P&M Aviation QUIK Maintenance Manual Download Page 39 | Manualshive

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Quik & Quik GT450 Maintenance Manual

29

th

March 2007

Issue 1

Page 39 of 54

Maximum diameter for the hangbolt 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 uprights must be
straight, the tube ends must not be distorted and the end fittings and rivets must be secure.

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Summary of Contents for QUIK

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

Page 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...

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

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

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