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2990-00-231-4807
Push-Pull Control Assembly
2990002314807 002314807 32-65251-4
A control consisting of a wire, wire rope, or a center load rail with ball bearings, within a flexible conduit. One end must have a threaded sleeve for mounting to a wall, bulkhead, or handle, or clevis. It is used to operate or control, either manually or mechanically a mechanical device. It may include such attaching devices as nut(s), washer(s), clevis, bracket(s), and/or the like. For items designed to transmit rotary motion, see SHAFT ASSEMBLY, FLEXIBLE. View more Push-Pull Control Assembly
January 2023
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Related Documents 2990-00-231-4807 1+ Documents (More...)
Control Assembly 2990002314807 32-65251-4 A control consisting of a wire, wire rope, or a center load
rail with ball bearings, within Every Day 2990-00-231-4807 RQST Updated Every Day 2990-00-231-4807 RQST
Restrictions 2990-00-231-4807
2990-00-231-4807 is a Push-Pull Control Assembly that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. This item does not contain a precious metal.
Import and Export 2990-00-231-4807
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 2990-00-231-4807
- Germany (ZG01)
- Effective Date:
- 1 Jan 2010
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 2990-00-231-4807
- Part Number
- Manufacturer
- Status
- 32-65251-4
- Manufacturer
- 76301 - The Boeing Company (Active)
- Primary Buy
- Primary Buy
Datasheet 2990-00-231-4807
- Characteristic
- Specifications
- FIIG
- Specifications
- A524C0
- Special Features [FEAT]
- Control Link From Left Cockpit Throttle To Engine
- End Item Identification [AGAV]
- F-4 Aircraft
- Part Name Assigned By Controlling Agency [CXCY]
- Tube Assembly Engine
Management Data 2990-00-231-4807
- Effective Date
- Organization
- Unit of Issue
- Unit Price
- Qty Unit Pack
- Unit of Issue
- Feb 2008
- 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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Freight Information 2990-00-231-4807
2990-00-231-4807 has freight characteristics managed by Germany.. 2990-00-231-4807 has a variance between NMFC and UFC when transported by rail and the description should be consulted.
Packaging Data 2990-00-231-4807
- Responsible Activity
- Packaging Data Source
- Primary Inventory Control Activity (PICA)
- Packaging Data does not meet current MIL-STD-2073-1E
Item Pack Level (Unpackaged)
- Item Size
- Item Weight
- Characteristics
- Weight/Dimensions Category
- Fragility
- Item Preservation
- Item Weight
- --
- --
- --
- --
- --
- --
Unit Pack Level (Packaged)
- Quantity per Pack
- Unit Size
- Unit Weight
- Unit Cube
- Preservation Method
- Cleaning/Drying
- Unit Size
- 1
- --
- --
- --
- Physical Protection
- Any Suitable Process
- --
- Preservation Material
- Wrapping Material
- Cushioning/Dunnage
- Cushioning Thickness
- Container
- Special Marking
- Wrapping Material
- No Requirement
- No Requirement
- No Requirement
- Not Applicable
- MIL-DTL-117, Type III, Class B, Style 2, Heavy Duty, Waterproof, Transparent Bag
- No special marking
- No Requirement
Intermediate Pack Level
- Quantity of Unit Packs
- Container
- --