Model: 1317M75G01

Aircraft Turbine Shroud Segment

Properties:

Overall Length
Between 1.785 inches and 1.800 inches
Diameter
Between 15.158 inches and 15.162 inches
Material Thickness
Between 0.038 inches and 0.044 inches
End Application
F110ge100 aircraft engine
Criticality Code Justification
Agav
Engine Section Location
Low pressure turbine
Stage Number
1
Material
Titanium alloy
Material Specification
B50tf76 cl-c mfr ref single material response
NSN
2840-01-326-0825
Part Number
1317M75G01
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 1317M75G01 NSN 2840-01-326-0825

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:
--
Paclk Weight:
1.0000lbs
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:
114730
UFC:
58790
LTL:
85.0
LCL:
85.0
WCC:
576
TCC:
Z
SHC:
9
ACC:
Trailers/Vehicles

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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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