Model: 4077434-01

Aircraft Turbine Shroud Segment

Special Features:

T.O. 2j-f100-54

Properties:

Overall Length
0.846 inches
Diameter
Between 19.207 inches and 19.213 inches
Material Thickness
0.486 inches
End Application
F100pw0229 aircraft engine
Design Type
Axial compressor
Criticality Code Justification
Agav
Engine Section Location
Compressor
Stage Number
4
Material
Nickel alloy
NSN
2840-01-321-4453
Part Number
4077434-01
Description
Shroud Segment,turbine,aircraft
CAGE
77445

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 4077434-01 NSN 2840-01-321-4453

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:
NZ
CRITL:
F

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:
2.5000lbs
Item Weight:
1.5000lbs
Item Dim:
010000200015
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000002XC6
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
118150
UFC:
64090
LTL:
70.0
LCL:
--
WCC:
593
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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