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SAE AS5798

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Aerospace Size Standard for Oversize O-rings

Available format(s)

Hardcopy , PDF

Superseded date

05-12-2019

Superseded by

SAE AS5798A

Language(s)

English

Published date

22-11-2013

€110.91
Excluding VAT

1. SCOPE
2. REFERENCES
3. REQUIREMENTS
4. NOTES

Applies to military and commercial aircraft. It specifies the dimensions, tolerances and size codes (dash numbers) for use in glands per MIL-G-5514 where squeeze at low temperature is often insufficient to provide a leak-tight seal.

DocumentType
Standard
Pages
15
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

This SAE Aerospace Standard (AS) is applicable to military and commercial aircraft. It specifies the dimensions, tolerances and size codes (dash numbers) for use in glands per MIL-G-5514 where squeeze at low temperature is often insufficient to provide a leak-tight seal. The dimensions and tolerances specified in this standard are suitable for any elastomeric material.This standard should not be used as a part standard, therefore no part numbers like AS5798-001X shall be created.Each dash number, which should be appended to an appropriate drawing or standard number, identifies one size O-ring only. An AS5798 sized O-ring is intended to replace an AS568 sized O-ring of the same dash number. An X suffix is part of the dash number to signify oversize.Temperature limitations of 275 °F (135 °C) and coefficient of thermal expansion of 9.0 × 102x unit length per °F (1.6 × 102x unit length per °C) were used for swell calculations. Applications that exceed these values should be evaluated for excessive gland fill.

SAE AS4716B Gland Design, O-ring and Other Elastomeric Seals
MS27595 Revision E:2006 RETAINER, PACKING BACKUP, CONTINUOUS RING, POLYTETRAFLUOROETHYLENE
SAE AS568D Aerospace Size Standard for O-rings
MIL-G-5514 Revision G:1993 GLAND DESIGN, PACKINGS, HYDRAULIC GENERAL REQUIREMENTS FOR

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