.: Chris Cooper's Revell & OzMods C-2 Greyhound "Hawkeye"

Brand:
Revell
Scale:
1/144th
Modelling Time:
3 months
PE/Resin Detail:
OzMods Conversion
Comments:

"Revell E-2 Geyhound with OzMods C-2 Hawkeye conversion kit & propellors"

Grumman C-2 Greyhound

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C-2 Greyhound
A C-2A in July 1988, based at Naval Air Station, Sigonella (Sicily, Italy)
Role Carrier-capable transport / Carrier onboard delivery
National origin United States
Manufacturer Grumman
Northrop Grumman
First flight 18 November 1964
Introduction 1966
Retired 1987, C-2A
Status 39 C-2(R) in service
Primary user United States Navy
Produced C-2A: 1965-1968
C-2A(R): 1985-1989
Number built 58
Unit cost US$38.96 million[1]
Developed from Northrop Grumman E-2 Hawkeye

The Grumman C-2 Greyhound is a twin-engine, high-wing cargo aircraft, designed to carry supplies and mail to and from aircraft carriers of the United States Navy. Its primary mission is carrier onboard delivery (COD). The aircraft provides critical logistics support to carrier strike groups. The aircraft is mainly used to transport high-priority cargo, mail and passengers between carriers and shore bases, and can also deliver cargo like jet engines and special stores.

Prototype C-2s first flew in 1964 and production followed the next year. The initial Greyhound aircraft were overhauled in 1973. More C-2s were ordered in the 1980s. Further improvements to the C-2 have followed.

Design and development

The C-2 Greyhound, a derivative of the E-2 Hawkeye, shares wings and power plants with the E-2, but has a widened fuselage with a rear loading ramp. The first of two prototypes flew in 1964. After successful testing, Grumman began production of the aircraft in 1965. The C-2 replaced the piston-engined Grumman C-1 Trader in the COD role. The original C-2A aircraft were overhauled to extend their operational life in 1973.

Interior view from the tail of a C-2A Greyhound assigned to Fleet Logistics Support Squadron 40 (VRC-40)

Powered by two Allison T56 turboprop engines, the C-2A can deliver up to 10,000 pounds (4,500 kg) of cargo, passengers or both. It can also carry litter patients in medical evacuation missions. A cage system or transport stand restrains cargo during carrier launch and landing. The large aft cargo ramp and door and a powered winch allow straight-in rear cargo loading and unloading for fast turnaround. The Greyhound's ability to airdrop supplies and personnel, fold its wings, and generate power for engine starting and other uses provide an operational versatility found in no other cargo aircraft.

The aircraft has four vertical stabilizers because of aircraft carrier hangar deck height restrictions. Only three of these stabilizers have working rudders.[citation needed] For adequate directional control of an aircraft of this size, a single rudder would have been too tall. It also places the outboard rudder surfaces directly in line with the propeller wash, providing effective yaw control down to low airspeeds, as during takeoff and landing.

In 1984, the Navy ordered 39 new C-2A aircraft to replace older airframes. Dubbed the Reprocured C-2A (C-2A(R)) due to the similarity to the original, the new aircraft has airframe improvements and better avionics. The older C-2As were phased out in 1987, and the last of the new models was delivered in 1990.

Upgrades

A C-2A taxis prior to takeoff on a flight to USS John F. Kennedy (CV-67) in Feb 1984. This was the first Greyhound delivered in 1966.

The 36 C-2A(R)s are undergoing a critical Service Life Extension Program (SLEP). The lifespan of the C-2A(R) was 10,000 hours, or 15,000 carrier landings; current plans require the C-2A to perform its mission supporting battle group operational readiness through 2015. The landing limit is quickly approaching for most of the airframes, and the SLEP will increase the Greyhound's projected life to 15,000 hours or 36,000 landings. Once the program is complete, it will allow the current 36 aircraft to operate until 2027. The SLEP includes structural improvements to the center wing, navigational upgrades including the addition of GPS and the dual CAINS II Navigation System, the addition of crash survivable flight incident recorders, and a Ground Proximity Warning System. The first upgraded C-2A(R) left NAVAIR Depot North Island on 12 September 2005, after sitting on the ground for three and a half years while the SLEP was developed and installed. A second airframe is currently nearing completion and it is anticipated that the remaining 34 aircraft will all undergo the SLEP upgrade within the next five years as operations and schedule permit. The eight-bladed NP2000 propeller is another part of this upgrade and is expected to be installed by 2010.[2][dead link]

In November 2008, the company also obtained a $37M contract for the maintenance, logistics and aviation administration services over five years for the C-2A fleet assigned to VX-20 test and evaluation squadron at Patuxent River. Northrop Grumman is currently working on an upgraded C-2 version, and has offered to modernize the fleet with components common to the E-2D Hawkeye.[3]

The C-2 Greyhound is competing with the V-22 Osprey for use as the future Carrier Onboard Delivery aircraft. Northrop Grumman has proposed modernizing the C-2 rather than replacing them with the Osprey. The proposal is to give the Greyhounds the same wings, glass cockpit, and engines as the E-2D Advanced Hawkeye in two phases. The first would replace the engines and avionics, and the second would replace the wing structures. Installing the Rolls Royce T56-427A engines would cut fuel consumption by 13-15 percent with the same 8-bladed propeller. Having the same cockpit as the E-2D would deliver a 10 percent savings on integrated logistics support over the life of the airplane. With the new engines, the C-2 would be able to take off with a 10,000 lb payload in 125 degree heat and fly in excess of 1,400 nmi (1,600 mi). Similar performance by the C-2A would require engine temperatures at 70 degrees F, with higher temperatures requiring trading fuel for payload. One of the Greyhound's most important features is its internal volume of 860 cubic feet of cargo space.[4]

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