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IS1 — TURBINE FUEL,AVIATION

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

IS1: TURBINE FUEL,AVIATION.

The TURBINE FUEL,AVIATION is a the manufacturer industrial component. Key specifications include density_temp: 15.0 CELSIUS DEGC, supply_classification: BULK, end_item_identification: BARRETT M82A1 50 CALIBER SYSTEM, viscosity_at_rated_temp: 8.00 MAXIMUM -20 DEG CELSIUS, fuel_grade_classification: JET A-1, freezing_point_maximum_temp: -47.0 DEG CELSIUS. This part is cataloged in the U.S.

Government catalog under NSN 9130-01-476-5132, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.

Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS
IS1
NSN: 9130-01-476-5132
NIINs: 014765132, 015031795
FSC: 9130 — Liquid Propellants and Fuels, Petroleum Base
CAGE: 81349 — MILITARY SPECIFICATIONS PROMULGATED BY MILITARY DEPARTMENTS/AGENCIES UNDER AUTHORITY OF DEFENSE STANDARDIZATION MANUAL 4120 3-M
SPECIFICATIONS
density_temp15.0 CELSIUS DEGC
special_featuresITEM OF SUPPLY IS JET A1 DELIVERED AT COMMERCIAL AIRPORTS WITH REFUELING SERVICE AND OTHER SERVICES PROVIDED THESE ADDITIONAL SERVICES INCLUDE BUT ARE NOT LIMITED TO ADDITIVE INJECTION AND STORAGE
supply_classificationBULK
end_item_identificationBARRETT M82A1 50 CALIBER SYSTEM
viscosity_at_rated_temp8.00 MAXIMUM -20 DEG CELSIUS
fuel_grade_classificationJET A-1
freezing_point_maximum_temp-47.0 DEG CELSIUS
maximum_amount_of_existent_gum7.0
minimum_heat_of_combustion_value42.8 MEGAJOULES PER KILOGRAM
minimum_flash_point_and_test_method38.0 CELSIUS TAG CLOSED CUP DEGC
maximum_aromatics_percentage_by_volume20.0
maximum_distillation_loss_volume_percentage1.5
NSN9130-01-476-5132
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available TURBINE FUEL,AVIATION TITLE COMPONENT PN IS1 MFR TURBINE FUEL,AVIATION
KEY FEATURES
•
SUPPLY CLASSIFICATION: BULK
•
MINIMUM HEAT OF COMBUSTION VALUE: 42.8 MEGAJOULES PER KILOGRAM
•
MAXIMUM SULPHUR CONTENT PERCENTAGE BY WEIGHT: 0.3
•
DENSITY TEMP: 15.0 CELSIUS DEGC
•
FREEZING POINT MAXIMUM TEMP: -47.0 DEG CELSIUS
•
MAXIMUM AROMATICS PERCENTAGE BY VOLUME: 20.0
•
MINIMUM FLASH POINT AND TEST METHOD: 38.0 CELSIUS TAG CLOSED CUP DEGC
•
VISCOSITY AT RATED TEMP: 8.00 MAXIMUM -20 DEG CELSIUS
TECHNICAL CHARACTERISTICS
SUPPLY CLASSIFICATIONBULK
MINIMUM HEAT OF COMBUSTION VALUE42.8 MEGAJOULES PER KILOGRAM
MAXIMUM SULPHUR CONTENT PERCENTAGE BY WEIGHT0.3
DENSITY TEMP15.0 CELSIUS DEGC
FREEZING POINT MAXIMUM TEMP-47.0 DEG CELSIUS
MAXIMUM AROMATICS PERCENTAGE BY VOLUME20.0
MINIMUM FLASH POINT AND TEST METHOD38.0 CELSIUS TAG CLOSED CUP DEGC
VISCOSITY AT RATED TEMP8.00 MAXIMUM -20 DEG CELSIUS
SPECIAL FEATURESITEM OF SUPPLY IS JET A1 DELIVERED AT COMMERCIAL AIRPORTS WITH REFUELING SERVICE AND OTHER SERVICES PROVIDED THESE ADDITIONAL SERVICES INCLUDE BUT ARE NOT LIMITED TO ADDITIVE INJECTION AND STORAGE
MAXIMUM DISTILLATION LOSS VOLUME PERCENTAGE1.5
SUBSTITUTES & CROSS-REFERENCES 1
ASTM D 1655Reference document
Same NSN cross-reference
Reference document — Identification reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
HAZMAT per U.S. Government catalogNo demilitarization required
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FREQUENTLY ASKED QUESTIONS
What is IS1?
IS1 is a TURBINE FUEL,AVIATION.
What parts can replace IS1?
There is 1 known substitute for IS1: ASTM D 1655. Substitute compatibility should be verified for your specific system.
What is the NSN for IS1?
IS1 is cataloged in the U.S. Government catalog under NSN 9130-01-476-5132. This indicates validated use in U.S. government and defense supply chains.
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