FR84C24P — RING,PISTON

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

FR84C24P: RING,PISTON.

The RING,PISTON is a the manufacturer industrial component. Key specifications include material: STEEL CORROSION RESISTING OVERALL, ring_style: CONCENTRIC, joint_style: VERTICAL JOINT, overall_width: 0.0590 INCHES MINIMUM AND 0.0600 INCHES MAXIMUM IN, special_features: WEAPON SYSTEM ESSENTIAL, fsc_application_data: LAUNCHER,GUIDED MISSILE,AIRCRAFT LAU-116/A. This part is cataloged in the U.S.

Government catalog under NSN 2805-01-153-1655, 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

FR84C24P

NSN: 2805-01-153-1655
FSC: 2805 — Gasoline Reciprocating Engines, Except Aircraft; and Components
CAGE: 84596 — AVIATION MANUFACTURING GROUP, LLC DBA THE FREEMAN COMPANY (USA)

SPECIFICATIONS

material	STEEL CORROSION RESISTING OVERALL
ring_style	CONCENTRIC
joint_style	VERTICAL JOINT
overall_width	0.0590 INCHES MINIMUM AND 0.0600 INCHES MAXIMUM IN
special_features	WEAPON SYSTEM ESSENTIAL
fsc_application_data	LAUNCHER,GUIDED MISSILE,AIRCRAFT LAU-116/A
radial_wall_thickness	0.0600 INCHES MINIMUM AND 0.0700 INCHES MAXIMUM IN
standard_bore_diameter	2.000 INCHES IN
end_item_identification	F/A-18 HORNET AIRCRAFT
cross-sectional_shape_style	PLAIN RECTANGULAR, STRAIGHT FACE
criticality_code_justification	FEAT
NSN	2805-01-153-1655

COMPONENT DIAGRAM

KEY FEATURES

•

FSC APPLICATION DATA: LAUNCHER,GUIDED MISSILE,AIRCRAFT LAU-116/A

•

CRITICALITY CODE JUSTIFICATION: FEAT

•

CROSS-SECTIONAL SHAPE STYLE: PLAIN RECTANGULAR, STRAIGHT FACE

•

JOINT STYLE: VERTICAL JOINT

•

RADIAL WALL THICKNESS: 0.0600 INCHES MINIMUM AND 0.0700 INCHES MAXIMUM IN

•

RING STYLE: CONCENTRIC

TECHNICAL CHARACTERISTICS

FSC APPLICATION DATA	LAUNCHER,GUIDED MISSILE,AIRCRAFT LAU-116/A
CRITICALITY CODE JUSTIFICATION	FEAT
OVERALL WIDTH	0.0590 INCHES MINIMUM AND 0.0600 INCHES MAXIMUM IN
CROSS-SECTIONAL SHAPE STYLE	PLAIN RECTANGULAR, STRAIGHT FACE
JOINT STYLE	VERTICAL JOINT
RADIAL WALL THICKNESS	0.0600 INCHES MINIMUM AND 0.0700 INCHES MAXIMUM IN
RING STYLE	CONCENTRIC
SPECIAL FEATURES	WEAPON SYSTEM ESSENTIAL
STANDARD BORE DIAMETER	2.000 INCHES IN
END ITEM IDENTIFICATION	F/A-18 HORNET AIRCRAFT

SUBSTITUTES & CROSS-REFERENCES 5

10106399Reference document

Same NSN cross-reference

Reference document — Informative reference only

ST7M342Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

J8-995Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

DW8015C24Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

ST7M342C24Same 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 FR84C24P?

FR84C24P is a RING,PISTON.

What parts can replace FR84C24P?

There are 5 known substitutes for FR84C24P: 10106399, ST7M342, J8-995 and 2 more. Substitute compatibility should be verified for your specific system.

What is the NSN for FR84C24P?

FR84C24P is cataloged in the U.S. Government catalog under NSN 2805-01-153-1655. This indicates validated use in U.S. government and defense supply chains.

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FR84C24P — RING,PISTON

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