Search Results

Standard

Universal Turnover Build-Up Stand for Small Propulsion Units Requiring Vertical Assembly

2012-12-05

CURRENT

ARP863B

This recommended practice covers a stand that may be used for assembly, disassembly, and maintenance. The stand incorporates the following design criteria: complete interchangeability of any and all components, collapsible frame construction, envelope dimensions (marked with an asterisk on the attached drawings), attachment pad configuration, and gearbox and caster specifications.

Standard

Universal Turnover Build-Up Stand Series for Propulsion Units and/or Components

2005-10-28

CURRENT

ARP680C

This recommended practice covers a series of stands that may be used for assembly, disassembly and maintenance; incorporating the following design criteria: a collapsible frame construction, envelope dimensions, attachment shear pad configuration and gear box and caster specifications.

Standard

Universal Leak Detector

2005-10-28

CURRENT

ARP726A

This recommended practice covers a self-contained detection system which is capable of pressurizing a closed system up to 70 psig with halogen (tracer) gas and up to 3500 psig with nitrogen.

Standard

ULD for Aircraft Transportation of Horses

2017-09-11

CURRENT

ARP1621C

This SAE Aerospace Recommended Practice (ARP) defines minimum requirements for an aircraft transport ULD to transport horses properly and safely by air, to protect the horse(s) from injuries, and to protect the aircraft from corrosion created by waste spill. The ULD is designed to accommodate one horse or several. There are two types of ULDs for aircraft transportation of horses:

Standard

Tie Down, Cargo, Aircraft, Nylon Web Net

2006-06-05

CURRENT

AS26780A

This specification covers two types of aircraft cargo tie downs, each having a capacity of 10,000 pounds.

Standard

Tie Down, Cargo, Aircraft, Nylon Web Net

2000-11-01

HISTORICAL

AS26780

This specification covers two types of aircraft cargo tie downs, each having a capacity of 10,000 pounds.

Standard

TRACK AND STUD FITTING FOR CARGO TRANSPORT AIRCRAFT, STANDARD DIMENSIONS FOR

2005-08-09

HISTORICAL

AS33601

Standard

Stands, Shipping and Storage, Aircraft Engines, Reusable

2017-10-25

WIP

ARP4898A

This SAE Aerospace Recommended Practice (ARP) recommends design and test criteria for reusable shipping and storage stands for aircraft engines. An optional hard cover (enclosure) is also specified.

Standard

Standardization of Drive End of Hydraulic or Geared Torque Wrenches for Use to an Upper Limit of 500,000 inch pounds

2012-12-05

CURRENT

ARP1135B

This SAE Aerospace Recommended Practice (ARP) covers the dimensions of an inside splined driver-wrench adapter, envelope of the housing-wrench reaction, the mechanical method of adapting the driver-wrench adapter to the wrench adapter driven end, and the housing-wrench reaction to the holder-counter torque.

Standard

Shipping Caps, Covers and Plugs

2017-11-06

CURRENT

ARP5862

The primary purpose of the shipping closure is to protect the aircraft parts or system from damage and foreign material ingress/egress (e.g., dust, dirt or other contaminants) during transport and storage. Shipping closures are not airworthy items. Therefore, their usage is defined as preventative for the parts to be protected as opposed to operational. Military and commercial customer requirements for the prevention of damage or contamination to stored parts are generally limited to the generic instructions “all openings should be sufficiently covered to prevent the entrance of dust, dirt, moisture or other foreign contaminants”. This recommended practice outlines basic minimum parameters for suggested item construction and usage. Additionally, this recommended practice provides instruction on how to apply these closures to various openings.

Standard

Nomenclature Guide for Propulsion Systems Support Equipment

2012-12-05

CURRENT

ARP480C

This document lists recommended noun titles for drawings of support equipment and provides definitions for each. The use of secondary modifiers to distinguish a part from similar parts is also covered.

Standard

METHODOLOGY OF CALCULATING AIRCRAFT CARGO VOLUMES

1995-03-01

HISTORICAL

AS1825A

The scope of this SAE Aerospace Standard (AS) shall cover the methodology of defining and determining the "internal volumes" of both the main deck and lower deck aircraft cargo compartments. The minimum required clearance between the compartment envelope and the unit load devices (ULDs) shall also be stated in order to provide the maximum ULD external contour and the methodology to define the ULD internal volumes.

Standard

Interline Air Cargo Pallet Nets

2023-01-13

CURRENT

AS1492C

This document establishes dimensional, structural, and environmental requirements for Type II/2 interline pallet nets. Type II/2 covers NAS3610/AS36100 code sizes.

Standard

Interline Air Cargo Pallet Nets

2012-09-05

HISTORICAL

AS1492B

This document establishes dimensional, structural, and environmental requirements for two types of interline pallet nets. Type II covers NAS 3610 code sizes and Type III covers other sizes not currently included in NAS 3610.

Standard

INTERLINE AIR CARGO PALLET NETS

1982-03-01

HISTORICAL

AS1492

This specification establishes dimensional, structural and environmental requirements for interline pallet nets.

Standard

INTERLINE AIR CARGO PALLET NETS

1985-01-01

HISTORICAL

AS1492A

This specification establishes dimensional, structural and environmental requirements for two types of interline pallet nets. Type II covers NAS 3610 code sizes and Type III covers other sizes not currently included in NAS 3610.

Standard

INSULATED AIR CARGO CONTAINER

1992-12-01

HISTORICAL

ARP1523

Perishable cargoes, e.g., dairy produce, fruit, vegetables, flowers, frozen foods, meat, fish, etc., require maintenance of specific temperature ranges during air related door-to-door transportation.

Standard

GENERAL REQUIREMENTS FOR POWERED DRIVE UNITS IN AIRCRAFT CARGO SYSTEMS

2008-06-22

HISTORICAL

AIR4165

This Aerospace Information Report (AIR) serves a dual purpose. It enables the user (aircraft manufacturer/airline) to do the following: a To make a positive decision for the installation of a powered drive system in the cargo loading system during the definition of the aircraft on-board cargo loading system to be developed/procured. b To provide the user with general requirements to be taken into consideration during the preparation of component specifications for powered drive units (PDUs) to be used in aircraft cargo systems. This is to provide the author of such a component specification with a selection of criteria in order to obtain an optimum component suitable for the users’ applications.

Standard

Fittings, Cargo Tiedown, Aircraft

2006-04-27

HISTORICAL

AS7092A

This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.

Standard

Fittings, Cargo Tiedown, Aircraft

2012-10-15

CURRENT

AS7092B

This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.