What you will study
Actual measurement and test boundaries
Locate N1 and N2 gearbox drives, torque manifold/transmitter, T5 junction, MT5 and oil sensors. Distinguish an actual sensor test from an injected electrical indication check.
Task-specific calibration and measured comparison
Compare pressure, voltage, resistance, temperature and frequency with the exact installed task band. Keep analog, Meggitt and Pro Line 21 methods distinct.
ITT and fuel-flow reasoning
Separate engine-loop resistance, insulation, early airframe harness and injected temperature. Compare proportional slope, constant offset and later no-adjustment fuel-flow branches.
Concentrator and display reversion
Follow normal DCU and secondary EDC paths, timed comparator observations and Pilot Display NORM/PFD presentation separately. Build a repeatable performance and restoration record.
Learning outcomes
- Select the correct instrument, concentrator and engine-model task branch.
- Trace each actual sensor signal and identify what an injected test excludes.
- Calculate task-specific measured deviations and classify each boundary.
- Distinguish DCU/EDC reversion from MFD/PFD display selection.
- Record comparable performance conditions, repeat results and complete restoration.
Aircraft and course applicability
Systems and measured maintenance-record training for PT6A-41 Model 200 and PT6A-42 B200 engine indication branches in Maintenance Manual 101-590010-19 Chapter 77, supplied LEP November 1, 2024. Individual analog/Regan/Meggitt and Pro Line 21 tasks retain their own serial, equipment and test conditions. B200GT/PT6A-52 performance procedures are outside these examples. Physical maintenance uses complete current applicable instructions and qualified personnel.
WWAOG provides independent training. Online completion records knowledge and simulation achievement; it does not replace observed practical qualification, employer authorization or applicable licensing. Use current aircraft-effective maintenance instructions for physical work.
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