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Information About

C-40 Clipper




The Boeing C-40 Clipper is the military version of the Boeing 737 airline transport. It is currently used by the United States Navy (C-40A) and United States Air Force (C-40B and C).

NAVY USE OF C-40


The C-40A Clipper provides critical logistics support to the United States Navy. Its flight deck features a flight management computer system with an integrated GPS . It is compatible with future GATM/FANS operating environment (RNP-1). It is RVSM capable. It has the Traffic Alert and Collision Avoidance System II on board. It also has an enhanced ground proximity warning system, predictive wind shear, head-up display and TACAN / UHF / IFF functions.

The U.S. Naval Reserve —which operates and maintains the aircraft—is the first customer for the newest member of the Boeing Next-Generation 737 family. The Clipper was ordered by the Navy to replace its fleet of aging C-9 Skytrain s. The C-40A is the first new logistics aircraft in 17 years to join the Naval Reserve . Currently, the Naval Reserve provides 100 percent of the Navy's worldwide in-theater medium and heavy airlift.

The Clipper meets or exceeds international noise and environmental requirements that plague the current fleet of Naval Reserve C-9s. It is also more fuel-efficient and offers increased range and payload capabilities.

The 737-700C aircraft is certified to operate in an all-passenger (121 passengers), all-cargo or combination ("combi") configuration that will accommodate up to three cargo pallets and 70 passengers on the main deck.

The Navy purchased the airplanes using standard commercial practices, and ordered six of the 737-700C models. The first two of four aircraft were delivered on April 21 , 2001 , to Logistics Support Squadron Fifty Nine ( VR-59 ) at the Naval Air Station/Joint Reserve Base Fort Worth, Texas . The remainder later in the year. The fifth and sixth aircraft were delivered in August 2002 to VR-58 at the Naval Air Station, Jacksonville, Florida . A seventh one was acquired on November 22 , 2004 , while the eighth will be delivered in early 2005 .


AIR FORCE USE OF C-40

The United States Air Force selected the C-40B, a military version of the Boeing 737 -700 Boeing Business Jet , to replace the aging fleet of C-137 aircraft for U.S. combatant commanders. The Air Force awarded the medium lift contract in August 2000 . By using commercial off-the-shelf acquisition practices and a new Lease program for the C-40C model, the Air Force reached a benchmark for aircraft procurement. The C-40C was the first military aircraft to be acquired in this manner. The 201st Airlift Squadron, Washington, D.C. Air National Guard , acquired two C-40C aircraft in October 2002 . The C-40C is intended to replace the aging C-22 . The 89th Airlift Wing acquired its first C-40B aircraft in December 2002. Both units are based at Andrews Air Force Base , Maryland . The 15th Airlift Wing, Hickam AFB , Hawaii , acquired its C-40B for U.S. Pacific Command in February 2003 .

The cabin area is equipped with a crew rest area, distinguished visitor compartment with sleep accommodations, two galleys and business class seating with worktables.

The C-40B is designed to be an "office in the sky" for senior military and government leaders. Communications are paramount aboard the C-40B which provides Broadband data/video transmit and receive capability as well as clear and secure voice and data communication. It gives combatant commanders the ability to conduct business anywhere around the world using on-board Internet and local area network connections, improved telephones, satellites, television monitors, and facsimile and copy machines. The C-40B also has a computer-based passenger data system. The C-40 is to replace the C-9 Skytrain II , the military version of the McDonnell Douglas DC-9 in USAF inventory.


SPECIFICATIONS <!-- (VARIANT) -->

  include 'capacity' Field yes
  plane Or Copter plane
  jet Or Prop prop
  include 'armament' Field no
  switch Order Of Units no
  crew 4
  capacity Murfle
  length Main 110 ft 4 in
  length Alt 3363 m
  span Main 112 ft 7 in
  span Alt 3432 m
  height Main 41 ft 2 in
  height Alt 1255 m
  area Main ft
  area Alt m
  empty Weight Main 126,000 lb
  empty Weight Alt 57,150 kg
  loaded Weight Main 134,000 lb
  loaded Weight Alt 61,000 kg
  max Takeoff Weight Main 171,000 lb
  max Takeoff Weight Alt 78,000 kg
  engine (jet) CFM International CFM-56 -7 SLST
  type Of Jet Turbofan s
  number Of Jets 2
  thrust Main 27,300 lbf
  thrust Alt 121 kN
  power Main hp
  power Alt kW
  max Speed Main 534 kt
  max Speed Alt 615 mph, 990 km/h
  cruise Speed Main mph
  cruise Speed Alt km/h
  range Main 3,000 nm
  range Alt 3,500 mi, 5,600 km
  ceiling Main 41,000 ft
  ceiling Alt 12,500 m
  climb Rate Main ft/min
  climb Rate Alt m/s
  loading Main lb/ft&sup2
  loading Alt kg/m&sup2
  thrust/weight 0407
  power/mass Main hp/lb
  power/mass Alt kW/kg




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