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25

O

WNER

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F

LIGHT

M

ANUAL

24

XL

Pilot Experience Requirements

Pilot Checkout

There is no such thing as a minimum number of total hours a

pilot should have to be qualified for checkout solo in a new air-
craft.The best pilot qualification is variety. He should be current in
more than one type of airplane.The Velocity is not difficult to fly,
but it is DIFFERENT: like a Yankee is different from a Cessna, or a
Cub is different from a Cherokee. A pilot who is used to the dif-
ferences between a Cessna and a Cub is ready to adapt to the dif-
ferences in a Velocity.The Velocity has entirely conventional flying
qualities. However, its responsiveness is quicker and its landing
speed is faster than most light training aircraft. It should not be
considered as a training airplane to develop basic flight proficien-
cy.The Velocity ranks with the best tricycle-geared types for
ground stability and has none of the ground-looping tendencies of
the taildraggers.

The requirement for a variety of experience applies to check-

out in any type of new aircraft, not only to Velocity. Velocity has
never experienced a problem in checking out a new Velocity pilot.
We always follow the criteria listed here for initial pilot checkout
and strongly recommend that you do:
1. Checkout should not be done in gusty winds, particularly
crosswind conditions.
2. Use runway at least 3500 ft. long for initial checkouts.The
beginning Velocity pilot often finds himself fast on approach and
the airplane is so clean that it is easy to use up a lot of runway in
the flare.
3. Give the potential pilot a copilot ride or two.This gives him a
first-hand look at the aircraft’s performance envelope and general
flying qualities.Trim the airplane up and let him “fly” it from the
right seat by leaning back and forth.This will give him an apprecia-
tion of the airplaneís 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 unless he flies the aircraft
smoothly and confidently from the right seat. Do not have him fly
solo on his first flights until he has the hang of it.
5. Weight and balance must be in the first flight box.
6. Briefing must emphasize that the aircraft should never be
rotated past the angle that places the canard on the horizon for
takeoff or landing.
7. Pilot being checked out must have a minimum of 10 hours
each in at least two type aircraft in the last 4 months (5 in the last
30 days) and feel competent and comfortable in them during mar-
ginal conditions, such as crosswind landings near demonstrated
limits, etc.

Initially some of the pilots checked out by Velocity tended to

do the following on their first takeoff: immediately after liftoff,
they would level off or descend, then re-establish a normal climb.
We have found that this is caused by the unusual visual cue pro-
vided by the canard wing. Even though the climb angle is similar to
other light planes, the canard wing gives the pilot the impression
that he has over-rotated. Since we found this was the cause, we
have told pilots the following and have found that the pitch “bob-
ble” no longer occurs: rotate smoothly to liftoff at 75 knots. If
you think you have over-rotated, do not overreact; do not shove
the stick forward. Hold the liftoff attitude and the airplane will
accelerate to 85 knots for climb.

Occasionally, a new Velocity pilot will tend to make a “full stall”

landing or flare too high.Tell him that if he has made the approach
at the correct speed and pulls power to idle before the flare, he
should not spend a lot of time in the flare. Make a complete flare,
then fly the airplane down onto the runway with finesse. Once
the main wheels make contact, continue to fly the canard and
lower the nose when speed allows.

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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