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NPFC - MIL-PRF-83861

FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE

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Organization: NPFC
Publication Date: 14 August 2013
Status: active
Page Count: 21
scope:

This specification covers disposable hydraulic line filter elements that retain all particles larger than 5 or 15 microns. For use, the element is inserted in a canister prior to use in a hydraulic system, and is intended for use with hydraulic fluids conforming to MIL-PRF-5606, MIL-PRF-83282, and MIL-PRF-87257.

intended Use:

The filter elements covered by this specification are intended for use in aircraft and missile hydraulic systems operating with hydraulic fluid conforming to MIL-PRF- 5606 (for guidance... View More

Document History

MIL-PRF-83861
October 11, 2019
Filter Elements, Disposable, Fluid Pressure, Hydraulic Line, 5 and 15 Micron Absolute
A description is not available for this item.
MIL-PRF-83861
August 14, 2013
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE
The filter elements covered by this specification are intended for use in aircraft and missile hydraulic systems operating with hydraulic fluid conforming to MIL-PRF- 5606 (for guidance if...
MIL-PRF-83861
January 31, 1998
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE
The filter elements covered by this specification are intended for use in aircraft and missile hydraulic systems operating with hydraulic fluid conforming to MIL-H-5606, MIL-H-83282, and MIL-H-87257...
MIL-F-83861
May 15, 1991
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE
A description is not available for this item.
MIL-F-83861
July 10, 1986
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE
This specification covers hydraulic line filter elements which retain all particles larger than five or fifteen microns as specified and are suitable for use as specified in 6.1, and the applicable...
MIL-F-83861A (2)
April 23, 1981
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE
A description is not available for this item.
MIL-F-83861
April 9, 1976
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE
A description is not available for this item.
MIL-F-83861
April 26, 1974
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE
A description is not available for this item.
MIL-F-83861
May 2, 1972
FILTER ELEMENTS, DISPOSABLE, FLUID PRESSURE, HYDRAULIC LINE, 5 AND 15 MICRON ABSOLUTE
A description is not available for this item.
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References

This document references:
ASME B46.1 - Surface Texture (Surface Roughness, Waviness, and Lay)
Published by ASME on January 1, 2019
This Standard is concerned with the geometric irregularities of surfaces. It defines surface texture and its constituents: roughness, waviness, and lay. It also defines parameters for specifying...
This document references:
ASQ Z1.4 - SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES
Published by ASQ on January 1, 2003
PURPOSE. This publication establishes sampling plans and procedures for inspection by attributes. When specified by the responsible authority, this publication shall be referenced in the...
This document references:
ISO 16889 - Hydraulic fluid power - Filters - Multi-pass method for evaluating filtration performance of a filter element AMENDMENT 1
Published by ISO on November 1, 2018
A description is not available for this item.
This document references:
RTCA DO-160 - Environmental Conditions and Test Procedures for Airborne Equipment
Published by RTCA on December 16, 2014
FOREWORD This report was prepared by RTCA Special Committee 135 (SC-135) and approved by the RTCA Program Management Committee (PMC) on December 16, 2014. RTCA, Incorporated is a not-for-profit...
This document references:
MIL-PRF-5606 - HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE
Published by NPFC on March 5, 2018
This specification describes the characteristics and provides the requirements for a petroleum base hydraulic fluid for use in the -54 °C to +135 °C temperature range . This fluid is identified by...
This document is referenced by:
DEF STAN 00-970: PART 0 - Certification Specifications for Airworthiness Part 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
Published by MODUK on March 14, 2021
Part 0 provides guidance and content information, together with definitions of terms used throughout this Standard.
This document is referenced by:
DEF STAN 00-970: PART 5 - Certification Specifications for Airworthiness Part 5: LARGE TYPE AIR SYSTEMS
Published by MODUK on March 14, 2021
Where CS 25 makes reference to ‘the Agency’, this should be considered to mean the certifying authority.
This document is referenced by:
DEF STAN 00-970: PT7 SEC1 - Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Section 1: Introduction
Published by MODUK on July 13, 2015
This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Rotorcraft Aircraft for UK Military operation.
This document is referenced by:
DEF STAN 00-970: PART 11 - Certification Specifications for Airworthiness Part 11: ENGINES
Published by MODUK on August 28, 2020
Unless otherwise specified in this Standard, the certification requirements of EASA CS-E (amendment 6) including related AMC and Appendices shall be applied. Additionally, the requirements of CS-E...
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