Model: 62719SP20

Internal Combustion Engine Piston

Properties:

Head Style
Flat
Overall Height
3.200 inches
Diameter
4.8541 inches
Oil Passage Type
Hole
Pinhole Diameter
1.1247 inches
Surface Finish
Finished
Finished Size Designation
Oversize
Oversize
0.020 inches
Skirt Type
Solid
Cut Depth
0.5475 inches
Skirt Bottom Cutaway Feature
Included
Ring Groove Quantity
3
Ring Groove Position
No.1, no.2 and no.3
Ring Groove Width
0.1280 inches and 0.1890 inches
Groove Taper Angle
7 degrees 26 min., porm 15 min.
Ring Groove Diameter
4.395 inches
Ring Groove Diameter
4.436 inches
Ring Groove Diameter
4.395 inches 2nd ring
Ring Groove Diameter
4.436 inches 1st ring
Oil Groove
Not included
Distance From Pin Hole Center To Extreme Top
1.7225 inches
Pin Hole Bushing
Not included
Distance Between Pin Bosses
1.750 inches
Retaining Ring Groove
Not included
Pin
Not included
Pin Type For Which Designed
Floating
Ring
Not included
Carbon Groove
Not included
Material
Aluminum
Material
Aluminum
Surface Treatment
Tin
Surface Treatment
Tin plated
Weight
42.0 ounces
Fsc Application Data
Engine, reciprocating, aircraft
NSN
2810-00-554-2185
Part Number
62719SP20
Description
Piston,internal Combustion Engine
CAGE
80254

Part 62719SP20 NSN 2810-00-554-2185

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
16509
FIIG:
T267-C
Concept No.:
1
App. Key:
CA
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:
U
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
593
TCC:
Z
SHC:
9
ACC:
Trailers/Vehicles

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Schedule B and Export
  • Schedule B: 8409100080
  • SITC: 71319
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts for spark-ignition or compression-ignition internal combustion piston engines for use in aircraft except civil

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