Model: 68A412739-2001

Helical Compression Spring Seat

Special Features:

First step diameter undercut and relieved shoulder; both ends countersink 30.0 deg

Properties:

Counterbore Diameter
1.7500 inches
Overall Height
0.9000 inches
First Step Diameter
Between 2.6050 inches and 2.6150 inches
First Step Length
0.1200 inches
Bore Diameter
1.5000 inches
Second End Diameter
Between 1.9650 inches and 1.9750 inches
Design Type
Solid
End Diameter
1.6850 mils and 1.6950 centimeters
Distance From End To First Step
0.1900 inches
Counterbore Length
0.4000 inches
Material
Aluminum alloy, qq-a-225/9, alloy 7075, t7351 or aluminum alloy, qq-a-200/11, t73511 or t7351 or t73 or t7351
Material
Aluminum alloy 7075 or aluminum alloy, qq-a-200/11, t73511 or t7351 or t73 or t7351
Material Specification
Qq-a-225/9, alloy 7075, t7351 federal specification 1st material response
Surface Treatment
Anodize
Surface Treatment Specification
Ps15548, mcdonnel aircraft co mfr ref single treatment response
Style Designator
Seat
Surface Treatment
Anodize, ps15548, mcdonnel aircraft co
NSN
5340-01-254-1470
Part Number
68A412739-2001
Description
Seat,helical Compression Spring
CAGE

Part 68A412739-2001 NSN 5340-01-254-1470

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
24328
FIIG:
T319-E
Concept No.:
App. Key:
EA
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:
LE
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.1000lbs
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:
013120
UFC:
05380
LTL:
100.0
LCL:
--
WCC:
713
TCC:
Z
SHC:
9
ACC:
Construction Materials

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