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Airplane Maintenance Manual
Section 4 – Airworthiness Limitations in Issue 01 of this manual was approved by
European Aviation Safety Agency on 24.5. 2012.
Issue 02 of this manual is approved by the manufacturer under the DOA privilege
EASA.21J.057 on 26.1. 2018.
Copyright © 2017
EVEKTOR, spol. s r.o.
This document contains proprietary information that is protected by copyright. All rights are reserved. No part of this document may
by copied, reproduced or translated to other languages without the prior written consent of Evektor spol. s r.o.
Airplane Type:
Model:
Airplane Serial No.:
Airplane Registration No.:
Document No.:
Date of Issue:
for
SportStar
RTC
ERTC022-10-AS
22.12.2017 / Edition 02
Airplane manufacturer:
EVEKTOR-AEROTECHNIK, a.s.
686 04 Kunovice – Letecká 1394
Czech Republic
www.evektoraircraft.com

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  • Page 1 Airplane Maintenance Manual Airplane Type: SportStar Model: Airplane Serial No.: Airplane Registration No.: Document No.: ERTC022-10-AS Date of Issue: 22.12.2017 / Edition 02 Section 4 – Airworthiness Limitations in Issue 01 of this manual was approved by European Aviation Safety Agency on 24.5. 2012. Issue 02 of this manual is approved by the manufacturer under the DOA privilege EASA.21J.057 on 26.1.
  • Page 3 GENERAL COVERAGE ln compliance with requirements of CS-LSA, Subpart G2, the manufacturer of SportStar RTC provides instructions for continued airworthiness of this airplane. The instructions are given in the following manuals issued by the airplane manufacturer and manufacturers of the equipment used in the airplane: •...
  • Page 4 ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 01-00 Effectivity: All Page 01-4 Edition 2 | Rev. 0 2017-12-22...
  • Page 5 MAINTENANCE MANUAL AIRPLANE CLASSIFICATION AIRPLANE DESCRIPTION SportStar RTC airplane is single-engine, two-seat low-wing monoplane with fixed landing gear and steerable nose wheel. The airframe is a combination of classic all-metal primary construction with some composite parts. The power plant standardly consists of four-cylinder, four-stroke Rotax 912 ULS2 or S2 engine and on-ground adjustable, three-bladed, composite propeller Woodcomp Klassic 170/3/R;...
  • Page 6 ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 01-10 Effectivity: All Page 01-6 Edition 2 | Rev. 0 2017-12-22...
  • Page 7 ERTC022-10-AS MAINTENANCE MANUAL MANUFACTURERS AIRPLANE MANUFACTURER EVEKTOR-AEROTECHNIK, a.s. Okružní 234 293 06 Bradlec Czech Republic Tel.: +420 572 537 323 Fax: +420 572 537 910 e-mail: service@evektor.cz http://www.evektorairplane.cz ENGINE MANUFACTURER BRP-Powertrain GmbH&Co. KG. Welser Strasse 32 A-4623 Gunskirchen Austria http://www.flyrotax.com PROPELLER MANUFACTURER Woodcomp s.r.o.
  • Page 8 ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 01-20 Effectivity: All Page 01-8 Edition 2 | Rev. 0 2017-12-22...
  • Page 9 Refer to the Supplement No. 1 Equipment List (Doc. No. ERTC 020-10-AS-001) of the Pilot´s Operating Handbook for SportStar RTC for actual equipment. SOURCE TO PURCHASE PARTS Spare parts can be ordered from airplane manufacturer by means of the SportStar RTC Illustrated Parts Catalogue (Doc. No. SPORTSTAR-0396G-02172-00). LIST OF DISPOSABLE REPLACEMENT PARTS...
  • Page 10 ERTC022-10-AS MAINTENANCE MANUAL GENERAL SAFETY INFORMATION Safety must be considered the first priority when performing maintenance or service on an aircraft or part. To minimize the risk to both yourself and others, begin by thinking through each task that is to be performed before starting any work.
  • Page 11 ERTC022-10-AS MAINTENANCE MANUAL ABBREVIATIONS Stall warning system Airworthiness Directive ADAHRS Air Data and Attitude Heading Reference System Automatic Direction Finder AHRS Attitude Heading Reference System Accumulator ATIS Automatic Terminal Information Service AUX, Aux Auxiliary BAT, Bat Battery Carbon, Carbon fibre Course Deviation Indicator Cylinder Heat Temperature COM, Com...
  • Page 12 ERTC022-10-AS MAINTENANCE MANUAL NACA National Advisory Committee for Aeronautics (meant NACA inlet) NAV, Nav Navigation Outside Air Temperature Overhead Valve Right Polycarbonate Polyethylene (foil) Primary Flight Display Pilot Operating Handbook Part Number PMMA Polymethylmethacrylate Polypropylen Pitot static Push to Talk Society of Automotive Engineers Serial Number Squelch...
  • Page 13 ERTC022-10-AS MAINTENANCE MANUAL LIST OF EFFECTIVE PAGES Chapter Page Date Chapter Page Date Title 2019-03-22 01-33 2019-03-22 01-34 2017-12-22 01-1 2017-12-22 01-35 2017-12-22 01-2 2017-12-22 01-36 2017-12-22 01-3 2019-03-22 01-37 2017-12-22 01-4 2017-12-22 01-38 2017-12-22 01-5 2019-03-22 01-39 2019-03-22 01-6 2017-12-22 01-40 2019-03-22...
  • Page 14 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 05-1 2019-03-22 05-37 2019-03-22 05-2 2017-12-22 05-38 2017-12-22 05-3 2017-12-22 05-39 2019-03-22 05-4 2017-12-22 05-40 2017-12-22 05-5 2017-12-22 05-41 2017-12-22 05-6 2019-03-22 05-42 2019-03-22 05-7 2019-03-22 05-43 2017-12-22 05-8 2017-12-22 05-44 2017-12-22 05-9 2019-03-22...
  • Page 15 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 07-5 2017-12-22 10-1 2017-12-22 07-6 2017-12-22 10-2 2017-12-22 10-3 2017-12-22 10-4 2017-12-22 10-5 2017-12-22 10-6 2017-12-22 10-7 2017-12-22 08-1 2017-12-22 10-8 2017-12-22 08-2 2017-12-22 10-9 2017-12-22 08-3 2017-12-22 10-10 2017-12-22 08-4 2017-12-22 10-11 2017-12-22...
  • Page 16 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 20-4 2017-12-22 20-5 2017-12-22 12-1 2017-12-22 20-6 2017-12-22 12-2 2017-12-22 20-7 2017-12-22 12-3 2017-12-22 20-8 2017-12-22 12-4 2017-12-22 20-9 2017-12-22 12-5 2017-12-22 20-10 2017-12-22 12-6 2017-12-22 20-11 2017-12-22 12-7 2017-12-22 20-12 2017-12-22 12-8 2017-12-22...
  • Page 17 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 23-1 2017-12-22 23-37 2017-12-22 23-2 2017-12-22 23-38 2017-12-22 23-3 2017-12-22 23-4 2017-12-22 23-5 2017-12-22 23-6 2017-12-22 23-7 2017-12-22 23-8 2017-12-22 24-1 2019-03-22 23-9 2017-12-22 24-2 2019-03-22 23-10 2017-12-22 24-3 2019-03-22 23-11 2017-12-22 24-4 2019-03-22...
  • Page 18 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 24-30 2019-03-22 25-17 2017-12-22 24-31 2019-03-22 25-18 2017-12-22 24-32 2019-03-22 25-19 2017-12-22 24-33 2019-03-22 25-20 2017-12-22 24-34 2019-03-22 25-21 2017-12-22 24-35 2019-03-22 25-22 2019-03-22 24-36 2019-03-22 25-23 2017-12-22 24-37 2019-03-22 25-24 2017-12-22 24-38 2019-03-22...
  • Page 19 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 27-7 2017-12-22 27-43 2017-12-22 27-8 2017-12-22 27-44 2017-12-22 27-9 2017-12-22 27-45 2017-12-22 27-10 2017-12-22 27-46 2017-12-22 27-11 2017-12-22 27-47 2017-12-22 27-12 2017-12-22 27-48 2017-12-22 27-13 2017-12-22 27-49 2017-12-22 27-14 2017-12-22 27-50 2017-12-22 27-15 2017-12-22...
  • Page 20 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 28-16 2017-12-22 31-1 2017-12-22 28-17 2017-12-22 31-2 2017-12-22 28-18 2017-12-22 31-3 2017-12-22 28-19 2017-12-22 31-4 2017-12-22 28-20 2017-12-22 31-5 2017-12-22 28-21 2017-12-22 31-6 2017-12-22 28-22 2017-12-22 31-7 2017-12-22 28-23 2017-12-22 31-8 2017-12-22 28-24 2017-12-22...
  • Page 21 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 32-6 2017-12-22 32-42 2017-12-22 32-7 2017-12-22 32-43 2019-03-22 32-8 2017-12-22 32-44 2017-12-22 32-9 2017-12-22 32-45 2017-12-22 32-10 2017-12-22 32-46 2019-03-22 32-11 2017-12-22 32-47 2017-12-22 32-12 2017-12-22 32-48 2017-12-22 32-13 2017-12-22 32-49 2017-12-22 32-14 2017-12-22...
  • Page 22 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 33-13 2017-12-22 34-20 2017-12-22 33-14 2017-12-22 34-21 2017-12-22 33-15 2017-12-22 34-22 2017-12-22 33-16 2017-12-22 34-23 2017-12-22 33-17 2017-12-22 34-24 2017-12-22 33-18 2017-12-22 34-25 2017-12-22 33-19 2017-12-22 34-26 2017-12-22 33-20 2017-12-22 34-27 2017-12-22 33-21 2017-12-22...
  • Page 23 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 55-16 2017-12-22 57-12 2017-12-22 55-17 2017-12-22 57-13 2017-12-22 55-18 2017-12-22 57-14 2017-12-22 57-15 2017-12-22 57-16 2017-12-22 57-17 2017-12-22 57-18 2017-12-22 57-19 2017-12-22 56-1 2017-12-22 57-20 2017-12-22 56-2 2017-12-22 56-3 2017-12-22 56-4 2017-12-22 56-5 2017-12-22...
  • Page 24 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 71-1 2019-03-22 74-1 2017-12-22 71-2 2017-12-22 74-2 2017-12-22 71-3 2017-12-22 74-3 2017-12-22 71-4 2017-12-22 74-4 2017-12-22 71-5 2017-12-22 74-5 2017-12-22 71-6 2017-12-22 74-6 2017-12-22 71-7 2017-12-22 74-7 2017-12-22 71-8 2017-12-22 74-8 2017-12-22 71-9 2017-12-22...
  • Page 25 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 76-9 2017-12-22 77-26 2017-12-22 76-10 2017-12-22 77-27 2017-12-22 76-11 2017-12-22 77-28 2017-12-22 76-12 2017-12-22 77-29 2017-12-22 76-13 2017-12-22 77-30 2017-12-22 76-14 2017-12-22 78-1 2017-12-22 78-2 2017-12-22 78-3 2017-12-22 77-1 2017-12-22 78-4 2017-12-22 77-2 2017-12-22...
  • Page 26 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 79-14 2017-12-22 91-19 2017-12-22 79-15 2017-12-22 91-20 2017-12-22 79-16 2017-12-22 91-21 2017-12-22 79-17 2017-12-22 91-22 2017-12-22 79-18 2017-12-22 91-23 2017-12-22 79-19 2017-12-22 91-24 2017-12-22 79-20 2017-12-22 91-25 2017-12-22 79-21 2017-12-22 91-26 2017-12-22 79-22 2017-12-22...
  • Page 27 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 91-55 2017-12-22 91-91 2019-03-22 91-56 2017-12-22 91-92 2017-12-22 91-57 2017-12-22 91-93 2019-03-22 91-58 2017-12-22 91-94 2017-12-22 91-59 2017-12-22 91-95 2017-12-22 91-60 2017-12-22 91-96 2017-12-22 91-61 2017-12-22 91-97 2017-12-22 91-62 2017-12-22 91-98 2017-12-22 91-63 2017-12-22...
  • Page 28 ERTC022-10-AS MAINTENANCE MANUAL Chapter Page Date Chapter Page Date 01-50 Effectivity: All Page 01-34 Edition 2 | Rev. 0 2017-12-22...
  • Page 29 ERTC022-10-AS MAINTENANCE MANUAL LOG OF REVISIONS Rev. Date of Inserted by / Affected Pages Description / Effectivity Approval Date Title page, 01-3, 01-5, 01-7, Added information concer- 01-11, 01-14, 01-17, 01-18, ning NVFR operation, added 01-19, 01-20, 01-21, 01-22, VFR definition, corrected 01-24, 01-25, 01-26, 01-29, airplane manufacturer 01-30, 01-31, 01-32, 01-33,...
  • Page 30 ERTC022-10-AS MAINTENANCE MANUAL Rev. Date of Inserted by / Affected Pages Description / Effectivity Approval Date 26-4, 26-5, 26-6 Changed fire extinguisher location 27-6 Changed Dwg. No. of elevator control pull rod 31-17 Changed color of signaling lamp, added information con- cernings P/S tube heating signalization with G3X system...
  • Page 31 ERTC022-10-AS MAINTENANCE MANUAL AIRWORTHINESS LIMITATIONS GENERAL The Chapter “Airworthiness Limitations” is approved by the European Aviation Safety Agency (EASA) in accordance with the applicable certification procedures and the type certification basis. This Chapter includes specification of the airworthiness restrictions required by the Certification Specification CS-LSA.
  • Page 32 ERTC022-10-AS MAINTENANCE MANUAL DESCRIPTION Maintenance limitations The scheduled maintenance requirements are included in Section 05-20 „Scheduled Maintenance“. Replacement limitations Unless otherwise specified, the following components must be replaced with new components, overhauled components, or components, which have life remaining, at the intervals specified: Item Service life Replacement...
  • Page 33 ERTC022-10-AS MAINTENANCE MANUAL Item Service life Replacement Overhaul Note Repack of parachute EPS Magnum 18 years and rocket check 601S-LSA every 6 years. Battery in the Additional information unit of ELT AK- 5 years about the service life is provided in Installation and Operation Manual for Model AK-451 -() Series 406 MHz ELT...
  • Page 34 ERTC022-10-AS MAINTENANCE MANUAL Structure restrictions The service life of the airframe is 7,000 flight hours. The initial service life of the airframe 2,100 flight hours applies to airplane S/N 20121601, if the bulletin No. RTC-002b was not implemented. 04-00 Effectivity: All Page 04-6 Edition 2 | Rev.
  • Page 35: Table Of Contents

    ERTC022-10-AS MAINTENANCE MANUAL CHAPTER 05 TIME LIMITS / MAINTENANCE CHECKS TABLE OF CONTENTS Title Section Page General ........................05-00 ...... 05-3 Introduction ..........................05-3 Definitions ........................... 05-3 Time limits / Inspection program ................05-10 ...... 05-5 Inspection requirements ......................05-5 Inspection program ........................
  • Page 36 ERTC022-10-AS MAINTENANCE MANUAL Exceeding of engine / propeller limitations................05-47 A. Exceeding of engine limitations ..................05-47 B. Exceeding of propeller limitations ..................05-47 Airplane immersing ........................05-47 Fuel contamination ........................05-47 ire burst ............................ 05-47 05-TOC Effectivity: All Page 05-2 Issue 2 | Rev.
  • Page 37: Inspection Requirements

    ERTC022-10-AS MAINTENANCE MANUAL TIME LIMITS / INSPECTION PROGRAM INSPECTION REQUIREMENTS The inspection program is based on number of flight hours (time in service), cycles of operation and / or calendar time. Calendar time for each airplane begins with the original certification date (Airworthiness lssue Date) recorded in the original Log Book for that airplane.
  • Page 38: Service Bulletins

    The owner or operator should be to ensure that all applicable bulletins are complied with. PUBLICATIONS, REFERENCES All inspections listed in this Chapter, should be accomplished with reference to the SportStar RTC Airplane Maintenance Manual, Airworthiness Directives, Service Bulletins, Service Instructions, Service Letters and applicable vendors publications.
  • Page 39: Scheduled Maintenance

    ERTC022-10-AS MAINTENANCE MANUAL SCHEDULED MAINTENANCE RESPONSIBILITY OF OWNER OR OPERATOR The airplane owner or operator is responsible for maintaining the airplane in an airworthy condition, including compliance with all applicable Airworthiness Directives. The owner or operator must ensure that the maintenance is done by qualified personnel. The owner or operator should ensure that the airframe, airplane systems and power plant mechanic inspecting the airplane has access to all necessary manuals and service information.
  • Page 40 ERTC022-10-AS MAINTENANCE MANUAL Fig. 05-1 Description and application of inspection tolerances 05-20 Effectivity: All Page 05-8 Issue 2 | Rev. 0 2017-12-22...
  • Page 41: Inspection Intervals

    ERTC022-10-AS MAINTENANCE MANUAL INSPECTION INTERVALS Each inspection interval can be exceeded by allowed tolerances or can be performed early at anytime prior to the regular interval as provided bellow: • In the even of late compliance of any operational scheduled (within permitted tolerances of inspections), the next operational in sequence retains a due point from the time to the late operational was originally scheduled.
  • Page 42: Inspections Of Parts - General

    ERTC022-10-AS MAINTENANCE MANUAL INSPECTIONS OF PARTS – GENERAL MOVABLE PARTS: lnspect for lubrication, attachments, security of attachments, excessive wear, safetying, proper operation, proper adjustment, correct travel, cracked fittings, security of hinges, defective bearings, cleanliness, corrosion, deformation, sealing and tension. FLUID LINES AND HOSES: Inspect for leaks, cracks, structure, collapsed, twisted, dents, kinks, chafing, proper radius, security, discoloration, deterioration, proper routing;...
  • Page 43 ERTC022-10-AS MAINTENANCE MANUAL SCHEDULED INSPECTION AFTER 100 FH OR ANNUAL INSPECTION Serial Number: ........Total flight hours: ......Registration: ........Total cycles: ......Maintenance type: ........Page: 1 of 12 Ref. Prescribed works Made by Checked by 1. GENERAL – PREPARATORY WORKS Check the airplane operational documentation for condition and check if all prescribed records are made (airplane log book, engine log book, propeller...
  • Page 44 ERTC022-10-AS MAINTENANCE MANUAL SCHEDULED INSPECTION AFTER 100 FH OR ANNUAL INSPECTION Page: 2 of 12 Ref. Prescribed works Made by Checked by 2. POWER PLANT AND ENGINE COPMARTMENT Engine cowlings 71-10 Check cowlings for condition, cracks, deformation and other damage. 71-10 Check quick closing locks and cowlings for condition and attachment.
  • Page 45 ERTC022-10-AS MAINTENANCE MANUAL SCHEDULED INSPECTION AFTER 100 FH OR ANNUAL INSPECTION Page: 3 of 12 Ref. Prescribed works Made by Checked by Fuel system 28-20 Check hoses and tubes for condition, integrity, attachment and security; replace damaged hoses. 28-20 Check fuel system for leaks. Cooling system 75-00 Check water cooler for condition and leaks.
  • Page 46 ERTC022-10-AS MAINTENANCE MANUAL SCHEDULED INSPECTION AFTER 100 FH OR ANNUAL INSPECTION Page: 4 of 12 Ref. Prescribed works Made by Checked by Heating and venting system 21-20 Check hoses for condition, integrity, attachment and 78-20 security. 21-00 Check heating / venting chambers for condition, cracks, deformation and damage.
  • Page 47 ERTC022-10-AS MAINTENANCE MANUAL SCHEDULED INSPECTION AFTER 100 FH OR ANNUAL INSPECTION Page: 5 of 12 Ref. Prescribed works Made by Checked by Wheel (continued) 32-41 Check valve for condition around the hole in the rim. Beware of cutting the valve when the tire slippage. 32-41 Check bearings for condition, free rotation and play.
  • Page 48 ERTC022-10-AS MAINTENANCE MANUAL SCHEDULED INSPECTION AFTER 100 FH OR ANNUAL INSPECTION Page: 6 of 12 Ref. Prescribed works Made by Checked by Wheels 32-41 Check wheels for cracks, permanent deformations; replace if damaged. 32-41 Check valve for condition around the hole in the rim. Beware of cutting the valve when the tire slippage.
  • Page 49 ERTC022-10-AS MAINTENANCE MANUAL SCHEDULED INSPECTION AFTER 100 FH OR ANNUAL INSPECTION Page: 11 of 12 Ref. Prescribed works Made by Checked by Rudder control 27-20 Check control for stiffness of movement. 27-20 Check joints for security. 27-20 Check stops at rudder control cables for condition. 27-20 Check rudder cables for condition and security.
  • Page 50 ERTC022-10-AS MAINTENANCE MANUAL SCHEDULED INSPECTION AFTER 100 FH OR ANNUAL INSPECTION Page: 12 of 12 Ref. Prescribed works Made by Checked by 11. FINISHING WORKS Check the completeness of tools and instruments used during the inspection. 12-20 Lubricate all items according to the lubrication chart. 25-10 Install upholstery and seats.
  • Page 51 ERTC022-10-AS MAINTENANCE MANUAL INSPECTION AFTER FIRST 25 FH Page: 2 of 6 Ref. Prescribed works Made by Checked by Cooling system 75-00 Check water cooler for condition and leaks. 75-00 Check hoses and tubes for condition, attachment, 79-20 leaks and security. Cooler left hose clearance from exhaust pipe approx.
  • Page 52 ERTC022-10-AS MAINTENANCE MANUAL INSPECTION AFTER FIRST 25 FH Page: 3 of 6 Ref. Prescribed works Made by Checked by 3. NOSE LANDING GEAR Nose landing gear leg 32-20 Check nose landing gear leg for condition and attachment. 32-20 Check joints for tightening and security. Tire 12-10 Check pressure;...
  • Page 53 ERTC022-10-AS MAINTENANCE MANUAL INSPECTION AFTER FIRST 25 FH Page: 6 of 6 Ref. Prescribed works Made by Checked by Wing flap control 27-50 Check control lever for free movement. 27-50 Check operation of flap control lever lock (push button). 9. FINISHING WORKS Check the completeness of tools and instruments used during the inspection.
  • Page 54 ERTC022-10-AS MAINTENANCE MANUAL SPECIAL INSPECTIONS Serial Number: ........Total flight hours: ......Registration: ........Total cycles: ......Page: 1 of 1 Ref. Prescribed works Period Made by Checked by 08-20 Weigh the airplane. 72 months or acc. to appropriate national regulations 34-10 Pitot-static system –...
  • Page 55: Hard Landing

    ERTC022-10-AS MAINTENANCE MANUAL HARD LANDING INSPECTION Page: 2 of 3 Ref. Prescribed works Made by Checked by 3. WING 57-10 Check wing structure / skin for condition, especially in 57-30 the area of attachments. 57-10 Check integral tank riveted joints for leakage. 57-40 Check wing attachments for condition.
  • Page 56 ERTC022-10-AS MAINTENANCE MANUAL HARD LANDING INSPECTION Page: 3 of 3 Ref. Prescribed works Made by Checked by 5. COCKPIT Ch. 27 Check all control systems for function and free movement. Ch. 27 Check control stops for condition and security. 76-10 Check engine control for function and free movement.
  • Page 57: Exceeding Of Load Factors / Flight In Severe Turbulence

    ERTC022-10-AS MAINTENANCE MANUAL EXCEEDING OF LOAD FACTORS / FLIGHT IN SEVERE TURBULENCE Exceeding the maximum flight load factors can occur when improperly performed flight maneuvers or from gust at flight through turbulence. Load factor summary Max. maneuvering load factors: = + 4 = - 2 Max.
  • Page 58 ERTC022-10-AS MAINTENANCE MANUAL EXCEEDING OF LOAD FACTORS / FLIGHT IN SEVERE TURBULENCE INSPECTION Page: 2 of 3 Ref. Prescribed works Made by Checked by POWER PLANT AND ENGINE COPMARTMENT (continued) 61-10 Check propeller fastener and propeller-engine fasteners for condition. UM-05 Check propeller blades for condition.
  • Page 59 ERTC022-10-AS MAINTENANCE MANUAL EXCEEDING OF LOAD FACTORS / FLIGHT IN SEVERE TURBULENCE INSPECTION Page: 3 of 3 Ref. Prescribed works Made by Checked by 6. WING 57-10 Check wing structure / skin for condition, especially in 57-30 the area of attachments. 57-10 Check integral tank riveted joints for leakage.
  • Page 60: Ground Gust

    ERTC022-10-AS MAINTENANCE MANUAL GROUND GUST Ground gusts are defined as conditions where a parked or taxiing airplane is exposed to side, aft quartering, or aft wind gusts exceeding 40 knots. Such conditions can cause control system damage due to rapid oscillation and/or slamming of the control surfaces against system stops. After every ground gust inspect the airplane in the following range: GROUND GUST INSPECTION Page: 1 of 2...
  • Page 61 ERTC022-10-AS MAINTENANCE MANUAL GROUND GUST INSPECTION Page: 2 of 2 Ref. Prescribed works Made by Checked by 4. WING 57-10 Check wing structure / skin for condition, especially in 57-30 the area of attachments. 57-40 Check wing attachments for condition. 57-40 Check play of wing attachments –...
  • Page 62: Lightning Strike

    ERTC022-10-AS MAINTENANCE MANUAL LIGHTNING STRIKE If flown through a region of the atmosphere where electrical discharge is occurring, the airplane may become part of the discharge path. During a lightning strike, the current enters the airplane at one point and exits another, usually at opposite extremities. It is in these entrance and exit points where damage is most likely to occur.
  • Page 63 ERTC022-10-AS MAINTENANCE MANUAL LIGHTNING STRIKE INSPECTIONS Page: 1 of 6 Ref. Prescribed works Made by Checked by 1. GENERAL – PREPARATORY WORKS Determine where the lightning struck the airplane and inspect the surrounding area carefully for damage. Determine where the lightning exited the airplane and inspect the surrounding area carefully for damage.
  • Page 64 ERTC022-10-AS MAINTENANCE MANUAL LIGHTNING STRIKE INSPECTIONS Page: 2 of 6 Ref. Prescribed works Made by Checked by Cooling system 75-00 Check water cooler for condition and leaks. 75-00 Check hoses and tubes for condition and evidence of damage. Oil system 79-10 Check oil tank for condition.
  • Page 65 ERTC022-10-AS MAINTENANCE MANUAL LIGHTNING STRIKE INSPECTIONS Page: 5 of 6 Ref. Prescribed works Made by Checked by Trim tab 55-20 Check tab for condition. 8. VERTICAL TAIL UNIT 55-40 Check VTU structure / skin for condition and evidence of damage; contact airplane manufacturer if any damage were found.
  • Page 66 ERTC022-10-AS MAINTENANCE MANUAL LIGHTNING STRIKE INSPECTIONS Page: 6 of 6 Ref. Prescribed works Made by Checked by 10. OPERATIONAL TEST 33-40 lnterior and exterior lighting – check function. 33-10 34-10 Pitot-static tube heating – check function. 34-10 Stall speed warning sensor – check function. 27-30 Pitch trim –...
  • Page 67 ERTC022-10-AS MAINTENANCE MANUAL EXCEEDING OF ENGINE / PROPELLER LIMITATIONS Exceeding of engine limitations If the engine limitations have been exceeded during the airplane operation, follow instructions in the Maintenance Manual (Line Maintenance) for Rotax Engine Type 912 Series (Ref. No. MML- 912, Part.
  • Page 68 ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 05-50 Effectivity: All Page 05-48 Issue 2 | Rev. 0 2017-12-22...
  • Page 69 ERTC022-10-AS MAINTENANCE MANUAL CHAPTER 06 DIMENSIONS AND AREAS TABLE OF CONTENTS Title Section Page Airplane 3-View Drawing..................06-10 ...... 06-3 Dimensions and Areas ..................... 06-20 ...... 06-5 External dimensions ........................06-5 Wing ............................... 06-5 Ailerons ............................06-5 Flaps ............................... 06-5 Horizontal Tail Units ........................
  • Page 70 ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 06-TOC Effectivity: All Page 06-2 Edition 2 | Rev. 0 2017-12-22...
  • Page 71 ERTC022-10-AS MAINTENANCE MANUAL AIRPLANE 3-VIEW DRAWING Figure 06-1 3-view drawing of the airplane SportStar RTC (page 1 of 2) 06-10 Effectivity: All Page 06-3 Edition 2 | Rev. 1 2019-03-22...
  • Page 72 ERTC022-10-AS MAINTENANCE MANUAL Figure 06-1 3-view drawing of the airplane SportStar RTC (page 2 of 2) 06-20 Platnost: Všechny letouny Page 06-4 Edition 2 | Rev. 1 2019-03-22...
  • Page 73 ERTC022-10-AS MAINTENANCE MANUAL LIDS AND COVERS ON THE AIRPLANE GENERAL Lids and covers on the airplane are shown in Figure 06-2. Legends of these figures include description of attachment of the lids / covers and the areas which can be accessed after they are open / removed. If the legend of the figure does not include description of attachment of the lids / covers, the following rule applies: –...
  • Page 74 ERTC022-10-AS MAINTENANCE MANUAL LIST OF COVERS AND LIDS ON THE AIRPLANE Figure 06-2 Lids and covers on the airplane 06-40 Effectivity: All Page 06-8 Edition 2 | Rev. 1 2019-03-22...
  • Page 75 ERTC022-10-AS MAINTENANCE MANUAL Designation Description Propeller spinner Engine upper cowling Cap for oil level check Cap for coolant level check Engine lower cowling Upper cover of the fuselage front section Inspection cap on the fuselage lower part Cover of the rear part of the fuselage Cover for access to the Pitot-static system drain sumps Rocket cover (if the emergency parachute system is installed;...
  • Page 76 ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 06-40 Effectivity: All Page 06-10 Edition 2 | Rev. 1 2019-03-22...
  • Page 77 ERTC022-10-AS MAINTENANCE MANUAL INTERIOR PLACARDS AND MARKINGS LIST OF INTERIOR PLACARDS AND MARKINGS SERIAL PLACARD COLOUR LOCATION FIG. R inner side of the cockpit in front of the ventilation window Black 11-2 (airplane equipped with the Klassic 170/3/R propeller). R inner side of the cockpit in front of the ventilation window Black...
  • Page 78 ERTC022-10-AS MAINTENANCE MANUAL SERIAL PLACARD COLOUR LOCATION FIG. L part of the instrument Black / panel at the pitch trim 11-2 white indicator. Central part of the Black / instrument panel below 11-2 white the choke controller. Central part of the Black / instrument panel above 11-2...
  • Page 79 ERTC022-10-AS MAINTENANCE MANUAL SERIAL PLACARD COLOUR LOCATION FIG. L part of the instrument Black / 11-2 panel at the selector white valve. Bulkhead of the area Black / behind the baggage 11-2 white compartment. Black / Central panel at the 11-2 white emergency hammer.
  • Page 80 ERTC022-10-AS MAINTENANCE MANUAL SERIAL PLACARD COLOUR LOCATION FIG. Central part of the instrument panel, on the Black 11-2 upper part of the canopy frame. Black / L part of the instrument 11-2 white panel. Black / L part of the instrument 11-2 white panel at the dimmer.
  • Page 81 ERTC022-10-AS MAINTENANCE MANUAL SERIAL PLACARD COLOUR LOCATION FIG. L part of the instrument panel at the auxiliary Black / 11-2 white generator signalling light. R part of the instrument Black / panel at USB 11-2 white connectors. L part of the instrument Black / panel at switches and 11-2...
  • Page 82 ERTC022-10-AS MAINTENANCE MANUAL SERIAL PLACARD COLOUR LOCATION FIG. R part of the instrument Black / panel at circuit 11-2 white breakers. NOTE: The above specified layout of the placards applies to the standard design of the airplane, it may vary depending on the installed equipment. Relay behind the Black instrument panel.
  • Page 83 ERTC022-10-AS MAINTENANCE MANUAL SERIAL PLACARD COLOUR LOCATION FIG. L and R side of the 11-2 canopy frame. L and R adjustable Black 11-2 pedals lever. L part of the instrument Black / panel at the signalling 11-2 white light of the EMS. L part of the instrument Various panel at circuit breakers...
  • Page 84 ERTC022-10-AS MAINTENANCE MANUAL SERIAL PLACARD COLOUR LOCATION FIG. Black / L part of the instrument 11-2 white panel at the dimmer. Black / L part of the instrument 11-2 white panel bellow the switch. Black / L part of the instrument 11-2 white panel above the switch.
  • Page 85 ERTC022-10-AS MAINTENANCE MANUAL Fig. 11-2 Interior placards and markings (page 1 of 2) 11-30 Effectivity: All Page 11-17 Edition 2 | Rev. 0 2017-12-22...
  • Page 86 ERTC022-10-AS MAINTENANCE MANUAL Fig. 11-2 Interior placards and markings (page 2 of 2) 11-30 Effectivity: All Page 11-18 Edition 2 | Rev. 1 2019-03-22...
  • Page 87 ERTC022-10-AS MAINTENANCE MANUAL Pressure check and inflation of tyres of the landing gear wheels Check and inflate the tyres of the landing gear wheels when the weather conditions are calm and the airplane stands on a flat and level surface. Procedure Brake the airplane with wheel blocks.
  • Page 88 ERTC022-10-AS MAINTENANCE MANUAL Bleeding of the brake system If the brake efficiency is reduced or the brake pumps don´t return, it is probable that air penetrated into the brake system. The air must be eliminated in order to ensure a correct braking efficiency.
  • Page 89 ERTC022-10-AS MAINTENANCE MANUAL Fig. 12-3 Bleeding screw Brake fluid change Brake fluid thickens during operation of the airplane and absorbs water. This condition causes malfunctions of the brake system. It is not possible to determine when the malfunction occurs. Period for the brake fluid replacement is mentioned in Section 05-30. Procedure Align the airplane in a horizontal position (Section 08-10).
  • Page 90 ERTC022-10-AS MAINTENANCE MANUAL SCHEDULED SERVICING INTRODUCTION This Section includes information which is necessary for regular maintenance of the airplane.This Section includes the Lubricating Chart and instructions for cleaning of the airplane exterior and interior including the necessary material. LUBRICATING CHART Lubrication fundamentals Lubricate the movable or revolving parts of the airplane in specified time intervals (Tab.
  • Page 91 ERTC022-10-AS MAINTENANCE MANUAL Lubricating points Every 100 hours Unit Lubricating point Lubricant annual Oil change in accordance with the Engine Manual Carburettor control cable at inlet into the bowden (in Oil WD-40 Engine the engine compartment) or equivalent Choke control cable at inlet into the termination (in the Oil WD-40 engine compartment) or equivalent...
  • Page 92 ERTC022-10-AS MAINTENANCE MANUAL Every 100 hours Unit Lubricating point Lubricant annual MOGUL MOLYKA G, All movable joints in the cockpit or equivalent Rudder MOGUL MOLYKA G, The passages of rudder control cables control or equivalent Brake system control cables at inlets in the bowdens MOGUL MOLYKA G, (at brake pedals) or equivalent...
  • Page 93 ERTC022-10-AS MAINTENANCE MANUAL Cleaning of display units and avionics hardware Use cleaning agents specially designed for display surfaces which are safe for antireflective layers. Use a soft, lint-free cloth to apply the agent. Cleaning of the engine CAUTION WHEN YOU CLEAN THE ENGINE, DO NOT USE HIGHLY FLAMMABLE LIQUIDS AND THINNERS! If necessary, clean the engine with due diligence.
  • Page 94 ERTC022-10-AS MAINTENANCE MANUAL UNSCHEDULED SERVICING WINTER OPERATION General It is considered a winter operation, if the outside temperature falls below +5 °C. Preparing the airplane for winter operation Airplane airframe Lubricate the airplane in accordance with the Lubricating Chart in the scope of inspection after 100 hours of operation, if the last inspection was not within 6 months (Section 12-20).
  • Page 95 ERTC022-10-AS MAINTENANCE MANUAL CHAPTER 24 ELECTRICAL POWER TABLE OF CONTENTS Item Section Page General ........................24-00 ...... 24-3 Introduction............................. 24-3 DC generation ......................24-30 ...... 24-7 Description and operation ......................24-7 A. Indication of electrical system ....................24-7 B. Signalization of electrical system .................... 24-7 C.
  • Page 96 ERTC022-10-AS MAINTENANCE MANUAL Maintenance practices ......................... 24-44 A. Switches ..........................24-44 B. Circuit breakers ........................24-45 24-TOC Effectivity: All Page 24-2 Edition 2 | Rev. 1 2019-03-22...
  • Page 97: General

    ERTC022-10-AS MAINTENANCE MANUAL GENERAL INTRODUCTION The electrical system of the aircraft is of a single-wire DC type. It works with a voltage of 14 V and the negative pole on the airframe. Optionally, the electrical system can be equipped with the auxiliary generator or the external alternator and the external power source socket.
  • Page 98 ERTC022-10-AS MAINTENANCE MANUAL Fig. 24-1 Source system without auxiliary generator 24-00 Effectivity: All Page 24-4 Edition 2 | Rev. 1 2019-03-22...
  • Page 99 ERTC022-10-AS MAINTENANCE MANUAL Fig. 24-2 Source system with auxiliary generator 24-00 Effectivity: All Page 24-5 Edition 2 | Rev. 1 2019-03-22...
  • Page 100 ERTC022-10-AS MAINTENANCE MANUAL Fig. 24-3 Source system with eaternal alternator 24-00 Effectivity: All Page 24-6 Edition 2 | Rev. 1 2019-03-22...
  • Page 101: Dc Generation

    ERTC022-10-AS MAINTENANCE MANUAL DC GENERATION DESCRIPTION AND OPERATION The primary source of electrical energy is the generator with a power of 250 W with an external rectifier. The secondary source of electrical energy is the battery FG Forte 12150 (12 V / 15 Ah) that is located in the engine compartment on the firewall.
  • Page 102: Auxiliary Generator

    ERTC022-10-AS MAINTENANCE MANUAL Technical parameters of the regulator: Type electronical Output voltage 14 ± 0,3 V (from 1000 ± 250 RPM) Range of operating temperatures Min. -25 °C, Max. +90 °C Weight 0,3 kg Auxiliary generator The auxiliary generator can be optionally installed on the airplane; the previously used type SD- or a newer type BC 425-H.
  • Page 103: Battery Sv-Bat-320

    ERTC022-10-AS MAINTENANCE MANUAL Technical parameters: Battery type FG12150 FG12200 Voltage 12 V 12 V Design service life 3 – 5 years 3 – 5 years Maximum discharging current (25 °C) 225 A (5 s) (25 °C) 300 A (5 s) Kind of charging Constant voltage (25 °C) Constant voltage (25 °C)
  • Page 104: Socket For 12 V Appliances

    ERTC022-10-AS MAINTENANCE MANUAL CAUTION CHARGE THE BATTERY ONLY VIA THE ONBOARD NETWORK AIRPLANE. ATTEMPT RECHARGE THE BATTERY BY USING AN EXTERNAL BATTERY CHARGER DIRECTLY CONNECTED TO THE INPUT OF THE BATTERY. I. Socket for 12 V appliances The socket for 12 V appliances is located in the right lower corner of the instrument panel. It is switched on/off by means of the switch SOCKET 12V/2A.
  • Page 105: Maintenance Practices

    ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Generator When removing / installing the generator, follow the engine manufacturer manual – Maintenance Manual (Heavy Maintenance) for Rotax Engine Type 912 Series, Doc. No. MMH- 912/MMH-914, 899603. Generator rectifier Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material:...
  • Page 106 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 24-4 Generator rectiofier Washer 5,3 Connector Nut M5 Capacitor Cable tie Holder of capacitor Spacing insert Wire with cable eye For information Screw M5x16 Firewall Fig. 24-4 Generator rectifier – removal / installation 24-30 Effectivity: All Page 24-12 Edition 2 | Rev.
  • Page 107: Auxiliary Generator

    ERTC022-10-AS MAINTENANCE MANUAL Auxiliary generator Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Wrench No. 10 1 pc. Phillips screwdriver No. 2 1 pc.
  • Page 108 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 24-5 Auxiliary generator Washer Cable Rubber cover of contact Regulator connector Hose fastener Propeller gearbox Fig. 24-5 Auxiliary generator – removal / installation 24-30 Effectivity: All Page 24-14 Edition 2 | Rev. 1 2019-03-22...
  • Page 109: Auxiliary Generator Regulator

    ERTC022-10-AS MAINTENANCE MANUAL Auxiliary generator regulator Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Wrench No. 10 1 pc. Phillips screwdriver No. 2 1 pc.
  • Page 110 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 24-6 Auxiliary generator regulator Nut M5 Wires Terminal strip of regulator Ground wire For information: Screw M5 Firewall Washer 5,3 Fig. 24-6 Auxiliary generator regulator – removal / installation 24-30 Effectivity: All Page 24-16 Edition 2 | Rev.
  • Page 111: External Alternator

    ERTC022-10-AS MAINTENANCE MANUAL External alternator Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Wrench No. 10 1 pc. Socket wrench No. 13 1 pc.
  • Page 112 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 24-7 External alternator Lock washer Cable Washer 8,4 Nut M5 V-belt Washer 6 For information: Connector Bracket Bolt M10x45 Tension bar Washer 10,1 V-belt pulley Bolt M8x20 Bolt M8x20 Fig. 24-7 External alternator – removal / installation 24-30 Effectivity: All Page 24-18...
  • Page 113 ERTC022-10-AS MAINTENANCE MANUAL Adjustment / test – V-belt tensioning Switch the electrical network off and disconnect the battery. Remove the engine cowlings (Section 71-10). Push the belt with a force of 50 N; the deflection can be max. 6 mm (see Fig. 24-8). If the deflection is larger, tension the belt: Loose the bolts (2;...
  • Page 114: External Alternator V-Belt / V-Belt Pulley

    ERTC022-10-AS MAINTENANCE MANUAL External alternator V-belt / V-belt pulley Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Wrench No. 17 1 pc. Hex bit No.
  • Page 115 ERTC022-10-AS MAINTENANCE MANUAL Install the engine cowlings (Section 71-10). Connect the battery, switch the electrical network on. Start the engine, do the engine test and check engine parameters. Legend to Fig. 24-9 V-belt pulley Screw M5x16 (8 pcs.) V-belt Lock washer 5 (8 pcs.) Pair of pulley carrier halves Engine flange Fig.
  • Page 116: Battery Fg Forte 12150 / Fg Forte 12200

    ERTC022-10-AS MAINTENANCE MANUAL Battery FG Forte 12150 / FG Forte 12200 Maintenance type: Line Personnel Independent verification personnel qualified in accordance with Part qualification: 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Tester capacity Aircraft Battery Check of battery Charger / Analyzer 1 pc.
  • Page 117 ERTC022-10-AS MAINTENANCE MANUAL Servicing – charging the battery FG Forte CAUTION THE RECOMMENDED TEMPERATURE FOR CHARGING THE BATTERY IS IN A RANGE OF +5 TO +30 °C. AT A LOWER TEMPERATURE THAN 5 °C OR HIGHER THAN 30 °C, THE BATTERY ISN´T FULLY CHARGED OR IS OVERHEATED, WHICH REDUCES THE BATTERY SERVICE LIFE.
  • Page 118 ERTC022-10-AS MAINTENANCE MANUAL Pull down the rubber cover of contact (6) and unscrew the screw (2). Remove the washers (4) and (5). In a suitable way, insulate the cable end. In the same way, disconnect the cable (3) of the positive pole. Cut the lockwire of the lock of buckle (6) or turnbuckle (7).
  • Page 119 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 24-10 Battery Rubber cap of contacts Screw M5 Holder of battery with buckle Cable Holder of battery with turnbuckle Spring washers For information: Washer Firewall Fig. 24-10 Battery FG Forte – removal / installation (page 2 of 2) Installation –...
  • Page 120: Battery Sv-Bat-320

    ERTC022-10-AS MAINTENANCE MANUAL Check the discharging time of 24 minutes: If the voltage of the battery doesn´t decrease after 24 minutes of discharging below 10,4 V, it is considered as complying. If the voltage of the battery decreases sooner than in 24 minutes of discharging below 10,4 V, it is considered as non-complying.
  • Page 121 ERTC022-10-AS MAINTENANCE MANUAL NOTE The procedure for removal / installation is identical for the left battery and also for the right battery. Removal – battery SV-BAT-320 Switch the electrical network off and disconnect the battery. Remove the cover of the upper part of fuselage F4 (Section 53-30). Disconnect the connector (2, Fig.
  • Page 122 ERTC022-10-AS MAINTENANCE MANUAL Installation – battery SV-BAT-320 Place the battery (1, Fig. 24-12) on the bracket (6) and attach it by means of the screws (3), washers (5) and the nuts (4). Connect the connector (2) to the harness. Install the cover of the upper part of the fuselage F4 (Section 53-30). Connect the battery.
  • Page 123: Battery Ibbs-12V-3Ah

    ERTC022-10-AS MAINTENANCE MANUAL I. Battery IBBS-12v-3ah Maintenance type: Line Personnel Independent verification personnel qualified in accordance with Part qualification: 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Wrench No. 7 1 pc. Flat screwdriver 1 pc. Cable tie 2,5x99 As needed...
  • Page 124 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 24-13 Battery IBBS-12v-3ah Washer 4.3 (4 pcs.) Wires with connector For information: Screw M4x10 (4 pcs.) Bracket Nut M4 (4 pcs.) Bracket Fig. 24-13 Battery IBBS-12v-3ah – removal / installation 24-30 Effectivity: All Page 24-30 Edition 2 | Rev.
  • Page 125: Socket For 12 V Appliances

    ERTC022-10-AS MAINTENANCE MANUAL Adjustment / test – capacity test of the battery IBBS-12v-3ah Turn off the MASTER SWITCH. Turn on the BATTERY G3X switch. Both screens must be in operation including all displayed data (PFD, MFD, GPS). Monitor and record whether any of the connected devices (PFD, MFD, ADAHRS 1 and EIS) will fail to function within 30 minutes of starting the test, or until the output voltage of the backup battery drops to 9,5V.
  • Page 126 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 24-14 Socket body For information: Wire with connector Instrument panel Wire with Faston connector Fig. 24-14 12 V socket – removal / installation 24-30 Effectivity: All Page 24-32 Edition 2 | Rev. 1 2019-03-22...
  • Page 127: Relay

    ERTC022-10-AS MAINTENANCE MANUAL Relay Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Flat screwdriver Small 1 pc. Flat screwdriver Middle 1 pc. Wrench No.
  • Page 128 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 24-15 Relay 12 V / 30 A Wire with cable eye Wire with connector Screw M5 Screw M4 Nut M5 Washer 4,3 Washer 5,3 Nut M4 Screw Relay 12 V / 75 A For information Wire with connector Bracket Fig.
  • Page 129 ERTC022-10-AS MAINTENANCE MANUAL Removal – relay 12 V / 75 A Switch the electrical network off and disconnect the battery. Remove the cover of the upper part of fuselage F4 (Section 53-30). Unscrew the screws (12, Fig. 24-15) attaching the cable eyes (8) to the relay contacts (6).
  • Page 130: Description And Operation

    ERTC022-10-AS MAINTENANCE MANUAL EXTERNAL POWER DESCRIPTION AND OPERATION Optionally, the socket of 12 V external source of Piper 11–041 type may be installed on the airplane. The socket is located on the right front part of the fuselage behind the firewall. After opening the socket cap, it is possible to connect the 12 V ground source of electrical energy provided with the corresponding plug (Piper).
  • Page 131 ERTC022-10-AS MAINTENANCE MANUAL Fig. 24-16 Source system with socket for ground source of electrical energy NOTE Fig. 24-16 supplements Fig. 24-1, Fig. 24-2 and Fig. 24-3. 24-40 Effectivity: All Page 24-37 Edition 2 | Rev. 1 2019-03-22...
  • Page 132: Maintenance Practices

    ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Socket of external power source Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher The recommended tools and material: Item Designation / Size Quantity Note Hex key No. 5 1 pc.
  • Page 133 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 24-17 Socket Nut M8 Cable of electrical bonding (-) Washer 8,4 Cable (+) For information: Screw M8 Right side skin of fuselage Fig. 24-17 Socket of external power source – removal / installation 24-40 Effectivity: All Page 24-39 Edition 2 | Rev.
  • Page 134: Electrical Load Distribution

    ERTC022-10-AS MAINTENANCE MANUAL ELECTRICAL LOAD DISTRIBUTION DESCRIPTION AND OPERATION The electrical system of the airplane is of a single-wire type, DC. It works with a voltage of 14 V and the minus pole on the airframe. The electrical energy is distributed to the individual systems by the main busbar and by the avionics busbar.
  • Page 135 Dynon SkyView system. The optional equipment isn´t included. The Pilot´s Operating Handbook for SportStar RTC airplane shows the layout of circuit breakers corresponding to particular airplane.
  • Page 136 ERTC022-10-AS MAINTENANCE MANUAL Designation Value (A) Description Not used Not used RPM IND. Circuit breaker of engine speed indicator ENG. INSTR. Circuit breaker of engine instruments FUEL IND. Circuit breaker of fuel gauges + fuel pressure indicator COMM Circuit breaker of transceiver Circuit breaker of navigation equipment ALT.
  • Page 137 ERTC022-10-AS MAINTENANCE MANUAL Designation Value (A) Description ACCU Circuit breaker of battery GEN - REF. Circuit breaker of generator excitation Circuit breaker of generator AUX. GEN Circuit breaker of auxiliary generator AUX. GEN. FIELD Circuit breaker of auxiliary generator excitation BATTERY G3X Circuit breaker of backup battery IBBS-12v-3ah BEACONS...
  • Page 138 ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Switches Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Flat screwdriver 1 pc. NOTE Removal / installation procedure of switches is identical for the type 1 PST, 2 PST and as well as for the illuminated rocker switches type R13-66 and S7 68-72 01.
  • Page 139 ERTC022-10-AS MAINTENANCE MANUAL Installation – the switches Insert the switch (1; 2, Fig. 24-18) into the appropriate hole in the instrument panel (3) until the flexible detents fit in. Connect the wires to the switch. Connect the battery, switch the electrical network on and check the function of the switch.
  • Page 140 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 24-19 Circuit breaker 2TC2 Screw Circuit breaker ETA Spring washer Holder of circuit breakers Spring washer Spring washer Spring washer Screw Fig. 24-19 Circuit breakers – removal / installation (typical) 24-60 Effectivity: All Page 24-46 Edition 2 | Rev.
  • Page 141 ERTC022-10-AS MAINTENANCE MANUAL GENERAL INTRODUCTION The equipment and furnishings of the airplane includes the seats for the crew, safety harnesses, baggage compartment, interior panels, carpets on the airplane cabin floor and emergency equipment (first aid kit, emergency hammer, ELT and optionally installed emergency parachute system). 25-10 Effectivity: All Page 25-3...
  • Page 142 ERTC022-10-AS MAINTENANCE MANUAL FLIGHT COMPARTMENT DESCRIPTION AND OPERATION The cockpit is equipped with two seats for the pilot and the second crewmember. Each seat is equipped with adjustable safety harnesses. Pilot seat The pilot seat (1; 2, Fig. 25-1) consists of a seat (4; 5) and a backrest (3). The seat consists of the metal sheet, which covers the main wing spar.
  • Page 143 ERTC022-10-AS MAINTENANCE MANUAL WHEN YOU CLEAN THE SAFETY HARNESS, MAKE SURE THAT THE CLEANING AGENTS WILL NOT COME INTO CONTACT WITH MECHANICAL PARTS OF THE SAFETY HARNESS. DO NOT USE SOAP OR WATER WHEN YOU CLEAN THE METAL PARTS. Safety harness Clean the belt chemically or carefully clean the belt with a soft brush and cold soap solution.
  • Page 144 ERTC022-10-AS MAINTENANCE MANUAL Interior panels Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Flat screwdriver 2 pcs. Wrench No. 5,5 1 pc. Wrench No.
  • Page 145 ERTC022-10-AS MAINTENANCE MANUAL Installation – instrument panel The installation procedure for the instrument panel is described in Section 39-10. Legend to Fig. 25-5 Left control rod cover Bolt M4 (4 pcs. + 4 pcs. / 8 pcs.) Right control rod cover Flexible clamp Fig.
  • Page 146 ERTC022-10-AS MAINTENANCE MANUAL Unscrew and remove the nuts (6), washers (8) and bolts (4) which attach the central ledge (2) to the central panel (10). Remove the central ledge (2). Installation – ledges of the instrument panel Align the ledge (1, Fig 25-6) with the instrument panel and attach it by the nuts (7) with washers (9).
  • Page 147 ERTC022-10-AS MAINTENANCE MANUAL CARGO COMPARTMENTS DESCRIPTION AND OPERATION The baggage compartment is located in the cabin behind the pilot seats (see Fig. 25-9). It is equipped with a net which prevents unwanted baggage movement. Both sides of the baggage compartment include mesh pockets (3;...
  • Page 148 ERTC022-10-AS MAINTENANCE MANUAL EMERGENCY DESCRIPTION AND OPERATION The airplane emergency equipment includes the Emergency Locator Transmitter (2, Fig. 25-10), first aid kit (1), and emergency hammer (3). Optionally may be installed the emergency parachute system (4). Emergency Locator Transmitter The Emergency Locator Transmitter (ELT) is designed to identify the airplane position after the emergency landing or crash.
  • Page 149 ERTC022-10-AS MAINTENANCE MANUAL GENERAL INTRODUCTION This chapter describes equipment of the airplane which is used to extinguish fire. Fire protection is provided by a hand fire extinguisher, mounted in the cockpit. Passive fire protection is provided as follows: • On the inner surface of the engine cowlings is applied fire resistant coating (Section 71-10). •...
  • Page 150 EXTINGUISHING DESCRIPTION AND OPERATION The Sportstar RTC airplane is equipped with a portable fire extinguisher (1, Fig. 26-1) mounted within a quick-release holder (5) attached on the bulkhead (4) separating the cockpit and baggage compartment. In a new version, the extinguisher (1) is located on the left control rod cover (5).
  • Page 151 ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Hand fire extinguisher Maintenance type: Line Personnel qualification: Pilot / Owner qualified in accordance with M.A.803. Recommended tools and material: Item Designation / Size Quantity Note Scale 1 pc. Removal – hand fire extinguisher Release quick-release clamps (3, Fig. 26-1) / Velcro fasteners (5) on the straps. Remove the fire extinguisher (1) from the holder (2) / cover (6).
  • Page 152 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 26-1 Hand fire extinguisher Bulkhead Holder Strap with Velcro fasteners Strap with quick-release clamp Left control rod cover Fig. 26-1 Hand fire extinguisher – removal / installation 26-20 Effectivity: All Page 26-6 Edition 2 | Rev. 1 2019-03-22...
  • Page 153 ERTC022-10-AS MAINTENANCE MANUAL After finishing all the work related to installations and Removal of parts of control system, check the securing of all the elements in the control systems and their functionality. Adjustment / check – adjustment of deflections Maintenance type: Heavy Personnel Independent verification personnel qualified in accordance with Part...
  • Page 154 ERTC022-10-AS MAINTENANCE MANUAL The adjustability means a possibility to regulate the length of pull-rod within the specified range (Fig. 27-1). When adjusting the lengths of pull-rods, the adjustable end piece must never be unscrewed below the level of the check hole in the pull-rod. The checking needle or mandrel, with a diameter capable of passing through the check hole, must always hit the threaded part of end piece (Fig.
  • Page 155 ERTC022-10-AS MAINTENANCE MANUAL CENTRAL WARNING SYSTEM DESCRIPTION AND OPERATION The airplane is equipped with optical and acoustic signalization, which informs the crew about unusual situations. Optical signalization The upper left section of the instrument panel includes signaling lights. Red signaling lights with the highest priority display failure states of the airplane systems.
  • Page 156 ERTC022-10-AS MAINTENANCE MANUAL The deflection of trim tabs of the airplane with analog devices is displayed on the pitch trim indicator (8, Fig. 31-7) which is installed in the left section of the instrument panel. For the wiring diagram of the optical signalization, refer to Chapter 91. Legend to Fig.
  • Page 157 ERTC022-10-AS MAINTENANCE MANUAL BRAKES DESCRIPTION AND OPERATION General The airplane is equipped with the opened hydraulic brake system S5 00-51 01. Optionally, the airplane can be equipped with the S5 00-61 01 brake system, which is assembled from the Matco manufacturer components. The brake system scheme is mentioned on Fig. 32-13. The brake system is equipped in both cases with the disk brakes on the main wheels.
  • Page 158 ERTC022-10-AS MAINTENANCE MANUAL The brake is provided with two brake pads, one of them serves as a pushing pad and the other one as a supporting pad. The brake pads are connected by means of two guide pins with the brake holder.
  • Page 159 ERTC022-10-AS MAINTENANCE MANUAL Put the sealing ring on the piston (5, Fig. 32-16). Insert the screw (7) into the piston (5) and put the sealing O-ring (12) on the screw shank (7). Insert the spring (8) into the body of the brake pump (1). Assemble the pistons (2) and (5) and insert them into the brake pump body (1).
  • Page 160 ERTC022-10-AS MAINTENANCE MANUAL Installation – brake pump CAUTION BEFORE THE INSTALLATION OF THE ASSEMBLED BRAKE PUMPS ON THE AIRPLANE, DO THE FUNCTION CHECK. NOTE The installation procedure is the same for all pumps. Position the brake pumps (1; 2; 3, Obr. 32-16) into the forks (10) on the intermediate shaft of the foot control.
  • Page 161 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 32-15 Brake pump E5 10-40 01 Fork pin Brake pump E5 10-40 02 Swivel nut Brake pump S5 20-40 01 Hose Pin 5x20 Intermediate shaft fork Washer 5,3 Pedal lever Cotter pin 1,6x12 Fig. 32-15 Brake pump – removal / installation 32-42 Effectivity: All Page 32-45...
  • Page 162 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 32-16 Pump body Ring U Fork with pin Piston Sealing ring ø 6x12 Securing nut Sealing ring ø 7,3x2.4 Spring Fig. 32-16 Brake pump S5 20-01 01 – disassembling / assembling 32-42 Effectivity: All Page 32-46 Edition 2 | Rev.
  • Page 163 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 32-17 Brake pump body Spring Piston Fork with pin Cylinder closure Locking ring Securing nut Sealing ring ø 4x2 Piston Sealing ring ø 7,3x2,4 Brake cylinder packing Sealing ring ø 11,3x2,4 Screw Sealing ring ø 5,6x2,4 Spring Fig.
  • Page 164 ERTC022-10-AS MAINTENANCE MANUAL Matco brakes Maintenance type: Line Personnel Independent verification personnel qualified in accordance with Part qualification: 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Wrench 7/16 in 1 pc. Alternative No. 11 Socket wrench No.
  • Page 165 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 32-20 Brake pump Washer 6,4 Pin 5x20 Angular connection Washer 5,3 Hose Cotter pin 1,6x12 Intermediate shaft fork Pin 6x20 Pedal lever Fig. 32-20 Matco brake pump – removal / installation 32-42 Effectivity: All Page 32-53 Edition 2 | Rev.
  • Page 166 ERTC022-10-AS MAINTENANCE MANUAL Parking brake valve NOTE The removal / installation procedure applies to both the Matco valve and the GoldFren valve. Removal – parking brake valve Remove the upholstery of the left pilot seat (Section 25-10). Remove the handgrip (4, Fig. 32-21) of the lever (1) attached by the screw (9) with the locking washer (14).
  • Page 167 ERTC022-10-AS MAINTENANCE MANUAL Fig. 32-21 Parking brake valve – removal / installation (page 1 of 2) 32-42 Effectivity: All Page 32-55 Edition 2 | Rev. 1 2019-03-22...
  • Page 168 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 32-21 Lever Washer 5,3 (4 pcs.) Bushing Washer 6,5 Nord-Lock Axis Bracket Handgrip Rubber washer (2 pcs.) Valve of parking brake Screw M4x12 (2 pcs.) Screw M5x14 Screw M4x8 (2 pcs.) Screw M5x35 Nut M4 (2 pcs.) Screw M4x10 (2 pcs.) Washer 4,3 (2 pcs.) Screw M6x16...
  • Page 169 ERTC022-10-AS MAINTENANCE MANUAL Remove the switch (1). Installation – switch of parking brake signaling Position the switch (1, Fig. 32-22) to the bracket (7) and attach it by means of screws (2), nuts (3) and the washers (4). Slide the new shrinkable hose on the wires (5), connect them to the switch by means of the soldering iron and solder.
  • Page 170 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 32-22 Switch For information: Screw M2x12 (2 pcs) Bracket Nut M2 (2 pcs) Bracket Washer 2.2 (4 pcs) Lever Wires Fig. 32-22 Switch of parking brake signaling – removal / installation 32-42 Effectivity: All Page 32-58 Edition 2 | Rev.
  • Page 171 ERTC022-10-AS MAINTENANCE MANUAL CHAPTER 33 LIGHTS TABLE OF CONTENTS Item Section Page General ........................33-00 ...... 33-3 Introduction............................. 33-3 Flight compartment ....................33-10 ...... 33-4 Description and operation ......................33-4 A. VFR day ..........................33-4 B. VFR day / night ........................33-4 Maintenance practices ........................
  • Page 172 ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 33-00 Platnost: Všechny letouny Strana 33-2 Vydání 2 | Rev. 0 2017-12-22...
  • Page 173: General

    GENERAL INTRODUCTION The system of interior (optionally) and exterior lighting is installed on the SportStar RTC airplane. The interior lighting includes the cockpit lighting which includes the instrument lighting and the instrument panel lighting. The exterior lighting includes position lights, strobe lights, landing / taxi light and optional taxi light.
  • Page 174: Flight Compartment

    ERTC022-10-AS MAINTENANCE MANUAL FLIGHT COMPARTMENT DESCRIPTION AND OPERATION VFR day The cockpit is illuminated by an adjustable lamp on the cockpit canopy frame. Use the switch COCKPIT LIGHT to control the lamp. This switch is located in the row of switches. Use the switch POS.
  • Page 175: Maintenance Practices

    ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Cockpit lighting Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Hex wrench No. 2,5 1 pc. Cable tie 2,5x99 23 pcs.
  • Page 176 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 33-1 Lamp Screw M3x16 (2 pcs.) Wires Bushing Guide rail Middle column Fig. 33-1 Cockpit lighting – removal / installation 33-10 Effectivity: All Page 33-6 Edition 2 | Rev. 1 2019-03-22...
  • Page 177: Controlled Power Source

    ERTC022-10-AS MAINTENANCE MANUAL Controlled power source Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Flat screwdriver 1 pc. Phillips screwdriver No. 2 1 pc.
  • Page 178: Pwm Dimmer

    ERTC022-10-AS MAINTENANCE MANUAL Installation – controlled power source Put the power source (1, Fig. 33-2) on the appropriate place on the firewall (6) and attach it with screws (2), washers (4) and nuts (3). Connect the wires (5). Refer to the wiring diagram in Chapter 91. Install the cover of the fuselage upper part F4 (Section 53-30).
  • Page 179 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 33-3 PWM dimmer Wire Knob For information: Instrument panel Fig. 33-3 PWM dimmer – removal / installation 33-10 Effectivity: All Page 33-9 Edition 2 | Rev. 1 2019-03-22...
  • Page 180: Exterior

    ERTC022-10-AS MAINTENANCE MANUAL EXTERIOR DESCRIPTION AND OPERATION The exterior lighting consists of positon / anti-collision lights and landing / taxi light (see Fig. 33-4). Optionally, the taxi light can be installed on the airplane. Standardly the airplane is equipped with Whelen 9034001 (green) and 9034002 (red) position / strobe lights and.
  • Page 181 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 33-4 Left position and strobe light Landing / taxi light Right position and strobe light Taxi light Fig. 33-4 Exterior lighting 33-40 Effectivity: All Page 33-11 Edition 2 | Rev. 1 2019-03-22...
  • Page 182: Maintenance Practices

    ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES 90340 series positon / strobe lights Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Philips screwdriver No. 2 1 pc.
  • Page 183 ERTC022-10-AS MAINTENANCE MANUAL CAUTION DO NOT TOUCH THE FLASHTUBE WITH BARE FINGERS. WHEN YOU HANDLE THE FLASHTUBE, WEAR SOFT GLOVES OR USE A CLEAN CLOTH. MOISTURE AND GREASE FROM YOUR FINGERS CAUSE MALFUNCTION OF THE FLASHTUBE. Remove the flashtube (3) and the seal (10). Installation –...
  • Page 184 ERTC022-10-AS MAINTENANCE MANUAL CAUTION DO NOT TOUCH THE FLASHTUBE WITH BARE FINGERS. WHEN YOU HANDLE THE FLASHTUBE, WEAR SOFT GLOVES OR USE A CLEAN CLOTH. MOISTURE AND GREASE FROM YOUR FINGERS CAUSE MALFUNCTION OF THE FLASHTUBE. Remove the flashtube (3) and the seal (10). Remove the lenses (5;...
  • Page 185 ERTC022-10-AS MAINTENANCE MANUAL Inspection / check – position / strobe lights Inspect the LED’s. If any one LED fails, the unit must be repaired or replaced. NOTE To reduce eye strain use an optical filter such as dark glasses or a blue covering dome during LED inspection. Inspect the lens.
  • Page 186 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 33-5 Light body Screw 6-32 5/16 (2 pcs.) Flashtube cover Seal Flashtube Screw M4x16 (3 pcs.) Flashtube lens Wires of the front pos. light Lens of the front light Connector with wires Seal Wires of the rear pos. light Lens of the rear light For information: Seal...
  • Page 187: Power Source Of The Strobe Lights

    ERTC022-10-AS MAINTENANCE MANUAL Power source of the strobe lights Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Phillips screwdriver No. 2 1 pc. Wrench No.
  • Page 188 ERTC022-10-AS MAINTENANCE MANUAL Connect the battery, switch the electrical network on and check function of the strobe lights. Legend to Fig. 33-6 Power source of the lights Washer 4,3 (4 pcs.) Connector with wires Grounding wire Screw M4x16 (4 pcs.) For information: Nut M4 (4 pcs.) Skin of the fuselage lower part...
  • Page 189: Orion 600 Series Positon / Anti-Collision Lights

    ERTC022-10-AS MAINTENANCE MANUAL Orion 600 series positon / anti-collision lights Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Philips screwdriver No. 2 1 pc.
  • Page 190 ERTC022-10-AS MAINTENANCE MANUAL If you install a new light, insert on the wires of the light the baseplate (3), crimp new contacts and install the connector (refer to the table Recommended tools and material). NOTE Refer to the wiring diagram in Chapter 91. Put the connector with wires (8) into the holes in the wingtip (9), align the baseplate (3) with the wingtip and attach it with screws (6).
  • Page 191 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 33-7 Light body Screw M3x16 (3 pcs.) Retainer Screw 2-56 3/16 (2 pcs.) Baseplate Connector with wires Lens For information: Screw 4-40 5/16 (3 pcs.) Wingtip Fig. 33-7 Position / anti-collision lights – removal / installation 33-40 Effectivity: All Page 33-21...
  • Page 192: 7114112 Landing / Taxi Light

    ERTC022-10-AS MAINTENANCE MANUAL 7114112 landing / taxi light Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Test jig 7810E2550001 1 pc. Light adjustment Jig with magnifier 7910S7911099 1 pc.
  • Page 193 ERTC022-10-AS MAINTENANCE MANUAL Fig. 33-8 Landing / taxi light – removal / installation (page 1 of 2) 33-40 Effectivity: All Page 33-23 Edition 2 | Rev. 0 2017-12-22...
  • Page 194 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 33-8 Landing / taxi light Spacer (2 pcs.) Wires with connector Bolt M6x45 (2 pcs.) Bracket Nut M6 (2 pcs.) Bolt M4x12 (4 pcs.) Washer 6,4 (2 pcs.) Nut M4 (4 pcs.) Washer 6,1 (2 pcs.) Washer 4,3 (8 pcs.) Cover Bracket...
  • Page 195: 7114112 Taxi Light

    ERTC022-10-AS MAINTENANCE MANUAL Fig. 33-9 Adjustment of the landing and taxi light 7114112 taxi light Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Test jig 7810E2550001...
  • Page 196 ERTC022-10-AS MAINTENANCE MANUAL Removal – taxi light Switch the electrical network off and disconnect the battery. Remove the light cover W8R (Fig. 06–2). Unscrew the bolts (17, Fig. 33-10) and remove the cover (16). Remove the nut (9), washer (10), bolt (8) and slightly pull the light out including the bracket (3).
  • Page 197 ERTC022-10-AS MAINTENANCE MANUAL Switch the electrical network and the switch TAXI LIGHT on. Use the adjusting screws (8; 12) to set vertical and horizontal position of the light so that the cone of light falls on the centre of the crosshair on the test jig.
  • Page 198 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 33-10 Taxi light Spacer (2 pcs.) Wires with connector Bolt M6x45 (2 pcs.) Bracket Nut M6 (2 pcs.) Bolt M4x12 (4 pcs.) Washer 6,4 (2 pcs.) Nut M4 (4 pcs.) Washer 6,1 (2 pcs.) Washer 4,3 (8 pcs.) Cover Bracket...
  • Page 199 ERTC022-10-AS MAINTENANCE MANUAL GENERAL INTRODUCTION SportStar RTC airplane may be equipped with Woodcomp Klassic 170/3/R propeller, or Woodcomp KW-31-033 propeller. 61-00 Effectivity: All Page 61-3 Edition 2 | Rev. 0 2017-12-22...
  • Page 200 The propeller blade pitch of the SportStar RTC airplane is set to 17°30‘. The composite propeller spinner is made of one piece. It is attached to the backplate with bolts.
  • Page 201 ERTC022-10-AS MAINTENANCE MANUAL Put the spinner (2) to the backplate (3) in the position marked by red dots on the circumference. Never install the spinner in other position. Attach the spinner with the bolts (7) with washers (8); secure the bolts with Loctite 243 adhesive.
  • Page 202 ERTC022-10-AS MAINTENANCE MANUAL Fig. 61-2 Bolt tightening sequence Check / inspection – Klassic 170/3/R propeller For information about the inspections of the propeller, refer to the document User Manual Klassic 170/3 Aircraft propeller (Doc. No UM-07 EN), date of issue 01.09. 2015, or later valid issue.
  • Page 203 ERTC022-10-AS MAINTENANCE MANUAL Woodcomp KW-31-033 propeller Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Hex wrench No. 6 1 pc. Wrench No. 13 1 pc.
  • Page 204 ERTC022-10-AS MAINTENANCE MANUAL Turn the propeller by hand and check the correct alignment of the carbons with the collector. The carbons must abut with the whole contact surface in the middle of the collector. Connect the battery, switch the electrical network on. Install the engine cowlings (Section 71-10).
  • Page 205 ERTC022-10-AS MAINTENANCE MANUAL CONTROLLING DESCRIPTION AND OPERATION KW-31-033 propeller blade pitch setting is enabled by a servomotor which is controlled by the electronic propeller governor CS 3-5 (Fig. 61-4). The propeller governor is standardly located on the central console below the instrument panel. The propeller governor operates in two modes: •...
  • Page 206 ERTC022-10-AS MAINTENANCE MANUAL Controls of the CS 3-5 propeller governor: CONSTANT SPEED / MANUAL Use the mode selector to switch between automatic mode and manual mode. Value setting control knob Turn the control knob to scroll through the menu and adjust the values. RPM INC / DEC In manual mode: position INC - speed will increase, position DEC - speed will decrease.
  • Page 207 ERTC022-10-AS MAINTENANCE MANUAL CHAPTER 71 POWER PLANT TABLE OF CONTENTS Item Section Page General ........................71-00 ...... 71-3 Introduction............................. 71-3 A. Operational and technical data ....................71-4 Troubleshooting ..........................71-5 Maintenance practices ........................71-6 A. Engine ............................. 71-6 Cowling ........................71-10 ....71-11 Description and operation ......................
  • Page 208 ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 71-TOC Effectivity: All Page 71-2 Edition 2 | Rev. 0 2017-12-22...
  • Page 209: General

    GENERAL INTRODUCTION The Sportstar RTC airplane is equipped with the engine ROTAX 912 ULS2 or ROTAX 912 S2. The ROTAX 912 is a four-cylinder four-stroke engine with opposed cylinders and one camshaft. Valve trains: OHV engine. Cylinder bore of the engine 84 mm, stroke 61 mm. Engine displacement 1352 .
  • Page 210: Operational And Technical Data

    ERTC022-10-AS MAINTENANCE MANUAL Operational and technical data Type of engine: ROTAX 912 ULS2 / S2 Max. takeoff 100 hp / 73.5 kW (5800 RPM) Power Max. continuous 93,8 hp / 69 kW (5500 RPM) Cruising 71 hp / 53 kW (4800 RPM) 5800 RPM (for a time of 5 min as a Max.
  • Page 211: Troubleshooting

    ROTAX ENGINE OPERATION HANDLING INSTALLED SPORTSTAR RTC AIRCRAFT IS INCLUDED IN THE ACCOMPANYING DOCUMENTATION PROVIDED BY THE ENGINE MANUFACTURER, AS AMENDED. IF THERE IS ANY DISCREPANCY BETWEEN THIS MANUAL AND THE DATA PROVIDED BY THE ENGINE MANUFACTURER, THE ENGINE MANUFACTURER´S DATA AND VALUES ARE VALID.
  • Page 212: Maintenance Practices

    ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Engine Maintenance type: Heavy Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Cable tie 4,8x368 As needed Cable tie 2,5x99 As needed Stainless lockwire ø...
  • Page 213 ERTC022-10-AS MAINTENANCE MANUAL Removal – engine from the airplane Switch the electrical network off and disconnect the battery. Switch the fuel cock control to the OFF position. Remove the upper part of the engine cowling (Section 71-10). Unscrew and remove the screws (3, Fig. 71–2) with the washers (5) that attach the liquid cooler to the lower cowling of the engine (2).
  • Page 214 ERTC022-10-AS MAINTENANCE MANUAL Install the strut between the engine mount and the airbox (Section 71-60). Suspend the engine with the engine mount on the workshop crane (Fig. 71–1). Install the silentblocks: Insert both parts of the silentblock (4) into the eye of the upper attachment (detail A, Fig.
  • Page 215 ERTC022-10-AS MAINTENANCE MANUAL Fig. 71–1 Engine – removal / installation (page 1 of 2) 71-00 Effectivity: All Page 71-9 Edition 2 | Rev. 0 2017-12-22...
  • Page 216 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 71–1 Bolt (4 pcs.) Washer (2 pcs.) Washer (2 + 2 pcs.) Crane Cup (2 + 2 pcs.) Straps Silent block (8 pcs.) Engine Insert (4 pcs.) Engine mount Washer (4 pcs.) Fig. 71-1 Engine – removal / installation (page 2 of 2) 71-00 Effectivity: All Page 71-10...
  • Page 217: Cowling

    ERTC022-10-AS MAINTENANCE MANUAL COWLING DESCRIPTION AND OPERATION The engine cowlings serve as an aerodynamic cover of the engine. The cowlings are designed as a two-piece composite pressed part; on the inner side, the cowlings are provided with a non-flammable coating. In the front part of the original engine cowlings, there is a circular cut-out for the flange and the propeller shaft.
  • Page 218: Maintenance Practices

    ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Engine cowlings Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Phillips screwdriver No. 2 1 pc. WARNING SWITCH OFF THE IGNITION AND TAKE OUT THE KEY! NOTE The removal / installation procedures for original and new wheel...
  • Page 219 ERTC022-10-AS MAINTENANCE MANUAL Fig. 71-2 Engine cowlings – removal / installation (page 1 of 2) 71-10 Effectivity. All Page 71-13 Edition 2 | Rev. 1 2019-03-22...
  • Page 220 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 71–2 Upper engine cowling Screw M4x12 (4 pcs.) Lower engine cowling Polyamide washer 3,7 (12 pcs.) Screw M4x16 (4 pcs.) Camlock Fig. 71-2 Engine cowlings – removal / installation (page 2 of 2) 71-10 Effectivity: All Page 71-14 Edition 2 | Rev.
  • Page 221: Mounts

    ERTC022-10-AS MAINTENANCE MANUAL MOUNTS DESCRIPTION AND OPERATION The engine is suspended on the engine mount in the airplane. The engine mount is composed of the spatial part welded from steel, Cr-Mo tubes. The engine mount is formed by a trapezoidal frame and the attachment eyes are welded on its tops.
  • Page 222 ERTC022-10-AS MAINTENANCE MANUAL Fig. 71–3 Engine mount (page1 of 2) 71-20 Effectivity: All Page 71-16 Edition 2 | Rev. 0 2017-12-22...
  • Page 223 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 77–3 Engine Washer Engine mount Washer Firewall Screw Washer Screw Locking washer Safety plug Cotter pin Silent block Bracket for attachment of exhaust pipe muffler Washer Fig. 71-3 Engine mount (page 2 of 2) NOTE The details A and B (Fig.
  • Page 224: Maintenance Practices

    ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Engine mount Maintenance type: Heavy Personnel Independent verification personnel qualified in accordance with Part qualification: 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Torque wrench 1 pc. Hex key No. 8 1 pc.
  • Page 225 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 71–4 Engine mount Locking washer Safety plug Cotter pin Screw of suspension Bracket for attachment of exhaust pipe muffler Fig. 71-4 Engine mount – removal / installation 71-20 Effectivity: All Page 71-19 Edition 2 | Rev. 0 2017-12-22...
  • Page 226: Air Intakes

    The inlet of hot air serves for carburettor preheating under the conditions specified in the POH of Sportstar RTC airplane, Chapter 4. The air entering the exchanger on the exhaust pipe muffler is heated here and then the air flows through the hose into the neck for hot air intake located on the airbox.
  • Page 227 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 71–5 Upper engine cowling Lower engine cowling Fig. 71-5 Air inlets 71-60 Effectivity: All Page 71-21 Edition 2 | Rev. 1 2019-03-22...
  • Page 228: Maintenance Practices

    ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Air system of engine Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Phillips screwdriver No. 2 1 pc. Air filter ROTAX P/N 1 pc.
  • Page 229 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 71–6 Air filter Sleeve Filter bracket Sleeve Air hose Fig. 71-6 Replacement of air filter Removal – airbox Switch the electrical network off and disconnect the battery. Remove the engine cowlings (Section 71-10). Remove the clamps (23, Fig. 71–7) of the connecting hoses (6; 7). Remove the wire (24) attaching the hoses (19) and (20) to the airbox (1);...
  • Page 230 ERTC022-10-AS MAINTENANCE MANUAL Unlock the clamps (22) of the drain hoses (17) and (18) of the airbox (1). Pull down the hoses (17) and (18) from the outlets on the airbox (1). Remove the nut (30) and take out the washer (32); when removing the nut (30), hold the screw (26) by means of wrench, thus preventing it from slipping.
  • Page 231 ERTC022-10-AS MAINTENANCE MANUAL Install the engine cowlings (Section 71-10). Connect the battery, switch the electrical network on. Fig. 71–7 Airbox – removal / installation (page 1 of 2) 71-60 Effectivity: All Page 71-25 Edition 2 | Rev. 0 2017-12-22...
  • Page 232 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 71–7 Airbox Strut attachment Left sump of carburettor Cobra clamp Right sump of carburettor Hose clamp Strut Wire Silent block Screw M4 Left connecting hose Screw M5 Right connecting hose Screw M4 Inlet hose – cold air Nut M4 Inlet hose –...
  • Page 233 ERTC022-10-AS MAINTENANCE MANUAL Put the handle (1) on the protruding part of the string (3) and secure it by means of the screw (7). Check the function of the carburettor preheating control. Legend to Fig. 71–8 Handle Washer 8,4 Terminal Screw M3x4 Bowden string with tube Screw M4x4...
  • Page 234: Description And Operation

    ERTC022-10-AS MAINTENANCE MANUAL ENGINE DRAINS DESCRIPTION AND OPERATION The engine drainage is composed of the carburettor venting, outlet from the condensate sumps under the carburettors and from the outlet from the airbox. The carburettors are vented by means the hoses interconnecting the draining outlets of the carburettors with the outlets on the front, upper part of the airbox.
  • Page 235 ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Engine drains Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Gripping pliers Cobra 1 pc. Nippers 1 pc. Cable tie 3,6x142 6 pcs.
  • Page 236 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 71–9 Airbox Condensate sump of L carburettor Engine mount Condensate sump of R carburettor Strut Cobra clamp Venting hose of L carburettor Left drain hose of airbox Venting hose of R carburettor Right drain hose of airbox Lockwire Left drain hose of condensate sump Carburettor L...
  • Page 237 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 79-2 Oil tank Venting hose Clamp 140-160 Clamp Rotax 853725 Hose to oil pump Clamp 14/7 Return hose from engine Firewall Fig. 79-2 Oil tank – removal / installation 79-10 Effectivity: All Page 79-7 Edition 2 | Rev.
  • Page 238 ERTC022-10-AS MAINTENANCE MANUAL DISTRIBUTION DESCRIPTION AND OPERATION This Section describes those parts of the oil system that are used for transporting the oil from and to the engine. These items include the oil cooler, thermostat and the oil filter. The oil cooler is located under the engine; the upper part of the cooler is attached by means of the brackets to the firewall, the lower part of the cooler is suspended on the engine mount by means of the strut.
  • Page 239 ERTC022-10-AS MAINTENANCE MANUAL MAINTENANCE PRACTICES Oil cooler Maintenance type: Line Personnel qualification: Independent verification personnel qualified in accordance with Part 66 or higher Recommended tools and material: Item Designation / Size Quantity Note Wrench No. 30 1 pc. Wrench No. 22 1 pc.
  • Page 240 ERTC022-10-AS MAINTENANCE MANUAL Valid for the smaller oil cooler P/N 886027: Unscrew and remove the screw fitting (3), reductions (4) and the sealing (5). Unscrew and remove the nuts (6) and remove the cooler (1) with the cover (2) and the washers (7). Close the cooler necks and the hoses with suitable blind plugs.
  • Page 241 ERTC022-10-AS MAINTENANCE MANUAL Fig. 79-3 Oil cooler – removal / installation (page 1 of 2) 79-20 Effectivity: All Page 79-11 Edition 2 | Rev. 1 2019-03-22...
  • Page 242 ERTC022-10-AS MAINTENANCE MANUAL Legend to Fig. 79-3 Oil cooler Lower strut Cooler cover Shock absorber Screw fitting Upper strut Reduction 14–18 Attachment 1x16 Sealing ring 14x18 Self-locking nut M6 Washer 6 Washer For information: Bolt M5x14 Engine mount Self-locking nut M5 Cooler holder Washer 5 Fig.
  • Page 243 ERTC022-10-AS MAINTENANCE MANUAL CHAPTER 91 CHARTS & WIRING DIAGRAMS TABLE OF CONTENTS Title Section Page General ........................91-00 ...... 91-3 Introduction............................. 91-3 Wiring diagrams ....................... 91-10 ...... 91-4 List of wiring diagrams ........................91-4 A. Standard equipment ........................ 91-7 B. Optional equipment ....................... 91-26 91-TOC Effectivity: All Page 91-1...
  • Page 244 ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 91-TOC Effectivity: All Page 91-2 Edition 2 | Rev. 0 2017-12-22...
  • Page 245 MAINTENANCE MANUAL GENERAL INTRODUCTION Chapter 91 contains wiring diagrams of the SportStar RTC airplane. The wiring diagrams covers interconnection of the components, instruments and electronic systems on the SportStar RTC airplane. The wiring diagram contain the name of part of the electricity system, identification number and wires parameters and other details required to install the system on the airplane.
  • Page 246 ERTC022-10-AS MAINTENANCE MANUAL WIRING DIAGRAMS This Section contains the list of wiring diagrams and own wiring diagrams of the SportStar RTC airplane. LIST OF WIRING DIAGRAMS Title Dwg. No. Sheets Standard equipment Hobbs hourmeter E7 19-10 01 Turn coordinator BZW 4B...
  • Page 247 ERTC022-10-AS MAINTENANCE MANUAL Title Dwg. No. Sheets Flight instruments (Winter) - ver. D E7 70-01 05 GTN750+GMA35+GTX33+SL40+A30+SV-ARINC429 E7 70-01 06 D10+D7+ADAHRS+ADAHRS+EMS+GPS E7 70-01 07 Becker AR6201+BXP6401+BE6400 E7 77-81 01 SL30+GI106A+PM3000+GTX328+A30 E7 89-30 01 GNC255A+GI106A+GTX328+A30 E7 89-50 01 GNC255A+GTX328+A30+DYNON CDI E7 89-70 01 GTR225A+GTX328+ACK30 E7 89-72 01 Instrument lighting with regulator...
  • Page 248 ERTC022-10-AS MAINTENANCE MANUAL Title Dwg. No. Sheets Strobe lights Whelen LED Orion 600 NVFR S7 91-01 99 Taxi light Whelen LED 71141 NVFR S7 91-10 99 Landing light Whelen LED 71141 NVFR S7 91-11 99 Cockpit light S7 99-51 01 Cockpit light NVFR S7 99-51 99 Cockpit light (Koger)
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