Grumman C-2A Greyhound (reprocured)

Explore the Grumman C-2A Greyhound (reprocured) in side view and top view to compare its silhouette and proportions.

Grumman C-2A Greyhound (reprocured), side profile
Grumman C-2A Greyhound (reprocured), side profile
17.32 m
Grumman C-2A Greyhound (reprocured), top view
Grumman C-2A Greyhound (reprocured), top view
24.56 m

From Wikipedia

The Grumman C-2 Greyhound is a retired twin-engine, high-wing aircraft designed to carry supplies, mail and passengers to and from aircraft carriers of the United States Navy. Its primary mission was carrier onboard delivery (COD). The aircraft provided critical logistics support to carrier strike groups. The aircraft was mainly used for high-priority cargo such as jet engines and special stores, mail, and passengers between carriers and shore bases. Prototype C-2s first flew in 1964, and production followed the next year. The initial Greyhound aircraft were overhauled in 1973.

Read on Wikipedia

Summary of “Grumman C-2 Greyhound” from Wikipedia, the free encyclopedia, used under CC BY-SA 4.0. Retrieved 2026-10-11.

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Use these drawings for anything, commercial too, under Creative Commons Attribution 4.0 International. Credit us like this:

Drawing of the Grumman C-2A Greyhound (reprocured) by AirwayControl Aircraft Library (https://aircraft.intelsystems.ai/aircraft/C2/), CC BY 4.0

Specifications

Length
17.32 m
Wingspan
24.56 m
Max take-off weight
27.22 t
Cruise speed
465 km/h
Max speed
635 km/h
Range
2,408 km
Ceiling
10,211 m
Engines
2 × Allison T56-A-425 turboprop engines
Power
4,600 shp (3,400 kW) each
First flight
1964
In service
1966

From the AirwayControl spec register, curated from Wikipedia and manufacturer pages. Figures vary by variant.