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BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, 300 CPM (13 FPM) OSCILLATION, -65 TO +160 °F, LINERS LESS THAN .015 INCH THICK

ACBG Plain Bearing Committee
  • Aerospace Standard
  • AS82819/1
  • Current
Published 2018-08-23 by SAE International in United States
No Abstract Available.
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Bearings, Plain, Self-Aligning, Self-Lubricating, 300 cpm Oscillation (13 fpm), -65 to +160 °F (-54 to +71 °C), Liners Less Than 0.015 inches

ACBG Plain Bearing Committee
  • Aerospace Standard
  • AS82819
  • Current
Published 2018-08-23 by SAE International in United States
This standard covers the requirements for spherical, self-aligning, self-lubricating, bearings which are for use in the ambient temperature range of -65 to +160 °F (-54 to +71 °C) at high cyclic speeds 300 cpm (13 fpm) for liners with a thickness less than 0.015 inch. The scope of this standard is to provide a liner system qualification procedure for helicopter sliding bearings defined and controlled by source control drawings. Once a liner system is qualified, the source-controlled bearings are further tested under application conditions. Under Department of Defense (DoD) Policies and Procedures, any qualification requirements and associated Qualified Products List (QPLs) are mandatory for DoD contracts. Any materials relating to QPLs have not been adopted by SAE and are not part of this SAE technical document.
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Bearings, Plain, Self-Aligning, Self-Lubricating, 1400 cpm (15 fpm), Oscillation, -65 to +160 °F (-54 to +71 °C)

ACBG Plain Bearing Committee
  • Aerospace Standard
  • AS83819
  • Current
Published 2018-08-23 by SAE International in United States
This standard covers the requirements for spherical, self-aligning, self-lubricating, bearings which are for use in the ambient temperature range of -65 to +160 °F (-54 to +71 °C) at high cyclic speeds 1400 cpm (15 fpm). The scope of this standard is to provide a liner system qualification procedure for helicopter sliding bearings defined and controlled by source control drawings. Once a liner system is qualified, the source-controlled bearings are further tested under application conditions. Under Department of Defense (DoD) Policies and Procedures, any qualification requirements and associated Qualified Products List (QPLs) are mandatory for DoD contracts. Any materials relating to QPLs have not been adopted by SAE and are not part of this SAE technical document.
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BEARINGS, PLAIN, SELF-ALIGNING, SELF-LUBRICATING, 1400 CPM (15 FPM) OSCILLATION, -65 TO +160 °F (-54 TO +71 °C)

ACBG Plain Bearing Committee
  • Aerospace Standard
  • AS83819/1
  • Current
Published 2018-08-23 by SAE International in United States
No Abstract Available.
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Plain Bearing Test Methods

ACBG Plain Bearing Committee
  • Aerospace Standard
  • ARP5448B
  • Current
Published 2018-08-23 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) establishes methods for testing airframe plain bearings. The purpose of ARP5448 and its associated slash sheets is to document test methods commonly used to evaluate airframe bearings. These test methods may be referenced in specifications, part standards, purchase orders, etc., when the test is deemed appropriate to the intended use of the bearing by the end user of the bearing. These test methods are not intended to encompass every conceivable requirement for an airframe bearing. The end user of the bearing must exercise engineering judgment to determine the most appropriate standard and/or nonstandard tests for the application.
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Plain Spherical Bearing Radial and Axial Clearance Measurement

ACBG Plain Bearing Committee
  • Aerospace Standard
  • ARP5448/8A
  • Current
Published 2018-08-23 by SAE International in United States
This test method provides a guidance for determining the total free play between the ball and outer ring of a spherical bearing when measured in both the radial and axial directions. Bearings covered by this test method include all plain spherical type bearings, both self-lubricated (lined) and metal-to-metal.
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Plain Bearing Bond Integrity - Peelable Woven Fabric PTFE Liners

ACBG Plain Bearing Committee
  • Aerospace Standard
  • ARP5448/4
  • Current
Published 2018-08-13 by SAE International in United States
This test method outlines a recommended procedure for performing bond integrity tests of bonded peelable woven fabric reinforced polytetrafluoroethylene (PTFE) liners, hereafter referred to within this document as "PTFE liner" or "liner". The data from these tests shall be used to determine if the product meets the "bond integrity" requirements of the applicable specifications.
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BUSHING, SLEEVE PLAIN, PRESS FIT, REAM TYPE

ACBG Plain Bearing Committee
  • Aerospace Standard
  • AS14237B
  • Current
Published 2018-05-16 by SAE International in United States
No Abstract Available.
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BEARING, PLAIN, SELF-LUBRICATING, SELF-ALIGNING, LOW SPEED, WIDE, GROOVED RACE, -65 TO +325 °F

ACBG Plain Bearing Committee
  • Aerospace Standard
  • AS14103F
  • Current
Published 2018-05-14 by SAE International in United States

SCOPE IS UNAVAILABLE.

BEARING, PLAIN, SELF-LUBRICATING, SELF-ALIGNING, LOW SPEED, WIDE, CHAMFERED RACE, -65 TO +325 °F

ACBG Plain Bearing Committee
  • Aerospace Standard
  • AS14102E
  • Current
Published 2018-05-14 by SAE International in United States
No Abstract Available.
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