Model: 9340M30P02

Aircraft Gas Turbine En Air Seal

Special Features:

Has 5 keys permanently attached with 2 rivets each, evenly spaced around circumference of seal

Properties:

Diameter
Between 12.600 inches and 12.640 inches
End Application
Used on jet engine (f110-ge-400)
Features Provided
Ring
Criticality Code Justification
Agav
Engine Section Location
Turbine
Material
Stainless steel outer case
Material Specification
Sae-ams 5643q assn standard single material response outer case
Reference Number Differentiating Characteristics
As differentiated by source control drawing
NSN
2840-01-504-1709
Part Number
9340M30P02
Description
Seal,air,aircraft Gas Turbine En
CAGE
07482

A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an engine, gas turbine, aircraft. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.

Part 9340M30P02 NSN 2840-01-504-1709

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50595
FIIG:
A10700
Concept No.:
App. Key:
H
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

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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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