Mobil Jet™ Oil 387

ExxonMobil aviation , Norway

Aircraft Type Gas Turbine Lubricant

Product Description

Mobil Jet Oil 387 has been developed to meet the performance requirements of both current and future, advanced gas turbine engines used in commercial and military service. Made from a specially prepared, ester base stock, Mobil Jet Oil 387 is fortified with a unique chemical additive package. The resulting lubricant has superior thermal and oxidation stability that resists deterioration and deposit formation. The physical properties of Mobil Jet Oil 387conform to required builder and military specifications.

 

Features and Benefits

Mobil Jet Oil 387 shows excellent performance controlling deposits typically experienced in both the liquid and vapor phases in bearing compartments, oil supply lines, and breather/scavenger lines. These properties have been confirmed in various laboratory tests, including the Corrosion-Oxidation Stability Test, Alcor Deposition Test, Vapor Phase Coker, Erdco High-Temperature Bearing Test, Ryder Gear, and the Mobil Thin Film Oxidation Test.

The closely controlled viscosity of Mobil Jet Oil 387 at -40°C (-40°F), and a pour point below -54°C (-65°F), ensure the good low-temperature fluidity which permits starting and lubrication at temperatures as low as -40°C. In extensive laboratory testing, Mobil Jet Oil 387 exhibits excellent bulk oil stability at temperatures greater than 225°C (437°F).

 

Features

Advantages and Potential Benefits

Long-duration fluorocarbon compatibility

Helps avoid premature or unscheduled engine repairs. Helps prevent leaks that can lead to air craft delays and cancellations.

Outstanding oil life characteristics, such as bulk oil stability, viscosity and TAN control

Helps minimize formation of sludge and carbon deposits which allows better engine efficiency and reduced engine repair costs as well potentially achieving longer oil drain intervals (in certain applications such as marine and land based turbines), effective lubrication at high operating temperatures

Very low vapor/mist and thin film deposition resistance

Helps control deposits in air vent tubes, bearingcompartments, and scavenge oil lines which will all result in reduced engine maintenance costs

Good low temperature fluidity

Permits start-up and ensures effective lubrication of critical components (such as APUs in ETOPS applications) at temperatures as low as -40 °F

 

Applications

Mobil Jet Oil 387 is approved against the new SAE AS5780 High Performance Capability (HPC) standard. This civil specification was developed to meet the growing performance and quality needs that commercial airlines seek, especially with the entrance of new, higher-output and lower consumption engines.

 

OEM in-house evaluation/approval programs are also underway. Once complete, Mobil Jet Oil 387 will be commercialized for use in aircraft gas turbine engines, including turbo-jet, turbo-fan, turbo-prop, and turbo-shaft (helicopter), in commercial and military service. In addition, it will be suitable for aircraft-type gas turbine engines in industrial and marine applications.

 

Mobil Jet Oil 387 is compatible with other synthetic gas turbine lubricants meeting U.S. Military Specification MIL-PRF-23699. Mixing with other products, however, could result in some loss of its superior performance features. The lubricant is completely compatible with all metals used in gas turbine construction, as well as with F Rubber (Viton A), H Rubber (Buna N), and other commonly used seal materials. Engine/OEM Evaluations

 

Mobil Jet Oil 387 has the following builder approvals: *

     •  General Electric Aviation

     •  Rolls Royce

     •  Pratt & Whitney

     •  Honeywell APUs

     •  UTC Aerospace Systems APUs, Generators and Starters

 

Mobil Jet Oil 387 has the following builder approvals  in progress  : *

     •  CFM International

     •  Engine Alliance

     •  International Aero Engines

     •  Honeywell turbine engines

 

* Specific engine or equipment approval must be verified with the builder

 

Specifications and Approvals

 

 

SAE AS 5780 HPC

MIL (US) MIL-PRF-23699 HTS

 

Properties and Specifications

Property

 

Autogenous-ignition temperature test, deg.C, 30 CFR 35.20

405

Change in Kinematic Viscosity, 72 h @ -40 C, %, ASTM D2532

0.1

Elastomer Compatibility, AMS-3217/4 (72hrs @204C), % swell, FTMS 791-3604

15

Elastomer Compatibility,AMS-3217/1(72hr @70C), % swell, FTMS 791-3604

15

Evaporation Loss, 6.5 h, 204 C, mass%, ASTM D972(mod)

4

Fire Point, °C, ASTM D92

292

Flash Point, Cleveland Open Cup, °C, ASTM D92

278

Foam, Sequence I, Tendency, ml, ASTM D892

10

Foam, Sequence II, Tendency, ml, ASTM D892

10

Foam, Sequence III, Tendency, ml, ASTM D892

10

Kinematic Viscosity @ 100 C, mm2/s, ASTM D445

5.2

Kinematic Viscosity @ 40 C, mm2/s, ASTM D445

25.9

Kinematic Viscosity @ -40 C, mm2/s, ASTM D445

10140

Pour Point, °C, ASTM D5950

-57

Ryder Gear Load Carrying, % vs ref., FTMS 791-6508

2806

Specific Gravity, 15 C/15 C, ASTM D4052

0.999

Total Acid Number, mgKOH/g, ARP 5088

0.03

 

Health and safety

Health and Safety recommendations for this product can be found on the Material Safety Data Sheet (MSDS) @ http://www.msds.exxonmobil.com/psims/psims.aspx

All trademarks used herein are trademarks or registered trademarks of Exxon Mobil Corporation or one of its subsidiaries unless indicated otherwise.

12-2024

Exxon Mobil Corporation
22777 Springwoods Village Parkway
Spring TX 77389
For additional technical information or to identify the nearest U.S. ExxonMobil supply source, call +1 800 662-4525.
http://www.exxonmobil.com

Due to continual product research and development, the information contained herein is subject to change without notification.  Typical Properties may vary slightly.