MPE_TexanTopClass_ISR_580_R912_v04
Contents
1. 5400 p Yeu Adouey pexoeuo pue NO UH 1S4S 821109 2 p u lse pue pajsnipe 5190 Mojes 440448 pue yooudy sjueuinasur JUG1 4 SHUI UIUNMA SJU9LUNIISUI 9UI6U3 440 duund jeny ou199 3 pesoj9 HI uedo Hu si8onej Xue jen4 440 duuej GuIUJem 10 eJeuec 53 1 40 992 101 19S sdej4 Q S G Ul DIC U LD 95 JIO NO duund jeny 91149913 INdH 0092 emoJu Je4noN UL SulAn l einuiui JUSWAAOW pu 89814 SIOJU09 11611 euo esned 095 Og XEN eJnpoooud uelis 430 340439 dOdd 4V472 19 lqo 10 uossad Aue jo 1eo o 51 ease sajjadoid ay ainsuq INdH 007 1 INdH Uunuuiul 9949 2 S G JO OSI INdH 0006 NO SieuDeui uoee Aoy sjeuDeui uonlub LUNLUIUILU V emojJu L NO duuej GUuIUJem J0 0J9u85 ojeuDeui uoee 10 NdH 00 NO UOIIMS 1 SE N eseeJoep LUNWIXEW INdH 000 sojeuDeuu wo WNWIUIW JV enoJu L JUSLUSAOLU pue 89814 s 01 Uu09 JUGI 4 440 Udy 08s Q1 10 NO duund jeny ou199 3 Jenow ULL e 440 wem euiDu3 ove ul silul UIUUM nss d 9 duro IO penea je NO pjoo eui6ue BAB 820459 pesoj9 H1 uedo HH sieonej Xue jen4 NO exeJq Guiyed 14 15 3NION3 54 of 57 25 021 11 C Cosatto C Cosatto C Cosatto Identification POH TC 580 Rev 3 Revision Description Converted speeds from knots in mph Page Issued Verified A2. C LASS 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 1 1 INTRODUCTION This Operating Handbook contains the necessary information for a sure and efficient employment of the aircraft FLY SYNTHESIS TEXAN TOP CLASS ROTAX 912 ULS 100 HP The POH has been prepared to comply with the requirements of BCAR Section S CS VLA and where relevant the ASTM standard The Pilot Operating Handbook is valid only for the particular aircraft identified on page 2 the identification page Read this manual before your first flight 1 2 WARNINGS SUGGESTIONS AND NOTES The observance of this manual is compulsory for the aircraft s use FLY SYNTHESIS S r l declines every responsibility for any damage to person and property derived by a missed or partial observance of the prescriptions contained in this manual FLY SYNTHESIS S r l reserves it to terms of law the exclusive ownership of this manual and also forbids the partial or integral reproduction of it and however to communicate it to competing firms without a preventive written authorization 1 3 DESCRIPTIVE AIRCRAFT DATA TYPE OF AIRCRAFT Texan Top Class is a light sport aircraft with airframe wings and control surfaces made of laminate and honeycomb sandwich composite materials The rectangular shape low wing utilizes a laminar flow airfoil
3. The contact with the ground should happen at the minimum possible speed maintain lifted the nose wheel for the longest possible time 3 7 OPENING PARACHUTE PROCEDURE IF INSTALLED The emergency parachute is located in the left back part behind the canopy situated in a special carbon canister inside the fuselage The emergency parachute is fixed to the aircraft through four steel ropes passing in the internal part of the fuselage attached to antitorsion tube of the wing The emergency parachute must be used only in case of complete loss of the control of the aircraft 24 PARACADUTE APERTO 55 1 PARACADUTE CHIUSO TEXAN RG TEXAN RG ftroleggero biposto Ultralaggero biposto FLYSYNTHESIS amp FLYSYNTHESIS a Shutdown the engine magnetos OFF b Pull red handle between the two seats at least 20 centimeters C Close both fuel faucets d Tighten the safety belts e Shutdown the electric plant Master OFF f Do crouch and to protect the face with the hands For further information and notes on function and maintenance consult the parachute manual 3 8 OTHER EMERGENCY OIL TEMPERATURE amp PRESSURE IN YELLOW ARC OR REL LINE If the oil pressure is low yellow arc but the oil temperature is in normal operation range green arc Land ASAP as per normal procedure If the oil pressure indication is too low or too high red arc Land ASAP and get ready for a force
4. 33050 M liano UD Ital ified Tel 2000 x 145017 TO P C LAS S 580 IS R 7 B 7 Fax 39 0 432 931280 for Rotax 9 12 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 5 1 GENERAL INFORMATION This section contains all the performance data required for accurate pre flight planning SCHEME OF TAKE OFF 8 LANDING PHASES Figure 5 1 shovv the take off and landing phases and medium value recorded SPEED CONVERSION DENSITY ALTITUDE The density altitude chart figure 5 2 is provided to determine the density altitude for outside air temperature and pressure altitude combinations UNIT CONVERSION Figure 5 3 shows the linear scales for conversion of Km h KTS m s Figure 5 4 shows the linear scales for conversion of m s feet min and KTS m s Figure 5 5 shows the linear scales for conversion of m feetl DEMONSTRATED CROSS WIND COMPONENT The maximum demonstrated crosswind is 19 KTS Figure 5 6 shows the RELATIVE WIND DIAGRAM VERSUS WIND COMPONENT ENVELOPE DIAGRAM Figure 5 7 shows the envelope diagram Y FLYSYNTHESIS Identification POH TC 580 Rev 3 Gf FLYSYNTHESIS Pilot Operating Handbook Bad 39 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 7 oxu 0 x TOP CLASS 580 18RA e Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mai
5. 164 93 89 44 47 9 5 63 57 7 166 78 90 4633 25 1349 10748 E 29 168 9 48 18 109 33 92 50 03 56 172 34 93 5374 5 176 05 55 59 177 90 57 44 1672 11860 064 EE 179 76 59 30 2 120 45 65 5 181 61 61 15 122 31 66 b 183 46 Figure 5 3 Af FLYSYNTHESIS A FLYSYNTHESIS Pilot Operating Handbook EL Provincial Road n 78 Km 12 150 FLY SYNTHESIS TEXAN E 7 33050 Mortegliano UD Ital ified Tel 439 042 992482 139 0 432 993557 TOP CLASS 580 ISR 7 3 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info flysynthesis com versions Converted speeds from knots in mph metres per second m s feet per minute 100 ft min k mnes mer d 1 96 10 66 21 41 33 20 82 80 70 3 93 11 17 22 43 30 21 33 82 67 5 90 11 68 23 45 27 21 84 84 64 7 87 12 19 24 47 24 22 35 86 61 9 84 12 75 25 49 21 22 86 B8 58 11 81 13 20 26 51 18 23 36 90 53 13 78 13 71 27 53 15 23 87 92 52 15 74 14 22 28 5511 24 38 94 48 17 71 14 73 29 57 08 24 89 96 45 19 68 15 24 30 59 05 25 45 98 42 21 65 15 74 31 61 02 25 90 100 4 23 62 16 25 32 62 92 26 41 102 3 25 51 16 76 33 64 96 26 92 104 3 27 55 17 27 34 66 92 27 43 106 2 29 52 17 78 35 68 89 27 94 108 2 31 49 18 28 36 70 86 28 44 110 2 33 46 18 79 37 72 83 28 95 112 2 35 43 19 30 38 74 80 29 46 114 1 37 40 19 81 39 76 77 29 97 116 1 39 37 20 32 40 78 74 30 48 118 1 0
6. DURING FLIGHT EMERGENCY PROCEDURES ENGINE ROUGHNESS ENGINE SHUTDOWN Throttle Check position and friction Check engine instruments Check parameters Choke lever OFF All rearward Fuel tank faucet Select tank with maximum fuel Electric fuel pump ON Fuel pressure Verify within limits Warm air to carburetors ON Ignition magnets key Both Verify Master switch Verify ON Throttle Position warm engine starting Start Operate start procedure Check all the engine parameters and land as soon as possible for a full check WARNING If the engine doesn t start up choose a proper zone for an emergency landing ENGINE ON FIRE Fuel tank faucet Close Electric fuel pump Off Throttle All forward Vent system All closed Cabin heating system Off Master switch amp ignition magnetos key Off Best glide speed 68 mph Landing ASAP ONO Or dea N WARNING Do not attempt to re start the engine even if engine fire has ceased but prepare for an emergency landing Y FLYSYNTHESIS Identification POH TC 580 Rev 3 FLYSYNTHESIS Pilot Operating Handbook page 23 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ram 33050 Mortegliano UD Ital ifiad Tel 1005205 E 25057 TO P C LASS 580 IS H 7 e Fax 439 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in m
7. Description e mail info flysynthesis com ver sions Converted speeds from knots in mph INSTRUMENTS Standard instruments Airspeed indicator altimeter vertical speed indicator magnetic compass slip indicator flap angle indicator tvvo fuel level tank indicators vvith tvvo lovv fuel level amber vvarning lamps CHT EGT RPM oll temperature indicator oil pressure indicator fuel pressure indicator engine run time indicator 12 Volt aux socket OTHER STANDARD EQUIPMENT Main wheels and nose wheel fairings main legs and nose leg aerodynamic fairing depth adjustable seats four points safety belts electric flap system travel 0 459 manual trim regulation system fully upholstered cabin interior canopy lock system with key hooks for ground anchorage landing lights Y FLYSYNTHESIS Identification POH TC 580 Rev 3 f FLYSYNTHESIS Pilot Operating Handbook 22 dar Peca Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 2 yes 33050 Mortegliano Ital ifiad Tel 777 E yess TOP CLASS 580 ISR 7 e Fax 39 0 432 931280 for Rotax 912 ULS u u Revision Description Sito web www flysynthesis com e mail info flysynthesis com versions Converted speeds from knots in mph 1 4 AIRCRAFT THREE VIEWS ef FLYSYNTHESIS Y FLYSYNTHESIS Identification POH TC 580 Rev 3 Gf FLYSYNTHESIS Pilot Operating Handbook Page 13 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 2 ni orteglia
8. and pressing downward to lift the dumper Verify the absence of obstacles or people animals in the aircraft range Push or pull the aircraft and direct it using only the principal wheels Operate the parking brake An optional front wheel tow bar is available for aircraft movement 7 2 AIRCRAFT GROUND ANCHORAGE The aircraft ground anchorage system is available as an option Anchorage of the aircraft can be performed by first setting ON the park brake then secure the ropes to each eyelet located on the underside surface of each wing near the wing tip When tightening the rope to ground mooring DO NOT apply too much tension force a small amount of tension will suffice to secure the aircraft without risking the potential to stress surfaces inadvertently during heavy wind conditions CAUTION It is a good practice to secure the control stick from inadvertent movement by latching to the seatbelts when the aircraft is left unattended or in windy conditions Y FLYSYNTHESIS f FLYSYNTHESIS Pilot Operating Handbook e e a ees Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ram 33050 Mortegliano UD Ital ified Tel 2000 25057 TO P C LAS S 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 7 3 AIRCRAFT CLEANING The aircraft is supplied vvith a kit for complete cle
9. e mail info Oflysynthesis com ver sions Converted speeds from knots in mph SECTION 7 Aircraft Ground Handling and Servicing Title 7 1 Aircraft ground movement 7 2 Aircraft ground anchorage 7 3 Aircraft cleaning 7 4 Aircraft servicing 4 FLYSYNTHESIS Gf FLYSYNTHESIS Pilot Operating Handbook pero 16 S80 nen Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 33050 Mortegliano UD Ital ified Tel 2000 C LASS 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com 4 Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 7 1 AIRCRAFT GROUND MOVEMENT Aircraft ground movement vvith engine running is as follovvs Get on board Either lock or secure the canopy in taxi mode Start engine Verify the absence of obstacles or people animals in the aircraft vicinity Remove the parking brake Use throttle to regulate the advancement speed and use the rudder pedals for steering the aircraft VVhen the aircraft has reached the destination shut off the engine operate the parking brake and leave the aircraft VVARNING never leave the aircraft vvith engine running this can be fatal both for you and for other people animals in the aircraft vicinity Aircraft ground movement with engine off is as follows Remove the parking brake Take the aircraft for the tail beam
10. e mail info flysynthesis com ver sions Converted speeds from knots in mph 3 1 INTRODUCTION An emergency situation is extremely rare even so the pilot responsible for the aircraft should meticulously carry out daily pre flight controls checks A safe airvvorthy aircraft should be maintained according to the requirements of the accompanying maintenance manual This section contains the recommended procedures should an emergency arise t is strongly advised that Pilots become familiar vvith these procedures 3 2 GROUND EMERGENCY PROCEDEDURES ENGINE ON FIRE 1 Fuel tank faucet Close Electric fuel pump Off Cabin heating Off Throttle All forward Master switch OFF Ignition magnets key OFF Get out of the aircraft immediately If possible use an extinguisher to extinguish the fire WARNING Not remove the engine cowling until the complete extinction of the fire Don t use water to extinguish the fire 3 3 TAKE OFF EMERGENCY PROCEDURES TAKE OFF INTERRUPTION during take off run Throttle All rearward reduce to minimum RPM Brakes Brake and avoiding skidding the wheels Flap Retract Ignition magnets key OFF Master switch Off Fuel tank faucet Off ENGINE FAILURE DURING TAKE OFF after rotation below 50 mt 1 Fuel tank faucet Close 2 Electric fuel pump Off 3 Master switch amp ignition magnets key Off 4 Safety belts Tighten well 5 Maintain a linear line of flight without t
11. free Neutral ON Set for take off 15 RH Open LH Closed Within limits Check and regulated adjusted and fastened check 4 locks are engaged and locked Check canopy open lamp OFF OFF Y FLYSYNTHESIS 4 FLYSYNTHESIS Provincial Road n 78 Rm 12 150 33050 Mortegliano UD Italy Tel 39 0 432 992482 39 0 432 993557 Fax 39 0 432 931280 Sito web www flysynthesis com e mail info Oflysynthesis com TAKE OFF Aircraft Throttle lever At 40KTS Pilot Operating Handbook FLY SYNTHESIS TEXAN TOP CLASS 580 SR for Rotax 912 ULS versions Align vvith runvvay Full open smoothly Rotation Identification Page Date Issued Verified Approved POH TC 580 Rev 3 35 of 57 25 021 11 C Cosatto C Cosatto C Cosatto Revision Description Converted speeds from knots in mph Rotation Climb speed 46 mph Vx 55 mph WARNING for a take off from short runway with an obstacle of 15 m use flap with 20 At an altitude of 100 m 300 ft if a steep climb is necessary to clear obstacles Flaps Trim Speed Throttle Electric fuel pump m Up As necessary Vx or Vy As necessary Off CAUTION Don t maintain the flaps extended with speed higher than 68 mph Vfe CLIMB Engine RPM Engine instruments Trim CRUISE Throttle Engine RPM Engine instruments Rotax 912 ULS 5000 RPM 5500rpm for varia
12. li O lov GIs a S s o knots kts metres per second m s 2 3 4 5 6 308 3 amp an 6 7 Less 729 77 823 874 926 2 B 14 40 34 98 Figure 5 4 f FLYSYNTHESIS 4 FLYSYNTHESIS Pilot Operating Handbook 5 ie Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 2 B CMS 33050 Mortegli UD Ital ified Tel 439 0 432 090482 439 0432 993557 TO P C LAS S 580 IS H 7 e Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info flysynthesis com versions Converted speeds from knots in mph metres m to feet ft conversion table feet metres feet metres feet ft m ft m ft 3 280 10 36 34 l 20 42 219 81 6 562 10 66 35 114 8 20 72 223 09 9 843 10 97 36 118 1 21 03 226 37 13 12 11 27 37 121 3 21 33 229 65 16 40 11 58 38 124 6 21 64 232 94 19 68 11 88 39 127 9 21 91 236 22 22 96 22 25 239 50 26 24 12 49 4l 134 5 22 55 242 78 29 52 12 80 42 137 7 22 86 246 06 32 B0 13 10 43 141 1 23 16 249 34 36 08 13 41 44 144 3 23 46 252 62 39 37 13 71 45 147 6 23 77 255 90 42 65 14 02 46 150 9 24 07 259 18 45 93 14 32 47 154 1 24 38 262 46 49 21 14 63 48 157 4 24 68 265 74 52 49 14 93 49 160 7 24 99 269 02 55 77 15 24 50 164 1 25 29 272 31 59 05 15 54 5I 167 3 25 60 275 59 62 33 15 84 52 170 6 25 90 278 87 65 61 16 15 53 173 8 26 21 282 15 68 89 16 45 54 177 1 26 51 285 43 72 17 16 76
13. tank Make sure the ignition and both magnetos are off Turn propeller 5 6 times in the normal direction for flight Make sure that no air is inside the cooling system Close the coolant tank cap and if necessary add coolant to the expansion tank Y FLYSYNTHESIS Identification POH TC 580 Rev 3 f FLYSYNTHESIS Pilot Operating Handbook ez 52 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 2 ni ortegliano Ital ified 270 129 0432993557 TOP CLASS 580 15 7 e ere Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com A Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 4 FLYSYNTHESIS Gf FLYSYNTHESIS Pilot Operating Handbook E e 16 S80 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN D cn 33050 Mortegliano UD Ital ified 1 Tel 1005205 25057 TO P C LAS S 580 IS H 7 e 5 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com A Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph SECTION 8 Aircraft Check Lists Title 8 1 Aircraft on board check lists 8 2 Aircraft ground pre flight check list NOTE these pages can be cut out and laminated 4 FLYSYNTHESIS 330 exeJq ued 340 yesq Hued GL H ye 10 uonisog sdej4 4 0 duup uedo Adoue 5 pexoeuo SIUSLUNIJSUI UOREGIAECN pexoo
14. the support Brake lever amp parking brake remove parking brake lock and check lever functionality Insert parking brake Trim lever check correct functionality Safety belts check correct functionality Seats fixed correctly Canopy clean no signs of cracks correct functionality of locking system Windshield clean fixed correctly on fuselage Luggage secured Weight amp balance calculated Flight logbook record the airtime BEFORE STARTING ENGINE Pre flight check completed Seats adjusted Safety belts adjusted and fastened Canopy closed and locked Parking brake ON Flight controls free Fuel faucets RH open LH closed Trim Neutral ENGINE START Engine cold ON Choke lever all rearward Engine warm OFF Choke lever all forward Electric fuel pump ON for 10 sec then OFF Throttle At minimum 1 cm Master switch ON Generator warning lamp ON Ignition magnets key each magnetos ON WARNING Ensure that the propeller area is clear of any person or object CLEAR PROP Start procedure Max 20 sec of starting rest one minute before retrying Throttle 2500 RPM for R912 Oil pressure Green arc in 5 sec Generator warning lamp OFF Electric fuel pump OFF Y FLYSYNTHESIS 4 FLYSYNTHESIS Provincial Road n 78 Rm 12 150 33050 Mortegliano UD Italy Tel 39 0 432 992482 39 0 432 993557 Fax 39 0 432 931280 Sito web www flys
15. 2 ULS LOG OF EFFECTIVE PAGES versions Identification POH TC 580 Rev 3 Page 5 of 57 Date 25 021 11 Issued C Cosatto Verified C Cosatto Approved C Cosatto Revision Description Converted speeds from knots in mph Section Page Date Revision Section Date Revision 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 25 02 11 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 18 11 10 25 02 11 18 11 10 20 12 10 25 02 11 18 11 10 18 11 10 18 11 10 CO OO CO CO CO NI NI 0 Od 02 02 O O1 OT O1 OT O1 O OJOIOJOJOIOJOJOICGIOIDOIOJO 25 01 11 25 02 11 20 12 10 18 11 10 25 02 11 25 02 11 18 11 10 25 02 11 25 02 11 18 11 10 25 01 11 18 11 10 25 02 11 18 11 10 18 11 10 25 01 11 18 11 10 25 01 11 25 02 11 25 02 11 18 11 10 25 02 11 25 02 11 O1 O1OI 01 By BR BR BR BR BR BR BI BI UUU CO 001091091 GO NO JO PO JO JO IO PO HS Sf Af sf tf st 18 11 10 OII OIW DIP OI DJ OJ OI PO OD W 091 O 9 W O uolo volo OO OO OO O Jooo ooo Y FLYSYNTHESIS f FLYSYNTHESIS
16. 32 993557 Fax 39 0 432 931280 Sito web www flysynthesis com e mail info flysynthesis com 25 021 11 C Cosatto C Cosatto C Cosatto Revision Description Converted speeds from knots in mph 2 4 POWERPLANT AND PROPELLER LIMITATIONS Refer always to Rotax operator manual Engine manufacturer Rotax 912 ULS 73 5 kW 69 kW 5800 rpm 5500 rpm 135 C 130 C 0 8 bar 7 bar 0 15 bar 0 4 bar minimum 95 RON See engine manual specifications Engine model Maximum take off power Maximum continuous power Maximum take off RPM Maximum continuous RPM Minimum cylinder head temperature Maximum oil temperature Minimum oil pressure Maximum oil pressure Minimum fuel pressure Maximum fuel pressure Usable type of fuel Usable type of oil Propeller manufacturer DUC H lices GT Propellers Propeller model Carbon 3 blades Wood 2 blades Ground variable pitch Fixed pitch 1750 mm 1730 mm Alisport Idrovario Composite 2 blade Auto Variable pitch Maximum diameter 1760 mm manual operations have been removed 2 5 POWERPLANT INSTRUMENTS MARKING Rotax 912 ULS engine version Instrument Min Red line limit Min Yellow arc Caution Green arc normal operations Max Yellow arc Caution Max Red line Limit RPM indicator nd nd 1 400 5 500 rpm 5 500 5 800 rom 5 800 rpm Fuel pressure gauge 0 15 bar nd 0 15 0 4 bar nd 0 4 bar Oil pressare ga
17. 55 180 4 26 B2 288 71 75 45 17 06 56 183 7 27 12 291 99 18 74 17 37 57 187 0 27 43 295 27 82 02 17 67 58 190 2 27 73 298 55 85 30 17 98 59 193 5 28 04 301 83 88 58 18 28 60 196 8 28 34 305 11 91 86 18 59 6l 200 1 28 65 308 39 95 14 18 89 62 203 4 28 90 311 68 98 42 19 20 63 206 6 29 26 314 96 101 7 19 50 64 209 9 29 56 318 24 104 9 19 81 65 213 2 29 87 321 52 108 2 20 12 66 216 5 30 17 324 80 oo O M jv N cle m Figure 5 5 1 FLYSYNTHESIS q FLYSYNTHESIS Pilot Operating Handbook S en m Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 33050 Mortegliano UD Ital ified C Cosatt Tel 0402971 x 145017 TO P C LAS S 580 IS R 7 C Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com A Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph CROSS WIND TABLE A T j H ini i EU iij Jd i MM Hil sarig H R SA H 2 x LE z 2 o a o a z RCR I SIN TAILWIND CROSSWIND COMPONENT KNOTS Figure 5 6 Y FLYSYNTHESIS A FLYSYNTHESIS Pilot Operating Handbook E e TC locuci Road n 78 Rm 12 150 FLY SYNTH ES IS TEXAN 7 62 ssued 33050 Mortegli UD Ital Verified C C Tel 439 0432 992482 139 0 432 993557 TO P C LAS S 580 IS R 7 C oats Fax 439 0 432 931280 for Rotax 912 ULS Sito web www flysynthes
18. 7 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ram ay nn 33050 Mortegliano UD Ital inan Tel 1000205 E 25057 TO P C LASS 580 IS H 7 e ere Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com 4 Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph NOTE This manual may be revised in the future and pages or sections re issued in part or vvhole Revisions will also be available on the Fly Synthesis website www flysynthesis com Any revisions and or sections should be printed and replaced in the manual at the earliest possible time for flight safety The revisions added to the manual should be logged and recorded in the table under log of ammendments of this manual by the owner user DEFINITIONS Definitions used in this handbook such as WARNING CAUTION and NOTE are employed in the following context WARNING Procedures or instructions that if not followed correctly may result in injury or death CAUTION Procedures or instructions that if not followed correctly may result in damage to the aircraft or its parts NOTE Procedures or instructions that affect safety of flight are highlighted INTELLECTUAL PROPERTY The data and information contained in this document is the property of FLYSYNTHESIS SRL This document may not be reproduced or transmitted to a third party in any form or by any means Any unauthorised copy or distribution is il
19. 90 2134 1 132 34 03 0 810 1 110 2438 0 850 30 47 0 785 1 128 2743 2 831 26 90 0 761 1 145 3090 4 812 23 33 0 738 1 163 3353 6 793 19 77 0 715 1 182 3658 8 774 16 20 0 693 1 201 3916 10 75 12 64 0 671 1 220 4267 12 73 9 074 0 649 1 240 4572 14 71 5 507 0 564 0 629 1 260 4877 16 69 1 941 0 541 0 608 1 281 5182 18 68 1 625 0 520 0 589 1 302 un 0 964 0 929 0 896 0 863 0 832 0 801 0 771 0 742 0 714 0 687 0 635 0 587 Figure 5 2 1 FLYSYNTHESIS Identification POH TC 580 Rev 3 Gf FLYSYNTHESIS Pilot Operating Handbook page 5 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Tel 39 0 432992482 390432993557 CLASS 580 SR yerse Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info Eflysynthesis com ver sions Converted speeds from knots in mph UNIT CONVERSIONS kilometers per hour km h knots kts metres per sec m s km h kts km h kts m s km h kts 1 853 63 00 18 34 124 16 67 3706 g 5 560 i 127 87 69 7413 i 129 72 70 9 266 131 57 71 EME i 133 43 72 12 97 i j 135 28 73 14 82 137 13 74 16 67 198 99 75 18 53 140 84 76 20 38 i 44 142 69 77 22 23 i 45 i 144 55 78 24 09 146 40 79 25 94 148 25 80 27 79 j 150 10 51 29 65 i i 151 96 82 31 50 1 153 81 83 33 35 155 66 B4 35 21 157 52 85 37 06 159 37 B6 38 91 j 161 22 87 40 77 55 163 08 88 42 62 56
20. FLY SYNTHESIS TEXAN TOP CLASS PILOT OPERATING HANDBOOR For Rotax 912 ULS versions 25 02 11 1 Converted speed in mph C Cosatto C Cosatto C Cosatto 25 01 11 1 Added checks propeller C Cosatto C Cosatto C Cosatto 20 12 10 Propeller auto pitch contr C Cosatto C Cosatto C Cosatto 00 18 11 10 C Cosatto C Cosatto C Cosatto Num Date Description x REVISION Verified Approved FlySynthesis s r l reserves in terms of law the exclusive ownership of this manual and also forbids the whole or partial reproduction of it THIS DOCUMENT MUST BE CARRIED IN THE AIRCRAFT AT ALL TIMES Identification POH TC 580 Rev 3 4 FLYSYNTHESIS Pilot Operating Handbook page 7 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 5 2 3 ortegliano UD Ital fiad Tel 129 002992482 139 0 432 993557 TOP CLASS 580 ISR 7 5 Fax 439 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph IDENTIFICATION Manufacturer FLY SYNTHESIS SRL Provincial Rd 78 Km 12 150 Mortegliano 33050 UD ITALY Model FLY SYNTHESIS TEXAN Version TEXAN 580 ISR Airframe Serial No Engine Model Address Engine Serial No Registration Date Signature Y FLYSYNTHESIS Identification POH TC 580 Rev 3 FLYSYNTHESIS Pilot Operating Handbook page 3 of 5
21. Pilot Operating Handbook E ev ar s Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Bol 33050 Mortegliano UD Ital ified Tel 2000 x 145017 TO P C LAS S 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com A Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph Title Section IDENTIFICATION DEFINITIONS LOG OF REVISIONS LOG OF EFFECTIVES PAGES INDEX General informations Limitations Emergency procedures Normal operations Performances VVeight and balance Aircraft ground handling and servicing Aircraft check lists Co NN O O B Co 4 FLYSYNTHESIS Identification POH TC 580 Rev 3 Gf FLYSYNTHESIS Pilot Operating Handbook Bad 7 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN ortegliano Ital ified Tel 139 0432992482 05 CLASS 580 ISR ees C Cosatto Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com A Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph SECTION 1 General information Introduction Warnings suggestions and notes Descriptive aircraft data Aircraft three views 4 FLYSYNTHESIS Gf FLYSYNTHESIS Pilot Operating Handbook 5 ev 16 Rev ions Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 33050 Mortegliano UD Ital ified Tel 2000
22. Rev 3 Gf FLYSYNTHESIS Pilot Operating Handbook Page 48 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 5 xu 0 x TOP CLASS 580 18RA e Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info flysynthesis com versions Converted speeds from knots in mph Where ML P2DX P2SX x X2 P1 x X1 Xt Xt MAC x 100 CG position in percentage to the wing chord ML Empty weight moment P2DX P2SX Weight measured on main wheel P1 Weight measured on nose wheel NOTE DX RHS SX LHS For greater W amp B detail refer to the maintenance manual 6 3 WEIGHT amp BALANCE REPORT The first recording of the Weighing Report amp the Center of Gravity Position of the aircraft is taken at the factory before the delivery of the same aircraft Every variation due to the installation of new components or repairs and painting implicate a new calculation of the empty weight and the relative positioning of the center of gravity Any weight and Balance changes should be recorded into the aircraft log book Y FLYSYNTHESIS Identification POH TC 580 Rev 3 Gf FLYSYNTHESIS Pilot Operating Handbook Bad 49 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 7 33050 Mortegliano UD Ital ified Tel 777 4390432993557 TOP CLASS 580 ISR 7 e Cake Fax 39 0 432 931280 for Rotax 912 ULS Revision Description Sito web www flysynthesis com
23. S 3NION3 Sum s Jejeuiniv ONIGN32S34 LUC QQSS ydw zy 062 peeds uudi 0008 ydw 211 061 peeds uidi 0087 ydw 211 u ux 081 p ds uld 0007 ydw 06 peeds AHPO DUI AJUO ase spaeds 211 S9X Jq WIEM UM Ssyui p x jou op sjuauinujsui y28u2 Aljeuonouny y99y9 seyelg syw UIUIM SIUSLUNIJSUI 9UI6U3 440 duund jeny 91498J3 Wd 0065 snonunuo xe INdH euiBu3 dN sde 4 1895909 sy enoJu p DINOU L asinuo ONIGNV1 H414V Alesse59U sy ULL eunpeoouJd aye 1eede punoJ y uonoi nof J SHUI UIUUM SIUSLUNIJSUI euiBu3 AN XA peeds 0006 INdH eui amp u3 oSl de gn AJeSsS899U sy duund jeny ou199 3 J MOd XEN V AJeSS809U sy emouu L OD HONOL AN JO XA p ds 4 ess o u Sy ULL ydw 9p u u GZ peeds umop yono dn sdel4 ydw GG uui 06 p ds uoeo ddy jeul4 gg XA p ds qul 09 yo uo eyeiq ued ydu 9r NO dundjenjoupep 202 lum dej esn JO ajqejsqo ue uum Aemuny LIOYS UIOJJ HO aye P 104 Aressaoeu sy epoJu L uonelon S190 1v 55 0 sy Wu 1801 youd ejgqeisn pe ji uiu 00 00 INdH Aess u sy dej4 Ajujoouus uedo in ydw G9 u uy GOL p ds UUM UBIV yeJoJly ONIGNV1 d40 ANVIL Identific
24. TO REACH MAXIMUM RPMs DURING TAKE OFF during take off run If it is not possible to reach maximum rpms during take off run ABORT the take off HYDRAULIC PITCH CONTROL SYSTEM FAILURE In case of loss of hydraulic oil pressure of the control system the system is designed to reduce the pitch to the minimum value This means that the propeller will be set in take off and climb position If this failure occurs land ASAP WARNING During the remaining part of flight reduce the power to avoid overpassing the maximum value of engine rpms For further details see the propeller manual For further details on possible failures of the CIP control system and propeller pitch control system see the respective manuals Y FLYSYNTHESIS Gf FLYSYNTHESIS Pilot Operating Handbook E ev Te ee Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 7 33050 Mortegliano UD Ital ifiad Tel io oss 25057 TO P C LAS S 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com A Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph SECTION 4 Normal procedures Title 4 1 Introduction 4 2 Speed for normal employment 4 3 Fuel circuit draining procedure and refueling operations 4 4 Pre flight Inspection 4 5 Flight inside heavy rain 4 FLYSYNTHESIS POH TC 580 Rev 3 f FLYSYNTHESIS Pilot Operating Handbook 2 ie P
25. acks fixed correctly Engine VIII Upper cowling remove Oil tank check level Coolant tank check level Radiator and air inlet no signs of cracks free from obstructions Engine clean no oil or coolant leakage Muffler amp silencer manifold no signs of cracks muffler hooked Oil and refrigerant tube system correct functionality no leakage Ignition amp electric plant correct functionality Throttle amp choke cables free movement governor oil pipe air bubbles present inside oil if installed Upper cowling reinstall and check tightness Check inside cabin IX Instruments panel fixed correctly all placards Master switch ON all instruments ON Master switch OFF all instruments OFF Control stick free movement fixed correctly in its support Rudder pedals no distortion no signs of cracks correct functionality fixed correctly in its support correct functionality of centering system Throttle amp choke levers free movement fixed correctly in there support Brake lever and parking brake remove parking brake lock check lever functionality Insert parking brake Trim lever check correct functionality Safety belts check correct functionality Seats fixed correctly Canopy clean no signs of cracks correct functionality of locking system Windshield clean fixed correctly on fuselage Luggage secured Weight amp balance calculated Y FLYSYNTHESIS
26. amination Karman absence of delamination fixed correctly Leading edge absence of delamination Wing tip no defects fixed correctly Trailing edge absence of delamination no signs of cracks Flap amp aileron absence of delamination no signs of cracks free movement no excessive play on hinges fixed correctly balancing mass fixed correctly no signs of lateral movement Fuselage left side III Fuselage surface absence of buckling absence of delamination inspection holes closed Empennage IV Vertical fin absence of buckling absence of delamination Rudder absence of delamination hinges fixed correctly CAUTION Lower the tail of the aircraft to lift the nose wheel check the free movement of the rudder any problem on the hinge Bowden cables fixed correctly Stabilator free movement during all travel range absence of buckling absence of delamination Stabilator hinge absence of delamination fixed correctly no play Balancing mass fixed no play Hinge pins fixed correctly Trim tab free movement absence of defects and no play 4 FLYSYNTHESIS Provincial Road n 78 Km 12 150 1 F LYSYNTHESIS 33050 Mortegliano UD Italy Tel 39 0 432 992482 39 0 432 993557 Fax 39 0 432 931280 Sito web www flysynthesis com e mail info flysynthesis com Fuselage right side V Pilot Operating Handbook page FLY SYNTHESIS TEXAN i TOP CLASS 580 ISR Identification POH TC 580 R
27. amination fixed correctly Leading edge absence of delamination Wing tip no defects fixed correctly Trailing edge absence of delamination no signs of cracks Y FLYSYNTHESIS f FLYSYNTHESIS Pilot Operating Handbook e e a ees Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 33050 Mortegliano UD Ital ified Tel 2000 C LASS 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com 4 Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph Flap amp aileron absence of delamination no signs of cracks free movement no excessive play on hinges fixed correctly balancing mass fixed correctly no signs of lateral movement Pitot tube no defects fixed correctly Right main landing gear VII Leg no distortion bolts locked no sign of cracks on the welding Brake assembly condition and tightness Tire general good condition inflated correctly Wheel fairing good conditions and free space between the wheel and fairing Nose wheel VIII Fixing axle bolts check correct tightness Wheel fairing good conditions and free space between the wheel and fairing Tire general good condition inflated correctly Damper no signs of cracks or distortion free movement Nose wheel support structure no signs of cracks or distortion Propeller VIII Hub amp blades no signs of cracks amp clean Spinner no signs of cr
28. aning The follovving procedure is suggested for cleaning the aircraft Do not use a pressure cleaner directiy on the aircraft as the gel coat is hygroscopic Use a micro fiber cloth and neutral soap to clean the aircraft Avoid vvater bathing of metallic parts Rinse vvith a damp and clean micro fiber cloth Dry excess moisture using a deerskin natural or synthetic chamois The cockpit can be cleaned vvith a dry micro fiber cloth and a vacuum cleaner CAUTION to avoid corrosion problems make sure that the metallic parts are not left damp The use of a water dispersant spray and or approved lubricant is advised T A AIRCRAFT SERVICING Servicing fuel Make sure the plane is set on the parking brake Open the fuel cap Pour in fuel as per specification Check that the amount poured equates to the reading from the dipstick Close the cap and make sure the fuel cap vent is directed to the front Make sure no spilled fuel is left on the plane Remove if necessary Servicing Oil Remove top cowling Make sure the ignition and both magnetos are off Turn propeller 5 6 times in the normal direction for flight Open the oil tank cap and check the level of the oil by the dipstick Oil should read within marked limits Add oil if necessary Close the cap Servicing Coolant Rotax engine Remove the top cowling Open the cap of the coolant tank and add coolant to fill up the
29. ated in the right lower part of the firewall Use a transparent and clean container drain about 80 100 cc of fuel Verify the absence of water CAUTION Perform the fuel circuit draining operation before moving the airplane from the parking area to avoid any mixing of condensate water if present on the fuel tanks If water is present repeat the fuel circuit draining operation until no water is evident Refuel through the fuel filler located on the upper layer of the wings either by jerry cans or directly with the gasoline pump CAUTION As the Texan employs an overflow fuel system that returns excess fuel to the Right hand side tank it is recommended to always use the right side fuel tank When the right tank is near empty use the left tank To avoid the right tank being overfilled with excess fuel frequently alternate the use of both fuel tanks during the cruise The drawing of fuel simultaneously from both tanks is not recommended Y FLYSYNTHESIS Gf FLYSYNTHESIS Pilot Operating Handbook e 16 S80 ee Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 57 33050 Mortegliano UD Ital iting Tel 757 25057 TO P C LAS S 580 IS H 7 e ere Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info flysynthesis com versions Converted speeds from knots in mph 4 4 PRE FLIGHT INSPECTION WARNING Before every flight the pilot m
30. ation Page Date Issued Verified Approved Revision Description Converted speeds from knots in mph for Rotax 912 ULS versions 4 FLYSYNTHESIS TOP CLASS 580 ISR x o o o av D o O o FLY SYNTHESIS TEXAN 4 FLYSYNTHESIS Provincial Road n 78 Rm 12 150 33050 Mortegliano UD Italy Tel 39 0 432 992482 39 0 432 993557 Fax 39 0 432 931280 Sito web www flysynthesis com e mail info Eflysynthesis com r 5ed 1s l YOOYD STN 216 xeiou ssejo d l uexeL eBed ISI 49949 STN 216 Xe1oH ssejo d l EX L Identification POH TC 580 Rev 3 4 FLYSYNTHESIS Pilot Operating Handbook page 207 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 5 25 33050 Mortegliano UD Ital ifia Tel 3909442 997487 139 0 432 993557 TOP CLASS 580 ISR 7 7 Fax 439 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info flysynthesis com versions Converted speeds from knots in mph 8 2 AIRCRAFT ON GROUND CHECK LIST EN TEXAN TOP CLASS PRE FLIGHT CHECK LIST Page 1 Remove all the protections pitot cover wheels stops mobile surfaces stops canopy covering propeller protection fuel draining procedure Left main landing gear I Leg no distortion bolts locked no sign of cracks on the welding Brake assembly condition and tightness Tire general goo
31. ble pitch propeller installed Within limits As necessary Rotax 912 ULS As necessary Max cont power 5500 RPM Within limits CAUTION Check frequently engine instruments and do not exceed limits DESCENT Altimeter Warm air to carburetor system Throttle Trim Engine instruments LANDING Speed Flap Trim Throttle Electric fuel pump Setting As necessary As necessary As necessary Within limits 66 mph As necessary As necessary As necessary ON Y FLYSYNTHESIS Identification POH TC 580 Rev 3 4 FLYSYNTHESIS Pilot Operating Handbook page 2 7 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 5 5 33050 Mortegliano UD Ital ifad Tel 3909442 997487 139 0 432 993557 TOP CLASS 580 ISR 7 7 Fax 439 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph Parking brake check see note b Check should be off Final Approach speed 55 mph Touch down speed 46 mph CAUTION a in conditions of strong cross wind or in presence of wind shear increase the landing speed by at least 5 mph b Before landing check brake system pressure by operating the brake lever a couple of times if the braking system is serviceable you should feel the resistance when pressure is applied TOUCH amp GO Throttle All forward Tr
32. can provoke serious problems of stability and govern ability of the aircraft 6 2 WEIGHING CONDITIONS For the weighing of the aircraft the followings conditions apply The equipment installed must be approved by the factory for the aircraft in question Must be included the brake fluid engine oil water coolant and the non usable fuel Must use three independent scales for each tire horizontal plan and of a thread to lead To determinate the empty weight and the position of the Center of Gravity the aircraft must be positioned on three autonomous scales one for each wheel It is fundamental that the longitudinal and lateral axes of the aircraft are both in the same horizontal plane You can verify the horizontal datum position when the fuselage side reaches 5 with reference to ground level as shown in the figure below Using a plum bob mark a line on the ground directly beneath the leading edge of the wing This point is your reference datum RD Measurements are to be taken from this point X1 is the distance from nose wheel axle centerline to projection of RD X2 is the distance from main wheel axle centerline to projection of RD The standard distance is X1 925mm 0 5 X2 655mm 40 599 The formula for CG calculation is as follows Xt ML PT CofG position in mm on the wing chord Y FLYSYNTHESIS Identification POH TC 580
33. d condition inflated correctly Wheel fairing good conditions and free space between the wheel and fairing Left wing 1 Wing surface absence of buckling absence of delamination Karman wing root absence of delamination fixed correctly Leading edge absence of delamination Wing tip no defects fixed correctly Trailing edge absence of delamination no signs of cracks Flap amp aileron absence of delamination no signs of cracks free movement no excessive play on hinges fixed correctly balancing mass fixed correctly no signs of lateral movement Fuselage left side III Fuselage surface absence of buckling absence of delamination inspection holes closed Empennage IV Vertical fin absence of buckling absence of delamination Rudder absence of delamination hinges fixed correctly Lower the tail of the aircraft to lift the nose wheel check the free movement of the rudder check for possible hinge problem Bowden cables fixed correctly Stabilator free movement during all travel range absence of buckling absence of delamination Stabilator hinge absence of delamination fixed correctly no play Balancing mass fixed no play Hinge pins fixed correctly Trim tab free movement absence of defects and no play Fuselage right side V Fuselage surface absence of buckling absence of delamination inspection holes closed Right wing VI Wing surface absence of buckling absence of delamination Karman wing root absence of del
34. d landing see relative paragraph 4 FLYSYNTHESIS Gf FLYSYNTHESIS Pilot Operating Handbook pero 16 Seo ee Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 33050 Mortegliano UD Ital ified Tel 2000 C LASS 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph LOVV FUEL PRESSURE 1 Electric fuel pump On 2 Fuel tank faucets Open alternately the faucets to check the fuel circuit 3 Fuel pressure Check vvithin limits 4 If the fuel pressure does not reach the normal operating range land ASAP UNINTENTIONAL FLIGHT WITHIN ICING CONDITIONS WARNING Flight in known icing conditions snow and heavy rain is prohibited If you meet unintentional icing condition during the flight descend as soon as possible to a lower height If the wing leading edge and the stabilator leading edge are covered by ice formations remember that stall speed will increase you will need more engine power to maintain the same velocity and the maneuverability of the airplane will decrease Carburetor heating system if installed On Engine RPM Maintain the maximum continuous engine power Cabin heating if installed On Move all control surfaces to break potential icing formations ICING FORMATIONS ON CARBURETTORS You can recognize icing formati
35. ere is enough free space from obstacles for a safe landing b Land as normal but maintain a landing speed not less than 55 mph LANDING VVITH A DEFLATED TIRE 1 Landing as per normal condition 2 Before contacting the ground shutdown the engine and turn off electrical equipment 3 When landing hold off contact with the ground on the side of the deflated tire for as long as possible 4 Get ready for a tendency to yaw on the side of the deflate tire b Maintain the directionality vvith rudder and nose vvheel steering 6 If nose wheel is deflated maintain backpressure on control stick and keep the nose wheel in a central position FORCED LANDING 1 Best glide speed 68 mph Safety belts Tighten well Throttle All rearward minimum position Fuel tank faucet Closed Electric fuel pump Off Master switch amp ignition magnetos key Off CAUTION Choose a suitable area for an emergency landing 7 Flap As necessary 8 Trim As necessary Y FLYSYNTHESIS 4 FLYSYNTHESIS Pilot Operating Handbook 5777 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ram 257 33050 Mortegliano UD Ital ified Tel 757 25057 TO P C LASS 580 IS R 7 x 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 9 Final Check velocity 10 Landing Check velocity at least 44 mph flap with 45
36. ev 3 32 of 57 25 021 11 C Cosatto C Cosatto C Cosatto Verified Approved for Rotax 912 ULS Revision Description versions Converted speeds from knots in mph Fuselage surface absence of buckling absence of delamination inspection holes closed Right vving VI VVing surface Rerman Leading edge VVing tip Trailing edge Flap amp aileron absence of buckling absence of delamination absence of delamination fixed correctly absence of delamination no defects fixed correctly absence of delamination no signs of cracks absence of delamination no signs of cracks free movement no excessive play on hinges fixed correctly balancing mass fixed correctly no signs of lateral movement Pitot tube Right main landing gear VII no defects no blockage and fixed correctly Leg no distortion bolts locked no sign of cracks on weldings Brake assembly condition and tightness Tire general good condition inflated correctly Wheel fairing bracket Nose wheel VIII Fixing axle bolts Wheel fairing Tire Damper Nose wheel support structure Propeller VIII Hub amp blades Spinner Engine VIII Upper cowling Oil tank Coolant tank Radiator and air inlet Engine Muffler amp silencer manifold Oil and coolant tube system Ignition amp electrical wiring Throttle amp choke cables Prop system oil tube Upper cowling good condition and free space between the wheel and mounti
37. exceed this speed in Cruising Speed 124 mph turbulent air condition 145 km h Do not use full stick and full rudder 78 KTS deflections above this speed Maximum speed with full 120 km h Do not exceed this speed with flap flaps 75 mph extended Do not descend this speed without j 7 flap to avoid undesired stall mph Vis conditions Do not descend this speed with flap in take off position to avoid undesired stall conditions Do not descend this speed with flap in landing position to avoid undesired stall conditions Never Exceed speed Maneuvering speed Stall speed without flap Stall speed in take off 70 km h position 15 44 mph Stall speed in landing 65 km h position full flap 45 40 mph 2 3 AIRSPEED MARKING Marking Speed range IAS Definition White VsO Vfe 40 75 KTS Speed range where flap may be extended Green arc Vs Vmol 40 121 KTS Speed range of normal operation Yellow arc Vmo Vne 124 155 KTS Maneuver the aircraft with great caution Red line Vne 155 KTS Maximum speed allowed Y FLYSYNTHESIS Identification Page Date Issued Verified Approved POH TC 580 Rev 3 15 of 57 Pilot Operating Handbook FLY SYNTHESIS TEXAN TOP CLASS 580 SR for Rotax 912 ULS versions 4 FLYSYNTHESIS Provincial Road n 78 Km 12 150 33050 Mortegliano UD Italy Tel 39 0 432 992482 39 0 4
38. flies WARNING Flight in known icing conditions snow and heavy rain is prohibited The pilot is responsible for determining the airworthiness of the aircraft before each flight including on board fuel level verification All maneuvers at load factor less than 0 5 g must be performed for no longer than 5 seconds In single pilot operation belt and shoulder harness of the vacant seat must be secured to avoid uncontrolled movement of seat back and belt 2 9 LOAD FACTOR LIMITATIONS The load factors limit used for the calculation of the structures are conforming to CS VLA rules Flap retracted Flap extended Maximum positive load factor 3 8 Maximum positive load factor 2 0 Maximum negative load factor 1 9 Maximum negative load factor 0 0 2 10 OPENING CANOPY LIMITATIONS During flight engine operation and taxi operation the canopy must remain closed and securely locked via the 4 point hook locking system The only exception is if the optional taxi open system safety locking mechanism has been fitted in this case it is possible to slightly maintain the canopy open only during taxi and ground operations WARNING during the flight is absolutely forbidden to hold the canopy in any position other than in the securely locked mode Never try to open the canopy during the flight Y FLYSYNTHESIS Identification POH TC 580 Rev 3 f FLYSYNTHESIS Pilot Operating Handbook page d ES Provi
39. im As necessary Flap 15 Speed Vx o Vy If you touch the ground repeat take off procedure AFTER LANDING Throttle Idle Flaps UP Electric fuel pump OFF Brakes Check functionality vvith vvarm brakes ENGINE SHUTDOVVN Throttle dle Parking brakes ON Electrical consumers OFF Magnetos OFF one by one check RPM drop Master svvitch OFF Fuel tank faucets closed 4 5 FLIGHT INSIDE OF HEAVY RAIN VVARNING Flying inside heavy rain is prohibited Flying inside heavy rain is forbidden as visibility and performance of the flight is reduced hovvever if unavoidable reduce speed to 92 mph and remember to increase the landing speed by at least 5 mph vvith vvet vving The activity of flight inside intense heavy rain is forbidden Y FLYSYNTHESIS Identification POH TC 580 Rev 3 Gf FLYSYNTHESIS Pilot Operating Handbook page 37 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN ortegliano UD Ital ified 1009095 25057 TO P C LAS S 580 IS H 7 e ere Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com A Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph SECTION 5 Performances Title 5 1 General information Y FLYSYNTHESIS Identification POH TC 580 Rev 3 4 FLYSYNTHESIS Pilot Operating Handbook Page 38 of 57 Proc Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 5 5 ssued
40. is com A Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph ENVELOPE DIAGRAM Stall Speed with flap 45 Stall Speed without flap Maximum speed with extended flap Maneuvering speed Max cruise speed in turbulent air Never exceed speed Y FLYSYNTHESIS Identification POH TC 580 Rev 3 Gf FLYSYNTHESIS Pilot Operating Handbook page 7 Provincial Road n 78 Km 12 150 FLY SYNTHESIS TEXAN RE e 7 33050 Mortegliano UD Ital iting 1 Tel 777 4390432993557 TOP CLASS 580 ISR 7 e ere Fax 39 0 432 931280 for Rotax 9 12 ULS Revision Description Sito web www flysynthesis com e mail info flysynthesis com versions Converted speeds from knots in mph SECTION 6 VVeight 8 balance Title 6 1 Introduction 6 2 VVeighing conditions 6 3 Weight amp balance report 4 FLYSYNTHESIS 4 FLYSYNTHESIS Pilot Operating Handbook 5777 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ram 5 7 33050 Mortegliano UD Ital ified Tel 757 25057 TO P C LASS 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info Eflysynthesis com versions Converted speeds from knots in mph 6 1 INTRODUCTION This section contains the information to affect a correct procedure of vveight and balance of the aircraft VVARNING exceeding the Centre of Gravity limits
41. l info flysynthesis com versions Converted speeds from knots in mph hz 15 mt IO SUPERATE AN OBSTACLE OF 15 mt T IAKE OFF RUN TAKE OFF DISTANCE DISTANCE TO OBSTACLE OF 15 mt LANDING RUN Figure 5 1 Take off run Take off distance Take off speed 125 m 360m 53 mph Landing distance Landing run Landing speed 275m 95 m 55 mph 4 FLYSYNTHESIS 4 FLYSYNTHESIS Pilot Operating Handbook pe IAS Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN C LAS S 580 IS R 7 e 5 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info E flysynthesis com versi ons Converted speeds from knots in mph SPEED CONVERSION DENSITY ALTITUDE This table helps you to calculate the TAS true airspeed from the IAS indicated airspeed using the simplified formula TAS IAS Cor factor ICAN international commitee for air navigation temperatures relative pressure relative density and IAS to TAS correction factors as related to altitude Altitude Temperature Relative Relative Cor factors feet metres eC F pressure density 2 000 610 18 96 66 13 1 074 1 059 0 971 305 16 98 62 56 1 036 1 029 0 985 0 15 305 13 01 55 43 0 971 1 014 610 11 03 51 86 0 942 1 029 914 9 056 48 30 0 915 1 045 1219 7 075 44 73 0 888 1 061 1524 5 094 41 16 0 861 1 077 1829 3 113 37 60 0 835 1 0
42. legal as per international agreements relating to property rights THIS AIRCRAFT WAS MANUFACTURED IN ACCORDANCE WITH THE FOLLOWING LIGHT SPORT AIRCRAFT AIRWORTHINESS STANDARDS BCAR Section S CS VLA F2279 F2295 AND F2483 AND DOES NOT CONFORM TO STANDARD CATEGORY AIRWORTHNESS REQUIREMENTS Y FLYSYNTHESIS Identification POH TC 580 Rev 3 FLYSYNTHESIS Pilot Operating Handbook page 4 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ram 2 33050 Mortegliano UD Ital ified Tel 1005205 E 25057 TO P C LASS 580 IS H 7 e Fax 439 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph LOG OF REVISIONS Revision No 1 Revision Date Signature 01 Propeller auto pitch control system 20 12 10 Cosatto C 02 Added checks and emergencies related to 25 01 11 Cosatto C propeller pitch variation system 03 Converted speeds from knots to mph 25 02 11 Cosatto C Y FLYSYNTHESIS FLYSYNTHESIS Provincial Road n 78 Km 12 150 33050 Mortegliano UD Ital Fax 439 0 432 931280 y Tel 39 0 432 992482 39 0 432 993557 Sito web www flysynthesis com e mail info Gflysynthesis com Pilot Operating Handbook FLY SYNTHESIS TEXAN TOP CLASS 580 SR for Rotax 91
43. ltered electric fuel pump Fuel specification Rotax 912ULS Premium Automotive Unleaded fuel min 95Ron For complete fuel specifications see engine manufacturer manual ELETRICAL SYSTEM Type 12 V CC electric wiring with starting battery Circuit breakers protected wiring Provision for gyroscopic instruments autopilot radio and gps AvMap EKP IV POWERPLANT Engine Rotax 912 ULS Type 4 stroke 4 cylinder horizontally opposed spark ignition engine liquid cooled cylinder heads ram air cooled cylinders two constant depression carburetors mechanical fuel pump air box friction clutch geared reduction drive radiator cooled oil warm air at carburetor system Ignition increased electric ignition system HD Battery Sealed Lead Acid Battery 12 Volts Applicable to both engines Standard propellers DUC composite three blades propeller diameter 1750 mm ground variable pitch GT 2 wood two blades propeller diameter 1730 mm fixed pitch 1550 mm Alisport Idrovario two blades variable pitch propeller diameter 1760 mm automatic in flight variable pitch with Custom Intelligent Propeller control box manual operations have been removed Y FLYSYNTHESIS Identification POH TC 580 Rev 3 Gf FLYSYNTHESIS Pilot Operating Handbook Page 11 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 7 0 a eee TOP CLASS 580 18RA e b coats Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com A Revision
44. lus accessories and equipment After painting or reparations of fuselage Weight and Center Gravity position must be recorded after every change to the weighing report inside this manual only by authorized personnel The weighing report must be recalculated and reissued if the empty weight changes by more than 0 596 of MTOW or 10 kg whichever is greater of the empty weight The location of the CG can be defined by reference to the MAC Maximum anterior limit 2796 M A C correspondent to 377 mms Maximum back limit 3696 M A C correspondent to 504 mms For methodology and conditions for weight and balance procedure see section 6 Y FLYSYNTHESIS Gf FLYSYNTHESIS Pilot Operating Handbook perro TC Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 5 33050 Mortegliano UD Ital ified Tel 2000 C LASS 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 2 8 MANOEUVRE LIMITATIONS All aerobatics maneuvers are prohibited The normal flight operations permitted are as follows Every connected maneuver to the normal flight operation Stalls with exclusion of the accelerated stall superior to 1 g Low speed figure eight chandelle turns below 60 The use of the aircraft has to conform with the Rules of the State within it
45. ncial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 5 26 33050 Mortegliano UD Ital fia Tel 3909442 997487 139 0 432 993557 TOP CLASS 580 ISR 7 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info Eflysynthesis com versions Converted speeds from knots in mph 2 11 CREVV The minimum crevv for flight operations is a person The pilot can choose the place of command either the right or the left The maximum number of people permitted on board is VVO 2 12 PLACARDS The following placards are to be located and visible to the pilot where an inspection or function is relevant and required in the designated area Located in baggage compartment 4 FLYSYNTHESIS BAGGAGE COMPARTMENT Maximum 12 KG Evenly distributed Located in baggage compartment 4 FLYSYNTHESIS Speed mph Weight Kg Vne Not Exceeded 155 Maximum Take off 580 Vmo Max Operating 124 Empty VVeight 330 Va Min Maneuvering 90 Minimum Pilot 70 Vfe Max Full Flap 75 Maximum Pilot Vs Stall 46 passenger 180 Vso Stall with flap AEROBATIC MANOEUVRES AND SPINS ARE PROHIBITED Y FLYSYNTHESIS Identification POH TC 580 Rev 3 Gf FLYSYNTHESIS Pilot Operating Handbook Page 19 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 7 xal 0 a si TOP CLASS 58018A 12 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com A Revision Description e mail info flysynthesi
46. ng check correct tightness good conditions and free space between the wheel and mounting bracket general good condition inflated correctly no signs of cracks or distortion free movement no signs of cracks or distortion no signs of cracks and is clean no signs of cracks fixed correctly remove check level check level no signs of cracks free from obstructions clean no oil or coolant leakage no signs of cracks and muffler springs hooked correct functionality no leakage correct functionality free movement No air bubbles inside reinstall and check tightness Y FLYSYNTHESIS Identification POH TC 580 Rev 3 4 FLYSYNTHESIS Pilot Operating Handbook page 20 77 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 5 5 33050 Mortegliano UD Ital ifad Tel 3909442 997487 139 0 432 993557 TOP CLASS 580 ISR 7 77 Fax 439 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info Eflysynthesis com versions Converted speeds from knots in mph Check inside cabin IX Instruments panel fixed correctiy all placards present Master svvitch ON all insiruments ON Master svvitch OFF all insiruments OFF Control stick full free movement fixed correctly in its support Rudder pedals no distortion or signs of cracking correct operation of centering system and support fixed correctly Throttle amp choke levers free movement fixed correctly in
47. no Ital ified 277 4390432993557 TOP CLASS 580 ISR 7 e Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph SECTION 2 Limitations Introduction Airspeed limitations Airspeed marking Power plant and propeller limitations Power plant instruments marking Weight limitations Center of gravity limitations Maneuver limitations Load factor limitations 2 10 Opening canopy limitations 2 11 Crew 2 12 Placards 4 FLYSYNTHESIS Identification POH TC 580 Rev 3 FLYSYNTHESIS Pilot Operating Handbook page 1 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ram 2 33050 Mortegliano UD Ital ified Tel 1005205 E 25057 TO P C LASS 580 IS H 7 e Fax 439 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 2 1 INTRODUCTION This section contains the operational limitations and instruments markings used for this aircraft the engine and the standard equipment The limitations of speed have been calculated follovving the CS VLA rules The structure has been tested follovving the same rules 2 2 AIRSPEED LIMITATIONS Rotax Speed 912 ULS Notes IAS 250 km h Never exceed this speed in every 155 mph condition or configuration Maximum Structural 200 km h Never
48. ons on carburetors if RPM decreases without moving the throttle You can find this phenomenon during a descent with low RPM in a day with a lot of humidity 1 Carburetor heating system if installed On 2 Throttle All forward when RPM starts to increase 3 Carburetor heating system if installed Off 4 Reinstate normal flight conditions ABNORMAL ENGINE VIBRATIONS 1 Verify the reduction of the vibrations vvith a reduction of the RPM s 2 Land as soon as possible 3 Be prepared for a possible engine failure and to commence a forced landing LANDING WITH BRAKE SYSTEM FAILURE 1 Look for a long grassy runway with absence of obstacles the grass has a light braking action 2 Land with the flaps to the maximum extension and reduce speed to the minimum safe speed After touching the ground 3 Master switch amp ignition magnets key Y FLYSYNTHESIS f FLYSYNTHESIS Pilot Operating Handbook e e r 57 locuci Road n 78 Rm 12 150 FLY SYNTH ES IS TEXAN Py Issued 33050 Mortegliano UD Italy Verified C Cosatto Tel 39 0 432 992482 39 0 432 993557 TO P C LAS S 580 IS H Approved C Cosatto Fax 39 0 432 931280 for Rotax 912 ULS 7 Sito web www flysynthesis com Revision Description e mail info flysynthesis com versions Converted speeds from knots in mph 3 9 PROPELLER PITCH CONTROL SYSTEM EMERGENCY only if equipped with Idrovario propeller and CIP control system NOT POSSIBLE
49. or Interrupted fuse 2 Landing ASAP LOW VOLTAGE ON GROUND 1 RPM Reduce 2 Navigation and landing lights Off 3 Voltmeter Verify within limits 4 If the check has negative result Shutdown engine 4 FLYSYNTHESIS Gf FLYSYNTHESIS Pilot Operating Handbook pero 16 S80 enl ions Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN OR 33050 Mortegliano UD Ital ified Tel 2000 C LASS 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph ELECTRICAL WIRING or EQUIPMENT ON FIRE An electrical fire is recognizable by the distinct odor of burning plastic and white smoke 1 Master switch Off 2 Vent systems All open 3 Cabin heating Off 4 Landing ASAP WARNING get ready to possibly land without the use of flaps and trim if electric SMOKE ELIMINATION FROM CABIN 1 Vent systems All open 2 Cabin heating Off 3 Master switch Off 4 If the smoke remains dense land immediately WARNING absolutely DO NOT open the canopy 3 6 LANDING EMERGENCY PROCEDURES LANDING WITHOUT FLAPS 1 Verify flap trim circuit breaker is in the ON position 2 Verify the position of both the flaps visually With flaps in symmetrical position both retracted or extracted at the same angle 3 Try to retract the flaps 4 Verify that th
50. p 16 Vertical fin with rudder Surface 1 150 m Height 1 350 Mean chord 0 850 Rudder Surface 0 600 Height 1 350 Mean chord 0 440 Travel 18 WEIGHTS Rotax 912 ULS Empty weight 330 kg Maximum allowed weight in baggage compartment 16 kg Maximum Take Off Weight 580 kg Minimum single pilot weight 70 kg Maximum pilot and passenger weight 180 kg LANDING GEAR Type Tricycle type landing gear with dampened nose wheel Main gear track 2 130 m Wheelbase 1 585 m Tire Main 4 00x6 Nose wheel 4 00x4 Tire pressure Main 2 2 2 4 bar Nose wheel 1 8 bar Brakes Main wheels hydraulic disc Y FLYSYNTHESIS FLYSYNTHESIS Pilot Operating Handbook e e 6 ees Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ram ni 33050 Mortegliano UD Ital ified Tel 2000 25057 TO P C LASS 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph FUEL SYSTEM Type Tvvo lines vvith mechanical and auxiliary electric fuel pump Fuel plan draining system and fuel back system in the right tank Tanks Tvvo integrated tanks vvith 50 liters of capacity for each tank Televel and fuel reservoir sensor for each tank Fuel tank caps and a vent line coming to belovv the lovver surface of the vving Non usable fuel 2 liter for each tank Fuel filter Gascolator on firevvall fi
51. ph STALL RECOVERY PROCEDURE Te Apply full power to reduce the loss of height 2 Push softly forward the control stick to eliminate the stall conditions NON INTENTIONAL SPIN RECOVERY PROCEDURE WARNING don t try to stop the rotation using the opposite ailerons 1 Throttle At minimum RPM 2 Rudder pedals All opposed to the sense of rotation 3 Control stick Neutral softly to dive 4 When the rotation stops and the aircraft is under control return to level flight WARNING do not exceed the Vne speed 3 5 ELETRICAL WIRING FAILURE GENERATOR WARNING LAMP LIGHTING 1 Voltmeter Check voltage if installed 2 Non essential electric equipment Off Land ASAP A fully charged and functional battery should permit the operation of trim flap and aux electric fuel pump for about 20 minutes OVERVOLTAGE Voltmeter indication if installed over 16 V 1 Master switch Off 2 Voltmeter Verify the decrease of voltage 3 Master switch On 4 Voltmeter Verify the increase of voltage within limits If the voltage does not return within limits proceed as follows 5 All non essential electrical equipment must be switched off 6 Land ASAP A fully charged and functional battery should permit the operation of trim flap and aux electric fuel pump for about 20 minutes LOW VOLTAGE IN FLIGHT 1 Possible causes Excessive consumption Too many appliances on Damage of the alternat
52. pproved Date versions 3NION3 lEHn N uu pesoj H1 usdo Hy Sjoonej jeny Ayessaoau SV emoJu JUSWSAOW pue lin 6 01400 JUGI 4 HNO jes pue NO exeq Buried S OJAB ssedwioo oneuDeui 399U9 sjueuinujsur JUGI 4 pey90 pue pesojo Adouey sjeped pue yons JUSWAAOW jjny 043009 14611 p u se pue pajsnipe seg Ajayes Ailenb ayesodo 100 xoeuo seyeig peisnf pe syeas ONIIXV L M 3HO IH T14 44d3 for Rotax 912 ULS Y FLYSYNTHESIS TOP CLASS 580 ISR x o o o D o O o FLY SYNTHESIS TEXAN 1 FL YSYNTHESIS Provincial Road 78 Km 12 150 33050 Mortegliano UD Italy 8 1 AIRCRAFT ON BOARD CHECK LIST cz 1s l 2eu5 51 216 xeiou ssejo d l EX L y eBed 1sil YOOYD STN 216 Xe OY ssejo d l uex L Tel 39 0 432 992482 39 0 432 993557 Fax 39 0 432 931280 Sito web www flysynthesis com e mail info flysynthesis com Swi UIUUMA sjueuinyjsui euiBu3 Ayessaoau sy ULL 55 sy emojJu 5 9 sy eou 55 of 57 25 021 11 C Cosatto C Cosatto C Cosatto POH TC 580 Rev 3 pesojo 240 euo Aq euo 440 240 NO IP sieonej Xue jen4 YOUMS JO Se A sojeuDe N oipeJ iueuudinbe e2u199 3 s ye q Guied e HnoJu p NMOGLNH
53. rovincial Road n 78 Km 12 150 FLY SYNTHESIS TEXAN 5 ssued 33050 M liano UD Ital ified 3 Tel 2000 x 145017 TO P C LAS S 580 IS R 7 e 57 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 4 1 INTRODUCTION This section contains the information for normal flight conditions and the checklist to follow before every flight 4 2 SPEED FOR NORMAL EMPLOYMENT Except otherwise suitable the following speeds refer to the maximum take off weight equal to 580 Kg and can be used for any inferior weight Take off Flap 157 Rotax 912 ULS Rotation 46 mph Speed at 50 ft 15 m obstacle 53 mph Climb Best angle of climb speed Vx 5 flap 55 mph Best rate of climb speed Vy 0 flap 81 mph Cruise Maneuvering speed Va 90 mph Max speed in turbulent air conditions Vmo 124 mph Never Exceeding Speed Vne 155 mph Landing approach 55 mph Landing Flap 45 44 mph Touch amp go Maximum power flap 20 55 mph Maximum demonstrated crosswind velocity 19 mph 4 3 FUEL CIRCUIT DRAINING PROCEDURE AND REFUELLING OPERATIONS The fuel circuit draining procedure must be done before the first flight of the day 10 minutes after the refueling and if the aircraft has remained parked for more than three hours between two flights The fuel circuit draining is performed through the Gascolator filter situ
54. s com ver sions Converted speeds from knots in mph Located on the tail boom 4 FLYSYNTHESIS TEXAN TC 580 ISR DATA PLATE Fuselage s n Date of Manufacture Engine Type Engine s n Located on the Instrument panel if custom Intelligent Propeller is installed Propeller Pitch Control Only Automatic Mode is approved Y FLYSYNTHESIS f FLYSYNTHESIS Pilot Operating Handbook Ee 16 ee Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 33050 Mortegliano UD Ital ified Tel 0402971 x 145017 TO P C LAS S 580 IS R 7 E 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com A Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph SECTION 3 Emergency procedures Title 3 1 Introduction 3 2 Ground emergency procedures 3 3 Take off emergency procedures 3 4 During flight emergency procedures 3 5 Electric plant failure 3 6 Landing emergency procedures 3 7 Opening parachute procedure 3 8 Other emergency 3 9 Propeller pitch control system emergency only if equipped 4 FLYSYNTHESIS Gf FLYSYNTHESIS Pilot Operating Handbook E e 16 SO ions Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ba 33050 Mortegliano UD Ital ified Tel 2000 C LASS 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com Revision Description
55. section The ailerons are differential whilst the flaps are electrically operated plain type the vertical tail control surface is composed by a fixed fin and by a mobile rudder and the horizontal tail control surface is completely mobile hinged in the central part with integrated trim The tricycle type landing gear is fixed with dampered nose wheel with the main legs made in spring steel construction The Texan Top Class aircraft is approved for Day VFR only Flight into bad weather with IFR conditions by VFR pilots and aircraft is extremely dangerous As the owner and operator of an aircraft you are responsible for the safety of your passenger and yourself DIMENSIONS General Wing span Length Height Wing Surface Wing chord Wing load Y FLYSYNTHESIS Identification POH TC 580 Rev 3 FFLYSYNTHESIS Pilot Operating Handbook page 7 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 5 25 3 ortegliano UD Ital fiad Tel 129 002992482 139 0 432 993557 TOP CLASS 580 ISR 7 F Fax 39 0 432 931280 for Rotax 9 12 ULS Sito web www flysynthesis com A Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph Flap Surface 0 570 m Span 1 700 m Chord 0 340 m Travel 0 45 Aileron Surface 0 570 m Span 1 700 m Chord 0 340 m Travel down 17 up 22 Stabilator Surface 1 950 m Span 3 000 m Chord 0 650 m Travel down 11 u
56. uge 0 8 bar 0 8 2 rpm 2 5 bar 5 7 rpm 7 bar Oil temp gauge 50 C 50 90 C 90 100 C 110 130 C 130 C CHT nd 50 100 C 110 135 C 135 C Y FLYSYNTHESIS POH TC 580 Rev 3 4 FLYSYNTHESIS Pilot Operating Handbook 507 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN 5 2 33050 Mortegliano UD Ital ified Tel 1005205 25057 TO P C LASS 580 IS H 7 e 7 Fax 39 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 2 6 VVEIGHT LIMITATIONS Rotax 912 ULS Empty vveight 330 Kg Maximum fuel vveight 77 Kg Maximum allovved vveight in baggage compartment 16 Kg Maximum Take Off VVeight 580 Kg 2 7 CENTER OF GRAVITY LIMITATIONS VVith the purpose to achieving the best performances of flight and operations in complete safety according to the procedures described in this manual the aircraft must have employed respecting all the schemes of load and balancing pointed out in the following pages Pilot must consider the limit of weighing and all correlated parameters Before the delivery of the airplane center gravity position and weight of the airplane are verified NOTE Empty weight amp Center gravity position must be updated after a new weighing in the following case Substitution and or modify of one or p
57. urning if possible and if the area allows it get ready for a forced landing see relative paragraph ENGINE FAILURE DURING TAKE OFF during climb If the height allows it proceed in the following way 1 Best glide speed 68 mph 2 Electric fuel pump Verify ON 3 Fuel tank faucet Verify RH tank faucet open 4 Fuel tank level check fuel quantity b Fuel pressure Verify within limits Y FLYSYNTHESIS Identification POH TC 580 Rev 3 FLYSYNTHESIS Pilot Operating Handbook e 7 7 7 22 of 57 Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ram Ba 33050 Mortegliano UD Ital ifiad Tel 1005205 E 25057 TO P C LASS 580 IS H 7 e Fax 439 0 432 931280 for Rotax 912 ULS Sito web www flysynthesis com a Revision Description e mail info flysynthesis com ver sions Converted speeds from knots in mph 6 Ignition magnets key Verify ON 7 Throttle Position warm engine starting 8 Engine start procedure If the engine immediately starts up climb to a safe height and land ASAP for a check If the engine doesn t start up prepare for an emergency landing amp proceed as follows 9 Flap As necessary 30 or 459 10 Fueltank faucet Close 11 Electric fuel pump Off 12 Master switch amp ignition magnets key Both Off WARNING Land AS SOON AS POSSIBLE in case of fire on board Never perform a 180 turn from too low a height in an effort to return to the runway 3 4
58. ust check completely the airplane with great attention and accuracy In this section there is a standard pre flight checklist Valid for each version The pre flight inspections must be carried out BEFORE EVERY FLIGHT The pilot in command is responsible for such inspections The inspection does not require any special tooling although a flashlight can be useful for inspecting dark areas The purpose of the pre flight inspection is to verify that there s no evidence of defective parts or problems that can endanger the safety of flight 4 FLYSYNTHESIS f FLYSYNTHESIS Pilot Operating Handbook e e Te 880 ees Provincial Road n 78 Km 12 150 FLY SYNTH ES IS TEXAN Ram 5 33050 Mortegliano UD Ital ified Tel 2000 x 145017 TO P C LASS 580 IS R 7 e 7 Fax 39 0 432 931280 for Rotax 9 12 ULS Sito web www flysynthesis com Revision Description e mail info Eflysynthesis com versions Converted speeds from knots in mph Remove all the protections 1 Pitot cover 2 VVheel stops Mobile surfaces stops Canopy covering Propeller protection Fuel draining procedure Left main landing gear I Leg no distortion bolts locked no sign of cracks on weldings Brake assembly condition and tightness Tire general good condition inflated correctly Wheel fairing good condition and free space between the wheel and mounting bracket Left wing II Wing surface absence of buckling absence of del
59. ynthesis com e mail info flysynthesis com BEFORE TAXIING Electrical system Navigation instruments Flaps Parking brake TAXIING Brakes Flight control Flight instruments Throttle ENGINE CHECK Parking brake Fuel tank faucets Temperature amp pressure Trim Flight controls Check magnetos Throttle Check minimum RPM Identification Page Date Issued Verified Approved POH TC 580 Rev 3 34 of 57 Pilot Operating Handbook FLY SYNTHESIS TEXAN TOP CLASS 580 ISR for Rotax 912 ULS versions 25 021 11 C Cosatto C Cosatto C Cosatto Revision Description Converted speeds from knots in mph ON and checked checked Position to take off 15 OFF check both operate equally free full movement stick and pedals Check magnetic compass and set altimeter and set gyross if fitted As necessary Rotax 912 ULS ON RH Open LH Closed Within limits in green arc Neutral Free 4000 RPM maximum decrease 300 RPM for each magnets All forward check minimum 5000 RPM 150 for 5 sec 5500 RPM min if in flight variable pitch propeller is installed 1400 RPM CAUTION Don t apply full power before 60 C of CHT During taxing don t allow the engine CHT to exceed 135 C BEFORE TAKE OFF Flight controls Trim Electric fuel pump Flaps Fuel tank faucets Engine instruments Flight instruments Safety belts Canopy Parking brake Full and
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