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MIL-DTL-5624 — TURBINE FUEL,AVIATION

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

MIL-DTL-5624: TURBINE FUEL,AVIATION.

The TURBINE FUEL,AVIATION is a the manufacturer industrial component. Key specifications include nato_code_number: F44, special_features: JP8 WITHOUT FSII, supply_classification: BULK, viscosity_at_rated_temp: 8.50 MAXIMUM -20 DEG CELSIUS, fuel_grade_classification: JP-5, freezing_point_maximum_temp: -51.0 DEG FAHRENHEIT. This part is cataloged in the U.S.

Government catalog under NSN 9130-00-256-8613, 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
MIL-DTL-5624
NSN: 9130-00-256-8613
NIINs: 002568613, 002568617, 002732379, 002732380, 014999521, 015487337, 016118268
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
nato_code_numberF44
special_featuresJP8 WITHOUT FSII
supply_classificationBULK
viscosity_at_rated_temp8.50 MAXIMUM -20 DEG CELSIUS
fuel_grade_classificationJP-5
freezing_point_maximum_temp-51.0 DEG FAHRENHEIT
nondefinitive_spec/std_dataJP-5 GRADE
maximum_amount_of_existent_gum7.0
minimum_heat_of_combustion_value18300.0 BRITISH THERMAL UNITS PER POUND
specific_gravity_value_at_15.56_deg_celsius36.000 MINIMUM AND 48.000 MAXIMUM
maximum_sulphur_content_percentage_by_weight0.3
NSN9130-00-256-8613
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available TURBINE FUEL,AVIATION TITLE COMPONENT PN MIL-DTL-5624 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
•
REID VAPOR PRESSURE RATING: 14.0 KILOPASCALS (KPA) MINIMUM AND 21.0 KILOPASCALS (KPA) MAXIMUM
•
NATO CODE NUMBER: F40
•
FREEZING POINT MAXIMUM TEMP: -50.0 DEG CELSIUS
•
NONDEFINITIVE SPEC/STD DATA: JP-4 GRADE
•
FUEL GRADE CLASSIFICATION: JP-4
TECHNICAL CHARACTERISTICS
SUPPLY CLASSIFICATIONBULK
MINIMUM HEAT OF COMBUSTION VALUE42.8 MEGAJOULES PER KILOGRAM
MAXIMUM SULPHUR CONTENT PERCENTAGE BY WEIGHT0.3
REID VAPOR PRESSURE RATING14.0 KILOPASCALS (KPA) MINIMUM AND 21.0 KILOPASCALS (KPA) MAXIMUM
NATO CODE NUMBERF40
FREEZING POINT MAXIMUM TEMP-50.0 DEG CELSIUS
NONDEFINITIVE SPEC/STD DATAJP-4 GRADE
FUEL GRADE CLASSIFICATIONJP-4
DENSITY VALUE0.751 KILOGRAMS PER LITER MINIMUM AND 0.802 KILOGRAMS PER LITER MAXIMUM KG
MAXIMUM AMOUNT OF EXISTENT GUM7.0
SUBSTITUTES & CROSS-REFERENCES 2
JP4Reference document
Same NSN cross-reference
Reference document — Secondary reference
MILT5624Reference document
Same NSN cross-reference
Reference document — Secondary 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 MIL-DTL-5624?
MIL-DTL-5624 is a TURBINE FUEL,AVIATION.
What parts can replace MIL-DTL-5624?
There are 2 known substitutes for MIL-DTL-5624: JP4, MILT5624. Substitute compatibility should be verified for your specific system.
What is the NSN for MIL-DTL-5624?
MIL-DTL-5624 is cataloged in the U.S. Government catalog under NSN 9130-00-256-8613. This indicates validated use in U.S. government and defense supply chains.
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