This document contains information necessary for operation and maintenance of the airplane according to LSA regulation. OFFICE: ROHÁČOVA 188/37, 130 00, PRAHA 3, CZECH REPUBLIC PRODUCTION FACILITY: NA ZÁHONECH Č.E. 212, KUNOVICE, 686 04, CZECH REPUBLIC www.czechsportaircraft.com INTENTIONALLY LEFT BLANK MIP RECORD OF REVISIONS Rev. Date and Reason for revision Changed pages Issue date No. signature 1 initial all 01/2007 2 Design changes See list of effective pages 01/2008 Ailerons and trims deflections, coolant See list of effective pages 3 operation limits 04/2008 4 Operating liquids See list of effective pages 02/2009 5 Reissue All 04/2009 Date of issue: 04/2009 Revision No. 5 0- 1 MIP LIST OF EFFECTIVE PAGES Chapter Page Date Chapter Page Date 0 0-1 04/2009 4-6 04/2009 0-2 04/2009 4-7 04/2009 0-3 04/2009 4-8 04/2009 0-4 04/2009 5 5-1 04/2009 5-2 04/2009 1 1-1 04/2009 5-3 04/2009 1-2 04/2009 5-4 04/2009 1-3 04/2009 5-5 04/2009 1-4 04/2009 5-6 04/2009 1-5 04/2009 5-7 04/2009 1-6 04/2009 1-7 04/2009 6 6-1 04/2009 6-2 04/2009 2 2-1 04/2009 6-3 04/2009 2-2 04/2009 6-4 04/2009 2-3 04/2009 6-5 04/2009 2-4 04/2009 6-6 04/2009 2-5 04/2009 6-7 04/2009 2-6 04/2009 6-8 04/2009 2-7 04/2009 6-9 04/2009 2-8 04/2009 6-10 04/2009 2-9 04/2009 6-11 04/2009 2-10 04/2009 6-12 04/2009 2-11 04/2009 6-13 04/2009 6-14 04/2009 6-15 04/2009 3 3-1 04/2009 6-16 04/2009 3-2 04/2009 6-17 04/2009 3-3 04/2009 6-18 04/2009 3-4 04/2009 6-19 04/2009 3-5 04/2009 6-20 04/2009 3-6 04/2009 6-21 04/2009 3-7 04/2009 6-22 04/2009 3-8 04/2009 6-23 04/2009 3-9 04/2009 7 7-1 04/2009 4 4-1 04/2009 7-2 04/2009 4-2 04/2009 7-3 04/2009 4-3 04/2009 7-4 04/2009 4-4 04/2009 4-5 04/2009 Date of issue: 04/2009 Revision No. 5 0- 2 MIP Chapter Page Date Chapter Page Date 8 8-1 04/2009 10-18 04/2009 8-2 04/2009 10-19 04/2009 8-3 04/2009 10-20 04/2009 8-4 04/2009 10-21 04/2009 8-5 04/2009 10-22 04/2009 8-6 04/2009 10-23 04/2009 8-7 04/2009 10-24 04/2009 8-8 04/2009 10-25 04/2009 8-9 04/2009 10-26 04/2009 8-10 04/2009 10-27 04/2009 8-11 04/2009 10-28 04/2009 8-12 04/2009 10-29 04/2009 8-13 04/2009 8-14 04/2009 8-15 04/2009 11 11-1 04/2009 11-2 04/2009 11-3 04/2009 9 9-1 04/2009 11-4 04/2009 9-2 04/2009 11-5 04/2009 9-3 04/2009 11-6 04/2009 9-4 04/2009 11-7 04/2009 9-5 04/2009 11-8 04/2009 9-6 04/2009 11-9 04/2009 9-7 04/2009 9-8 04/2009 9-9 04/2009 12 12-1 04/2009 12-2 04/2009 12-3 04/2009 10 10-1 04/2009 12-4 04/2009 10-2 04/2009 12-5 04/2009 10-3 04/2009 12-6 04/2009 10-4 04/2009 12-7 04/2009 10-5 04/2009 10-6 04/2009 10-7 04/2009 13 13-1 04/2009 10-8 04/2009 13-2 04/2009 10-9 04/2009 13-3 04/2009 10-10 04/2009 13-4 04/2009 10-11 04/2009 10-12 04/2009 10-13 04/2009 14 14-1 04/2009 10-14 04/2009 14-2 04/2009 10-15 04/2009 14-3 04/2009 10-16 04/2009 10-17 04/2009 Date of issue: 04/2009 Revision No. 5 0- 3 MIP Chapter Page Date Chapter Page Date 15 15-1 04/2009 15-2 04/2009 15-3 04/2009 15-4 04/2009 15-5 04/2009 15-6 04/2009 15-7 04/2009 15-8 04/2009 15-9 04/2009 15-10 04/2009 15-11 04/2009 15-12 04/2009 15-13 04/2009 15-14 04/2009 15-15 04/2009 15-16 04/2009 15-17 04/2009 15-18 04/2009 15-19 04/2009 15-20 04/2009 15-21 04/2009 15-22 04/2009 16 16-1 04/2009 16-2 04/2009 16-3 04/2009 16-4 04/2009 16-5 04/2009 16-6 04/2009 16-7 04/2009 16-8 04/2009 16-9 04/2009 17 17-1 04/2009 17-2 04/2009 17-3 04/2009 17-4 04/2009 17-5 04/2009 Date of issue: 04/2009 Revision No. 5 0- 4 MIP TABLE OF CONTENTS Chapter 1 - General ..................................................................................... 1-1 Chapter 2 - Limitations/Maintenance checks ............................................ 2-1 Chapter 3 - Fuselage ................................................................................... 3-1 Chapter 4 - Wing..........................................................................................4-1 Chapter 5 - Tail unit.....................................................................................5-1 Chapter 6 - Controls.................................................................................... 6-1 Chapter 7 - Equipment ................................................................................ 7-1 Chapter 8 - Landing gear ............................................................................ 8-1 Chapter 9 - Fuel system .............................................................................. 9-1 Chapter 10 - Power unit .............................................................................. 10-1 Chapter 11 - Electrical system.................................................................... 11-1 Chapter 12 - Pitot-static system/Instruments............................................ 12-1 Chapter 13 - Venting/Heating...................................................................... 13-1 Chapter 14 - Airplane handling................................................................... 14-1 Chapter 15 - Airplane repairs...................................................................... 15-1 Chapter 16 - Wiring diagrams..................................................................... 16-1 Chapter 17 - Appendices............................................................................. 17-1 Date of issue: 01/2007 Revision No. 1 0- 5 MIP INTENTIONALLY LEFT BLANK MIP CHAPTER 1 - GENERAL 1.1 Introduction ............................................................................................................ 1-2 1.2 Airplane classification ............................................................................................ 1-2 1.2.1 Power unit................................................................................................. 1-2 1.2.2 Main technical data................................................................................... 1-3 1.3 Airplane manufacturer and type certificate holder ................................................. 1-5 1.4 Chapter order......................................................................................................... 1-5 1.4.1 Page numbering ....................................................................................... 1-5 1.5 Warnings, cautions and notes ............................................................................... 1-5 1.6 Definitions and abbreviations................................................................................. 1-6 GENERAL Date of issue: 04/2009 Revision No. 5 1 - 1 MIP Introduction Czech Sport Aircraft a.s. as manufacturer of SPORTCRUISER airplane provides in accordance with requirements of the ASTM LSA regulations information on maintaining airworthiness of the SPORTCRUISER airplane. Information is also contained in the following manuals issued by airplane manufacturer or by manufacturers of equipment used on the airplane: • Sportcruiser Pilot Operating Handbook • Sportcruiser Maintenance and Inspection Procedures • Sportcruiser Illustrated Parts Catalog • Operator's Manual for ROTAX 912 ULS engine • Maintenance Manual for ROTAX 912 ULS engine • Technical description and operation instructions for the propeller This document (Maintenance and Inspection Procedures) contains information on airplane maintenance including description of airplane structure and function. Airplane classification SPORTCRUISER 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. Power unit Power unit consists of: • four-stroke, four-cylinder engine with opposite pistons Rotax 912 ULS with max. continuous power of 69 kW (92.5 hp) at 5500 RPM • Three-blade, ground adjustable propeller. GENERAL Date of issue: 04/2009 Revision No. 5 1 - 2 MIP Main technical data Wing • span ..........................................................................8.81m (28.90 ft) • area ...........................................................................12.3m 2 (132.3 sqft) • MAC ..........................................................................1500mm (59.1 in) • wing loading ..............................................................49kg/m 2 (10.0 lb/sqft) • aileron area ..............................................................0.46m 2 (4.98 sqft) • flap area ...................................................................0.65m 2 (7.0 sqft) Fuselage • length ........................................................................6.5m (21.33 ft) • width..........................................................................1.28m (50.4 in) • height ........................................................................2.37m (7.78 ft) • cockpit width..............................................................1.17m (46 in) Horizontal tail unit • span ..........................................................................2.93m (9.61 ft) • HTU area...................................................................2.2m 2 (23.7 sqft) • elevator area .............................................................0.8m 2 (8.6 sqft) Vertical tail unit • height ........................................................................1.07m (3.51 ft) • VTU area...................................................................1m 2 (10.7 sqft) • rudder area................................................................0.4m 2 (4.3 sqft) Landing gear • wheel track ................................................................1.52m (4.98 ft) • wheel base ................................................................2.07m (6.79 ft) • nose landing gear wheel diameter............................343mm