Tu Axial Compressor Disk And Hub NSN 2840-01-006-1118

Item Description

Inc 61831 cancelled/replaced by ,inc 50561, fiig a10700, app-key f ,inc 50562, fiig a10700, app-key f ,inc 50563, fiig a10700, app-key f ,inc 50564, fiig a10700, app-key f ,inc 50565, fiig a10700, app-key f ,inc 50566, fiig a10700, app-key f ,on 021513 ~(all except usa). A disk having provisions on the outer periphery for attaching compressor blades and an integral hub that provides support and alignment for the compressor rotor. See also disk,axial compressor,turbine engine.

NSN: 2840-01-006-1118

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Features and Characteristics

Special Features

Cres, m3710 fscm 91547, passivated finish, p6402 fscm 91547, rockwell c scale 37 min, 44 max hardness, 4.577 in. Min, 4.589 in. Max o/a lg, 1st end tapered disk, 5.872 in. Min, 5.882 in. Max smallest od disk, 5.927 in. Min, 5.937 in. Max largest od disk, 1.121 in. Min, 1.123 in. Max lg disk, 31 blade grooves equally spaced on outer periphery of disk, 2nd end stepped hub, ext thd 2nd end, 1.750 in.-16 un series cl 3a thd, 0.356 in. Nom lg thd, 1.645 in. Min, 1.655 in. Max od 1st step 2nd end, 0.150 in. Nom lg 1st step 2nd end, ext splines 2nd step 2nd end, 45 teeth, 30 degrees pressure angle, 1.9137 in. Min, 1.9167 in. Max od, 1.8750 in. Nom pitch dia, 0.163 in. Min, 0.173 in. Max lg splines, 1.725 in. Min, 1.735 in. Max od 3rd step 2nd end, 0.120 in. Nom lg 3rd step 2nd end, 1.9685 in. Min, 1.9687 in. Max diameter 4th step 2nd end, 1.060 in. Min, 1.062 in. Max lg 4th step 2nd end, 2.220 in. Nom od 5th step 2nd end tapered 30 deg, 0.310 in. Nom lg 5th step 2nd end, 2.423 in. Min, 2.431 in. Max od 6th step 2nd end, 0.820

General Description

FSC

2840 Prime Moving; And Components Aircraft Gas Turbines And Jet Engines

NIIN

010061118

NSN

2840010061118

Manufacturer Part Numbers

Part numbers registered to this national stock number.

Part Number

Cage

Status

MSDS

Part Number:

1-100-495-07

Cage Code:

99193

Status:

MSDS:

Foreign Trade & Schedule B

What is a Schedule B number? Find more information at help.cbp.gov

Schedule B Number: 8411997050
NAICS: 336412
SITC: 71499
Description: Parts of gas turbine aircraft engines, other than for use in civil aircraft
End Use (Code 50020):
Engines and turbines for military aircraft

Q & A

Frequently asked questions for NSN 2840-01-006-1118

What are the manufacturers of nsn 2840010061118?

Honeywell International Inc. (99193)
U S Army Aviation And Missile (81996)

Does this nsn 2840010061118 have a shelf life?
No. This NSN does not have an applicable shelf life.

What is the formal definition of nsn 2840010061118
Inc 61831 cancelled/replaced by ,inc 50561, fiig a10700, app-key f ,inc 50562, fiig a10700, app-key f ,inc 50563, fiig a10700, app-key f ,inc 50564, fiig a10700, app-key f ,inc 50565, fiig a10700, app-key f ,inc 50566, fiig a10700, app-key f ,on 021513 ~(all except usa). a disk having provisions on the outer periphery for attaching compressor blades and an integral hub that provides support and alignment for the compressor rotor. see also disk,axial compressor,turbine engine.

Does nsn 2840010061118 contain any precious metals?
Precious metal content is unknown.

Does nsn 2840010061118 contain any hazardous materials?
No MSDS. No hazardous material.

What is the ESD classification of nsn 2840010061118?
No known electrostatic discharge.

Identification Group

Item Identification Guide (IIG) and Item Name Code (INC)

INC

FIIG

App. Key

Cond. Code

Status

INC:

61831

FIIG:

A23900

App. Key:

Cond. Code:

Status:

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Certificate of Conformance
Quality Inspected Parts
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