Refine Your Search

Search Results

Standard

Air Cargo Equipment Tracking Device - Performance and Test Requirements

2018-10-16
WIP
AS7353
Develop an AS for the minimum performance requirements for tracking devices that are utilized to track the location and other environmental conditions of a piece of equipment that will be transported on-board an aircraft, .i.e ULD, TCC, FRC. The AS will define test requirements or regulation that a device will need to meet to demonstrate no impact to its use on-board an aircraft operation and its crew. The goal would be to request a TSO be developed based on this new standard.
Standard

Predicting Photometric Degradation of Exterior Aircraft Lights

2018-10-16
WIP
ARP6621
This Aerospace Recommended Practice provides guidance for designers and specifiers of aircraft exterior lighting. Typical causes of light degradation and methods of predicting performance degradation in the aircraft environment are given.
Standard

Icing Wind Tunnel Interfacility Comparison Tests

2018-10-16
CURRENT
AIR5666A
This SAE Aerospace Information Report (AIR) presents and discusses the results of tests of three models in six icing wind tunnels in North America and Europe. This testing activity was initiated by the Facility Standardization Panel of the SAE AC-9C Aircraft Icing Technology Subcommittee. The objective of the testing activity was to establish a benchmark that compared ice shapes produced by icing wind tunnels available for use by the aviation industry and to use that benchmark as a basis for dialogue between facility owners to improve the state-of-the-art of icing wind tunnel technology.
Standard

Spacers and Washers, Procurement Specification for, Metric

2018-10-16
CURRENT
MA1784A
This specification covers metric aircraft quality spacers for use as positioners for tubes, flat washers for use as load spreaders, galling protection of adjacent surfaces and or material compatibility, and key or tab washers for use as locks for bolts, nuts, and screws.
Standard

Nuts, Self-Locking, UNS N07001, 730 °C, 1100 MPa, and 1210 MPa, Procurement Specification for, Metric

2018-10-16
CURRENT
MA1943B
This procurement specification covers aircraft quality self-locking nuts for wrenching (hex, spline) and anchor (plate, gang channel, shank) types of nuts made from a corrosion and heat-resistant nickel-base alloy of the type identified under the Unified Numbering System as UNS N07001. Tension height nuts having overall length of threaded portion not less than 1.2 times the nominal thread diameter have 1210 MPa minimum tensile strength at room temperature. Shear height nuts having shorter threaded portion have 1100 MPa minimum tensile strength at room temperature. Maximum test temperature of parts is 730 °C.
Standard

Part Qualification Guidelines

2018-10-16
WIP
AIR7352
Provide non-binding guidelines for qualifying a part by a regulatory agency such as FAA, NASA, etc.
Standard

Crew Station Lighting - Commercial Aircraft

2018-10-16
WIP
ARP1161B
This SAE Aerospace Recommended Practice covers the recommended requirements for the lighting and characteristics of instruments; information plates and displays, emergency, cautionary, advisory and status displays; circuit breaker and toggle switch positions; and the recommended requirements for the utility lighting system.
Standard

Air Cargo Unit Load Devices - Performance Requirements and Test Parameters

2018-10-16
WIP
AS36100C
This SAE Aerospace Standard (AS) defines the minimum performance requirements and test parameters for air cargo unit load devices requiring approval of airworthiness for installation in an approved aircraft cargo compartment and restraint system that complies with the cargo restraint requirements of Title 14 CFR Part 25, except for the 9.0g forward ultimate inertia force of § 25.561 (b)(3)(ii).
Standard

Test Method for Aerospace Firewall Sealant Flame Penetration

2018-10-15
WIP
AS5127/2C
This SAE Aerospace Standard (AS) describes the procedures for the flammability testing of aircraft firewall sealants in accordance with the requirements of FAR Part 25 Sections 25.865, 25.867, 25.1191, and 25.1193. This test method is intended to determine the capability of sealant materials to control the passage of and effects from fire.
Standard

Integrated Rudder and Brake Pedal Unit, General Requirements for Fly-By Wire Transport and Business Aircraft

2018-10-15
CURRENT
ARP6252
This Aerospace Recommended Practice (ARP) provides general requirements for a generic, integrated rudder and brake pedal unit, incorporating a passive force-feel system that could be used for fixed-wing fly-by wire transport and business aircraft. This ARP addresses the following: - The functions to be implemented - The mechanical interconnection between captain and F/O station - The geometric and mechanical characteristics - The mechanical, electrical, and electronic interfaces - The safety and certification requirements
Standard

J1349 Certified Power Engine Data for Fiat Chrysler as used in 2019 BV - Level 2

2018-10-15
CURRENT
CPFC2_19BV
This product includes information on the manufacturer, engine, applications, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds. In addition, this product contains complete engine information such as displacement, cylinder configuration, valve train, combustion cycle, pressure charging, charge air cooling, bore, stroke, cylinder numbering convention, firing order, compression ratio, fuel system, fuel system pressure, ignition system, knock control, intake manifold, exhaust manifold, cooling system, coolant liquid, thermostat, cooling fan, lubricating oil, fuel, fuel shut off speed, etc. Also included are all measured test parameters outlined in J2723.
X