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First Flight Operations

On the first flight day, only the necessary personnel will be present.  No spectators of any sort 

unless they are incidental and not in the area.  There should be a ground crew with a vehicle 

capable of tending to the aircraft should it go down, this includes a fire extinguisher and plans 

to get to the nearest hospital.  They should be watching for incoming traffic and alerting the pilot 

by visual signals when other aircraft are in the area (in case there is no radio communication 

between aircraft on the ground and/or in the air).  Needless to say a thorough preflight inspec-

tion should be done by at least one rated pilot in addition to the test pilot.  It is easy in such an 

emotional situation for one person to overlook something.  Spend a few hours driving around the 

surrounding area or survey with another aircraft, identify your alternative landing sites in case of 

failure.

After initial warmup on the first flight day, several taxi tests will be conducted at intervals of 5mph 

from 30 up to 45 mph covering the range of minimum aerodynamically controllable speed to full 

flap stall speed.  As speed increases, tendencies should be noted, i.e. rolls to the right, to the 

left.  A tape recorder or video camera will be helpful but a lap board with secure pin will suffice.  

Taxi tests with and without flaps will be conducted.  It should take 10 runs the length of the run-

way to get a good feel of the aircraft.

Start with no flaps and at 30mph and work into full flaps at 45mph (the airplane may fly at this 

point).  Look for in advertent tendencies that indicate something way out of trim.  After taxi tests 

the following should be able to be corrected:

 

Align rudder with nose wheel if necessary

 

Add a preliminary rudder trim tube (be sure to test its effects)

 

Adjust the horizontal stab position if it is way off

 

Play with the ailerons and adjust the position of the stick if off-center

As I envision it, the plane rolls down the runway and reaches 30mph, then the throttle is cut back 

and adjusted until positive speed control can be achieved.  All the while the stick is held back 

somewhat to keep the nose light, but not off the ground.  After speed control is attained, the nose 

can be lifted and held high for the remainder of the run.  After this first run it is again repeated, 

this time adding the element of aileron control to determine effectiveness.  Easing into this nose 

high attitude with feathered throttle control will give the pilot a great deal of feel for the airplane’s 

control charcteristics.  This should be done next with one notch of flaps, then go back to no flaps 

and 35 mph, then 35 with flaps and so forth.  Prior to proceding to the next step, a flag or marker 

should be placed on the runway for the pilot to make the cutoff decision.  This is the point where 

if the aircraft is flying and power is cut, it can still stop safely (factor 2) before the end of the run-

way.

Make any and all adjustment that are possible at this point!  Refuel the airplane, do a complete 

preflight inspection (again) and go to the runway; this time with the intent of leaving the runway (if 

the aircraft became airborne before this point it should have been inadvertent and considered a 

minor mistake).  Ease the airplane into it’s minimum liftoff speed and add just a little more power 

to get airborne.  This should NOT be done in the nose high attitude used previously because 

the airplane may jump into the air and settle down hard.  Do it easy and gentle.  Keep the nose 

light but not excessively high.  Keep the airplane 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 further adjustments and continue with a 

couple more ‘crow hops’.  If there are no poor tendencies in the aircraft rigging you can continue 

up to 100 feet or more, so long as a healthy safety margin is maintained with respect to the end 

of the runway.  Now is NOT the time to decide to fly a full pattern unless an emergency would 

otherwise merit such action!  With the information from crow hops you will be able to make bet-

ter decisions with the full flight should an emergency occur, such as gliding distance, lost power 

procedure.  It is important to note that smooth throttle inputs should be used during this crow 

hop procedure.  Pay attention to the moment created by the propeller.  I already experienced this 

today and just realized what happened!  I had the nose high with moderate stick pressure, cut 

the power and with great ease I was able to keep the nose up (because the thrust was no longer 

imparting a nose-down moment to the aircraft!

And now it is the pilots decision and the pilots decision only wether or not to continue.  The 

whole procedure can continue on another day with only minimal setback.  Just come back tomor-

row, warm it up, do a little taxing to get in the groove and you will soon be flying.  This time off 

could give you a fresh perspective and keep an otherwise overlooked problem seem trivial.

Take the aircraft to the hanger, inspect it AGAIN and re-fuel it.  The next time it leaves the run-

way is likely to be for an hour or more and it is not prudent to decide to do so with anything less 

than full tanks.

When you have made the decision to fly, be sure to have a good plan.  Start with the most run-

way remaining and do a high performance take off.  You want to climb to a reasonable altitude 

as soon as possible.  Keep your alternatives in mind.  Climb to pattern altitude, watch the engine 

closely and try to focus on keeping the aircraft in moderate control.  There may be rigging prob-

lems that require constant stick forces but these should not cause departure from controlled flight 

but rather represent something that needs to be corrected on the ground.  If it is severe, land 

and fix it before continuing with the stresses of such a physically demanding airplane.  If pos-

sible, continue with the flight to gain as much rigging information as possible.  The idea of this 

first flight is to become familiar with the power characteristics of the engine and the rigging of 

the airframe.  Beyond that, do not push the limits of airspeed, loading or maneuvering!!  Just get 

comfortable with the pattern first and if all is well, leave the pattern for a close-by field for a few 

circuits.  Try releasing the stick and making notes about how the plane flies.  Work in a notch of 

flaps to see if they cause any roll moment when actuated.  Play with the elevator trim, use the 

ball and the string to get an idea of the straightness of the aircraft.  Land the airplane unevent-

fully after 1 hour of flight or sooner if required.

Make adjustements to the airframe and powerplant, inspect everything closely, retorque the prop 

and so forth and continue with flight two which should focus on the pilot becoming familiar with a 

few of the finer points of rigging.  This flight should be a repeat of the first flight.  It will be surpris-

ing how much is missed on flight one.

Taxi tests, first flight and second flight will take an 8 hour day if there is much rigging changes to 

be made so keep this in mind!  With respect to all flights after the first two, I have not yet envi-

sioned them and will do so in the near future!  -KRO

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Содержание S-12

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 33: ...PAGE 33...

Страница 34: ...PAGE 34...

Страница 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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