Brand
Shell
Type
Aviation turbine oils
Primary standard
NATO Code O-154
Manufacturer code
001A0085

AeroShell Turbine Oil 560

Low-coking 5 mm²/s synthetic oil for aircraft turbine engines

Specifications

Brand
Shell
Manufacturer code
001A0085
Availability
On order

Approved for

Typical characteristics

PropertyTypical valueLimit
Oil typeEster sinteticEster sintetic
Kinematic viscosity la 100°C5.244.90 to 5.40
Kinematic viscosity la 40°C26.7123.0 min
Kinematic viscosity la -40°C935113000 max
Flash point (COC)°C268246 min
Pour point°C-60-54 max
Total aciditymgKOH/g0.201 max
Pierderi prin Evaporation 6.5 hours @204°C2.010.0 max
Spumaretrecetrebuie sa treaca
Standard umflare Rubber sintetic - SAE-AMS 3217/4, 72 hours la 204°Cumflare %12.95 la 25
Compatibilitate elastomer, schimbare de greutate dupa 24/120 hours: Fluorocarbon la 200°C7.5/9.010/15 max.
LCS Fluorocarbon la 200°C6.5/8.5 max.10/20 max.
Nitril la 130°C6.5/6.0Report
Silicon la 175°C14.5/13.5Report
Perfluoroelastomer la 200°C0.5/0.5
Stabilitate termica / Corozivitate 96 hours - schimbare greutate metal la 274°Cmg/cm20.234 max
Stabilitate termica / Corozivitate 96 hours - schimbare viscozitate la 37.8°C%0.35 max
Stabilitate termica / Corozivitate 96 hours - schimbare TANmgKOH/g1.56 max
Corrosion stability si Oxidation 72 hours la 175°Ctrecetrebuie sa treaca
Corrosion stability si Oxidation 72 hours la 204°Ctrecetrebuie sa treaca
Corrosion stability si Oxidation 72 hours @218°Ctrecetrebuie sa treaca
Test Pasager de viteze, evaluare relativa Hercolube A%112102
Bearing test rig (100 hours), conditii tip 1 1/2 - evaluare generala depuneri2180 max
Bearing test rig (100 hours), conditii tip 1 1/2 - schimbare viscozitate la 40°C24-5 la +30
Bearing test rig (100 hours), conditii tip 1 1/2 - schimbare TAN0.812.0 max
Bearing test rig (200 hours), conditii tip 1 1/2 - depozite filtrug0.553 max
Stabilitate sonica la forfecare - schimbare viscozitate la 40°C%0.34 max

Complete documentation

We email you this product's sheets in a single archive.

Manufacturer's description

AeroShell Turbine Oil 560 is a third-generation, high-performance, low-coking 5 mm2/s synthetic ester oil incorporating a carefully selected and finely balanced combination of additives to improve thermal and oxidation stability.

Applications

  • The changes that have taken place over the last twenty years in engine performance (in terms of fuel efficiency, high operating temperatures and pressures) and in maintenance practices have led to increasingly severe operating conditions for the lubricant.
  • AeroShell Turbine Oil 560 was developed to withstand the hostile environments of high-compression, high-output engines, where the older generation of oils can be stressed to and beyond their thermal limits, as evidenced by oil coking in high-temperature bearing areas.
  • By overcoming the problems created by using older-technology oils in newer-technology engines, AeroShell Turbine Oil 560:
  • in both new and existing engines. So that the military authorities could take advantage of this improved performance in military engines, the MIL-PRF-23699 specification was rewritten to include a "high thermal stability" (HTS) grade, as well as Standard (STD) and corrosion inhibited (C/I). AeroShell Turbine Oil 560 is fully approved as an HTS oil. With the advent of a new civil turbine oil specification, SAE AS5780, which has more stringent requirements than the military specification, AeroShell Turbine Oil 560 was approved as an SPC (Standard Performance Capability) oil.
  • With effect from 1 January 2002, AeroShell Turbine Oil 560 has been produced with an improved formulation to enhance its anti-coking performance.
  • extends bearing life in both new and existing engines
  • So that the military authorities could take advantage of this improved performance in military engines, the MIL-PRF-23699 specification was rewritten to include a "high thermal stability" (HTS) grade, as well as Standard (STD) and corrosion inhibited (C/I). AeroShell Turbine Oil 560 is fully approved as an HTS oil. With the advent of a new civil turbine oil specification, SAE AS5780, which has more stringent requirements than the military specification, AeroShell Turbine Oil 560 was approved as an SPC (Standard Performance Capability) oil

Performance & benefits

  • GE 90, CF6 (all models), CJ610, CF700, CT34, GEnX
  • Approved MIL-PRF-23699F Grade HTS (US). Approved SAE AS5780B Grade SPC
  • Analogous to VNII NP 50-1-4F, B3V, LZ-240, VNII NP 50-1-4U and 36/Ku-A (Russian)
  • AeroShell Turbine Oil 560 is approved for use in all models of the following engines
  • Honeywell: TFE 731, TPE 331, APUs (most models), LTS 101, LTP 101, ALF 502, LF 507, AS907, AS977, GTCP 30, 36, 85, 331, 660, RE220
  • AeroShell Turbine Oil 560 contains a synthetic ester oil

Standards & approvals

  • NATO Code O-154

    NATO Code O-154 — aviation turbine oil

    A NATO supply code identifying an aviation gas-turbine engine oil.

  • Allison EMS-53

    Allison gas-turbine engine oil specification (EMS-53, obsolete)

    Allison's (now Rolls-Royce) obsolete specification for gas-turbine engine oil, historically used to qualify oils for Allison/Rolls-Royce turboprop and turboshaft engines such as the Model 250 series.Source

  • Joint Service Designation OX-27

    Synthetic ester aviation turbine oil, standard grade

    UK MOD Joint Service Designation code for a 5 mm²/s synthetic ester aviation turbine oil, equivalent to MIL-PRF-23699 grade STD and DEF STAN 91-101 grade OX-27.Source

  • DEF STAN 91-101

    DEF STAN 91-101 — aviation turbine oil

    The UK Defence Standard for a synthetic 5 cSt aviation gas-turbine engine oil, matching NATO Code O-156.Source

  • MIL-PRF-23699

    MIL-PRF-23699 — aviation turbine engine oil

    The US military specification for synthetic aviation gas-turbine (jet) engine oils; STD, HTS and CI are its sub-classes by thermal stability/corrosion-inhibition level.

Also listed

  • Pratt & Whitney : Aprobat 521C Tip II
  • General Electric : Aprobat D-50 TF1
  • IAE : Serie V2500
  • IHI : FJR 710
  • Echivalent DCSEA 299/A (French)
  • Aprobare COMAC QPL-CMS-OL-202
  • Hamilton Sundstrand : APS 500, 1000, 2000, 3000

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