sheet for Superplastic Forming-Edition P 1 |
|
AECMA PREN 3115 |
Aerospace Series Aluminium Alloy AL-P7050-Wire for Rivets D Less Than or Equal to 10 mm |
|
AECMA PREN 3115 |
Aerospace Series Aluminium Alloy AL-P7050-Wire for Rivets D Less Than or Equal to 10 mm-Edition P1 |
|
AECMA PREN 3119 |
Aerospace Series Titanium Alloy TI-P46001 not Heat Treated Grade 2 Forging Stock, for Solution Treated and Aged Forgings a or D Less Than or Equal to 360 mm-Edition P 2 |
|
AECMA PREN 3120 |
Aerospace Series Titanium Alloy TI-P64003 Cold Worked and Stress Relieved Seamless Tube for Pressure Systems 4 mm Less Than or Equal to D Less Than or Equal to 51 mm 690 MPa Less Than or Equal to Rm Less Than or Equal to 1 030 MPa-Edition P 2 |
|
AECMA PREN 3120 |
Aerospace Series Titanium Alloy TI-P64003 Cold Worked and Stress Relieved Seamless Tube for Pressure Systems 4 mm Less Than or Equal to D Less Than or Equal to 51 mm-Edition P 3 |
|
AECMA PREN 3122 |
Aerospace Series Aluminium Alloy AL-C27 Solution Treated and Artificially Aged (T6) High Strength Structural Precision Castings-Issue P 1 |
|
AECMA PREN 3123 |
Aerospace Series Aluminium Alloy AL-C27 Solution Treated and Artificially Aged (T6) Structural Precision Castings-Issue P 1 |
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AECMA PREN 3124 |
Aerospace Series Aluminium Alloy AL-C26 Solution Treated and Artificially Aged (T6) High Strength Structural Precision Castings-Issue P 1 |
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AECMA PREN 3124 |
Aerospace Series Aluminium Alloy AL-C42201 T6 High Strength Casting a Less Than or Equal to 20 mm-Edition P2 |
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AECMA PREN 3124 |
Aerospace Series Aluminium Alloy AL-C42201 T6 High Strength Castings a Less Than or Equal to 20 mm-Issue P 2 |
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AECMA PREN 3137 |
Aerospace Series Rivets, Solid, 100 Degree Normal Countersunk Head with Dome, in Corrosion Resisting Steel EN 2470, Passivated-Edition 1 |
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AECMA PREN 3137 |
Aerospace Series Rivets, Solid, 100 Degree Normal Countersunk Head with Dome, in Corrosion Resisting Steel FE-PA11, Passivated-Issue P 1 |
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AECMA PREN 3137 |
Rivets, Solid, 100 Degrees Normal Countersunk Head with Dome, in Corrosion Resisting Steel EN 2470, Passivated |
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AECMA PREN 3138 |
Aerospace Series Rivets, Solid, 100 Degree Countersunk Normal Head with Dome, in Corrosion Resisting Steel FE-PA92HT, Passivated, Inch Based Series-Edition P 2; Supersedes Edition P 1: February 1995; Replaced by EN 3138 |
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AECMA PREN 3139 |
Aerospace Series Rivets, Solid, 100 Degree Countersunk Normal Head, in Corrosion Resisting Steel FE-PA11, Passivated Inch Based Series-Edition P 2; Supersedes Edition P 1: February 1995; Replaced by EN 3139 |
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AECMA PREN 3140 |
Aerospace Series Rivets, Solid, 100 Degree Normal Head, in Corrosion Resisting Steel FE-PA92HT, Passivated, Inch Based Series-Edition P 2; Supersedes Edition P 1: February 1995; Replaced by EN 3140 |
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AECMA PREN 3141 |
Aerospace Series Rivets, Solid, Universal Head, in Nickel Base Alloy NI-P11, Cadmium Plated-Issue P 1 |
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AECMA PREN 3142 |
Aerospace Series Rivets, Solid, Universal Head, in Nickel Base Alloy NI-P11-Issue P 1 |
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AECMA PREN 3143 |
Aerospace Series Rivets, Solid, 100 Degrees Countersunk Normal Head, in Nickel Base Alloy NI-P11, Cadmium Plated, Inch Based Series-Edition P 1 |
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AECMA PREN 3144 |
Aerospace Series Rivets, Solid, 100 Degrees Countersunk Normal Head, in Nickel Base Alloy NI-P11, Inch Based Series-Edition P 1 |
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AECMA PREN 3145 |
Aerospace Series Round Bars with Normal Tolerances Hot Formed, in Steel Diameter 6 mm Less Than or Equal to D Less Than or Equal to 250 mm Dimensions-Edition P 1 |
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AECMA PREN 3146 |
Aerospace Series Round Bars with Close Tolerances Hot Formed in Steel 6 mm < D Less Than or Equal to 250 mm Dimensions-Edition P 1 |
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AECMA PREN 3148 |
Aerospace Series Shank Nuts, Self-Locking, Flange Restrained Installation Procedure-Issue P 2 |
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AECMA PREN 3149 |
Aerospace Series Shank Nuts, Metric Installation Holes-Issue P 1 |
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AECMA PREN 3155-001 |
Aerospace Series Electrical Contacts Used in Elements of Connection Part 001 - Technical Specification-Edition P 1 |
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AECMA PREN 3155-001 |
Aerospace Series Electrical Contacts Used in Elements of Connection Part 001 - Technical Specification-Edition P 2 |
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AECMA PREN 3155-001 |
Aerospace Series Electrical Contacts Used in Elements of Connection Part 001: Technical Specification-Edition P 3 |
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AECMA PREN 3155-001 |
Aerospace Series: Electrical Contacts Used in Connection Devices Technical Specification |
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AECMA PREN 3155-002 |
Aerospace Series Electrical Contacts Used in Elements of Connection Part 002: List and Utilization of Contacts-Edition P 2 |