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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

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

AIRCRAFT GROUND AIR CONDITIONING SERVICE CONNECTION

2005-07-11
HISTORICAL
AS4262A
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

Aircraft Damage Caused by Ground Support Equipment

2009-12-09
HISTORICAL
AIR1589A
Only those incidents where a piece of ground support equipment directly associated with the "turnaround" servicing of an aircraft was involved are reviewed. Specifically excluded are those incidents that occurred during heavy maintenance, overhaul activity, or aircraft taxiing.
Standard

Aircraft Damage Caused by Ground Support Equipment

2016-06-06
HISTORICAL
AIR1589B
Only those incidents where a piece of ground support equipment directly associated with the "turnaround" servicing of an aircraft was involved are reviewed. Specifically excluded are those incidents that occurred during heavy maintenance, overhaul activity, or aircraft taxiing.
Standard

Aircraft Damage Caused by Ground Support Equipment

2022-05-16
CURRENT
AIR1589C
Incidents where a piece of ground support equipment or personnel damages an aircraft under the control of ground or maintenance operations that requires corrective action by aircraft maintenance personnel. Operations include, but are not limited to servicing, line maintenance, heavy maintenance, and aircraft movement, e.g., marshalling/pushback/tow/reposition/taxi.
Standard

Aircraft Ground Service Connections Locations and Type

2021-09-30
CURRENT
ARP4084B
The purpose of this SAE Aerospace Recommended Practice (ARP) is to standardize locations of aircraft ground service connections to accommodate the trend toward fixed systems, which use the passenger boarding bridge and/or underground “pop-up” or pit systems as a source of utilities. It must be recognized that, in standardizing the locations of the aircraft service connections, they must continue to be served efficiently in those instances where mobile ground support equipment is used. There is an ever increasing number of fixed installations for aircraft servicing. The objectives to be met by standardizing the locations of the aircraft service connections are the following:
Standard

Aircraft Ground Support Equipment – General Requirements

2018-02-12
CURRENT
ARP1247E
This SAE Aerospace Recommended Practice (ARP) outlines the basic general design requirements for ground support equipment used in the civil air transport industry. It is intended to assist in standardizing requirements for various configurations of equipment. For procurement of equipment, sections of this document should be specified with due consideration of the functional and environmental requirements of the equipment, and to the relative cost of satisfying those requirements.
Standard

Aircraft Ground Support Equipment — General Requirements

2010-07-22
HISTORICAL
ARP1247D
This SAE Aerospace Recommended Practice (ARP) outlines the basic general design requirements for ground support equipment used in the civil air transport industry. It is intended to assist the airlines in standardizing requirements for various configurations of equipment. For procurement of equipment, sections of this document should be specified with due consideration of the functional and environmental requirements of the equipment, and to the relative cost of satisfying those requirements.
Standard

Aircraft Tow Bar

2005-04-06
HISTORICAL
ARP1915C
This SAE Aerospace Recommended Practice (ARP) outlines the basic general design considerations for transport aircraft tow bars. It does not cover the requirements for tow bars intended for aircraft with a maximum ramp mass (MRW) below 8,600 kg (19,000 lb).
Standard

Aircraft Tow Bar

2010-09-13
HISTORICAL
ARP1915D
This SAE Aerospace Recommended Practice (ARP) outlines the basic general design considerations for transport aircraft tow bars. It does not cover the requirements for tow bars intended for aircraft with a maximum ramp mass (MRW) below 8600 kg (19 000 lb).
Standard

Aircraft Towbar

1985-03-01
HISTORICAL
ARP1915
This Aerospace Recommended Practice (ARP) outlines the basic general design considerations for aircraft towbars.
Standard

Aircraft Towbar

1997-12-01
HISTORICAL
ARP1915B
This SAE Aerospace Recommended Practice (ARP) outlines the basic general design considerations for aircraft towbars.
Standard

Four Wheel Drive Aircraft Tow Tractors - Factors for Design Consideration

2020-09-23
CURRENT
AIR1363A
This Aerospace Information Report (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. Although the design engineers could also use the formulas and data in their calculations of the performance specifications of aircraft tow tractors, this AIR is not intended to provide the methods and all data necessary for detailed calculations and design of an aircraft tow tractor.
Standard

GENERAL REQUIREMENTS FOR AEROSPACE GROUND SUPPORT EQUIPMENT MOTORIZED AND NON-MOTORIZED

1992-12-01
HISTORICAL
ARP1247B
This Aerospace Recommended Practice (ARP) outlines the basic general design requirements for ground support equipment used in the civil air transport industry. It is intended to assist the airlines in standardizing requirements for various configurations of equipment; use only applicable sections for non-motorized equipment.
Standard

GENERAL REQUIREMENTS FOR AEROSPACE GROUND SUPPORT EQUIPMENT MOTORIZED AND NONMOTORIZED

1993-11-01
HISTORICAL
ARP1247C
This SAE Aerospace Recommended Practice (ARP) outlines the basic general design requirements for ground support equipment used in the civil air transport industry. It is intended to assist the airlines in standardizing requirements for various configurations of equipment. For procurement of equipment, sections of this document should be specified with due consideration of the functional and environmental requirements of the equipment, and to the relative cost of satisfying those requirements.
Standard

GROUND ELECTRICAL POWER UNIT, TRANSPORTABLE 115/200 VOLT AC (NOMINAL) 400 HERTZ, 3-PHASE 4-WIRE (GROUNDED NEUTRAL) Y-CONNECTED SYSTEM

1970-02-01
HISTORICAL
ARP1148
This Recommended Practice outlines the general requirements for a transportable self-contained, continuous duty, diesel engine driven brushless alternator unit for supplying 400-Hertz electrical power to high performance commercial transport aircraft. It is intended to assist the airlines in standardardizing recommendations for various sizes and configurations of equipment and it is a guide for the preparation of detailed specifications by the purchaser. The unit is primarily intended to supply power to the aircraft during passenger loading and unloading, and during servicing operations at airports throughout the world. The combination of the equipment specified herein and the interconnecting cable(s) between the 400-Hertz alternator and the aircraft shall provide power characteristics at the aircraft receptacle which meet MIL-STD-704A requirements for Category "B" equipment. Other limits which are necessary to meet specific conditions must be specified by the purchaser.
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