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2840-01-467-9426

Aircraft Gas Turbine Engine Turbine Rotor

2840014679426 014679426 799371

A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Turbine Rotor

2840-01-467-9426 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014679426 014679426

Managed by United States
NSN Created on 21 Sep 1999
Data Last Changed
May 2023
NATO Update Count
4
NATO Data Quality
2840-01-467-9426 ROTOR,TURBINE,AIRCRAFT GAS TURBINE ENGINE 2840014679426 014679426 1/1
NSN 2840-01-467-9426 (Generic Image) 1/1

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2840-01-467-9426 Related Documents Related Documents 2840-01-467-9426 5+ Documents (More...)

2840-00-915-8261 2840009158261 009158261 is a single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. it consists of disks, blades, hubs, and the like. it is the moving part of a turbine assembly, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
2840-00-089-6150 2840000896150 000896150 is a single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. it consists of disks, blades, hubs, and the like. it is the moving part of a turbine assembly, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
2840-00-831-6077 2840008316077 008316077 is a single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. it consists of disks, blades, hubs, and the like. it is the moving part of a turbine assembly, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
2840-00-918-2026 2840009182026 009182026 is a single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. it consists of disks, blades, hubs, and the like. it is the moving part of a turbine assembly, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.
2840-01-160-6481 2840011606481 011606481 is a single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. it consists of disks, blades, hubs, and the like. it is the moving part of a turbine assembly, aircraft gas turbine engine. it has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.

2840-01-467-9426 Demil Restrictions 2840-01-467-9426

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

IUID Required

2840-01-467-9426 is a Aircraft Gas Turbine Engine Turbine Rotor 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 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.

2840-01-467-9426 HTS and ScheduleB Import and Export 2840-01-467-9426

2840-01-467-9426 End Users End Users 2840-01-467-9426

US Air Force (FXX4)
Effective Date:
1 Sep 1999

2840-01-467-9426 Manufacturers Approved Sources 2840-01-467-9426

2840-01-467-9426 Technical Data Datasheet 2840-01-467-9426

Characteristic
Specifications
FIIG
A10700
Criticality Code Justification [CRTL]
Agav
Diameter [ABMZ]
38.000 Inches Nominal
End Item Identification [AGAV]
Tf33 Acft Engine
Engine Section Location [CZBJ]
Low Pressure Turbine
Material [MATT]
Steel Disk
Material [MATT]
Steel Shaft
Material [MATT]
Nickel Alloy And Cobalt Alloy Blade
Reference Data And Literature [RDAL]
T.O. 2J-Tf33-34 Fig31, Ind 2
Special Features [FEAT]
2840014679426,P/N Supersedes P/N 752880, 2840011606481
Overall Length [ABHP]
73.500 Inches Nominal
Part Name Assigned By Controlling Agency [CXCY]
Turbine Rotor Assy-Front Compressor Drive

2840-01-467-9426 Management Data Management Data 2840-01-467-9426

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Oct 2022
Department of the Air Force (DF)
EA
Subscribe
1
Feb 2022
Department of the Air Force (DF)
EA
Subscribe
1
Oct 2021
Department of the Air Force (DF)
EA
Subscribe
1
Nov 2020
Department of the Air Force (DF)
EA
Subscribe
1
Oct 2019
Department of the Air Force (DF)
EA
Subscribe
1
MOE
USC
Code
Statement
Order of Use
Jump To Code
Qty Per Assy
UOM
Technical Document
Quantative Expression
Department of the Air Force (DF)
L
G
Replaces 2840-00-831-6077
AAA
Department of the Air Force (DF)
L
G
Replaces 2840-00-918-2026
AAB
Department of the Air Force (DF)
L
G
Replaces 2840-00-089-6150
AAC
Department of the Air Force (DF)
L
G
Replaces 2840-00-915-8261
AAD
Department of the Air Force (DF)
L
G
Replaces 2840-01-160-6481
AAE
Department of the Air Force (DF)
L
R
Refer To Net Price 284265.73
NET PRICE 284265.73
Department of the Air Force (DF)
L
Dod I&S Family Master Nsn - - -
AAF

Air Force Air Force

Fund:
RO
Major Repair
Budget:
8
97X4830.FCL4 - Materiel Support DIV (MSD) - Materiel Support Division (MSD), which includes those Air Force Centrally Managed Investment Items (ERRC XD1=C and XD2=T) except for those still managed in budget programs (BP) 15, 25, 82, 83, and 84 as stock fund exempt. MSD also includes items centrally procured and managed as Expense Items (ERRC XB3=N and XF3=P). Reference AFMAN 23–110, Volume 1, Part 3, Chapter 7, Paragraph 7.3.1
Aggregation Code:
RV
PRATT & WHITNEY JET ENGINES & COMPONENTS TF-33
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 “L” or “F”, 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).

2840-01-467-9426 Related Items NATO Stock Numbers Related to 2840-01-467-9426

2840-01-467-9426 Freight Data Freight Information 2840-01-467-9426

2840-01-467-9426 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 114215. A Sub NMFC of Z. It has a NMFC Description of ASSEMBLIES JET AIRCRAFT ENGINE. 2840-01-467-9426 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 63220 which rates the freight between FCL and LCL. 2840-01-467-9426 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 671 for ocean manifesting and military sealift. 2840-01-467-9426 is not classified as a special type of cargo when transported by water. 2840-01-467-9426 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.

2840-01-467-9426 Packaging Data Packaging Data 2840-01-467-9426

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
73.5" H x 38.0" W x 38.0" L
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--
--
--

Unit Pack Level (Packaged)

Quantity per Pack
Unit Size
Unit Weight
Unit Cube
Preservation Method
Cleaning/Drying
1
96.2" H x 44.5" W x 48.0" L
--
--
--
Any Suitable Process
Preservation Material
Wrapping Material
Cushioning/Dunnage
Cushioning Thickness
Container
Special Marking
Special 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
No special marking

Intermediate Pack Level

Quantity of Unit Packs
Container
--
No Requirement