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1620-01-503-1393

Landing Gear Cylinder And Piston Assembly

1620015031393 015031393 2021600-123

The main shock absorption portion of an aircraft landing gear, consisting of the main cylinder and piston and other associated parts. May be with or without axle(s). Excludes LANDING GEAR, FIXED and LANDING GEAR, RETRACTABLE. View more Landing Gear Cylinder And Piston Assembly

1620-01-503-1393 CYLINDER AND PISTON ASSEMBLY,LANDING GEAR 1620015031393 015031393

Managed by United States
NSN Created on 5 Dec 2002
Data Last Changed
May 2023
NATO Update Count
7
NATO Data Quality
1620-01-503-1393 CYLINDER AND PISTON ASSEMBLY,LANDING GEAR 1620015031393 015031393 1/1
NSN 1620-01-503-1393 (Generic Image) 1/1

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1620-01-503-1393 Related Documents Related Documents 1620-01-503-1393 4+ Documents (More...)

Documents 1620-01-539-8293 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-16/fsc-1620/us 1620-01-503-1393
Landing Gear Cylinder And Piston Assembly 1620-01-503-1393 1620015031393 015031393 is the main
DAC 5 Datasheet 5365-01-496-0714 CharacteristicSpecificationsFIIGA045A0Special Features [FEAT]Nha 2021600-123
1620-01-502-8988 1620015028988 015028988 is the main shock absorption portion of an aircraft landing gear, consisting of the main cylinder and piston and other associated parts. may be with or without axle(s). excludes landing gear, fixed and landing gear, retractable.
6214 Landing Gear Cylinder And Piston Assembly 9927116-30RNCC: 3 | RNVC: 2 | DAC: 2 7 Sep 1999 1620-01-503-1393

1620-01-503-1393 Demil Restrictions 1620-01-503-1393

DEMIL: B | DEMILI: 3 | CRITICALITY: F | HMIC: N | PMIC: A | EDC: | ADPEC: 0

IUID Required

1620-01-503-1393 is a Landing Gear Cylinder And Piston Assembly that is an aviation critical safety item or flight safety critical aircraft part. This item has been confirmed as a Critical Munitions List Item or a Sensitive Commerce Control List Item and cannot be in the possession of any party anywhere in the World who is not an authorized NATO Government. Any other possessor of this item should mutilate it now as possession violates international and local laws. This item is a US Munitions List Item and must be mutilated to scrap. This item is not suspected to be hazardous. This item does not contain a precious metal.

1620-01-503-1393 HTS and ScheduleB Import and Export 1620-01-503-1393

1620-01-503-1393 End Users End Users 1620-01-503-1393

US Air Force (FLL4)
Effective Date:
1 Dec 2002

1620-01-503-1393 Manufacturers Approved Sources 1620-01-503-1393

1620-01-503-1393 Technical Data Datasheet 1620-01-503-1393

Characteristic
Specifications
FIIG
A525C0
End Item Identification [AGAV]
F-22 Raptor
Part Name Assigned By Controlling Agency [CXCY]
Shock Strut Assy

1620-01-503-1393 Management Data Management Data 1620-01-503-1393

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Jun 2022
Department of the Air Force (DF)
EA
Subscribe
1
Dec 2011
Department of the Air Force (DF)
EA
Subscribe
1
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Air Force (DF)
L
F
When Exhausted Use 1620-01-539-8293
Department of the Air Force (DF)
L
R
Refer To Afto95req
AFTO95REQ

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
FR
F-22 AIRCRAFT
Price Validation Code:
N
The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of ā€œLā€ or ā€œFā€, then it must be evaluated locally where purchased or fabricated.
Expendability
Recoverability
Repairability:
T
Expendable. Reparable. Condemn at Depot. AF Recoverable Assembly Management System (AFRAMS).

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1620-01-503-1393 Freight Data Freight Information 1620-01-503-1393

1620-01-503-1393 has freight characteristics.. 1620-01-503-1393 has a variance between NMFC and UFC when transported by rail and the description should be consulted.