ST7M342 — RING,PISTON

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

ST7M342: 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

ST7M342

NSN: 2805-01-153-1655
NIINs: 011531655, 011603722
FSC: 2805 — Gasoline Reciprocating Engines, Except Aircraft; and Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (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	0.0880 INCHES MINIMUM AND 0.0980 INCHES MAXIMUM IN
standard_bore_diameter	1.000 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

FR84C24PReference document

Same NSN cross-reference

Reference document — Advisory reference — outside the item-of-supply concept

10106399Reference document

Same NSN cross-reference

Reference document — Informative 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 ST7M342?

ST7M342 is a RING,PISTON.

What parts can replace ST7M342?

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

What is the NSN for ST7M342?

ST7M342 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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