Mil Mi-54

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{{Infobox aircraft begin

| name = Mi-54

| image = Khokhloma helicopter.jpg

| caption = Mil Mi-54 mock up at MAKS 2007 Airshow

}}{{Infobox aircraft type

| type = Civil Utility helicopter

| national origin = Russia

| manufacturer = Mil

}}

The Mil Mi-54 was a projected twin-turbine civil utility helicopter, first announced in 1992, intended to replace the Mi-2 and the Mi-8 helicopters. It was planned to use two 574 kW Saturn/Lyulka AL-32 turboshaft engines, four-bladed main and tail rotors, and fixed tricycle-type landing gear with one nosewheel and two rear wheels on sponsons.{{Cite web |title=Mil Moscow Mi-54 Multirole Transport Helicopter - Aerospace Technology |url=https://www.aerospace-technology.com/projects/mil-mi-54-transport/ |access-date=2022-03-21 |website=www.aerospace-technology.com}}

Specifications

{{Aircraft specs

|ref={{Cite web |title=Mil Moscow Mi-54 Multirole Transport Helicopter - Aerospace Technology |url=https://www.aerospace-technology.com/projects/mil-mi-54-transport/ |access-date=2024-05-11 |website=www.aerospace-technology.com}}

|prime units?=met

|crew=2

|capacity=10-12 passengers

|length m=13.113

|length note=

|height m=4.8

|height note=

|empty weight kg=3000

|empty weight note=

|gross weight kg=

|gross weight note=

|max takeoff weight kg=4700

|max takeoff weight note=with external cargo on the sling, 4,500 kg (9920,802 lb) with internal cargo

|fuel capacity=

|more general=

|eng1 number=2

|eng1 name=Saturn/Lyulka AL-32

|eng1 type=turboshaft engines

|eng1 shp=771

|eng1 note=

|rot number=1

|rot dia m=13.5

|rot area sqm=143.16

|rot area note=

|max speed kmh=280

|max speed note=

|cruise speed kmh=260

|cruise speed note=

|never exceed speed kmh=

|never exceed speed note=

|range km=600

|range note=

|combat range km=

|combat range note=

|ferry range km=

|ferry range note=

|endurance=

|ceiling m=5500

|ceiling note=

|climb rate ms=

|climb rate note=

|time to altitude=

|disk loading kg/m2=

|disk loading note=

|fuel consumption kg/km=

|power/mass=

|more performance=

|avionics=

}}

References

{{Reflist}}