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Standard

ELECTROMAGNETIC TESTING BY EDDY CURRENT METHODS

1991-03-01
HISTORICAL
J425_199103
The purpose of this SAE Information Report is to provide general information relative to the nature and use of eddy current techniques for nondestructive testing. The document is not intended to provide detailed technical information but to serve as an introduction to the principles and capabilities of eddy current testing, and as a guide to more extensive references listed in Section 2.
Standard

LIQUID PENETRANT TEST METHODS

1991-03-01
HISTORICAL
J426_199103
The scope of this SAE Information Report is to supply the user with sufficient information so that he may decide whether liquid penetrant test methods apply to his particular inspection problem. Detailed technical information can be obtained by referring to Section 2.
Standard

Tonne Kilometer Per Hour Application

1991-03-01
HISTORICAL
J1098_199103
This SAE Standard establishes the procedures for the application of Tonne Kilometer Per Hour (TKPH) rating values for off-the-road tires; utilizing empirical data formula, it describes the procedure for evaluating and predicting off-the-road tire TKPH requirements as determined by a work cycle analysis.
Standard

Tonne Kilometer Per Hour Test Procedure

1991-03-01
HISTORICAL
J1015_199103
This SAE Standard establishes the Tonne Kilometer Per Hour Test Procedure for off-the-road tires. This document is applicable to only those tires used on certain earthmoving machines referenced in SAE J1116.
Standard

Bolts and Screws, Steel, Corrosion and Moderate Heat Resistant Heat Treated, Roll Threaded

1991-02-28
HISTORICAL
AS7470
This procurement specification covers aircraft quality bolts and screws made from a corrosion and moderate heat resistant martensitic iron base alloy of the type identified under the Unified Numbering System as UNS S41800 and of 140 000 psi and 152 000 psi tensile strengths at room temperature. Primarily for aerospace propulsion system applications where corrosion and moderate heat resistant is required.
Standard

Some Factors Affecting Visibility of Aircraft Navigation and Anticollision Lights

1991-02-27
HISTORICAL
AIR1106A
The scope of this Aerospace Information Report (AIR) is to discuss factors affecting visibility of aircraft navigation and anticollision lights, enabling those concerned with their use to have a better technical understanding of such factors, and to aid in exercising appropriate judgement in the many possible flight eventualities.
Standard

Steering Effect of Tilted, Free-Swiveling Nose Gears

1991-02-27
CURRENT
AIR4358
This Aerospace Information Report (AIR) considers the origin of cornering forces generated by tilted, free-swiveling nose gears; the effect of various landing gear parameters on the measured cornering forces; and a method of towing aircraft to measure the resulting steering forces.
Standard

COMBINATION EVACUATION SLIDE/RAFT - CIVIL AIR TRANSPORT

1991-02-22
HISTORICAL
ARP1146B
This Aerospace Recommended Practice (ARP) is to establish criteria for design and installation of combination evacuation slide/raft devices for use both as ground and water escape devices in the event of emergency. NOTE: This document is not intended to specify design methods, mechanisms, or equipment to be used in accomplishment of the objectives set forth herein.
Standard

Aircraft Engine Fuel Feed and Transfer Component Pressure Definitions

1991-02-13
CURRENT
AIR1749
The information in this document is limited to aircraft engine fuel feed, refueling, and transfer components (reference 2.1). It is assumed that isothermal, liquid fluid conditions exist, herein referred to as fuel. Where a unit of measure is suffixed, this is intended to show a generally associated unit for illustration only and is not an exclusive endorsement of this particular term. Where applicable and allowable it is understood that a referee fluid may be substituted for fuel.
Standard

AIRCRAFT GROUND AIR CONDITIONING SERVICE CONNECTION

1991-02-12
HISTORICAL
AS4262
This SAE Aerospace Standard (AS) defines interface configurations for the ground air conditioning service connection on commercial transport aircraft. In addition, it defines the clearances required to accommodate the connection of ground air conditioning hose couplings. Two types of service connections are included. The Type A connection (Figure 1) is a slotted ring with integral locking pads and is comparable to the MS33562 connection. The Type B connection (Figure 2) is a flanged tube with external locking lugs (Figure 3). The Type B connection has the same interface dimensional requirements as the Type A connection.
Standard

GUIDE TO TEMPERATURE MONITORING IN AIRCRAFT GAS TURBINE ENGINES

1991-02-07
HISTORICAL
AIR1900
This Aerospace Information Report (AIR) provides an overview of temperature measurement for engine monitoring systems in various areas of aircraft gas turbine engines while focusing on current usage and methods, systems, selection criteria, and types of hardware. This document emphasizes temperature monitoring for diagnostics and condition monitoring purposes.
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