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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

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

1962-01-01
HISTORICAL
ARP680A
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 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.
Standard

UNIVERSAL TURNOVER BUILD-UP STAND FOR SMALL PROPULSION UNITS REQUIRING VERTICAL ASSEMBLY

1968-05-15
HISTORICAL
ARP863
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 asterik on the attached drawings), attachment pad configuration, and gearbox and caster specifications.
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

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

COVER SHIPPING FLEXIBLE (NONREUSEABLE)

1997-04-01
CURRENT
ARP4732
This SAE Aerospace Recommended Practice (ARP) defines and establishes design, construction, and performance requirements for a flexible nonreuseable waterproof cover for shipment of aircraft engines, major components, and other military and commercial items not intended for storage; items to be removed within fourteen (14) days.
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

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

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.
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