Aircore Cadet

{{Short description|American ultralight aircraft}}

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

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

{{Infobox aircraft begin

| name=Cadet

| image=

| caption=

}}{{Infobox aircraft type

| type=Ultralight aircraft

| national origin=United States

| manufacturer=Aircore Industries

| designer=Jim Scott

| first flight=

| introduced=

| retired=

| status=Production completed

| primary user=

| more users=

| produced=

| number built=between 30-50 kits shipped

| developed from=

| variants with their own articles=

}}

The Aircore Cadet is an American ultralight aircraft that was designed by Jim Scott and produced by Aircore Industries in the early 1980s. The aircraft was supplied as a kit for amateur construction.Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page E-9. Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}{{Cite web|url = http://virtualultralightmuseum.com/c.htm|title = Aircraft C|accessdate = 4 November 2011|last = Virtual Ultralight Museum|archiveurl = https://web.archive.org/web/20150406060220/http://virtualultralightmuseum.com/c.htm|archivedate = 6 April 2015}}

Design and development

The Cadet was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of {{convert|254|lb|kg|0|abbr=on}}. The aircraft has a standard empty weight of {{convert|248|lb|kg|0|abbr=on}}. It features a strut-braced high-wing, single-seat, open cockpit, single tractor engine configuration, and is equipped with tricycle landing gear.

The aircraft is made from bolted together aluminum alloy tubing, with the wings and tail covered in Dacron sailcloth. Its {{convert|30|ft|m|1|abbr=on}} span wing employs "V" lift struts and jury struts. The aircraft keel is an aluminum tube that runs from the tail, mounts the wings and the engine at its forward end. The standard factory-supplied engine is the {{convert|28|hp|kW|0|abbr=on}} Rotax 277, driving a {{convert|60|in|cm|0|abbr=on}} diameter fixed-pitch propeller with a {{convert|28|in|cm|0|abbr=on}} pitch. The pilot sits on an open seat without a windshield. The control system is conventional three-axis, with half-span ailerons. The main landing gear is sprung steel and the nosewheel incorporates steering. There is a small tail caster to protect the tail. Brakes are optionally available.

Reviewer Andre Cliche describes the Cadet as "a clean and simple design that is inexpensive to maintain."

Specifications (Cadet)

{{Aircraft specs

|ref=Cliche.

|prime units?=imp

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|crew=one

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|span ft=30

|span in=0

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|wing area sqft=163

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|empty weight kg=

|empty weight lb=248

|empty weight note=

|gross weight kg=

|gross weight lb=530

|gross weight note=

|fuel capacity={{convert|5|u.s.gal}}

|more general=

|eng1 number=1

|eng1 name=Rotax 277

|eng1 type=single cylinder, two-stroke aircraft engine

|eng1 kw=

|eng1 hp=28

|prop blade number=2

|prop name=wooden

|prop dia m=

|prop dia ft=5

|prop dia in=0

|prop dia note=, 28 in (71 cm) pitch

|perfhide=

|max speed kmh=

|max speed mph=55

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=45

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=18

|stall speed kts=

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|never exceed speed mph=73

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|range km=

|range miles=110

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|ceiling m=

|ceiling ft=12500

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|g limits=+6/-4

|roll rate=

|glide ratio=8:1

|climb rate ms=

|climb rate ftmin=600

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=320

|sink rate note=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=3.25

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}}

{{aircontent

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References

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