
Art Mitchell
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Art Mitchell has been involved
in professional aviation for more than 20 years with over 4,000 hours flying and 14 years
in maintenance and repair. He has taught at Trinity Western University in Langley, B.C.
and helped develop a course in mountain flying. Since 1980 he has been with Mission
Aviation Fellowship, flying mostly in East and Central Africa. Flypass Ltd. is Zenith Aircraft's
central Canada distributor. The company built the prototype STOL CH 801 under the
design and construction supervision of designer Chris Heintz. |
Designer Chris Heintz has
announced his newest design - a high wing all metal four seat kit aircraft. The new
design, called the STOL CH 801, is a utility kit aircraft based on the successful two seat
STOL CH 701 design developed by Heintz in the mid eighties. Since its introduction
in 1986, more than 400 short take-off and landing STOL CH 701 aircraft have been
successfully flown around the world, many being used for light utility purposes.
The larger STOL CH 801 has been developed to expand the utility of the 701 model by
increasing the useful load from 500 lbs. (225 kg) to over 1000 lbs. (450 kg.) while
retaining the original design's short and rough field capability. While the two
designs share many similarities in appearance, they actually do not share any airframe
parts due to the significantly larger size of the STOL CH 801.
Development of the STOL CH 801 actually began in 1988 when Chris Heintz started design
of the four seat aircraft for an offshore customer, but a prototype was never completed
when the customer postponed the order due to the lack of a suitable powerplant for the
design at the time (conventional aircraft engines were deemed unsuitable by the customer
due to cost and spare parts availability). The prototype was powered with a 180-hp
Subaru automotive conversion .
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"For the last
four years, we at Flypass have been involved in the development of the
Zenair CH 801 Super STOL. Our purpose has been to help produce
an aircraft that would be useful for workers in underdeveloped regions
of the world, particularly missionaries and nationals. In this
type of environment simplicity, durability, economy and reliability
are not luxuries but essentials." Art
Mitchell - Flypass Ltd.
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"The
CH 801 has proven itself to be all we had hoped for. It has
flown well with several engines to date. I have flown three of
them so far and normally I would be reluctant to say that one is a
great deal better than the other but… I really love this Walter-LOM
M337B. It is a 235 hp, inline, inverted, injected, supercharged,
100% aircraft engine." Art
Mitchell - Flypass Ltd. |
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The
Engine
The original design is by Walter Aircraft Engines. For
the last several years these engines have been manufactured,
overhauled and serviced by LOM Praha. The heritage behind this
machine is as long as that of Lycoming and Continental.
Unfortunately it has been hidden behind the "Iron Curtain"
for these many years. If you were to walk through the Aviation Museum at
Litneny airport in Prague, you would see saw aircraft from the 1920s and 30s with
Walter engines. You would also see Lycomings from the same era.
The difference is that the Walters have changed since then. |
With
Zenair's production facilities devoted to the production of the type-certificated design,
including the ZENITH CH 2000, the
prototype STOL CH 801 is being built by Flypass Ltd. in Guelph, Ontario. Headed by
Art Mitchell, a veteran missionary pilot, Flypass began construction of the prototype STOL
CH 801 in the fall of 1997 under the design supervision of Chris Heintz. Flypass
Ltd. is the central Canada representative for Zenair kit aircraft designs. It
operates a flight school using Zenair aircraft, and houses a builder assistance center at
its facilities at Waterloo Regional Airport in Kitchener, Ontario.
With form following function, the STOL CH 801 looks like the
workhorse it is designed to be. Not designed to be just another "pretty"
aircraft, the STOL CH 801 was developed to provide maximum short field performance while
being easy to build and maintain.
| Design Features of the STOL CH
801: |
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- All metal semi-monocoque construction, utilizing proven "Zenair easy build
technology," including extensive use of Textron Avdel blind rivets;
- Fixed leading edge wing slats;
- Full length flaperons (combined ailerons and flaps);
- "Above Cab" wing design for superior visibility;
- All flying rudder for increased responsiveness at slow flight and superior cross-wind
capability;
- Rugged landing gear for rough field capability;
- Tricycle gear configuration for improved ground handling and visibility;
- Short wing span to allow operation in areas with obstacles;
- "Open Design" to allow for a wide choice of engine installations;
Overall design and construction simplicity for field maintainability,
including easy remove cowls for quick access to the engine.
PERFORMANCE AND SPECIFICATIONS
Preliminary Figures
| SPECIFICATIONS |
STOL CH
801 |
| LENGTH |
23 Ft. 2 In. |
7.06 m. |
| HEIGHT |
8 Ft. 9 In. |
2.7 m. |
| WING SPAN |
30 Ft. 10 In. |
9.4 m. |
| WING AREA |
152 SQ.FT. |
15 m.sq. |
| WING CHORD |
5 Ft. 3 In. |
1.6 m. |
| HORIZONTAL TAIL SPAN |
8 Ft. 4 In. |
2.57 m. |
| HORIZONTAL TAIL AREA |
25 SQ.FT. |
2.7 m.sq.. |
| EMPTY WEIGHT |
1,015 LBS. |
460 kg. |
| DESIGN GROSS WEIGHT |
2,020 LBS. |
920 kg. |
FUEL CAPACITY (Std)
- Fuel weight (Std) |
40 US Gal.
= 240 LBS. |
150 l.
= 110 kg. |
DESIGN PAYLOAD
- Occupants + Baggage / Cargo |
760 LBS.
= 190 lbs X 4 |
340 kg.
= 85 kg. X 4 |
| WING LOADING |
13.3 LBS/FT< |
61.3 kg/m< |
| POWER LOADING |
11.2 LBS/BHP |
5.1 kg/BHP |
| DESIGN LOAD FACTOR |
+6 G / -3G |
| CABIN WIDTH (shoulders) |
44 INCHES |
112 cm. |
| NEVER EXCEED SPEED (Vne) |
150 MPH |
240 km/h |
| Performance |
STOL CH 801 |
| TAKE OFF ROLL |
200 FT |
60 M |
| TAKE OFF OVER 50' OBSTACLE |
400 FT |
120 M |
| LANDING ROLL |
150 FT |
47 M |
LANDING FROM OVER 50'
OBSTACLE |
300 FT |
92 M |
| STALL SPEED (flaps down) |
39
MPH |
62
KPH |
| STALL SPEED (flaps up) |
49
MPH |
78
KPH |
| RATE OF CLIMB (maximum) |
1,050
FPM |
5.3
M/S |
| CRUISE SPEED (75%) |
110
MPH |
175
KPH |
| MAX LEVEL SPEED |
125
MPH |
200
KPH |
Visit the Zenith Aircraft website:
http://www.zenithair.com

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