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1680-01-338-1592
Aircraft Control Stick
1680013381592 013381592 17P1F6021-507 17P1F6021-1
A lever used for maintaining control of an aircraft about its pitch and roll axis. Excludes operation of trim tabs or the like. It is distinguished from a CONTROL COLUMN in that its side to side movement controls the aircraft about its roll axis. View more Aircraft Control Stick
Managed by United States
NSN Created on 26 Apr 1991
Data Last Changed
November 2023
November 2023
NATO Update Count
8
8
NATO Data Quality
Marketplace 1680-01-338-1592
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Related Documents 1680-01-338-1592 1+ Documents (More...)
17P1F6021-507 17P1F6021-1 A lever used for maintaining control of an aircraft about its pitch and roll
United States (US) 4. 1680-01-338-1592 Marketplace Restrictions Approved Sources Datasheet Management
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United States (US) 4. 1680-01-338-1592 Marketplace Restrictions Approved Sources Datasheet Management
Request a Quotation from participating marketplace vendors Request Updated Every Day 1680-01-338-1592
Restrictions 1680-01-338-1592
IUID Required
1680-01-338-1592 is a Aircraft Control Stick that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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.
Approved Sources 1680-01-338-1592
- Part Number
- Manufacturer
- Status
- 17P1F6021-507
- Manufacturer
- 88277 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
- 17P1F6021-1
- 88277 - The Boeing Company (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Management Data 1680-01-338-1592
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Jan 2014
- Department of the Air Force (DF)
- EA
- Subscribe
- 1
- EA
- MOE
- USC
- Code
- Statement
- Order of Use
- Jump To Code
- Qty Per Assy
- UOM
- Technical Document
- Quantative Expression
- Code
- Department of the Air Force (DF)
- I
- V
- Discontinued Without Replacement
- V
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