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Mars ATL-15 SL, Руководство по эксплуатации и обслуживанию

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7 

CHAPTER I 

 

Technical description of emergency parachute ATL - 88/90 - 1B (ATL-15 SL) 

 

 

1. 

Designation   

 

Emergency parachute ATL 

– 88/90 – 1B (ATL-15 SL), (hereinafter referred to as 

the  parachute)  is  designed  as  personal  parachute  assemblies  for  flight  crew 
equipment and for passengers in emergency situation. 
The  parachute  complies  with  standards  of  European  technical  standard  order 
ETSO C23d and standard SAE AS8015B.  

 

 

 

2. 

Technical parameters 

 

a) 

Basic parameters 

         - Canopy area   

 

            

 

36 m

2

 

         - Max. parachute mass:  
           Part number   09996   

5,9 kg      with metal parts H335 + H 337 

                                   09995    

6.4 kg      with metal parts H405 + H 323 

                                   09994    

6.5 kg      with metal parts H395 + H 323 

 

The parachute mass are defined without the portable bags and back 
padding.  

 
         - dimensions of the packed parachute    length 

530 mm 

   

 

 

 

 

                  width 

330 mm 

   

 

 

 

                            height 

80 mm 

 

- force required for pulling out the ripcord   

23 ÷ 97 N 

 

b) 

Design 

        The parachute is made in three designs. 

 

c) 

Functional parameters

  

 

- average vertical descent speed 

                  at load G = 122 kg 

 

 

 

 

up to 7.1 m.s

-1

 

- 

turning by 360° 

 

 

 

           8.6 s 

 

d) 

Limiting of parachute using: 

                 - max. operating weight 

 

 

 

122 kg (269 lb) 

                 - max. operating speed (at the moment   

         of the container opening)   

 

 

278 km.h

-1

 (150 kt EAS)                                                                                      

- min. allowable altitude of the use              

100 m AGL 

   at the aircraft speed   

 

            

110 km.h

-1

 

                - environmental immunity 

 

                     from - 40 to + 93.7 

°C

 

 

 
 
Note:  The  parachutes  showed  the  reliable  function  at  the  tests  with  the  loaded 

weight  147  kg  (324  lb)  -  max.  operating  weight  x  1,2  at  the  speed         
333,6 km.h

-1 

(180 kt EAS)  - max. operating speed x 1,2.     

Содержание ATL-15 SL

Страница 1: ...1 TECHNICAL DESCRIPTION OPERATION AND MAINTENANCE MANUAL for Emergency parachute ATL 88 90 1B ATL 15 SL number P 006 15 Number of issue 2 Date of issue 14 12 2016 Validity from serial number 1645001...

Страница 2: ...2...

Страница 3: ...l is obliged to record the received changes in the List of changes and replace the invalid sheets for the applicable sheets The changed or amended parts of the text will be indicated on the side by me...

Страница 4: ...4...

Страница 5: ...5 TECHNICAL DESCRIPTION OPERATION AND MAINTENANCE MANUAL for Emergency parachute ATL 88 90 1B ATL 15 SL number P 006 15...

Страница 6: ...instructions 19 2 Inspection of the parachute before packaging 19 3 Packaging tools 20 4 Parachute package 20 CHAPTER III Instructions for using the parachute 1 Preparation of the parachute before fl...

Страница 7: ...23 The parachute mass are defined without the portable bags and back padding dimensions of the packed parachute length 530 mm width 330 mm height 80 mm force required for pulling out the ripcord 23 97...

Страница 8: ...achute logbook marked as COPY Visual inspection of the parachute can be performed at the manufacturer s site An entry specifying the parachute s condition is made into the Check sheet If the parachute...

Страница 9: ...1 Static line application After leaving the aircraft the effects of the weight of the paratrooper s body and of the static line anchored on board the aircraft will cause the checking bonds to break a...

Страница 10: ...IV Canopy V 070 2A 1 pcs V Harness PS 041 1A 1 pcs VI Container OP 094 1B 1 pcs VII Ripcord U 094 1 pcs VIII Back padding P 032 1 pcs IX Portable bag G 225 1 pcs On user request static line available...

Страница 11: ...cond end includes the attached extension 4 from polyamide cord fitted with ribbon closure 5 for connecting the extension to the container and with two pins 6 designed for closing the container The sta...

Страница 12: ...ed with 15 mm strap The pole vent is reinforces with pole vent cords 8 The rear part of the canopy includes two fields 9 partially filled with curtain woven fine which provides the stability forward s...

Страница 13: ...13 Fig 5...

Страница 14: ...re of the leg straps on the pilot s legs The container is designed for placing the canopy with the lines bridle and the pilot chute The container is made of polyamide or polyester fabric in the shape...

Страница 15: ...of the metal hose 9 is sewn to it for the ripcord wire On the right from the upper side centre it includes a sewn ribbon closure 44 for the connection of the static line extension It is also fitted w...

Страница 16: ...16 Fig 6...

Страница 17: ...k padding is designed for comfortable pilot leaning in the aircraft seat The external parts of the back padding are made of cotton canvas 1 and airtight polyamide fabric 2 interior area is fitted with...

Страница 18: ...olyamide canvas in the shape of a block with dimensions 550x400x170 mm The upper part of the bag includes a zip 1 for closing the bag The portable bag includes two holders 2 and a pocket sewn on the s...

Страница 19: ...red threads with 49 to 68 8 N strength 1 8 During the parachute packing we recommend to protect the canopy from direct sunlight 2 Inspection of the parachute before packaging 2 1 The inspection is com...

Страница 20: ...closures for damage 2 1 9 Inspection of the portable bag Check the fabric stains holder straps and the state of zip for damage 2 2 Damaged parts replacement The operation enables to replace the parts...

Страница 21: ...h way the lines No 1 to 10 were placed on the right and the lines No 11 to 20 on the left fig 10 Pass the ripcord wire with the lug through the ripcord hose The ripcord handle is located into the pock...

Страница 22: ...22 Fig 12 Fig 13...

Страница 23: ...3 The unfolded right half of the canopy is thrown over the folded left side fig 14 and folded identically to the left half fig 15 The field between lines No 1 and 20 is placed to the left Fig 14 Fig 1...

Страница 24: ...24 The canopy at the lower edge is folded from the lines at an angle 45 fig 16a and the left and right half of the canopy is folded to one half fig 16b a b Fig 16...

Страница 25: ...25 Such folded canopy is folded to thirds in such way that the canopy right side is placed and then the left canopy side on top and the canopy is secured with weights fig 17 Fig 17...

Страница 26: ...r its left side and the rubber bands on the left side of the closing flap are passed through the openings in the metal grommets in the right side of the closing flap fig 19b The front side of the clos...

Страница 27: ...27 Fig 19 a b c d e...

Страница 28: ...the lines placing for correctness 4 6 Placing of the canopy into the container Risers of the harness are bent into the container Attach the red threads with strength 48 to 69 N to the red tape loops s...

Страница 29: ...eads are cut at distance 15 to 20 mm from the nodes fig 22 The same task is performed for the second riser Fig 22 Within compliant distance from the risers pass the lines through the rubber bands at t...

Страница 30: ...lines is bent crosswise with the container and attached to the lower flap edge fig 24 Fig 24 Such prepared canopy is then inserted into the area below the lower container flap fig 25 Pass the auxiliar...

Страница 31: ...py is placed in S shape above the closing cord lug until the whole area of the container bottom is filled Fig 26 Part of the canopy below the upper edge is placed in S shape into the elastic pockets o...

Страница 32: ...loop in the upper part of the container bottom passes through the grommet in the cover flap centre and it is secured by inserted double folded bridle fig 28 Fig 28 The bridle is placed in layers betw...

Страница 33: ...rommet in the lower flap Use the auxiliary packing cords to pull up the closing cord lugs which are secured by means of packaging mandrels fig 30 Fig 30 The auxiliary packing cords are passed through...

Страница 34: ...4 Fig 31 The auxiliary packing cords are passed through the metal grommets in the right side flap and it pulls out the closing cord lugs which are secured by means of the packing mandrels fig 32 Fig 3...

Страница 35: ...ans of the packing mandrels fig 33 Fig 33 Auxiliary packing cords are passed through the metal grommets in the internal flap of the top flap the internal flap is placed to the side flaps and the auxil...

Страница 36: ...ternal flap by means of the ribbon closure and it is placed on internal flap fig 35 Fig 35 Insert the ripcord lug on the pin which be located next to ribbon closure and use the auxiliary packing cord...

Страница 37: ...king mandrel and replace it with the end pin The auxiliary packing cords are fastened below the pins and pulled up in such way to prevent the closing cord damage fig 37 Fig 37 The snap hook on the sec...

Страница 38: ...opening fig 39 Fig 39 Tilt the external flap of the top flap on the container and the snap hook passes through the metal ring sewn between the external and cover flap fig 40 Pass the whole length of t...

Страница 39: ...sions and the ends of the static line to the red tape loop in the centre of the external flap by passing the rip thread with strength 48 to 69 N fig 41 Fig 41 The connection is provided with the check...

Страница 40: ...atic line extension between the ring and the check bond is inserted below the cover tape fig 43 Fig 43 Further process for the static line location into the rubber bushings is performed as per fig 44...

Страница 41: ...41 Fig 45 Fig 46...

Страница 42: ...static line is connected to the red tape loop in the upper part of the external flap at the metal ring by passing the rip thread with strength 48 to 69 N fig 47 Fig 47 The connection is provided with...

Страница 43: ...43 The remaining length of the static line is placed into the upper rubber bushings fig 49 Fig 49 The snap hook is inserted into the tape pocket fig 50 Fig 50...

Страница 44: ...44 The located static line is covered with the cover flap by inserting the side flaps and the narrowed lower part of the cover flap into the respective openings in the external flap fig 51 Fig 51...

Страница 45: ...gh the closing cord lug and behind the pressed pin part the thread ends are tightened with three nodes The thread ends are bound together at 20 to 30 mm from the nodes and the node is secured with pap...

Страница 46: ...o sides by means of the side flaps and its lower part is inserted into the opening in the lower flap fig 53 The parachute packing is completed The packer shall make a record into the parachute logbook...

Страница 47: ...st the length of the straps by means of buckles on the harness 2 The parachute use with static line VL 037 2 1 Conditions for use The static line can be anchored in the aircraft solely in the designat...

Страница 48: ...ce of the shelves from the walls must be at least 0 5 m and at least 1 m from the heating units If the parachutes are stored for longer period they must be aired at least once after every 365 days for...

Страница 49: ...ation storage and transport conditions In case of contamination metal parts are cleaned with fabric Potential damage of the surface protection can be painted with a paint of suitable shade 2 Parachute...

Страница 50: ...50...

Страница 51: ...51 The label completion and marking of the emergency parachute ATL 88 90 1B ATL 15 SL...

Страница 52: ...52 2016 Producer MarS a s Okru n II No 239 569 43 Jev ko Czech Republic Telephone 420 461 353 841 fax 420 461 353 861 http www marsjev com e mail mars marsjev cz...

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