1620-14-556-2584

Landing Gear Strut Piston

1620145562584 145562584 T321A10T0006 C25094130-1

A cylinder, closed at the lower end, which telescopes within an outer shock strut cylinder assembly. It may contain an integral metering pin or hydraulic damping device to control the rate of compression and extension travel. A wheel axle, pivot fork, or provisions for the mounting of torque arms and towing eyes may be included. View more Landing Gear Strut Piston

1620-14-556-2584 PISTON,LANDING GEAR STRUT 1620145562584 145562584

Managed by France
NSN Created on 18 Feb 2008
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
1620-14-556-2584 PISTON,LANDING GEAR STRUT 1620145562584 145562584 1/1
NSN 1620-14-556-2584 (Generic Image) 1/1

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1620-14-556-2584 Landing Gear Strut Piston 1620145562584
T321A10T0006 C25094130-1 A cylinder, closed at the lower end, which telescopes within an outer shock
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1620-14-556-2584 is a Landing Gear Strut Piston

1620-14-556-2584 End Users End Users 1620-14-556-2584

Spain (YB)
Australia (ZA)
France (ZF)
Germany (ZG)

1620-14-556-2584 Manufacturers Approved Sources 1620-14-556-2584

Part Number
Manufacturer
Status
T321A10T0006
F0210 - Airbus Helicopters (Ets De (Active)
Source Control
RNCC 1 RNVC 2 DAC 2
C25094130-1
F0189 - Safran Landing Systems Ex Messier (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 4

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