Model: 9523M21P01

Aircraft Turbine Shroud Segment

Special Features:

T.O. 2j-f108-4; high pressure turbine shroud and 1st stage l.P. Turbine nozzle; u-shaped clips

Properties:

Overall Length
Between 0.254 inches and 0.375 inches
Material Thickness
Between 0.077 inches and 0.085 inches
End Application
B1b acft/f108 aircraft engine
Design Type
Compressor
Engine Section Location
High pressure turbine
Stage Number
1
Material
Nickel alloy outer case
NSN
2840-01-175-3023
Part Number
9523M21P01
Description
Shroud Segment,turbine,aircraft
CAGE
07482

A stationary arched metal segment used to establish clearance and a seal for the tip of a blade, turbine rotor, aircraft gas turbine engine. The inner dimension may have open honeycomb or composition filled surface or may be formed by the knife edge metal protrusions of a seal ring, labyrinth, aircraft gas turbine engine.

Part 9523M21P01 NSN 2840-01-175-3023

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50603
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:
JF
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.1000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
095190
UFC:
49790
LTL:
RATING VARIABLE
LCL:
70.0
WCC:
713
TCC:
Z
SHC:
Z
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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