AeroShell™ Turbine Oil 560 Synthetic Turbine Engine Oil - Quart Can

Our Part #: SGP51304
Manufacture Part #: 550050223Q
Our Price: $16.82 (Each)
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Approvals and Conformities

Approvals and Conformities

NSN
9150-01-439-0756
MIL-SPEC#
MIL-L-23699 MIL-PRF-23699
Alternate PN#s
AEROSHELL 560 550042550

Product Attributes

Country of Origin
United States
Size
Quart
Shipping Weight
2.5 pounds
ECCN
EAR99
Manufacturer P/N
Turbine Oil 560
Schedule B Code
2710.19.3020
Pack Quantity
1
Ship Dimensions
5 x 5 x 6 inches
Size
Quart (948 mL)
AeroShell Turbine Oil 560 is a 5 mm2/s synthetic ester oil incorporating additives to improve thermal and oxidation stability. A corrosion inhibitor has also been added.

Approvals/References/Specification

  • US Military Specification: MIL-L-23699
  • US Military Specification: MIL-PRF-23699
  • US Military Specification: MIL-PRF-23699 HTS
  • 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

  • Oil Type: Synthetic ester
    Kinematic Viscosity mm 2/s
  • @ 100°C: 5.24
  • @ 40°C: 26.71
  • @ –40°C: 11000
  • Flashpoint, Cleveland Open Cup °C: 268
  • Pourpoint °C: –60
  • Total Acidity mgKOH/g: 0.14
  • Evaporation Loss 6.5 hrs @ 204°C %m: 2.0
  • Foaming: Passes
  • Swelling of Standard Synthetic Rubber
  • SAE-AMS 3217/1, 72 hrs @ 70°C swell %: 12.9
  • SAE-AMS 3217/4, 72 hrs @ 204°C swell %: 12.9
  • Standard silicone rubber 90 hrs @ 121°C: 8.9
    Thermal Stability/Corrosivity 96 hrs @ 274°C
  • Metal weight change mg/cm2: 0.23
  • Viscosity change @ 37.8°C %: 0.3
  • Total Acid Number Change mgKOH/g: 1.5
    Corrosion & Oxidation Stability
  • 72 hrs @ 175°C: Passes
  • 72 hrs @ 204°C: Passes
  • 72 hrs @ 218°C: Passes
  • Ryder Gear Test, Relative Rating Hercolube A %: 126
    Bearing Test Rig (200 hrs) Type 1-1/2 conditions
  • Overall deposit demerit rating: 26
  • Viscosity change @ 40°C %: 30.8
  • Total Acid Number change mgKOH/g: 0.98
  • Filter deposits g: 0.55
    Sonic shear stability
  • Viscosity change @ 40°C %: NIL
  • Trace metal content: Passes

    Downloads

    download icon Safety Data Sheet

  • Product Attributes

    Approvals and Conformities

    NSN
    9150-01-439-0756
    MIL-SPEC#
    MIL-L-23699 MIL-PRF-23699
    Alternate PN#s
    AEROSHELL 560 550042550

    Product Attributes

    Country of Origin
    United States
    Size
    Quart
    Shipping Weight
    2.5 pounds
    ECCN
    EAR99
    Manufacturer P/N
    Turbine Oil 560
    Schedule B Code
    2710.19.3020
    Pack Quantity
    1
    Ship Dimensions
    5 x 5 x 6 inches
    Size
    Quart (948 mL)
    AeroShell Turbine Oil 560 is a 5 mm2/s synthetic ester oil incorporating additives to improve thermal and oxidation stability. A corrosion inhibitor has also been added.

    Approvals/References/Specification

  • US Military Specification: MIL-L-23699
  • US Military Specification: MIL-PRF-23699
  • US Military Specification: MIL-PRF-23699 HTS
  • 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

  • Oil Type: Synthetic ester
    Kinematic Viscosity mm 2/s
  • @ 100°C: 5.24
  • @ 40°C: 26.71
  • @ –40°C: 11000
  • Flashpoint, Cleveland Open Cup °C: 268
  • Pourpoint °C: –60
  • Total Acidity mgKOH/g: 0.14
  • Evaporation Loss 6.5 hrs @ 204°C %m: 2.0
  • Foaming: Passes
  • Swelling of Standard Synthetic Rubber
  • SAE-AMS 3217/1, 72 hrs @ 70°C swell %: 12.9
  • SAE-AMS 3217/4, 72 hrs @ 204°C swell %: 12.9
  • Standard silicone rubber 90 hrs @ 121°C: 8.9
    Thermal Stability/Corrosivity 96 hrs @ 274°C
  • Metal weight change mg/cm2: 0.23
  • Viscosity change @ 37.8°C %: 0.3
  • Total Acid Number Change mgKOH/g: 1.5
    Corrosion & Oxidation Stability
  • 72 hrs @ 175°C: Passes
  • 72 hrs @ 204°C: Passes
  • 72 hrs @ 218°C: Passes
  • Ryder Gear Test, Relative Rating Hercolube A %: 126
    Bearing Test Rig (200 hrs) Type 1-1/2 conditions
  • Overall deposit demerit rating: 26
  • Viscosity change @ 40°C %: 30.8
  • Total Acid Number change mgKOH/g: 0.98
  • Filter deposits g: 0.55
    Sonic shear stability
  • Viscosity change @ 40°C %: NIL
  • Trace metal content: Passes

    Downloads

    download icon Safety Data Sheet

  • Description

    Approvals and Conformities

    NSN
    9150-01-439-0756
    MIL-SPEC#
    MIL-L-23699 MIL-PRF-23699
    Alternate PN#s
    AEROSHELL 560 550042550

    Product Attributes

    Country of Origin
    United States
    Size
    Quart
    Shipping Weight
    2.5 pounds
    ECCN
    EAR99
    Manufacturer P/N
    Turbine Oil 560
    Schedule B Code
    2710.19.3020
    Pack Quantity
    1
    Ship Dimensions
    5 x 5 x 6 inches
    Size
    Quart (948 mL)
    AeroShell Turbine Oil 560 is a 5 mm2/s synthetic ester oil incorporating additives to improve thermal and oxidation stability. A corrosion inhibitor has also been added.

    Approvals/References/Specification

  • US Military Specification: MIL-L-23699
  • US Military Specification: MIL-PRF-23699
  • US Military Specification: MIL-PRF-23699 HTS
  • 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

  • Oil Type: Synthetic ester
    Kinematic Viscosity mm 2/s
  • @ 100°C: 5.24
  • @ 40°C: 26.71
  • @ –40°C: 11000
  • Flashpoint, Cleveland Open Cup °C: 268
  • Pourpoint °C: –60
  • Total Acidity mgKOH/g: 0.14
  • Evaporation Loss 6.5 hrs @ 204°C %m: 2.0
  • Foaming: Passes
  • Swelling of Standard Synthetic Rubber
  • SAE-AMS 3217/1, 72 hrs @ 70°C swell %: 12.9
  • SAE-AMS 3217/4, 72 hrs @ 204°C swell %: 12.9
  • Standard silicone rubber 90 hrs @ 121°C: 8.9
    Thermal Stability/Corrosivity 96 hrs @ 274°C
  • Metal weight change mg/cm2: 0.23
  • Viscosity change @ 37.8°C %: 0.3
  • Total Acid Number Change mgKOH/g: 1.5
    Corrosion & Oxidation Stability
  • 72 hrs @ 175°C: Passes
  • 72 hrs @ 204°C: Passes
  • 72 hrs @ 218°C: Passes
  • Ryder Gear Test, Relative Rating Hercolube A %: 126
    Bearing Test Rig (200 hrs) Type 1-1/2 conditions
  • Overall deposit demerit rating: 26
  • Viscosity change @ 40°C %: 30.8
  • Total Acid Number change mgKOH/g: 0.98
  • Filter deposits g: 0.55
    Sonic shear stability
  • Viscosity change @ 40°C %: NIL
  • Trace metal content: Passes

    Downloads

    download icon Safety Data Sheet

  • Approvals and Conformities

    Approvals and Conformities

    NSN
    9150-01-439-0756
    MIL-SPEC#
    MIL-L-23699 MIL-PRF-23699
    Alternate PN#s
    AEROSHELL 560 550042550

    Product Attributes

    Country of Origin
    United States
    Size
    Quart
    Shipping Weight
    2.5 pounds
    ECCN
    EAR99
    Manufacturer P/N
    Turbine Oil 560
    Schedule B Code
    2710.19.3020
    Pack Quantity
    1
    Ship Dimensions
    5 x 5 x 6 inches
    Size
    Quart (948 mL)
    AeroShell Turbine Oil 560 is a 5 mm2/s synthetic ester oil incorporating additives to improve thermal and oxidation stability. A corrosion inhibitor has also been added.

    Approvals/References/Specification

  • US Military Specification: MIL-L-23699
  • US Military Specification: MIL-PRF-23699
  • US Military Specification: MIL-PRF-23699 HTS
  • 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

  • Oil Type: Synthetic ester
    Kinematic Viscosity mm 2/s
  • @ 100°C: 5.24
  • @ 40°C: 26.71
  • @ –40°C: 11000
  • Flashpoint, Cleveland Open Cup °C: 268
  • Pourpoint °C: –60
  • Total Acidity mgKOH/g: 0.14
  • Evaporation Loss 6.5 hrs @ 204°C %m: 2.0
  • Foaming: Passes
  • Swelling of Standard Synthetic Rubber
  • SAE-AMS 3217/1, 72 hrs @ 70°C swell %: 12.9
  • SAE-AMS 3217/4, 72 hrs @ 204°C swell %: 12.9
  • Standard silicone rubber 90 hrs @ 121°C: 8.9
    Thermal Stability/Corrosivity 96 hrs @ 274°C
  • Metal weight change mg/cm2: 0.23
  • Viscosity change @ 37.8°C %: 0.3
  • Total Acid Number Change mgKOH/g: 1.5
    Corrosion & Oxidation Stability
  • 72 hrs @ 175°C: Passes
  • 72 hrs @ 204°C: Passes
  • 72 hrs @ 218°C: Passes
  • Ryder Gear Test, Relative Rating Hercolube A %: 126
    Bearing Test Rig (200 hrs) Type 1-1/2 conditions
  • Overall deposit demerit rating: 26
  • Viscosity change @ 40°C %: 30.8
  • Total Acid Number change mgKOH/g: 0.98
  • Filter deposits g: 0.55
    Sonic shear stability
  • Viscosity change @ 40°C %: NIL
  • Trace metal content: Passes

    Downloads

    download icon Safety Data Sheet

  • Product Attributes

    Approvals and Conformities

    NSN
    9150-01-439-0756
    MIL-SPEC#
    MIL-L-23699 MIL-PRF-23699
    Alternate PN#s
    AEROSHELL 560 550042550

    Product Attributes

    Country of Origin
    United States
    Size
    Quart
    Shipping Weight
    2.5 pounds
    ECCN
    EAR99
    Manufacturer P/N
    Turbine Oil 560
    Schedule B Code
    2710.19.3020
    Pack Quantity
    1
    Ship Dimensions
    5 x 5 x 6 inches
    Size
    Quart (948 mL)
    AeroShell Turbine Oil 560 is a 5 mm2/s synthetic ester oil incorporating additives to improve thermal and oxidation stability. A corrosion inhibitor has also been added.

    Approvals/References/Specification

  • US Military Specification: MIL-L-23699
  • US Military Specification: MIL-PRF-23699
  • US Military Specification: MIL-PRF-23699 HTS
  • 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

  • Oil Type: Synthetic ester
    Kinematic Viscosity mm 2/s
  • @ 100°C: 5.24
  • @ 40°C: 26.71
  • @ –40°C: 11000
  • Flashpoint, Cleveland Open Cup °C: 268
  • Pourpoint °C: –60
  • Total Acidity mgKOH/g: 0.14
  • Evaporation Loss 6.5 hrs @ 204°C %m: 2.0
  • Foaming: Passes
  • Swelling of Standard Synthetic Rubber
  • SAE-AMS 3217/1, 72 hrs @ 70°C swell %: 12.9
  • SAE-AMS 3217/4, 72 hrs @ 204°C swell %: 12.9
  • Standard silicone rubber 90 hrs @ 121°C: 8.9
    Thermal Stability/Corrosivity 96 hrs @ 274°C
  • Metal weight change mg/cm2: 0.23
  • Viscosity change @ 37.8°C %: 0.3
  • Total Acid Number Change mgKOH/g: 1.5
    Corrosion & Oxidation Stability
  • 72 hrs @ 175°C: Passes
  • 72 hrs @ 204°C: Passes
  • 72 hrs @ 218°C: Passes
  • Ryder Gear Test, Relative Rating Hercolube A %: 126
    Bearing Test Rig (200 hrs) Type 1-1/2 conditions
  • Overall deposit demerit rating: 26
  • Viscosity change @ 40°C %: 30.8
  • Total Acid Number change mgKOH/g: 0.98
  • Filter deposits g: 0.55
    Sonic shear stability
  • Viscosity change @ 40°C %: NIL
  • Trace metal content: Passes

    Downloads

    download icon Safety Data Sheet

  • Description

    Approvals and Conformities

    NSN
    9150-01-439-0756
    MIL-SPEC#
    MIL-L-23699 MIL-PRF-23699
    Alternate PN#s
    AEROSHELL 560 550042550

    Product Attributes

    Country of Origin
    United States
    Size
    Quart
    Shipping Weight
    2.5 pounds
    ECCN
    EAR99
    Manufacturer P/N
    Turbine Oil 560
    Schedule B Code
    2710.19.3020
    Pack Quantity
    1
    Ship Dimensions
    5 x 5 x 6 inches
    Size
    Quart (948 mL)
    AeroShell Turbine Oil 560 is a 5 mm2/s synthetic ester oil incorporating additives to improve thermal and oxidation stability. A corrosion inhibitor has also been added.

    Approvals/References/Specification

  • US Military Specification: MIL-L-23699
  • US Military Specification: MIL-PRF-23699
  • US Military Specification: MIL-PRF-23699 HTS
  • 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

  • Oil Type: Synthetic ester
    Kinematic Viscosity mm 2/s
  • @ 100°C: 5.24
  • @ 40°C: 26.71
  • @ –40°C: 11000
  • Flashpoint, Cleveland Open Cup °C: 268
  • Pourpoint °C: –60
  • Total Acidity mgKOH/g: 0.14
  • Evaporation Loss 6.5 hrs @ 204°C %m: 2.0
  • Foaming: Passes
  • Swelling of Standard Synthetic Rubber
  • SAE-AMS 3217/1, 72 hrs @ 70°C swell %: 12.9
  • SAE-AMS 3217/4, 72 hrs @ 204°C swell %: 12.9
  • Standard silicone rubber 90 hrs @ 121°C: 8.9
    Thermal Stability/Corrosivity 96 hrs @ 274°C
  • Metal weight change mg/cm2: 0.23
  • Viscosity change @ 37.8°C %: 0.3
  • Total Acid Number Change mgKOH/g: 1.5
    Corrosion & Oxidation Stability
  • 72 hrs @ 175°C: Passes
  • 72 hrs @ 204°C: Passes
  • 72 hrs @ 218°C: Passes
  • Ryder Gear Test, Relative Rating Hercolube A %: 126
    Bearing Test Rig (200 hrs) Type 1-1/2 conditions
  • Overall deposit demerit rating: 26
  • Viscosity change @ 40°C %: 30.8
  • Total Acid Number change mgKOH/g: 0.98
  • Filter deposits g: 0.55
    Sonic shear stability
  • Viscosity change @ 40°C %: NIL
  • Trace metal content: Passes

    Downloads

    download icon Safety Data Sheet