Model: 56-2416-2096

Push-pull Control Assembly

Properties:

Effective Length
24.313 inches
Core Construction
Wire rope
Flexible Conduit Material
Rubber and steel
Core Diameter
0.095 inches
Core Processed End Connection Type
Adjustable threaded adapter
Flexible Conduit Outside Diameter
0.375 inches
Travel Distance
1.000 inches
Features Provided
Adapter
Core Material
Steel
Fsc Application Data
Miscellaneous aircraft accessories and components
NSN
1680-00-803-4315
Part Number
56-2416-2096
Description
Control Assembly,push-pull
CAGE
5S058

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 56-2416-2096 NSN 1680-00-803-4315

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:
SX
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.5000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
128400
UFC:
65030
LTL:
85.0
LCL:
--
WCC:
671
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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