Search Results

Standard

YARN, ORGANIC FIBER (PARA-ARAMID), HIGH MODULUS OY 390 (2689)/23.5 Tensile Strength, 16.5 (114)/900 Tensile Modulus 720 Denier, 1.2% Finish

1996-02-01

HISTORICAL

AMS3901/17

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

Standard

YARN, ORGANIC FIBER (PARA-ARAMID), HIGH MODULUS OY 390 (2689)/22.6 Tensile Strength, 16.5 (114)/840 Tensile Modulus 2450 Denier, 0.6% Finish

1996-02-01

HISTORICAL

AMS3901/13

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

Standard

YARN, ORGANIC FIBER (PARA-ARAMID), HIGH MODULUS OY 390 (2689)/22.5 Tensile Strength, 16.5 (114)/830 Tensile Modulus 2840 Denier, 0.6% Finish

1996-02-01

HISTORICAL

AMS3901/14

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

Standard

YARN, ORGANIC FIBER (PARA-ARAMID), HIGH MODULUS OY 390 (2689)/22.0 Tensile Strength, 16.5 (114)/825 Tensile Modulus 2160 Denier, 0.6% Finish

1996-02-01

HISTORICAL

AMS3901/7B

This specification covers one type of organic fiber in the form of yarn. The product shall be formed as a multiplicity of filaments drawn together and gathered into an approximately parallel arrangement.

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, Polyvinylidene Fluoride Jacket, Tin-Coated Copper Conductor, 600-Volt, 110°C

2017-12-07

CURRENT

AS50861/5A

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, Polyvinylidene Fluoride Jacket, Tin-Coated Copper Conductor, 600-Volt, 110°C

2012-12-12

HISTORICAL

AS50861/5

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, Polyvinylidene Fluoride Jacket, Silver-Coated Copper Alloy Conductor, 600-Volt, 110°C

2018-01-02

CURRENT

AS50861/6A

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, Polyvinylidene Fluoride Jacket, Silver-Coated Copper Alloy Conductor, 600-Volt, 110°C

2012-12-12

HISTORICAL

AS50861/6

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, PVC-Glass-PVC-Nylon, Tin-Coated Copper Conductor, 600-Volt, 105°C

2012-12-12

HISTORICAL

AS50861/3

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, PVC-Glass-PVC-Nylon, Tin-Coated Copper Conductor, 600-Volt, 105°C

2017-12-07

CURRENT

AS50861/3A

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, PVC-Glass-Nylon, Tin-Coated Copper Conductor, 600-Volt, 105°C

2012-12-12

HISTORICAL

AS50861/2

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, Nylon Jacket, Tin-Coated Copper Conductor, Medium Weight, 600-Volt, 105°C

2012-04-04

HISTORICAL

AS50861/7

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, Nylon Jacket, Tin-Coated Copper Conductor, 600-Volt, 105°C

2012-04-04

HISTORICAL

AS50861/1

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, Nylon Jacket, Tin-Coated Copper Conductor, 3000-Volt, 105°C

2018-02-06

CURRENT

AS50861/4A

Standard

Wire, Electrical, Polyvinyl Chloride Insulated, Nylon Jacket, Tin-Coated Copper Conductor, 3000-Volt, 105°C

2012-12-12

HISTORICAL

AS50861/4

Standard

Wing Inspection Lights – Design Criteria

2018-10-10

HISTORICAL

ARP4087C

This SAE Aerospace Recommend Practice (ARP) is intended to cover the external lights on fixed wing aircraft for illuminating the wing leading edge and engine nacelles and the upper surfaces of the wing. The addition of an ice detection system should be implemented when the areas to inspect are not visible from the aircraft cockpit. It is not intended that this Recommended Practice require the use of any particular light source such as Halogen, LED or other specific design of lamp.

Standard

Wing Inspection Lights - Design Criteria

2006-09-12

HISTORICAL

ARP4087B

This SAE Aerospace Recommend Practice (ARP) is intended to cover the external lights on fixed wing aircraft for illuminating the wing leading edge and nacelles and the upper surfaces of the wing. The addition of ice detection system should be implemented when the areas to inspect are not visible from the aircraft cockpit.

Standard

Wing Inspection Lights - Design Criteria

2023-02-06

CURRENT

ARP4087D

This SAE Aerospace Recommend Practice (ARP) is intended to cover the external lights on fixed wing aircraft for illuminating the wing leading edge and engine nacelles and the upper surfaces of the wing. The addition of an ice detection system should be implemented when the areas to inspect are not visible from the aircraft cockpit. It is not intended that this recommended practice require the use of any particular light source such as halogen, LED, or other specific design of lamp.

Standard

Wheels and Brakes, Supplementary Criteria for Design Endurance Civil Transport Aircraft

2008-02-07

HISTORICAL

ARP597D

This document recommends supplementary design criteria to enhance endurance and reliability of transport aircraft wheels and brakes.

Standard

Wheels and Brakes, Supplementary Criteria for Design Endurance Civil Transport Aircraft

2015-05-07

CURRENT

ARP597E

This document recommends supplementary design criteria to enhance endurance and reliability of transport aircraft wheels and brakes.