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check, return the throttle to idle.  Each of the 4 cylinders in the engine has 2 spark plugs.  One 

ignition circuit controls one spark plug in each cylinder.  Two ignition systems increase the 

efficiency of the combustion (as evidenced by an RPM drop when you turn off one ignition 

switch) and secondarily provide a redundancy feature that if one circuit should fail, there is a 

second system to provide adequate power to land the airplane.

Using the Parking Brake Valve

The parking brake valve, if closed while the brakes are held on, will maintain better stop-

ping power than using the brakes alone.  This is because most of the hydraulic energy lost in 

this particular brake system is due to the flexure of the plastic brake line.  While holding the 

brakes on hard, switch the valve to the closed position and release the brakes with your feet.  

Now the length of brake line holding hydraulic pressure is cut approximately in half, increas-

ing stopping power.  This technique should be employed for short field takeoffs and landings 

where stopping power is critical.  It is also recommended for run-up procedure when checking 

magneto operation (the engine generates an enormous amount of thrust at mag-check RPM 

of 3750).  Although when the valve is closed, it does allow you to apply brakes, it is recom-

mended to hold the brakes on, then close the valve.  Due to the ease with which the parking 

brake valve can be closed and open, it must remain an item on all checklists.  It is not wise to 

takeoff or land when the valve is closed.  When taxiing, use the brakes as little as possible and 

avoid using them lightly for extended periods, it is better to brake hard for a short period than 

to ride them lightly.  If the situation ever becomes critical, cut the engine power and as soon as 

the aircraft is slow enough, put the airplane off the runway on the grass, there the rolling resis-

tance is greatly increased.

High Wind Taxi Methods

Taxiing in high winds and operating on the runway with high crosswinds is no laughing mat-

ter.  This is a very light aircraft and can be quite easily tipped over of thrown about by wind.  

Taxi with the utmost care in control orientation and always fly with authority and decisiveness 

when in high crosswinds.  Once the airplane starts to tip over there is little you can do to stop 

it.  If necessary, treat low wind or no wind days like high wind days.  If you create the habit of 

continuously correcting for wind on the ground, you will likely be much safer when the winds 

do come.  Take the time to create a chart for yourself showing control orientation for each type 

of cross wind (quartering from the front, quartering from the rear, head on, tail wind, direct 

crosswind).  Remember that wind blowing backwards across the control surfaces (quartering 

tailwind) causes them to work in reverse of what they normally do.

Take-Off Overview

For take-off it is important for you to remember a few things.  First of all, if you loose 

power in a high angle climb with full flaps or even 2 notches of flaps, you will have to 

IMMEDIATELY put in a large amount of nose down control inputs to maintain airspeed.  It 

is easy to hesitate for a second or two and in this time your airplane can go from 70mph to 

30mph.  Second of all, you should treat the nose gear gently.  Use a generous amount of eleva-

tor control to get the weight off the nosewheel as soon as possible, this also keeps the wheel 

from spinning any faster than necessary and minimizes vibration.  The nose will come off the 

ground at 35mph with full throttle; with the throttle at idle, it is possible to hold the nose up at 

25 to 30mph.  This also keeps the rotational speed down for the large front wheel which is not 

in perfect balance.  In high crosswind operations, you may have to compromise a bit and keep 

some weight on the nose for steering until you attain enough airspeed to keep the plane aligned 

with the runway.

Take-Off Procedure

Be sure your take-off checklist is complete, add power smoothly and hold a large amount of 

back stick until you feel the nosewheel come off the ground.  Keep reducing back pressure as 

the airspeed increases so that the nosewheel remains 4-5 inches off the ground.  If you keep 

the nosewheel off the ground you will be able to easily feel when the plane is ready to fly.  Be 

careful not to pull up too hard and scrape the tail skid on the ground.  Climb the first 50 or 100 

feet at 65mph unless you need to clear an obstacle, in which case use the best angle of climb 

speed.  After reaching 150 feet, ease out the flaps (if used) and continue the climb to your 

cruise altitude.  Always observe the maximum flap extension speed on takeoff and landing.  

If the flap lever is difficult to pull, it is because there is too much wind pressure on the flaps.  

Push the nose over and reduce the throttle to cruise.  When adjusting the power setting, do so 

in a slow and even manner.  If you treat the engine with respect, it will respond when you ask 

it to.  However if you rev the motor recklessly with rapid and erratic power settings, it will 

likely develop abnormal wear qualities.

Just As You Leave the Ground

As soon as you are off the ground, tap the brakes and stop the mains from spinning, you may 

notice a considerable amount of shaking if they are spinning fast.  Liftoff speed at gross weight 

and two notches of flaps is approximately 40mph indicated airspeed.  Continue your climb at 

Vx or Vy as required.

Engine/Throttle Usage

The airplane can be held in a climb attitude at full power setting for as long as 5 minutes.  

After this period of time you should allow for a short rest period or reduce the power of 

your climb.  The engine is not meant to run at full power indefinitely.  Also, if you are in a 

prolonged decent it is wise to periodically add power for a few seconds to clear the motor 

of excessive fuel build-up and provide a chance for increased circulation of fluids.  Be par-

ticularly careful after idling the engine for a minute or so on final approach and then adding 

power for a go-around, give the engine a moment to respond to the first 1/4” of throttle input.  

Another important aspect of the aircraft is it’s excess power.  With the exception of steep 

climbs, no matter what attitude the airplane is in, it is possible to quickly exceed 75mph.  The 

throttle in this aircraft becomes just as important as any of the other controls when maneuver-

ing and typically the airplane responds very rapidly to throttle inputs.

Cowl Flaps

This airplane does not have cowl flaps but there is something to be said on this subject.  After 

the initial flight test period and when the weather turned cold, the typical in flight engine 

parameters started running too low.  This is because of the highly effective radiator and the 

exposed mounting configuration of the engine.  If the aircraft is operated in cold weather, the 

radiator inlet should be blocked either partially or completely.  A completely blocked radia-

tor inlet in operational weather of 30 degrees F will yield engine temperatures that are on the 

verge of too cool.  If you discover the engine running too cool (out of the green) in flight, 

descend to a lower altitude and continue to the nearest point where you can land to cover up 

the inlet to the radiator.  Running the engine at low temperatures is not healthy.

Rudder Usage

The rudder is trimmed for most normal flight conditions, however in a low airspeed high 

power setting configuration, the aircraft will require a little more right rudder pressure.  In 

PAGE 6

Summary of Contents for S-12

Page 1: ...omposite 3 blade Gear Reduction 1 2 27 Fuel G P H 4 1 gal 80 PERFORMANCE 0 MSL Take Off Roll 285 ft Rate of Climb 900 fpm Service Ceiling 14 000 ft Cruise 75 mph VNE 100 mph Stall Clean 42 mph Stall F...

Page 2: ...typographical fixes included Table of Contents Chapter 1 Familiarization Page 3 Learn the basic configuration and behavior of the airplane as well as the most impor tant operating rules regarding oper...

Page 3: ...approach The unwary pilot adding full power from an idle power setting at very low altitude and low airspeed will notice a very high stick force required to keep the nose in a climb attitude This air...

Page 4: ...ve himself 750 feet of runway If all conditions are in the pilots favor pilot skill sea level 15mph headwind solo pilot smooth runway no obstacles then 200 feet of runway can suffice for takeoff and 3...

Page 5: ...istry on behalf of the pilot to get a stubborn engine to idle when cold The starting carburetor sends a specific fuel air mixture to the engine which lets it run when cold it is only set for a conditi...

Page 6: ...d down for the large front wheel which is not in perfect balance In high crosswind operations you may have to compromise a bit and keep some weight on the nose for steering until you attain enough air...

Page 7: ...t pre heat time for the engine to warm up if you shut it off during flight in cold weather Emergency Procedures Off Field Emergency Landings In the case of an engine that will not start in flight firs...

Page 8: ...ht turn at 65mph indicated airspeed the outside wing is traveling significantly faster than the inside wing and as a result has more lift The remedy is to use a slight amount of opposite aileron The e...

Page 9: ...sewheel For example after touchdown on a rough field it is better to taxi the remaining distance required at 30mph with the nose off the ground than it is to taxi at 5mph with the nose on the ground I...

Page 10: ...in optional in Weight Arm Moment If combined pilot and passenger weight are between 108 and 345 pounds that CG will be acceptable regardless of fuel conditions However flying at the aft CG limit requi...

Page 11: ...nger by moving horizontally from total weight to the pilot passenger line then read down to moment Find fuel pounds and moment by reading along the fuel line to the total fuel on board in gallons read...

Page 12: ...assembly to the floor pan produce undue force and may eventually cause failure of the mounting tabs or other associated hardware This entire sub system should be inspected under load to ensure it s in...

Page 13: ...rectly near holes and joints and so forth the water will find it s way out of the plane After washing the aircraft a good automotive wax will help protect the airplane from the elements A good wax to...

Page 14: ...er tube to the bottom of the oil tank thru the dipstick hole Pump out all oil possible approximately 66 gallons Remove the oil filter carefully avoiding any excessive spills by placing rags underneath...

Page 15: ...llowing satisfactory completion of the required number of flight hours in the flight test area the pilot shall certify in the logbook that the aircraft has been shown to comply with FAR Section 91 319...

Page 16: ...74 www vdona com PS Engineering Inc 9800 Martel Road Lenoir City Tennessee 37772 423 988 9800 FAX 423 988 6619 www ps engineering com PM501 Intercom S N XA 07690 Ameri King Corporation 18842 Brookhurs...

Page 17: ...racks bends bolts lubricated Battery secure pins cracks wiring Pitot Static clear REMOVE COVER Left Fuselage Lexan scratches cracks Structure rivets Doors hinges handles Left Main Gear Leg cracks bend...

Page 18: ...00RPM Engine Start hot Choke OFF Throttle IDLE Area CLEAR Ignition BOTH Brakes ON Starter ENGAGE Oil PRESSURE Engine Warmup 2 minutes 2000RPM Continue 2500RPM Oil Temp 120F Taxi Checklist Brakes CHECK...

Page 19: ...gap oOil system integrity ooil coloration and age 50 hrs ooil quantity olines routed without interference and free of chaffing ooil overflow line routing and condition oconnections for tightness ooil...

Page 20: ...ts operating handbook with current weight and balance is on board the aircraft oinstru ment panel for structural integrity opitot and static tubes for cleanliness and line routing conflicts or chafing...

Page 21: ...ity 18 Gal Sight Gauge Markings Total Fuel On board 7 6 3 8 11 4 Full Capacity 18 Gal Sight Gauge Markings Total Fuel On board 7 6 3 8 11 4 SPINS PROHIBITED Amateur Built Aircraft This airplane is ama...

Page 22: ...gun voltmeter optical tachometer camera and or video camera feeler gauges spark plug gapping tool plastic brush floor jack antifreeze concentration checker Consumables paper filters paper towels rags...

Page 23: ...ufficient flaps roll tendencies wing washout wing high or low rudder and vertical stabilizer ball position wings level horizontal stabilizer stick position in trimmed flight prop pitch adjustments rev...

Page 24: ...ne within 10 feet of the ground or less preferably just a few feet and continually watch for the end of the runway Make any notes regarding the rigging of the aircraft after you stop the airplane Make...

Page 25: ...r this flight attitude What is the yaw tendency of the aircraft What is the roll tendency of the aircraft What other tendencies does the aircraft have Release the ailerons and use the rudder pedals to...

Page 26: ...e rudder pedals Use the controls to maintain straight and level at this setting What rudder input is required for straight and level What aileron input is required for straight and level What other te...

Page 27: ...do you expect What is the wind direction and speed What is the outside air temperature High performance takeoff Take out all flaps Climb at 65mph Continue climb to 1500AGL 4500MSL and to a nearby fie...

Page 28: ...ncy of the aircraft What other tendencies does the aircraft have Control the airplane in a straight and level attitude at this air speed Release the controls Does the airplane YAW first or ROLL first...

Page 29: ...ps Reduce power to enter slow flight near Vs0 What is the airspeed What is the RPM What tendencies does the aircraft have Add 2nd notch of flaps Reduce power to enter slow flight near Vs1 What is the...

Page 30: ...l for the follwing No flaps 1 Notch 2 Notches 3 Notches What tendencies What is the power on climbing stall speed for the following No flaps 1 Notch 2 Notches 3 Notches What tendencies What is the pow...

Page 31: ...gather during other flight tests i e with 10mph wind etc Lift and Drag performance Ratios Power on and off Climb for 1 minute and record the VSI reading along with actual altimeter readings at start...

Page 32: ...procedure What are the dangers What are the parameters FPM airspeed etc Lazy Eights What is the procedure What are the parameters altitude loss speed etc What are the dangers Chandelles What is the p...

Page 33: ...PAGE 33...

Page 34: ...PAGE 34...

Page 35: ...Weight lbs Pilot and Passenger 49 in Aft Fuel 6 lb gal 78 in aft 1 8 g a l 1 0 5 reposition group to lower left at 1 1 1 120 1 090 1 060 1 030 970 940 910 880 820 790 760 730 1 150 1 000 850 700 83 8...

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