1967-02-01

C-5A Flight Control System 670574

The C-5A flight control system is explained with individual schematics illustrating each subsystem. Several mechanical failure situations and necessary pilot actions are described. The distribution of hydraulic power and its importance on an airplane which uses fully powered hydraulic flight controls is explained. The handling quality requirements and some results of ground based simulation studies are presented.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
X