Zenair STOL CH 701, Руководство по эксплуатации самолета

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1. General
Introduction
The pilot’s handbook has been prepared
to provide pilots and instructors with
information for the safe and efficient operation of this UL-aeroplane.
Certification basis
This type of aircraft has been approved by PFA according to British Civil Airworthiness
Requirements CAP 482 Section S Small Light Aeroplanes, Issue 1 including BCAR Paper
S901 proposed amendments.
Descriptive data
CH 701 is a side-by-side two place, strut-braced high wing monoplane with all-metal
structure. CH 701 is a reliable two seat aircraft designed with pilot and passenger comfort in
mind for short-field capability, excellent performance and good visibility. The STOL CH
701 is truly the aircraft which combines the advantages of a conventional aircraft with those
of an advanced Ultralight.
Standard powerplant is Rotax 912, 4-cylinder, 4-stroke, w/
opposed cylinders
Wing span ................................................................ 8,220 mm
Length ...................................................................... 6,100 mm
Height.. ..................................................................... 2,350 mm
MAC ........................................................................ 1.43 m
Wing area ................................................................. 11.33 m.sq.
Wing loading ............................................................ 39.7 kg/m.sq.
Engine ...................................................................... Rotax 912 80 HP
Propeller.. ................................................................. two or three blade composite or wood
Diameter ................................................................... 1700 mm.