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19

Check-intervals

Personnel authorised to carry out checks

Identification of glider

All paragliders used in flight must be checked at least every 24 months. For paragliders

used by paragliding schools the period is 12 months.

A valid flying license and training course by National association are the basis for

permission to carry out paraglider checks

An identity sticker with details of certification and serial number is attached to the glider.

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 points 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.

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 theAline attachment points. The exact verification should be made

in accordance with the Bettsometer user manual.

Line strengths should be as specified in accordance with the DHV 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 measured value > 8 x maximum take-off weight and higher then

800 kg for theA+ B arrays.

- C + D mean lines x measured value > 6 x maximum take-off weight and higher then

600 kg for theA+ B arrays.

Replacements for damaged lines must be with new original lines. Line lengths are taken

from the lines data page.

Components of the check

Porosity

Overall strength check

Line strength check

MANUAL FOR PARAGLIDER CHECKS

20

Linelengthmeasurement

Canopyline-attachmentpointscheck

Canopyfabriccheck

Lines

Connectorcheck

Risers

Finalcheck

Lines should be separated and each line measured under a tension of 5 kg. Measurement

ismadefromthelinekarabinertothecanopyaccordingtotheDHVmethod.Ribnumbering

beginsinthemiddleofcanopyandleadstothewingtip.

Measured full lengths should be documented in the inspection record and are compared

with the DHV type protocol. Lengths should not differ by more than 20 mm. The opposite

sidesshouldbecheckedforsymmetry.

Attachment points should be checked for damage and stretching. Defects, loops and

flaresshouldberepaired.

Ribs, diagonal ribs, top and bottom surface should be checked.Any damage to sewing or

tearstothefabric,whichcouldinfluenceflyingcharacteristicsmustberepaired.

All lines should be checked for tears, breaks any damage to the sheath or signs of wear.

Special attention should be paid to the sewing of the line loops. Damaged lines must be

replaced.

Theresultsshouldbedocumentedintheinspectionrecord.

Alllinecarabineers,trimmers(ifused),speedsystemsandpulleysshouldbeinspectedfor

visibledamage.Openorimproperlysecuredconnectorsshouldbesecuredinaccordance

withtheproducersrecommendations.

Bothrisersshouldbecheckedfortears,signsofwearoranydamageandmeasuredwitha

pullof5daNstrength.Measureddatashouldbedocumentedintheinspectionrecord. The

differencemustnotbehigherthen5mmwhencomparedtospecifiedlengths.

The glider sticker and check sticker must be inspected for readability and correctness.

The check must be documented with date, signature and stamp on the canopy and in the

usermanual.

Содержание MAGUS XC

Страница 1: ...MAC PARA TECHNOLOGY LTD 1 máje 823 756 61 Ro nov pod Radhoštìm Czech Republic Tel 420 571 842 235 Tel fax 420 571 842 332 e mail mailbox macpara cz www macpara com USER MANUAL MAGUSxc ...

Страница 2: ...r with maximum possible safety The MAGUS XC is designed for thermal and cross country flying and will enable pilots to get maximum enjoyment Please read this manual carefully before you start this way you will get the most out of your glider and enjoy many nice flights Paragliding is a sport which demands besides the optimum equipment a high degree of attentiveness good judgement and theoretical k...

Страница 3: ...itions 4 Construction Trim Safety equipment The MAGUS XC is a third rib diagonal construction paraglider Every third main rib is attached to the lines and other ribs are attached at A B C and D points thanks to the diagonal ribs These ribs lead to top surface of canopy Line geometry and a system of load bearing tapes between top lines cascades give the canopy stability The glider is delivered with...

Страница 4: ...he harness after a hard landing 6 Check whether the rescue system is correctly installed and secured 7 Inspection of the karabiner Inspection of the attachment and securing of the karabiner Find a suitable take off spot from which you can abort the take off at any point After checking the glider following the checklist lay it out with the cell openings upwards so that the canopy forms the shape of...

Страница 5: ...l the brakes as abruptly as possible This dynamically increases the angle of attack and gives you the maximum braking effect Flight Steering Approach and landing Turns with brakes Turns with brakes and weight shifting 8 Flight with speed system Towed and motorized flight To make faster flight possible the MAGUS XC is equipped with a special speed system To accelerate the paraglider we recommend th...

Страница 6: ...g the brake lines on the closed side If it is tangled pumping the brake line should help Take care to avoid applying too much brake when pumping out the deflation as this may disrupt the airflow over the canopy and lead to a stall Asymmetrical collapse Initiation 10 WARNING NOTE In the case of a cravat which pumping of the brakes fails to release apply 50 70 brake on the open side of the canopy to...

Страница 7: ...pin or if the canopy is caught in a cravat USEYOUR RESERVE Spin negative spirals Full stall Stalls Turbulence or rapid braking can lead to a pendulum effect and thus to changes in the angle of attack In extreme cases this can make the airflow break away from the upper surface of the canopy even without the brakes being activated Pull the brakes slowly down until you have no more forward speed The ...

Страница 8: ...consciousness in a steep spiral dive Spiral dive 14 Fly as far as possible from steep rises to give yourself space to lose height Sink rate approximately 3 5 m sec Sink rate approximately 4 6 m sec This allows rapid descent without stalling Sink rate depending on pilot 5 20 m sec Sink rate approximately 5 8 m sec End the stall with sufficient time for the airflow to re establish itself In principl...

Страница 9: ...es Dynema DC 60 DC 100 Main Lines A1 B1 C2 C3 D1 D2 Gin Teijin Aramid Polyester 1 6 220 kg Main Lines A2 A3 B2 B3 Gin Teijin Aramid Polyester 1 8 280 kg Main Lines C1 Gin Teijin Aramid Polyester 1 4 140 kg Stabilo Line Gin Teijin Aramid Polyester 1 1 80 kg Main Brake Liene Gin Teijin Dynema Polyester 2 3 240 kg NYLON TAPE 13 mm Breaking Load 110 kg Polyestertape 20 mm Breaking Load 1100 kg ROSENBE...

Страница 10: ...br10 br17 st1 st2 stD C30 C33 C36 mC3 C15 C18 C21 C24 C27 sC2 sC2 mC2 C3 C12 C6 C9 mC1 sC1 sC1 sC1 D12 D9 D6 D3 C4 br4 br22 18 LINE PLAN BD stA stB stC stE st0 br2 br1 br3 br4 br5 br6 br8 br9 br19 br7 br20 br12 br13 mBR br21 br11 br16 br15 br14 br18 br22 br10 br17 D15 D21 D24 D27 D18 st1 st2 D30 D36 D33 sD2 sD2 stD mD1 mD2 B3 B30 B15 B12 B21 B24 B33 B36 B27 sB2 B6 B9 mB3 mB2 mB1 sB1 sB2 B18 ...

Страница 11: ... measured value 6 x maximum take off weight and higher then 600 kg for theA B arrays Replacements for damaged lines must be with new original lines Line lengths are taken from the lines data page Components of the check Porosity Overall strength check Line strength check MANUAL FOR PARAGLIDER CHECKS 20 Linelengthmeasurement Canopyline attachmentpointscheck Canopyfabriccheck Lines Connectorcheck Ri...

Страница 12: ...106 Area flat m 2 21 53 24 21 26 00 29 21 Area projected m 2 19 11 21 49 23 08 25 93 Span flat m 11 58 12 28 12 73 13 49 Aspect ratio flat 6 23 6 23 6 23 6 23 Root cord m 2 32 2 46 2 55 2 70 Cells 75 75 75 75 Weight kg 6 1 6 4 6 7 7 1 Weight range kg 70 85 80 95 90 110 105 130 Min speed km h 23 25 23 25 23 25 23 25 Max speed km h 37 39 37 39 37 39 37 39 Top speed accelerator km h 52 55 52 55 52 55...

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