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ALLEGRO 2007 SW 

Ultralight Aircraft 

 
Type Certificate DEAC e.V.Germany No.61173 and 1249 from December 23.1999 
Type Certificate LAA Czech Republic No.05/2000 from October 17.2000      
 
 
 
 

 

 
 
 
 
 
 
 
 

FLIGHT  MANUAL 

 
 
 
 

FANTASY AIR s.r.o  
Kollárova 511   
397 07 Písek 
Czech Republic 
 
Tel.: 00420/777 112 144  Fax:  00420/382 212 962   
e-mail: [email protected] 

© Fantasy Air

Page 1 of 30

Revison 1.4  October 2007

Summary of Contents for ALLEGRO 2007 SW

Page 1: ...49 from December 23 1999 Type Certificate LAA Czech Republic No 05 2000 from October 17 2000 FLIGHT MANUAL FANTASY AIR s r o Kollárova 511 397 07 Písek Czech Republic Tel 00420 777 112 144 Fax 00420 382 212 962 e mail info fantasyair com Fantasy Air Page 1 of 30 Revison 1 4 October 2007 ...

Page 2: ...ble Turns 14 Load Factors 14 Cautions 14 Kinds of Operation 14 Emergency Procedures 14 15 How to Use the Emergency System 15 Normal Operation Procedures 15 22 Performance and Recommended Speeds 23 24 Other Information 24 25 Aircraft Assembly 25 Aircraft Disassembly 25 Aircraft Anchoring 26 Aircraft Repairs 26 Aircraft Cleaning and Washing 26 Periodic Inspections 27 30 Compulsory Adjustments Prescr...

Page 3: ...ays choose the flight direction and altitude with respect to the possibility of making a safe emergency landing manoeuvre 6 Always fly with sufficient speed margin especially during the take off and landing manoeuvres 7 Do not make any aerobatics e g wing overs even if you might feel that your piloting skills and the flying qualities and handling characteristics of the aircraft were good enough fo...

Page 4: ...hts be finished with graceful landing The microlight aircraft Allegro received the official Type Licence from the Light Aircraft Association of the Czech Republic No 05 2000 dated October 17 2000 Caution This Flight Operating Manual must be thoroughly studied by every owner aircraft business operator and pilot of this aircraft The manual describes the necessary flight and maintenance procedures an...

Page 5: ...________________ Name Address Date From To Assigned Aircraft Identification Sign ___________________________________________________________________________ Name Address Date From To Assigned Aircraft Identification Sign _________________________________________________________________________________________ Fantasy Air Page 5 of 30 Revison 1 4 October 2007 ...

Page 6: ...AR SERIAL NUMBER NOSE LANDING GEAR SERIAL NUMBER STRUT SERIAL NUMBERS ENGINE MOUNT SERIAL NUMBER ENGINE Manufacturer Engine Type Year of Manufacture Serial Number Reduction Gearbox type reduction ratio Further information can be found in the ENGINE LOG BOOK PROPELLER Manufacturer Type Serial Number Further information can be found in the PROPELLER LOG BOOK Fantasy Air Page 6 of 30 Revison 1 4 Octo...

Page 7: ...ttached to the front engine bulkhead made of laminate sandwich The central pilot bulkhead serves for attaching adjustable seats at the rear end of the fuselage there are two ribs made of laminate sandwich to stiffen the tail fin The centroplane is welded together from duralumin tubes the cockpit is covered by a transparent windshield made of polycarbonate splinter proof material Beware of fuel sta...

Page 8: ...d aircraft engine and its sudden stoppage can occur at any time It has not received any safety or durability testing and conforms to no aircraft standards Never fly the aircraft equipped with this engine at locations airspeeds altitudes or other circumstances from which a successful no power landing cannot be made after sudden engine stoppage For all eventual consequences of such a sudden engine s...

Page 9: ... enabled when the switch is set to the up position MAIN WHEEL BRAKES are controlled by means of a lever located on the control stick The lever is also equipped with a control of the parking brake Manoeuvring and Gust Envelope Operation Limitations Allegro Limiting Speeds never to be exceeded Wing flaps lever position Flaps Deflection Never Exceed Speed knots Cruise position 0 4 5 V NE 118 Take off...

Page 10: ... Determine the Aircraft s Centre of Gravity Position Place the aircraft with its wheels onto three scales The aircraft must be in the cruise position i e with its fuselage axis levelled horizontally Determine the total weight of the aircraft G in kilograms as a sum of the weight readouts from the scales located under the main wheels Gh which is the total of the weight readouts from the scales loca...

Page 11: ...f the mean aerodynamic chord SAT is X 100 x Xt bSAT Determined values bMAC mm La mm one pilot kg Gp kg Lp mm Gh kg Lt mm G kg Xt mm X The position of the aircraft s centre of gravity has to be from 25 to 35 of SAT Note The position of the centre of gravity of an empty aircraft almost exactly equals to that of an aircraft in the cruise position with one or two pilots and with the fuel tank empty or...

Page 12: ... by pushing the control stick forward bring the aircraft to the glide path turn off the ignition and set the throttle lever fully backwards tighten the safety harness set the wing flaps to the landing position when the aircraft is approximately 30 meters above the ground make the landing manoeuvre in the open area free from any obstacles against the wind if possible If the engine fails while the a...

Page 13: ...us damages cracks Check oil or fuel leakage Check fuel tank cap Fixed fuel tank cap tightness Check 2 Front fuselage Propeller propeller cone no cracks no clearance problems Check cone screws tightness Check propeller blades no damage Check attachment screws Fixed 3 Front fuselage right side Cowling camlocks Fixed obvious damage cracks Check oil and fuel leakage Check Engine room engine mount and ...

Page 14: ...deformation Check no cracks on the rivet fastening spot Check drive control axis fixed up and down movement free and fluent drive control axis fixed 6 Main undercarriage right leg Undercarriage leg no cracks no surface breaks Check wheel axes right placed and secured general state no deformations Check Wheel rim no damage tyre inflation no damage Check creep marks on the rim Check distance between...

Page 15: ... fixing fixed and secured elevator hinge clearance corrosion Check elevator movement free and fluent control no corrosion Check trim tab placing and hinge Check 8 Main undercarriage left leg identical as by No 6 9 Left wing rear part identical as by No 5 10 Left wing front part identical as by No 4 Pitot tube Pitot tube cover Removed and put aside hose for static and dynamic pressure connected sta...

Page 16: ...ug prospectively the tank desludging plug drain off 120 ccm fuel into a prepared transparent cup and Check its quality impurities water etc repeat until fuel is clear tighten the drain plug prospectively the desludging plug and Check the tank tightness after having finished the complete operation Refuelling To be made only after the engine and all aircraft electric installation is switched off It ...

Page 17: ...ck fuel pressure minimum 0 2 bar 22 Radio Intercom switch on 23 Transponder if fitted switch on control position stand by 24 Artificial horizon if fitted reset horizon 25 Taxing Landing light switch on 26 After reaching the CHT minim 600 C start taxiing Starting the engine Before you first start the engine secure the aircraft so that it could not move spontaneously by means of wedges make sure the...

Page 18: ...to the centreline of runway 3 Maximum engine power 4 Check engine revolutions oil and fuel pressure Take off by opening the throttle make the aircraft move when you reach the take off speed pull the control stick slightly backwards to get the aircraft off the ground after you take off keep on flying level close above the earth for a while until you reach the climbing speed and then maintain that s...

Page 19: ...y and bring the throttle lever to minimum pull the control stick slightly backwards to make the aircraft stall the aircraft lands at the speed of about 38 to 35 knots Operations to be made after landing set the wing flaps to the cruise position 0 observe the recommended taxiing speed before turning the engine off let it cool down to the recommended temperature according to the engine manual and sw...

Page 20: ...e Ratio by engine off 1 12 Power Off Descent Rate 60knots flaps Position 0 300 ft min Power Off Descent Rate 60knots flaps Position 1 400 ft min Power Off Descent Rate 60knots flaps Position 2 700 ft min Fuel Consumption at the Cruise Speed of 85knots and Maximum Weight approx 12 litres hour Flight Range 4 hour 30 minutes Take off distance MSL 15ºC wind 0 knots MTOW 450 KG 100 m Take off distance ...

Page 21: ... be a label specifying the tank capacity and the required fuel quality RON 95 Min c Aircraft Registration Label Aircraft Registration Letters Aircraft Manufacturer Fantasy Air s r o Empty Weight 266kg Aircraft Type Allegro Maximum Take off Weight 450 Kg Year of Manufacture Aircraft Serial Number The aircraft user operator is responsible for all labels legibility within the whole aircraft lifecycle...

Page 22: ...t must fit in place easily If it does not the position of the wing in respect to the centre section is not correct Do not force as the mounts could become damaged When the wing is in place insert the front bolt Then fit the strut onto the mount on the wing and secure by a bolt too Next fit the back bolt through the back wing centre section mount All the time during the assembly somebody must be ho...

Page 23: ...ce to duralumin and laminate are you not sure about All insects stuck on the aircraft can influence distinctly performances and air characteristic of the aircraft That s why it is necessary to remove them in time The best way how to do it is to wet the surface first and let them soak for a while before we wiping it with a sponge Avoid any using of raw sponges which could damage the aircraft surfac...

Page 24: ...Check of the desludging of the fuel tank contingent engine and propeller inspections according to the manufacturers ENGINE LOG BOOK and PROPELLER LOG BOOK Inspection B all the Check listed under Inspection A checkout condition of bolts used for attaching the wing and struts Check of the wear and tear of the bolts of the undercarriage and replacement if necessary Check of the silent blocs used for ...

Page 25: ...Periodic Inspections of the Engine and Propeller to be made according to the respective manuals Fantasy Air Page 26 of 30 Revison 1 4 October 2007 ...

Page 26: ...Periodic Inspections DATE INSPECTION TYPE DEFECTS FOUND TECHNICIAN S NAME AND SIGNATURE Fantasy Air Page 27 of 30 Revison 1 4 October 2007 ...

Page 27: ...Periodic Inspections DATE INSPECTION TYPE DEFECTS FOUND TECHNICIAN S NAME AND SIGNATURE Fantasy Air Page 28 of 30 Revison 1 4 October 2007 ...

Page 28: ...Compulsory Adjustments Prescribed by the Manufacturer NUMBER DATE DESCRIPTION OF THE ADJUSTMENT TECHNICIAN S NAME AND SIGNATURE Fantasy Air Page 29 of 30 Revison 1 4 October 2007 ...

Page 29: ... Fantasy Air Page 30 of 30 Revison 1 4 October 2007 ...

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