An aircraft air management system comprising: a support structure; a fan air plenum; and a bleed valve control system (143, 243) mounted to the support structure adjacent to the fan air plenum (32, 232) within an aircraft, the bleed valve control system (143, 243) comprising: a bleed valve module (144, 244) comprising: a pipe (152, 252) for containing a flow of bleed air, the pipe comprising a plurality of inlets (28, 30) and an outlet (140, 240); a plurality of bleed valves (156a-c, 256a-c) connected to the pipe 152, 252) to control the flow of bleed air in the pipe (152, 252); a plurality of pneumatic actuators (158a-c, 258a-c) connected to the plurality of bleed valves (156a-c, 256a-c) to actuate the plurality of bleed valves (156a-c, 256a-c); and a pneumatic valve controller (146, 270) comprising a plurality of torque motors (164a-c, 264a-c), wherein the pneumatic valve controller (146, 270) is within the fan air plenum (32, 232); a plurality of pneumatic control lines (148a-c, 248a-c); and a pneumatic supply line (150, 250) connecting the pipe (152, 252) to the pneumatic valve controller (146, 270) to supply pressurized air to the pneumatic valve controller (146,270). a support structure; a fan air plenum; and a bleed valve control system (143, 243) mounted to the support structure adjacent to the fan air plenum (32, 232) within an aircraft, the bleed valve control system (143, 243) comprising: a bleed valve module (144, 244) comprising: a pipe (152, 252) for containing a flow of bleed air, the pipe comprising a plurality of inlets (28, 30) and an outlet (140, 240); a plurality of bleed valves (156a-c, 256a-c) connected to the pipe 152, 252) to control the flow of bleed air in the pipe (152, 252); a plurality of pneumatic actuators (158a-c, 258a-c) connected to the plurality of bleed valves (156a-c, 256a-c) to actuate the plurality of bleed valves (156a-c, 256a-c); and a pneumatic valve controller (146, 270) comprising a plurality of torque motors (164a-c, 264a-c), wherein the pneumatic valve controller (146, 270) is within the fan air plenum (32, 232); a plurality of pneumatic control lines (148a-c, 248a-c); and a pneumatic supply line (150, 250) connecting the pipe (152, 252) to the pneumatic valve controller (146, 270) to supply pressurized air to the pneumatic valve controller (146,270). a bleed valve module (144, 244) comprising: a pipe (152, 252) for containing a flow of bleed air, the pipe comprising a plurality of inlets (28, 30) and an outlet (140, 240); a plurality of bleed valves (156a-c, 256a-c) connected to the pipe 152, 252) to control the flow of bleed air in the pipe (152, 252); a plurality of pneumatic actuators (158a-c, 258a-c) connected to the plurality of bleed valves (156a-c, 256a-c) to actuate the plurality of bleed valves (156a-c, 256a-c); and a pneumatic valve controller (146, 270) comprising a plurality of torque motors (164a-c, 264a-c), wherein the pneumatic valve controller (146, 270) is within the fan air plenum (32, 232); a pipe (152, 252) for containing a flow of bleed air, the pipe comprising a plurality of inlets (28, 30) and an outlet (140, 240); a plurality of bleed valves (156a-c, 256a-c) connected to the pipe 152, 252) to control the flow of bleed air in the pipe (152, 252); a plurality of pneumatic actuators (158a-c, 258a-c) connected to the plurality of bleed valves (156a-c, 256a-c) to actuate the plurality of bleed valves (156a-c, 256a-c); and a pneumatic valve controller (146, 270) comprising a plurality of torque motors (164a-c, 264a-c), wherein the pneumatic valve controller (146, 270) is within the fan air plenum (32, 232); a plurality of pneumatic control lines (148a-c, 248a-c); and a pneumatic supply line (150, 250) connecting the pipe (152, 252) to the pneumatic valve controller (146, 270) to supply pressurized air to the pneumatic valve controller (146,270).