Model: 204-83532-3

Push-pull Control Assembly

Special Features:

C/o 1 sleeve, 1 jacket repair kit, 1 nut seal, 2 clevis, 12 nut-jam, 1 cable assembly, 2 swivel assembly, 1 casing assembly; materials shall be corrosion resistant

Properties:

Effective Length
72.570 inches
End Application
Airborne warning and control system (awacs) 411l
Core Diameter
0.460 inches
Travel Distance
6.760 inches
Fsc Application Data
Aircraft accessory equipment
NSN
1680-01-021-4081
Part Number
204-83532-3
Description
Control Assembly,push-pull
CAGE
81205

A control consisting of a wire, wire rope, or a center load rail with ball bearings, within a flexible conduit. One end must have a threaded sleeve for mounting to a wall, bulkhead, or handle, or clevis. It is used to operate or control, either manually or mechanically a mechanical device. It may include such attaching devices as nut(s), washer(s), clevis, bracket(s), and/or the like. For items designed to transmit rotary motion, see shaft assembly, flexible.

Part 204-83532-3 NSN 1680-01-021-4081

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
07468
FIIG:
A524C0
Concept No.:
App. Key:
Cond. Code:
2
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:
AW
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
4.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
061480
UFC:
34500
LTL:
77.5
LCL:
77.5
WCC:
658
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8803300060
  • SITC: 79295
  • End Use: Parts for military-type goods
  • NAICS: 336413
  • USDA: 1

Freight Class: Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts thereof)

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