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Standard

AIRCRAFT ENVIRONMENTAL FACTORS FOR DESIGN CONSIDERATION

2002-12-16
CURRENT
AIR1309
This AIR is presented in two parts - the first part, to alert the engineer with respect to the environmental factors which he might have to consider - the second part, as tabular data and figures to which he can refer with respect to a specific geographical location.
Standard

SELECTION CRITERIA FOR RECIPROCATING PRIME MOVERS

1989-10-01
HISTORICAL
ARP1052
This Recommended Practice covers the following categories: a Basic engine rating (requirements for) - (Para. 3) b Suggested minimum conditions for selection - (Para. 4) c Recommended horsepower rating reductions - (Para. 5) d Special considerations - (Para. 6) e Recommended safety devices - (Para. 7) f Recommended minimum instrumentation - (Para. 8) g Recommended selection support data - (Para. 9) h Recommended usage of ARP - (Para. 10)
Standard

CHARGER FOR BATTERY POWERED GROUND SUPPORT EQUIPMENT

1991-04-01
HISTORICAL
ARP1816A
This recommended practice describes an industrial battery charger, solid state type, hereafter called charger, for use in charging lead acid batteries in ground support equipment.
Standard

CHARGER FOR BATTERY POWERED GROUND SUPPORT EQUIPMENT

1984-09-01
HISTORICAL
ARP1816
This recommended practice describes an industrial battery charger, solid state type, hereafter called charger, for use in charging lead acid batteries in ground support equipment.
Standard

Charger for Battery Powered Ground Support Equipment

2009-06-29
HISTORICAL
ARP1816C
This SAE Aerospace Recommended Practice (ARP) describes two general types of Ground Support Equipment (GSE) battery chargers. The conventional industrial battery charger typically requiring up to 8 hours to recharge a 100% discharged battery, hereafter called “Conventional Charger”. The other type a fast battery charger typically used as an opportunity charger for ground support equipment, hereafter called “Fast Charger”. Recommendations that apply to both types will refer generically to “charger”.
Standard

CHARGER FOR BATTERY POWERED GROUND SUPPORT EQUIPMENT

1996-07-01
HISTORICAL
ARP1816B
This SAE Aerospace Recommended Practice (ARP) describes an industrial battery charger, solid state type, hereafter called charger, for use in charging lead acid batteries in ground support equipment.
Standard

Charger for Battery Powered Ground Support Equipment

2020-09-23
CURRENT
ARP1816D
This SAE Aerospace Recommended Practice (ARP) describes three general types of Ground Support Equipment (GSE) battery chargers. The battery charger typically requiring up to 8 hours to recharge a 100% discharged battery, hereafter called “Conventional Charger.” A charger, hereafter called “Opportunity Charger,” which has the ability to charge at a slightly faster rate than a conventional charger. A charger, hereafter called “Fast Charger,” which has the ability to charge at a much faster rate than a conventional charger. Recommendations that apply to all types will refer generically to “charger.”
Standard

Battery Powered Aircraft Tow Tractors - Factors for Design Consideration

2018-09-27
CURRENT
AIR1854A
This SAE Aerospace Information Report (AIR) identifies and summarizes the various factors that must be considered and evaluated by the design or specifying engineer in establishing the specifications and design characteristics of battery-powered aircraft tow tractors. This AIR is presented in two parts. The first part is simply a summarization of design factors that must be considered in establishing vehicle specifications and design characteristics. The second part refers particularly to the performance characteristics of an aircraft tow tractor. Some definitions, formulas, data, and an example are provided mainly for assisting the specifying engineers of potential buyers and users of aircraft tow tractors in the evaluation and comparison of their requirements with the performance capabilities of the various tow tractors offered by the tow tractor manufacturers.
Standard

ELECTRICAL CONNECTORS FOR USE IN BATTERY POWERED GROUND SUPPORT EQUIPMENT

1985-07-01
HISTORICAL
ARP1892
This recommended practice describes a two-pole electric connector for use in battery powered ground support equipment i.e. traction batteries. Alternatively, the connector can have two or more auxiliary contacts for auxiliary circuits. A handle may be added as an option to assist in connecting and disconnecting.
Standard

ELECTRICAL CONNECTORS FOR USE IN BATTERY POWERED GROUND SUPPORT EQUIPMENT

1991-04-29
HISTORICAL
ARP1892A
This recommended practice describes a two-pole electric connector for use in battery powered ground support equipment, i.e., traction batteries. Alternatively, the connector can have two or more auxiliary contacts for auxiliary circuits. A handle may be added as an option to assist in connecting and disconnecting.
Standard

Wheel Chocks

2021-04-08
CURRENT
AIR4905A
The purpose of this document is to present general considerations for the design and use of aircraft wheel chocks. The design and use of aircraft wheel chocks is a good deal more complicated than it may appear at first glance.
Standard

Wheel Chocks

2011-05-16
HISTORICAL
AIR4905
The purpose of this document is to present general considerations for the design and use of aircraft wheel chocks. The design and use of aircraft wheel chocks is a good deal more complicated than it may appear at first glance.
Standard

GROUND EQUIPMENT - 400 HERTZ GROUND POWER PERFORMANCE REQUIREMENTS

1996-06-01
HISTORICAL
ARP5015
This SAE Aerospace Recommended Practice (ARP) covers the requirements for ground power equipment that supplies 115/200 V, 3-phase, 400 Hz output capable of powering aircraft type loads requiring MIL-STD-704E/DFS-400 quality power. All forms of ground power including mobile and fixed systems are addressed by this document. High voltage (270 V DC) systems are not included in this specification.
Standard

Ground Equipment - 400 Hertz Ground Power Performance Requirements

2011-01-14
HISTORICAL
ARP5015A
This SAE Aerospace Recommended Practice (ARP) covers the requirements for ground power equipment that supplies 115/200 V, 3-phase, 400 Hz output capable of powering aircraft type loads requiring MIL-STD-704E/DFS-400 quality power. All forms of ground power including mobile and fixed systems are addressed by this document. High voltage (270 V DC) systems are not included in this specification.
Standard

VEHICLE ELECTRICAL SYSTEMS

2007-08-29
HISTORICAL
AIR1336A
This SAE Aerospace Information Report (AIR) considers the following major areas: 1 Major components and their ratings 2 Selection criteria for optimum design balance for electrical systems 3 Effects of operating conditions and environment on both maintenance and life of components 4 Trouble signals—their diagnosis and cure
Standard

Ground Support Equipment Electrical Systems

2018-09-27
CURRENT
AIR1336B
This SAE Aerospace Information Report (AIR) considers the following major areas: 1 major components and their ratings; 2 selection criteria for optimum design balance for electrical systems; 3 effects of operating conditions and environment on both maintenance and life of components; 4 trouble signals - their diagnosis and cure.
Standard

VEHICLE ELECTRICAL SYSTEMS

1975-05-01
HISTORICAL
AIR1336
This document considers the following major areas: 1 Major components and their ratings 2 Selection criteria for optimum design balance for electrical systems 3 Effects of operating conditions and environment on both maintenance and life of components 4 Trouble signals -- their diagnosis and cure
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