2MLV21121-0005 — LANDING GEAR,RETRACTABLE

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

2MLV21121-0005: LANDING GEAR,RETRACTABLE.

The LANDING GEAR,RETRACTABLE is a the manufacturer industrial component. Key specifications include design_type: MAIN LANDING GEAR, special_features: LANDING/ARRESTMENT GEAR, end_item_identification: F-35 AIRCRAFT, aircraft_for_which_designed: F-35, criticality_code_justification: FEAT, gear_extension_and_retraction_method: HYDRAULIC CYLINDER. This part is cataloged in the U.S.

Government catalog under NSN 1620-01-650-7657, 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

2MLV21121-0005

NSN: 1620-01-650-7657
FSC: 1620 — Aircraft Landing Gear Components
CAGE: 81755 — LOCKHEED MARTIN CORPORATION DIV LOCKHEED MARTIN AERONAUTICS COMPANY (USA)

SPECIFICATIONS

design_type	MAIN LANDING GEAR
special_features	LANDING/ARRESTMENT GEAR
end_item_identification	F-35 AIRCRAFT
aircraft_for_which_designed	F-35
wheel_quantity_accommodated	1
criticality_code_justification	FEAT
gear_extension_and_retraction_method	HYDRAULIC CYLINDER
part_name_assigned_by_controlling_agency	MAIN LANDING GEAR ASSEMBLY-STOVL, LEFT HAND SIDE
landing_shock_absorption_and_dissipation_method	AIR/OIL SHOCK STRUT
NSN	1620-01-650-7657

COMPONENT DIAGRAM

KEY FEATURES

•

WHEEL QUANTITY ACCOMMODATED: 1

•

DESIGN TYPE: MAIN LANDING GEAR

•

CRITICALITY CODE JUSTIFICATION: FEAT

•

GEAR EXTENSION AND RETRACTION METHOD: HYDRAULIC CYLINDER

•

AIRCRAFT FOR WHICH DESIGNED: F-35

TECHNICAL CHARACTERISTICS

WHEEL QUANTITY ACCOMMODATED	1
DESIGN TYPE	MAIN LANDING GEAR
CRITICALITY CODE JUSTIFICATION	FEAT
SPECIAL FEATURES	LANDING/ARRESTMENT GEAR
GEAR EXTENSION AND RETRACTION METHOD	HYDRAULIC CYLINDER
PART NAME ASSIGNED BY CONTROLLING AGENCY	MAIN LANDING GEAR ASSEMBLY-STOVL, LEFT HAND SIDE
END ITEM IDENTIFICATION	F-35 AIRCRAFT
AIRCRAFT FOR WHICH DESIGNED	F-35
LANDING SHOCK ABSORPTION AND DISSIPATION METHOD	AIR/OIL SHOCK STRUT

OTHER ITEMS IN FSC 1620 — Aircraft Landing Gear Components

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

1620-00-491-0877 1620-00-699-0282 1620-00-718-6770 1620-00-736-1020 1620-00-756-9181

SUBSTITUTES & CROSS-REFERENCES 1

2649A4001-13Reference document

Same NSN cross-reference

Reference document — Secondary reference

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 2MLV21121-0005?

2MLV21121-0005 is a LANDING GEAR,RETRACTABLE.

What parts can replace 2MLV21121-0005?

There is 1 known substitute for 2MLV21121-0005: 2649A4001-13. Substitute compatibility should be verified for your specific system.

What is the NSN for 2MLV21121-0005?

2MLV21121-0005 is cataloged in the U.S. Government catalog under NSN 1620-01-650-7657. This indicates validated use in U.S. government and defense supply chains.

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2MLV21121-0005 — LANDING GEAR,RETRACTABLE

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