MAC PARA MacJet User Manual

1
2
Contents
GENERAL................................................................................................................... 3
PILOT LEVEL REQUIREMENTS................................................................................ 4
DESIGN...................................................................................................................... 4
TECHNICAL DESCRIPTION ...................................................................................... 5
RISERS....................................................................................................................... 6
TRIMMING.................................................................................................................. 9
MATERIALS.............................................................................................................. 10
TECHNICAL SPECIFICATIONS............................................................................... 11
CHECKS ON A NEW PARAMOTORING GLIDER ................................................... 11
SETTING UP THE CONTROLS................................................................................ 12
FLYING THE MACJET.............................................................................................. 13
TOWING, JUMPS FROM AIRCRAFT, AEROBATICS.............................................. 21
EXTREME FLYING MANOEUVRES ........................................................................ 22
RAPID DESCENTS................................................................................................... 25
GOLDEN RULES...................................................................................................... 27
LOOKING AFTER YOUR GLIDER ........................................................................... 28
TREATING NATURE WITH RESPECT.................................................................... 30
LINE PLANS ............................................................................................................. 31
Line plan MacJet – 22 (S)......................................................................................... 32
Line plan MacJet – 24 (M)......................................................................................... 33
Line plan MacJet – 26 (L).......................................................................................... 34
Line plan MacJet – 28 (XL) ....................................................................................... 35
Line plan MacJet – 31 (XXL)..................................................................................... 36
MANUAL FOR PARAMOTORING GLIDER CHECKS.............................................. 37
TEST FLIGHT CERTIFICATE................................................................................... 39
TECHNICAL SPECIFICATION ................................................................................. 39
3
GENERAL
We congratulate you on your purch ase of a MAC PARA paramotoring glider. Extensiv e development work and numerous tests make the MacJet a state-of-the-art param otoring glider. The MacJet is a full reflex paramotoring gli der and was designed for advanced paramotoring pilots looking for an easy gl ider with a wide speed range. T he MacJet has easy launch and landing, performs better and flies faster than oth er wings with excellent stability and manoeuvrability. Please read this manual carefully before you start, this way you will get the most out of your glider, and enjoy many pleasant flight s.
Please read this manual carefully and note following details:
The purpose of this manual is to offer guide lines to the pilot in the use of the MacJet and is in no way intended to be used as a trainin g manual for th is or an y other param otoring glider or even a paraglider. Parag liding and paramotoring are a sport, which demands, besides the optimum equipment, a high de gree of attentiveness, good judgement, and theoretical knowledge. Paramotoring can be a dangerous sport, which may lead to injury and death. You may only fl y an aircraft of any description when qualified to do so or when undergoing training from an accredited school or instructor. The use of this paramotoring glider is solely at the user's o wn risk! The manufacturer and distributor do not accept any liability. Pilots are responsibl e for their o wn safet y and their paramotor in g glider airworthiness. The paramotoring gli der carries no warranty! The author assumes that the pilot is in possession of a valid paramotoring licence for glider's category, insurance etc.
Before delivery, as well as during production, each paramotoring gli der goes through a strict visual inspection, and is test-flown by your dealer. Sta mps on th e pla card, tog ether with a completed test-flight certificate, confirm this. Check that the paramotoring glider has been test-flown before your first take-off. If it has not, consult your dealer.
Any inadequate use or misuse increases the risks considerably. The MacJet must not be used outside the manufacturers recommended weight range. The MacJet must not be used during rain or snow-fall. The MacJet must not be used i n high or gusty winds. The MacJet must not be used in clou d and fog. The MacJet must not be used by pilots without sufficient knowledge or experience. Any changes made to this paramotoring glider invalidate the certificate of airworthiness.
If, after carefully reading this handbook, you still have questions, suggestions or criticism regarding this product do not hesitate to contact your dealer or us. We will be glad to help and advise.
MAC PARA wish you many pleasant flights with your
MacJet
4
PILOT LEVEL REQUIREMENTS
As pilots you practise paramotoring for some time and your skills are like ly to continue growing. You know and appreciate the performance and safety of reflex gliders. We recommend that to fly the MacJet, a minimum level of pilot experience of at least 50hrs and one full year’s season of flying paramotoring gliders with adjustable trim is desirable.
The MacJet can adapt to suit a full range of conditions and types of powered flying except acrobatic flying. Nevertheless, strong turbulence a nd gusting winds can lead to a partial or complete collapse of the canopy. Therefore never fly in such conditions.
Even though it is possible to use the MacJet for free flying, please note it is not EN certified. We have made a great paramotoring glider but do not want to deceiv e you with EN certification like some manufacturers do.
DESIGN
Wing tip steering
Top surface
Bottom surface
Leading edge
Brake handle
Main karabineer
Rapid links
Main lines
Risers
Main brake line
Brake line
Stabilizer
Glider's label on the central main rib
Trailing edge
5
TECHNICAL DESCRIPTION
Construction of the canopy:
The canopy of the MACJET consists of 58 cells over the wingspan. The wingtips are slightly pulled down and this acts as a kind of stabilizer. The MacJet is a second rib diagonal-construction paramotoring glider. Every main rib is attached to 4 or 5 suspension lines. Between these main suspension ribs, intermediate ribs are suspended by diagonal segments. This construction ens ures a smooth top surface and precise airfoil reproduction. The internal reinforcements ma intain the precise form of th e canopy and provide stability. The cell openings on the under-surface of the profile's nose provide airflow into the glider. Stretch r esistant flares, integrated with diagonal rib s at the suspension points, ensure an even d istribution of load throughout the canopy. A stretch resistant Mylar strip on the top and bottom panels alongside the openings and running the length of the trailing edge define s the wingspan, together with an optimiz ed sail tension; this guarantees high form stabilit y. Large cross ports allow effective airflo w inside the canopy, providing good re-inflation without reducing the profile accuracy.
The MacJet is mainly made of the proven Nylon fabrics Porcher Marin e Skytex Rip-stop 9092 E85A, 9017 E38A and 9017 E29A. Like any synthetic material, this can deteriorate through excessive exposure to UV.
Rigging system:
The suspension lines are comprised of “cascaded top lines” (attached to the under­surface),”cascaded middle lines” (cascade 2 to 2 top lines together on middle main lines), and “main lines”. Main lines lead to the “quick link” (a Maillon which connects lines and risers). The “stabilizer lines” connect the upper stabilizer lines on the outer suspension points with the quick link. The “br ake lines” are not loa d carrying suspension lines. They lead from the trailing edge of the canopy to the main brake lines and run through the pulleys on the D-risers to the brake h andles. A mark on the main brak e line indicates the position of the brake handle. This adjustment, on the one hand, allows sufficient brake to be applied during extrem e flying situations and when landing, while on the other hand, this ensures that brakes are not perma nently applied to the canopy (especially when fully accelerated). This trimming should not be altered. For differentiation purposes the A-lines are coloured red, the brake lines are orange, all remaining lines are yellow. Also the main suspens ion loop, on the bottom of the riser, is covered red. This is where the main karabiner should be h ooked in, which then in turn connects the risers to the harness.
The lines of the MacJet are made of proven strong and st retch resistant Polyester HMA Aramid/Kevlar (yellow core) lines and PES/Dynema (white core) for brake lines. The entire rigging system comprises individual suspension li nes looped and stitched at e ach end. The Aramid main lines have strengths from 140 up to 340 kg. T he Aramid upper cascade lines have strengths from 60kg up to 120 kg. The Aramid middl e cascade lines have strengths from 80kg up to 160 kg. The Dynema brake lines have st rengths from 100kg up to 240 kg.
6
RISERS
The MacJet is equipped with 5 risers per si de (A, A1, B, C, D). The two central A-lines per side are attached to the main A-risers (colored in red) while outerm ost A main lines are attached to A1 risers. The 3 B-main lines and the B stabil izer lines are attached to the B-riser. The 3 C-main lines and the C stabilizer/comp ensator lines are attached to the C-riser and the 3 D-main lines to the D-ri ser. The main brake li nes lead through the pulleys on the D riser. The higher one for low main karabiner attachment of the paramotor and the lower one for higher main karabiner attachment of the paramotor.
The line connections are made to triangular Maillons (quick links) fitted with a rubber ”o- ring” in the form of a ”figure eight” which prevents any slipping of the lines on the quick link.
Riser`s scheme
swivel
trim buckle
brake
handle
lower pulley for
hight hangpoints
trim handle
magnet
button
trim strap
speed
system
speed system
pulleys
brummel
hook
Torque moments
compensato
r
WTST
handle
upper pulley for
low hangpoints
loop for main
carabinner
A
A
1BC DB
r
magnet
button
color
markingg
Adjuster of TMC
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RISERS
Brake handles:
Special MacJet brake handles are equipped with swivels, neodyme magnets and extending soft loops. The brake handle can be modified according to the pilot’s wishes from soft to semi-rigid or to rigid using different inserts.
Strong neodyme magnets hold the brake handles perfectly to the D risers while attaching and releasing works very easily and quickly durin g flight. This minimises the danger of getting them into a running propeller. Controlling the canopy with extended soft loops is less tiring during long flights when retaining them with two fingers especially with opened trims.
Wing tip steering (WTST):
Wing tip steering handles (small-two finger-brake han dles) allow easy tur ns with a small radius by providing higher drag o n the wing tip. When stee ring with the main brakes in the reflex mode (trims open) they become too heavy and the canopy los es the stability advantages of a reflex airfoil. When applying wing tip steering the pilot can steer the
glider whilst keeping the reflex profile in the main part of the can opy. Note: Sharp turns
are easily possible.
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RISERS
Torque moments compensator (TMC):
The yellow line (equipped with small plastic ball) on the outer side of each riser is connected to the line of C-line stabiliser. With the torque compensator you correct engine torque moments and keep your wing flying in a st raight direction without using brakes for corrections. Especially powerful paramotors with heavier propellers tend to turn your wing in the opposite direction to that the prop eller is turning. The compens ator is very useful during long navigation flights. T he compensator line with two knots leads through a plastic tube with a groove. According to the trims position and adjusted propeller turns you can use the lo wer or higher knot. Bef ore take off you can adjust the position of each knot according to your needs.
Speed system:
The MacJet is equipped with a stirrup operated speed-system, which returns automatically to the normal position when the stirrup is released. The speed system affects the A-, A1-, B- and C-risers and changes the a ngle of attack. In normal flight all risers have an overall length of 49 cm without quick links. When the stirrup is pushed out the A-risers are shortened by up to a maximum of 20 cm, the A1-risers are shortened by up to a max of 15 cm, the B-risers by up to a max. of 10 cm, the C-risers by up to a max. of 9 cm, the D-risers retain their original length.
Trims:
The MacJet has a wide speed range in flight thanks different trim settings. The MacJet trims have a deceleration range of 6 cm and 12 cm of acceleration. On the faster setting (trims fully open or accelerated) the wing’s speed increases. The wing is less sensitive to turbulence and the stability improves. On slower settings (neutral or trims pulled down), sink rate improves and handling becomes lighter and the wing is more sensitive to turbulence.
The speed with closed trims is around 40 - 43km/h with a relatively low effort of the engine. With additional pressure on the brakes the cruise speed is around 34 37 km/h with the best sink rate and an effortless thrust from the motor. This position is ideal for economy navigation tasks. The neutral trim position is marked with a white line on the risers and it is the position where the risers are level. (The most useful configuration for navigation and for precision ground tasks). The MacJet still turns very well, and restores plenty of energy flying around 49-52 km/h. It requires a little more RPM than with closed trims! This is the position we recommended for using the speed system. With the trimmer fully open you reach around 52-54 km/h. The main brakes are getting hard. Control the MacJet with the wingtip steering. In this configuration the canopy is solid. Fully accelerated the speed increases to around 60-63k m/h with high fuel consumption. (Risers lengths on page 30).
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TRIMMING
10
MATERIALS
Tissue
(PORCHER SPORT, Rue du Ruisseau B.P. 710,38290 ST. QUENTIN FALLAVIER, FRANCE)
Top Sail - Leading Edge - SKYTEX 45 E85A - 100% nylon 6.6 , 33 Dtex, 45 g/m
2
Top Sail - Trailing Edge - SKYTEX 40 E38A - 100% nylon 6.6 , 33 Dtex, 40 g/m
2
Bottom Sail - SKYTEX 40 E38A - 100% nylon 6.6 , 33 Dtex, 40 g/m
2
Main ribs, Diagonals - SKYTEX 40 E29A - 100% nylon 6.6 , 33 Dtex, 40 g/m
2
Ribs - SKYTEX 40 E38A - 100% nylon 6.6 , 33 Dtex, 40 g/m
2
Reinforcement Main Ribs - Grille Polyester 200 g/m
2
Reinforcement Ribs - W382 Polyester 180 g/m
2
Lines
(EDELMAN+RIDDER+CO. Achener Weg 66, D-88316 ISNY IM ALLGEAU, GERMANY)
Upper lines - Aramid/Polyester A-6843-060, Breaking Load 60 kg Upper lines - Aramid/Polyester A-6843-080, Breaking Load 80 kg
Upper lines - Aramid/Polyester A-6843-120, Breaking Load 120 kg
Brake lines - Dynema/Polyester A-7850-100, Breaking Load 100 kg
Main lines C1,D2,D3 - Aramid/Polyester A-7343-140, Breaking Load 140 g
Main lines C2,C3 - Aramid/Polyester A-6843-160, Breaking Load 160 g
Main lines D1 - Aramid/Polyester A-6843-080, Breaking Load 80 g
Main lines A1,B1 - Aramid/Polyester A-7343-190, Breaking Load 240 kg
Main lines A2,A3,B2,B3 - Aramid/Polyester A-7343-230, Breaking Load 340 kg
Wing tip line - Aramid/Polyester A-6843-060, Breaking Load 80 kg
Main brake line - Dynema/Polyester A-7850-240, Breaking Load 240 kg
Attachment straps
(STAP a.s., 407 80 VILEMOV, CZECH REPUBLIC)
STAP-POLYESTERBRIDLE 13 mm, Breaking Load 70 kg
Risers
(MOUKA TISNOV ltd, Koráb 133, 66601 Tišnov, Czech Republic)
Polyester 367 040 020 912 25x1,5 mm Breaking Load 800 kg
Thread
(AMANN SPONIT ltd, Dobronická 635, 148 25 PRAHA 4, CZECH REPUBLIC)
Lines-SYNTON 60, Main lines-SERABOND 60, Canopy-SYNTON 40, Riser-SYNTON 30
Rapid links
(ELAIR SERVIS, CZECH REPUBLIC)
NIRO TRIANGLE 200 - Max. Load 200 kg
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TECHNICAL SPECIFICATIONS
Paramotoring (reflex) glider MacJet MacJet MacJet MacJet MacJet Size 22 24 26 28 31
Zoom flat [%] 88,0 92,5 96 100 104,5 Area flat
[m
2
]
22,02 24,33 26,21 28,44 31,06
Area projected
[m
2
]
19,06 21,06 22,68 24,61 26,87 Span flat [m] 10,73 11,28 11,71 12,2 0 12,75 Span projected [m] 8,54 8,98 9,32 9,71 10,15 Aspect ratio flat - 5,23 5,23 5,23 5,23 5,23 Root cord [m] 2,45 2,57 2,67 2,78 2,91 Cells [kg]5858585858 Weight [kg] 5,8 6,0 6,3 6,6 7,0 Weight range * [kg] 77-100 85-110 100-130 115-147 140-180 Min.speed [km/h] 24-26 24-26 24-26 24-26 24-26 Speed Trimmers closed [km/h] 40-43 40-43 40-43 40-43 40-43 Speed Trimmers open [km/h] 49-52 49-52 49-52 49-52 49-52
Top speed (accelerator) [km/h] 60-63 60-63 60-63 60-63 60-63 Glide ratio - 8,2 8,2 8,2 8,2 8,2 Min. Sink rate [m/s] 1,3 1,3 1,3 1,3 1,3
* powered pilot equipped = weight naked + cca. 35 - 40 Kg
CHECKS ON A NEW PARAMOTORING GLIDER
Before delivery, as well as during production, each paramotoring gli der goes through a strict visual inspection. Additionally we recommend that you check your new glider in accordance with the following points. Additionally we recommend that you make this check after flying extreme manoeuvres or after tree landings or similar.
Inspection of the canopy for tears or damage, especially the seams which join the ribs to the upper and lower surfaces, but also the area of the attachment tapes and brake-line connections.
Inspection of the lines for damage to the stitc hes. T he li ne le ngths m ust be checked after 50 hours flying time and whenever the flight behaviour of the glider changes
Inspection of attachment tapes for damage to the stitches. It is also important to check the attachment tapes and brake-lines for tangles.
Inspection of the risers for faultless condition. Rapid links must be secured.
With even slight damage the glider loses its airworthiness!
12
SETTING UP THE CONTROLS
Brakes adjustment and brake handles:
We strongly recommend the following actions be supervised by a paramotoring instructor. Very often improper brake line adjustment can lead to different reactions of your glider or loss of flight comfort or speed. With a brake line adjusted too sh ort the canopy will lose its easy take off behaviour. On the risers di agram you can see there are two brake line pulleys on each riser , higher and lower.
Before flying the glider please check the setting of the brak e lines and adjust them in accordance to your hang p oints. When flying paramotors with lower hang points (main karabiner 50-60 cm from seat plate) the brake lin es should lead through the higher pulleys only and the brake handl es should be adjusted on the higher marks of the brake lines. When flying paramotors with higher hang points (higher the n 70 cm or trikes) the brake lines should lead through the lower pulleys and the brake handles should be adjusted on the lower marks of the brake lines.
Check the set up by inflating the glider on the take off site with a constant breeze 2­3 m/s with the engine off. When the canopy is stabilised above your head, check that the trailing edge of the wing is not being pulled down. When you gently pull the brakes you should have only a 5-10 centimetres of movement before the brakes start to pull down on the trailing edge of the wing. Make sure it is the same length on both sides.
It is safer to have this adjustment a bit longer than too short. When free flying the wing should be set up though the top pulley and with the shorter lines
Note!! All new gliders leave the factory rigged for lower hang points!
Fitting the speed-system:
Most modern paramotoring harnesses have pulleys attached for speed system fitting. The MacJet speed system, including the Brummel-ho oks supplied, must be assembled as per instructions.
The speed system cord is firmly attached (use bo wline or other non sliding knot) to the foot stirrup (webbing or alloy bar). The other end of the c ord is run through a pulley on the harness and then in an upward direction to be then firml y attached to the Brummel­hooks!
The length of the cord leading to the stirrup should be adjusted so that it is easy to put your feet into the stirrup in flight but stil l short enough to allow full spe ed system travel. (Use of 2 stirrups in a ladder fashion can enabl e you to reach the full range if your l egs are not long enough.) Ensure both cords on the stirrup are of equal length, to avoid putting a turn in the glider.
Test your speed system for the correct length of cord on the ground first (simulating flying position), with your harness and risers, before flying with it! The full range is reached when the 2 pulleys join tog ether. Before launch, attach the glid er's risers to the harness with the main karabiners. Ensure that the speed system is untangled and operates freely before flying! T here should be a spare inch or so before they activate. Remember that it is always safer to set the margin of play too big than too small.
13
FLYING THE MACJET
The following information must not under any circumstances be taken as a manual for practising paramotoring. We would like to advise you of the MacJet features and important information for your flying and security.
Preparing for take off:
As for any aircraft a thorough pre-flight check must be made prior to each flight on the MacJet!
Before every launch check lines, risers and canopy for damage! Do not launch with even the slightest damage!
Also check the maillons connecting the lines and the risers. They have to be closed tight.
Put on the harness with maximum care and check the handle of the safety system and that all the flaps of the outer container are fastened securely and correctly. The main karabiner must also be checked carefully. Replace it if any damage is visible, or generally after 300 flying hour s. Finally connect the r isers to your h arness with the m ain karabiners.
Check carefully that they are properly closed.
Attention! Never fly with an open main karabiner! Do not take off if you find any damage on your equipment!
Having unpacked and laid out the paramotoring glider in a slight horseshoe pattern the following checks must be made:
Checklist before every flight:
Preparing the wing:
canopy without any damage
risers without damage
maillons (quick links) closed tight
Stitching of the main lines near the risers are o.k.
all main lines run free from the riser to the canopy, brake lines are free
Before putting on the harness:
warm up your engine and stop the engine before clipping in the risers
rescue handle and deployment pins secure
buckles (leg- ,front riser) closed
main karabiners attached and properly closed
Before takeoff:
the helmet is on and locked
speed-system mounted and connected properly
risers not twisted
the trims are properly set
brake handle and brake lines are free and not twisted
14
FLYING THE MACJET
nothing will get in propeller's way
pilot's position relative to the wing (centred: all lines same tensi on)
the engine delivers full power
wind direction
obstacles on the ground
free airspace
When laying out the glider, the wind direction should be observed. The canopy should be deployed into the wind so both sides of it are loaded symmetrically. The paramotoring glider should be arrange d in a semicircle against the wind. This ensures that the A-lines in the centre section of the canopy will tension befor e the ones at the wing tips. Thus the canopy inflates evenly and an easy launch in the desir ed direction is guaranteed. All lines and risers should be carefully untangled and arranged in a way that they do not catch on anything. It is equally important to unta ngle the brake lines so that they are clear and can not catch on any thing during launch. T he brake li nes shou l d run freely through the pulleys to the trailing edge of the canopy. Make sure the risers are not twisted; this can prevent the brake lines from runn ing freely through their pulleys. It is often impossible to untangle lines during flight. It is important that no lin es are looped around the canopy. Also called a “line-over”, this may have disastrous consequences during take off. Finally connect the risers to your harness by using the main karabiners. Check carefully that they are closed properly.
Launch
The MacJet is easy to launch but with a very weak or zero wind it requires appropriate launch technique. Before take off, recheck the canopy and trimmer setting, the direction of the wind and the air space around you! When the pilot is ready to take off he/she holds all A-risers and the brake handles in each hand. To facilitate differentiation between the risers, the A-lines, including the sleeves on the A-risers, are coloured red. Before take-off, place yourself centrally at the gliders axis. Let the B-, C- and D-ris ers fall into the crook of your arm and hold the A risers with arms outstretched behind you. Pull up the canopy dynamically using the A-risers. (The stronger the h eadwind the less run-up you need to pull the canopy up). After the i nitial effort of inflation, keep applying forward pressure on the A-risers (pushing them forward, not pulling down):
1. Paragliding technique - Once the pressure on the A risers eases. The canopy
should now be directly over the pilot's head . As soon as the glider is above you, stop pulling on the A-risers. A good progressive run ensures your MacJet will inflate and come up equally and quickly. Should the canopy surge forward, control it by gently braking. Now, do a visual check upwards, to ensure the canopy is completely open (otherwise, abort the take-off). Only then is the final decision to continue the launch taken! If anything is not completely safe the launch should be aborted! Now accelerate continuously until you lift off. It is easier to take-off in a light headwind, if after reaching minimum flying speed you apply the brakes slightly. After the take-off, gently release the brakes again. The canopy should be braked gently to stabiliz e the glider and possibly correct for drift. Moving the pilot's body to the centre of the glider is the best method of correction, if there is sufficient room.
15
FLYING THE MACJET
2. Paramotoring technique – Once the canopy is up to the angle of 80° open up full
power and lean back to counter the engine thrust, so that it can push yo u forward rather than towards the ground. Continue to run in this position. When you approac h take off speed gently apply the brak es (max 30% of t he brake ran ge). The faster t he trim setting is, the more brake input is required to take off. Once you have safely taken off, continue heading into the wind with released brakes to gain enough height.
Paraglider pilots, especially those who are used to flying, usually have a tendency when running to lean forward with already slightly applied brakes. When taking off with a paramotor the pilot needs to stand up stra ight and all ow the thrust of the en gine to push pilots body horizontally forward rather than diagonally down. Paraglider pilots starting paramotoring therefore need to lear n how to stand up strai ght while continuing to move forward into wind. Don’t try to get into the seat when you leave the ground as yo u are still relatively low and in the event of an engine failure you will be back on the ground very quickly. Instead, climb to a safe height, into wind, and then gently throttle back before getting into the seat. Properly fastened leg straps before take off makes getting into the harness much easier. If you need to us e your hand be sure to put the brake toggle on the magnet first to avoid it being sucked back into the prop.
WARNING!! Do not jump or lift your legs immediatel y after taking off! This could have dire consequences when done with a paramotor if the wing has not reac hed the proper take off speed.
WARNING!! Do not attempt to get into the seat while holding the toggles. WARNING!! Do not use the forward launch in very strong winds. Make s ure you don't
pull the risers too much towards yourself or downwards as this can result in a frontal collapse, or in an asymmetric take-off
Reverse launch
The MacJet is easy to reverse launch. When doing a reverse launch or when launching in strong winds the paramotoring glider c an possibly surge forward more quickly or lift off sooner than desired. To avoid this, walk uphill following the canopy during inflation. We recommend pulling the trims down 2-3 cm. As this launch techniqu e can be difficult and turning the wrong way can result in the pilot taking off with twisted risers. It is recommended to practice reverse launching on a trai ning hill or slight slope first. When on the flat with your paramotor then only with the engine off. The most important thing is ground handling. You need to be abl e to keep the wing dire ctly into wind while taking off on flat ground. When deflating the c anopy in strong winds, or ab orting a launch, us e the C- or D- risers, not the brakes. Using the brakes in strong wind will cause more lift, lifting the pilot up and dragging him/her much furth er back. A good way to la unch the MacJet in reverse with a stronger wind is using the A lines in th e left hand, along with the left brake toggle and the throttle (if you hav e it on the left side), and the D lines i n the right hand along with the right toggle (and the throttle if you have it on the right side). It is better to start to learn this A and D reverse technique without the paramotor and once you practise a bit you can start with the paramotor. Using this technique the pilot can build a wall directly into wind with the pilot in centre of the canopy.
16
FLYING THE MACJET
Launch the canopy over your head and use the D lines to stop it over shooting. This stops you from applying both brakes (as when using standard reverse launch method) and pushing your hands back towards the propeller. Once the canopy is above your head you release the A and D straps and tur n for 180 degrees i nto wind and accel erate. Once you are safely airborne, continue heading into the wind to gain en ough height. Do not try to climb too steeply by applying too much brake. The additiona l drag caused by brakes decreases actual climbing rate. If there are no obstacles pr esent, it is safer to fly level for a while after take-off and gain some speed before converting it to height. Don`t try to get into the seat when you leave the ground as you are still relatively low and in the event of an engine failure you will be bac k on the gr oun d ver y quick ly. Instead, climb to a safe height, into wind, and then gently throttle back before getting into the seat. Another reason not to try climbing too steepl y is the risk co nnecte d with engi ne failur e at low altitude. Golden rule! For any aircraft the most important thing on take off is a proper amount of speed. High angles of attack and a low speed are more likely to cause a stall. You should always be able to land safely in case of engine failure. Therefore note! Too much brake input d uring take off is ris ky. Depending on the design and power of your paramotor unit, it is possible that you will notice torque moments while not sitting properly in your harness. So be ready to counter-steer with a brake input to correct turning tendency and keep flying straight. You also can compensate torque moments by adjusting cross bracing if present on your harness or by adjusting torque compensator on the opposite riser of the turn tendenc y. Different settings of trims on each riser and shifting you r weight to the opp osite side of the turn tend ency will hel p to keep the glider in a straight direction after take off.
Wind
Trim settings
Launching technique & additional settings
under 1 (m/s) Neutral position
(on the white line) or released for 1-2 cm.
Forward launch
- start with loose lines. 2 steps back toward the canopy to increase the speed of the run.
- start with full help of the thrust
- try to minimize use of the brakes.
- correct position of the wing by moving toward in appropriate direction rather than by using brakes
1 - 3 (m/s)
Neutral
Forward launch
- start with lines under tension
- you can use brakes to correct the position of the wing during the run, but moving in the appropriate direction during the run is most effective technique.
- use of full thrust when canopy at 80°
over 3 (m/s)
Neutral or closed for 1-2 cm
Reverse Launch
17
FLYING THE MACJET
Flight
Once in the air after take off at a higher angle of attack it some gliders may have a tendency to roll under full power. The torque and gyro mom ents lift the pilot to one side; you then drop back only to swing up again. G enerally such roll oscillatio ns usually occ ur with greater engine output and propeller diameter, lo wer wing loading. The more brake input the bigger the roll tendency. In this case the safest way to deal with this is to throttle back a bit and release the brakes. Novice paramotoring pilots tend to be especially prone to overreacting. Do not forget - release the brakes.
The MacJet can reach speeds of 39-43 km/h on neutra l setting d epend ing o n the weight of the pilot. Always fly with sufficient clearance from the terrain. With power off the MacJet glides best with open brakes, descends best with lightly applied brakes and trims closed. We recommend that, to give yourself the chance to get used to it, your first flights should be made on or just below the neutral range of trim settings, where, the glider will feel more familiar, like a conventional wing. With this trim, try to fly with a small amount of brake - at the point where the y just b egin to feel h eav ier. In turbule nt air fly with brakes lightly applied (10-15 cm) to maintain some internal pr essure and avoid canopy collapse. If the canopy pendulums f orward, this should be corrected by prompt application of the brakes. A pendulum move ment of the canopy backwards is correct ed by easing the brakes in good time. When you have become fully confiden t in your wing, try experimenting with slower and faster trim-settings, weight-shift and speed bar and enjoy the extra speed and security the MacJet offers you.
Different trim settings
The MacJet has a wide speed range in flight by virtue of the different trim settings. This may demand higher pilot attention in flight. Anyway once used to it you will appreciate the abilities of the wide speed range.
With the trims fully open (trim buckle over the white line) the wing’s speed increases (good for long transitions). The canopy becomes stiffer and is less sensitive to turbulence and its stability improves. On faster trim setting s or when flyin g on speed bar the brake forces rapidly increase and the handling decreases. When the trims are fully opened and you are not flying close to the gr ound we recommend steering with the wing tip steering handles. It is the special feature of the reflex prof ile - the faster you fly, the safer your glider is. Some pilots with free-flying experience may have a tendency to keep the brakes slightly applied at al l times. Such a technique, while quite reasonable on a free-flying wing, is not advisable for reflex gliders. W hen you app ly the brakes wit h released trims, the wing loses its reflex characteristic (and the advantage of stability) and may be more prone to collapse.
On the slower settings (trim buckle under the white line), sink rate improves and handling becomes lighter, whilst giving you an improved climb rate for thermaling and shorter and slower take-offs and landings. Do not hesitate to use thermals in order to gain some altitude and save fuel.
18
FLYING THE MACJET
Note!! If trims are asymmetrically adjusted, the wing will turn. Therefore trim setting is an important part of the checklist before every flight!
Accelerated flight (speed bar applied)
When flying with the speed system applied the angle of attack is lower and the glider increases flight speed. In contrast to most paragliders it does not decrease wing stability; in fact the reflex gliders seem to counter turbulence even better.
To use the speed system, simply place yo ur feet on the stirrup and push forward in a horizontal plane. If a loss of back pressure of the stirrup o n your l egs is noticed, th is is a warning that the canopy is probably about to collapse. Rel ease the stirrup and thus the speed system immediately. Do not use the s peed system in very turbulent conditions, close to the ground or near other airspace users. Always fly with sufficient clearance from the terrain and always keep the brake handles in your hands!
Warning!! Do not apply brakes when fully accelerat ed! Braking increases lift near the trailing edge. The main lift point moves backwards. Due to this th e wing can loose stability and can lead to frontal or side collapse on accelerated flight. When fully accelerated (maximum speed bar and trims open) using full thrust and you rapidly decrease the thrust (e.g. close the throttle co mpletely) you can cause the “pendulum effect” and then the glider can surge forward which automatically decrease the angle of attack. This also can easily lead to collapse in turbulent air.
At maximum speed-bar and fully open trims we strongly recommend steering with wing tip steering handles. At first learn to fly using the speed s ystem with the trims in neutral position. It is advisable to use the speed syst em with neutral or half opene d trims. T urns executed in this way will be slightly wider, but the strength needed to initiate the turn is smaller then with brakes.
Steering - turns:
The MacJet is a very responsive paramotoring glider and reacts very directly and instantly to any steering input. Weight shift input quickens turns and ensures minimal height loss.
From neutral to closed trim settings the turns can be done much tighter and are more effective using a combined technique while steering with serial brake together with wingtip steering brake. This technique is ver y useful for slalom competitions. Turns can be much improved by additional use of thr ottle weight shift etc. With gro wing experience you will be able to master these techniques and to make fully coor dinated and effective turns.
In case it is impossible to control the MacJet with the brake lines the D-risers may be used to steer and land the canopy. Attention! Pulling brake too fast or too hard can result in the canopy entering a negative spin.
19
FLYING THE MACJET
Study the following drawings of different trimmer setting and speed-system use and their influence to the wing stability.
Released trims without brakes
Preferred setting for fast and safe flying. The centre of gravity of the airfoil is moved forward, the wing has higher resistance to collapses. Pitching moment decreases.
Released trims with brakes applied
The MacJet uses a flap system in the centre o f the wing on the trailing edge for improved take-offs and landings. This provokes more lift in the centre of the wing and also increases the pitching moments. Even slight brake input (especially on full speed bar) produce lift close to the trailing edge. The centre of gra vity of the airfoil is moved back and the higher pitchin g moment significantly decreases the stability.
Warning!! Especially in turbulence th is can lead to a collapse on full speed with trims released! Therefore we recommend pilots only use the wing tip steering system.
20
FLYING THE MACJET
Closed trims
Using this trim setting serial brakes are the normal and predefined steering system. Additional use of the wing tip steering system combined with serial brakes can execute sharper turns. Slower trim setting is used for landing and thermaling. The canopy behaviour is similar to that of classic paragliders.
Approach and Landing:
To avoid excessively demanding situ ations on the appr oach to landing, it is importa nt to initiate the process at an adequate altitude. This leaves you eno ugh time to observe and appropriately deal with wind direction and any other aircraft in your vicinity.
The MacJet is easy to land. T he final leg of the lan ding app roach must be into the wind. There is a choice of two methods of landing with a paramotor. One without power (this minimises the risk of propeller damage) and the second with power.
Power off landing
When approaching the landing spot check the wind direction and your height. Po wer off your engine at about 30m and glide like a paraglid er with trims in the neutral or closed setting and brakes released. During this final glide the glider should be decelerated slowly with regard to conditions, converting your excess speed into lift. The pilot should flare the canopy with his feet just 0,5m over the ground before the touchdown. If too much brake is used too early the glider may climb again, gaining height,. Strong wind landings require correspondingly less br ake. Ever y pi lot sho uld practic e la n dings without power, because one day your engine will fail and you will need this skill.
21
FLYING THE MACJET
Power on landing
Make a flat approach at a shallow angle. While flaring the wing a nd losing speed switch off the engine immediately after touchdo wn. In nil wind conditio ns you should r un a few steps after touchdown and pull the brakes few times dynamically (like a fluttering bird).
This stops the canopy over your head and gives you time to turn and put the glider gently on the ground. Do not apply full brake before the pilot is safely on the ground. Do not turn before the propeller stops turning.
The advantage of this method of course is that if you get it wrong you can power up and go round again at any time. The disadvantages are the increased risk of (expensive) propeller/cage damages if you stuff it up, the dangers involved in falling over with the engine running and getting your lines in the prop eller if you forget to switch off before the wing deflates.
Attention! The final glide during the landing appro ach should be straight a nd not marked by steep or alternating turns as these can result in a da ngerous pendulum movements close to the ground.
Attention! Do not allow the canopy to fall onto the leading edge with energy. This can destroy the material and affects the life of the ribs at the leading edge!
Note!
If possible, get to know the landing field before the approach.
Check the wind direction before planning the approach.
Landing with power off requires much less space.
Training makes the master, practice the landing until you feel totally safe.
TOWING, JUMPS FROM AIRCRAFT, AEROBA TICS
WARNING!! The MacJet is not suitable for towing. WARNING!! The MacJet is not suitable for jumps from aircraft. WARNING!! The MacJet is not designed to be used for aerobatics.
22
EXTREME FLYING MANOEUVRES
WARNING!! All the critical flight conditions described here require thorough knowledge. They should only be carried out during safety training courses (SIV) under proper guidance. Under any circumstances the present descriptions can not be taken as manual for practising the manoeuvres.
This section describes flying conditions whic h can be deliberatel y induced, or which can develop unintentionally due to turbulence or pilot error. Any pilot who flies through turbulence is sure to be faced with these speci al flight conditions at some point. So be aware of these flight manoeuvres and prepare for them by SIV (safety training over water). We expect you are an advanced paramotoring pilot and you already have the proper experience. Mastering these flying c onditions significantly improves your active flight safety. Bear in mind that all disturbances of the canopy can increase the sink rate by 2 - 10 m/sec, depending on the degree of disturbance. Carrying out these manoeuvres wrongly may lead to a crash.
Asymmetric collapse
A negative angle of attack can cause all or part of the leading-edge of the MacJet to collapse (e.g. in very turbulent air). The MacJet will re-open spontaneously from closures of up to 50%. The time this takes, and the associ ated height loss, can ho wever be noticeably reduced by appropriat e action by the pilot. Apply opposite brake on the inflated side, the outside of the curve, to stop the turning movement of the canopy. If you react immediately, 30% brake on the open si de shoul d suffice to hol d the canop y on a straight course. In the event of a big collapse, this braking should be applied very carefully to avoid stalling the remaining infl ated wing. The pilot's correction for direction can be aided by a pumping out the deflation; a slo w, long pumping actio n of the brake of the deflated side of the wing helps the canopy to re-inflate. If the pilot do es not correct, the canopy can enter a stable spiral dive.
“Cravat” / Line-over:
In the event of some lines becoming tangled during flight (caused by whatever), the following action is recommended:
The pilot stabilizes the glider by gently applying the opposite brake. Please be aware that in this condition the brake pressure can be higher and the brake travel shorter.
Without pilot input a line-over will result in a stable spiral dive. Here are the various options to untangle a line-over:
- pumping the collapsed side.
- pulling the stabilizer line or a sharp pull on the D riser can solve the prob lem.
Attention! If these manoeuvres fail or if in any doubt, the pilot shoul d instantly use their emergency parachute system!
23
EXTREME FLYING MANOEUVRES
Frontal Collapse:
When flying with a paramotor the refl ex profile makes it prac tically impossible to induc e a front tuck, except with trim closed setting using special techniques. Such collapses provoked at higher speeds can lead to extremely deep collapse and its recovery requires short and equal application of both brakes.
When experiencing a very large front tuck, a frontal rosette can occur (the wingtips move forwards: forming a horseshoe shape). Short and gentle braking can avoid this deformation.
A quick recognition of the situation and a q uick reaction by braking on both sides for as long as the collapsed wing is beh ind the pilot helps the recovery and limit s the altitude loss.
Parachutal stall (deep stall):
A parachutal stall can be caused by, among other reasons, turbulence at too slow a speed trim or too much brake application when a power unit is added. Porous canopies (UV influence) or canopies out of trim (stretched or shrunken lines) are much more susceptible to a parachutal stall and therefore should not be flown. These are some of the reasons regular checks should be carried out on your glider. A wet canopy or temperatures below zero centigrade (0°C) may also cause a stable parachutal stall.
When releasing the brakes the MacJet will usually spontaneously recover from a parachutal stall within 2-3 seconds. If the canopy remains in a parachutal stall, it is sufficient to release trims or to push the accelerator.
Attention! If brakes are applied while in a parachutal stall, the glider may suddenly enter a full stall!
Full-stall:
Practically does not occur, may happen onl y as a result of serious ne glect or intentional action of the pilot. You have to be careful when flying at lo w speeds until fully familiar with brake operation. The wing recovers spontaneously in the initial phase of stall, otherwise use standard procedures.
To recover from a full stall, smoothly release both brakes simultaneously until 90% of leading edge reopens, then release brakes rapi dly. The glider ends the full stall on its own without surging forward.
WARNING!! If the brakes are rele ased rapidly and asymme trically, the glider ma y surge almost 90° and suffer an extensive asymmetric collapse.
The danger of overcorrecting and overreacting exists during all extreme flight manoeuvres. Thus, any corrective action must be gentle and contro lled and done with feel for the glider!
24
EXTREME FLYING MANOEUVRES
Spin (or negative spin):
Normally it does not occur. You have to be careful when fl ying at low speeds until fully familiar with brake operation. Pulling brake on one side too fast or too hard can result i n a negative spin. During a spin the canopy turns relativel y fast around the centre section of the canopy while the inner wing flies backwards (hence the term negative).
There are two usual reasons for an unintentional spin:
One brake line is being pulled down too far and too fast (e.g. when inducing a spiral dive in slow setting)
When flying at low speed the opposite brake to torque moments is app lied too hard
To recover from an unintentional spin, the pulle d down brake line should be immediately released as soon as a spin is suspected. The canopy will accelerate and return to its normal straight and stable flying position, without losing too much height. If the spin is allowed to develop for some time, the glider surges a long way for ward on one side and a dynamic asymmetric collapse or a line-over can occur. Gently apply the brakes to avoid side or central collapse of the c anopy and the possibility of a cravat (one of the tips becoming entangled in the lines).
WARNING!! If you are LOW and are in an unintentional spin, or if the canopy is c aught in a cravat USE YOUR RESERVE.
Wingover:
To induce a wingover the pilot flies consecutive alternating turns to gradually steepen the angle of bank. During wingovers with a high bank angle, the outsid e wing begins to unload. Further increase of the angle of bank must be avoided, because any poss ible resulting collapse may be quite dynamic!
WARNING! Full-stall, spin and wingover (over 90 degree angle of bank) are prohibited aerobatic manoeuvres and may not be performed during normal flying. Incorrect recovery procedures or overreaction of the pilot may have dangerous consequences! Attention! The MacJet is not designed to be used for aerobatics.
Alternative (emergency) steering:
If for some reason it becomes impossible to control the MacJet with the brake lines th e D-risers may be used to steer and land the canopy. Attention! Of course the range is much shorter (10-15 cm) then with the brakes. It is also possible to control the direction of the flight by pulling on a stabilizer line or by weight-shifting.
25
RAPID DESCENTS
Spiral dive:
Attention! Trim setting in slow or neutral and the power off when executing spiral dive.
A spiral dive is the fastest way to lose altitude, however, the very hi gh G-forces make it difficult to sustain a spiral dive for long and it can place high loads on the pilot and glider. By tensing ones abdominal muscl es and a higher body tensio n you can to some extent resist the high G-forces. Don't forget proper breathing! As soon as any, even slight, light dizziness or impaired vision is noticed the spiral should be exited immediately.
The MacJet has a very effective spiral dive. T his allows rapid descent without stalling. To enter a spiral dive the pilot should weight-shift on one side while slowl y pulling the brake gradually on the same side as weight-shifting. During a spiral dive the angle of bank can be controlled by increasing or reducing the amount of inside brake. When spiral diving the MacJet it is recommended that the outside brake is lightly applied. T his helps stabilize the wing and enables an easier and safer exit from the spiral. To exit, release the inside brake slowly. The MacJet did not show a tendency to remain in a stable spiral during testing. At high sink s peeds or if the pilot keeps his weight on the inside, the wing can stay in a continued deep spir al and ha s to be activ ely exited. This is done by weight shifting to the outside and gentle braking of the outside wing.
WARNING!! Nearly all gliders will have a tend ency to stay in the spiral if the sink-rate exceeds around 15-m/s, depending on weight -shifting, wing loading and G-force. In fact most gliders need a counter-input to end a turn.
Attention! Due to energy retention, the glider will climb a lot after a deep spiral-dive release. If you apply inner brake and decelerate the glider for two or three turns, big pendulum effects can be avoided.
WARNING!! Practise spiralling with caution and lower sink-rates to get a feel for the gliders behaviour. A pilot who is dehydrated or not accustomed to spiralling can lose consciousness in a steep spiral dive!
WARNING!! Never do big ears in spiral ! In this manoeuvre a smaller number of lines is carrying an excessive load multiplied b y the centrifugal force, what can lead to dam age of the lines or even the paraglider itself.
Big ears:
As there is a lot of load on the “A’s” especially on the faster trim settings as we do not recommend using big ears as descent techniqu e under power. With a hard pull on the outermost A-lines there is higher risk of collapse. A spiral may be a more efficient way to get down.
When in big-ears without power, the horizontal speed is higher than the si nk rate, unlike a spiral dive or a B-line stall. This rapid descent technique is used to quickly and horizontally exit a dangerous area in the desired direction. In order to collapse the outside wing, pull the outside A-lines.
26
RAPID DESCENTS
When the pilot holds the outside A1-risers on both sides and pulls them down, the MacJet easily tucks the outside wings and enters a stable descent mode. The pilot keeps hold of the brake handles along with the outside A1-risers in his hands. By braking on one side and weight-shifting, the canopy remain s steerable.
In order to increase the sink rate as well as the h orizontal s pee d, this m anoeuvr e sh ould be done together with use of the speed system. Apply t he speed system after big ears are induced (step into the speed-bar before you grab the outer A1-risers). Big-ears substantially reduce the risk of canopy stability problems in turbulent air. To exit Big­ears release the A1-risers. The canopy does slo wly self-recover. If not, or t o quicke n the recovery, the pilot can gently apply brakes to the glider.
WARNING! Never do big-ears in spirals, as this may drastically reduce the number of lines taking the already high loads, causing structural failure.
B-line stalls:
As there is a lot of load on the “B’s” as we do not recommend using B-Stall as descent technique under power.
To induce a B-line stall without power, symmetrically pull do wn slowly on both B-risers, until the canopy folds (parallel to its long axis). The airflo w over the top surface is almost fully detached and the canopy enters a vertical descent flight mode without forward movement. Further pulling of the B-risers reduces the surface area more and increases the sink rate. (Up to 8 m/s) Be careful, pulling too far or too rapidly m ay cause a frontal horseshoe to form. To exit from this flight mode release t he B-risers at first rapidly but then gently (1 sec). The canopy surges forward re-attaching the airflow over the top surface and resumes normal flight. When the B-risers are released, the brakes should not be activated. This will give the canopy t he chanc e to gain s peed an d resume normal flight. On exit from a B-line stall on no account just release the B-risers, as this can cause overloading. If canopy does not recover apply both brakes gently to recover or pull the A-risers, until the canopy regains forward speed.
Summary:
For all extreme manoeuvres and rapid descents please note:
first practise manoeuvres with an instructor during safety training!
before inducing any manoeuvre the pilot must check that there are no other
airspace users below him!
during the manoeuvre the pilot must have the canopy within his view!
27
GOLDEN RULES
Always carry out full pre-flight checks before launching.
Never place your paramotor downwind of the glider.
Check that there is no fuel leakage. Do you have enough fuel for the flight? It is
always better to have too much than to need an emergency la nding.
Check for any loose articles th at could trail or fall into the propeller while fl ying and
fasten them securely.
If you spot a problem, no matter how small, fix it at once!
Always put on and secure your helmet before getting into the harness.
Do not ask for trouble - do not fly over water, between trees or power lines and
other places where engine failure will leave you helpless.
After lan ding, control the wing facing the direction of flight to keep the li nes out of
the propeller. You should only turn to face the glider to av oid fallin g back wards onto your paramotor.
Do not take a risk - do not fly over water, between trees or power lines and other
places where engine failure will leave you helpless.
Keep in your mind the turbulence caused by other powered gliders, especially
heavy trikes.
Keep in mind the turbulence caused b y yo urself, esp ecially whe n flying s harp tur ns,
spiralling or flying low.
It is unwise to fly hands-off below about 100m, because a possible power unit
malfunction may require immediate attention.
Unless it is absolute ly necessary (e.g. collision avo idance), do not make tight turns
against the torque moments. During steep climbs you easil y can enter a stall under power and consequent negative spin.
Never trust yo ur engine! It can stop at any moment. Always fly the wing prepared
for this, especially at low altitudes.
Avoid downwind low flying. It drastically reduces your options!
Do not wait for the problem to grow. Be se nsitive and ready to listen. A noticeable
change in engine tone or a new vibration m ay indicate trouble. Land and check it out.
Be certain of your navigation
Not everyone is a friend of your paramotor noise. Keep within the rules and the
laws. Care must be taken when flying near livestock and animals.
28
LOOKING AFTER YOUR GLIDER
Looking after your canopy correctly will prolong the life of your paramotoring glider.
Deterioration: a few tips!
The canopy is mainly made of NYLON, cloth which, like any synthetic material,
deteriorates through excessive exposure to UV. Hence, it is recommended that you reduce UV exposure to a minimum by keeping the paramotoring glider packed away when not in use. Even when packed in the bag do not leave it in the sun.
Keep the canopy and lines clean as dirt may penetrate into the fibre and damage
the lines or the cloth.
Ensure that the lines are not folded tightly. It's extremely important to avoid any
sharp bending of the lines, especially the main lines. Pay careful attention to the lines to avoid damaging them. Any over stretching of lines apart from the strain imposed during normal flight, should be av oided as over stretching is irreversible.
Be careful, not to allow snow, sand or stones to enter inside the canopy's cells: the
weight can change the angle of attack, or even stall the glider; additionally the sharp edges can destroy the cloth!
Check line lengths after tree or water landings. They can stretch or shrink lines.
Never drag the wing over rough ground! This will damage the cloth on the wear
points. When preparing the wing on a takeoff with rough gr ound, don't pull the wing over it (i.e. by pulling the brakes). Please try to pack the wing on soft ground.
Uncontrolled strong wind takeoffs or landing s can result in the leading edge of the
canopy hitting the ground at high speed which may cause rips in the profile and damage the rib material.
Clean the paramotoring glider with fresh water after contact with salt water. Salt
water crystal can reduce line strength, even after rinsing in fresh water. Replace lines immediately after contact with salt water. Also check canopy material after water landings, as waves can place uneven forces and cause cloth to distort in specific areas. Always remove gliders from the water by holding only the trailing edge.
Prevent lines from catching on anything as they may be ove r stretched. Do not step
onto the lines. Although the lines were tested with a bending test they can be damaged if stepped on whilst on a hard surf ace, or if they come into contact with sharp objects.
Do not always fold the canopy symmetrically to the centre cell as this can cause
constant stress on the centre cell (centre cell always to the outside).
Clean the paramotoring glider with water and a soft sponge. Do not use any
chemicals or spirits for cleaning, as these can permanently damage the cloth.
29
LOOKING AFTER YOUR GLIDER
Storage:
Store the paramotoring glider in a dry space at ambient temperature away from
chemicals and UV light.
Never pack or store the glider wet. This shortens the life of the cloth. Always dry
glider thoroughly before any packing or storage.
During transport it has to be considered, that some materials of the paramotoring
glider are temperature sensitive. Avoid subjecting your wing to high temperatures (e.g. the luggage space of a parked car in the sun)!
Keep it lonely. Insects, such as grass-hoppers an d a nts will simpl y eat th eir way out
if rolled up with the wing. Grazing cattle can literally lick the co atings off the fabric and mice love to make homes in canopies ! Therefore hang up your wing in its bag during long term storage.
When sending your wing as a parcel, take extr a care with packing.
Repairs and checks:
Tears in the canopy must be professionally sewn. Adhesive patches are only
adequate for very minor damage.
Repairs should only be carried out by the manufacturer, distributor or authorized
workshops. Only original spare parts may be used!
The lines m ust be checked after every 50 hours flying time and whenev er the flight
behaviour changes
Any changes to the canopy lines or risers, except those approved by the
manufacturer, will void the certificate of airworthiness.
The MacJet must be checked as a minimum, after two years or after 100 flying
hours by the manufacturer or authorized workshops.
Disposal:
The synthetic materials used in a paramotoring glider need professional disposal.
Please send disused canopies back to us: we will dismantle and dispos e of it.
In Conclusion:
The MacJet is a modern paramotoring glid er. You will enjoy many safe years of flying with your MacJet if you look after it correctly and adopt a mature and responsible approach to the demands and dangers flying can pos e.
It must be clearly understood that all air spor ts are potentially dangerous and that you r safety is ultimately dependent upon you. We strongly urge you to fly safely. This includes your choice of flying conditions as well as safety margins during flying manoeuvres. We recommend once more that you only fly with a certified harness, reserve parachute, and
30
LOOKING AFTER YOUR GLIDER
helmet. Also the certification placard must be present on the g lider. Every pilot should be suitably qualified, have a valid license and 3rd party insurance.
The MacJet is delivered with a stuff-sack, Velcro compression strap, MAC PARA backpack, repair kit and user manual.
Warranty
MAC PARA guarantees free of charge repairs caused by the material or production faults according to the following scheme:
For powered flying the warranty covers 24 months (2 years) or 200 flight hours (whichever comes first).
Warranty does not cover:
canopy colour fading
damage caused by chemicals or salt water
damage caused by incorrect use
damage caused by emergency situations
damage resulting from accidents (airborne or not)
Warranty is only valid if :
every flight is correctly registered in the logbook of the wing
conditions, temperatures of each flight are registered in the logbook
the paraglider is handled in accordance with the operating manual
the purch aser has not carried out any repair by him/herself (excl. mi nor repairs with
self-adhesive patches)
carried out any modifications
the paraglider has been inspected according to prescribed timetable.
If you have bought your paraglider second-hand, ask the previous owner of the paraglider for a copy logbook (total of flying hours since the date of first purchase and details of any checks).
TREATING NATURE WITH RESPECT
Finally the call to practise our sport with respect for nature and wildlife! Not everyone is a friend of your paramotor noise. Follow the rules and the laws. Care must be taken when flying near livestock and animals.
31
LINE PLANS
Riser lengths - MacJet
A A1 B C D
Trims in neutral position 520 520 520 520 520 Trims closed ( slower ) 520 520 520 495 480 Trims open ( faster ) 520 520 520 580 640 Accelerated + trims in neutral 320 370 420 470 520 Accelerated + trims open * 320 370 420 530 640
The lengths are measured from main attachment point to the lower edge of rapid links.
* Read more on the page 19.
Line descriptions:
The following printed line plans show the line configurations and line lengths.
Line strengths in colours
Background color at a length determines line material it is made.
A
ramid/Polyester A-6843-060
A
ramid/Polyester A-6843-080
A
ramid/Polyester A-6843-120
A
ramid/Polyester A-6843-160
A
ramid/Polyester A-6843-240
A
ramid/Polyester A-6843-340
A
ramid/Polyester A-7343-140
A
ramid/Polyester A-7850-080
A
ramid/Polyester A-7850-100
Dynema/PolyesterA-7850-240
32
Line plan MacJet – 22 (S)
33
Line plan MacJet – 24 (M)
34
Line plan MacJet – 26 (L)
35
Line plan MacJet – 28 (XL)
36
Line plan MacJet – 31 (XXL)
37
MANUAL FOR PARAMOTORING GLIDER CHECKS
Check-intervals
All paramotoring gliders used in flight must be checked at least every 24 months. For paramotoring gliders used by paramotoring schoo ls the period is 12 months.
Personnel authorised to carry out checks
A valid flying license and training course by National association are the basis for permission to carry out paramotoring glider checks
Identification of glider
An identity sticker with details of certification and serial number is attached to the glider.
Components of the check
Porosity
The porosity should be checked with a porosity meter (JDC). Compare the resultant data with the producer's manual.
Porosity measures should be taken on at least three point s of both the top and bottom surface. The first point should be placed 20-30 cm from leading edge in the middle of canopy. Second and third points are placed left and right from first measure point at 25% of the span. One additional measurement should be made on the top surface of the wing tip.
The identified time should be higher than 30 second (JDC). In the event of the result being less than 30 seconds, the result of the check is a fail.
Overall strength check
The check of canopy strength should be made with a Bettsometer (B.M.A.A approved Patent No. GB 2270768 Clive Betts Sales). On the top and bottom surfaces make small holes with a needle at the A-line attachment points. The exact verification should be made in accordance with the Bettsometer user manual.
Line strength check
Line strengths should be as specified in accordance with the certification requirements. One main line should be taken from each array and have its strength checked with a tension-meter.
Required strengths should be higher than:
A + B main lines x measur ed value > 8 x maximum take-off weight and higher
then 800 kg for the A + B arrays.
C + D mean lines x measured value > 6 x maximum take-off weight and higher
then 600 kg for the A + B arrays.
Replacements for damaged lines must be with ne w original lines. Lin e lengt hs are taken from the lines data page.
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MANUAL FOR PARAMOTORING GLIDER CHECKS
Line length measurement
Lines should be separated and each line measured under a tension of 5 kg. Measurement is made from the line karabiner to the canopy accordin g to the method of certification. Rib numbering begins in the middle of canopy and leads to the wing tip.
Measured full lengths should be documente d in the ins pection rec ord and are compared with certified full line lengths protocol. Lengths sh ould not differ by more than 20 mm. The opposite sides should be checked for symmetry.
Canopy line-attachment points check
Attachment points should be checked for damage and stretching. Defects, loops and flares should be repaired.
Canopy fabric check
Ribs, diagonal ribs, top and bottom surface should be checked. Any damage to sewing or tears to the fabric, which could influence flying characteristics must be repaired.
Lines
All lines should be checked for tears, breaks any damage to the sheath or signs of wear. Special attention should be paid to the se wing of the li ne loops. Dama ged lines must be replaced.
The results should be documented in the inspection record.
Connector check
All line carabineers, trims (if used), speed systems and pull eys should be inspected for visible damage. Open or improperly secured connectors should be secured in accordance with the producers recommendations.
Risers
Both risers should be checked for tears, signs of wear or any damage and measured with a pull of 5 daN strength. Measured dat a should be documented in the inspection record. The difference must not be higher then 5 mm when compared to specified lengths.
Final check
The glider sticker and check sticker must be inspected f or readability and correctness. The check must be documented with date, signature and stamp on the canopy and in the user manual.
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TEST FLIGHT CERTIFICATE
Paramotoring glider type: MacJet –
Serial number: _________________________________
Test flown on: _________________________________ by
MAC PARA TECHNOLOGY
_________________________________
Confirmation by dealer: _________________________________
TECHNICAL SPECIFICATION
Paramotoring (reflex) glider MacJet MacJet MacJet MacJet MacJet Size 22 24 26 28 31
Zoom flat [%] 88,0 92,5 96 100 104,5 Area flat
[m
2
]
22,02 24,33 26,21 28,44 31,06
Area projected
[m
2
]
19,06 21,06 22,68 24,61 26,87 Span flat [m] 10,73 11,28 11,71 12,2 0 12,75 Span projected [m] 8,54 8,98 9,32 9,71 10,15 Aspect ratio flat - 5,23 5,23 5,23 5,23 5,23 Root cord [m] 2,45 2,57 2,67 2,78 2,91 Cells [kg]5858585858 Weight [kg] 5,8 6,0 6,3 6,6 7,0 Weight range * [kg] 77-100 85-110 100-130 115-147 140-180 Min.speed [km/h] 24-26 24-26 24-26 24-26 24-26 Speed Trimmers closed [km/h] 40-43 40-43 40-43 40-43 40-43 Speed Trimmers open [km/h] 49-52 49-52 49-52 49-52 49-52
Top speed (accelerator) [km/h] 60-63 60-63 60-63 60-63 60-63 Glide ratio - 8,2 8,2 8,2 8,2 8,2 Min. Sink rate [m/s] 1,3 1,3 1,3 1,3 1,3
* powered pilot equipped = weight naked + cca. 35 - 40 Kg
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