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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.
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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: •...
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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;...
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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...
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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.
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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...
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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...
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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...
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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...
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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,...
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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...
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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.
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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...
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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...
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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.
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.
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.
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.
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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...
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.
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;...
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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...
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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.
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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.
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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.
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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.
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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.
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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.
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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.
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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.
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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;...
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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.
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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 –...
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.
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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.
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.
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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.
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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.
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...
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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 –...
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.
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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.
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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.
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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.
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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 –...
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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.
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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 ........................
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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...
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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...
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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: –...
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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...
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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;...
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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...
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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...
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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.
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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.
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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...
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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.
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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...
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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.
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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...
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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...
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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.
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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.
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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).
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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.
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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...
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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...
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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.
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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).
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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.
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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...
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.
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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...
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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...
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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...
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.
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.
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)
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.
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:...
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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.
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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;...
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.
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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.
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.
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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.
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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).
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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 –...
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.
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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.
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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.
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.
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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...
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.
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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.
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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).
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).
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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...
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.
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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.
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.
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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.
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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.
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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...
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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.
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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.
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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.
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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...
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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.
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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.
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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.
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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.
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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).
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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;...
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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.
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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). •...
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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).
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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).
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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...
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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...
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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.
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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.
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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.
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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.
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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.
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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).
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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.
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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.
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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.
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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.
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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).
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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.
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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.
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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 ........................
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ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 33-00 Platnost: Všechny letouny Strana 33-2 Vydání 2 | Rev. 0 2017-12-22...
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.
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.
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).
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.
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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...
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.
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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 –...
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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;...
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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.
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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...
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.
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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...
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.
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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).
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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...
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...
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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).
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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.
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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...
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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.
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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.
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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.
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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.
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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).
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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: •...
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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.
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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 ......................
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ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 71-TOC Effectivity: All Page 71-2 Edition 2 | Rev. 0 2017-12-22...
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 .
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.
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.
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...
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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).
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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.
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.
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...
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.
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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...
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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.
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.
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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...
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.
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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);...
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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.
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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...
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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 –...
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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...
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.
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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.
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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...
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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.
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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.
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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.
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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.
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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...
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ERTC022-10-AS MAINTENANCE MANUAL Intentionally Left Blank 91-TOC Effectivity: All Page 91-2 Edition 2 | Rev. 0 2017-12-22...
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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.
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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...
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