Model: 709451CL11

Aircraft Gas Turb Turbine Nozzle

Special Features:

1.207-1.217 sq in. Flow area

Properties:

Overall Length
Between 2.019 inches and 2.099 inches
Overall Width
Between 1.919 inches and 1.923 inches
End Application
Tf30 aircraft engine
Criticality Code Justification
Agav
Engine Section Location
Turbine
Material
Nickel alloy vane
Material Specification
Ams5540 assn standard single material response vane
NSN
2840-00-063-6787
Part Number
709451CL11
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 709451CL11 NSN 2840-00-063-6787

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:
--
Paclk Weight:
50.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
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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