P&M Aviation QUIK GT450 Скачать руководство пользователя страница 41

Quik & Quik GT450 Aircraft Operating Instructions 

 

 

29

th

 March 2007 

Issue 1 

 

Page 41 of 68 

 

 
 
Tuning turns   

Example

: The aircraft turns right at all speeds. The trim speed is correct. 

 
Solution

: In this case the tip turn adjusters. On the tips you will find an adjustment scale where 

the leading edge emerges from the sail.  Rotate the starboard tip plug  1mm on the scale anti-
clockwise (i.e. trailing edge down).  Check in flight.  If the turn persists, rotate the tip one further 
mm.    Check  fly.    Rotate  the  left  tip  1mm  anti-clockwise  (i.e.  trailing  edge  up).  Check  results 
before moving the tips further. 

 
 
 
 
 
 

 
 
 
 
 

Example

:  At  high  speed,  the  aircraft  turns  to  the  right.  At  low  speed,  the  turn  is  not  so 

pronounced. The trim speed is correct. 

 

 

 

Solution

:  Use  ribs  numbers  7-10  (the  tip  rib  is  number  11  and  has  very  little  effect)  on  the 

starboard  (right  wing)

  side  to  tune  out  the  turn.  The  tip  ribs  respond  well  to  “tab  effect”,  i.e. 

application of reflex near to the trailing edge will produce a downforce at the trailing edge which 
will increase the incidence of the section as a whole. The overall effect is to increase the lift on 
the side where reflex is applied, so correcting the turn. The effect becomes more pronounced as 
the  speed  rises.  The  reflex  should  be  applied  200mm  (8  inches)  from  the  trailing  edge  and 
applied  in  small  increments  up  to  a  maximum  of  25mm  (1  inch).    Start  with  10mm  (3/8  inch) 
reflex, test fly, then 15 - 20 - 25mm (5/8 - 3/4 - 1 inch) as required.  Do not exceed 25mm reflex! 

 
 

Example

: The wing flies completely straight sometimes, and turns to the right at other times! 

 

 

 

Solution

:  This  is  happily  an  easy  problem  to  solve,  since  it  usually  only  happens  when  you 

have  to rig  everytime you fly.   Then it is a question  of  exactly how  the  tension sets  up  on the 
outer  leading  edge  webbings.    Simply  take  hold  of  the  leading  edge  cloth  right  out  near  the 
trailing edge and twist it anti-clockwise; you should feel it move.  It will then be held there by the 
tension.  

 

 
 
Tuning in pitch 

The GT450 wing is designed to be stable in pitch even with the trimmer fully fast, at a trim speed of 73 - 80 
mph. The bar force when pulling in must steadily rise to at least 7kg (15 lbs) to achieve 95mph. 
 

 

The  electric  trimmer  applies  a  spring  nose-up  moment  to the wing  directly. In  the  fast  trim setting, the trim 
cord should be just slack with the bar fully in to the pilot’s chest. 
 

 

When making adjustments in pitch, always tune in smooth air and climb to test altitude with the trimmer set at 
60   mph,  before  winding  the  trimmer  gradually  to the test position.  The settling of the sail on the  airframe 
generally tends to slow the wing down and make it more stable both in pitch and laterally/directionally, as the 
washout increases. 
 

 

If  the  wing  has  slowed  unacceptably  with  the  trimmer  fully  fast,  then  the  tip  adjusters  can  be  rotated  both 
together  by  1mm  on  the  scale  so  as  to  bias  the  trailing  edges  downwards.  Check  the  result  at  each  1mm 
adjustment until the trim speed and pitch feel are correct.  Do not exceed 5mm of adjustment. 
 

 

As  a  rough  guide,  the  sail  should  ride  approximately  25mm (1  inch)  clear  of  the  washout  rods  when  flying 
solo at fast trim. 
 

 

If the trim speed is too fast and pitch feel too light at the fast trim setting, then the tips can  be rotated both 
upwards until the correct speed is set. Again, use small adjustments to achieve the desired result. If the wing 
is very new (less than 5hrs) then it will probably settle down by 4-5mph over the next 20hrs. 
 

 

Once the fast trim has been set, then the slow trim can be checked by winding to the full slow position. The 
slow trim will be 5 mph faster at maximum all-up weight than at minimum loading. 
 

 

Do  not  exceed  the  adjustment  range  which  is 
±6mm  (1/4  inch)  from  the  initial  factory  setting, 
or the aircraft may become unstable.

 

WARNING 

!

 

Содержание QUIK GT450

Страница 1: ...ting Instructions Issue 1 P M Aviation Ltd Unit B Crawford St Rochdale Lancashire OL16 5NU Great Britain Tel 44 0 1706 655134 Fax 44 0 1706 631561 E E M Ma ai il l f fl ly yi in ng g p pm ma av vi ia...

Страница 2: ...re flight Checks 21 4 5 Safety Harness 21 4 6 Ground Handling 21 4 7 Airstrip Criteria 21 4 8 Special Hazards 22 5 Pre flight Inspection 24 5 1 Wing 24 5 2 Trike 24 6 Preparation for Flight 26 6 1 Gen...

Страница 3: ...11 7 Secondary Structures and Systems Cockpit and Fairing 55 11 8 Secondary Structures and Systems Electrical System 55 11 9 Secondary Structures and Systems Carburettor Heat 55 11 10 Secondary Struct...

Страница 4: ...r personal safety the safety of others and the safe operation of the aircraft it is very important that this operator s manual is read in full before operating or flying the aircraft for the first tim...

Страница 5: ...TE This NOTE symbol indicates points of particular interest for more efficient and convenient operation This WARNING symbol identifies special instructions or procedures which if not correctly followe...

Страница 6: ...ch may make a particular item unsuitable for the use for which it was originally purchased He must also satisfy himself totally that a purchased item is suitable for the use to which he intends to emp...

Страница 7: ...ght pilot s licence syllabus to attain awareness of the mental and physical requirements necessary for flexwing Microlight operation To ensure a long and trouble free life from your Quik or Quik GT450...

Страница 8: ...etre sq ft Square Feet cu in Cubic Inches cm 3 Centimeter Cube mb Millibars N Newton Nm Newton Meter kW KiloWatt HP Horse Power RPM Revolutions Per Minute ft lbs Foot Pounds in lbs Inch Pounds psi Pou...

Страница 9: ...1 6 MPH Pressure PSI Pounds per Square Inch in Hg inches of Mercury mb millibar Distances in inches 25 4 millimeters ft foot feet 305 meters Weights Kg kilograms 2 2 lbs 2 2 pounds Misc 1 Pound Ib 0 4...

Страница 10: ...h The electric trim system gives precise fingertip control of hands off trim speeds from approximately 50 to 80 mph A roll augmentation system has been developed for the GT450 wing which actuates the...

Страница 11: ...Quik Quik GT450 Aircraft Operating Instructions 29th March 2007 Issue 1 Page 11 of 68 1 1 GENERAL ARRANGEMENT DRAWINGS...

Страница 12: ...Quik Quik GT450 Aircraft Operating Instructions 29th March 2007 Issue 1 Page 12 of 68...

Страница 13: ...s 4 4 Reduction ratio 2 27 1 2 43 1 Overload Clutch No Yes Fuel oil ratio n a n a Min fuel rating 95 RON 95 RON Prop manufacturer Warp Drive Warp Drive Prop type Warp Drive 1 72m 90mm parallel chord W...

Страница 14: ...t full power at less than 40mph 75kph 35kt Do not exceed more than 60 of bank ALL aerobatic manoeuvres including whipstalls wingovers tail slides loops rolls and spins are prohibited GENERAL LIMITATIO...

Страница 15: ...0kph 10kn 2 2 POWERPLANT LIMITATIONS Engine ROTAX 912 ROTAX 912S Max RPM 5800 5min 5800 5min Max continuous RPM 5500 5500 Idle RPM Approx 1400 Approx 1400 Min fuel spec Min RON 90 EN228 Premium EN228...

Страница 16: ...f temperature refer to the Engine Manual for appropriate oil viscosity See also engine operators manual and P M Service Bulletin 0094 for Rotax 912 912S especially if using AVGAS If any limitations ar...

Страница 17: ...erate the electric starter FORCED LANDING DRILL Throttles SHUT Both ignition switches OFF Fuel OFF Brakes OFF Harness secure do not over tighten pilots shoulder strap Plan approach Engine off Landings...

Страница 18: ...uch as the oil pressure gauge are also essential for flight safety If these basic instruments fail a landing should be made as soon as it is safe to do so In the case of an over voltage fault it may b...

Страница 19: ...h you intend to operate Air Law can vary from country to country and from state to state be sure to always fly within the letter of the Air Law that operates in your state or country Make sure you hav...

Страница 20: ...ee Section 10 3 Before each flight you should calculate the combined weight of the aircraft fuel pilot and passenger and ensure that it never exceeds 990lb 450 kilograms Fuel Before each flight you sh...

Страница 21: ...has been stopped the aircraft has been securely parked and picketed or hangared and the pilot and passenger have disembarked Do not make the mistake of losing concentration just because you have lande...

Страница 22: ...OM AHEAD IN CASE THE AIRCRAFT BREAKS FREE WHILE RUNNING UP 2 Check the ground around the propeller area for loose stones etc and remove any such objects 3 Tie the aircraft to a solid object a large an...

Страница 23: ...erly strapped in and with his her fingers on the ignition switches at all times when the engine is running 8 Maintain an adequate look out while conducting tests adults children animals may approach f...

Страница 24: ...rectly fitted Rigging tool detached and stowed 5 2 TRIKE Action Done Ignition off engine controls closed Front strut secure safety rings attached Pylon catch locked Front tyre inflated and in good con...

Страница 25: ...tions 29th March 2007 Issue 1 Page 25 of 68 In addition carry out pre flight checks in engine operators manual You should never under any circumstances consider flying the aircraft before you have com...

Страница 26: ...ps etc are secure Pockets empty and no loose objects in the cockpit Describe takeoff landing and intention of flight Explain that there are hot and rotating engine parts directly behind which should n...

Страница 27: ...k the aircraft securely All controls should be checked closed and ignition should be off The parking brake if fitted should be applied Check the fuel is turned on ROTAX 912 912S ENGINES Before the fir...

Страница 28: ...S ARE ALMOST INVISIBLE AND CAN CAUSE INJURY OR DEATH Extreme care must be exercised during engine warm up Ensure that all spectators children pets are kept well clear of the propeller and the propelle...

Страница 29: ...against a full power run up Exercise extreme caution when ground running the engine When starting an aircraft engine it is essential that you keep spectators well clear of the immediate area and ensur...

Страница 30: ...e she must fly the aircraft accordingly He must also be trained and in current practice for forced landing procedures This means the pilot should only over fly terrain where a safe landing is possible...

Страница 31: ...o the stall a buffet felt through the control bar should be noticed At the stall there may be a mild wing drop with a very new wing at low weight minimum washout situation To recover use standard flex...

Страница 32: ...Wing Down Set the parking brake with the aircraft across and slightly downwind Bank the into wind wing down till the tip touches the ground Apply the Velcro parking tie to the control frame Into wind...

Страница 33: ...Operators should note that with the engine running above idle the aircraft may tend to creep forward with the rear wheels locked on some surfaces See warning Section 6 4 Inspection The amount of wear...

Страница 34: ...to takeoff position WIND DIRECTION STRENGTH within both aircraft and pilot limits ALL CLEAR to taxi to line up for finals check for other aircraft in the circuit Mixture Magnetos Fully rich on both PO...

Страница 35: ...emperature at 4000 ft is 32 C 90 F the factor will be 0 52 Climb QUIK GT450 The speed at which maximum climb rate is achieved is 55mph Once established in the climb the bar force can be removed with t...

Страница 36: ...at low airspeeds so the bar should be pulled in slightly to increase airspeed before commencing the turn For roll out the control bar is moved towards the lower wing tip and the nose is lowered as the...

Страница 37: ...uld be applied to check the nose down rotation and then the pitch adjusted to resume normal flight At the stall a light wing drop may be found but is easily corrected If necessary hold the bar firmly...

Страница 38: ...nce on the ground puts unnecessary load on the nosewheel and should only be used in an emergency situation where the available stopping distance is marginal in normal landings the wing should be set a...

Страница 39: ...ss wind landings you must inspect the aircraft thoroughly Check the Maintenance and Repair section in this Manual Even after a flight without incident you should still carry out a thorough Post Flight...

Страница 40: ...djustments made to the wing to ensure that it is properly trimmed out and flies hands off at the right speed Owners are discouraged from making any adjustments If you feel your new P M aircraft is not...

Страница 41: ...d of the leading edge cloth right out near the trailing edge and twist it anti clockwise you should feel it move It will then be held there by the tension Tuning in pitch The GT450 wing is designed to...

Страница 42: ...oll response should not exceed 3 seconds at 60mph to reverse a 30 degree bank at a control force of 15kg In addition the response to very small inputs of 1 2kg should be good so that it is possible to...

Страница 43: ...km h 80 km h With electric trimmer 74km h 74km h 74km h VNE 184 km h 184 km h 184 km h Flight manoeuvre loads 4g 0g 4g 0g 4g 0g Best rate of climb MAUW 390kgs ISA 4 3m s 4 3m s 6 1m s Airspeed for bes...

Страница 44: ...power off 47mph 47mph Best Glide Angle at the above airspeed 8 1 8 1 VNE 110 mph 110 mph Flight manoeuvre loads 4 0 4 0 Airspeed for best rate of climb 55mph 55mph Take off distance to 50 Max AUW 921...

Страница 45: ...recovery Min AUW 50ft Max pitch down below horizon Min AUW 30 o Wings level stall power on Min AUW 30mph Max pitch down power on recovery Min AUW 0 o 30 degree banked stalls power off Min AUW 31mph NO...

Страница 46: ...h for 912 85mph 0 5 10 15 20 25 30 35 40 45 50 0 10 20 30 40 50 60 70 80 90 100 mph TAS L P H H rs s tatu te m ile s ran g e x 1 0 lph gt450 Endurance hrs range miles x 10 Fuel consumption figures are...

Страница 47: ...pty weights for the Quik GT450 are as follows 912 912 S 214kg 217kg 470lbs 477lbs Following modification repair or at any time required by the CAA or other Airworthiness Authority the aeroplane must b...

Страница 48: ...Therefore maximum fuel 27 0 718 37 litres or 59 1 58 37 litres FUEL LOADS QUIK GT450 The fuel tank is 65 litres capacity including 1 6 litres unusable giving 63 4 litres useable The weight of the fuel...

Страница 49: ...d variation Solo flight is from the front seat only Wing The CG of the wing is critical Due to the materials used and the quality control in manufacture the CG of the wing does not vary significantly...

Страница 50: ...ling edge and a spanwise Kevlar tape maintain the wing s performance over a long life The aerofoil section is defined by pre formed aluminium and pre formed aluminium composite ribs with chord wise te...

Страница 51: ...iceable in the light weight high power condition above 70mph They also reduce the induced drag and increase trim speed by 5 10mph 11 2 PRIMARY STRUCTURES AND SYSTEMS THE TRIKE 1640 H A N GPO IN T PY L...

Страница 52: ...d System Fuel is fed from a single fuel tank mounted beneath the seats The fuel system has a fuel cock and external filter backed up by an internal strainer fitted to the end of the fuel tank pick up...

Страница 53: ...leaning control is a valve on the instrument panel which applies either ambient pressure rich or partial carburettor venturi pressure lean to the float chambers The pressure can be monitored by a gaug...

Страница 54: ...nted via a pipe to discharge clear of the aircraft A sump with water drain is provided The tank may be 49L or 65L the 65L tank has a third mounting point at the centre of the tank Fuel is supplied to...

Страница 55: ...gnals to be used in instrumentation Two independent sets of cables to the two separate ignition switches are provided Ignition is independent of the battery alternator regulator system The power avail...

Страница 56: ...g that the oil temperature remains within the correct limits is therefore the pilot s Regular in flight checks should be made to ensure that the oil temperature remains within the desired range of 85...

Страница 57: ...tice is not recommended as it puts unnecessary load on the system In this case it is permissible to reset the C B after 2 minutes The C B will also trip if the trim motor should run past the normal li...

Страница 58: ...Warning folded pylon On pylon fairing Warning Loose hair On seat rear left Warning Hot Engine On rear of cowling Warning hand throttle closed On seat next to hand throttle Operating Instructions On c...

Страница 59: ...ng the fitting of optional electrical equipment must not be carried out under any circumstances without official modification authorisation issued by the factory CAUTION When the aircraft is stored fo...

Страница 60: ...and secure Hang point roll bearing adjustment bolt secure 7 Control frame uprights straight end fittings and fasteners secure 8 All sail seams intact with no frayed stitching 9 No tears in the sail 1...

Страница 61: ...s 10 After fitting the upper surface ribs remove the safety pin from the crossboom restraint cable stud just inside the rear end of the keel pocket Make sure that the crossboom rigging tool extension...

Страница 62: ...of the keel Ensure that the previously fitted ribs are pushed FULLY home and that the upper and lower elastics are fitted to all ribs 12 Locate the washout tubes onto the sockets ensuring they are sea...

Страница 63: ...d by walking towards the trike when sufficient height has been attained start to allow the A frame to take the weight of the wing When fully up the rear wires will become taught keep the wing horizont...

Страница 64: ...ed correctly Now is a good time to inspect the interior of the trike including the engine mounts and fuel lines Depress the drain valve on the underside of the fuel tank and drain off a little fuel in...

Страница 65: ...ket Note You may find it convenient to fashion two wooden wedges and jam them one each side of the hang bracket between the hang bracket and the uprights these will hold the hang bracket firmly in a c...

Страница 66: ...ging gas strut is not fitted locate the pylon using the over centre catch but do not overcentre lock it at this stage Get a helper to hold the bar or strap it back using the rear seat harness if it is...

Страница 67: ...t wheel will roll through the A frame and over the control bar as you do this Remove the safety pin and special nut from the hang bolt and then remove the hang bolt from the hang bracket If electric t...

Страница 68: ...n nose down with rigging extension inserted Undo the wing undersurface inspection zips and pass tie down ropes around the cross boom or side wires The nose cone should be removed and stowed under the...

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