946 mL – 1 U.S. Quart - BP
946 mL – 1 U.S. Quart - BP
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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