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1620-01-518-0007

Landing Systems Trunnion Strut

1620015180007 015180007 17P2C7875-1

A machined casting used to anchor various aircraft systems to withstand impact with landing surfaces. It is used on such systems as landing gear, arresting gear, nose wheel steering, and the like, but is so constructed that it may pivot forward and backward. View more Landing Systems Trunnion Strut

1620-01-518-0007 TRUNNION STRUT,LANDING SYSTEMS 1620015180007 015180007

Managed by United States
NSN Created on 26 Feb 2004
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
1620-01-518-0007 TRUNNION STRUT,LANDING SYSTEMS 1620015180007 015180007 1/1
NSN 1620-01-518-0007 (Generic Image) 1/1

1620-01-518-0007 Stock and Availability Marketplace 1620-01-518-0007

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1620-01-518-0007 Demil Restrictions 1620-01-518-0007

DEMIL: Q | DEMILI: 3 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: | ADPEC: 0

1620-01-518-0007 is a Landing Systems Trunnion Strut that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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 confirmed Commerce Control List Item (CCLI). This item is not suspected to be hazardous. This item does not contain a precious metal.

1620-01-518-0007 HTS and ScheduleB Import and Export 1620-01-518-0007

1620-01-518-0007 End Users End Users 1620-01-518-0007

US Air Force (FBB5)
Effective Date:
1 Feb 2004
NATO Maintenance and Supply Agency (ZX01)
Effective Date:
1 Jan 2014

1620-01-518-0007 Manufacturers Approved Sources 1620-01-518-0007

1620-01-518-0007 Technical Data Datasheet 1620-01-518-0007

Characteristic
Specifications
FIIG
A23900
Material [MATT]
Steel Corrosion Resisting
Overall Length [ABHP]
1.755 Inches Nominal
Overall Height [ABKW]
1.265 Inches Nominal
Overall Diameter [ADAV]
1.000 Inches Nominal
Special Features [FEAT]
Material Descripton;Bar,Cres;Material Spec Ams 5659
End Item Identification [AGAV]
C-17 Aircraft
Part Name Assigned By Controlling Agency [CXCY]
Trunnion,Lwr-Door Link,Stabstrut

1620-01-518-0007 Management Data Management Data 1620-01-518-0007

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Nov 2018
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
Price Validation Code:
E
The current standard price is an estimated price.
Estimated Price challenges are allowed but follow procedures in para 60.b. (3) of section L of this manual.
This code will be changed to a P code upon notification of a contract price or this code will be changed to an updated code upon determination of a valid price.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

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1620-01-518-0007 Freight Data Freight Information 1620-01-518-0007

1620-01-518-0007 has freight characteristics.. 1620-01-518-0007 has a variance between NMFC and UFC when transported by rail and the description should be consulted.