PS-28 Cruiser
PS-28N Cruiser
CR-MM-1-0-00
CHAPTER 1 – GENERAL
Revision No.: 24
Date of issue: 2020-11-19
1 - 4
1.1
Introduction
In accordance with requirements of the ASTM LSA regulations, the Czech Aircraft Group s.r.o.,
as manufacturer of PS-28 Cruiser airplane, provides information on maintaining airworthiness
of the PS-28 Cruiser airplane. Information is also contained in the following manuals issued by
airplane manufacturer or by manufacturers of equipment used on the airplane:
•
Pilot Operating Handbook
•
Maintenance Manual
•
Illustrated Parts Catalog
•
Operator's Manual for ROTAX Engine Type 912 Series
•
Maintenance Manual for ROTAX Engine Type 912 Series
•
Technical description and operation instructions for the propeller
This Maintenance Manual contains information on airplane maintenance including description
of airplane structure and function.
1.2
Airplane Classification
PS-28 Cruiser airplane is two-seat, single engine, low-wing, all-metal airplane with fixed three-
wheel landing gear.
The airplane is designed for basic and advanced training and for leisure time flying.
1.2.1 Power Unit
Power unit consists of:
•
Four-stroke, four-cylinder engine with opposite pistons Rotax 912 S2 / 912 ULS2 with max.
continuous power of 69 kW (92.5 hp) at 5,500 RPM.
•
Three-blade, ground adjustable propeller or
•
Two-blade, ground adjustable propeller or
•
Two-blade, in flight adjustable propeller.