Model: 1961M83P01

Turbine Supervisory Control Unit

Properties:

Overall Length
Between 14.031 inches and 14.105 inches
End Application
F118-ge-100 aircraft engine
Part Name Assigned By Controlling Agency
Digital electronic control
Nuclear Hardness Critical Feature
Hardened
General Description
Replaces nsn's 6620-01-379-1235 which has 5 assets and 2925-01-290-6822which has 23 assets
Reference Number Differentiating Characteristics
As differentiated by source control drawing
NSN
2995-01-518-7092
Part Number
1961M83P01
Description
Control Unit,supervisory,turbine
CAGE
07482

An electronic unit that continously monitors engine speed, temperature, and air flow and adjusts the fuel control, main, turbine engine to compensate for changes. Features may include load sharing capabilities, rotor speed governing, loss-of-load protection and analog or manual backup modes. It may contain automatic start capability or self-diagnostic circuitry.

Part 1961M83P01 NSN 2995-01-518-7092

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
47093
FIIG:
A23900
Concept No.:
App. Key:
A
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:
JU
CRITL:
H

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
25.0 X 19.0 X 16.5
Paclk Weight:
44.0000lbs
Item Weight:
30.0000lbs
Item Dim:
014201120067
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000003XE7
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
671
TCC:
Z
SHC:
9
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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