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Spacek SD-1 Minisport TG, Руководство по эксплуатации для пилотов, Страница: 18 / 19

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SD-1 Minisport TG, SE-33, P.O.H 

 

 

18 

Issue 1 

Action 

Nr.

 

Description

 

Performed 

by

 

Checked by 

7 

Cowling

 

Check cowling for loosenes, cracks or any damage. 
Check completeness of hardware.  

 

 

8 

Propeller

 

Check tips and leading edge on damage. Repair using 
epoxy or varnish..  

 

 

9 

Fuel system

 

Check tighteness of whole system and condition of all 
hoses. Check smoothness of fuel valve run. Check fuel 
filter and exchange if necessary.  

 

 

10 

Battery

 

Check voltage. Charge if necessary. 

 

 

11 

Cockpit

 

Clean using wet towel. Remove dirty on floor using 
vacuum cleaner. 

 

 

12 

Cabine hood

 

Use agent suitable for cleaning of polycarbonates. Do 
not use gasoline, alcohol etc. 

 

 

 

 

 

 

 
7.3.2. Inspection after 100 hours or year examination 

Action 

Nr.

 

Description

 

Performed 

by 

Checked by 

1 

Generaly

 

Clean  all  outside  and  inside  skin  of  airplane.  Check  on 
damage, wear and corrosion. 

 

 

2 

Front  of the airplane

 

Check engine (see engine manual), hoses, engine 
mount, propeller, battery, exhaust, firewall and rescue 
system.  
Check tightening and securing of hardware.  

 

 

3 

Fuel system

 

Check tube on cracks and valve function. Check fuel filter 
and exchange it if necessary. 

 

 

4 

Fuselage 

Check

 

outside skin on cracks and inside structure on 

possible rust. 

 

 

 

5 

Controls

 

Check free movement, wear of cable, tubing, bushes in 
stick, brackets, mixer and rod ends. Check end stops. 

 

 

6 

Instruments

 

Check screws, fuses, placards, switches and pitot 
system. Assure that all instruments work fine. 

 

 

Содержание SD-1 Minisport TG

Страница 1: ...O H 1 Issue 1 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 ...

Страница 2: ...oved maneuvers 2 5 G forces 2 6 Other limitations 2 7 Limitations labels 3 Operation data and procedures 3 1 Emergency procedures 3 1 2 Engine failure 3 1 3 Smoke and fire 3 1 4 Emergency and safety landing 3 1 5 Recovery of unintentional spin 4 Normal procedures 4 1 Assembling and Disassembling 4 2 Pre flight Check 4 3 General procedures and check list 4 3 1 Prior to engine starting 4 3 2 Engine ...

Страница 3: ...ion applies to warnings cautions and notes used in the Flight manual WARNING MEANS THAT NON OBSERVATIONS OF THE CORRESPONDING PROCEDURE LEADS TO AN IMMEDIATE OR IMPORTANT DEGRADATION OF FLIGHT SAFETY CAUTION MEANS THAT NON OBSERVATIONS OF THE CORRESPONDING PROCEDURE LEADS TO A MINOR OR TO A MORE OR LESS LONG TERM DEGRADATION OF THE FLIGHT SAFETY NOTE Draws the attention to any special item not dir...

Страница 4: ...f 12 kg Elevator weight 3 kg Maximum take off weight 240 kg Payload 110 kg Fuel tank volume 35 l Unusable fuel volume 0 5 l 1 5 Engine and propeller Engine SE 33 simple V twin OHV 4 stroke air cooled direct drive magneto ignition Max continuous power 25kW 3600 rpm Max take off power 22kW 3100 rpm Min CHT 60 C Max CHT 240 C Min oil temp 25 C Max oil temp 140 C Oil pressure 0 3 2 5 bar indicated by ...

Страница 5: ... Never exceed speed 220 119 Do not exceed this speed in any operation VA Maximum maneuvering speed 163 88 Do not make full or abrupt control movement above this speed because under certain conditions the aircraft may be overstressed by full control movement VFE Maximum flap extended speed 104 57 Do not exceed this speed with the given flap setting ...

Страница 6: ...c 163 220 88 119 Maneuvers must be conducted with caution and only in smooth air Yellow line 163 88 Maximum maneuvering speed Va Red line 220 119 Maximum airspeed Vne 2 1 3 Limitation of maximum acceptable wind speed The maximum acceptable wind speed for take off and landing is 10 m s 20kts The maximum acceptable perpendicular component of wind for take off and landing is 5 m s 10kts 2 1 4 Power p...

Страница 7: ...recommended entering airspeed is 130 km h 71kt Horizontal eights recommended entering airspeed is 130 km h 71 kt Climbing turns recommended entering airspeed is 160 km h 87 kt 2 5 Maneuvering load factors Maneuvering speed Airspeed km h kt Load factor VA maneuver with maximum deflection of a control surface 163 88 4 VNE maximum acceptable airspeed 220 119 4 VA maneuver with maximum deflection of a...

Страница 8: ...these conditions is recommended to increase take off and landing speed by 5 knots 2 7 Limitation labels Airspeed IAS Maximum airspeed VNE 220 km h 119 kt Maximum maneuvering speed VA 163 km h 88 kt Maximum flap extended speed VFE 104 km h 57 kt AEROBATICS AS WELL AS INTENTIONAL SPINS ARE PROHIBITED Flights according to IFR and intentional flights under icing conditions are prohibited ...

Страница 9: ...ttle lever FULL 3 When the engine stops master switch OFF 4 Extinguish fire by slip Do not start the engine again 5 Make a safety landing 3 1 4 Emergency and precautionary landing Emergency landing 1 Airspeed adjust to 110 km h 59kt 2 Choose landing area free space without obstacles 2 Tighten up the safety harness 3 Flaps according to your need 4 Fuel selector OFF 5 Ignition OFF 6 Master switch OF...

Страница 10: ...trol handle to the flaperon stone and the control handle into the flaperon slot link Fix up the auxiliary hinge and push on the main hinges into the stubs circa 1 cm deep using an extension stick In the same way put the left wing on Both wings are on push the main hinges in and fix them up by pins Secure the auxiliary hinges by binding wire When mounting the horizontal tail units HTU push the cont...

Страница 11: ... engine bed and exhaust system visual check on fuel and electrical system condition other checks according to the engine manufacturer instructions wing surface condition leading edge condition check Pitot tube condition wing tip surface condition attachment check flaperon surface condition attachment allowance free movement landing gear check on wheels attachment brakes condition and inflation of ...

Страница 12: ...emperature bellow 15 ºC Prolong warm up time adequately at lower air temperatures The CHT should not be below 120 ºC during run up At least 3100 RPM static should be achieved at run up 4 3 3 Taxying Use the engine power and brakes according to your need Do not use brakes continuously The rudder is efficient from 20 knots speed Taxi carefully in the strong wind Hold the control stick in stick back ...

Страница 13: ...uted from actual flight tests If not stated otherwise the performances given in this section are valid for the max take off weight and flight under ISA conditions 5 1 Take off distance Grass runway Take off roll distance Distance over 15ft screen hight 130 m 300 m Paved runway concrete asfalt Take off roll distance Distance over 15ft screen hight 120 m 280 m 5 2 Landing distance Grass runway Landi...

Страница 14: ... speed are measured in MTOW and level flight Position Stall speed km hod kt IAS Flaps retracted 78 42 Flaps 1 stage T O 7 I 70 38 Flaps 2 stage L D 20 II 64 34 5 7 Airspeed Indicator Calibration System IAS km h CAS km h 60 61 70 70 80 80 90 89 100 98 110 107 120 116 130 126 140 135 150 144 160 153 170 163 180 172 190 181 200 190 210 200 ...

Страница 15: ...o the side The NACA inlet for ventilation is on the side of cabine hood 7 2 WING It consists of composite main spar with carbon caps on which are glued XPS ribs The structure is covered with 1 mm plywood Wingtips are made of sandwiched glass composite Connection of wings to fuselage is made thru two main and two auxiliary pins The connection of flaperons to controls is performed by inserting of co...

Страница 16: ...TRUMENTS AND PITOT STATIC SYSTEM The airplane is fitted with basic flying instruments speedmeter altimeter compass and vario The RPM s total hours head and exhaust gas temperatures are checked on the engine The COM antenna is built in the airframe The pitot tube is placed on the leading edge of right wing The static ports are placed from bothe sides of fuselage in front of tails 7 10 RESCUE SYSTEM...

Страница 17: ... 8 3 1 Inspection after first 25 hours and after 50 hours Action Nr Description Performed by Checked by 1 Generaly Wash whole airframe using wet sponge and suitable detergent Remove cowling and covers and check fixing of all parts fuel oil and electrical installation Check tightening and securing of all hardware 2 Controls Check control cables on damage Check metal parts for corrosion Repair if ne...

Страница 18: ...tes Do not use gasoline alcohol etc 7 3 2 Inspection after 100 hours or year examination Action Nr Description Performed by Checked by 1 Generaly Clean all outside and inside skin of airplane Check on damage wear and corrosion 2 Front of the airplane Check engine see engine manual hoses engine mount propeller battery exhaust firewall and rescue system Check tightening and securing of hardware 3 Fu...

Страница 19: ...ubricate all moving parts see e plan 11 Check all hinges of control surfaces and moving parts Perform repair action if free movement in hinge exceed 0 4 mm The free play in hinge of horizontal tail should not exceed 0 1 mm Assembly all dismantled parts after performed inspection and or maintenance and perform engine test run 8 3 3 Lubricating plan a Lubricant used Use suitable lubricating grease C...

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