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Standard

Landing and Taxiing Lights - Design Criteria for Installation

2018-07-02
CURRENT
ARP693E
This document includes requirements of installations of adequate landing and taxiing lighting systems in aircraft of the following categories: a Single engine personal and/or liaison type b Light twin engine c Large multiengine propeller d Large multiengine turbojet/turbofan e Military high-performance fighter and attack f Helicopter This document will cover general requirements and recommended practices for all types of landing and taxi lights. More specific recommendations for LED lights in particular can be found in ARP6402.
Standard

Rings, Retaining – Spiral Wound, Uniform Section Corrosion and Heat Resistant, UNS S66286

2018-07-02
CURRENT
AS4299B
This procurement specification covers retaining rings of the spiral wound type with uniform rectangular cross-section, made of a corrosion and heat resistant age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286, work strengthened and heat treated to a tensile strength of 185 to 240 ksi at room temperature.
Standard

Ramp De-Icing

2018-06-28
CURRENT
AIR1335B
This Technical Report has been declared “CANCELLED” as of June 2018 and has been superseded by AS6285, AS6286, and AS6332. By this action, this document will remain listed in the respective index, if applicable. Cancelled Technical Reports are available from SAE.
Standard

Static Seal Test Fixture

2018-06-28
WIP
AS7982
This SAE Aerospace Standard (AS) provides dimensions and procedures for a standardized test fixture used to evaluate the static performance of O-rings and other seals in glands per AS4617 and AS5857
Standard

Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings 72Ni - 15.5Cr - 0.95Cb(Nb) - 2.5Ti - 0.70Al - 7.0Fe 1800 °F (982 °C) Solution Heat Treated, Precipitation Hardenable

2018-06-27
CURRENT
AMS5747E
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and flash welded rings up to 4.00 inches, including (101.6 mm, including) in nominal diameter or least distance between parallel sides, and stock of any size for forging or flash welded rings (see 8.5).
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