Model: 9526M77

Aircraft Turbine Shroud Segment

Special Features:

Mat is hastalloy x; honeycombed; item is preground; superseded p/n 9526m77g02 per cid 808396

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
Matt and czbj and czcj and abhp and abmz
Engine Section Location
Turbine
Stage Number
2
Material
Chromium and iron and cobalt alloy
Material Specification
Ams5838 assn standard single material response
Reference Data And Literature
T.O. 2j-f101-4, fig 61, ind 12
NSN
2840-01-430-2595
Part Number
9526M77
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 9526M77 NSN 2840-01-430-2595

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:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
77.5
WCC:
593
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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