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O

WNER

S

F

LIGHT

M

ANUAL

51

50

XL

of trim direction, if the airplane needs adjustment.You will notice
a small roll trim change when you reduce the power.The airplane
will require more right trim with power off. Limit your first flight
to feeling out roll, pitch and yaw responses and checking engine
operation, temperatures, pressures, etc. Make your approach at 80
knots. Have a fast touch down (75-80 knots), leaving full stall
landings for later in the test program.

After this first flight make a thorough systems check, clean and

flush the fuel filter, electric fuel pump screen, and carb screen.Also
remove and clean out carb float bowl. Check float needle valve
and seat for cleanliness on carburated engine.

Envelope Expansion

With first flight completed and any squawks resolved, you are

ready to expand your flight envelope. Do not promptly charge out
and test fly your aircraft at the extreme CG position and weights.
Expand your envelope in small increments. Remember, you have
to spend 40 hours in your test area, so put the time to good use
and do a professional job of flight testing. Before expanding the
weight and CG range shown for initial testing, spend a few hours
and become thoroughly comfortable in your piloting tasks.When
you feel at home in the airplane, begin your expansion of the
weight, CG position, load factor and airspeed ranges. Don’t feel
obliged to expand into the full ranges shown in the plans and in
this handbook. Expand your limitations slowly, and if you reach a
point that you feel uncomfortable, stop.The ranges shown are
those demonstrated by the designer. Feel free to restrict your air-
plane as you determine in your own testing; just don’t exceed the
design limits shown.

Do not assume that your aircraft will fly exactly the same as

N97XL. Minor homebuilder construction tolerances can effect fly-
ing qualities and performance; for example, your aircraft may
exhibit less or more stall margin.As with any aircraft, completely
determine your 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 rudders can both be deployed simultaneously and the
pilot should be careful not to inadvertently do this in flight.

There are two differences in a Velocity that must be thorough-

ly understood prior to flight:
1. The non-standard rudder pedals: Be sure not to inadvertently
deploy both rudders at the same time in flight. If this happens, one
will usually be out more than the other, producing unwanted yaw.
The Velocity rudders are quite effective.Adjust the pedals so your
foot does not press the pedals naturally.
2. Pitch over-controlling: The novice pilot will expect the
Velocity to handle like the C-150, or whatever he last flew.The
experienced pilot knows that J-3 Cubs and Bonanzas handle dif-
ferently and will make the transition easily. Spend enough time on
the runway just above rotation speed but below lift off speed and
practice controlling pitch so you can put and hold the desired/
selected pitch proficiently. Hold the forearm on the arm rest and
control pitch with the wrist only. Do not over-rotate! The highest
rotation you should see during this or the later flights is the
canard up to, but never above, the horizon. Better yet, keep it
always at least 2° below the horizon.

Remember the first flight of your aircraft is just one baby step

up from the lift off that you’ve just completed and is just the bare
beginning of your flight test program. First flight should again be
made under ideal weather conditions.The weight and CG position
should be within the limited envelope for “first flight box”. First
flight is not intended to demonstrate the capability of your air-
craft or of the pilot and should be flown very conservatively.
Leave the gear down and give yourself one less thing to worry
about. Limit your airspeed to a range of from 80 knots to 130
knots. Stay over the airport and resist the urge to buzz your
observers. During your climb out, set your pitch and roll trims to
trim the airplane for hands-off flight.This will be a handy reminder

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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