Mobil Jet™ Oil II
Mobil Jet™ Oil II was the first standard Type II oil on the market. With more than five decades of flight experience, it has accrued over 5 billion hours of on-wing performance.
This legendary, hassle-free, second-generation oil helps keep engines clean and operating at peak efficiency. Laboratory tests and engine inspections confirm it can handle extreme speeds, temperatures (up to 204 degrees Celsius/400 F) and stresses without breaking down.
Reasons to trust Mobil Jet Oil II
- It offers excellent deposit control, helping maintain engine cleanliness and reducing maintenance costs
- Provides superb elastomer compatibility, helping operators maximize component life and minimize oil consumption
- Offers exceptional wear performance, helping reduce component replacement costs and extend engine gear and bearing life
- Provides exceptional low-temperature fluidity and outstanding protection at high speeds
- It carries an extensive range of approvals, giving operators increased levels of flexibility
Product information
Data sheets
Technical Resources
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Using FIFO Inventory Method | ExxonMobil™ aviationLearn what grease compatibility is, and how it impacts grease conversion and performance.
Technical topics
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Port Allen plant begins production of Mobil Jet Oil | ExxonMobil™ aviationThe Port Allen aviation lubricants plant has achieved full production for the entire line of Mobil Jet™ engine lubricants. The state-of-the-art facility is part of a $200 million ExxonMobil investment in the Baton Rouge area.
Aviation News, Article
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jet engine oil system part 1 | ExxonMobil aviationInternational air regulations require that each engine is equipped with a self-contained oil system capable of providing continuous oil flow to the engine. Visit the page to find out more.
Technical topics
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Jet engine oil system, part 2 | ExxonMobil aviationMain engine shafts are supported by bearings in certain strategic places, depending on the load on the shafts and the length of the engine. Visit the page to find out more.
Technical topics
Features and Benefits
Mobil Jet Oil II is formulated to meet the demanding requirements of aircraft-type gas turbines operating over a wide range of severe operating conditions. The product has a high specific heat in order to ensure good heat transfer from oil-cooled engine parts. In extensive laboratory testing and in-flight performance, Mobil Jet Oil II exhibits excellent bulk oil stability at temperatures up to 204ºC (400 ºF). The evaporation rate at these temperatures is low enough to prevent excessive loss of volume. Key features and benefits include:
|
Features |
Advantages and Potential Benefits |
|
Excellent thermal and oxidation stability |
Reduces the formation of carbon and sludge deposits Maintains engine efficiency and extends engine life |
|
Excellent wear and corrosion protection |
Extends gear and bearing life Reduces engine maintenance |
|
Retains viscosity and film strength across wide temperature range |
Provides effective lubrication at high operating temperatures |
|
Chemically stable |
Reduces evaporation losses and lowers oil consumption |
|
Low pour point |
Eases start-up in low ambient temperature conditions |
Applications
Mobil Jet Oil II is recommended for aircraft gas turbine engines of the turbo-jet, turbo-fan, turbo-prop, and turbo-shaft (helicopter) types in commercial and military service. It is also recommended for aircraft-type gas turbine engines used in industrial or marine applications. Mobil Jet Oil II is approved against the Standard Performance (STD) classification of U.S. Military Specification MIL-PRF-23699. It is also compatible with other synthetic gas turbine lubricants meeting MIL-PRF-23699. However, mixing with other products is not recommended because the blend would result in some loss of the performance characteristics of Mobil Jet Oil II. Mobil Jet Oil II is compatible with all metals used in gas turbine construction, as well as with F Rubber (Viton A), H Rubber (Buna N), and silicone seal materials.
Mobil Jet Oil II has the following builder approvals *
Engines
• Honeywell/Lycoming-Turbines
• Rolls-Royce/Allison Engine Company
• CFM International
• General Electric Company
• International Aero Engines
• Pratt and Whitney Group
• Pratt and Whitney, Canada
• Rolls-Royce Limited
• SNECMA
• Honeywell/Garrett Turbine Engine Company
• Turbomeca
Accessories
• Honeywell-Auxiliary power units and air cycle machines
• Hamilton Standard-Starters
• Hamilton Sundstrand Corp.-APUs, constant-speed drives and integrated-drive generators
* Specific engine or equipment approval must be verified with the builder
Specifications and Approvals
|
This product has the following approvals: |
|
PRI-QPL-AS5780/SPC |
Properties and Specifications
|
Property |
|
|
Autogenous-ignition temperature test, deg.C, 30 CFR 35.20 |
404 |
|
Change in Kinematic Viscosity, 72 h @ -40 C, %, ASTM D2532 |
0.15 |
|
Density @ 15 C, kg/l, ASTM D4052 |
1.0035 |
|
Elastomer Compatibility, AMS-3217/4 (72hrs @204C), % swell, FTMS 791-3604 |
15.6 |
|
Elastomer Compatibility,AMS-3217/1(72hr @70C), % swell, FTMS 791-3604 |
16.4 |
|
Evaporation Loss, 6.5 h, 204 C, mass%, ASTM D972(mod) |
3.0 |
|
Evaporation Loss, 6.5 hr @ 232 C, 29.5" Hg, mass %, ASTM D972(mod) |
10.9 |
|
Evaporation Loss, 6.5 hr @ 232 C, 5.5" Hg, mass %, ASTM D972(mod) |
33.7 |
|
Fire Point, °C, ASTM D92 |
285 |
|
Flash Point, Cleveland Open Cup, °C, ASTM D92 |
270 |
|
Foam, Sequence I, Tendency, ml, ASTM D892 |
8 |
|
Foam, Sequence II, Tendency, ml, ASTM D892 |
10 |
|
Foam, Sequence III, Tendency, ml, ASTM D892 |
8 |
|
Kinematic Viscosity @ 100 C, mm2/s, ASTM D445 |
5.1 |
|
Kinematic Viscosity @ 40 C, mm2/s, ASTM D445 |
27.6 |
|
Kinematic Viscosity @ -40 C, mm2/s, ASTM D445 |
11000 |
|
Pour Point, °C, ASTM D5950 |
-59 |
|
Shear Stability, %KV loss, ASTM D2603 |
0.9 |
|
Total Acid Number, mgKOH/g, ARP 5088 |
0.03 |
|
Ryder Gear Load Carrying, % vs ref., FTMS 791-6508 |
115 |
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
CFM 56-3B/3C
CFM 56-7B
CFM Leap 1A
CFM Leap 1B
CFM Leap 1C
Engine Alliance (EA) GP7200
GE Aviation CF34-10
GE Aviation CF34-10E
GE Aviation CF34-3
GE Aviation CF34-8C
GE Aviation CF34-8E
GE Aviation CF6-50
GE Aviation CF6-80E
GE Aviation GE90
GE Aviation GEnX-1B
GE Aviation GEnX-2B
Hamilton Sundstrand/UTAS IDG
Hamilton Sundstrand/UTAS VFSG
Hamilton Sundstrand/UTAS VFG
Hamilton Sundstrand/UTAS APS 1000
Hamilton Sundstrand/UTAS APS 2000
Hamilton Sundstrand/UTAS APS 2100
Hamilton Sundstrand/UTAS APS 2300
Hamilton Sundstrand/UTAS APS 2600
Hamilton Sundstrand/UTAS APS 3200
Hamilton Sundstrand/UTAS APS 500
Hamilton Sundstrand/UTAS Starters
Honeywell 131-9
Honeywell 131-9B
Honeywell 131-9C
Honeywell 331-200
Honeywell 331-350
Honeywell 331-500
Honeywell 331-600
Honeywell GTCP 36-300
Honeywell GTCP-85
Honeywell HGT-1700
Honeywell HGT-750
Honeywell RE220
International Aero Engines (IAE) V2500
Pratt & Whitney PW1100G-JM
Pratt & Whitney PW1500G
Pratt & Whitney PW2000
Pratt & Whitney PW4000
Pratt & Whitney PW6000
Pratt & Whitney 127
Pratt & Whitney 150
Pratt & Whitney Canada 901
Pratt & Whitney Canada 980
Pratt & Whitney JT8-D
Rolls Royce - RB211-500
Rolls Royce Trent 500
Rolls Royce Trent 700
Rolls Royce Trent 800
Rolls Royce Trent 900
Aerolec VFG
CFM 56-2C
Turbomeca
Pratt & Whitney PW1400G-JM
Rolls Royce BR715
GE Aviation CF6-6
GE Aviation CF6-80
GE Aviation 9X
GE Aviation CF34-10A
Pratt & Whitney JT9-D
Pratt & Whitney PW1700G
Pratt & Whitney PW1900G
Honeywell GTCP 660
Honeywell HW TSCP-700
Safran VFG
Deposit control
Foaming resistance
Military use
Wear protection
Corrosion protection
High/Low temperature viscosity
- MIL-PRF-23699-STD
- PRI-QPL-AS5780/SPC
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