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Fantasy Air ALLEGRO 2007 SW Flight Manual

Summary of ALLEGRO 2007 SW

  • Page 1

    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...

  • Page 2: Table

    Table of contents contents……………………………………………………………………………………….. 2 ten rules of safe flying............................................................................................................ 3 introduction ...........................................................................................

  • Page 3: Ten Rules of Safe Flying

    Ten rules of safe flying 1) observe the relevant regulations for microlight aircraft. 2) do not overestimate your piloting skills and never show off for the sake of spectators. On the contrary, try to use suitable strips of land for practising the procedure of emergency landing. 3) watch the weather...

  • Page 4: Introduction

    Introduction the allegro is a 2-seat microlight aircraft with strut-construction high-wing monoplane designed for sport, leisure-time recreational or tourist flying as well as for the training of new student pilots. Among its major merits we should mention are its excellent handling characteristics,...

  • Page 5: General Information

    General information aircraft owner name: address: date: from: to: assigned aircraft identification sign: ___________________________________________________________________________ name: address: date: from: to: assigned aircraft identification sign: _________________________________________________...

  • Page 6

    Aircraft allegro aircraft serial number: fuselage shell serial number: wing serial numbers: horizontal tail unit serial number: vertical tail unit serial number: centroplane weldment serial number: main landing gear serial number: nose landing gear serial number: strut serial numbers: engine mount s...

  • Page 7: Brief Technical Description

    Brief technical description the allegro aircraft is an aerodynamically controlled, two-seat side by side, high-wing microlight aircraft with the engine at the front and a t-shaped tail. Tricycle landing gear with main wheel brakes, steerable nose wheel, landing gear suspension by rubber pads. The ai...

  • Page 8

    Main specifications – allegro pr. No. Airframe dimensions aileron and rudder deflection wing span 10800 mm(vla) or 9600mm(sw-450kg) aileron: up 165 mm +- 5 mm airframe length 6360 mm down 55 mm +- 5 mm total height 2050 mm elevator: up 79 mm +- 5 mm wing area 11.37 m 2 down 66 mm +- 5 mm aspect rati...

  • Page 9: Aircraft Control

    Aircraft control foot control – when the left pedal is depressed the aircraft turns to the left, both on land and in the air, and vice versa. Hand control (located in the middle of the cockpit) – when the control stick is pulled backwards, the nose of the aircraft raises upwards (the angle of incide...

  • Page 10: Position

    Limiting speed: vne = 118 knots do not exceed this speed in any event! Limiting wind speeds: maximum allowable crosswind speed (i.E. 90 degrees to the direction of the flight)...............12 knots do not try to take off or land with a tail-wind except for emergencies! -----------------------------...

  • Page 11

    Calculation for determining the aircraft’s centre of gravity position: ] g p x l p l t = ————— = the distance of the aircraft centre of gravity from the main undercarriage axis g (mm) g x t = l a - l t – x sat / allegro/- b sat = 1115mm x sat = 14mm this distance expressed as the percentage of the m...

  • Page 12: Load Factors

    Load factors maximum positive load factor in the centre of gravity................................... + 4.0 g maximum negative load factor in the centre of gravity.............................…. - 2.0 g cautions besides the prohibitions ensuing from the relevant valid regulations it is also forbidde...

  • Page 13

    Normal operation procedures attention: all inspection steps mentioned in this chapter must be done very carefully before each flight. At first check magneto switches 1+2 – are off and key is out 1. Front fuselage – left side nose undercarriage - wheels axis fixed and tightened - distance between pne...

  • Page 14

    4. Right wing - front part - wing surface leading edge state - deformation, damages check - dirt and water on the wing leading edge clean - wing and strut attachment screws, bolts and metal cover fixing control check - fittings of spar fixing check - rivets inspection check - drive control connected...

  • Page 15

    7. Tail unit tail fin: - leading edge no deformation, no damage check rudder: - general state, no deformation check - rivets no cracks check - feathering hinge, clearance, corrosion, securing check - rudder free movement , after the tail is pushed down and nose wheel is up check - fixing and rudder ...

  • Page 16

    Control stick: - movement full and free - operating rod seating check pedal-operation: - no deformation check - nose leg+rudder+pedals adjustment check control - throttle, choke, brakes, trimmer: - movements full and free -bowden cable condition check centre-section: - no deformation, welded points ...

  • Page 17

    Operations to be done before the take-off a. Operations to be done on the aircraft stand 1. Inspection according to the flight & operating manual 2. Position the seat for height and fore and aft. 3. Position and fasten safety belts – check also the second crew member 4. Make sure the cockpit is clos...

  • Page 18

    C. Operations to be done on the holding point 1.Cockpit door closed - check – check the passenger side too 2. Check the security and tightness of safety belts – check the passenger side too 3. Choke – closed 4. Rescue system – unlocked (if fitted) 5. Fuel cock – open 6. Trimmer in the position take-...

  • Page 19

    Flying in the rain: - it is not recommended to take off in the rain! - if you get into the rain during the flight, maintain the speed above 60knots - if you must land during the rain, approach at higher speed 60 knots - keep in mind that both the stall speed and the landing speed are higher when the...

  • Page 20

    Performance and recommended speeds total weight of the aircraft (kg) 360 kg 450 kg take-off speed (knots) 40 45 climbing speed (knots) 60 60 landing approach speed (knots) 60 60 maximum rate of climb with engine r912 –ft/min 1200 1000 caution: all above mentioned ias speeds values were measured at a...

  • Page 21: Other Information

    Other information obligatory labelling: a) in the pilot’s cockpit there must be a label located on a well visible place with the following text: ”this aircraft has not been certified to an international requirement aerobatics and deliberate spins are prohibited.” b) besides, there must be another la...

  • Page 22: Aircraft Assembly

    Aircraft assembly there must be at least two people to assemble the aircraft, preferably three. Follow the instructions below: 1) fit the horizontal tail unit onto the tail fin, connect them using a bolt having a diameter of 6 mm and secure by a slotted nut with a cotter pin. When you are fitting th...

  • Page 23: Aircraft Anchoring

    Aircraft anchoring if the aircraft is parked in an open area, it is necessary to anchor it using ropes and anchoring tie downs. In order to avoid movement. Turn the aircraft with its nose against the wind, fix the ropes to the catches on the rings on the strut ends and to the noise wheel, and if nec...

  • Page 24

    Periodic inspections of the aircraft the inspections to be carried out before each flight and after each landing are described in the section ”pre-flight inspection”. After the first 20 flight hours the guarantee inspection shall be carried out by the manufacturer’s technician in the extent of inspe...

  • 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

    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

    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.