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2840-01-680-6441

Aircraft Gas Turbine Engine Exhaust Duct Liner

2840016806441 016806441 4322636

A liner designed for a DUCT, EXHAUST, AIRCRAFT GAS TURBINE ENGINE or DUCT AND CONE, EXHAUST, AIRCRAFT GAS TURBINE ENGINE or one of their components. View more Aircraft Gas Turbine Engine Exhaust Duct Liner

2840-01-680-6441 LINER,EXHAUST DUCT,AIRCRAFT GAS TURBINE ENGINE 2840016806441 016806441

Managed by United States
NSN Created on 15 May 2019
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-01-680-6441 LINER,EXHAUST DUCT,AIRCRAFT GAS TURBINE ENGINE 2840016806441 016806441 1/1
NSN 2840-01-680-6441 (Generic Image) 1/1

2840-01-680-6441 Stock and Availability Marketplace 2840-01-680-6441

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2840-01-680-6441 Related Documents Related Documents 2840-01-680-6441 4+ Documents (More...)

4322636 A liner designed for a DUCT, EXHAUST, AIRCRAFT GAS TURBINE ENGINE or DUCT AND CONE, EXHAUST,
United States (US) 4. 2840-01-680-6441 Marketplace Restrictions Approved Sources Datasheet Management
Request a Quotation from participating marketplace vendors Request Updated Every Day 2840-01-680-6441
4940Hatch Dog Assembly2040014754940 014754940 124-4322618 ASSY 81 124-4322634 PC 12 124-4322635 PC 12 124-4322636
PC 11 4322635 4322636 4322618 4322634 A component of a marine hull hatch closing mechanism.
124-4322635 PC 12 53711 - Naval Sea Systems Command (Active) Primary Buy RNCC 3 RNVC 2 DAC A 124-4322636
Account Upgrade 5315-01-473-7766Cotter Pin5315014737766 014737766 124-5588673 PC 19 3/16 LG=1-1/2 124-4322636
/fsc-5315/us 5315-01-473-7766 Cotter Pin 5315014737766014737766 124-5588673 PC 193/16 LG=1-1/2124-4322636
4364817 PC 22 124-4364818 PC 23124-5754756 PC 23124-4364815 PC 23124-4322640 PC 19124-5588672 PC -4322636
5306-01-475-6657 5306014756657 014756657 is an externally threaded fastener designed for insertion through holes in assembled parts and normally intended to be tightened or released by torquing a nut. the threaded and unthreaded portions are both of one nominal diameter of 0.190 inch (5 mm) or larger. the head is not designed to be held or driven with an inserted driver or by the thumb and fingers. a locking feature may be incorporated in the design of the head or threads. head dimensions and sizes of threaded and unthreaded portions shall conform to internationally recognized fastener standards. for items having a grip length portion machined to a tolerance of 0.0015 inch (0.038 mm) or less, bolt, shear. see also screw, cap, hexagon head and screw, machine.

2840-01-680-6441 Demil Restrictions 2840-01-680-6441

DEMIL: D | DEMILI: 1 | CRITICALITY: Y | HMIC: N | PMIC: A | EDC: | ADPEC: 0

IUID Required

2840-01-680-6441 is a Aircraft Gas Turbine Engine Exhaust Duct Liner that does not have a nuclear hardened feature, but does have another critical feature or features such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. This item is a US Munitions List or Commerce Control List Item which must be destroyed to prevent restoration or repair. Only authorized parties may possess this item. This item is not suspected to be hazardous. This item does not contain a precious metal.

2840-01-680-6441 HTS and ScheduleB Import and Export 2840-01-680-6441

2840-01-680-6441 Manufacturers Approved Sources 2840-01-680-6441

2840-01-680-6441 Management Data Management Data 2840-01-680-6441

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
May 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)
F
R
Refer To Afto 95 Required
AFTO 95 REQUIRED

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