Understand how flight guidance becomes control-surface response

ATA 22 • King Air Fusion

TM-025B | King Air Fusion Flight Guidance & Troubleshooting

Distributed architecture

Paired guidance computers, displays, servos and pitch trim

Modes & startup tests

Armed versus active modes and preflight-test evidence

Diagnostic evidence

Compare command, communication and physical response
Beechcraft B300/B300C with the described Fusion FGC-3000/FGP-3000 flight-guidance installation. Includes axis-specific servo/mount comparisons and linked task selection. This is a maintenance-understanding course, not a generic Fusion pilot course or approval for every King Air configuration. Includes a 25-page handbook, interactive workbench, six prediction exercises, eight two-stage cases and a 40-question final.

What's included?

  • 8 focused lessons
  • Completion certificate
  • 40-question final
  • 8 guided fault cases
  • 25-page handbook

Understand the connected system

Trace the paired flight-guidance computers, mode selection, display evidence, servo command and pitch-trim response. Understand why a valid mode command may still be inhibited, how protective disconnects interrupt control, and how axis-specific torque observations distinguish an electronic fault from a mechanical resistance problem. Applies to the described King Air Fusion installation.

Practise defensible fault isolation

Work through six prediction-and-Apply exercises, an axis-specific torque bench, eight two-stage diagnostic cases and twelve independent decisions. Complete all lab requirements and pass the 40-question final at 80%. Study source: supplied King Air 300-series manual 434-590169-0009, ATA 22 study edition dated 1 May 2018. Current aircraft-effective instructions govern physical work. Online completion is separate from observed practical qualification.