Model: 12W8810-542

Wing Landing Flap

Special Features:

Provided lift and drag during take off and landing; t6 and honeycomb core

Properties:

Overall Length
40.000 inches
Overall Width
19.000 inches
Material Thickness
3.900 inches
Side For Which Designed
Right side
Aircraft Location
Flap ay, wing no.4
Aircraft Mission Design Series
F-111a, d, e, f, ef
Material
Aluminum alloy 2024
NSN
1560-01-294-5129
Part Number
12W8810-542
Description
Flap,wing Landing
CAGE
81755

A movable airfoil, whether hinged, pivoted or mounted on tracks, forming part of the leading or trailing edge of a wing of an aircraft. it is designed for the specific purpose of lowering the landing speed by varying the effective camber and may be used in accelerated takeoffs and improved climbs. excludes leading edge devices that prevent stalls by ducting air over the top of a wing through extended slats. excludes slat, aircraft.

Part 12W8810-542 NSN 1560-01-294-5129

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
60494
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:
011760
UFC:
04705
LTL:
200.0
LCL:
200.0
WCC:
671
TCC:
Z
SHC:
9
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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