text: Chapter 5
  UC-35 AIRCRAFT
  5-13. The UC-35 is a twin-engine turbofan medium range aircraft. Its principle mission is air movement of
  passengers and cargo (figure 5-7 and table 5-7).
  Figure 5–7. UC-35 aircraft
  Table 5–7. UC-35 aircraft specifications
  Specifications:
  Fuselage Length 48 feet 9 inches
  Height 15 feet 0 inches
  Main Wing Span 54 feet 2 inches
  Propulsion 2x JT15D-5D turbofan jet engines
  Maximum Gross Take-Off Weight 16,300 pounds
  Maximum Ceiling 45,000 feet mean sea level
  Cruise Airspeed 430 knots
  Range 2,925 kilometers
  AN/MSQ-135 MOBILE TOWER SYSTEM
  5-14. Organic to the air traffic company in the CAB and the airfield operations battalion, the AN/MSQ-135
  mobile tower system is a rapid-deployable ATC tower and airfield lighting system that quickly establishes
  ATS for arrival, departure, and ground operations. Equipment is included to remotely command airfield
  operations, including control of existing airfield lighting. Controllers manage airspace from the surface to
  10,000 feet out to a 5-mile radius. When assisted by appropriate navigation aids (not organic), the
  AN/MSQ-135 provides ATS in all-weather conditions, night or day, for military and civilian aircraft. The
  AN/MSQ-135 is transportable by all standard land, rail, and sea methods. Additionally, the complete
  AN/MQS-135 is transportable by C-17 and larger FW aircraft. However, only the ATC tower, airfield
  lighting system generator/equipment trailer, airfield lighting system lighting/equipment trailer, and airfield
  lighting system movers 1 and 2 can be sling-loaded by CH-47 and larger RW aircraft. Figure 5-8, page 5-
  11, depicts an AN/MSQ-135. More information can be found in TC 3-04. 6.