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Atec 321 FAETA NG Flight And Operation Manual

With rotax 912 ul/uls
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The Sole Manufacturer and Distributor in Czech Republic:
ATEC v.o.s.
Factory address: ATEC v.o.s., Opolanská 350, 289 07 Libice nad Cidlinou
Czech Republic
ATEC 321 FAETA NG
with ROTAX 912 UL/ULS
Flight and Operations Manual
Libice nad Cidlinou, Czech Republic, November 2016
Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS
ATEC v.o.s., Libice nad Cidlinou, Czech Republic
Page 1 of 56

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Summary of Contents for Atec 321 FAETA NG

  • Page 1 ROTAX 912 UL/ULS Flight and Operations Manual Libice nad Cidlinou, Czech Republic, November 2016 Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 1 of 56...
  • Page 2 The aircraft must be operated according to informations and limits listed in this manual. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 2 of 56...

  • Page 3: Table Of Contents

    Weight, Centre of Gravity Enclosures: 1. Log Book (example) 2. Records of Revisions 3. Service and Maintenance Book Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 3 of 56...

  • Page 4: General

    1.2. Personal Data of the Owner 1.3. Aircraft Description 1.4. Modifications and Changes 1.5. Aircraft Technical Data 1.6. Three-View Sketch Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 4 of 56...
  • Page 5 1.1. Introduction Information provided within this manual is a necessary requirement for an effective and save operation of the ATEC 321 FAETA NG aircraft. The manual contents information which Manufacturer considers as important. 1.2. Personal Data of the Owner Owner of aircraft:...
  • Page 6 1.3. Aircraft Description ATEC 321 FAETA NG is an ultralight, two-seater, cantilever, low-wing aircraft of all carbon composite construction. The landing gear has a fixed tricycle gear with a steerable nose wheel. The propulsion unit is in pulling configuration and consists of ROTAX 912 UL or ROTAX 912 ULS engine and two or three- blade fix or ground adjustable FITI propeller.
  • Page 7 Normal, Super or Super Plus / min. RON 90 912 ULS/100HP MOGAS EN228 Super or Super Plus/ min. RON 95 Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 7 of 56...
  • Page 8 The pilot of sport flying device is obliged to consider the flight altitude and flight track so that to be able to make safety landing in case of engine failure. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 9 1.6. Three-View Sketch (mm) Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 9 of 56...

  • Page 10: Operating Limits

    2.8. Type of Operation 2.9. Crew 2.10. Fuel tank 2.11. Wind 2.12. Other Restrictions 2.13. Labels and Markings Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 10 of 56...
  • Page 11 Flying this speed with flaps extended in position III. results in loss of lift force and stall! Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 11 of 56...
  • Page 12 Centre of Gravity ( CG ) CG of the empty aircraft % MAC CG range allowance 25-35 % MAC Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 12 of 56...
  • Page 13 59,4 59,4 85,9 90,2 85,3 89,6 124,2 133,9 134,5 145,3 144,7 156,6 298,8 161,3 175,0 Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 13 of 56...
  • Page 14 6 m/s Never operate the aircraft when above listed wind range limits are exceeded! Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 14 of 56...
  • Page 15 Definition of aircraft category, its airworthiness conditions and restrictions • Prohibition of intentional spins, stalls and aerobatics Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 15 of 56...
  • Page 16 INTENTIONALLY LEFT BLANK Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 16 of 56...

  • Page 17: Emergency Procedures

    3.4. Fire on Board 3.5. Engine Loss 3.6. Emergency Landing 3.7. Safety Landing 3.8. Aborted Landing 3.9. Vibrations Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 17 of 56...
  • Page 18 Open the throttle Switch off the main switch and ignition Make emergency landing Get off the aircraft Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 18 of 56...
  • Page 19 Retract flaps Maintain the aircraft in take-off axis by using rudder control throughout the flight. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 19 of 56...
  • Page 20 Set the engine run up to appropriate RPM on which the vibrations are the lowest Carry out safety landing, eventually find the nearest airfield to land Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 21 INTENTIONALLY LEFT BLANK Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 21 of 56...

  • Page 22: Standard Procedures

    4.7. Cruising Flight 4.8. Descending and Landing 4.9. Flight in Rainy Conditions 4.10. Engine Shut-off Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 22 of 56...
  • Page 23 11/ Right wing – coating, condition, plays, fuel tank cap, drain valve, fuel tank ventilation 12/ Nose wheel – condition, play, wheel, tyre condition and inflation Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 24  10. Ignition switched off  11. Instruments check condition, zero values, altimeter setting Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 24 of 56...
  • Page 25 Note: The RPM speed difference between ignition circuits running separately must not be more than 115 RPM.  reduce to idle run Throttle Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 25 of 56...
  • Page 26 4.7. Cruising Flight ATEC 321 FAETA NG has good flight characteristics within the whole range of permitted speeds and position of the centre of gravity. The cruising speed range is 120 – 248km/h (65 – 134kt). Pay attention to values displayed on flight and engine instruments. The values must not be exceeded throughout the flight.
  • Page 27 Always keep the fuel valve open for appropriate fuel tank in use. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...

  • Page 28: Performances

    5.5. Take-off Distance up to 15m / 50ft 5.6. Rate of Climb 5.7. Cruising Speed 5.8. Flight Range Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 28 of 56...
  • Page 29 72,0 km/h 67 km/h 60 km/h 472,5 kg 43 kt 38,9 kt 36,2 kt 32,4 kt Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 29 of 56...
  • Page 30 Air speed Fuel consumption km/h 3500 3700 4100 10,1 4500 13,2 4800 14,7 5200 17,5 5500 Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 30 of 56...
  • Page 31 The flight range is considered as theoretic, when windless conditions. When planning the flight track, do consider these factors and safe amount of fuel reserve! Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 32 Chapter 6 Aircraft Assembly/Disassembly 6.1. Introduction 6.2. Horizontal Tail Assembly/Disassembly 6.3. Wings Assembly/Disassembly Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 32 of 56...
  • Page 33 HT stabilizer by any suitable white plastic tape which avoids water intrusion into the fuselage. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 34 Your assistant holds the wing by the wingtip and you hold it by the root. (The second assistant who can hold the wing by the flap would be helpful). Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 35 This ensures correct neutral position of ailerons. Secure the connection with the pin Ø5mm and spacer + split pin (all parts delivered attached to the pushrod). Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 36 Store the wings on safe and dry place with stable temperature. Wings need to be properly secured and prevented from structural and surface damage. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 37 7.6. Propulsion 7.7. Fuel System 7.8. Instruments 7.9. Controlling Elements 7.10. Canopy 7.11. Cockpit Equipment Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 37 of 56...
  • Page 38 The propulsion unit is ROTAX 912 UL or ROTAX 912 ULS engine and three or two blade FITI ECO COMPETITION propeller, which can be fix, ground or in-flight adjustable. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 39 Engine throttle By pushing the throttle lever forward, the engine power increases and vice versa. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 39 of 56...
  • Page 40 (optional equipment). 7.11. Cockpit Equipment (picture and description as by individual configuration) Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 40 of 56...

  • Page 41: Maintenance

    8.3. Engine Major Overhaul 8.4. Anchorage of the Aircraft 8.5. Cleaning and Care 8.6. Aircraft Storage Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 41 of 56...
  • Page 42 Check probes and indicators interconnections. Propeller Attachment Check condition of bolts, torques, securing. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 42 of 56...
  • Page 43 Fuselage Check general condition, integrity, purity. Antennas, lights, covers and cowlings attachment. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 43 of 56...
  • Page 44 For this purpose, the aircraft is equipped with screw mounting points for eyelets on the underside of the wingtips. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 45 The tyres inflation pressure shall be periodically checked. For engine maintenance during the aircraft storage, follow the instructions of the engine producer. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 46 9.3. Maximum Take-off Weight 9.4. CG Range 9.5. CG Determination 9.6. Useful Load, Weight Sheet Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 46 of 56...
  • Page 47 Range of centre of gravity in flight 25 - 35 % MAC Operation over this range is prohibited! Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 47 of 56...
  • Page 48 = 0,57 – 1,43 * G * 100 / 1,112 = CG-MAC% CG-MAC = 51,26 – 129,5 * G Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 48 of 56...
  • Page 49 CG position in % b If above listed limits are kept, the centre of gravity is situated in permitted position range. Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic...
  • Page 50 Total Fuel Take-off Date Pilot name Track Time Flight (filled (number) /day Time up/L) EXAMPLE Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 50 of 56...
  • Page 51 Revision Affected Affected Insertion Approval Date Approved by Signature Number Section Pages Date Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 51 of 56...
  • Page 52 Works performed / reason Date (mandatory inspection works, bulletins, reparations, modifications, Signature replacements, inspection reports, notes) Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 52 of 56...
  • Page 53 Works performed / reason Date (mandatory inspection works, bulletins, reparations, modifications, Signature replacements, inspection reports, notes) Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 53 of 56...
  • Page 54 Works performed / reason Date (mandatory inspection works, bulletins, reparations, modifications, Signature replacements, inspection reports, notes) Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 54 of 56...
  • Page 55 Works performed / reason Date (mandatory inspection works, bulletins, reparations, modifications, Signature replacements, inspection reports, notes) Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 55 of 56...
  • Page 56 Issued by the Manufacturer: Atec, v.o.s. Opolanská 301 289 07 Libice nad Cidlinou Czech Republic www.atecaircraft.eu Flight and operations manual of ATEC 321 Faeta NG aircraft with Rotax 912 UL/ULS ATEC v.o.s., Libice nad Cidlinou, Czech Republic Page 56 of 56...