Model: 5338079-1

Cowling Flap

Special Features:

Hinged connection

Properties:

Material Thickness
0.032 inches
Material
Aluminum alloy
Material Specification
Qq-a-250/5 federal specification single material response
NSN
1560-00-213-2989
Part Number
5338079-1
Description
Flap,cowling
CAGE
88277

A hinged section forming a part of the aircraft engine cowling, usually located aft of the engine. The purpose of the flap is to regulate the flow of air over and around an engine to control the temperature.

Part 5338079-1 NSN 1560-00-213-2989

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
60488
FIIG:
A11500
Concept No.:
App. Key:
B
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:
P
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
013120
UFC:
05380
LTL:
100.0
LCL:
--
WCC:
576
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8803909060
  • SITC: 79297
  • End Use: Parts for military-type goods
  • NAICS: 336419
  • USDA: 1

Freight Class: Other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites)

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