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MH/T 6137.1-2025Testing method for performance of aviation turbine engine lubricating oils - Part 1: High temperature bearing deposition characteristics (English PDF)

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Issued by

Civil Aviation Administration of China

Level / Type

National · Recommended

Issue date

July 18, 2025

Implementation date

August 1, 2025

Scope

MH/T 6137.1-2025 (Testing method for performance of aviation turbine engine lubricating oils - Part 1: High temperature bearing deposition characteristics) is available as an English-translated PDF.

MH/T 6137.1-2025 — This standard specifies the test method for the deposition performance of aero-turbine engine lubricating oil (hereinafter referred to as "turbo lubricating oil") on engine bearings under specific temperature, pressure, flow rate, speed, and load test conditions.

It includes instruments and equipment, reagents and consumables, test preparation, test procedures, data processing, and reporting.

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Document preview — MH/T 6137.1-2025

National Standard of the People's Republic of China

ICS
75.100
Classification
E 34

Issued by: Civil Aviation Administration of China

Contents

  • What this standard covers1
  • Document data2

What this standard covers

This standard specifies the test method for the deposition performance of aero-turbine engine lubricating oil (hereinafter referred to as "turbo lubricating oil") on engine bearings under specific temperature, pressure, flow rate, speed, and load test conditions. It includes instruments and equipment, reagents and consumables, test preparation, test procedures, data processing, and reporting. This document applies to the testing of the high-temperature bearing deposition performance of turbo lubricating oil.

Document data

International classification (ICS): 75.100.

Chinese classification (CCS): E34.

Estimated length of the Chinese original: 24,253 words.

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This preview omits tables, figures, formulas and parts of the technical clauses. The complete document — 16 pages — is available in the English PDF.

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MH/T 6137.1-2025

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