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19

Check-intervals

All paragliders used in flight must be checked at least every 24 months. For paragliders 
used by paragliding schools 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 paraglider checks

Identification of glider 

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 the Aline 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 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 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

Line length measurement

Canopy line-attachment points check

Canopy fabric check

Lines 

Connector check

Risers 

Final check 

Lines should be separated and each line measured under a tension of 5 kg. Measurement 
is made from the line karabiner to the canopy according to the DHV method. Rib numbering 
begins in the middle of canopy and leads to the wing tip. 
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 
sides should be checked for symmetry.

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

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. 

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.
The results should be documented in the inspection record.

 All line carabineers, trimmers (if used), speed systems and pulleys should be inspected for 
visible damage. Open or improperly secured connectors should be secured in accordance 
with the producers recommendations.

Both risers should be checked for tears, signs of wear or any damage and measured with a 
pull of 5 daN strength. Measured data should be documented in the inspection record.   The 
difference must not be higher then 5 mm when compared to specified lengths.

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 
user manual.

Summary of Contents for VELVET

Page 1: ...MAC PARA TECHNOLOGY LTD 1 máje 823 756 61 Rožnov 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 ...

Page 2: ...ety The VELVET is designed for paramotoring and will enable pilots to get maximum enjoyment The Velvet is also suitable for paragliding 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 and paramotoring are sports which demands besides the optimum equipment a high degree of attentiveness good judgement and t...

Page 3: ... VELVET 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 a standard set up and its speed can reach 39 43 ...

Page 4: ... other damage You must also check the 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...

Page 5: ...ust pull 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 Motorized flight and towed flight To make faster flight possible the VELVETis equipped with a special speed system To accelerate the paraglider we r...

Page 6: ...lines on the closed side If it is tangled pumping the brake line should help WARNING 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 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 stop rot...

Page 7: ...in an unintentional spin 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 Initiation Pull the brakes slowly down until you...

Page 8: ...position of the trimmers A pilot who is dehydrated or not accustomed to spiralling can lose 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...

Page 9: ...8316 ISNY IM ALLGEAU GERMANY Main lines A2 A3 B2 B3 Aramid Polyester A 6843 240 Breaking Load 340 kg KOLON INDUSTRIAL CO 45 MU KYO DONG JUNG GU SEOUL KOREA NYLON TAPE 13 mm Breaking Load 110 kg Güth Wolf GmbH Herzebrockestr 1 3 33330 Gütersloh Germany Polyestertape 20 mm Breaking Load 1100 kg AMANN SÖHNE GmbH Co Industriestrasse 1 74391 ERLIGHEIM GERMANY High Tenacity Polyester Yarn 150 D 3 225D 3...

Page 10: ...0 19 19 18 18 15 15 16 16 17 17 14 14 13 13 12 12 8 8 11 11 10 10 9 9 7 7 6 6 5 5 4 4 3 3 2 2 1 1 D6 A2 A28 A29 C29 C28 18 LINE PLAN BD 2 2 1 1 28 28 27 27 26 26 25 25 24 24 23 23 22 22 18 18 19 19 17 17 15 15 16 16 14 14 11 11 13 13 12 12 20 20 21 21 7 7 6 6 5 5 10 10 8 8 9 9 4 4 3 3 28 28 27 27 26 26 25 25 24 24 23 23 21 21 22 22 20 20 19 19 18 18 15 15 16 16 17 17 14 14 13 13 12 12 8 8 11 11 10...

Page 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...

Page 12: ...5 Root cord m 2 47 2 60 2 73 2 87 Cells 56 56 56 56 Weight kg 6 1 6 4 6 7 6 9 Weight range free flight kg 60 80 70 90 80 105 100 125 Weight range powered kg 85 125 93 140 107 160 133 190 Min speed km h 23 25 23 25 23 25 23 25 Max speed free flight km h 37 39 37 39 37 39 37 39 Max speed powered km h 39 43 39 43 39 43 39 43 Top speed accelerator km h 51 53 51 53 51 53 51 53 Top speed long trimmers k...

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