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946 mL – 1 U.S. Quart - BP

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P roduct Description<br />

<strong>BP</strong>TO 2380 is a synthetic oil having a viscosity of 5<br />

centistokes at 210°F that is approved against US<br />

military specification MIL-PRF-23699F-STD, DEF STAN<br />

91-101/2* (DERD 2499), and meets the requirements of<br />

most jet engines and associated accessories. It is a<br />

Type II oil which provides a more balanced combination<br />

of thermal and oxidation stability, load-carrying capacity,<br />

lower volatility and low temperature flow characteristics<br />

than other 5 cSt jet engine oils. These features provide<br />

long trouble-free performance under most conditions.<br />

Synthetic oils of this type are not all identical. The<br />

performance advantages of <strong>BP</strong>TO 2380 are achieved by<br />

careful selection and balance of basestocks and<br />

additives to provide the desired performance.<br />

Details of laboratory analyses of physical, chemical,<br />

and performance properties are provided in the<br />

Appendix. Significant performance properties are<br />

discussed below. Where detailed information on the<br />

laboratory test methods and the significance of results<br />

is desired, a member of our <strong>BP</strong> technical staff will be<br />

happy to provide them.<br />

V I S C O S I T Y : While most Type II synthetic turbo oils<br />

have essentially the same viscosity at 99°C (between 5<br />

and 5.5 centistokes), <strong>BP</strong>TO 2380 is less viscous at very<br />

cold temperatures than other Type II oils. This offers a<br />

distinct advantage, which permits <strong>BP</strong>TO 2380 to be<br />

used in some critical applications where other Type II<br />

oils are excessively viscous. For example, at -40°C the<br />

viscosity of <strong>BP</strong>TO 2380 is well below that of<br />

competitive products.<br />

Competitive Products<br />

<strong>BP</strong>TO 2380 A B<br />

Viscosity, cSt<br />

at -40°C 7950 12 , 390 10 , 640<br />

VAPOR PHASE DEPOSITS: A major advantage of<br />

<strong>BP</strong>TO 2380 is its ability to limit vapor-phase deposits.<br />

With some competitive oils, heavy deposits have<br />

formed where the oil mist and vapors come in contact<br />

with hot engine surfaces resulting in migrating deposits.<br />

LOAD CARRYING: <strong>BP</strong>TO 2380 provides load carrying<br />

ability, as measured in the Ryder Gear Test well in<br />

excess of requirements established by the engine and<br />

equipment manufacturers. Long life of bearings, gears,<br />

and other highly loaded lubricated surfaces is thus<br />

assured under normal operating conditions.<br />

C L E A N L I N E S S : Minimum formation of varnish or<br />

sludge deposits is one of the characteristic advantages<br />

of <strong>BP</strong>TO 2380. Long periods of operation are possible<br />

without the danger of scavenge pump screen plugging<br />

or the corrosion that often accompanies excessive<br />

d e p o s i t s .<br />

BULK STABILITY (resistance to physical or chemical<br />

change resulting from oxidation): The high<br />

degree of oxidation resistance of <strong>BP</strong>TO 2380 permits<br />

long periods of operation without significant increase in<br />

viscosity or total acidity, the two principal indicators of<br />

product oxidation. The need to change oil because of<br />

oxidation effects is rare when using <strong>BP</strong>TO 2380. Most<br />

users find it unnecessary to make oil changes in spite of<br />

occasional mechanical abnormalities that create<br />

unusually severe oxidizing conditions.<br />

C O M P A T I B I L I T Y :While considerable laboratory data is<br />

available to demonstrate the compatability of <strong>BP</strong>TO<br />

2380 with metals, elastomers and other lubricants, the<br />

extensive airline experience most adequately demonstrates<br />

this property. Details are given in the section on<br />

“Product Performance.”<br />

SEAL WEAR: Proper functioning of carbon seals is<br />

essential for the life of the engines that use this type of<br />

bearing compartment sealing arrangement. Poor seal<br />

performance may be caused by lubricant properties that<br />

promote (or fail to prevent) wear of the carbon at the<br />

carbon-to-steel face. <strong>BP</strong>TO 2380 has provided the<br />

dependable performance in numerous airlines that was<br />

predicted by extensive laboratory tests.<br />

* <strong>BP</strong>TO 2380 is approved against DEF STAN 91-101/2 (DERD 2499)<br />

for both OX-27 and OX-28 requirements. OX-27 is for use in military<br />

gas turbines and accessories. OX-28 is for use in marine gas<br />

t u r b i n e s .<br />

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