Pop's Props Zing

{{Short description|American homebuilt light aircraft}}

{{Use mdy dates|date=January 2023}}

{{Use American English|date=January 2023}}

{{Infobox Aircraft Begin

| name=Zing

| image=

| caption=

}}{{Infobox Aircraft Type

| type=Kit aircraft

| national origin=United States

| manufacturer=Pop's Props
Simplex Aeroplanes

| designer=Scott Land

| first flight=1996

| introduced=

| retired=

| status=In production

| primary user=

| more users=

| produced=

| number built=5 (1998)

| developed from= Pop's Props Cloudster

| variants with their own articles=

}}

The Pop's Props Zing is a single seat, open-cockpit, parasol wing, single-engine monoplane, first flown in 1996. The aircraft was designed by Scott Land and produced by Pop's Props of Cooksville, Illinois in the form of plans and an aircraft kit. The company is no longer in business and the aircraft kit is now available from Simplex Aeroplanes of Old Saybrook, Connecticut.Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page B-65. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 222. BAI Communications. {{ISBN|0-9636409-4-1}}Downey, Julia: 1999 Kit Aircraft Directory, Kitplanes, Volume 15, Number 12, December 1998, page 62. Primedia Publications. ISSN 0891-1851{{cite web|url = http://simplexaero.com/|title = Home|accessdate = 28 February 2012|last = Simplex Aeroplanes|date = 2011}}

The aircraft was designed for the FAR 103 Ultralight Vehicles category, including the category's {{convert|254|lb|kg|0|abbr=on}} empty weight limit. The standard empty weight of the Zing is {{convert|249|lb|kg|0|abbr=on}}.

Design and development

The Zing was designed as a higher performance version of the Cloudster, with a smaller wing with a span {{convert|4.5|ft|m|1|abbr=on}} less than the Cloudster, yielding higher cruise speeds at the price of a higher stall speed.

The Zing is constructed of wood and covered in aircraft fabric. The landing gear is conventional with sprung aluminum main gear and a steerable tailwheel. The double surfaced wing is strut-braced with two parallel main struts and jury struts per side. The wing features 60% span ailerons and the whole wing can be removed for transport or storage. Available engines include the Kawasaki 340-LC liquid-cooled engine of {{convert|35|hp|kW|0|abbr=on}}, the Half VW of {{convert|45|hp|kW|0|abbr=on}} as well as several Rotax engines. The designer recommended power range is {{convert|28|to|40|hp|kW|0|abbr=on}}.

Due to the laborious wood and fabric construction, builder completion time is estimated at 300-500 man-hours from plans or 200 man-hours from the kit. The kit is available as a single kit or as several sub-kits.

Specifications (Zing)

{{Aircraft specs

|ref=Cliche, Purdy and Kitplanes

|prime units?=imp

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|crew=One

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|length ft=17

|length in=0

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|span ft=25

|span in=5

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|height ft=5

|height in=10

|height note=

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|wing area sqft=118.8

|wing area note=

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|airfoil=

|empty weight kg=

|empty weight lb=249

|empty weight note=

|gross weight kg=

|gross weight lb=500

|gross weight note=

|fuel capacity=5 US gallons (19 litres)

|more general=

|eng1 number=1

|eng1 name=Kawasaki 340-LC

|eng1 type=

|eng1 kw=

|eng1 hp=35

|prop blade number=2

|prop name=wooden propeller

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|max speed kmh=

|max speed mph=70

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=55

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=26

|stall speed kts=

|stall speed note=

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|range km=

|range miles=

|range nmi=120

|range note=

|endurance=

|ceiling m=

|ceiling ft=6000

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=675

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=4.2

|wing loading note=

|power/mass=

|thrust/weight=

|more performance=

|avionics=*none

}}

See also

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References

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