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The Pilots Desk
variant of the AgustaWestland AW101

Lockheed Martin VH-71 Kestrel

Lockheed Martin VH-71 Kestrel

The Lockheed Martin VH-71 Kestrel was a variant of the AgustaWestland AW101 helicopter that was being manufactured to replace the United States Marine Corps' Marine One U.S. presidential transport fleet. Originally marketed for various competitions as the US101, it was developed and manufactured in the US by a consortium headed by Lockheed Martin, consisting of Lockheed Martin Systems Integration – Owego (LMSI), AgustaWestland and Bell Helicopter. In January 2005, the US101 was selected for the VXX Presidential Helicopter Replacement Program, and was promptly re-designated as the VH-71. However, development was subject to delays, cost overruns, and engineering issues; Lockheed attributed much of these issues to unanticipated and extensive modifications being demanded by the government that had been absent from the request for proposal (RFP) issued. A Government Accountability Office (GAO) report in 2011 also recognised that a lack of flexibility and compromise on the part of the government had negatively impacted the program. By late 2008, the cancellation of the VH-71 was looking increasingly likely. In February 2009, President Barack Obama asked Secretary of Defense Robert Gates about placing the project on hold or canceling it because of its high cost: over $13 billion for the planned 28 helicopters. In June 2009, the U.S. Navy terminated the contract after spending about $4.4 billion and taking delivery of nine VH-71s. After the cancellation, the delivered helicopters were sold to Canada for $164 million, where they were used as source of spare parts for its fleet of AgustaWestland CH-149 Cormorant search-and-rescue helicopters.

Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.

Manufacturer
Bell Textron
Country of origin
United States
First flight
2007-07-03
Length
19.53 m

Specifications

Cruise speed
150 kt
Max speed
167 kt
Range
750 nm
Service ceiling
15,010 ft
Rate of climb
2,010 ft/min
Max takeoff weight
34,392 lb
Empty weight
23,149 lb
Powerplant
General Electric CT7-8E
Engines
3
Seats
18
Length
64.1 ft
Height
21.7 ft
Number built
9

Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).

Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.