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Standard

A MEANS OF TESTING TURBOJET ENGINE STARTER PERFORMANCE
1963-11-01
HISTORICAL
ARP715
This Recommended Practice covers a means of determining the performance acceptability of new production or overhauled starters that will be used for cranking turbine engines and is intended for use where torque measuring equipment is not available or desirable. This method determines acceptability of the overall performance of the starter on a flywheel test stand, rather than the performance at specific speed conditions. It allows a slight variation of output torque outside specified limits, as long as the overall performance is up to standard.
Standard

AEROSPACE STANDARD, GLAND DESIGN, O-RING AND OTHER ELASTOMERIC SEALS
1993-06-11
HISTORICAL
AS4716
This SAE Aerospace Standard provides standardized gland (groove) design criteria and dimensions for elastomeric seal glands for static and dynamic applications. The glands have been specifically designed for applications using SAE AS568 size O-rings at pressures exceeding 1500 psi utilizing one or two anti-extrusion (backup) rings and applications at pressures under 1500 psi without backup rings. The glands have been sized to provide sufficient squeeze for effective sealing while at the same time limiting squeeze to allow satisfactory operation in dynamic applications. While specifically designed for standard size O-rings, these glands are also to be used with other elastomeric seals.
Standard

AIRCRAFT CABIN PRESSURIZATION CONTROL CRITERIA
1993-06-01
HISTORICAL
ARP1270
These recommendations cover the basic criteria for the design of aircraft cabin pressurization control systems as follows: (1) To ensure aircraft safety. (2) Physiology and limits which govern maximum permissible pressure time relations as related to aircraft passenger comfort. (3) General pressurization control system performance requirements designed to satisfy (2). (4) Technical considerations relevant to satisfying (3).
Standard

AIRCRAFT DEICING VEHICLE - SELF-PROPELLED, LARGE CAPACITY
1992-12-01
HISTORICAL
ARP1971
This specification covers requirements for a self-propelled, boom type aerial device, equipped with an aircraft deicing fluid spraying system. The unit shall be highly maneuverable for deicing all exterior surfaces of wide-body and intermediate size aircraft, e.g., B-747 and B-737. The vehicle will also be used for aircraft maintenance and inspection. The vehicle shall be suitable for day and night operations.
Standard

AIRCRAFT DEICING VEHICLE SELF-PROPELLED, SMALL CAPACITY
1987-03-01
HISTORICAL
ARP4047
This aerospace recommended practice covers requirements for a self-propelled, boom type aerial device, equipped with an aircraft deicing fluid spraying system. The unit shall be highly maneuverable for deicing all exterior surfaces of intermediate size aircraft, e.g. DC-9, B-727 and B-737. The vehicle will also be used for aircraft maintenance and inspection. The vehicle shall be suitable for day and night operations.
Standard

AIRCRAFT DEICING/ANTI-ICING METHODS WITH FLUIDS
1996-10-01
HISTORICAL
ARP4737A
This document establishes the minimum criteria for ground based aircraft deicing/anti-icing with fluids to ensure the safe operation of aircraft during icing conditions. This document does not specify requirements for particular airplane models.
Standard

AIRCRAFT DEICING/ANTI-ICING METHODS WITH FLUIDS
1997-03-01
HISTORICAL
ARP4737B
This document establishes the minimum criteria for ground based aircraft deicing/anti-icing with fluids to ensure the safe operation of aircraft during icing conditions. This document does not specify requirements for particular airplane models.
Standard

AIRCRAFT DEICING/ANTI-ICING METHODS WITH FLUIDS, FOR LARGE TRANSPORT AIRCRAFT
1992-10-01
HISTORICAL
ARP4737
This document provides information to assist in the preparation of particular airline aircraft ground deicing/anti-icing procedures and to ensure safe operation of large transport aircraft during adverse conditions conducive to aircraft icing on the ground, in accordance with aircraft manufacturers’ recommendations.
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