9398M83 — FUEL CONTROL,MAIN,TURBINE ENGINE

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9398M83: FUEL CONTROL,MAIN,TURBINE ENGINE.

FUEL CONTROL,MAIN,TURBINE ENGINE. Key specifications include material: ALUMINUM ALLOY, end_item_identification: F110-GE-100 TURBO FAN AUGMENTED JET ENGINE, reference_data_and_literature: T.O.6J3-4-115-513 (TCTO);2J-F110-4,F.20,I.113, part_name_assigned_by_controlling_agency: MAIN ENGINE CONTROL, reference_number_differentiating_characteristics: AS DIFFERENTIATED BY SOURCE CONTROL DRAWING. This part is cataloged in the U.S.

Government catalog under NSN 2915-01-448-0588, 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

9398M83

NSN: 2915-01-448-0588
FSC: 2915 — Engine Fuel System Components, Aircraft and Missile Prime Movers
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY
end_item_identification	F110-GE-100 TURBO FAN AUGMENTED JET ENGINE
reference_data_and_literature	T.O.6J3-4-115-513 (TCTO);2J-F110-4,F.20,I.113
part_name_assigned_by_controlling_agency	MAIN ENGINE CONTROL
reference_number_differentiating_characteristics	AS DIFFERENTIATED BY SOURCE CONTROL DRAWING
NSN	2915-01-448-0588

COMPONENT DIAGRAM

KEY FEATURES

•

REFERENCE DATA AND LITERATURE: T.O.6J3-4-115-513 (TCTO);2J-F110-4,F.20,I.113

•

FUNCTIONAL DESCRIPTION: FUEL-METERING DEVICE USED ON TURBINE ENGINES THAT METERS THE PROPER QUANTITY OF FUEL TO BE FED INTO THE COMBUSTION CHAMBERS OF THE ENGINE.IT INTEGRATES THE PARAMETERS OF INLET AIR TEMPERATURE, COMPRESSOR SPEED, COMPRESSOR DISCHARGE PRESSURE, AND EXHAUST GAS TEMPERATURE WITH THE PROPER POSITION OF THE COCKPIT POWER CONTROL LEVER AND DEMANDS FROM THE ELECTRONIC ENGINE CONTROL SYSTEM

•

MATERIAL: ALUMINUM ALLOY

•

REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS: AS DIFFERENTIATED BY SOURCE CONTROL DRAWING

TECHNICAL CHARACTERISTICS

REFERENCE DATA AND LITERATURE	T.O.6J3-4-115-513 (TCTO);2J-F110-4,F.20,I.113
FUNCTIONAL DESCRIPTION	FUEL-METERING DEVICE USED ON TURBINE ENGINES THAT METERS THE PROPER QUANTITY OF FUEL TO BE FED INTO THE COMBUSTION CHAMBERS OF THE ENGINE.IT INTEGRATES THE PARAMETERS OF INLET AIR TEMPERATURE, COMPRESSOR SPEED, COMPRESSOR DISCHARGE PRESSURE, AND EXHAUST GAS TEMPERATURE WITH THE PROPER POSITION OF THE COCKPIT POWER CONTROL LEVER AND DEMANDS FROM THE ELECTRONIC ENGINE CONTROL SYSTEM
PART NAME ASSIGNED BY CONTROLLING AGENCY	MAIN ENGINE CONTROL
END ITEM IDENTIFICATION	F110-GE-100 TURBO FAN AUGMENTED JET ENGINE
MATERIAL	ALUMINUM ALLOY
REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS	AS DIFFERENTIATED BY SOURCE CONTROL DRAWING

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.

2915-00-001-2369 2915-00-001-2370 2915-00-001-2627 2915-00-001-4681 2915-00-001-5421 2915-00-001-5423 2915-00-001-9122 2915-00-001-9139

SUBSTITUTES & CROSS-REFERENCES 2

9398M83P19Reference document

Same NSN cross-reference

Reference document — Secondary reference

8062-672Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Terminal item — no further procurement; issued until stock is exhaustedDemilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 9398M83?

9398M83 is a FUEL CONTROL,MAIN,TURBINE ENGINE.

What parts can replace 9398M83?

There are 2 known substitutes for 9398M83: 9398M83P19, 8062-672. Substitute compatibility should be verified for your specific system.

What is the NSN for 9398M83?

9398M83 is cataloged in the U.S. Government catalog under NSN 2915-01-448-0588. This indicates validated use in U.S. government and defense supply chains.

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9398M83 — FUEL CONTROL,MAIN,TURBINE ENGINE

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