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1620-01-454-6651

Landing Systems Trunnion Strut

1620014546651 014546651 17P2C1100-506

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

1620-01-454-6651 TRUNNION STRUT,LANDING SYSTEMS 1620014546651 014546651

Managed by United States
NSN Created on 8 Apr 1998
Data Last Changed
January 2023
NATO Update Count
5
NATO Data Quality
1620-01-454-6651 TRUNNION STRUT,LANDING SYSTEMS 1620014546651 014546651 1/1
NSN 1620-01-454-6651 (Generic Image) 1/1

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1620-01-454-6651 Related Documents Related Documents 1620-01-454-6651 2+ Documents (More...)

United States (US) 4. 1620-01-454-6651 Marketplace Restrictions Approved Sources Datasheet Management
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RQST NE Updated Every Day 1620-01-454-6651 RQST Updated Every Day 1620-01-454-6651 RQST NE Restrictions
AssyUOMTechnical DocumentQuantative ExpressionDepartment of the Air Force (DF)LFWhen Exhausted Use 1620-01-454-6651

1620-01-454-6651 Demil Restrictions 1620-01-454-6651

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

IUID Required

1620-01-454-6651 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.

1620-01-454-6651 HTS and ScheduleB Import and Export 1620-01-454-6651

1620-01-454-6651 End Users End Users 1620-01-454-6651

US Air Force (FBB4)
Effective Date:
1 Oct 1999
Former MOE Rule:
FEE4
Canada (ZC01)
Effective Date:
1 Mar 2011

1620-01-454-6651 Manufacturers Approved Sources 1620-01-454-6651

1620-01-454-6651 Technical Data Datasheet 1620-01-454-6651

Characteristic
Specifications
FIIG
A23900
Material [MATT]
Steel
Overall Length [ABHP]
35.000 Inches Nominal
Overall Width [ABMK]
16.000 Inches Nominal
Overall Height [ABKW]
8.500 Inches Nominal
End Item Identification [AGAV]
C-17 Aircraft

1620-01-454-6651 Management Data Management Data 1620-01-454-6651

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Oct 2018
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
7
Substitute For 1620-01-549-6658
AAA
Department of the Air Force (DF)
L
Dod I&S Family Master Nsn - - -
ABA

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
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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1620-01-454-6651 Freight Data Freight Information 1620-01-454-6651

1620-01-454-6651 has freight characteristics.. 1620-01-454-6651 has a variance between NMFC and UFC when transported by rail and the description should be consulted.