6842657

Aircraft Gas Turbi Turbine Shaft

NSN 2840-00-011-0692

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

000110692

Product Features

3.250-4.922 in. Id.; 0.263-0.270 in. Dia. Of 8 holes eq sp; 0.188 in. Diameter of 2 holes; external spline data: 4.680 in. Od; 4.571 in. Pitch dia.; 32 teeth; 2nd external spline data: 4.781in. Od; 4.750 in. Pitch dia.; 76 teeth; 0.125 in. Dia. Of 5 holes

Product Technical Spec.

Overall Length:

20.165 inches

Diameter:

13.967 inches

End Application:

Aircraft eng t56

Criticality Code Justification:

Agav

Part Name Assigned By Controlling Agency:

Manufacturers suggested name shaft, 60a prop

Engine Section Location:

Turbine

Material:

Steel shaft

Material Specification:

Ams6415 assn standard single material response shaft

Precious Material:

Silver

NSN:

2840-00-011-0692

Item Name:

Shaft,turbine,aircraft Gas Turbi

Cage Code:

63005

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

6842657

Cage Code:

73342

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

50601

FIIG:

A10700

Concept No.:

App. Key:

Cond. Code:

Status:

Part Materials

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators

HMIC

PMIC

ESD/EMI

ENAC

MMAC

CRITL

HMIC:

PMIC:

ESD:

MMAC:

CRITL:

Packaging & Shipping

Est. Pack Size

Est. Pack Weight

Est. Item Weight

Est. Item Dim.

Pack Size:

17.8 X 14.8 X 21.8

Paclk Weight:

75.6000lbs

Item Weight:

Item Dim:

OPI

SPI No.

SPI Rev.

SPC Mkg.

LVL A

LVL B

OPI:

SPI No.:

8013226184

SPI Rev.:

SPC Mkg:

LVL_A:

LVL_B:

Freight Classification

NMFC

UFC

LTL

LCL

WCC

TCC

SHC

ACC

NMFC:

129920

UFC:

65750

LTL:

85.0

LCL:

WCC:

593

TCC:

SHC:

ACC:

Equipment for Aircraft

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Aircraft Gas Turbi Turbine Shaft"

An item designed to transfer rotary motion from a rotary, turbine, aircraft gas turbine engine to a rotor, compressor, aircraft gas turbine engine and/or a rotor, fan, aircraft gas turbine engine. It may include the hub, turbine, aircraft gas turbine engine. It may include provisions for mounting bearings and/or seals.