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APU bleed command, priority over engine bleed, backup command path, source transitions and isolation.
Fan-air valve, remote-servo control, precooler heat exchange, dual temperature sensing and thermal protection.
Detailed PADS architecture covering source ducts, left/right manifolds, crossfeed and aircraft pneumatic users.
Understand the regulated path from engine bleed source to manifold without memorizing maintenance test steps.
Complete system-level study of pneumatic sources, distribution, engine bleed regulation, leak protection, indication and maintenance reasoning.
Learn how left/right distribution can be connected or isolated and why configuration changes the system picture.
Pneumatic interfaces with packs, service air, ice protection, engine start, water pressurization, ventilation and aircraft data systems.
Bleed/ground-air pressurization, air manifold, electric pump, pressure control and backup modes.
This Computer-Based Training is generally used for training pilot Type Rated Boeing 737 Next Generation (NG). This is old version of Computer Based Training, used it for reference only. Some of the step, proce…
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