Model: 17P2C1552-1

Bell Crank

Properties:

Slot Width
0.285 inches 1st end and 0.289 inches 1st end
End Application
C-17 aircraft
Part Name Assigned By Controlling Agency
Crank, alternate release, mlg
Center To Center Distance Between Fulcrum And Arm End Hole/slot/ball
1.722 inches 1st end
Center To Center Distance Between Fulcrum And Arm End Hole/slot/ball
6.500 inches 2nd end
End Hole/ball Diameter
0.2505 inches 1st end and 0.2515 inches 1st end
Material
Aluminum alloy
NSN
1680-01-430-0444
Part Number
17P2C1552-1
Description
Bell Crank
CAGE
88277

An item in the form of two arms at an angle, having its fulcrum at the apex of the angle, and used to provide a means of changing the direction or varying the intensity of a pushing or pulling force. See also arm (as modified); and lever (as modified).

Part 17P2C1552-1 NSN 1680-01-430-0444

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
22321
FIIG:
A523Z0
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:
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
9.3 X 6.3 X 4.0
Paclk Weight:
1.3000lbs
Item Weight:
0.5000lbs
Item Dim:
007600270015
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000004XC4
SPI Rev.:
SPC Mkg:
03
LVL_A:
LVL_B:

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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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