SLM2000 (Structural Life Management)
Feature
SLM2000 has process flight data of the basic trainer series (KT-1, KA-1, KT-1P, KT-1T) to perform structure validation, individual aircraft tracking, operational analysis, reports issue.

 

Spec
  • MIL-STD-1530C
  • flight data validation
  • flight log creation
  • database management
  • individual aircraft tracking
  • load/environmental spectrum survey
  • report publication

 

 

DPS (Data Processing System)
Feature
DPS has process flight data of the T-50 series (T-50, FA-50, T-50B, T-50IQ) to perform structure validation, individual aircraft tracking, operational analysis, reports issue.

 

Spec
  • MIL-STD-1530C
  • flight data validation
  • flight log creation
  • database management
  • individual aircraft tracking
  • load/environmental spectrum survey
  • report publication

 

IEMMS (Intelligence Engine Maintenance and Management Software)
Feature
Manages various data generated during operation of the F404-GE-102 engine, and perform predicts engine maintenance time, serial information analysis of engine, TCTO, technical communication analysis, maintenance history analysis to improve the efficiency of engine maintenance and lifetime management.

 

Spec
  • engine basic information management
  • engine serial and configuration management
  • lifetime data management
  • Maintenance data management
  • TCTO and technical communication management
  • view engine data and view users
  • various reports
  • data input / output (transmission / transfer data))
  • account management and smart updates

 

ELMS (Engine Life Management Software)
Feature
Manages various data generated during operation of the PT6A-62 engine, and perform predicts engine maintenance time, serial information analysis of engine, TCTO, technical communication analysis, maintenance history analysis to improve the efficiency of engine maintenance and lifetime management.

 

Spec
  • engine basic information management
  • engine serial and configuration management
  • lifetime data management
  • Maintenance data management
  • TCTO and technical communication management
  • view engine data and view users

 

 

MDAS (Mishap Data Analysis Software)
Feature
MDAS support aircraft accident investigation by acquiring flight data from flight data recorder of T-50 series aircraft to reproduce actual flight situation at aircraft accident time and provide data for analysis of cause of accident.

 

Spec
  • flight data interpolation
  • flight data parameter list
  • flight data parameter graph
  • 2D flight path
  • 3D flight simulation
  • flight simulation control

 

CFDAS (Crash Flight Data Analysis Software)
Feature
CFDAS support aircraft accident investigation by acquiring flight data from flight data recorder of KT-1 series aircraft to reproduce actual flight situation at aircraft accident time and provide data for analysis of cause of accident.

 

Spec
  • flight data interpolation
  • flight data parameter list
  • flight data parameter graph
  • 2D flight path
  • 3D flight simulation
  • flight simulation control

 

IMDAS (Integrated Mishap Data Analysis Software)
Feature
IMDAS support aircraft accident investigation by acquiring flight data from flight data recorder of F-16, F-15K aircraft to reproduce actual flight situation at aircraft accident time and provide data for analysis of cause of accident.

 

Spec
  • flight data interpolation
  • flight data parameter list
  • flight data parameter graph
  • 2D flight path
  • 3D flight simulation
  • flight simulation control

 

KTFAP (KT-1 Total Fatigue Analysis Program)
Feature
KTFAP generates load spectrum and stress spectrum for aircraft structural fatigue analysis and performs S-N analysis, damage tolerance analysis and internal load analysis.

 

Spec
  • load spectrum generation
  • stress spectrum generation
  • S-N Analysis
  • ?-N Analysis
  • gust load generation
  • Inner load interpretation
  • S-N curve generation/display
  • crack growth analysis

 

FLSG (Fatigue Load Spectrum Generator)
Feature
FLSG generate operational load spectrum for aircraft structural fatigue analysis and verifies the generated spectrum, and issues a summary report of the result.

 

Spec
  • summary of fatigue load spectrum generation results
  • design limit load verification
  • generated spectrum maximum / minimum load comparison
  • creation/display of Load Exceedance Curve