1128HM40111-11 — LEVER,REMOTE CONTROL

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1128HM40111-11: LEVER,REMOTE CONTROL.

The LEVER,REMOTE CONTROL is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, style_designator: CLEVIS LINK END, SECURING HOLE(S) SHAFT END, link_end_thickness: 0.627 INCHES MINIMUM AND 0.633 INCHES MAXIMUM IN, shaft_end_thickness: 0.500 INCHES MINIMUM AND 0.505 INCHES MAXIMUM IN, link_end_hole_diameter: 0.189 INCHES MINIMUM AND 0.191 INCHES MAXIMUM IN, end_item_identification: GRUMMAN MODEL EA-6B AIRCRAFT. This part is cataloged in the U.S.

Government catalog under NSN 1680-00-409-9506, 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

1128HM40111-11

NSN: 1680-00-409-9506
FSC: 1680 — Miscellaneous Aircraft Accessories and Components
CAGE: 79RG9 — NORTHROP GRUMMAN SYSTEMS CORPORATION (USA)

SPECIFICATIONS

material	ALUMINUM ALLOY
style_designator	CLEVIS LINK END, SECURING HOLE(S) SHAFT END
link_end_thickness	0.627 INCHES MINIMUM AND 0.633 INCHES MAXIMUM IN
shaft_end_thickness	0.500 INCHES MINIMUM AND 0.505 INCHES MAXIMUM IN
link_end_hole_diameter	0.189 INCHES MINIMUM AND 0.191 INCHES MAXIMUM IN
end_item_identification	GRUMMAN MODEL EA-6B AIRCRAFT
distance_between_fork_inside_spread	0.441 INCHES MINIMUM AND 0.447 INCHES MAXIMUM IN
material_document_and_classification	QQ-A-225/9, ALLOY 7075, T7351 FED SPEC SINGLE MATERIAL RESPONSE
center_to_center_distance_between_link_and_shaft_holes	2.620 INCHES MINIMUM AND 2.630 INCHES MAXIMUM IN
NSN	1680-00-409-9506

COMPONENT DIAGRAM

KEY FEATURES

•

LINK END THICKNESS: 0.627 INCHES MINIMUM AND 0.633 INCHES MAXIMUM IN

•

LINK END HOLE DIAMETER: 0.189 INCHES MINIMUM AND 0.191 INCHES MAXIMUM IN

•

SHAFT END THICKNESS: 0.500 INCHES MINIMUM AND 0.505 INCHES MAXIMUM IN

•

STYLE DESIGNATOR: CLEVIS LINK END, SECURING HOLE(S) SHAFT END

•

MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-225/9, ALLOY 7075, T7351 FED SPEC SINGLE MATERIAL RESPONSE

•

DISTANCE BETWEEN FORK INSIDE SPREAD: 0.441 INCHES MINIMUM AND 0.447 INCHES MAXIMUM IN

•

CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES: 2.620 INCHES MINIMUM AND 2.630 INCHES MAXIMUM IN

TECHNICAL CHARACTERISTICS

LINK END THICKNESS	0.627 INCHES MINIMUM AND 0.633 INCHES MAXIMUM IN
LINK END HOLE DIAMETER	0.189 INCHES MINIMUM AND 0.191 INCHES MAXIMUM IN
SHAFT END THICKNESS	0.500 INCHES MINIMUM AND 0.505 INCHES MAXIMUM IN
STYLE DESIGNATOR	CLEVIS LINK END, SECURING HOLE(S) SHAFT END
MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-225/9, ALLOY 7075, T7351 FED SPEC SINGLE MATERIAL RESPONSE
DISTANCE BETWEEN FORK INSIDE SPREAD	0.441 INCHES MINIMUM AND 0.447 INCHES MAXIMUM IN
CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES	2.620 INCHES MINIMUM AND 2.630 INCHES MAXIMUM IN
END ITEM IDENTIFICATION	GRUMMAN MODEL EA-6B AIRCRAFT
MATERIAL	ALUMINUM ALLOY

SUBSTITUTES & CROSS-REFERENCES 1

1128HM40111Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 1128HM40111-11?

1128HM40111-11 is a LEVER,REMOTE CONTROL.

What parts can replace 1128HM40111-11?

There is 1 known substitute for 1128HM40111-11: 1128HM40111. Substitute compatibility should be verified for your specific system.

What is the NSN for 1128HM40111-11?

1128HM40111-11 is cataloged in the U.S. Government catalog under NSN 1680-00-409-9506. This indicates validated use in U.S. government and defense supply chains.

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1128HM40111-11 — LEVER,REMOTE CONTROL

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