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Boeing C-40C Clipper Airlift

Boeing C-40C Clipper Airlift

Manufacturer: Boeing
Category: Bombers & Strategic Aircraft
  • Maximum Speed 530 mph (Mach 0.8)
  • Range 4,500 to 5,000 nautical miles
  • Payload Capacity 42 to 111 passengers
  • Crew 10, varies by mission

Full Specifications

1. General Information

Name Boeing C-40C Clipper
Manufacturer Boeing
Country of Origin United States
Introduction / In Service Since 2002
Status In operational service
Category High-priority personnel transport
Crew 10, mission dependent
Unit Cost Approximately $70 million, historical figure

2. Dimensions & Structure

Length 110 ft 4 in (33.6 m)
Wingspan 117 ft 5 in (35.8 m)
Height 41 ft 2 in (12.5 m)
Wing Area Not publicly specified in the cited Air Force fact sheet
Empty Weight Not publicly specified
Maximum Takeoff Weight (MTOW) 171,000 lb (77,565 kg)

3. Performance

Maximum Speed 530 mph (Mach 0.8)
Range 4,500 to 5,000 nmi, payload dependent
Combat Radius Not applicable
Service Ceiling 41,000 ft (12,727 m)
Rate of Climb 3,000 ft/min

4. Powerplant

Engine Type 2 × GE CFM56-7B27 turbofans
Thrust (per engine) 27,000 lb
Total Thrust 54,000 lb

5. Payload & Armament

Internal Payload Capacity 42 to 111 passengers
Weapons Bay None
Compatible Weapons None
Hardpoints None

6. Avionics & Systems

Radar System Enhanced weather radar
Navigation Integrated GPS and flight management system
Electronic Warfare (EW) No dedicated combat EW suite publicly identified
Stealth Features None

7. Operational History

Primary Operator U.S. Air Force, including Air National Guard and Air Force Reserve
Conflict Usage Executive and operational support rather than direct combat
Notable Missions Congressional delegations, Cabinet travel, senior leader transport, special envoys and diplomatic support

8. Additional Information

Variants C-40B, C-40C
Successor / Future Replacement No single direct replacement publicly designated
Notable Features Reconfigurable cabin, winglets, military avionics and long-range capability
Estimated Operational Life Dependent on airframe condition, modernization and sustainment

Our Rating

The overall rating is based on review by our experts

3.2
  • Stealth Capability 2 / 10
  • Payload Capacity 3 / 10
  • Range & Endurance 4 / 10
  • Electronic Warfare 3 / 10
  • Maintenance Efficiency 4 / 10

PROS

  1. Flexible 42 to 111 passenger configuration
  2. Long-range executive airlift capability
  3. Proven Boeing 737-derived airframe
  4. Modern navigation and flight safety systems
  5. Suitable for worldwide government and military missions

CONS

  1. Not designed for combat operations
  2. No weapons or dedicated weapons systems
  3. Limited tactical airlift capability
  4. Commercial-derived airframe lacks battlefield protection
  5. Specialized military configuration adds maintenance requirements
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Boeing C-40C Clipper: U.S. Executive Airlift

The Boeing C-40C Clipper is a military executive transport aircraft operated by the U.S. Air Force for high-priority personnel movement, including congressional delegations, Cabinet officials, senior military leaders, special envoys, and other government passengers. Based on the Boeing 737-700 business jet, the C-40C combines a commercial airliner-derived airframe with military avionics, auxiliary fuel capacity, and a flexible passenger cabin. The aircraft entered U.S. military service in the early 2000s and was selected to replace older C-22 aircraft in its executive airlift role.

A major feature of the C-40C is its reconfigurable interior. Unlike the C-40B, which is optimized for combatant commanders and advanced airborne communications, the C-40C can be configured to carry approximately 42 to 111 passengers. This flexibility allows the aircraft to support distinguished visitor missions as well as larger personnel movements.

Manufacturer

Boeing is the prime airframe contractor, while the aircraft uses two GE CFM56-7B27 turbofan engines. The C-40C incorporates the Boeing 737-700 fuselage with winglets and military-specific equipment, including integrated GPS, flight management systems, electronic flight instrumentation, a heads-up display, traffic collision avoidance technology, and enhanced weather radar.

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Speed and Range

The C-40C has a maximum speed of about 530 mph, or approximately Mach 0.8, and can operate at altitudes up to 41,000 feet. Its published unrefueled range is approximately 4,500 to 5,000 nautical miles, depending on payload. Each CFM56-7B27 engine produces about 27,000 pounds of static thrust.

Cost/Price

The U.S. Air Force lists a historical unit cost of approximately $70 million for the C-40 family. This figure should be treated as a historical reference rather than a current procurement price, because configuration, support, modernization, inflation, and acquisition arrangements can significantly affect actual costs.

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