BELL UH-1D "HUEY"

Year of construction: 1969
License plate: D-xxxx

General

The Bell UH-1D is a variant of the legendary "Huey" family (from UH-1, "Utility Helicopter"), which is one of the best-known and most-built helicopters in the world. Originally developed by Bell Helicopter in the USA, it became a symbol of the Vietnam War and shaped the image of modern air mobility like almost no other aircraft. In the 1960s, the UH-1D, a medium-weight multi-purpose helicopter, was built under license by Dornier in Germany for the German Armed Forces - the "D" in the designation stands for "Dornier", the German licensed manufacturer.

The helicopter is based on the American Bell UH-1, which was originally developed for the US Army. In Germany, the UH-1D was primarily used as a transport, SAR (search and rescue) and liaison helicopter.

Variants at a glance

Version Period Main differences / features
UH-1A from 1959 First series version with 770 kW engine; low payload
UH-1B from 1961 Extended cabin, more powerful T53-L-5 engine, wider rotor blades
UH-1C from 1965 Specially optimized for gunship role, improved control and performance
UH-1D from 1963 (USA) / 1967 (Dornier) Extended airframe (15 seats), Lycoming T53-L-11 engine with 1100 kW
UH-1H from 1966 Same airframe as UH-1D, but more powerful T53-L-13 engine (1400 kW), improved avionics
UH-1N from 1970 Two-motor version (Twin Huey), significantly more powerful
UH-1Y from 2008 Highly modernized version with four-blade rotor, glass cockpit, modern avionics

 

History

Picture right: Historical production of Hueys from the 1950s to 1970s at the Bell plant (USA). Image source: Bell Textron Inc.

UH-1D German Armed Forces

Between 1967 and 1981, over 350 aircraft were built for the German Armed Forces, which served in a wide variety of roles: Troop and material transport SAR (Search and Rescue) Liaison and VIP flight Disaster control and forest fire fighting The German UH-1D differed slightly from the US version in terms of technology due to specific avionics, instrumentation in metric units and adaptations to NATO standards.

Highlights

Year of construction

1969

Empty weight - kg

2140

Maximum speed - km/h

165

Technical data

Height - m

4.26

Width - m

2.43

Length - m

17.41