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Approvals and Conformities
Product Attributes
Country of Origin
Changes which have taken place over the last twenty years in engine performance (in terms of improved fuel consumption, higher operating temperatures and pressures) and maintenance practices have resulted in increased severity in lubricant operating conditions
AeroShell Turbine Oil 560 was developed to withstand the hostile environments of today's high powered, high compression engines in which the older generation of oils can be stressed up to and beyond their thermal limits, as evidenced by oil coking in the high temperature bearing areas.
By overcoming the problems associated with using old technology oils in new technology engines, AeroShell Turbine Oil 560:
in both new and existing engines.
In order for military authorities to take advantage of this better performance in military engines the specification MIL-PRF-23699 was re-written to include a "High Thermal Stability" (HTS) grade as well as the Standard (STD) and Corrosion Inhibited (C/I) grades. AeroShell Turbine Oil 560 is fully approved as an HTS oil. With the advent of the new civil turbine oil specification, SAE AS5780, which has more stringent requirements than the military specification, AeroShell Turbine Oil 560 was approved as a SPC (Standard Performance Capability) oil.
With effect from January 1st 2002, AeroShell Turbine Oil 560 has been manufactured with an improved formulation to further enhance its anti-coking performance. AeroShell Turbine Oil 560 contains a synthetic ester oil and should not be used in contact with incompatible seal materials and it also affects some paints and plastics.
Approvals/References/Specification
Features
AeroShell Turbine Oil 560 is approved for use in all models of the following engines:- Honeywell TPE 331, APUs (majority of models), LTS 101, LTP 101, ALF 502, LF 507, AS907, AS977, GTCP 30, 36, 85, 331, 660, RE220
- Allison Rolls-Royce 250 Series
- BMW-Rolls-Royce BR710, BR715
- CFM International CFM 56 (all models)
- CFE CFE 738
- Engine Alliance GP7200
- GE GE 90, CF6 (all models) CJ610, CF700, CT34, GEnX
- IAE V2500 Series
- IHI FJR 710
- Hamilton Sundstrand APS 500, 1000, 2000, 3000
- Pratt & Whitney JT3D, JT8D, JT9D, PW4000 Series (cleared for flight evaluation in PW2000 engines)
- Pratt & Whitney Canada PT6T, PT6A (some models only), PW120,121 Series, JT15D, PW200 Series, PW300 Series, PW500 Series, PW901A APU
- Rolls-Royce Spey, Tay RB183, Adour, RB199
- Turbomeca Ardiden, Arriel, Arrius, Arrius 1D, AST 600, Astazou XVI, Makila, TM333. Approved with restrictions: Artouste, AST 950, Bastan, Turmo
Kinematic Viscosity mm 2/s
Thermal Stability/Corrosivity 96 hrs @ 274°C
Corrosion & Oxidation Stability
Bearing Test Rig (200 hrs) Type 1-1/2 conditions
Sonic shear stability