What you will study
Trace main-wing and auxiliary fuel to the nacelle
Follow the actual gravity-feed network and distinguish it from motive-fuel-powered auxiliary jet transfer. Separate the nacelle reservoir, auxiliary center-section cell, motive-flow valve and jet transfer pump.
Distinguish engine feed, standby power and crossfeed
Trace the firewall shutoff, engine-driven boost pump, firewall filter, fuel-flow transmitter, heater and engine fuel pump/FCU. Explain the standby hot feed and identify which tank supplies the opposite engine through crossfeed.
Read quantity and pressure findings correctly
Keep FUEL PRESSURE, NO TRANSFER and FUEL CROSSFEED separate. Interpret MAIN/AUX probe selection, individual-probe capacitance, insulation conductance and a controlled P281 connector comparison.
Complete measured and independent jobs
Use ten lesson decisions, ten two-part coached cases and three five-field work records to connect the configuration, complaint, observations, next isolation and required restoration. All lab groups are required before passing; the final contains 40 questions at 80%.
Learning outcomes
- Select the correct schematic using aircraft serial number and S.I. 1021 status.
- Explain main gravity feed, auxiliary transfer and the normal nacelle-to-engine component path.
- Distinguish standby-pump power and crossfeed donor pressure from tank-to-tank transfer.
- Interpret named pressure, quantity, capacitance and insulation findings in their stated test conditions.
- Use a controlled comparison to identify the next isolation task and retain restoration requirements.
Aircraft and course applicability
King Air 200/B200 maintenance-system training using the supplied Model 200-series Maintenance Manual 101-590010-19 Chapter 28, whose list of effective pages is dated November 1, 2024. Individual task dates, aircraft serial numbers and S.I. 1021 status identify each branch. The course does not transfer B300/B300C limits to the 200 series. Original teaching scenarios and measured records support diagnosis practice; the qualitative schematic does not simulate hydraulic rates or automatic command timing. Physical aircraft work requires current applicable controlled instructions and the installed configuration.
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.
