Model: 4056200

Aircraft Gas Turb Turbine Nozzle

Special Features:

T.O. 2j-f110-4; augmentor nozzle lever; balance & convergent nozzle segment; 15 units per assembly; 0.159-0.163 in. Diameter of 1 hole; 0.190-0.192 in. Diameter through 2 lugs

Properties:

Overall Length
20.600 inches
Overall Width
Between 5.535 inches and 5.545 inches
End Application
F100pw100/200 aircraft engine
Criticality Code Justification
Agav
Engine Section Location
High pressure turbine
NSN
2840-01-164-9087
Part Number
4056200
Description
Nozzle,turbine,aircraft Gas Turb
CAGE
77445

A single stationary item designed for the purpose of directing air at the proper angle and velocity to a rotor, turbine, aircraft gas turbine engine. it has provisions for attaching to a case (3), turbine, aircraft gas turbine engine. it may have an inner support shroud.

Part 4056200 NSN 2840-01-164-9087

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50585
FIIG:
A10700
Concept No.:
App. Key:
A
Cond. Code:
1
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:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
27.0 X 10.0 X 9.3
Paclk Weight:
10.0000lbs
Item Weight:
3.0000lbs
Item Dim:
022000700030
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000001XE8
SPI Rev.:
SPC Mkg:
17
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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