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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

Shipping Caps, Covers and Plugs

2009-07-27
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

Aircraft Engine Transport Devices

2007-02-21
CURRENT
ARP1840B
The tests are static in nature to minimize complexity and cost of required testing facilities. As far as practical, applied static loads should take into account the combined static and dynamic loads anticipated in service.
Standard

TERMINOLOGY GUIDE FOR AIRCRAFT GAS TURBINE ENGINES

2002-07-23
HISTORICAL
AS509
This Aeronautical Standard covers terms frequently applied to aircraft gas turbine engines and their operation but does not include names of particular parts, the latter being covered by AS 341, Drawing Title Rules and Nomenclature for Aircraft Engine Parts.
Standard

Drum, Metal-Shipping and Storage

2001-03-01
CURRENT
AS6054
This specification covers new cylindrical drums to be used as exterior shipping containers (see 6.1).
Standard

Aircraft Engine Transport Devices

2000-01-01
HISTORICAL
ARP1840A
The tests are static in nature to minimize complexity and cost of required testing facilities. As far as practical, applied static loads should take into account the combined static and dynamic loads anticipated in service.
Standard

Containers, Shipping and Storage, Reusable

1999-12-01
HISTORICAL
ARP1967A
This SAE Aerospace Recommended Practice (ARP) recommends design and test criteria for reusable shipping and storage containers for aircraft engines and modules, weapon systems and components, etc. The containers are to provide water-vaporproof and physical protection.
Standard

Indicator, Humidity, Plug, Color Change

1998-02-01
CURRENT
AS26860
This specification establishes requirements for externally mounted color change humidity indicators for determining relative humidity within rigid containers and flexible moisture-vapor-proof envelopes or bags.
Standard

Universal Leak Detector

1997-12-01
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

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

1997-12-01
HISTORICAL
ARP863A
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

AIRCRAFT ENGINE TRANSPORT DEVICES

1986-01-01
HISTORICAL
ARP1840
The tests are static in nature to minimize complexity and cost of required testing facilities. As far as practical, applied static loads should take into account the combined static and dynamic loads anticipated in service.
Standard

UNIVERSAL TURNOVER BUILD-UP STAND SERIES FOR PROPULSION UNITS AND/OR COMPONENTS

1968-10-01
HISTORICAL
ARP680B
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.
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