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JAA — TURBINE FUEL,AVIATION

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

JAA: TURBINE FUEL,AVIATION.

The TURBINE FUEL,AVIATION is a the manufacturer industrial component. Key specifications include density_value: 0.775 KILOGRAMS PER LITER MINIMUM AND 0.840 KILOGRAMS PER LITER MAXIMUM KG, nato_code_number: F24, special_features: MRAP BUFFALO MK2A2, supply_classification: BULK, viscosity_at_rated_temp: 8.00 MAXIMUM -20 DEG CELSIUS, fuel_grade_classification: JET A. This part is cataloged in the U.S.

Government catalog under NSN 9130-00-359-2026, 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
JAA
NSN: 9130-00-359-2026
FSC: 9130 — Liquid Propellants and Fuels, Petroleum Base
CAGE: 52838 — DLA ENERGY DBA DLA ENERGY (USA)
SPECIFICATIONS
density_value0.775 KILOGRAMS PER LITER MINIMUM AND 0.840 KILOGRAMS PER LITER MAXIMUM KG
nato_code_numberF24
special_featuresMRAP BUFFALO MK2A2
supply_classificationBULK
viscosity_at_rated_temp8.00 MAXIMUM -20 DEG CELSIUS
fuel_grade_classificationJET A
freezing_point_maximum_temp-40.0 DEG FAHRENHEIT
nondefinitive_spec/std_dataJET A TYPE
specification/standard_data81346-ASTMD-1655 MANUFACTURERS STANDARD
maximum_amount_of_existent_gum7.0
minimum_heat_of_combustion_value18400.0 BRITISH THERMAL UNITS PER POUND
maximum_sulphur_content_percentage_by_weight0.3
NSN9130-00-359-2026
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available TURBINE FUEL,AVIATION TITLE COMPONENT PN JAA MFR TURBINE FUEL,AVIATION
KEY FEATURES
•
SUPPLY CLASSIFICATION: BULK
•
MINIMUM HEAT OF COMBUSTION VALUE: 18400.0 BRITISH THERMAL UNITS PER POUND
•
MAXIMUM FATTY ACID METHYL ESTER (FAME) CONTENT IN MILLIGRAMS PER KILOGRAM: 50.00 MILLIGRAMS PER KILOGRAM MAXIMUM
•
MAXIMUM SULPHUR CONTENT PERCENTAGE BY WEIGHT: 0.3
•
NATO CODE NUMBER: F24
•
FREEZING POINT MAXIMUM TEMP: -40.0 DEG FAHRENHEIT
•
SPECIFICATION/STANDARD DATA: 81346-ASTMD-1655 MANUFACTURERS STANDARD
•
NONDEFINITIVE SPEC/STD DATA: JET A TYPE
TECHNICAL CHARACTERISTICS
SUPPLY CLASSIFICATIONBULK
MINIMUM HEAT OF COMBUSTION VALUE18400.0 BRITISH THERMAL UNITS PER POUND
MAXIMUM FATTY ACID METHYL ESTER (FAME) CONTENT IN MILLIGRAMS PER KILOGRAM50.00 MILLIGRAMS PER KILOGRAM MAXIMUM
MAXIMUM SULPHUR CONTENT PERCENTAGE BY WEIGHT0.3
NATO CODE NUMBERF24
FREEZING POINT MAXIMUM TEMP-40.0 DEG FAHRENHEIT
SPECIFICATION/STANDARD DATA81346-ASTMD-1655 MANUFACTURERS STANDARD
NONDEFINITIVE SPEC/STD DATAJET A TYPE
VISCOSITY AT RATED TEMP8.00 MAXIMUM -20 DEG CELSIUS
SPECIAL FEATURESMRAP BUFFALO MK2A2
SUBSTITUTES & CROSS-REFERENCES 2
ASTMD1655JETAReference document
Same NSN cross-reference
Reference document — Secondary reference
ASTM D1655Reference document
Same NSN cross-reference
Reference document — Design control — primary 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 JAA?
JAA is a TURBINE FUEL,AVIATION.
What parts can replace JAA?
There are 2 known substitutes for JAA: ASTMD1655JETA, ASTM D1655. Substitute compatibility should be verified for your specific system.
What is the NSN for JAA?
JAA is cataloged in the U.S. Government catalog under NSN 9130-00-359-2026. This indicates validated use in U.S. government and defense supply chains.
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