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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.
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

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.
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