Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 1. GENERAL This Maintenance Manual is updated regularly. The latest versions can be downloaded as a PDF file on the Web site of the manufacturer (www.promecc.com). The current version number is prin- ted on each page in the header (V ---).
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 1.2. DIMENSIONS WING ELEVATOR Wing span 8,777 m Elevator span 2,972 m Wing chord 1,209 m Surface 0,77 m Wing surface 10,13 m Stroke 20° (up) Dihedral 5° 15° (down) TRIM AILERONS...
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 1.3. LIFETIME RESTRICTIONS 1.4. FUEL AND OTHER LIQUIDS General overhauls are fixed on 1200 flight hours or 10 year of use. CAPACITY As for the engine and some special elements, refer to the following table:...
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 2. TECHNICAL DESCRIPTION 2.2. ENGINE COVER The engine is covered by a cover made of a top part and a lower one. The two pieces are fixed to This Section contains a description of the airplane and its equipments.
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 2.4. FIREWALL 2.6. WINGS The firewall is a structural element situated on the front part of the fuselage and it separates the The aircraft is provided with a low and tapered wing made up of 2 half-wings in carbon fibre that engine from the cabin.
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 2.7. EMPENNAGES 2.8. AILERONS CONTROL Classic type and provided with rudder, tail plane, elevator and trim electrically moved. The ailerons control is differential (when the right aileron moves upwards, the left one goes down- wards and vice versa).
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 2.9. FLAPS CONTROL Flaps control is electric-type, made of a linear actuator driven by electric switch. The control sys- tem is positioned inside the fuselage, accessible removing the trunk. Flaps control is an electric switch with up-down positions located on the instrument panel in the cockpit, on the control panel;...
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA Adjustment of The Elevator Control The control stick’s neutral position in the cockpit must correspond to the elevator control’s neutral position. The rigging of the elevator’s angles of steering is possible through an adjustable connecting-rod.
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 2.12. RUDDER CONTROL 2.13. UNDERCARRIAGE Rudder control constists of pedals, connecting rods, bearings, bowed cables. The left and right It is a fixed three-wheel undercarriage with a turning nose wheel and disc brakes on the main lan- pedals have independent-rotation axles.
Main switch is ON. Engine removal, installation and replacement can only be done by Pro.Mecc authorized Each system is protected by circuit breaker which is permanently on. If some circuit is overloaded, service center.
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Coolant Fluid: see Engine Operator Manual. FUEL SYSTEM Freccia in basic version is equipped of a fuel tank installed inside right wing, having capacity of 50 liters. The drenable quantity of fuel is 48.5 liters. It is available as option the second fuel tank that can be installed on the left wing.
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 2.18. PITOT – STATIC PRESSURE SYSTEM The pitot-static tube is located under the leading edge of the right wing and consists of a air duct. Total system pressure is sensed through the hole in the pitot-tube face and static pressure is sensed through the holes on both sides of the rear part of fuselage.
It is reasonable to proceed according to a prescheduled scheme of lubrication and maintenance, Propeller removal, installation and replacement can only done of Pro.Mecc or propeller ma- appropriate to the operating conditions and climate. nufacturer authorized service center.
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Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA CONTROLS (LO every 100 hrs or yearly) first 5 1000 10 000 Daily hours hours hours hours hours hours hours general free play ...
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA ELECTRICAL WIRING 3.3. INSPECTION AFTER 100 HOURS OF FLIGHT (AT LEAST ONCE A YEAR) battery Note: the inspections on engine after 100 hours of flight must be carried out in accordance battery fluids with the engine’s operating manual, as well as the following hours.
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 21 Check by a protractor the rudder surfaces’ angles of deviation. If these deviations are more 3.4. LUBRICATION INSTRUCTION important than their tolerances, adjust them. UNIT AREA OF LUBRICATION 25 H 100 H LUBRICANT 22 Remove the cover’s top, check the fuel circuit’s tubes and the valves about the absence of...
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 4. GROUND HANDLING 4.2. PARKING 1 1. Position the airplane pointing into wind. The dimensions of the standard airplane are given in the airplane drawings. This allows the size of 2 2. Apply chocks to the main wheels.
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 5. CLEANING AND CARE 4.4. LIFTING AND LEVELLING When jacking the airplane the following procedure should be followed: It is essential for the reliability of the airplane components to always keep them clean.
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 6. REPARATIONS 6.2. REPLACEMENT OF BRAKES’ PADS As for the replacement of brakes’ pads and of brakes’ discs, follow these steps: Any repair or modification of the airplane design may only be performed by authorized personnel.
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 7. INFORMATION SIGNS AND MARKINGS 7.2. FURTHER MARKINGS MARKINGS This chapter describes the labels and the location of signs are described on the aircraft. 7.1. PANEL static port - keep clean All designations for switches, controls and fuses are printed directly on the panel. The printing depends on the cockpit configuration.
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 8. RESCUE SYSTEM 8.2. INSTALLATION DRAWINGS CABLE SETUP PARACHUTE-BRIDLE CONNECTION POINT 8.1. TECHNICAL DATA OF THE MAGNUM LIGHT SPEED SOFTPACK ENGINE MOUNT CABLE LENGTH 2200 mm CABLE LENGTH 2250 mm Length of container...
Maintenance Manual V001 Maintenance Manual V001 FRECCIA FRECCIA 9. WEIGHING PROCEDURE 8.3. MAINTENANCE OF THE MAGNUM LIGHT SPEED SOFTPACK Throughout the dismantling – or assembly process never use violence or bring tension on the acti- This Section contains the limitations of the useful load, within which the airplane may be opera- vation cord! All steps must be made smooth.