Model: 6828551-21

Aircraft Turbine Nozzle Assembly

Special Features:

Heat treat eps 266; 76 vanes

Properties:

Overall Length
3.159 inches
Diameter
Between 17.175 inches and 17.179 inches
End Application
Aircraft eng t56
Criticality Code Justification
Agav
Engine Section Location
Turbine
Stage Number
1
Material
Stainless steel vane
Material Specification
Ams5652 assn standard single material response vane
NSN
2840-00-072-8963
Part Number
6828551-21
Description
Nozzle Assembly,turbine,aircraft
CAGE
63005

A 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. the assembled item forms a complete circle.

Part 6828551-21 NSN 2840-00-072-8963

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50581
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:
12.5 X 8.3 X 4.0
Paclk Weight:
11.0000lbs
Item Weight:
3.0000lbs
Item Dim:
010000350035
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000001XC6
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
011790
UFC:
04720
LTL:
RATING VARIABLE
LCL:
--
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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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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