DESCRIPTION
Turbonycoil 13 B is a lubricating oil with a viscosity of 3 cSt at 100°C. It is based on a
synthetic ester and contains anti-oxidant, anti-wear and anti-corrosion additives.
APPLICATIONS
• Turbine oil (power plant, APU, starter, IDG, etc.) for aircraft and helicopter
Turbonycoil 13 B has been specially developed to lubricate aircraft turbine engines equipped with a total loss
lubrication system such as SNECMA ATAR, fitted on Dassault Mirage III, IV, F1 and 5 ; Super Etendard.
It is also approved for use on SNECMA M53 engine (Dassault Mirage 2000 series) and many Turbomeca engines
(Artouste II and III ; Astazou II ; IV M ; XIV ; XVI, Makila, Arriel, Turmo IV, TM 319 and TM 333). These engines power a
large number of civil and military helicopters.
SPECIFICATIONS * / OEM’s & Airframers reference
• Approved AIR 3514/A
AIRCRAFT SYNTHETIC OIL FOR TURBOPROPELLER ENGINE
DESCRIPTION
TURBONYCOIL 98 is a lubricating oil with a viscosity of 7,50 cSt at 100°C.
It is made of a polyalkyleneglycol thickened diester and contains specific additives to improve its anti-oxidant properties.
APPLICATIONS
TURBONYCOIL 98 is intended for the lubrication of some aircraft and marine turbine engines as well as accessory equipment, particularly on turbopropeller engines where a high viscosity oil is required to protect the gears from heavy wear.
TURBONYCOIL 98 is widely used on helicopters as an analog for B-3V oil (specification TU 38.101295-85) to lubricate the engine and the main rotor gearbox.
SPECIFICATIONS, OEMS & AIRFRAMERS REFERENCE
DEF STAN 91-98
TU 38.101295-85
B-3V analog
Turbonycoil 160 is a 3 cSt oil at 100°C and is made of neopolyol esters containing additives to
improve its anti-oxidant, anti-corrosion and extreme-pressure properties. It is designed to
withstand the high temperature experienced by the military engines.
APPLICATIONS
• Turbine oil of fighter engines (McDonnel Douglas F-15, Lockheed Martin F-16, etc.)
• Turbine oil of civil engines below -40°C ambient temperature
• Turbine and tail rotor gearbox of helicopter in cold weather
• APU of civil aircraft for easy in-flight restart
• Trimmable Horizontal Stabilizer (THS) of civil aircraft
SPECIFICATIONS * / OEM’s & Airframers reference
• Approved MIL-PRF-7808 M Grade 3 • Listed in Airbus CML 03ABB1
• Meets OX-9 • Listed in ATR CML 03-003
• Listed in BOEING CML D00071 & CML D00109
SYNTHETIC AVIATION TURBINE OIL
DESCRIPTION
TURBONYCOIL 210 A is based on a blend of synthetic hydrocarbons and esters with a viscosity of 3,70 cSt at 100°C.
It contains a carefully selected package of anti-oxidant and anti-wear additives.
It offers a unique combination of high resistance to oxidation.
APPLICATIONS
TURBONYCOIL 210 A has been designed for the lubrication of the latest generation gas turbines.
It has been approved as an analog to IPM-10 oil (specification TU 38.1011299-2006).
TURBONYCOIL 210 A is recommended for a large number of APU and turbocoolers fitted on aircrafts, it can also be used as substitute for 36/1-KUA (specification TU 38.101384-78) and VNIINP-50-1-4F oils (specification GOST 13076-86).
SPECIFICATIONS, OEMS & AIRFRAMERS REFERENCE
TU 38.1011299-2006
TU 38.101384-78
GOST 13076-86
IPM-10 analog
36/1-KUA substitute
VNIINP-50-1-4F substitute
PETROLEUM AVIATION TURBINE OIL
DESCRIPTION
TURBONYCOIL 306 is a petroleum lubricating oil made from a mixture of 75% TURBONYCOIL 321 (approved as analog to MS-8P oil under OST 38.01163-78 specification) and 25% TURBONYCOIL 308 (approved as analog to MS-20 oil under GOST 21743-76 specification).
It has a viscosity of 4,50 cSt at 100°C.
APPLICATIONS
TURBONYCOIL 306 is intended for the lubrication of turboprop engines with heavily loaded gear-boxes.
It has been approved as an analog to SM-4,5 oil (specification OST 54-3-175-72-99).
SPECIFICATIONS, OEMS & AIRFRAMERS REFERENCE
OST 54-3-175-72-99
SM-4,5 analog
PETROLEUM LUBRICATING OIL FOR AIRCRAFT PISTON ENGINE
DESCRIPTION
TURBONYCOIL 308 is a lubricating oil with a viscosity of 21 cSt at 100°C.
It is based on petroleum base stocks with a pour point depressant.
APPLICATIONS
TURBONYCOIL 308 is designed for lubrication of aircraft piston engines.
It has been approved as an analog to MS-20 oil (specification GOST 21743-76).
SPECIFICATIONS, OEMS & AIRFRAMERS REFERENCE
GOST 21743-76
MS-20 analog
PETROLEUM AVIATION TURBINE OIL
DESCRIPTION
TURBONYCOIL 321 is based on a petroleum base stock and contains additives to improve the high temperature oxidation stability and prevent wear of gas turbine engines.
It has a viscosity of 8 cSt at 50°C.
APPLICATIONS
TURBONYCOIL 321 has been designed for the lubrication of the majority of gas turbines and recommended for a large number of APU and turbocoolers fitted on aircrafts.
It has been approved as an analog to MS-8P oil (specification OST 38.01163-78) and can be used as an anti-corrosion oil MS-8RK (specification TU 38.1011181-88).
TURBONYCOIL 321 has been used since the early 1990’s on civil airliners with hundreds of thousand flying hours accumulated.
It is also approved for use on industrial and marine gas turbines.
SPECIFICATIONS, OEMS & AIRFRAMERS REFERENCE
OST 38.01163-78
GOST 6457-66
TU 38.1011181-88
MS-8P analog
MK-8 substitute
MK-8P substitute
MS-8RK substitute
PETROLEUM AVIATION TRANSMISSION OIL
DESCRIPTION
TURBONYCOIL 329 is a petroleum lubricating oil containing extreme pressure additives.
APPLICATIONS
TURBONYCOIL 329 is intended for the lubrication of heavily loaded gears of the hypoid type.
It is used for secondary transmissions and joints in helicopters.
It has been approved as an analog to TSGIP oil (specification TU 38.1011332-90)
SPECIFICATIONS, OEMS & AIRFRAMERS REFERENCE
TU 38.1011332-90
Substitute to TSGIP
TURBONYCOIL® 400 is based on neopentyl polyol esters, fortified with carefully selected anti-oxidant, anti-wear and anti-corrosion additives. It has a viscosity of 4 cSt at 100°C. TURBONYCOIL® 400 is especially recommended in hot-running engines and environnements where fluidity at low temperature is required.
SYNTHETIC AVIATION TURBINE OIL
DESCRIPTION
TURBONYCOIL 600 is a lubricating oil with a viscosity of 5 cSt at 100°C, it is based on high thermal stable neopentyl polyol esters, fortified with carefully selected anti-oxidant, anti-wear and anti-corrosion additives.
TURBONYCOIL 600 features a much lower volatility at high temperature and a higher flash point than oils from competition.
It possesses excellent resistance to foaming and demonstrates superior lubricity.
APPLICATIONS
TURBONYCOIL 600 is designed for use in gas turbine engines and accessories of military and civil aircrafts and helicopters as well as in stationary industrial applications including off-shore installations.
It has been approved by all major engine manufacturers for use in most of military and civil engines, APUs, IDGs and propellers.
TURBONYCOIL 600 has logged over 60 million hours of operation since 1985.
It has been approved as a substitute to B-3V (specification TU 38.101295-85), VNIINP-50-1-4F (specification GOST 13076-86) and LZ-240 oils (specification TU 301-04-010-92).
SPECIFICATIONS, OEMS & AIRFRAMERS REFERENCE
NATO Code O-156
MIL-PRF-23699G STD
DCSEA 299/A
DEF STAN 91-101 Issue 3
OX-27, OX-28
SAE AS5780 SPC
Airbus CML 03ABA1
Airbus Helicopters CM103
ATR CML 03-002
ATR CML 03-008H
Bombardier CML 03-001F
Bombardier CML 03-009G
Bombardier CML 03-012G
Bombardier CML 03-015L
Bombardier CML 03-016B
Boeing CML D00068
Boeing CML D00523
TU 38.101295-85
GOST 13076-86
TU 301-04-010-92
B-3V substitute
VNIINP-50-1-4F substitute
LZ-240 substitute
DESCRIPTION
Turbonycoil 601 is a lubricating oil with a viscosity of 5 cSt at 100°C. It is based on neopentyl polyol
esters with high thermal stability, fortified with carefully selected anti-oxidant, anti-wear and anticorrosion additives.
APPLICATIONS
• Turbine of military and commercial aircrafts and helicopters requiring rust and corrosion protection due to exposure to saltladen air and ambient tropical environments
• Ground gas turbines (aero-derivative) used for power generation, gas pipelines and off-shore platforms requiring rust and
corrosion exposure to salt-laden air and ambient tropical environments
SPECIFICATIONS * / OEM’s & Airframers reference
• Approved MIL-PRF-23699 G Class C/I
• Approved OX-152
• Approved MIL-PRF-23699 G Class STD
• Listed in Airbus Helicopters CM128
DESCRIPTION
Turbonycoil 640 is a lubricating oil with a viscosity of 5 cSt at 100°C. It is based on neopentyl
polyol esters with high thermal stability, fortified with carefully selected anti-oxidant, anti-wear
and anti-corrosion additives.
APPLICATIONS
Turbonycoil 640 has been designed for use in gas turbine engines in commercial and military aircrafts and helicopters as well as in
aero-derivative gas turbines. It is tailor-made to address the following requirements regarding low coking propensity, high resistance
to oxidation and thermal degradation, high electrical conductivity. Therefore Turbonycoil 640 is recommended for use in hot running
engine designs where evidence of oil coking and/or oil degradation was noted.
• Turbine oil of commercial and military aircrafts and helicopters, recommended in hot engines
• Accessories (APU, IDG, starter)
• Main and tail helicopter gearbox
• Aeroderivative Gas Turbines
SPECIFICATIONS / OEM’s & Airframers reference
• Approved MIL-PRF-23699 G Class HTS
• Approved SAE AS 5780 Class HPC
• Listed in Airbus Helicopters CM129
SYNTHETIC AVIATION TURBINE OIL
DESCRIPTION
TURBONYCOIL 699 is a lubricating oil with a viscosity of 5 cSt at 100°C.
It is based on neopentyl polyol esters with high thermal stability, fortified with selected additives.
It exhibits an improved anti-wear performance over turbine oils of same viscosity (MIL-PRF-23699 Class STD and HTS).
APPLICATIONS
TURBONYCOIL 699 is designed for use in gas turbine engines in military and commercial aircrafts as well as in stationary industrial applications.
TURBONYCOIL 699 is best used in jet engines that require a very high load-carrying capacity to reduce wear of highly loaded components (gearbox, bearings).
TURBONYCOIL 699 is recommended for helicopter gearboxes that are exposed to both high loads and high temperature for long period of time.
TURBONYCOIL 699 has been used since 1996 on the RB199 engine of Panavia Tornado multi-role fighter.
It has been approved as an analog to B-3V oil (specification TU 38.101295-85) and as a substitute to VNIINP-50-1-4F (specification GOST 13076-86) and LZ-240 oils (specification TU 301-04-010-92).
SPECIFICATIONS, OEMS & AIRFRAMERS REFERENCE
DEF STAN 91-100 Issue 3
OX-26
TU 38.101295-85
GOST 13076-86
TU 301-04-010-92
B-3V analog
VNIINP-50-1-4F substitute
LZ-240 substitute
MINERAL TURBINE OIL
DESCRIPTION
TURBONYCOIL 3516 is a mineral turbine oil blended from mineral naphthenic base stocks and anti-oxidant additives, with a viscosity of 3 cSt at 100°C.
It retains a low viscosity at very low temperature, down to – 60°C.
APPLICATIONS
Turbines and accessories (APU, starter, IDG) of commercial and military aircraft and helicopters of first generation.
Preservation oil for aircraft engine fuel control system.
SPECIFICATIONS, OEMS & AIRFRAMERS REFERENCE
NATO Code O-133
MIL-PRF-6081E Grade 1010
AIR 3516/A
Airbus CML 03BEB1
Airbus Helicopters CM133
Boeing CML D00124
CFMI CP 5066
DESCRIPTION
Turbonycoil 3560 SAE 50 is a non-dispersive petroleum lubricating oil with a viscosity of 19 cSt at 100°C.
Turbonycoil 3560 SAE 50 is produced from blends of selected petroleum base stocks and contains a pour
point depressant additive to improve low temperature properties.
Turbonycoil 3560 SAE 50 complies with SAE J1966 Grade 50 requirements, as well as former military
specification MIL-L-6082 E grade 1100 and AIR 3560/D grade 100, now obsolete.
APPLICATIONS
• 4-stroke reciprocating piston aircraft engine
• Piston engine of vintage airplanes (WWI and WWII warplanes)
SPECIFICATIONS * / OEM’s & Airframers reference
• Meets SAE J1966 Grade 50
• Meets MIL-L-6082 E Grade 100 (obs)
• Meets AIR 3560/D Grade 100 (obs)
PISTON AIRCRAFT ENGINE LUBRICATING OIL
DESCRIPTION
TURBONYCOIL 3570 15W50 is a semi-synthetic dispersive lubricating oil with a 20 mm²/s viscosity at 100°C.
TURBONYCOIL 3570 15W50 is produced from selected mineral and synthetic base stocks blended with ashless additives to improve low temperature fluidity and engine cleanliness.
Moreover it also contains in the correct proportion an anti-wear additive equivalent to the Lycoming additive LW-16702.
TURBONYCOIL 3570 15W50 complies with SAE J1899 15W50 requirements, as well as former military specification MIL-L-22851 15W50 now obsolete.
APPLICATIONS
Four-stroke reciprocating piston aircraft engines.
It has been approved as a substitute to VO-12 oil (specification TU 38.401-58-359-2005).
SPECIFICATIONS, OEMS & AIRFRAMERS REFERENCE
SAE J1899 15W50
MIL-L-22851D 15W50
TU 38.401-58-359-2005
VO-12 substitute
LZ-240 substitute
DESCRIPTION
Turbonycoil 3570 SAE 40 is a petroleum dispersive lubricating oil with a 15 mm²/s viscosity at
100°C.
Turbonycoil 3570 SAE 40 is produced from selected mineral base stocks blended with ashless
additives to improve low temperature fluidity and engine cleanliness.
Moreover Turbonycoil 3570 SAE 40 also contains in the correct proportion an anti-wear additive equivalent to the
Lycoming additive LW-16702. As a consequence LW-16702 additive DOES NOT have to be added to Turbonycoil 3570
SAE 40 during the oil changes.
Turbonycoil 3570 SAE 40 complies with SAE J1899 Grade 40 requirements, as well as former military specification MILL-22851 type III and AIR 3570/D grade 80, now obsolete.
APPLICATIONS
• 4-stroke reciprocating piston aircraft engine
SPECIFICATIONS * / OEM’s & Airframers reference
• Meets SAE J1899 Grade 40
• Meets MIL-L-22851 Type III (obs)
• Meets AIR 3570/D Grade. 80 (obs)
DESCRIPTION
Turbonycoil 3570 SAE 50 is a petroleum dispersive lubricating oil with a 19 mm²/s viscosity at
100°C.
Turbonycoil 3570 SAE 50 is produced from selected mineral base stocks blended with ashless
additives to improve low temperature fluidity and engine cleanliness.
Moreover Turbonycoil 3570 SAE 50 also contains in the correct proportion an anti-wear additive
equivalent to the Lycoming additive LW-16702. As a consequence LW-16702 additive DOES NOT have to be added to
Turbonycoil 3570 SAE 50 during the oil changes.
Turbonycoil 3570 SAE 50 complies with SAE J1899 Grade 50 requirements, as well as the former military specifications
MIL-L-22851D commercial grade 100 and AIR 3570/D grade 100, now obsolete.
APPLICATIONS
• 4-stroke reciprocating piston aircraft engine
SPECIFICATIONS / OEM’s & Airframers reference
• Meets SAE J1899 Grade 50
• Meets AIR 3570/D Grade 100 (Obs)
DESCRIPTION
Turbonycoil 3570 SAE 60 is a petroleum dispersive lubricating oil with a 25 mm²/s viscosity at
100°C.
Turbonycoil 3570 SAE 60 is produced from selected mineral base stocks blended with ashless
additives to improve low temperature fluidity and engine cleanliness.
Moreover Turbonycoil 3570 SAE 60 also contains in the correct proportion an anti-wear
additive equivalent to the Lycoming additive LW-16702. As a consequence LW-16702 additive DOES NOT have to be
added to Turbonycoil 3570 SAE 60 during the oil changes
Turbonycoil 3570 SAE 60 complies with SAE J1899 Grade 60 requirements, as well as former military specification MILL-
22851 type II and AIR 3570/D grade 120, now obsolete.
APPLICATIONS
• 4-stroke reciprocating piston aircraft engine
SPECIFICATIONS * / OEM’s & Airframers reference
• Meets SAE J1899 Grade 60
• Meets MIL-L-22851 Type II (obs)
• Meets AIR 3570/D Gr. 120 (obs)
