Model: HG2011AC03

Aircraft Attitude Computer

Special Features:

Uses digital ring-laser gyros andquartz accelerometers to keep track ofchanges in aircraft heading and attitude

Properties:

End Application
Aircraft, embraer, model erj135 and erj145
Power Source
External
Intelligence Input Method
Electrical
Part Name Assigned By Controlling Agency
Attitude heading reference syste m
NSN
6605-01-500-0499
Part Number
HG2011AC03
Description
Computer,aircraft Attitude
CAGE

A computer that contains the follow-up servo for pitch and roll information from the platform, and the circuitry for computing vertical attack angles, climb angle, vertical velocity, and ground speed to altitude ratio.

Part HG2011AC03 NSN 6605-01-500-0499

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
53058
FIIG:
A30800
Concept No.:
1
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:
P
PMIC:
A
ESD:
A
ESD:
A
MMAC:
CRITL:
X

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Schedule B and Export
  • Schedule B: 9014900000
  • SITC: 87412
  • End Use: Marine engines, parts
  • NAICS: 334511
  • USDA: 1

Freight Class: Parts & accessories for direction finding compasses and other navigational instruments and appliances

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