Model: 383766-2-3

Gas Turbine Engine Starter

Properties:

General Description
J90.0 horsepower output, single stage radial outflow turbine, compound planetary type reduction gear, 18.3-1.0, counterclockwise rotationoutput shaft cutout speed, 3100 to 3300 rpm, output shaft shear load 850 ft-lbs
Fsc Application Data
Tf41-a-1 engine, a7d
NSN
2995-00-469-0101
Part Number
383766-2-3
Description
Starter,engine,gas Turbine
CAGE
99193

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.

Part 383766-2-3 NSN 2995-00-469-0101

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
21907
FIIG:
A23900
Concept No.:
App. Key:
A
Cond. Code:
2
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
36.0 X 26.0 X 19.0
Paclk Weight:
120.0000lbs
Item Weight:
81.0000lbs
Item Dim:
024002000120
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000004XE9
SPI Rev.:
SPC Mkg:
19
LVL_A:
LVL_B:

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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