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Viewing 1 to 30 of 3483
2014-12-10
WIP Standard
ARP4050A
Characteristics of vertical hard-bearing balancing machines are described which make such machines suitable for gas turbine rotor balancing.

This document specifies the following: a. general dimensions and capacities; b. performance requirements; c. balancing speed ranges; d. drive power requirements; e. balancing machine spindle flange dimensions; and f. test procedures.

Proving rotors and associated test masses required for the performance tests are described in ARP4162.

Test procedures are described in detail and test log samples along with a polar diagram for evaluating the test results are furnished.

The predecessor document ARP588, ISO 2953, and the available technology of hard-bearing balancing machines have been considered in the preparation of this document.

This document was developed for hard-bearing balancing machines but may also be used for existing soft-bearing balancing machines.

2014-12-10
WIP Standard
AS7460B
This procurement specification covers aircraft-quality bolts and screws made of 6.0Al 4.0V titanium alloy and of 160 ksi tensile strength at room temperature. Primarily for aerospace propulsion system applications where high strength, light weight fasteners are required for use up to approximately 600 °F.
2014-12-07
WIP Standard
AS9808A
No scope available.
2014-12-06
WIP Standard
AS7220A
This procurement specification covers rivets fabricated from an aluminum alloy designated as 1100-H14, strain hardened. Primarily for joining aluminum parts where a low shear strength is adequate.
2014-12-06
WIP Standard
AS7228A
This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion resistant steel of the type identified under the Unified Numbering System as UNS S30200.

Primarily for joining corrosion resistant steel parts requiring corrosion, heat, and oxidation resistance up to approximately 800 degrees F but not requiring high shear strength.

2014-12-06
WIP Standard
AS7454B
This procurement specification covers aircraft quality bolts and screws made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675. AS7454 ~ 135 000 psi ultimate tensile strength at room temperture. AS7454-1 ~ 135 000 psi ultimate tensile strength at room temperture, nickel-cadmium plated.

Primarily for aerospace propulsion system applications where good strength at temperatures up to approximately 900 °F is required and the part is protected against corrosion.

2014-12-06
WIP Standard
AS7455B
This procurement specification covers aircraft quality bolts and screws made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675. The following specification designations and their properities are covered: AS7455 ~ 140 000 to 195 000 psi ultimate tensile strength at room temperture; AS7455-1 ~ 140 000 to 195 000 psi ultimate tensile strength at room temperature, nickel-cadmium plated.

Primarily for aerospace propulsion system applications where high strength at temperatures up to approximately 900 °F is required and the part is protected against corrosion.

2014-12-06
WIP Standard
AS9589A
No scope available.
2014-12-06
WIP Standard
AS9806A
No scope available.
2014-12-06
WIP Standard
AS9788A
No scope available.
2014-12-05
WIP Standard
AS3397A
No scope available.
2014-12-05
WIP Standard
AS4723A
This procurement specification covers inserts made from A286 alloy of the type identified under the Unified Numbering System as UNS S66286, solid film lubricated with a plastic self locking device, integrated locking keys to positively secure the insert against rotation when properly installed in threaded holes.
2014-12-05
WIP Standard
AS20253B
Scope is unavailable.
2014-11-25
Standard
ARP1953B
To describe general guidelines for achieving selected levels of cleanliness in gas turbine engine fuel system components and to describe laboratory methods for measuring and reporting the contamination level of the wetted portion of fuel system components. As in SAE J1227 (covering hydraulic components) this practice includes guidelines for levels of acceptance but does not attempt to set those levels.
2014-11-20
Standard
ARP1827C
This SAE Aerospace Recommended Practice (ARP) delineates two complementary filter element performance ratings: (1) dirt capacity, and (2) filtration efficiency, and corresponding test procedures. It is intended for non-cleanable (disposable), fine fuel filter elements used in aviation gas turbine engine fuel systems.
Viewing 1 to 30 of 3483

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