P&M Aviation QUIK Скачать руководство пользователя страница 37

Quik & Quik GT450 Maintenance Manual 

 

 

29

th

 March 2007 

Issue 1 

 

Page 37 of 54 

 

 
The Airframe 

All the main tubing used in the airframe is a high quality aluminium alloy from aircraft quality billets using a 
special  process  of  mandrel  extrusion  followed  by  being  drawn  to  agreed  industry  specifications.    All  tubes 
and inserts are anodised to give protection against corrosion.  

 

There are no welded components in the wing frame, and sheet fittings are plated, anodised or stainless steel. 
All bolts are of high tensile steel. Rigging wires are PVC covered where necessary to afford protection to the 
occupants and to also serve as an anti-kink measure. 
 

Wing tip fins 

The Quik GT450 wing is fitted with composite wing tip fins, which improve directional/lateral stability, which is 
most  noticeable in the light weight/high  power condition  above  70mph. They  also  reduce the induced  drag 
and increase trim speed by 5-10mph. 

 

4.17.  WING 

 

 

General 

 

Careful attention to the recommended rigging and derigging sequences will protect the wing from the risk of 
unnecessary  damage.  The  wing  must  always  be  transported  inside  its  bag,  and  the  bag  zip  should  face 
downwards to minimize the entry of rainwater. Following transport of the wing through rain, open the bag and 
loosen  the  ties  to  dry  the  sail  in  case  any  damp  has  penetrated  the  bag.    During  transportation,  or  when 
stored on slings, the wing must be supported by at least two points not more than 2.6 metres apart. Supports 
should  be  softly  padded,  and  any  support  systems  used  for  transport,  such  as  roof  racks,  must  use 
attachment  straps  which  are  sufficiently  secure  to  eliminate  the  possibility  of  damage  from  vibration  and 
abrasions.  STRAPS SHOULD NOT BE OVERTIGHTENED. 

 
 
Wing Fabric Maintenance

 

Despite  the  best  care  you  can  take,  you  may  still  have  accidents  with  the  odd  wall  or  wire  fence  or  your 
protection  pads  may  slip  and  you  will  be  faced  with  slight  damage  to  the  fabric.    Where  this  takes  place 
influences repair; high load areas such as a trailing edge being critical. Any cuts or tears through the trailing 
edge, sail  fixing  points  or similar high load  areas must  be repaired  at  a P&M Aviation  approved workshop. 
Small damage to panels, leading edge cover etc. can be repaired with self adhesive tape which is cut to size, 
pressed  into  place  on  the  clean  dry  sail  and  warmed  gently  with  a  hair  dryer  to  melt  the  adhesive,  being 
careful not to apply too much heat. We define small damage as abraded holes no more than 10mm (3/8 inch) 
diameter  and  small  cuts  no  larger  than  15mm  (5/8  inch).  Anything  larger,  or  near  the  trailing  edge  (within 
150mm/ 6 inches) should be inspected by a qualified engineer. 
   

Long term exposure to ultra violet light must be avoided

 - keep the wing de-rigged in the bag or rigged 

with wing covers. The sail should be checked with a Bettsometer   

 
 
 
 
 
 
 
 

 

 

 

Stitching Damage 

All the seams are firstly joined with a double sided sail adhesive tape and then double zig zag sewn.  Thread 
damage never ever gets  better and eventually runs. Since the wing is held together with stitches, its pretty 
obvious  what  will  happen  when  the  stitching  fails.  If  you  abrade  a  seam,  then  have  the  damage  repaired 
before it gets worse.  
 
Small  non-loaded  areas  can  often  be  repaired  in-situ  by  the  tedious  but  effective  method  of  hand  sewing 
back through the original stitch holes. Never use anything but matching spun PTFE thread which is available 
from P&M Aviation Ltd. 
 
 

Wing Fabric Cleaning

   

There is no easy answer for cleaning sails; it is certainly best if possible to keep them clean!  If all else fails 
and you  need to  wash  your wing, then select  a  dry  day  and  have  access to  a  good  hose  and clean  water 

Check  your  sail  for  ultra  violet  damage 
regularly.  Flying  with  a  damaged  sail  could 
cause structural failure, injury or death.

 

          

CAUTION

 

NEVER  STORE  THE  WING  IN  A  SEALED  WING 
BAG WHEN WET  -  leave  the  zip  open  to  allow  the 
moisture to evaporate.

 

WARNING 

!

 

Содержание QUIK

Страница 1: ...ce Manual 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 at ti io...

Страница 2: ...4 Primary Structures and Systems The Trike 26 4 5 Trike 26 4 6 Lubrication 26 4 7 Secondary Structures and Systems Engine Controls 29 4 8 Secondary Structures and Systems Braking System 30 4 9 Seconda...

Страница 3: ...uik Quik GT450 Maintenance Manual 29th March 2007 Issue 1 Page 3 of 54 7 De Rigging the Aircraft 49 7 1 De Rigging 49 7 2 Rigged Wing Storage 50 7 3 Wing Overnight Parking 50 APPENDIX A Wiring Diagram...

Страница 4: ...onal 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 time and...

Страница 5: ...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 followed could...

Страница 6: ...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 employ it...

Страница 7: ...ing to attain awareness of the mental and physical requirements necessary for weight shift control LSA operation To ensure a long and trouble free life from your P M Aviation LSA give it the proper ca...

Страница 8: ...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 Pounds per...

Страница 9: ...s Misc 1 Pound Ib 0 4536 Kilogram kg 1 Pound per sq in psi 6 895 Kilopascal kPa 1 Inch in 25 4 Millimeters mm 1 Foot ft 0 3048 Meter m 1 Statute mile 1 609 Kilometres km 1 Nautical mile NM 1 852 Kilom...

Страница 10: ...MODIFICATIONS You must not carry out unauthorised modification to the aircraft It is illegal and for the most part unsafe to carry out unauthorised modifications to your aircraft 1 3 PRE FLIGHT CHECK...

Страница 11: ...s surrounded by trees or other obstacles should be avoided particularly in windy conditions since low level turbulence and rotor are likely to be present Exercise great care when visiting other airstr...

Страница 12: ...uctions 7 Make sure there is a qualified pilot on board properly 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 w...

Страница 13: ...ed flight at very low fuel consumption short takeoff and landing as well as cruising speeds up to 95mph The electric trim system gives precise fingertip control of hands off trim speeds from approxima...

Страница 14: ...Quik Quik GT450 Maintenance Manual 29th March 2007 Issue 1 Page 14 of 54 2 1 GENERAL ARRANGEMENT DRAWINGS...

Страница 15: ...Quik Quik GT450 Maintenance Manual 29th March 2007 Issue 1 Page 15 of 54...

Страница 16: ...on Quik Quik GT450 912 912S registration mark engine type has been weighed empty including full oil electrolight and unusable fuel WEIGHT MODIFICATION STATE DATE 3 2 FUEL LOADS FUEL LOADS QUIK The fue...

Страница 17: ...with 65 litres A pilot weight fuel weight placard must be filled in showing the trade off between fuel load and cockpit load calculated according to the actual empty weight of the aeroplane 3 3 CENTRE...

Страница 18: ...saving 1 7kg It may be fitted as a customer option The modification specification and empty weight of your aircraft appears in section 3 1 3 6 RUNNING GEAR Tyre Pressures front and rear 22 0 psi 1 5 b...

Страница 19: ...for replacement Any fastener which is bent or shows sign of wear or corrosion should be immediately replaced Rigging Cables The main danger with the rigging lies in kinking the cable usually caused b...

Страница 20: ...Inspect ELECTRICAL CONNECTIONS Check all connections are tight and that no corrosion is visible Check all cables for chaffing LM Inspect AIRFILTERS Check the condition of the air filters Clean and re...

Страница 21: ...the torque and re wirelock every 50 hours LM Inspect Service TRIKE FRAME Pre flight First 10 hrs Every 25 hrs Every 50 hrs Annually 100 hrs Other PYLON TUBE check for cracks bends fatigue Also after e...

Страница 22: ...leaks LM Inspect WHEEL BEARINGS check seals and general condition Check for free play and listen for any rumbling when rotating wheels LM Inspect WHEEL HUBS check for damage and wear after every heav...

Страница 23: ...M Inspect Inspect NOSE PLATE check plates for wear damage Check plates are straight and that there are no signs of damage around holes LM Inspect Inspect NOSE PLATE Check fasteners for corrosion LM In...

Страница 24: ...may be returned to service Leading edges Keel Pylon Seat frame Trike base tube Front strut channels Control frame upright top and bottom fittings Control bar end holes Control bar end knuckles Leading...

Страница 25: ...tubular seat frame The seat incorporates a foldable backrest for the front seat occupant The rear undercarriage comprises Chro Mo steel alloy tubular wishbones with suspension by polyurethene elastom...

Страница 26: ...Duck Oil or similar to prevent corrosion Spray the engine with WD40 or Silicone Spray 4 6 LUBRICATION Trike The rear steering bar foot throttle hand throttle and choke lever pivots should be lubricate...

Страница 27: ...ion that meets British Civil Airworthiness Requirements Section S When dismantling the suspension legs to lubricate the sliders it is essential that the trike is supported to ensure that it cannot top...

Страница 28: ...leading edge tape is replaced or added or if any undue vibration has been noticed or if a blade has been chipped and in any case at the recommended service intervals not to exceed 25 hours see engine...

Страница 29: ...ard for choke ON Normal operation is always with choke off Contact Switches Two ignition kill switches one for each ignition system up for on down for off are fitted one in front of the other on the s...

Страница 30: ...hen the brake pedal is pressed NOTE Do not press on the end of the locking ratchet to engage parking brake There is a risk it could bend The travel of the hydraulic brake pedal will be such that the l...

Страница 31: ...TEM The aircraft is fitted with two standard wiring systems one for transmission of electrical power derived from the engine alternator and the other for sensor signals to be used in instrumentation T...

Страница 32: ...requirements specify that all electrical equipment attached to the wiring system must be protected by overload protection devices and that no protective device may protect more than one circuit essent...

Страница 33: ...s jacket is 1 To make it easier to reach 100 C in normal use in order to minimise the risk of humidity building up in the oil system 2 To speed up the warm up procedure Note If your aircraft regularly...

Страница 34: ...ilst selecting slow trim The trimmer takes approximately 18 seconds to run through the whole range In the cruise there may be a delay of a few seconds when selecting nose up trim as the trimmer takes...

Страница 35: ...Adjustment With the control bar held back against the pilot s stomach in the fast trim position the trim cord and bungee should be just coming under tension With the bar at the pilot s stomach the cor...

Страница 36: ...T T ENS K INGPO S T L UFF LINE S A ND T O P RIG G INGW IR ES A FRA M E The Sail The GT450 wing is the product of one the most experienced flexwing design teams in the world today The sail fabric is c...

Страница 37: ...ction pads may slip and you will be faced with slight damage to the fabric Where this takes place influences repair high load areas such as a trailing edge being critical Any cuts or tears through the...

Страница 38: ...subject to degradation by UV light Spun ptfe Stitches can be weakened by abrasion The Bettsometer test gives a good indication of the capability of the sailcloth to transfer load at a stitch hole The...

Страница 39: ...hole is 10 7mm The hangbolt is NOT intended to rotate in the bracket and should be tightened securely by hand The control frame pivot bolts must be secure yet allow easy movement The control frame up...

Страница 40: ...Openpage Repairs must be by replacement using genuine Rotax parts or by Rotax approved repair scheme only Replacement parts must be obtained from P M Aviation Ltd or Authorised Rotax aero engine dist...

Страница 41: ...ure 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 10 Batten...

Страница 42: ...Ensure that all wires are untangled particularly at the connections 8 Excluding the nose rib fit all the top surface ribs starting with the outboard main ribs and working in board towards the root Do...

Страница 43: ...e front rigging tool pulley onto the keyhole tang and secure with a safety pin Ensure that the cord between the two pulleys is not tangled Using the pulley cord pull back the crossboom until the keyho...

Страница 44: ...acing the wing but at least ten feet away to give clearance for the wing to be raised onto its control frame 16 Ensure that the lower flying wires are not tangled and that the nose wires are laid out...

Страница 45: ...Join the nose cone rigging cable slot edges with the Velcro s provided and attach the nose cone underside to the wing undersurface Velcro 18 Adjust either the upper or lower wing attachment Velcro pat...

Страница 46: ...damage and wear to the wing and scraped knuckles as you lift the wing from the ground Ensure that the ground is level clear of clutter wing bags tools twigs and inspect the ground for holes or any ot...

Страница 47: ...n inspect the nose plate and cross boom hinge areas attach the nose cone Lift the nose further while rolling the trike rearwards until the wing keel engages with its stop The nose wheel of the trike w...

Страница 48: ...have a helper at hand Fit the front strut first attaching it at the top with a pin and safety ring and then at the bottom with two pins and safety rings Secure the Overcentre Lever in its latch 8 Rel...

Страница 49: ...en carried out correctly However if you do not use the correct procedures or technique it is possible to injure yourself It is therefore essential that you receive formal instruction on how to rig and...

Страница 50: ...refully ensuring that the protection patches are correctly positioned at the following positions a Control frame knuckle joints b Roll bracket and upper control frame c Washout tube plugs Rigging cabl...

Страница 51: ...sue 1 Page 51 of 54 CAUTION Never store a wet wing in a sealed bag This may result in mildew on the sail or general degradation of the airframe and fittings If possible dry the wing before de rigging...

Страница 52: ...Quik Quik GT450 Maintenance Manual 29th March 2007 Issue 1 Page 52 of 54 Appendix A Wiring Diagrams Wiring Diagrams Included as a guide only as some variation may exist due to different instrument fit...

Страница 53: ...Quik Quik GT450 Maintenance Manual 29th March 2007 Issue 1 Page 53 of 54...

Страница 54: ...Quik Quik GT450 Maintenance Manual 29th March 2007 Issue 1 Page 54 of 54...

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