Summary of Contents for P&M Aviation QUIK-GTR
- Page 1 QUIK-GTR Operator’s Manual - Issue 1.1 SERIAL NO: P&M Aviation Ltd, Elm Tree Park, Manton, Marlborough, Wiltshire SN81PS Telephone 01672 861328 email: flying@pmaviation.co.uk www.pmaviation.co.uk...
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Page 2: Table Of Contents
4.2. Powerplant Limitations 4.3 ASI calibration 5. Rigging the Aircraft 5.1. General 5.2. Wing Rigging 5.3. Preparing the Trike 5.4. Connecting the Wing to the Trike 6. Pre-flight Inspection 6.1. Wing 6.2. Trike P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 2... - Page 3 12.5. Inspection and Servicing Schedules 12.6. Component Inspection Criteria 12.7 Fatigue life 13. Repairs 13.1. Wing 13.2. Trike Appendix A – Approved Optional Modifications Appendix B – Wiring Diagrams Appendix C – Roll Trimmer P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 3...
- Page 4 Elm Tree Park Manton Marlborough Wiltshire SN81PS Telephone 01672-861350 flying@pmaviation.co.uk WARNING Failure to register will mean that you may not get important safety information issued by the company in support of its products. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 4...
- Page 5 NOTE This NOTE symbol indicates points of particular interest for more efficient and convenient operation. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 5...
- Page 6 Company and acceptance of or payment for goods is an implicit acceptance of this Warning. The Quik-GTR Microlight/Ultralight aircraft must only be flown where the following conditions apply: 1. The aircraft must not be flown over any terrain except where it...
- Page 7 Microlight operation. To ensure a long and trouble free life from your P&M Aviation Quik-GTR, give it the proper care and maintenance described in this manual.
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Page 8: Preparation For Safe Microlight/Ultralight Operation
5kt cross wind and at least 400m clear unobstructed runway. The Quik-GTR is easy to fly, but has a very wide trimmable speed range. It is essential that proper control of speed is exercised for different phases of flight, especially landing approaches. -
Page 9: Modifications
Doctor, or when feeling depressed. 1.3. 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. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 9... -
Page 10: Pre-Flight Checks
If any damage is visible, do not fly until the damaged blade has been repaired or replaced and the engine has been inspected for shock load damage. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 10... - Page 11 - using webbing or rope which is sufficiently strong to take a load of 225 kilos (500lbs) minimum. Securely attach both ends of the rope/webbing to the rear axles of the Quik-GTR just inboard of the wheels. Then, ensuring that the V bridle is long enough to give sufficient clearance from the propeller, attach it to your chosen solid object.
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Page 12: General Description
2. GENERAL DESCRIPTION The P&M Aviation Quik-GTR is an advanced weight-shift controlled aircraft. It may be flown solo or dual without ballast. The aircraft has been developed for advanced cross-country touring performance; a stable hands-off cruise of 70 to 95 mph makes long cross-country trips very practicable. Using appropriate airfields and the instructor control bars, it can also be used as a safe and reliable training machine. -
Page 13: Primary Structures And Systems - The Wing
Quik-GTR in compact folded configuration using a nosewheel skate with control bar channel. 2.2. PRIMARY STRUCTURES AND SYSTEMS - THE WING P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 13... -
Page 14: Primary Structures And Systems - The Trike
The Sail The Quik-GTR wing is the product of one the most experienced flexwing design teams in the world today. The sail fabric is cut with exacting accuracy from stabilised polyester using tight, virtually non-porous and tear- resistant weave construction. Double-stitched seams using PTFE UV resistant thread ensure complete panel join integrity. - Page 15 When flying, use your watch to time the flight against known fuel burn at a given rpm, and always leave plenty of fuel in reserve. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 15...
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Page 16: Secondary Structures And Systems - Engine Controls
The key switch only switches the power to the instruments, comms & starter. Remember to switch on the ignition switches before start-up! The hand throttle cutout switch option makes it necessary for the hand throttle to be CLOSED in order for the starter circuit to operate. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 16... -
Page 17: Secondary Structures And Systems - Braking System
Avoid prolonged or repeated contact with skin or breathing of vapour. KEEP FUEL OUT OF REACH OF CHILDREN. Rotax 912 As above except that 90RON min. fuel may be used, due to the lower compression ratio. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 17... -
Page 18: Secondary Structures And Systems - Seat Belts
The screen extension is removable with Dzus Fasteners. The Quik-GTR wing tip fins are optional. Without fins, the roll handling is lighter but the high speed directional stability is slightly reduced and the fully fast trim speed will be slower by a few mph. The trim speed can be recovered by turning the tip adjusters down 2-3 scale divisions, so as to give more lift at the tips. -
Page 19: Secondary Structures And Systems - Radiator Covers
At the same time the STARS system cords are pulled tight, pulling both washout rods up. The combined effect increases pitch stability and reduces the trim speed. Normal operation P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 19... - Page 20 Select trim towards the fast position and the turn will steadily diminish. Then an approach can be made at normal speeds, accepting the out of trim pitch force. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 20...
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Page 21: General Information
3. GENERAL INFORMATION 3.1. EMPTY WEIGHT Typical empty weights for the P&M Aviation Quik-GTR are as follows: 912 S Rotax 912 234kg 515lbs Following modification, repair or at any time required by the CAA or other Airworthiness Authority, the aeroplane must be weighed so that the composition of useful load can be determined. -
Page 22: Centre Of Gravity
The CG of the wing is critical. Due to the materials used and the quality control in manufacture, the CG of the Quik-GTR wing does not vary significantly in production. Items should not be attached to the wing which significantly change the CG. The hang point position on the wing keel must not be moved from the designed and tested position. -
Page 23: Running Gear
Take off distance to 50’, Max AUW** 1131ft 1239ft Landing distance from 50’, MAUW 1050ft 1050ft Trimmed fast cruise @ Max/Min AUW,rear 90/90mph 90/90mph hangpoint Trimmed slow speed @ Max/Min AUW, rear 65/55mph 65/55mph P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 23... - Page 24 @ 15° Celsius (59°F) (ISA). Temperature, air density, altitude and take off surface can severely affect take- off and landing performance. Make the appropriate calculations before take-off. Fuel Consumption P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 24...
- Page 25 Wings level stall, power on, @ Min AUW 34mph Max. pitch down, power on recovery, @ Min AUW 30 degree banked stalls, power off, @ Min AUW 34mph NOTE (See also Section 8.5 paragraph on Stall Characteristics.) P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 25...
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Page 26: Electrical System Specification
CAUTION When the aircraft is stored for an extended period of time, remove the battery and charge it fully. Then P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc store it in a warm dry place. Never leave the battery Page 26... - Page 27 WARNING Unauthorised modifications, including the fitting of optional electrical equipment, must not be carried out under any circumstances without official modification authorisation issued by the factory. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 27...
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Page 28: Operating Limitations
Flight Envelope, or outside any of the limitations detailed below. The P&M Aviation Quik-GTR must be operated in compliance with the following limitations: The aircraft is to be flown only in daytime visual meterological conditions ( VMC). -
Page 29: Powerplant Limitations
The static port is provided with an adjustable pressure dam behind the static port hole. A calibration chart is shown below, for the factory standard setting, which is with the dam bent up by 2.0mm. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 29... - Page 30 Use of cockpit static pressure will cause considerable over-reading (typically 10-15mph at 90mph). If desired, the ASI can be calibrated against GPS using BMAA procedure TIL042. If the ASI over-reads, bend the tab UP. If it under reads, flatten the tab. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 30...
- Page 31 QUIKR asi calibration static port dam UP 2.0mm IAS vs CAS CAS mph P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 31...
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Page 32: Rigging The Aircraft
The design brief for the P&M Quik-GTR called for easy inspectability, so those components not open to view may be reached from zipped inspection panels. (See airframe parts drawings). -
Page 33: Wing Rigging
Select a clean, dry area and lay the wing down, opening the zip to reveal the control frame and underside of the wing. Remove the sail ties and padding. Open out the control frame and attach the base bar to the corner joints. Inspect the basebar holes for damage. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 33... - Page 34 45 degrees each side of the keel. Lifting the trailing edge will assist the washout rods to swing into position. Stop if resistance is felt and investigate. DO NOT ALLOW THE TIPS TO SCUFF THE GROUND AS EVENTUALLY THE WEBBING AND STITCHING MAY BE DAMAGED. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 34...
- Page 35 Fit the lift struts noting they are handed Left and Right, using the AN-5 bolts, wingnuts and rings. It may prove easiest to attach the top spherical joint first. WARNING Do not lever the strut joint beyond it’s range of articulation or damage may occur. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 35...
- Page 36 P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 36...
- Page 37 The tang is located in the stud recess. b) The tensioner cables are not twisted. c) The safety pin secures the cable onto the stud and is re-fitted correctly into restraint cable stud. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 37...
- Page 38 Velcro panel in the undersurface. 13. Ensure the STARS system is routed correctly as shown by the GA drawing. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 38...
- Page 39 14.Fit the undersurface battens and secure them with the single bungees. Rigging stage 13 15.Engage each tip fin on the leading edge spigot and then attach the two clevis pins with nylon washers and safety clips. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 39...
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Page 40: Preparing The Trike
Fit the nose extension (rigging tool) to the wing and position the wing on it’s control frame and nose extension facing into wind. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 40... - Page 41 P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 41...
- Page 42 If thermals etc are present, the aircraft may be picketed using weights or ground anchors on the corner of the A frame or top of the lift strut. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 42...
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Page 43: Pre-Flight Inspection
Hang bolt secure, head on the LH side and tight as possible using hand, lanyard and clip in place. WARNING You should never, under any circumstances, consider flying the aircraft before you have completed a thorough pre-flight check! P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 43... -
Page 44: Preparation For Flight
(see below). 2. Rotating propellers (which are very difficult to see), hot coolant, hot and moving engine parts can all be very dangerous if not treated with due care and respect. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 44... -
Page 45: Strapping In
2-stroke’s, and the choke system automatically raises the idle speed quite considerably, so you MUST have brakes applied. For all other starts unless hot, use about 1/3 choke. Before start-up, check that both carbs are shut. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 45... - Page 46 WARNING Never attempt to hand start an engine by swinging the propeller! This practice is very dangerous and could result in injury or death. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 46...
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Page 47: Engine Warm Up
Exercise extreme caution when ground running ONLY the foot throttle during run-up, and be the engine. ready to turn off at the ignition switch. Failure to follow these instructions could result in injury or death. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 47... -
Page 48: Flight
The Quik-GTR wing has low drag and an extremely wide speed range. Care must be taken not to fly the aircraft beyond VNe or into a steep nose up pitch attitude. The wing will stall if the control bar is pushed out to the front strut and held there. -
Page 49: Primary Controls
Engine speeds up WARNING It is absolutely essential that all persons wishing to fly the Quik-GTR are trained to a minimum standard of the syllabus as published by the British Microlight Aircraft Association, carried out by a recognised training organisation for this type of aircraft. It is absolutely essential that all persons with experience of 3 axis aircraft undertake a flexwing conversion course on a dual-control flexwing aircraft before attempting to fly the P&M Aviation Quik-GTR. -
Page 50: Ground Handling
Flexwing Microlights require special ground handling techniques. Parking The Quik-GTR is best parked into wind, though the wing down method may be used in light winds. 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. -
Page 51: Take-Off
Idle speed should be set at around 1400 RPM for the Rotax 912S/912 engine. Run engine to 3850 RPM, then turn OFF front magneto. Listen for any misfire and observe mag drop (see also Engine Operators P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 51... -
Page 52: En-Route
Take-off Technique The hand throttle should not be used during take-off. Set the pitch trim control to the Quik-GTR placarded take- off position. Check brakes are OFF. The correct technique on smooth surfaces is to allow the wing to trim in pitch during the initial stages of the take off run so as to reduce the drag and increase the acceleration. - Page 53 Do not exceed more than 60 of bank. Trim – Longitudinal The Quik-GTR has a powerful electric trim system giving a very wide trim speed range of 55 – 95mph solo, 60-95 mph at maximum weight. The aircraft should be set at the desired steady speed/attitude/power and then the trimmer operated to remove the pilot’s pitch force on the control bar.
- Page 54 At the stall, a light wing drop may be found but is easily corrected. If necessary, hold the bar firmly to counter any tendency for the nose to pitch up excessively during the recovery. The P&M Quik-GTR wing is remarkably stable, and even if stalled in a turn will not spin, but pitch down, increase air speed and roll out into a shallow turn or straight flight.
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Page 55: Landing
Periodically warm the engine in the descent, particularly in cold and moist conditions. Because of the great speed range of the Quik-GTR, the aircraft must be trimmed to a reduced speed for landing in order not to overshoot the runway. If the speed and/or the altitude are too high, make the decision to go around early. -
Page 56: Emergency Procedures
FLY THE AIRCRAFT. Set up a steady glide. The best glide of the Quik-GTR is approximately 10:1 at 55 mph, but this can be reduced to 5:1 at 90 mph. - Page 57 In this case, select fast trim whereupon the whole system will go slack and so not affect the wing. Land with fast trim set, being prepared for a stronger than normal push-out to flare for landing. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 57...
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Page 58: Post-Flight Inspection
The undercarriage, tyres & wheels Loose objects Oil and coolant levels NOTE If leaving the aircraft rigged, the trimmer should be left slack in the high speed position. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 58... -
Page 59: De-Rigging The Aircraft
The Quik-GTR strutted wing/trike configuration can be quickly folded to minimise hangarage space. Only configuration 3 is recommended for road transport. 10.1 Folding Configuration 1. -
Page 60: Fold Configuration 1
Secure the trailing edges with ties, or if all battens are removed, roll up each wing and secure it with sail ties. 10) Protect the sail with UV light proof covers. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 60... -
Page 61: Fold Configuration
To rig for flight from configuration 2, use the reverse procedure. It is possible to open the wings by pulling on the cross boom cord in this position, though assistance may help. Lift the trailing edges as the wings open to assist correct deployment of the washout rods. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 61... -
Page 62: Rigged Wing Storage
If storing the wing alone rigged, it should be parked in a sheltered location 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 leading edge Mylar. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 62... -
Page 63: Wing Overnight Parking
This may result in mildew on the sail or general degradation of the airframe and fittings. If possible dry the wing before de-rigging. Otherwise open the bag zip before the wing is stored. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 63... -
Page 64: Tuning The Wing
With the STARS system, it has been found best to move the tip adjuster plugs symmetrically, only for trim speed adjustment. Instead of adjusting the tips asymmetrically, the STARS cords can be used to tune out low speed turns and the wing rib reflex technique used for high speed turns. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 64... -
Page 65: Tuning Guide
The reflex should be applied 230mm from the trailing edge and applied in small increments up to a maximum of 20mm. Start with 5mm reflex, test fly, then adjust in 5mm increments as required .Do not exceed 20mm reflex! P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 65... - Page 66 The standard setting is just enough tension to keep the D ring secure. Differential tensioning of the tips to attempt to tune out a turn has not been found effective. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 66...
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Page 67: Tuning Pitch
11.3.3 Selection of Hang Point There are two hang points, only the rear hangpoint is approved for the Quik-GTR and should be set to give approximately 90mph hands off trim speed with the trimmer set fully fast. For economical cruising or training, the rear position is recommended. - Page 68 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. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 68...
- Page 69 On no account should the washout rod settings be dropped in an effort to increase trim speed, as dangerous pitch instability may result. Combinations of pitch and roll tuning: The above adjustments for pitch and roll may be superimposed, up to the adjustment limits specified. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 69...
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Page 70: Maintenance
Apart from the consequences of heavy landing, or of exceeding flight limitations, the major factors for attention are corrosion, fatigue and UV light. There is no inherent fatigue problem with the P&M Quik-GTR, but excessive loads and vibration can weaken the structure, and a regular watch for hair-line cracks, most likely in areas under high stress, such as around bolt holes, should be carried out. -
Page 71: General
Never use spirits, alcohol, thinners or any strong detergents when cleaning the sail. These may damage the cloth or threads, leading to structural failure of the sail fabric which could result in injury or death. P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 71... - Page 72 It is essential that they are reformed at frequent intervals and checked against the template. If you have to rig regularly, you should check your rib profiles every 25 hours. If you leave your Quik-GTR rigged, check the ribs every 100 hours. The best way to reform the rib is to hold it against your knee and, whilst applying pressure to bow the rib, slide it side to side over the area you want to bend.
- Page 73 P&M QUIK-GTR Manual, ref. QUIK-GTR Man 1.0.doc Page 73...
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Page 74: Trike
12.3. TRIKE General The Quik-GTR trike has been designed to permit easy inspection and operators should have no difficulty in assessing problems or recognising damage if visual checks are carried out conscientiously. The trike may be transported and stored fully assembled or folded down. If folded down, for transport - The pylon must be supported to prevent damage to the structure. -
Page 75: Lubrication
Failure to do so could result in injury or death. All other bearings are life sealed and require no additional lubrication. P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 75... -
Page 76: Inspection And Servicing Schedules
Lubricate the throttle, choke and brake cables with WD40 if they ever become too stiff. This is particularly important on the Rotax 912S/912 powered Quik-GTR. Work the WD40 into the cable outers by moving the pedal backwards and forwards as you spray. Lubricate the throttle splitter-box at least every 100 hours with WD40 by pulling the cable outers away from their location holes and using the WD40 extension tube inserted in each hole in turn, spray for a second or so. - Page 77 Inspect security of fasteners ELECTRIC TRIM SYSTEM Pre- First 10 Every Every Annually Other flight 25 hrs 50 hrs /100 hrs Connected, operates correctly, full and free check movement of controls, trim display P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 77...
- Page 78 NOT MORE THAN 500hrs/4 years (in 4 years normal use). A second inspection by an approved inspector must be carried out and a check flight by an approved check pilot before return to service. P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 78...
- Page 79 12.6. INSPECTION CRITERIA: General In the main, the safe working life of the structural components of the P&M Quik-GTR is dictated by the environment in which the aircraft is used and the care taken during day to day operations. Inspection, therefore, is an essential tool in deciding the continued use of most components.
- Page 80 Increased washout improves pitch stability and also prevents the possibility of tip stalling. Tension in cord 3 also applies a direct mechanical nose-up pitch relative to the trike. The combined effect is to slow the trim speed and increase pitch stability. P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 80...
- Page 81 The overall effect is to increase washout in the right wing and reduce it in the left wing. Typically the roll rate from 30 degrees left to 30 degrees right is reduced from 5 seconds to 3.5 seconds at 50mph. The wing remains controllable in roll right down to the stalling speed. P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 81...
- Page 82 The main charging fuse from the regulator to the battery should be 30A when electric trim is fitted. The main fuse from the master switch to the main electrical bus should be 20A when electric trim is fitted. P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 82...
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Page 83: Fatigue Life
For the following small items, inspection is not practical and so replacement is strongly recommended at the following times: Hang bolt 250 hours. WARNING It is vitally important that the lifing & NDT of all components is strictly observed, or serious injury or death could occur. P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 83... -
Page 84: Repairs
13. REPAIRS WARNING The P&M Aviation Quik-GTR airframe is deceptively simple, but like all aircraft requires skilled and qualified attention. We do not recommend self repair or re-assembly by other than P&M Aviation or P&M Aviation nominated repair agents. No replacement parts should be fitted unless they are factory supplied and identified. - Page 85 Note that other approved modifications may exist which are not listed here. The P&M Quik-GTR wing can be flown on the Quik or GT450 trike provided the following essential modifications are embodied. New placarding for the trim indicator, Vne and weights will be required. Note that only the 912S engine with slipper clutch and Warp Drive propeller, or 912 engine with Warp Drive propeller are approved for the Quik-GTR.
- Page 86 Fournales shocks 23/06/2014 Explorer steering stop material 31/07/2014 Hangbolt anti rotation 22/09/2014 200mm Spinner 24/11/2014 Modified throttle cable bracket 22/06/2015 GT450 G-CFIM parachute step 15/09/2015 Vhf antenna routing 07-Oct-15 Underseat carry bags 09-Dec-15 P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 86...
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Page 88: Appendix B - Wiring Diagrams
Appendix B – Wiring Diagrams Wiring Diagrams – Included as a guide only as some variation may exist due to different instrument fit. P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 88... - Page 89 P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 89...
- Page 90 P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 90...
- Page 92 Appendix C, Modification M275, Roll Trimmer Roll Trimmer for QuikR ( STARS equipped) and GTR flexwings. General Both the QuikR and GTR use the STARS system ( mod M252) which operates the outer washout rods. In roll, the washout rods are operated asymmetrically to aid roll response, and when slow pitch trim is selected, both washout rods are pulled upwards, increasing pitch stability and avoiding tip stalling.
- Page 93 Replace with genuine 3mm dyneema cord if there is any sign of damage. Check the STARS cords runs are straight and not twisted around either washout rod. Drawings P&M Aviation Quik-GTR Manual, Quik-GTR1.0doc Page 93...
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