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Viewing 211 to 240 of 35892
2017-12-07
WIP Standard
AS7232A
This procurement specification covers aircraft quality solid rivets and tubular end rivets made form a corrosion and heat resistant nickel base alloy of the type identified under the Unified Numbering System as UNS N06600. Primarily for fastener applications requiring corrosion resistance and heat and oxidation resistance up to 2000 degrees F, but with reduced strength at the elevated temperatures. Rivets shall not be hand peened during driving.
2017-12-07
WIP Standard
AS848A
No scope available.
2017-12-07
WIP Standard
MA3287A
Scope is unavailable.
2017-12-07
WIP Standard
MA3344A
Scope is unavailable.
2017-12-07
WIP Standard
MA3350A
Scope is unavailable.
2017-12-07
WIP Standard
MA1421A
This SAE Aerospace Standard (MA) establishes the diameter-pitch combinations of ISO metric 60° screw threads recommended for use in the aerospace industry for metric module shaft or bearing retaining screw threads.
2017-12-07
WIP Standard
AS24586C
SCOPE IS UNAVAILABLE.
CURRENT
2017-12-07
Standard
ARP5718B
This document describes: the preparatory steps to test experimental Type II, III, and IV fluids according to AMS1428; the recommendations for the preparation of samples for endurance time testing according to ARP5485; a short description of wind tunnel testing; a short description of the recommended field spray test; the protocol to generate draft holdover time guidelines from endurance time data obtained from ARP5485; the protocol for inclusion of Type II, III, and IV fluids on the FAA and Transport Canada lists of fluids and the protocol for updating the lists of fluids; the role of the SAE G-12 Aircraft Deicing Fluids Committee; the role of the SAE G-12 Holdover Time Committee; and the process for the publication of Type II, III, and IV holdover time guidelines. This document does not describe laboratory testing procedures. This document does not include the qualification requirements for AMS1424 Type I fluids (these are provided in ARP6207).
CURRENT
2017-12-07
Standard
AMS5350K
This specification covers a corrosion and moderate heat-resistant steel in the form of investment castings.
CURRENT
2017-12-07
Standard
AMS6349E
This specification covers an aircraft-quality, low-alloy steel in the form of bars.
CURRENT
2017-12-07
Standard
AMS4035M
This specification covers an aluminum alloy in the form of sheet and plate 0.010 to 1.750 inch (0.25 to 44.45 mm) in thickness, supplied in the annealed (O temper) condition (see 8.4). When specified, product shall be supplied in the “as fabricated” (F) temper.
CURRENT
2017-12-07
Standard
AMS5532H
This specification covers a corrosion and heat-resistant iron alloy in the form of sheet, strip, and plate.
CURRENT
2017-12-07
Standard
AMS6931D
This specification covers a titanium alloy in the form of bars and forgings up through 10.000 inches (254.00. mm), inclusive, in diameter or least distance between parallel sides with a maximum cross-sectional area of 79.0 in2 (506.45 cm2) and forging stock of any size (see 8.7).
CURRENT
2017-12-07
Standard
AMS5537J
This specification covers a corrosion and heat-resistant cobalt alloy in the form of sheet, strip, foil, and plate up to 2.250 inches (57.15 mm) inclusive, in nominal thickness (see 8.4).
CURRENT
2017-12-07
Standard
AMS4928W
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes up through 10.000 inches (254.00 mm) inclusive in diameter or least distance between parallel sides and stock of any size for forging or flash welded rings.
CURRENT
2017-12-05
Standard
AMS6466G
This specification covers a corrosion-resistant steel in the form of welding wire.
2017-12-01
WIP Standard
ARP1176B
This SAE Aerospace Recommended Practice (ARP) provides recommended practices for cleaning aircraft oxygen equipment such as tubing, pieces, parts (including regulator and valve parts), cylinders and ground-based equipment that may be used to support aircraft oxygen systems. This revision introduces a cleanliness coding scheme that can be referenced as a requirement, and/or referenced to identify compliance to meeting such a requirement. These methods may apply to gaseous and liquid oxygen equipment. This document specifies work area details, methods to select suitable cleaning agents, cleaning methods, test methods to verify cleanliness level, and methods of packaging the components and parts after cleaning. Technicians designated to clean oxygen equipment must be qualified and trained to clean oxygen equipment. This ARP is applicable to metallic and non-metallic parts.
2017-12-01
WIP Standard
AMS3021F
This specification covers a neopentyl polyol ester fluid.
CURRENT
2017-11-30
Standard
AIR5709A
To present the results of a survey taken concerning future applications for high-temperature electronics and sensors.
CURRENT
2017-11-30
Standard
AIR34B
The scope of this SAE Aerospace Information Report (AIR) is to present a guide for the determination of probable power output and the effect on the aircraft system that will be experienced when operating three-phase motors with one phase open. Unfortunately, the above subject cannot be resolved by specific rules. Modern aircraft or missile electrical systems are composed of a wide variety of electrical and electronic components. These components react differently under identical impetus due to the latitude of their design. This latitude of design must be allowed wherever possible to the accessory designer due to the various specification requirements. Therefore, it cannot be over-emphasized that the effect on the airplane or missile system, as well as motor operation, of three-phase motors on two-phase power must be thoroughly investigated.
Viewing 211 to 240 of 35892