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2840-01-130-2407

Aircraft Gas Turbine Engine Diffuser Case

2840011302407 011302407 4059312

A case that is an integral part of an ENGINE, GAS TURBINE, AIRCRAFT, designed to surround and protect a DIFFUSER, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Diffuser Case

2840-01-130-2407 CASE,DIFFUSER,AIRCRAFT GAS TURBINE ENGINE 2840011302407 011302407

Managed by United States
NSN Created on 18 Apr 1982
Data Last Changed
January 2023
NATO Update Count
35
NATO Data Quality
2840-01-130-2407 CASE,DIFFUSER,AIRCRAFT GAS TURBINE ENGINE 2840011302407 011302407 1/1
NSN 2840-01-130-2407 (Generic Image) 1/1

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4059312 A case that is an integral part of an ENGINE, GAS TURBINE, AIRCRAFT, designed to surround and
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2840-01-130-2407 Demil Restrictions 2840-01-130-2407

DEMIL: B | DEMILI: 3 | CRITICALITY: F | HMIC: N | PMIC: A | EDC: | ADPEC:

2840-01-130-2407 is a Aircraft Gas Turbine Engine Diffuser Case that is an aviation critical safety item or flight safety critical aircraft part. 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 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.

2840-01-130-2407 HTS and ScheduleB Import and Export 2840-01-130-2407

2840-01-130-2407 End Users End Users 2840-01-130-2407

Belgium (ZB01)
Effective Date:
28 Apr 2003
Republic of Korea (ZH01)
Effective Date:
1 Apr 1991
Denmark (ZS01)
Effective Date:
1 Sep 2005

2840-01-130-2407 Manufacturers Approved Sources 2840-01-130-2407

2840-01-130-2407 Technical Data Datasheet 2840-01-130-2407

Characteristic
Specifications
FIIG
A10700
End Item Identification [AGAV]
F100-Pw-100/200 Aircraft Gas Turbine Engine
Design Type [APGF]
Axial Compressor
Diameter [ABMZ]
28.245 Inches Minimum And 28.265 Inches Maximum
Engine Section Location [CZBJ]
Diffuser
Hardness Rating [CQFM]
36.0 Rockwell C Nominal Outer Case
Overall Length [ABHP]
17.818 Inches Minimum And 17.822 Inches Maximum
Part Name Assigned By Controlling Agency [CXCY]
Original Name Case,Combustion Chamber,Aircraft Gas Turbine Engine

2840-01-130-2407 Related Items NATO Stock Numbers Related to 2840-01-130-2407

2840-01-130-2407 Freight Data Freight Information 2840-01-130-2407

2840-01-130-2407 has freight characteristics.. 2840-01-130-2407 has a variance between NMFC and UFC when transported by rail and the description should be consulted.

2840-01-130-2407 Packaging Data Packaging Data 2840-01-130-2407

Responsible Activity
Packaging Data Source
Primary Inventory Control Activity (PICA)
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Item Pack Level (Unpackaged)

Item Size
Item Weight
Characteristics
Weight/Dimensions Category
Fragility
Item Preservation
32.0" H x 32.0" W x 21.0" L
--
--
Over 10lb
Less than 85G
No Requirement

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
--
38.2" H x 38.2" W x 29.7" L
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--
--
Special Requirements
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
No Requirement
Special Requirements – see Specific Instructions or Drawings provided
Special Requirements. See Specific Instructions or Drawings Provided
Special Requirements. See Specific Instructions or Drawings Provided
Special requirement – See specific instructions or drawings provided
Special requirements

Intermediate Pack Level

Quantity of Unit Packs
Container
--
No Requirement