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Standard

Ground Support Equipment Electrical Systems

2013-03-28
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
Standard

VEHICLE ELECTRICAL SYSTEMS

1996-06-01
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

EXHAUST EMISSION LIMITS FOR DIESEL ENGINES USED IN AIRCRAFT GROUND SUPPORT EQUIPMENT AT AIRPORT ENVIRONMENTS

2002-12-16
CURRENT
AIR1312
This Aerospace Information Report (AIR) outlines the conditions which diesel engines should meet when installed and used as prime movers for aircraft ground support equipment at commercial airports. All aircraft ground support equipment with a heavy duty diesel engine as defined on page 24293 of the November 15, 1972 Federal Register and used as a prime mover for the vehicle or equipment should meet all requirements as outlined herein. Typical equipment includes fuel trucks, commissary trucks, baggage tractors, ground power units, air start units, etc.
Standard

COMMERCIAL AIRCRAFT TOWBAR ATTACH FITTING INTERFACE

1982-10-01
HISTORICAL
AS1614A
Operators of commercial passenger and cargo aircraft in unanimity will request aircraft manufacturers to follow this standard in the design of the nose gear (when towing operations are normally done from the nose gear) in conventional tricycle type landing gears.
Standard

Commercial Aircraft Towbar Attach Fitting Interface

1994-12-01
HISTORICAL
AS1614B
Operators of commercial passenger and cargo aircraft in unanimity will request aircraft manufacturers to follow this standard in the design of the nose gear (when towing operations are normally done from the nose gear) in conventional tricycle type landing gears.
Standard

Chassis Mounted Lifts Used to Board Airline Passengers With Mobility Impairments

1999-07-01
HISTORICAL
ARP5141
This SAE Aerospace Recommended Practice (ARP) is intended to recommend a minimum standard, for the design and manufacturer of a self-propelled, chassis mounted passenger boarding vehicle. The vehicle will permit safe operation while minimizing aircraft damage and personnel safety hazards associated with commercial aircraft boarding operations. The vehicle described is intended to be used for assisting wheelchair passengers and passengers with disabilities on and off aircraft with door sill heights of 60 in (152.4 cm) and above.
Standard

Chassis Mounted Lifts Used to Board Airline Passengers With Mobility Impairments

2014-03-11
CURRENT
ARP5141A
This SAE Aerospace Recommended Practice (ARP) is intended to recommend a minimum standard, for the design and manufacturer of a self-propelled, chassis mounted passenger boarding vehicle. The vehicle will permit safe operation while minimizing aircraft damage and personnel safety hazards associated with commercial aircraft boarding operations. The vehicle described is intended to be used for assisting wheelchair passengers and passengers with disabilities on and off aircraft with door sill heights of 60 in (152.4 cm) and above.
Standard

Pallet/Container Loader Auto-Levelling Systems

1994-03-01
CURRENT
ARP4776
The data in this document is, at this stage, primarily concerned with the interface of pallet/container loaders and lower-deck compartments of standard and wide-body aircraft although the principles illustrated may be applied to the main-decks of narrow and wide-body aircraft. NOTE: For the purpose of this document, in accordance with Part 3 of the Directives for the technical work of ISO and with accepted IATA practice, minimum essential criteria defined by the word "shall" are absolute requirements. Recommended criteria identified by the word "should", while considered important, are not mandatory.
Standard

Regional Aircraft Towbarless Tow Vehicle - Test Requirements

2002-12-13
HISTORICAL
ARP5911
The present Aerospace Recommended Practice specifies for airplane operator and tow vehicle manufacturers the basic testing requirements for towbarless tow vehicles to be used on the nose gear of conventional tricycle type landing gears of commercial civil transport aircraft with maximum ramp weight between 8,600 kg (19,000 lb) and 50,000 kg (110,000 lb), commonly designated as “regional aircraft”. Its purpose is to achieve testing results, or equivalent computer modeling, demonstrating that the loads induced by the tow vehicle will not exceed the design loads of the airplane's nose landing gear and associated structure, reduce the certified safe life limit of the nose landing gear, or otherwise compromise the airplane's structural integrity and airworthiness certification.
Standard

Regional Aircraft Towbarless Tow Vehicle - Test Requirements

2012-08-22
CURRENT
ARP5911A
The present Aerospace Recommended Practice specifies for airplane operator and tow vehicle manufacturers the basic testing requirements for towbarless tow vehicles to be used on the nose gear of conventional tricycle type landing gears of commercial civil transport aircraft with maximum ramp weight between 8600 kg (19 000 lb) and 50 000 kg (110 000 lb), commonly designated as “regional aircraft”. Its purpose is to achieve testing results, or equivalent computer modeling, demonstrating that the loads induced by the tow vehicle will not exceed the design loads of the airplane’s nose landing gear and associated structure, reduce the certified safe life limit of the nose landing gear, or otherwise compromise the airplane’s structural integrity and airworthiness certification.
Standard

Regional Aircraft Towbar Attach Fitting Interface

2002-09-20
HISTORICAL
AS5488
This SAE Aerospace Standard (AS) specifies the interface requirements for towbar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft with a maximum ramp weight between 8600 kg (19 000 lb) and 50 000 kg (110 000 lb), commonly designated as “regional aircraft”. Its purpose is to achieve towbar attachment fittings interface standardization by aircraft weight category (which determines towbar forces) in order to ensure that one single type of towbar with a standard connection can be used for all aircraft types within or near that weight category, so as to assist operators and airport handling companies in reducing the number of different towbar types used.
Standard

Regional Aircraft Towbar Attach Fitting Interface

2011-06-20
CURRENT
AS5488A
This SAE Aerospace Standard (AS) specifies the interface requirements for towbar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft with a maximum ramp weight between 8600 kg (19 000 lb) and 50 000 kg (110 000 lb), commonly designated as "regional aircraft". Its purpose is to achieve towbar attachment fittings interface standardization by aircraft weight category (which determines towbar forces) in order to ensure that one single type of towbar with a standard connection can be used for all aircraft types within or near that weight category, so as to assist operators and airport handling companies in reducing the number of different towbar types used.
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

1997-12-01
CURRENT
ARP1892B
This SAE Aerospace Recommended Practice (ARP) 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

AIRCRAFT CARGO CONVEYOR - BATTERY POWERED

1994-12-01
HISTORICAL
ARP1836A
This SAE Aerospace Recommended Practice (ARP) outlines the functional and design requirements for a battery powered, self-propelled belt conveyor for handling baggage and cargo at aircraft bulk cargo holds.
Standard

AIRCRAFT CARGO CONVEYOR - BATTERY POWERED

1985-07-01
HISTORICAL
ARP1836
This Recommended Practice outlines the functional and design requirements for a battery powered, self propelled belt conveyor for handling baggage and cargo at aircraft bulk cargo holds.
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