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Summary of Contents for Spacek SD-1 Minisport TG
- Page 1 SD-1 Minisport TG, SE-33, P.O.H PILOT OPERATING HANDBOOK (P.O.H) FAI UL / SSDR SD-1 MINISPORT Type: SD-1 Minisport TG, engine SE-33, propeller Helix H30F Airplane must be operated in compliance with the information and limitations stated in this manual. Issue 1...
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Page 2: Table Of Contents
SD-1 Minisport TG, SE-33, P.O.H CONTENTS 1. General 1.1 Description of airplane 1.2 Warning, cautions notes 1.3. Description of airplane 1.4. Main technical data 1.5. Engine and propeller 1.6. Three-view airplane drawing 2. Operation Limitations 2.1 Airspeed Limits 2.1.2 Air speed indicator marking 2.1.3 Limitation of maximal permitted wind speed... -
Page 3: General
SD-1 Minisport TG, SE-33, P.O.H 1. General The airplane SD-1 Minisport belongs to the FAI-UL category, according to the CAA UK as Single Seat Deregulated microlight (SSDR). 1.1. Important information Attention! This product is not liable to be approved by Civil Aviation Authority, and it is operated at someone’s own risk. -
Page 4: Main Technical Data
SD-1 Minisport TG, SE-33, P.O.H 1.4 Main technical data Measurements Wing span…...…………………...… ..5,98 m Fuselage length..…………………..4,35 m Wing area .…………………………..6,1 m Wing aspect ratio…..…………….… ..5,85 MAC depth b ………………………1,05 m Horizontal tail unit span……..………1,96 m Elevator Area…………………………0,95 m Vertical tail Area……………………...0,44 m... -
Page 5: Three-View Airplane Drawing
SD-1 Minisport TG, SE-33, P.O.H 1.6 Three-view airplane drawing 1. Operation Limitation 2.1 Airspeed limitation Speed Meaning (km/h)/(kt) Never exceed speed 220 / 119 Do not exceed this speed in any operation Maximum maneuvering Do not make full or abrupt... -
Page 6: Airspeed Indicator Marking
SD-1 Minisport TG, SE-33, P.O.H 2.1.2 Airspeed indicator marking Airspeed indicator markings and their color meanings are shown in the table below: Marking Value ( IAS ) Meaning Range (km/h)/(kt) Operation range with extended flaps. (The lower limit is 1.1 V... -
Page 7: Loads
SD-1 Minisport TG, SE-33, P.O.H 2.3. Load Maximum allowed filling of the fuel tank in liters Weight of Pilot’s weight (kg) baggage (kg) Full fuel tank Full fuel tank Full fuel tank 2.4. Approved maneuvers SD-1 is approved as FAI UL. Following maneuvers are approved to be performed: ... -
Page 8: Other Limitations
SD-1 Minisport TG, SE-33, P.O.H 2.6. Other limitations SMOKING IS PROHIBITED on the airplane board! Heavy rain and very high humidity reduce aircraft performance! In flight under these conditions is recommended to increase take-off and landing speed by 5 knots. -
Page 9: Operation Data And Procedures
SD-1 Minisport TG, SE-33, P.O.H Operation data and procedures 3.1 Emergency procedures 3.1.2 Engine failure Engine failure at take-off below 50 m (150ft) 1. Adopt the glide airspeed to 110 km/h (59kt) 2. Choose an area for landing straight ahead, only in a case to prevent from frontal crash change the direction 3. -
Page 10: Normal Procedures
SD-1 Minisport TG, SE-33, P.O.H 6. Correct the glide path to be able to touch-down immediately after flying over the edge of chosen area. 7. After touch-down use brakes for prompt stop. 8. After stop shut off engine and master switch, close fuel valve and safe the airplane. - Page 11 SD-1 Minisport TG, SE-33, P.O.H ignition - OFF master switch - OFF instrument equipment - check on condition fuel indicator - check on fuel condition controls -visual check, function, allowance, free movement to its stop - check of lift flaps run ...
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Page 12: Prior To Engine Starting
SD-1 Minisport TG, SE-33, P.O.H 4.3 Normal procedures and check list 4.3.1 Prior to engine starting CHECK POSITION OF FRONT WHEEL BEFORE ENGINE STARTING!!! DANGER OF AIRPLANE DAMAGE. 1. Controls ..........free movement 2. Canopy ..........close and lock 3. Brakes ..........push on 4. -
Page 13: Performance
SD-1 Minisport TG, SE-33, P.O.H 4.3.6 Landing On downwind leg maintain 110-130 km/h (59-70kt). On base leg slow down to 57 knots and set flaps to first stage. Slow down to 90-100 km/h (49-54kt) and set full flaps flaps on final. In case of wind from 45º and more to runway centerline or turbulence do not apply full flaps and land at 100 km/h (54kt). -
Page 14: Glide
SD-1 Minisport TG, SE-33, P.O.H 5.5 Glide Best glide speed 110 km/h / 59 kt Glide ratio @ 110 km/h / 59 kt 1: 13 5.6 Stall Speeds Stall speed are measured in MTOW and level flight. Stall speed Position... -
Page 15: Weight And Balance
SD-1 Minisport TG, SE-33, P.O.H 6. Weight and balance Empty weight measured 118-137 kg C.G. position movement from 22 to 34% MAC Allowed centre of gravity position range Front end point 22 % MAC= 231 mm from leading edge Rear end point... - Page 16 SD-1 Minisport TG, SE-33, P.O.H 7.5 CONTROLS The horizontal tail and flaperons are controlled via pushrods and bellcranks. Flaps are controlled using mixer placed bellow seat. Rudder is controlled via cables. 7.6 ENGINE The airplane is driven by SE-33 engine. Engine mount is made of CrMo tubing. Helix H30F fixed pitch propeller.
- Page 17 SD-1 Minisport TG, SE-33, P.O.H 8. Handling, treatment and maintenance of the airplane 8.1. FOREWORD This chapter contains procedures recommended by manufacturer for proper airplane operation. 8.2. PERIODICAL INSPECTION OF AIRPLANE The time intervals in which is necessary to perform comprehensive inspections or maintenance depend on the service and whole airplane condition.
- Page 18 SD-1 Minisport TG, SE-33, P.O.H Action Performed Description Checked by Cowling Check cowling for loosenes, cracks or any damage. Check completeness of hardware. Propeller Check tips and leading edge on damage. Repair using epoxy or varnish.. Fuel system Check tighteness of whole system and condition of all hoses.
- Page 19 SD-1 Minisport TG, SE-33, P.O.H Action Performed Description Checked by Wing Check skin for cracks and possible bonding failure. Check possible free movement in main and auxiliary assembly pins. Check flaperon hinges and possible free movement in control connection pin.
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