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2840-01-422-1998

Aircraft Gas Turbine Engine Turbine Rotor Blade

2840014221998 014221998 A8A2742

An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT. View more Aircraft Gas Turbine Engine Turbine Rotor Blade

2840-01-422-1998 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840014221998 014221998

Managed by United States
NSN Created on 24 Nov 1995
Data Last Changed
January 2023
NATO Update Count
3
NATO Data Quality
2840-01-422-1998 BLADE,TURBINE ROTOR,AIRCRAFT GAS TURBINE ENGINE 2840014221998 014221998 1/1
NSN 2840-01-422-1998 (Generic Image) 1/1

2840-01-422-1998 Stock and Availability Marketplace 2840-01-422-1998

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2840-01-422-1998 Related Documents Related Documents 2840-01-422-1998 1+ Documents (More...)

A8A2742 An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
United States (US) 4. 2840-01-422-1998 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 2840-01-422-1998 RQST Updated Every Day 2840-01-422-1998 RQST NE Related Documents

2840-01-422-1998 Demil Restrictions 2840-01-422-1998

DEMIL: A | DEMILI: | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC: 0

IUID Required

2840-01-422-1998 is a Aircraft Gas Turbine Engine Turbine Rotor Blade that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. 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.

2840-01-422-1998 HTS and ScheduleB Import and Export 2840-01-422-1998

2840-01-422-1998 End Users End Users 2840-01-422-1998

US Air Force (FBB4)
Effective Date:
1 Nov 1999
Former MOE Rule:
FEE4

2840-01-422-1998 Manufacturers Approved Sources 2840-01-422-1998

2840-01-422-1998 Technical Data Datasheet 2840-01-422-1998

Characteristic
Specifications
FIIG
A10700
Design Type [APGF]
Axial Compressor
Engine Section Location [CZBJ]
Low Pressure Turbine
Stage Number [CZCJ]
6
Blade Attachment Method [BGLW]
Lock
Criticality Code Justification [CRTL]
Agav
End Item Identification [AGAV]
Acft Eng F117

2840-01-422-1998 Management Data Management Data 2840-01-422-1998

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
May 2010
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BE
C-17 ENGINE
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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2840-01-422-1998 Freight Data Freight Information 2840-01-422-1998

2840-01-422-1998 has freight characteristics.. 2840-01-422-1998 has a variance between NMFC and UFC when transported by rail and the description should be consulted.