background image

O

WNER

S

F

LIGHT

M

ANUAL

49

48

XL

speed to be thoroughly proficient/ comfortable with the unique
Velocity rudder system.There should be no tendency for the pilot
to inadvertently push/deploy both rudders at the same time,
unless during braking.

Next step is to practice speed control before attempting nose

wheel lift offs. It is important to be able to control speed accu-
rately so as not to get airborne inadvertently.You will find that
once a speed is attained it takes VERY LITTLE power to maintain
it. Practice accelerating to and maintaining different target speeds.
(30, 40, 50, 60 knots) Do not rotate.

You will find that once the target speed is reached you must

reduce power to idle or just a “hair” above to keep from exceed-
ing it. Be proficient and comfortable in holding speed before mov-
ing onto nose wheel liftoffs.The aircraft will rotate at different
speeds depending on gross weight and center of gravity.To deter-
mine rotation speed, accelerate to 50 knots, set power to main-
tain speed (close to idle), then attempt to rotate. If 50 knots is
too slow to rotate, then go back to the start and try 55 knots,
etc. Find the speed that will just rotate the nose (about 60 knots),
reduce power to near idle and practice holding the nose at a pre-
determined position. Be careful to not over-rotate.Always keep
the canard well below the horizon.The pilot should not allow the
aircraft to exceed 65 knots or rotate to a point of becoming air-
borne during this exercise.

When you’ve done enough runs down the runway so that you

can comfortably, smoothly and precisely control speed, pitch and
yaw with the nose wheel off the ground, you should be ready for
the first flight.

First Flight

You should be proficient in rudder operations and positive

control of pitch control and are ready for the “big one”. But be
sure you review and understand the following.

The Velocity does not fly like a Cessna 150 or some other

sluggish trainer.The Velocity is a high performance, responsive air-

High Speed Taxi and Nose Wheel Liftoffs

Before conducting the following tests with your new Velocity,

do all of them first with two other different airplanes in which
you are proficient.These maneuvers (nosewheel liftoffs at low
power) are a little strange at the average pilot. Doing them in a
familiar airplane takes the strangeness out of the maneuver and
better prepares you to do them in a new airplane. It also gives
you a first-hand look at runway length requirements and wind
conditions.

Some of the following requirements and procedures may

seem excessive.This is not due to any special feature of the
Velocity; we feel they should be required of any homebuilt during
their initial testing.The safety record of homebuilts during first
flights is not as good as it could be if the owners and pilots would
follow the following cautious procedures during initial testing.

• Weather - wind calm or smooth wind straight down the

runway. Smooth air - check turbulence in another airplane.

• Runway - at least 3500 ft., preferably over 4000 ft
• Fuel - 10 gallon each side
• Pilot - see pilot experience requirements for absolute min-

imum criteria. Do not test fly a new airplane while fatigued:
go home, get some dinner, sleep; you are more alert in the
morning.

The reason for the long runway requirement is to allow you

to do nosewheel lift-offs and decelerations without concern for
stopping distance or 

BRAKE HEATING

.The air must be smooth and

without crosswind. Be sure you removed your wheel pants. Set
the pitch trim for takeoff. Set neutral roll trim.

The purpose of this phase of testing is to evaluate the air-

craft’s performance and trim during high speed taxi/nose wheel
liftoffs, to acquaint the pilot with the pitch and yaw characteristics
of the Velocity, and, most importantly, to give him the correct visu-
al cue of zero height to allow him to judge flare height on his first
landing.The pilot should spend enough time just below rotation

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...

Reviews: