Model: 5103T25P02

Ai Augmentor Nozzle Section Seal

Properties:

End Application
Ge f414-400 engine
NSN
2840-01-443-4133
Part Number
5103T25P02
Description
Seal,augmentor Nozzle Section,ai
CAGE
99207

A rigid item designed to complete the circumference when the nozzle,augmenter exhaust,aircraft gas turbine engine is in the open position allowing the nozzle to maintain control of the hot exhaust gases. it is situated between the augmentor nozzle section,outer,aircraft gas turbine engine and the augmentor nozzle section,outer,aircraft gas turbine engine and the augmentor nozzle section,convergent,aircraft gas turbine engine; augmentor nozzle section,inner,aircraft gas turbine engine.

Part 5103T25P02 NSN 2840-01-443-4133

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
53243
FIIG:
A526N0
Concept No.:
App. Key:
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:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
--
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
99
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114030
UFC:
64100
LTL:
200.0
LCL:
--
WCC:
671
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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