Model: 9663M23G11

Aircraft Turbine Shroud Segment

Properties:

Overall Length
Between 2.720 inches and 2.740 inches
Diameter
48.660 inches
End Application
Aircraft eng tf39
Criticality Code Justification
Agav
Engine Section Location
Turbine
Material
Steel outer case
Material Specification
B50tf25cl-a mfr ref single material response outer case
NSN
2840-01-122-1881
Part Number
9663M23G11
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 9663M23G11 NSN 2840-01-122-1881

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:
NY
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
4.3 X 4.3 X 12.5
Paclk Weight:
2.0000lbs
Item Weight:
0.5000lbs
Item Dim:
010800080028
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000001D02
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
65.0
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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