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O

WNER

S

F

LIGHT

M

ANUAL

47

46

XL

to check out your engine system thoroughly. Ground run it for an
hour or so at low to medium power. Run it with the top cowling
off and look for excessive vibration, unsafetied hardware, leaky
fuel lines, or anything else unpleasant.After this initial run-in peri-
od (or the manufacturer’s recommended run-in for new or over-
hauled engines), check everything over very carefully. Recheck the
exhaust nuts for torque, look for leaks around gaskets, loose
clamps, check fit of cowling baffles, etc. Check everything thor-
oughly before you button up the cowling to begin taxi tests. Be
sure the engine compartment is clean. Check for nuts, washers,
bits of safety wire, etc., because in a pusher everything that comes
off goes right through the prop.

Low Speed Taxi

For fixed gear aircraft, make all initial taxi/runway flights 

WITH

-

OUT

wheel pants for better brake cooling.

Low speed taxi is defined as that slower than required to lift

the nose wheel off the ground - 45 knots. Spend at least a full
hour doing low speed taxi to fully familiarize yourself with the
cockpit environment and to thoroughly check the engine, brakes,
controls, landing gear, etc.

Thirty five knots is sufficient speed to evaluate rudder steering

and brake effectiveness.You may find that 

EXTENSIVE TAXIING CAN

OVERHEAT THE BRAKES

.At 35 knots you will note that the sloppy feel

of the control stick is gone and airloads now provide a comfort-
able centering feel.

Now is the time for the final FAA inspection and issuance of

your airworthiness certificate. The necessary inspections by the
FAA must be done prior to any flight testing!  Be sure you have
complied with all pertinent FAA regulations. Refer to FAA
Advisory Circular AC # 20-27D for the details (Display of N-
numbers, warning & ID plates, etc.)  AC #20-27D is a must to
have prior to calling for an FAA inspection. Be sure all the paper
work is done!

“homebuilder syndrome”, give the only key to your bird to a close
friend (preferably one who really likes you and to whom you owe
money) and give the absolute authority to say “go” or “no go” to
your initial flight tests.With all the other things you are thinking
about, it is best to give the decision of whether the airplane is
ready to someone else. If you really get a bad case of “home-
builder syndrome”, your friendship may be strained somewhat,
but you will be able to make up after you have tested your new
bird safely.

The “homebuilder syndrome” has been a major factor in many

first-flight accidents.Typical of this problem is where an individual
spends all his time and money building his airplane, and, for several
years, lets his flying proficiency lapse.Very typically we find a fin-
ished homebuilt with the owner/pilot seriously lacking in pilot
proficiency. In one case, the pilot who tried to fly the first flight on
his homebuilt had only one flight in the last two years! Another
problem surfaces about the time the aircraft is ready to fly:
“EGO” – that is,“I built the machine, I’ll fly it.After all, who knows
more about my machine than me...I built it.” The homebuilder is
understandably proud of his creation and becomes very posses-
sive. So we find the proud builder/pilot at the end of the runway,
“ready” for takeoff, with possibly a bad case of “homebuilder syn-
drome”. But he will not know it until just after liftoff, when he
finds himself suddenly thrust into an environment he is ill pre-
pared to handle.

The best remedy for “homebuilder syndrome” is to accept

help on your flight testing from an experienced Velocity or Long
EZ pilot.Then get a good checkout from him after you meet the
currency requirements.

Ground Testing

Do not just race out and fly your airplane first thing.You will

spend a while checking out all of your systems on the ground
before you leap off on the first flight.The first order of business is

Summary of Contents for XL RG

Page 1: ......

Page 2: ...bic feet of baggage room This area can also be used for added fuel to bring the total to over 90 gallons The design load factors of theVelocity are 9 G s 7 G s with a tested airframe load of 6 G s The...

Page 3: ...e lightweight MT CS wood propellers are currently approved Turbo charging and variable pitch metal propellers are not recommended until factory testing can confirm there safe use Extensive development...

Page 4: ...the side stick and two rudder pedals for yaw The side stick controller is employed to give the pilot the smallest workload control arrange ment possible The rudders located on the winglets at the wing...

Page 5: ...al Apply full throttle smoothly As the aircraft accelerates use rudder and brake as necessary for directional control Maintain slight aft stick pressure as you accelerate to relieve the nose wheel Rot...

Page 6: ...11 OWNER S FLIGHT MANUAL 10 XL NOTE This must be a re settable pullable breaker if alternator does not require a field wire...

Page 7: ...ed Do not try to jerk the aircraft off prematurely this only places the prop closer to the ground and increases the chance of damage High Density Altitude At density altitudes above 5000 ft follow the...

Page 8: ...ventional aircraft of gargantuan proportions like Cessna 150 s and may ignore you completely Best pattern speed is 85 to 90 knots slowing to 80 knots on final approach 85 to 90 in turbu lence or gusty...

Page 9: ...ude one to two degrees and about one half to one bucks per second If the full aft stick is relieved during exaggerated cross control and slow flight Third with the majority of the fuselage being forwa...

Page 10: ...h high sink rate If any of your aft cg characteris tics are undesirable adjust your cg limit forward accordingly XL Emergency Procedures FIRE There are normally only two sources of aircraft fires elec...

Page 11: ...ils to retract or extend when the gear switch is placed in the respective position the pump does not run the first thing to do is to position the gear switch in the down position and push the momentar...

Page 12: ...Slow deceleration Accelerated Stall 110 knots 126 mph Intentional spins are not permitted Engine Limitations Lycoming IO540 RPM 2700 max CHT 475 max 435 continuous Oil Temp 245 max 180 200 desired Oi...

Page 13: ...will give him an apprecia tion of the airplane s sensitivity Show him the use of the trim sys tems pitch and roll Let him get used to the pitch and roll feel Do not transition him to the left seat unl...

Page 14: ...and canard incidence jigs Water level or a good 6 8 level Step 1 Leveling the aircraft Locate a cement floor that is as flat and level as possible The aircraft must be level for the procedure so you w...

Page 15: ...umb bob some 2 masking tape and a sharp point marker pen The tape goes on the floor to receive the mark from the plumb bob as well as the iden tification marks Record measurements for all those indica...

Page 16: ...Right Main Wheel Weight with Full Fuel Combined Total Weight with Full Fuel This information is needed to calculate the FUEL ARM for your Velocity STEP 7 Establish the Static CG of your aircraft Here...

Page 17: ...e difference of the moments by the difference of the weights the pilot weight and the result will be the Pilot co pilot ARM 14884 8 inch lbs _______________ 80 45 aft of datum 185 lbs Repeat this proc...

Page 18: ...d Once all the known information is entered make some extra photocopies Know go ahead and figure in some weight and balance examples for your aircraft just like we did in the previous sample You must...

Page 19: ...Ballast nose TOTAL MAXIMUM ACTUAL Gross Weight Useful Load C G SAMPLE ONLY Velocity XL Fuel Weight ARM Aft Moment Gallons LBS Datum Inches in lbs Basic Empty 1 6 4 0 141 63 232273 20 Sump Tank Fuel 6...

Page 20: ...s inducing a stall in the canard first If either one or both of these rules are broken the result will be an extremely dangerous aircraft So always operate your aircraft within the prescribed CG box T...

Page 21: ...mass balance level to 10 nose down Check for 1 16 minimum clearances around all mass bal established by the factory If you add accessories to your airframe in the future the prop er procedure is to we...

Page 22: ...nd bal ance data kept aboard the airplane see weight balance section When loading the aircraft for the initial flight testing and for initial pilot checkouts it is important that the weight and CG fal...

Page 23: ...ss weight for takeoff of 5 may be used but only under the following limitations 1 Taxi and takeoff only on smooth hard surface 2 Maximum landing weight limited to 2700 lbs 3 Maneuvers limited to norma...

Page 24: ...to have prior to calling for an FAA inspection Be sure all the paper work is done homebuilder syndrome give the only key to your bird to a close friend preferably one who really likes you and to whom...

Page 25: ...Velocity does not fly like a Cessna 150 or some other sluggish trainer TheVelocity is a high performance responsive air High SpeedTaxi and Nose Wheel Liftoffs Before conducting the following tests wit...

Page 26: ...our stall characteristics at a safe altitude then operate craft with differences It has a side stick and the pilot should keep his forearm on the arm rest and use his wrist to control pitch Also the r...

Page 27: ...unresolved find and fix prob lems as you encounter them Airplanes usually give a hint of impending trouble The problem is we pilots do not always listen If something changes a slight roughness vibrat...

Page 28: ...c ignition w 1 mag then Electronic ignition off Hand prop engine Both mags on if Electronic ignition w 1 mag then Electronic ignition on Tires check wear and inflation Cooling Engine Inlet clear Drain...

Page 29: ...y resistant to damage or fatigue If the structure is damaged it will show up as a crack in the paint The strain characteristics of the material are such that it cannot fail internally without first fa...

Page 30: ...aint or wrinkle in the skin remove the paint around the crack by sand ing and inspect the glass structure Do not use enamel or lacquer paint remover If the glass structure is damaged it will have a wh...

Page 31: ...The aircraft should be reweighed at the first annual You may be surprised Update the weight and balance form Reweigh every 3 years or after any major modification Main Wheel Bearings Repack Air filter...

Page 32: ...air vents 18 Inspect all radios and avionics for operation and condition 19 Inspect cabin door latches for operation and condition 5 Inspect and clean the suction screen 6 Replace oil filter and insp...

Page 33: ...ons H Operational Checks 1 Check fuel pump and selector 20 Inspect wet compass for calibration card and security D Fuselage and Canard Group 1 Inspect battery for security 2 Service battery with water...

Page 34: ...prop 14 Check engine idle speed 15 Check electronic equipment operation 16 Check operation of all lighting interior exterior I General 1 After shut down check for oil fuel leaks 2 Check aircraft docu...

Page 35: ...____________ ______________________________ ______________________________ ______________________________ ______________________________ ______________________________ ______________________________ _...

Page 36: ...INC 200 West Airport Road Sebastian FL 32958 Ph 561 589 1860 Fax 561 589 1893 www VelocityAircraft com Owner s Flight Manual Weight Balance XL Series Aircraft...

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