Air Command Commander Sport

{{Infobox Aircraft Begin

| name= Commander Sport

| image=

| caption=

}}{{Infobox Aircraft Type

| type=Autogyro

| national origin=United States

| manufacturer=Air Command International

| designer=

| first flight=

| introduced=

| retired=

| status=Production completed

| primary user=

| more users=

| produced=

| number built=At least one

| program cost=

| unit cost= US$10,670.76 (kit, including engine, 1998)

| developed from= Air Command Commander

| variants with their own articles=

}}

The Air Command Commander Sport is an American autogyro that was designed and produced by Air Command International of Wylie, Texas. Now out of production, when it was available the aircraft was supplied as a kit for amateur construction.Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 316. BAI Communications, 15 July 1998. {{ISBN|0-9636409-4-1}}

Design and development

The Commander Sport was designed to comply with the US Experimental - Amateur-built aircraft rules. It features a single main rotor, a single-seat open cockpit with a small cockpit fairing with a windshield, tricycle landing gear with a steerable nose wheel and wheel pants, plus a tail caster. The standard engine supplied was the twin cylinder, liquid-cooled, two-stroke, dual-ignition {{convert|64|hp|kW|0|abbr=on}} Rotax 582 engine in pusher configuration. The {{convert|50|hp|kW|0|abbr=on}} Rotax 503 and {{convert|40|hp|kW|0|abbr=on}} Rotax 447 engines were factory options.

The aircraft fuselage is made from metal tubing, while the fairing is fiberglass. Its two-bladed rotor has a diameter of {{convert|23.00|ft|m|1|abbr=on}}. The aircraft has a typical empty weight of {{convert|275|lb|kg|abbr=on}} and a gross weight of {{convert|750|lb|kg|abbr=on}}, giving a useful load of {{convert|475|lb|kg|abbr=on}}. With full fuel of {{convert|9|u.s.gal}} the payload for the pilot and baggage is {{convert|421|lb|kg|abbr=on}}.

The standard day, sea level, no wind, take off with a {{convert|64|hp|kW|0|abbr=on}} engine is {{convert|100|ft|m|0|abbr=on}} and the landing roll is {{convert|5|ft|m|0|abbr=on}}.

Original factory kit options were a pre-rotator, cockpit fairing, wheels pants and long range fuel tank. The manufacturer estimated the construction time from the supplied kit as 30 hours and put completion time as 3–4 days work.

Specifications (Commander Sport)

{{Aircraft specs

|ref=Purdy

|prime units?=imp

|genhide=

|crew=one

|capacity=

|length m=

|length ft=10.66

|length in=

|length note=

|width m=

|width ft=

|width in=

|width note=

|height m=

|height ft=

|height in=

|height note=

|airfoil=

|empty weight kg=

|empty weight lb=275

|empty weight note=

|gross weight kg=

|gross weight lb=750

|gross weight note=

|fuel capacity={{convert|9|u.s.gal}}

|more general=

|eng1 number=1

|eng1 name=Rotax 582

|eng1 type=twin cylinder, liquid-cooled, four stroke aircraft engine

|eng1 kw=

|eng1 hp=64

|prop blade number=3

|prop name=ground adjustable, composite

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|rot number=1

|rot dia m=

|rot dia ft=23.00

|rot dia in=

|rot area sqm=

|rot area sqft=415

|rot area note=

|perfhide=

|max speed kmh=

|max speed mph=95

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=65

|cruise speed kts=

|cruise speed note=

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|range km=

|range miles=

|range nmi=

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|endurance=

|ceiling m=

|ceiling ft=15000

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=1200

|climb rate note=

|time to altitude=

|disk loading kg/m2=

|disk loading lb/sqft=1.80

|disk loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=

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}}

References

{{reflist}}