383934-1-2

Gas Turbine Engine Starter

NSN 2995-00-115-3532

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

001153532

Detail Specifications

End Application:

J79-ge-15 aircraft engine

General Description:

Solid propellent cartridge, af type mxu-4/a, w/provisions for air turbine starting, 50.0 psi air inlet pressure, 95.0 lb per min flow, maxelec data, 32 v, 3 amp, dc, ccn drive rotation viewing output shaft, drive spline data, 24 teeth, 20/30 pitch, 1.200 in. Pitch dia, 1.090 in. Min. Dia, 1.2645 in. Max dia, 0.700 in. Lg, mtg data, std mounting and10266, type xvi&a, w/quick detachable mtg

Fsc Application Data:

Starter, engine, gas turbine

NSN:

2995-00-115-3532

Item Name:

Starter,engine,gas Turbine

Cage Code:

99193

Manufacturer Part Numbers

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

383934-1-2

Cage Code:

59364

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

383934-1-1

Cage Code:

59364

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

383934-1-1

Cage Code:

99193

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

21907

FIIG:

A23900

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:

21.3 X 21.3 X 25.5

Paclk Weight:

78.0000lbs

Item Weight:

60.0000lbs

Item Dim:

011001100170

OPI

SPI No.

SPI Rev.

SPC Mkg.

LVL A

LVL B

OPI:

SPI No.:

F007262809

SPI Rev.:

SPC Mkg:

LVL_A:

LVL_B:

Freight Classification

NMFC

UFC

LTL

LCL

WCC

TCC

SHC

ACC

NMFC:

133300

UFC:

63220

LTL:

92.5

LCL:

100.0

WCC:

671

TCC:

SHC:

ACC:

Equipment for Aircraft

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Gas Turbine Engine Starter"

An item designed to accelerate a gas turbine engine from rest to starter cutoff speed by means of a combustion gas driven turbine and reduction gear assembly constructed to be mounted on the engine starter drive. The combustion gas is generated from ignited liquid fuel and air in the combustion chamber or from a solid propellant cartridge attached to the combustion chamber of the starter. May have provision for energizing the turbine by low pressure air from engine bleed or ground equipment air supply.