Model: 9511M38P01

Aircraft G Compressor Blade Lock

Special Features:

T.O. 2j-f110-4

Properties:

Overall Length
10.226 inches
Overall Width
Between 0.187 inches and 0.212 inches
Material Thickness
Between 0.009 inches and 0.011 inches
End Application
Aircraft eng f101
Criticality Code Justification
Agav
Stage Number
4
Material
Steel
Material Specification
Ams5537 assn standard single material response
NSN
2840-01-171-0864
Part Number
9511M38P01
Description
Lock,compressor Blade,aircraft G
CAGE
07482

An item used to maintain the position of a blade, compressor, aircraft gas turbine engine in the proper place on a disk, compressor, aircraft gas turbine engine. this item eliminates axial movement of the blade.

Part 9511M38P01 NSN 2840-01-171-0864

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50454
FIIG:
A503Q0
Concept No.:
App. Key:
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:
N
PMIC:
A
ESD:
ESD:
MMAC:
JF
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.2000lbs
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:
095190
UFC:
49790
LTL:
RATING VARIABLE
LCL:
70.0
WCC:
713
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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