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2840-01-318-4855

Turbine Engine Fan Duct Boss Cover

2840013184855 013184855 4073899 2840PL0664377

2840-01-318-4855 COVER,FAN DUCT BOSS,TURBINE ENGINE 2840013184855 013184855

Managed by United States
NSN Created on 19 Apr 1990
Data Last Changed
November 2023
NATO Update Count
12
NATO Data Quality
2840-01-318-4855 COVER,FAN DUCT BOSS,TURBINE ENGINE 2840013184855 013184855 1/1
NSN 2840-01-318-4855 (Generic Image) 1/1

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2840-01-318-4855 Related Documents Related Documents 2840-01-318-4855 5+ Documents (More...)

2840-01-318-4856 2840013184856 013184856 is a metallic item of various shapes designed to reduce vibration and to secure a component part of an engine, gas turbine, aircraft to the engine case or housing as modified. for mounting accessories to the outside of the engine, see plate, mounting.
Turbine Engine Augmentor Nozzle Support 4071122RNCC: 5 | RNVC: 2 | MEDALS: Y | DAC: 5 19 Apr 1990 2840-01-318-4855
3120-01-385-6048 3120013856048 013856048 is an item of any peripheral shape usually having one flat or spherical surface and a centrally located hole. it is designed for applications involving moving (kinetic) loads. except for items fabricated from bearing quality synthetic (plastic) or composed of multilayer material, one bearing surface must either have a specific surface finish designation of 32 microinch (0.8 micrometre) or less, arithmetical average (aa) (arithmetic mean deviation) or one of the following conditions: be lapped or ground; have visible or detectable means of lubrication; grooves, indentations; or self-lubrication. the thickness must not exceed 25 percent of the outside diameter of the shortest distance between peripheral flats (when thickness and/or outside diameter is designated as a tolerance dimension, the maximum dimension will be used to determine compliance). excludes straight, tubular (without flange) items having a bearing surface(s) parallel to the axis of the bore only. see also washer, flat and spacer, sleeve.

2840-01-318-4855 Demil Restrictions 2840-01-318-4855

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

2840-01-318-4855 is a Turbine Engine Fan Duct Boss Cover 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.

2840-01-318-4855 HTS and ScheduleB Import and Export 2840-01-318-4855

2840-01-318-4855 End Users End Users 2840-01-318-4855

US Air Force (FXGG)
Effective Date:
1 Jul 2006
Former MOE Rule:
FXCX
Poland (WP01)
Effective Date:
1 Jun 2011
Singapore (YJ01)
Effective Date:
1 Jun 1996
Republic of Korea (ZH01)
Effective Date:
1 Oct 2002
Greece (ZU01)
Effective Date:
1 May 2008

2840-01-318-4855 Manufacturers Approved Sources 2840-01-318-4855

2840-01-318-4855 Technical Data Datasheet 2840-01-318-4855

Characteristic
Specifications
FIIG
A23900
End Item Identification [AGAV]
F100pw0229 Aircraft Engine
General Characteristics Item Description [TEXT]
O/A Dia. 2.810; O/A Width 0.310; Matl Aluminum Alloy,Ams 4027; Groove O/A Dia. 2.594; Groove O/A Width 0.16 5

2840-01-318-4855 Weapon Systems (WSDC) Weapon Systems (WSDC) 2840-01-318-4855

2840-01-318-4855 Stock, Inventory and Procurement DLA Procurement Analysis 2840-01-318-4855

Last Stock Position:
3 In Stock
DLA Administrative Lead Time:
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DLA Production Lead Time:
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2840-01-318-4855 Management Data Management Data 2840-01-318-4855

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Oct 2022
Department of the Air Force (DF)
EA
Subscribe
1
Oct 2021
Department of the Air Force (DF)
EA
Subscribe
1
Oct 2020
Department of the Air Force (DF)
EA
Subscribe
1
Oct 2019
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Fund:
SF
Stock fund applicable to items managed for the Air Force by the respective Inventory Control Point
Budget:
9
57X4921.070 - General Support DIV - Air Force decentralized managed expense items (ERRC XB3, XF3) with a unit cost of less than $250,000 that are requisitioned/procured at base (retail) level from DLA, GSA, Army, Navy, Depot Maintenance Service, Air Force Industrial Fund (AFMC), local manufacture and commercial vendors
Aggregation Code:
NZ
PRATT & WHITNEY JET ENGINES & COMPONENTS, F-100–P-100
Price Validation Code:
P
The current standard price is the initial negotiated provisioned price.
This is the price paid by DoD for the item as the result of price negotiation of the Provisioned Item Order (PIO) or other initial negotiated price.
ZOP or Standard Price challenges are permissible but should be supported with adequate justification.
Expendability
Recoverability
Repairability:
N
Expendable. Condemn at User. Stock Fund (except Munitions).

2840-01-318-4855 Related Items NATO Stock Numbers Related to 2840-01-318-4855

2840-01-318-4855 Freight Data Freight Information 2840-01-318-4855

2840-01-318-4855 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 133320. A Sub NMFC of X. It has a NMFC Description of MACHINERY PARTS OIL/FUEL FILTER. 2840-01-318-4855 is rated as class 70 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 64100 which rates the freight between FCL and LCL. 2840-01-318-4855 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 593 for ocean manifesting and military sealift. 2840-01-318-4855 is not classified as a special type of cargo when transported by water. 2840-01-318-4855 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.

2840-01-318-4855 Packaging Data Packaging Data 2840-01-318-4855

Responsible Activity
Packaging Data Source
Primary Inventory Control Activity (PICA)
--

Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation
--
--
Bare Metal Item
Over 10lb
Less than 85G
Special Requirement

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
1
--
--
--
--
Any Suitable Process
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
--
--
--
--
--
No special marking

Intermediate Pack Level

Quantity of Unit Packs
Container
ASTM - D5118, Fiberboard Box

2840-01-318-4855 Procurement History Procurement History 2840-01-318-4855 2 Records

Contract
Date
CAGE
Quantity
Net Price
Std Price
SPE4AX22F0533
20 Oct 2021
Subscribe
2
Subscribe
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SPE4AX22F0533
20 Oct 2021
Subscribe
2
Subscribe
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2840-01-318-4855 Contracting Technical Data File (CTDF) Contracting Technical Data File (CTDF) 2840-01-318-4855 October 2021

Criticality and Quality

Critical Item Code:
Flight Safety:
Life Support:
Certified Samples:
Serialization:
First Article Test (FAT):
Certificate of Quality Compliance:
Production Lot Testing:
Special Testing:
Qualified Products List (QPL):

Commercial Properties

Government Furnished Material:
Government Furnished Tooling:
Government Furnished Property:
Price Evaluation Code:
Diminshing Manufacturing Sources:
Warranty:
Commerical Off The Shelf (COTS):
End Item Application:
Auctioning Candidate:
Source of Procurement:
Contract Option:

Restrictions

Boeing Rights Guard:
Export Controlled:
Controlled Technical Data Package (TDP):
Restricted Technical Data Package (TDP):
Contains Classified Material
Weapons System Indicator Code (WSIC):
T

Packaging Requirements

Packaging Determination Table:
Packaging Review Code:
N
Special Packaging Instruction Number (SPIN):
Special Packaging Instruction Number Revision:
Special Packaging Instruction Number Date:
Pallet Reference Number Required: