Model: 9526M77G02

Aircraft Turbine Shroud Segment

Properties:

Overall Length
Between 1.901 inches and 1.911 inches
Diameter
37.530 inches
End Application
F101 aircraft gas turbine engine
Design Type
Axial compressor
Criticality Code Justification
Abhp and czbj and matt and czcj
Engine Section Location
Turbine
Stage Number
2
Material
Chromium
Reference Data And Literature
T.O. 2j-f101-4, fig 61, ind 12
NSN
2840-01-146-7570
Part Number
9526M77G02
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 9526M77G02 NSN 2840-01-146-7570

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:
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
10.5 X 3.0 X 3.0
Paclk Weight:
1.0000lbs
Item Weight:
0.0000lbs
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

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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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