Zivko Edge 540

{{Short description|Racing aircraft in the US}}

{{more citations needed|date=February 2021}}

{{Infobox aircraft

| name = Edge 540

| image = File:Zivko Edge 540 at Red Bull Air Race on Langley Park Monty-1.jpg

| caption = Zivko Edge 540 flying across Langley Park in Perth, Western Australia

| alt = An aircraft flying close to the ground

| type = Competition aerobatic and racing aircraft

| national_origin = United States

| manufacturer = Zivko Aeronautics

| designer =

| first_flight = 1996

| introduction =

| retired =

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File:Edge 540 In Flight 1.jpg

The Zivko Edge 540 manufactured by Zivko Aeronautics is a highly aerobatic aircraft. Capable of a 420 degree per second roll rate and a 3,700 foot per minute climb rate, it has been flown to victory on the international Unlimited aerobatics circuit several times since the mid-1990s. A tandem-seat version is sold as the Edge 540T.

The Zivko Edge 540 is the most common aircraft used in the Red Bull Air Race World Series.

Specifications (Edge 540)

{{Aircraft specs

|ref=Edge 540 Aerobatic Aircraft{{cite web |title= Edge 540 Aerobatic Aircraft |url= http://www.zivko.com/edge/ | publisher = Zivko |access-date=23 September 2019}}

|prime units?=kts

|crew=1 (540T 2)

|length ft=20

|length in=7

|length note=

::::{{cvt|23|ft|0}} 540T

|span ft=24

|span in=4

|span note=

::::{{cvt|25|ft|10|in|0}} 540T

|height ft=7

|height in=9

|height note=

|wing area sqft=98

|wing area note=

::::{{cvt|106|sqft|0}} 540T

|aspect ratio=

|airfoil=John Roncz symmetrical{{cite web |last1= Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website= m-selig.ae | publisher = Illinois U |access-date=16 April 2019}}

|empty weight lb=1170

|empty weight note=

:::: {{cvt|1319|lb|0}} 540T

|gross weight lb=

|gross weight note=

|max takeoff weight lb=1800

|max takeoff weight note=

:::: {{cvt|1950|lb|0}} 540T

  • Maximum aerobatic weight: {{cvt|1550|lb|0}}

:::: {{cvt|1600|lb|0}} 540T

|fuel capacity=AVGAS 100LL {{cvt|61.5|USgal|impgal l}} total ({{cvt|17.5|USgal|impgal l}} fuselage + {{cvt|22|USgal|impgal l}} in each wing)

|more general=

|eng1 number=1

|eng1 name=Lycoming AEIO-540-EXP (modified)

|eng1 type=6-cylinder air-cooled horizontally-opposed piston engine

|eng1 hp=310

|eng1 note=at 2700 rpm - rated power

::::{{cvt|327|hp}} 540T

|prop blade number=3

|prop name=Hartzell HC-C3YR-4AX composite constant-speed propeller

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|max speed kts=

|max speed note=

|cruise speed kts=

|cruise speed note=

|stall speed kts=51

|stall speed note=(VSO) at {{cvt|1550|lb|0}}

::::{{cvt|59|kn|mph km/h}} at {{cvt|1950|lb|0}} 540T

|never exceed speed kts=230

|never exceed speed note=

  • Max aerobatic airspeed (Va): {{cvt|170|kn|mph km/h}}

|range nmi=

|range note=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling ft=

|ceiling note=

|g limits=±12

::::±8 540T dual

::::±10 540T solo

|roll rate=420°/sec

|glide ratio=

|climb rate ftmin=3700

|climb rate note=

|time to altitude=

|lift to drag=

|wing loading lb/sqft=12.4

|wing loading note=empty 540T

|fuel consumption lb/mi=

|power/mass=

|more performance=

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}}

See also

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References

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