What you will study
Control paths and adjustment consequences
Trace power, condition and propeller controls. Practise dry geometry, deadband position and width, idle branches, reverse, governing, torque and beta proof through fifteen guided stages.
Integrated faults and repeat proof
Seven integrated fault cases link the as-found condition to the appropriate source-supported branch. Explain which checks an adjustment invalidates, repeat the required proof and restore the system.
Independent job decisions
Solve an unnamed independent case after the guided stages. Saved progress, hints and page-specific Manual Help support remediation; the separate 50-question final requires 80%.
Learning outcomes
- Trace power, condition and propeller control paths.
- Predict the consequences of a rigging adjustment.
- Select a source-supported branch from the as-found evidence.
- Repeat invalidated checks and document restoration of the complete job.
Aircraft and course applicability
Standard King Air B300/B300C PT6A-60A installation using the 55-page Rev E course manual and identified source figures. Other engine or airframe configurations need their own applicable instructions.
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.
