Model: 804351CL21

Aircraft Gas Turb Turbine Nozzle

Special Features:

Flow area 1.455 - 1.464; pitch is 34deg 29min 28sec

Properties:

Overall Length
Between 1.110 inches and 1.130 inches
Overall Height
4.153 inches
Overall Width
2.045 inches
End Application
Tf-33
Blade Attachment Method
Slot
Criticality Code Justification
Abmk
Part Name Assigned By Controlling Agency
Vane-hpt, 1 stg
Engine Section Location
High pressure turbine
Stage Number
1
Material
Cobalt alloy vane
Reference Data And Literature
T.O. 2j-tf33-4 fig31 ind50
NSN
2840-01-394-5883
Part Number
804351CL21
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 804351CL21 NSN 2840-01-394-5883

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:
RV
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
6.0 X 4.0 X 1.0
Paclk Weight:
0.6000lbs
Item Weight:
0.5000lbs
Item Dim:
003000130042
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
200.0
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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