Zenair CH 640

{{Short description|Canadian homebuilt light aircraft}}

{{Use dmy dates|date=January 2022}}

{{Use Canadian English|date=January 2022}}

{{Infobox aircraft begin

| name=CH 640

| image=Zenair Zodiac CH-640 N756GA.jpg

| caption=

}}{{Infobox aircraft type

| type=Kit aircraft

| national origin=Canada

| manufacturer=Zenair

| designer=Chris Heintz

| first flight=

| introduced=

| retired=

| status=In production

| primary user=

| more users=

| produced=

| number built=50 (Dec 2011)

| developed from= AMD Alarus

| variants with their own articles=

}}

The Zenair Zodiac CH 640 is a Canadian light aircraft that was designed by Chris Heintz and is produced by Zenair in the form of a kit for amateur construction.Vandermeullen, Richard: 2011 Kit Aircraft Buyer's Guide, Kitplanes, Volume 28, Number 12, December 2011, page 77. Belvoir Publications. {{ISSN|0891-1851}}{{Cite web |url=http://www.kit-plane.com/index640.html |title=Zodiac CH 640 |access-date=13 December 2011 |last=Zenair |date=n.d. |url-status=dead |archive-url=https://web.archive.org/web/20111202041535/http://www.kit-plane.com/index640.html |archive-date=December 2, 2011 }}

File:Zenith CH-640.jpg

Design and development

The CH 640 was developed from the two-seat type certified AMD Alarus, also called the Zenair CH 2000, by increasing the span of the wings and stabilator, to accommodate the larger engine and increase in gross weight. The design was also influenced by the Zenith CH 601 and the Zenair CH 300. The design goals were to produce a simple four-seat aircraft capable of flying cross country flights with full seats.

The CH 640 is a four-seat, low-wing touring aircraft with tricycle landing gear and a single engine in tractor configuration. It has a standard empty weight of {{convert|1147|lb|kg|0|abbr=on}}, a gross weight of {{convert|2200|lb|kg|0|abbr=on}} and an acceptable engine power range of {{convert|150|to|240|hp|kW|0|abbr=on}}. The recommended engine is the Lycoming O-360 of {{convert|180|hp|kW|0|abbr=on}}.

The aircraft is made from 6061-T6 aluminum. Its {{convert|31.5|ft|m|1|abbr=on}} span wing is a cantilever structure and is equipped with flaps. The {{convert|46|in|cm|1|abbr=on}} wide cabin is accessed via two gull-winged doors. The construction time from the factory-supplied standard kit is estimated at 1250 hours to complete and the quick-build kit at 750 hours. In 2011 the kit cost US$28,995, while finishing a completed aircraft was estimated to cost between US$45,000 to $99,000, depending on options, engine and avionics installed. In December 2011 there were 50 completed and flying.

Operational history

In evaluating the CH 640 AeroNews Network said, "It's a tremendously stable little airplane and a fair amount faster than what you might think."

Specifications (CH 640)

{{Aircraft specs

|ref=Kitplanes{{Cite web|url = http://www.kit-plane.com/specifications.html|title = Zodiac CH 640 Specifications|access-date = 13 December 2011|last = Zenair|date = n.d.|url-status = dead|archive-url = https://web.archive.org/web/20111214230540/http://www.kit-plane.com/specifications.html|archive-date = 14 December 2011}}

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|crew=one

|capacity=three passengers

|length m=

|length ft=23

|length in=0

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|span ft=31

|span in=6

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|height ft=7

|height in=4

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|wing area sqft=150

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|empty weight kg=

|empty weight lb=1147

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|gross weight lb=2200

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|fuel capacity=standard tanks: {{convert|38|u.s.gal}}, optional tanks: {{convert|46|u.s.gal}}

|more general=

|eng1 number=1

|eng1 name=Lycoming O-360

|eng1 type=four cylinder, horizontally opposed, four-stroke piston engine

|eng1 kw=

|eng1 hp=180

|prop blade number=2

|prop name=metal propeller

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|perfhide=

|max speed kmh=

|max speed mph=160

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=150

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=47

|stall speed kts=

|stall speed note=flaps down

|never exceed speed kmh=

|never exceed speed mph=175

|never exceed speed kts=

|never exceed speed note=

|range km=

|range miles=510

|range nmi=

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|endurance=

|ceiling m=

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|g limits=+5.7/-2.9

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|climb rate ftmin=950

|climb rate note=

|time to altitude=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=14.6

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}}

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|related=

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References

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