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Standard

400 Hz CONNECTION AIRCRAFT ELECTRICAL MAINTENANCE PROCEDURES

1994-12-01
HISTORICAL
AIR4365
This SAE Aerospace Information Report (AIR) describes field-level procedures to determine if 400 Hz electrical connections for external power may have been subjected to excessive wear, which may result in inadequate disengagement forces.
Standard

400 Hz Connection Aircraft Electrical Maintenance Procedures

2008-03-28
HISTORICAL
AIR4365A
This SAE Aerospace Information Report (AIR) describes field-level procedures to determine if 400 Hz electrical connections for external power may have been subjected to excessive wear, which may result in inadequate disengagement forces.
Standard

400-CYCLE GROUND POWER UNIT PROVISIONS FOR AIRCRAFT ELECTRICAL SYSTEM PROTECTION

2002-12-16
CURRENT
ARP760
This SAE Recommended Practice which defines the terms and tabulates the limits of the characteristics for various protective devices used in conjunction with 400-cycle ground power for civil aircraft is intended to assist the airlines in standardizing on 400-cycle protective systems. The limits found to be acceptable in the civil aircraft industry are presented.
Standard

AIRCRAFT MAINTENANCE JACKS - GENERAL REQUIREMENTS

1994-07-01
HISTORICAL
AS4775
This document covers the general requirements for hydraulic jacks as used on commercial aircraft. It can be applied to tripod, unipod, and axle jacks which may be used on open ramp areas as well as in the aircraft hanger.
Standard

Aircraft Cargo Conveyor

2023-03-29
WIP
ARP1836D
This SAE Aerospace Recommended Practice (ARP) outlines the functional and design requirements for a b self-propelled belt conveyor for handling baggage and cargo at aircraft bulk cargo holds. Additional considerations and requirements may legally apply in other countries. As an example, for operation in Europe (E.U. and E.F.T.A.), the applicable EN standards shall be complied with.
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 Support Equipment - Wind Stability Determination

2012-10-15
HISTORICAL
ARP1328B
This SAE Aerospace Recommended Practice (ARP) is intended to recommend: a uniform criteria for determination of wind loads that aircraft ground support equipment can encounter and yet allow personnel to work safely, b uniform systems for maintaining stability (i.e., stabilizers, outriggers, spring lockout devices), c standardization of specific types of interlock systems and actuation systems, d a standard formula with its associated design criteria for calculating the steady-state wind stability (i.e., tip point) for aircraft ground support equipment, e a standard method for testing these systems.
Standard

Aircraft Ground Support Equipment - Wind Stability Determination

2017-05-04
HISTORICAL
ARP1328C
This SAE Aerospace Recommended Practice (ARP) is intended to recommend: a uniform criteria for determination of wind loads that aircraft ground support equipment can encounter and yet allow personnel to work safely, b uniform systems for maintaining stability (i.e., stabilizers, outriggers, spring lockout devices), c standardization of specific types of interlock systems and actuation systems, d a standard formula with its associated design criteria for calculating the steady-state wind stability (i.e., tip point) for aircraft ground support equipment, e a standard method for testing these systems.
Standard

Aircraft Ground Support Equipment – General Requirements

2024-04-26
WIP
ARP1247F
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 requirement for maintenance and operation of Preconditioned Air units (PCA) and Passenger Boarding Bridge (PBB) supplying air to the cabin

2022-07-11
WIP
ARP6986
The provisions of this standard cover minimum performance requirements and design parameters for Preconditioned Air units (PCA) devices supplying air the aircraft cabin. It identifies the need for interim and future performance improvement for ground equipment delivery systems, to meet industry requirement for reducing airborne compounds or particulates (“source types”) in aircraft cabin and flight deck.
Standard

Aircraft Maintenance Jacks - General Requirements

2011-01-14
HISTORICAL
AS4775A
This document covers the general requirements for hydraulic aircraft jacks. It can be applied to tripod, unipod, and axle jacks that may be used on open ramp areas as well as in the aircraft hanger. Throughout this Aerospace Standard, the minimum essential criteria are identified by the key word “shall”. Recommended criteria are identified by use of the key word “should”. Deviation from recommended criteria should only occur after careful consideration and thorough service evaluation have shown alternate methods to provide an equivalent level of safety. The term “vertical load” throughout this Aerospace Standard is defined as the force imposed on the aircraft jack at the airframe jack point.
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 Tow Bar

2021-04-08
CURRENT
ARP1915E
This SAE Aerospace Recommended Practice (ARP) specifies dimensional and physical requirements of tow bar connections to tractor and aircraft (see Figure 1). It is applicable to all types of commercial transport category aircraft tow bar. The purpose of this SAE Aerospace Recommended Practice (ARP) is to standardize tow bar attachments to airplane and tractor according to the mass category of the towed aircraft, so that one tow bar head with different shear levels can be used for all aircraft that are within the same mass category and are manufactured in compliance with AS1614 or ISO 8267.
Standard

Aircraft Towbar

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