Model: 9538M24G01

A Outer Augmentor Nozzle Section

Properties:

Overall Length
Between 23.320 inches and 23.360 inches
End Application
Aircraft eng f110
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Flap, outer
Material
Titanium alloy
NSN
2840-01-192-1068
Part Number
9538M24G01
Description
Augmentor Nozzle Section,outer,a
CAGE
07482

A rigid item designed to help direct the flow of hot gases from an afterburner,turbine engine. it is an integral part of a nozzle,augmenter exhaust,aircraft gas turbine engine. the item is external to the augmentor nozzle section,convergent,aircraft gas turbine engine and the augmentor nozzle section,inner,aircraft gas turbine engine.

Part 9538M24G01 NSN 2840-01-192-1068

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
53242
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:
PR
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
28.0 X 15.0 X 5.0
Paclk Weight:
9.0000lbs
Item Weight:
3.0000lbs
Item Dim:
027201200022
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
593
TCC:
Z
SHC:
Z
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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