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#2354

Kaman K-MAX

first flew 1991· medium lift helicopter

🚁 helicopter turboshaft ✓ still flying
Kaman K-MAX, photo 1 of 1
1/1 André Völzke· CC BY-SA 3.0

what is it?

The Kaman K-MAX (company designation K-1200) is a helicopter with intermeshing rotors (synchropter) designed and produced by the American manufacturer Kaman Aircraft. It first flew in 1991 and was produced for military and civilian operators. Developed in the 1980s and 1990s, the K-MAX builds on the work of the German aeronautical engineer Anton Flettner.

How to recognise it: 1 turboshaft engine · 14.7 m main rotor

base stats

  • range 556 kmwithout refuelling
  • size 2,948 kgmax take-off weight
  • built 38made in total

Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).

fun facts

  • First flew 35 years ago, in 1991.
  • Rotor of 14.7 m: about 3 cars parked nose to tail.

turboshaft: A turbine that turns a shaft, usually a helicopter rotor.

spec sheet

first flight
1991-12-23
introduced
1994
status
still flying
number built
38
role
medium lift helicopter
makers
Kaman Corporation
engines
1× Honeywell T5317A-1
crew
1
length
15.9 m
rotor diameter
14.7 m
height
4.1 m
max take-off weight
2,948 kg
top speed
—
range
556 km
ceiling
4,572 m

Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.

Sources: Wikidata Q1722851, Wikipedia: Kaman K-MAX (CC BY-SA 4.0).Updated 2026-10-24.

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