Model: 1820M92P02

Turbine Engine Main Fuel Control

Properties:

Reference Data And Literature
6j3-4-131-3/4
General Description
The control is a fuel operated; by-passing type, electrohydro-mechanical fuel flow regulator.Control schedules valve strator vane position and controls fuel flow based on electrical inputs; a new design mec support a digital electronic controlled f110-ge-100b engine
Reference Number Differentiating Characteristics
As differentiated by source control drawing number
NSN
2915-01-424-0966
Part Number
1820M92P02
Description
Fuel Control,main,turbine Engine
CAGE
07482

A self contained metering unit consisting primarily of pumping, controlling, valving, and/or governing components. It is designed for regulating the delivery of fuel into the main fuel system of a turbine engine.

Part 1820M92P02 NSN 2915-01-424-0966

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
61547
FIIG:
A23900
Concept No.:
App. Key:
A
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:
PR
CRITL:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
20.0 X 20.0 X 20.5
Paclk Weight:
65.0000lbs
Item Weight:
50.0000lbs
Item Dim:
010001400170
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F012406209
SPI Rev.:
F
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
WCC:
671
TCC:
1
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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