Aeronca Arrow

{{Infobox aircraft

| name=Aeronca Arrow

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| national_origin=United States of America

| manufacturer=Aeronca

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| introduction=1947

| retired=

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The Aeronca Model 9 Arrow was a low-wing all-metal cabin monoplane with retractable landing gear.{{cite book|last1=Simpson|first1=R.W.|title=Airlife's general aviation : a guide to postwar general aviation manufacturers and their aircraft| date=1995| publisher=Airlife| location=Shrewsbury| isbn=9781853105777| edition=2nd}} It was marketed to returning pilots from World War II{{cite book|title=Your personal plane|publisher= Duell, Sloan And Pearce |date=1945 |author=John Paul Andrews}} and unveiled in 1947 but never went into production.

The single prototype (registered NX39581) was destroyed in a crash during a test flight due to propeller failure.

Specifications

{{Aircraft specs

|ref=Jane's all the World's Aircraft 1947{{cite book |title=Jane's all the World's Aircraft 1947 |editor1-last=Bridgman |editor1-first=Leonard |year=1947 |publisher=Sampson Low, Marston & Co |location=London |page=176c}}

|prime units?=imp

|crew=2

|length ft=19

|length in=9

|span ft=30

|height m=

|height ft=

|height in=

|height note=

|wing area sqft=137

|aspect ratio=6.57

|airfoil=

|empty weight lb=850

|gross weight lb=1450

|max takeoff weight kg=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity={{convert|25|USgal|impgal l|abbr=on}}

|more general=

|eng1 number=1

|eng1 name=Franklin 4AC

|eng1 type=4-cyl. horizontally-opposed air-cooled piston engine

|eng1 hp=90

|prop blade number=2

|prop name=wooden fixed pitch propeller

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|max speed mph=135

|cruise speed mph=125

|cruise speed note=

  • Landing speed (flaps): {{convert|48|mph|kn km/h|abbr=on}}
  • Landing speed (no flaps): {{convert|54|mph|kn km/h|abbr=on}}

|stall speed kmh=

|stall speed mph=

|stall speed kts=

|stall speed note=

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|range km=500

|ferry range km=

|ferry range miles=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling m=

|ceiling ft=

|ceiling note=

|g limits=

|roll rate=

|climb rate ftmin=550

|time to altitude=

|wing loading kg/m2=10.6

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=15.9 lb/hp (9.65 kg/kW)

|more performance=

}}

See also

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References

{{reflist}}

Further reading

  • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=31 }}