104030-3 — PUMP,FUEL,JET ENGINE

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

104030-3: PUMP,FUEL,JET ENGINE.

The PUMP,FUEL,JET ENGINE is a the manufacturer industrial component. Key specifications include overall_width: 2.205 INCHES MAXIMUM IN, overall_height: 4.085 INCHES MAXIMUM IN, pressure_rating: ERR-060, special_features: SPLINE SHAFT DRIVEN, fsc_application_data: ENGINE FUEL SYSTEM COMPONENT,NON AIRCRAFT, end_item_identification: FUEL CONTROL, STARTING, TURBINE ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2915-01-055-6515, 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

104030-3

NSN: 2915-01-055-6515
FSC: 2915 — Engine Fuel System Components, Aircraft and Missile Prime Movers
CAGE: 55820 — RTX CORPORATION DIV PRATT & WHITNEY (USA)

SPECIFICATIONS

overall_width	2.205 INCHES MAXIMUM IN
overall_height	4.085 INCHES MAXIMUM IN
pressure_rating	ERR-060
special_features	SPLINE SHAFT DRIVEN
fsc_application_data	ENGINE FUEL SYSTEM COMPONENT,NON AIRCRAFT
end_item_identification	FUEL CONTROL, STARTING, TURBINE ENGINE
general_characteristics_item_description	ANODIZED ALUMINUM CASTING PER MIL-A-8625 TYPE I
reference_number_differentiating_characteristics	AS DIFFERENTIATED BY SOURCE CONTROL DRAWING 102-203-5
NSN	2915-01-055-6515

COMPONENT DIAGRAM

KEY FEATURES

•

FSC APPLICATION DATA: ENGINE FUEL SYSTEM COMPONENT,NON AIRCRAFT

•

GENERAL CHARACTERISTICS ITEM DESCRIPTION: ANODIZED ALUMINUM CASTING PER MIL-A-8625 TYPE I

•

SPECIAL TEST FEATURES: OPERATING CONDITIONS: SPEED NOMINAL 4200 RPM; BOOST PRESSURE: 5 PSI ABOVE TRUE VAPOR PRESSURE OF THE FUEL TO THE MAXIMUM WORKING PRESSURE OF 90 PSIA; FUEL TEMPERATURE: -65 DEGREES FAHRENHEIT TO +200 DEGREES FAHRENHEIT; AMBIENT TEMPERATURE: -65 DEGREES FAHRENHEIT TO +250 DEGREES FAHRENHEIT; EXTERNAL SPLINE DATA: PITCH: 48/96; PRESSURE ANGLE: 45 DEGREES; NUMBER OF TEETH: 11; PITCH DIAMTER: .2292; BASE DIAMETER: .1621; MAJOR DIAMETER: .2470-.2500; MINOR DIAMETER: .2013-.2083; TOOTH THICKNESS MAXIMUM EFFECTIVE: .0369; TOOTH THICKNESS MINIMUM ACTUAL: .0317; TOOTH THICKNESS, MAS ACTUAL: .0329 RPM

•

PRESSURE RATING: ERR-060

TECHNICAL CHARACTERISTICS

OVERALL HEIGHT	4.085 INCHES MAXIMUM IN
FSC APPLICATION DATA	ENGINE FUEL SYSTEM COMPONENT,NON AIRCRAFT
GENERAL CHARACTERISTICS ITEM DESCRIPTION	ANODIZED ALUMINUM CASTING PER MIL-A-8625 TYPE I
SPECIAL TEST FEATURES	OPERATING CONDITIONS: SPEED NOMINAL 4200 RPM; BOOST PRESSURE: 5 PSI ABOVE TRUE VAPOR PRESSURE OF THE FUEL TO THE MAXIMUM WORKING PRESSURE OF 90 PSIA; FUEL TEMPERATURE: -65 DEGREES FAHRENHEIT TO +200 DEGREES FAHRENHEIT; AMBIENT TEMPERATURE: -65 DEGREES FAHRENHEIT TO +250 DEGREES FAHRENHEIT; EXTERNAL SPLINE DATA: PITCH: 48/96; PRESSURE ANGLE: 45 DEGREES; NUMBER OF TEETH: 11; PITCH DIAMTER: .2292; BASE DIAMETER: .1621; MAJOR DIAMETER: .2470-.2500; MINOR DIAMETER: .2013-.2083; TOOTH THICKNESS MAXIMUM EFFECTIVE: .0369; TOOTH THICKNESS MINIMUM ACTUAL: .0317; TOOTH THICKNESS, MAS ACTUAL: .0329 RPM
OVERALL WIDTH	2.205 INCHES MAXIMUM IN
PRESSURE RATING	ERR-060
SPECIAL FEATURES	SPLINE SHAFT DRIVEN
END ITEM IDENTIFICATION	FUEL CONTROL, STARTING, TURBINE ENGINE
REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS	AS DIFFERENTIATED BY SOURCE CONTROL DRAWING 102-203-5

OTHER ITEMS IN FSC 2915 — Engine Fuel System Components, Aircraft and Missile Prime Movers

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

2915-00-037-7971 2915-00-037-8234 2915-00-124-0534 2915-00-166-4957 2915-00-650-8936 2915-00-705-9720 2915-01-484-4365 2915-01-551-1643

SUBSTITUTES & CROSS-REFERENCES 1

4102-203005Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Insurance item — stocked against contingency demandNo demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 104030-3?

104030-3 is a PUMP,FUEL,JET ENGINE.

What parts can replace 104030-3?

There is 1 known substitute for 104030-3: 4102-203005. Substitute compatibility should be verified for your specific system.

What is the NSN for 104030-3?

104030-3 is cataloged in the U.S. Government catalog under NSN 2915-01-055-6515. This indicates validated use in U.S. government and defense supply chains.

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104030-3 — PUMP,FUEL,JET ENGINE

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