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Standard

Icing Tunnel Tests for Thermal Ice Protection Systems
2010-05-11
WIP
AIR6440
This document is intended to provide guidance for conducting icing tunnel tests for assessment and design of thermal anti-ice systems for wing, stabilizers and engine inlets (considering both hot air and electrical power as a heat source).
Standard

Ice Shape Test Matrix Development for Unprotected Surfaces
2010-10-19
WIP
ARP6455
This document is intended to provide guidance for development of a test matrix for generation of ice shapes on unprotected surfaces. It introduces the reader to scaling of flight conditions to capabilities of typical icing tunnels and provides an example of the process.
Standard

Thermal Anti-Icing Equipment, Wing and Empennage
2001-07-01
CURRENT
AS18607A
This specification covers the general requirements for the design, installation, and performance of thermal anti-icing equipment for the wings and empennage surfaces in aircraft.
Standard

THERMAL ANTI-ICING EQUIPMENT, WING AND EMPENNAGE
1997-08-01
HISTORICAL
AS18607
This specification covers the general requirements for the design, installation, and performance of thermal anti-icing equipment for the wings and empennage surfaces in aircraft.
Standard

Droplet Sizing Instrumentation Used in Icing Facilities
2013-04-23
CURRENT
AIR4906
A review of droplet sizing instruments used for icing research is presented. These instruments include the Forward Scattering Spectrometer Probe, the Optical Array Probe, the Phase Doppler Particle Analyzer, the Malvern Particle Size Analyzer, the oil slide technique, and the rotating multicylinder. The report focuses on the theory of operation of these instruments and practical considerations when using them in icing facilities.
Standard

Aircraft Inflight Icing Terminology
2002-09-17
HISTORICAL
AIR5504
This SAE Aerospace Information Report (AIR) provides definitions for terms commonly used in aircraft inflight icing system design and analysis, research, and operations. Some general thermodynamic terms are included that are frequently used in icing analysis, but this document is not meant to be an inclusive list of such terms.
Standard

Aircraft Inflight Icing Terminology
2009-11-24
CURRENT
AIR5504A
This SAE Aerospace Information Report (AIR) provides definitions for terms commonly used in aircraft inflight icing system design and analysis, research, and operations. Some general thermodynamic terms are included that are frequently used in icing analysis, but this document is not meant to be an inclusive list of such terms. The purpose of this document is to provide an assemblage of definitions for terms commonly used in aircraft icing. Over time, the field of aircraft icing has evolved a set of terms that are sometimes used in different ways and have different meanings. This document is a compendium of icing terms and their associated definitions. The SAE does not endorse or recommend any particular definition given in this report.
Standard

Aircraft Inflight Icing Terminology
2018-09-27
WIP
ARP5624A
This SAE Aerospace Recommended Practice (ARP) provides recommended definitions for terms commonly used in aircraft inflight icing system design and analysis, research, and operations. Some general thermodynamic terms are included that are frequently used in icing analysis, but this document is not meant to be an inclusive list of such terms.
Standard

Aircraft Inflight Icing Terminology
2013-04-23
CURRENT
ARP5624
This SAE Aerospace Recommended Practice (ARP) provides recommended definitions for terms commonly used in aircraft inflight icing system design and analysis, research, and operations. Some general thermodynamic terms are included that are frequently used in icing analysis, but this document is not meant to be an inclusive list of such terms.
Standard

ICING TECHNOLOGY BIBLIOGRAPHY
1996-07-01
HISTORICAL
AIR4015A
This Icing Technology Bibliography is a compendium of references from the open literature, including both national and foreign sources. Due to the generality of the subject, and the difficulty of fully investigating every available source, the present Bibliography is not intended to be complete. However, it will be updated every 18 months by the SAE AC-9C Aircraft Icing Technology Subcommittee. Any suggestions in terms of additional references, sources, and corrections should be referred to the Icing Technology Bibliography Panel of the SAE AC-9C Aircraft Icing Technology Subcommittee.
Standard

Icing Technology Bibliography
2013-03-15
CURRENT
AIR4015D
This Icing Technology Bibliography is a compendium of references from the open literature that were published prior to the original 1987 issuance of the AIR, including both national and foreign sources. Due to the generality of the subject, and the difficulty of fully investigating every available source, the Bibliography in this document is not intended to be complete.
Standard

Icing Technology Bibliography
2007-04-11
HISTORICAL
AIR4015B
This Icing Technology Bibliography is a compendium of references from the open literature that were published prior to the original 1987 issuance of the AIR, including both national and foreign sources. Due to the generality of the subject, and the difficulty of fully investigating every available source, the Bibliography in this document is not intended to be complete.
Standard

Airborne Icing Tankers
2019-06-17
CURRENT
ARP5904
This SAE Aerospace Recommended Practice (ARP) document establishes criteria and recommended practices for the use of airborne icing tankers to aid in design and certification of aircraft ice protection systems and components. Several icing tankers are described, along with their capabilities and suggested use. Sample data for these tanker spray systems are included, shown with 14 CFR Parts 25 and 29, Appendix C icing envelopes for continuous maximum and intermittent maximum icing conditions. (Note: In the remainder of this document, the phrase “Appendix C icing envelopes” will be used for brevity.) This ARP is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances.
Standard

Deicing System, Pneumatic Boot, Aircraft, General Specification for
2001-07-01
CURRENT
AS8804A
This specification covers the general requirements for pneumatic deicing systems for wings, empennages, radomes, radio masts, air induction system entrance cones, and ducts of aircraft. Deicing boots shall be of one type, operating at 15 to 22 psig pressure.
Standard

Deicing System, Pneumatic Boot, Aircraft, General Specification For
1997-09-01
HISTORICAL
AS8804
This specification covers the general requirements for pneumatic deicing systems for wings, empennages, radomes, radio masts, air induction system entrance cones, and ducts of aircraft. Deicing boots shall be of one type, operating at 15 to 22 psig pressure.
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