Zenith STOL CH 701: Difference between revisions
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Revision as of 01:37, 15 May 2010
| CH 701 & CH 750 | |
|---|---|
| |
| Zenair CH 701 on amphibious floats | |
| Role | Sport, personal and trainer aircraft |
| Manufacturer | Zenith Aircraft Company |
| Designer | Chris Heintz |
| First flight | 1986 |
| Introduction | 1986 |
| Produced | 1986-present |
| Number built | 750[1] |
| Variants | Zenith STOL CH 801 |
The Zenith STOL CH 701 and CH 750 are a family of light, two place aircraft designed by Canadian aeronautical engineer Chris Heintz through his Midland, Ontario based company, Zenair. The CH 701 first flew in 1986 and the design is still in production in 2008.[1] The CH 750 was first introduced in 2008.[2]
Manufacturers
The kit is produced and distributed in the USA by the Zenith Aircraft Company, and complete drawings (blueprints and manuals) are also available for the design.
Several distributors modify existing kits into so called quick-build kits.
In Europe, the CH 701 was manufactured under license by Czech Aircraft Works (CZAW) from 1992 until 2006, when the license agreement was ended.
In Iran, Raht-Aseman produces an aircraft designated Fajr-22 which appears to be identical to the CH 701[3].
Design
Designed for off-runway operations, the CH 701 has many unique features, such as a high-lift wing with full-span, non-movable leading edge slats (also known as slots), an all flying rudder, large tires, flaperons and an inverted elevator, that contribute to the aircraft's STOL capabilities. Heintz also designed a unique tricycle gear amphibious float system for the CH 701.
The STOL CH 701 has the unique distinction of being what is probably the most copied light aircraft in production today. Several dozen unauthorized versions have been produced around the world[4]
The CH 701 was developed into a four place version designated the Zenith STOL CH 801.[1]
CH 750
Zenith introduced a variant of the CH 701 called the STOL CH 750 at AirVenture 2008. The 750 has an enlarged cabin and is optimized for the US Light Sport Aircraft rules with a gross weight of 1320 lbs (600 kg), compared to the 701's 1100 lbs (500 kg).[2]
Production
By the fall of 2007 750 CH 701s had been completed and were flying.[1]
Regulatory status
Designed to the Light Aircraft Manufacturers Association of Canada (LAMAC) design standard DS 10141, in its native country of Canada the CH 701 can be built and flown as a basic ultra-light[5], advanced ultra-light[6] or amateur-built.[7]
The CH 701 can be flown under microlight/ultralight rules in several other countries also. American pilots may fly the CH 701 under FAA Light-sport Aircraft rules or as an experimental amateur-built.[1]
The CH 750 is designed to comply with the US Light sport aircraft rules.[2]
Specifications (CH-701)
Data from Jane's All The World's Aircraft 1993-94[8]
General characteristics
- Crew: 2
- Length: 20 ft 0 in (6.10 m)
- Wingspan: 27 ft 0 in (8.23 m)
- Wing area: 122.0 sq ft (11.33 m2)
- Aspect ratio: 5.98:1
- Empty weight: 460 lb (209 kg)
- Max takeoff weight: 960 lb (435 kg)
- Fuel capacity: 16 US Gal (60 L)
- Powerplant: 1 × Rotax 582 two-cylinder liquid cooled piston engine, 65 hp (48 kW)
Performance
- Maximum speed: 85 mph (137 km/h, 74 kn) at sea level
- Cruise speed: 75 mph (121 km/h, 65 kn)
- Stall speed: 28 mph (45 km/h, 24 kn)
- Range: 287 mi (462 km, 249 nmi) standard fuel
- Ferry range: 518 mi (834 km, 450 nmi) with wing tanks
- Endurance: 1 hr 40 min
- Service ceiling: 16,000 ft (4,900 m)
- g limits: +6/-3
- Rate of climb: 1,200 ft/min (6.1 m/s)
References
- ^ a b c d e Kitplanes Staff: 2008 Kit Aircraft Directory, page 80, Kitplanes Magazine December 2007 Volume 24, Number 12, Belvior Publications, Aviation Publishing Group LLC.
- ^ a b c Zenith Aircraft Company (2008). "STOL CH 750". Retrieved 2008-08-09.
{{cite web}}: Unknown parameter|month=ignored (help) - ^ http://www.janes.com/extracts/extract/jawa/jawa5333.html
- ^ Zenith Aircraft Company (undated). "STOL CH701". Retrieved 2007-12-06.
{{cite web}}: Check date values in:|year=(help) - ^ Transport Canada (2007). "Ultra-light Transition Stategy". Retrieved 2007-12-06.
{{cite web}}: Unknown parameter|month=ignored (help) - ^ Transport Canada (2007). "Listing of Models Eligible to be Registered as Advanced Ultra-Light Aeroplanes (AULA)". Retrieved 2007-12-06.
{{cite web}}: Unknown parameter|month=ignored (help) - ^ Transport Canada (2006). "EXEMPTION FROM SECTION 549.01 OF THE CANADIAN AVIATION REGULATIONS AND CHAPTER 549 OF THE AIRWORTHINESS MANUAL – AIRWORTHINESS STANDARDS - AMATEUR-BUILT AIRCRAFT". Retrieved 2007-12-06.
{{cite web}}: Unknown parameter|month=ignored (help) - ^ Lambert 1993, p.41.
- Lambert, Mark (editor) (1993). Jane's All The World's Aircraft 1993-94. Coulsdon, UK: Jane's Data Division. ISBN 0 7106 1066 1.
{{cite book}}:|first=has generic name (help)