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Assembly and Operating Instructions Lifting, rolling and

1. 12 37 34 7 63 54 24 T 3 TR 5 8 un pt gr TT UE SO un STINS NN E T 95 HET 5 el ml L ES I n a 8 I 7 ule b r 1 wiwa m Zu E f E o 9 ES Pos Description Order No Qty DIN No Dimension 2 King pin compl 109086 1 3 Locking piece compl 108411 2 4 Lever compl 116509 1 5 Brake wave compl 118811 1 6 Gear wheel compl 118807 1 7 Excentric compl 118814 2 8 Mounting link compl 118801 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 68 Description jOrderNo Gty DINNo Dimension il Bearing compl 11 Bearing compl right 118830 1 12 Bearingcompl let 118832 1 L 13 107927 1 e 15 Axis 107986 2 16 Bot 107982 11 b A3 J 17 Safetywasher 109073 2 We H i 1 19 Wave 118805 1 20 Limtstop 118806 1 4 22 Side amelie 11001200 22 Side frame left 118815 1 23 Sideframeright
2. Fa Krichel DIN No Dimension Fa Krichel Fa Penny Giles Fa M hler 00941 008 Fa Allbright Fa Gould Fa Gould Fa Wieland WIELAND 78 000 0653 0 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 90 Plates english Order No 129689 The system has to be turned 1 off to the main switch excepl during lifling or lowering process on lo upper ond lower limils bel below and on each outrigger sure lo switch off molor drive when limil mark the of the 4 rocks has been reached 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 91
3. Pos Description OrderNo Gt DINNo Dimension 4 Baecomp WS _ 2 Mow ngimkcomp 10898 2 3 weycp 058111 redoap 6 rensionsping 2 1 ww 2 8 washer foss 2 9 Dampmgpn torso 2 808782 oasa 006 18 identifcationpiate 0947 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 78 Steering lever compl Order No 123173 NS N l STI gt F 5 p mi ri NE i li t ES rn 270 o gt 1 o S 4 56611102 5 Intermediate piece 1 1 G 16652 1 8 leuh 1 o i 1 2 7 E 16 lidentifeationpiate 12888 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 79 Bolt mont compl Order No 109146 Pos Description Order No Qty DIN No Dimension 1 Bolt compl 109130 1 2 Wire cable 109812 1 DIN 3055 292x500 3 Safety clip 100555 1 11024 6 3 A3A 4 Wire rope clip 100570 2 3093 3 Al 5 Clamping pin 100149 1 ISO
4. 99e u 1691 492125 WN eq 0 pue OLIN 5 25 u V 94 1S L 2 9 9 ulo1s s 1 epinc woog epinc 1299 uoneubisog 1691 45 haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 094216 h gb hrlsys s Boom S e lin nn lt HHT PI LS 5 Q ____ y L Wear slot as delivered Wheel unit 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 46 C 6 4 Troop maintenance Gear unit Boom Changing the guide plate If the sliding surfaces of the guide plates are flush with the milled in slots the guide plates must be replaced Unscrew the countersunk bolts 1 Raise the guide plates 2 off the clamping pins 3 Insert new guide plates 2 Tighten the countersunk bolts 1 M 8 Nm Gear unit 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 47 Crankcase
5. G7LE l 20 i p yaz Hh ndsjpwy gt s 2 z M 5 on a 8 Ab 2 o 9l 102 62 82 92 54 9 RR r Ui 01002104 i amp ROO 20 pounou u GZ LL Bund gt Sl f re E CZ AHH 3 0JUOZIJOY p adupy T 194917 360105 Ndsjiaig Sui 9 7 N X 1 mE jew 2 11 OL Sl Sl 7 EE AG x lt c EN ENCES ERE E ee n L 5e wi i E o ZL 5 I 2 5 2 wug509 22 Jaulp uo gt 1 5 2 Y 09 bun1 i agpulJauip uo 9 5 bl 1712 0612 OELI 1712 Na 9 L te Sel EE 9 haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 094216 h gb hrlsys s B Basic structure of the system Explanation of the bar lock The method used to fasten the bars to the cabin is the same on all four bars All bars are bolted twice into the lower ISO corners for rolling and onc
6. E o 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 86 Frame mont Order No 208644 Frame mont 129564 Drum side Flat rod Tube 29555 16 Lamellar cap 120124 8 1255 Steering wheel 126235 2 L V100R ST Jack wheel 26236 2 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 87 Geared motor compl Order No 208622 Ansicht A Pos Description OrderNo Gt DINNo Dimension 1 Howigboompartmon 12848 1 72 yep 104 1 75 6 1 7 Menseew 956 1 8 leer 1088 asaos 2 1094 2 GLYPG202315E 49 Springwasher 100450 8 lomi 727 identifcation plate 12888 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 88 Control box compl Order No 209902 Housing compl i gt Electric parts for controlbox 120602 4 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 89 Electric parts for control box Order No 120602
7. 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 56 1 Pos Qty Safety blocking device compl 114961 1 2 114958 3 4 104729 5 104730 6 103827 7 8 9 114959 10 11 103623 2 104732 13 Washer 104733 1 14 Washer 104734 1 15 Allen screw 100050 3 ISO 4762 M10x70 A2 70 16 Spring washer 100470 8 DIN 7980 A10 A2 70 17 Hexagonal screw 100210 5 11504017 M10x40 8 8 A3P 18 Hexagonal nut 100363 5 11504032 M10 8 A3D 19 Hexagonal screw 100195 6 ISO 4017 M8x25 A2 70 20 Sping lock washer 100456 6 DIN 137 B8 A2 21 Closing screw 100682 2 DIN 910 M16x1 5 A2 22 Usit ring 100908 2 16 7x24x1 5 23 Oylinder pin 100773 2 ISO 2338 B 10x40 St 24 opa ore 2 DNS40 Joss 25 26 27 Gast Wm 1 28 aet 29 090 60650 _ 30 Bushings 1088 895 8980 31 Bushing 100969 2 GLYPG252815F 32 Bushings 100970 125 280 33 Bushings I Bushings 10959 1 685 35 Shaftsealingring 100898 I BASL60x80x10 36 Shaftsealingring 106300 I 8 35 4757 85 37 Shaftsealngring 100875 2 2540 8 38 Thrustwasher 10084 8 39 Thrustwasher 10088 1 82099 40 Thrustwasher 10082 1 41 Compression spring
8. 2 n zel 15430 EN CC 16 1 Center part E 22 0 kg it 2 Steorngiowr m 601712010 1 Bolt 109146 3 0 kg 1 Steeringrod rod 123614 HM Ee 2 Retaining console 123689 5 0 e 10 0 kg Option Open ended spanner a f 30 300569 0 5 kg Single end open ended spanner 301104 0 5 kg a f 24 Lifting rolling an loading total RUM approx approx 1350 kg approx 1350 kg _ Mounting thread 209153 19 0 kg 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 6 A 3 Technical information on the system Please note Notice plates prevent accidents and damage on the system Q 106200 106383 126188 115435 123916 Attention When using the wheel unils make absolulely 5 sure thal 1 no cranking is carried out while the shelter container is lowered immediately after the first corner reaches the ground manual operation for if necessary Ihe connecting shafis have lo remaining 1 be disengoged and the second corner is 3 motor stop lowered individually to the ground Under no circumstances moy the rack be cranked D upwards again after the corner has reached o Haut Ihe ground 2 when dissembling the wheel unils take bolls out of Ihe racks first before Ihe racks are cranke
9. Block the sets of wheels on the cabin side not being steered to prevent them turning No after steering is permitted Rolling speed It is allowed to roll with a speed of 16 km h on plain and solid ground e g tar or concrete The manoeuvring area must be free of obsta cles potholes kerbstone edges water chan nels and gaps in between concrete surfaces It is not allowed to reduce the speed jerkily Attention If after steering is necessary e Max permissible speed walking pace lt 6 km h The brakes are also off on the after stee ring side pin and thereby non functional After steering with fitted steering levers 21 and steering rod 22 no individual stee ring of the sets of wheels is permissible Applying the brake If the cabin should be in the rolling direction on sets of wheels for a short time without a tractor the brakes on all four sets of wheels must be activated Attention On sloping ground Before de coupling the tractor pull the bolt 56 on the sets of wheels 10 with the two wheel caster assembly Page 17 then remove the two wheel caster assembly Note Slightly raise the brake shoes The bolt 56 can then be pulled more easily two wheel caster assembly ane NE seat E ete m mm a sets of wheels with rotation blocked haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375
10. a 5 Pate 2 7 pot 1 mreadedbot oon 1 9 i i 12 10032 8 608752 M Allen screw 100820 DIN GT M8x20 A2 E 7 Notice plate 18 Indication plate 875 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 59 Rack compl Order No 108765 16 18 17 Pos Description Order No Qty DINNo Dimension 1 Rack tube compl 108760 1 2 Ballbearngcomp 107918 1 8 Rek 108802 1 4 Pate 19795 1 J 5 Pate 19796 1 J 6 1797 2 7 Bot 1 8 Threadedbot 1 2 2 Grease nipple 1 onra _ Allen screw 100066 1 ISO 4762 M6x16 12 Threaded pin 100706 1 DIN 913 M10x12 A2 70 13 Clamping pin 100132 8 1150 8752 6x18 A 14 Allen screw 100620 9 DIN 6912 M8x20 A2 15 Countersunk screw 100635 16 10642 M6x12 A2 70 16 Grooved pin 201418 4 150 8746 3 5x6 St A3A 17 Notice plate 108554 1
11. g u r 1 Moddns Pay Jed 01 9 WW p 8 oJnssaJd uonipuoo 9 u OL L S segejans 5 5 uea yog u qioe r WONOA 490 2 lou 104 2 sjulod V r 2 2 6 uea yoey e u aee zz seuwoq rz seosnmsDupisoseeiDop use uoog u qJoe r 2 1 seoegns Bulpiis 1 1 aseauBap ue oO 2899 L jueoniqn W al 3891 uoneubisog jo juiodjes 159 1 34 2125 9 2 9 2 40 haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 094216 h gb hrlsys s 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 41 13 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 42 MEM l19Juejiesuuniugr 9 8269 9 1 0 16 4equunu Ajddns reus 9 suluouu 9 Alena Y JO M 08 GH u 9 JO q L 9850919 pony ued aque r u 9 JO q r 250
12. s mrt E Mig RE EET E seni d 3 amp St fuselage profile b rack extension C 130 is removed c ramp bottom Avoid impacting against parts of the aircraft Set down the cabin on the roller ways of the ramp by cranking e Remove the connecting shafts 14 15 Remove the corner units near to the aircraft bars boo gear unit racks set of wheels Roll in the cabin on the roller ways of the ramp so that the corner units still fitted to the cabin do not impact against the aircraft e Remove the two wheel caster assembly and the rear corner unit Roll the cabin to its location in the aircraft Lash down the cabin securely Note The lifting rolling and loading unit can be supplied stowed in crates or on flight pallets The stowage crate is not part of the scope of delivery C 4 2 Unloading Page 35 gt Page 36 Undo the lashing Secure the deflection roller to the bars 7 8 with cable Attention When rolling out the cabin the safeguard against the cabin accidentally rolling away is the on board aircraft winch cable 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 34 Roll out the cabin on the roller way until the two rear
13. 106084 2 68425480 a2 Bushing WA 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 57 Boom compl Order No 123167 ii To Nor T PX VI E IX isa TE Sr Pos Description Order No Qty DIN No Dimension Folding pin compl 103597 Boom 107984 Guide plate 103627 Guide plate 103628 Guide plate 103629 Guide plate 104739 Ratchet 123608 Flat headed screw 115477 Allen screw 100065 Clamping pin 100153 ISO 8752 8x20 A Countersunk screw 100635 ISO 10642 M6x12 A2 70 4 Gmewdpn 20Mi8 6 508746 3 506 6 74 lidentiiation plate 123978 1 Ts 716 lidentiiation pite 1 DIN 923 M4x4 A3C ISO 4762 M6x12 A2 70 2 3 4 5 6 1 8 9 SOS 5 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 58 Rack compl Order No 108764 dd 44 r NA 9 2 4 7 10 6 s PS EZ ae Sa m e r e 6 16 18 17 Rack tube compl 1922 1 2 bearing comp 1 398 1
14. Connect the rack 4 with the rack extensi on 6 as above 11 5 6 Special feature on the rack The rack 3 and the rack extension 5 form a single unit The same applies to the rack parts 4 6 They remain bolted during setting down and rolling across the inclined aircraft ramp Standard 8 x 8 x 20 cabins can only be loa ded via the inclined aircraft ramp Shorter cabins can be loaded via the horizon tal aircraft ramp In this case the rack upper parts 5 6 must be removed on the racks nearest to the aircraft This prevents collision with the aircraft s fuselage haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 15 Fitting Gear unit 1 e Remove the upper bolt 9 on the boom 2 The lower bolt secures the rack 3 5 4 6 to prevent it tipping out Move the gear unit 1 between the upper eyes of the boom 2 pin with bolt 9 and secure with the linchpin 10 Remove the lower bolt 9 on the boom 2 Swivel in the gear unit 1 pin with the bolt 9 and secure with the linchpin Note If the gear unit cannot be swivelled into the pinning position in the boom the gear pinion and the rack are not flush Remedy Place the crankcase 12 onto the gear unit 1 and turn until the teeth of the gear pinion engage with the rack The pinning position has now been reached B1 3 Fitting the wheel units 27 56 3 4 5 6 Before fitting check the tyre pressure
15. Pull the wheel 51 with its rim and flange off the hub 52 B 5 4 Rotation blockage wheel unit In various individual cases the rotation of rotatable wheel units 10 must be blocked to produce rigid wheel units 10 Push the lock 67 parallel to the rack tube 3 5 The steering is blocked If the lock 67 remains in the parking positi on the wheel unit 10 can be steered B 5 5 Base plate e Lift the racks 3 4 approx 200 mm off the floor Position the base plate 24 centrally below the opening of the rack ends 3 4 Lower the rack 3 4 onto the ball support of the base plate 24 52 51 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 22 C Use C 1 Instructions for loading and unloading the carrier vehicle To load and unload the cabins the carrier vehicle must be on a level and firm surface runway concrete surface Attention Loading and unloading are carried out with the sets of wheels 10 Figure 24 The brakes 55 are activated on all four sets of wheels 10 The rotation of the sets of wheels 10 is blo Cked It is not permissible for the cabins to remain on the sets of wheels for long periods If a longer standing time is required remove the sets of wheels 10 and fit the base plate 24 C 1 1 Unloading onto the ground at rolling height Lowering the cabin Basic structure B 1 Basic struct
16. Unscrew the threaded bolt 1 Pull off the wheel 2 Undo and remove the collar nut 3 Pull the wheel 2 off the flange 4 Let the air out of the wheel e Remove the retaining bolts 5 of the rim Replace the worn or defective part min 4mm E Assemble in reverse order Fill the fitted wheel with air Tyre pressure 6 bar 094216_h_gb_hrlsys_s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 49 Brake adjustment Set of wheels fitted to the system under the rackebaut e Fit the steering lever 1 on the set of wheels Raise the steering lever 1 and insert the bolts 2 brake non functional In this position the air between the eccentric and the tyre must be min 1 mm and max 5 mm Functional check e Slightly raise the steering lever 1 and pull out the bolt 2 Lower the steering lever 1 until the eccentric 6 is on the tyre 5 Steering lever to be lifted until end of way with adapted dynamometer Steering lever with adapted dynamometer to be lowered until excenter 6 has a distance of 1 mm to the tire In this position the force must be more than 50 N e If both work steps raising the steering lever and lowering the steering lever are possible without a fault occurring e g sticking the automatic brake is functional Attention If the space between the eccentric 6 and the tyres 5 is not sufficient or too great off
17. 8466 27 094216 h gb hrlsys s C 3 Instructions for loading and unloading an aircraft via the inclined ramp Position of the cabin in the transport aircraft The precise location depends on the center of gravity of the cabin with a load Transport aircraft prerequisites The transport aircraft is lowered to the lowest loading position and is supported Height at the ramp joint approx 760 mm The ramp is lowered to the ground There are four approx 1200 mm long wedges Ramp and aircraft floor without roller ways The aircraft s own cable winch is used to pull in the cabin Use deflection rollers to halve the rolling in speed 2980 1875 2438 3150 Attention The permissible ground pressure in the reinforced rolling area of the aircraft must not exceed 6 kp cm T O 1C 160 9 Technical manual Loading aircraft TRANSALL C 160 If the individual load of the support is lt 4 t this value is not exceeded gt Page 38 loading attempt with wheel unit C 3 1 Loading The cabin is rolled into the rolling position until just in front of the ramp end and is aligned to the aircraft axis Fitting B 3 Basic structure loading via the inclined ramp B 3 1 Fitting the tow bar and the after steering rod on the cab Align the wedges to the track position of the sets of wheels 10 This must be identical to the r
18. Bolt compl Order No 109367 1996 1 2 4 1 S Wheel unit compl Order No 123168 Droufsicht m je gt Whedcamagemon 1 4 indication plate 1288 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 65 Wheel compl Order No 123213 527 SZ NZ 52 52 iii gt ZZ HART mmm o 2 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 66 Wheel assembly Order No 120519 X OS RR i 904 2 3280 Tube 99e 4 Tubeban 6707 1 lensen 094216 gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 67 Wheel carriage mont Order No 119695 52 63 31 6
19. haacon hilft heben haacon Assembly and Operating Instructions Lifting rolling and loading system Type 1350 10 012 DP No 209841 With swivel bar cable breakage brake and electric drive Order N 257 922 01 01 Certified in accordance with DIN EN ISO 9001 Member of the DWT haacon hebetechnik gmbh Josef Haamann Str 6 D 97896 Freudenberg Main Phone 49 0 93 75 84 0 Fax 49 0 93 75 84 66 e mail haacon haacon de Internet www haacon de 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 2 Content A General description of the 2 5 A 1 SYSTEMMASSCHIPTION E qt ee 5 A 2 u s uu videat o ete adnate en do Cc s asa ashuy aes 5 A 3 Technical information on the System 7 A 4 Part designations and depiction anna a 8 B Basic Structure of Ine SVSIOIYE seele 10 B 1 Basic structure for loading and unloading the carrier vehicle 11 DAS L u uu a ee tn 12 B1 1 1 Fitting the bars under special conditions 2 0 0 1 1 0 0 0 0 13 B1 1 2 Fitting with mounting thread
20. 7 8 is above the ISO corner Hook the bar 7 8 into the ISO corner from above and lower the cable when doing so Remove the mounting thread Lock the bars See B 1 1 Fitting the bars setting down Bar with wheel unit E PENN i spring hook b belt c load hook 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 14 B1 2 Fitting the boom rack tooth pitch and gear unit The boom 2 racks 3 5 tooth pitch 4 6 and gear unit 1 are interchangeable and are used on all four cabin corners Fitting Boom 2 Pull the bolt 23 Push the boom 2 with the Top sign facing upwards without a guide plate onto the bar fasten and secure with the bolt 23 sign When fitting on cabins that are on the truck the mounting thread 33 can be used as an aid to fitting Use the supplied belt to do this See B 1 1 2 Fitting with mounting thread Fitting Rack 3 5 4 6 Remove the bolt 9 on the boom 2 Insert the rack 3 5 4 6 into the sup port of the boom 2 with the opening fa cing downwards for the set of wheels The teeth face outwards Insert the bolt 9 on the boom 2 094216 h gb hrlsys s Assembly of the rack with the associated rack extension Fit together the rack 3 with the rack ex tension 5 so that the rack rails are flush Tighten with the crank 11
21. Operating Instructions 094047 enclosed 14 B1 2 Fitting the boom rack tooth pitch and gear unit 2222 0 0 15 BLS Fitting the wheel uns auraen E el ree Ri 16 B 2 Basic Structure TONG varene 17 B 2 1 Fitting the two wheel caster assembly 2 17 B 3 Basic structure loading via the inclined 43 18 B 3 1 Fitting the tow bar and the after two wheel caster assembly 18 B 4 Basic structure loading via the horizontal ramp 19 8 441 Fitting the two wheel caster assembly and the steering 20 B 5 Fitting THe feen eR TL TIE ES LT QST ILS 21 B 5 1 Connecting shaft Deere seen 21 sn ur der JE NE ERE 21 B 5 3 Wh elunits wheels uu een eier 22 B 5 4 Rotation blockage wheel unit E eth 22 B 5 5 PE ve nt wisi edet 22 C B PC 23 C 1 Instructions for loading and unloading the carrier vehicle 23 C 1 1 Unloading onto the ground at rolling height 23 C 1 2 Loading from the ground to rolling 24 C3
22. Tyre pressure 6 bar for a speed of 6 km h and loading into the aircraft Tyre pressure 10 bar for a speed of more than 6 km h max 16 km h All sets of wheels are interchangeable Position the wheels 51 onto the hub 52 so that a positive fit of the wheel driver is guaranteed e With the a f 24 spanner 31 unscrew and tighten the bolt 53 that secures the wheel Fit the steering lever 21 on the wheel unit 10 pin with the bolt 54 and secure with the linchpin Release the brake 55 by lifting the stee ring lever 21 and pin with the bolt 56 This renders the brake 55 inactive e Lift the rack 3 5 4 6 with the crankca se approximately 150 mm Roll the wheel unit 10 under the rack 3 5 4 6 and position it Rotate the rack 3 5 4 with the crankcase 12 downwards until the verti cal journal 57 of the wheel unit 10 has entered the rack 3 5 4 Connect the set of wheels 10 and the rack 3 5 4 6 with the bolt 58 The position of the bolt is acknowledged and held by a ball catch Fit the other sets of wheels 10 in the same way 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 16 B 2 Basic structure rolling Additional parts must be fitted to the basic structure B 1 for rolling between the carrier vehicle and the aircraft Attention If the rolling distance to the a
23. ewivellingdle DAS u ee ae EV 25 C 2 Narrow TACK 27 Instructions for loading and unloading an aircraft via the inclined ramp 28 CSA 28 22322 conet 30 2 33 SFUNCHONPOr the automatic Brake vs eu 31 C 4 Instructions for loading unloading an aircraft via the horizontal 32 GA 2 80 lo cad Obr a 33 225 Unloading Hrs en D eR M dE 34 C 4 3 Loading trials wheel units oio Eve Rc pee domi 35 5 BIGGIE AVE IR TU eae ae 36 Gol General 36 C 5 2 gt Operating euntis oue leds 37 C 5 3 Electrical wiring diagramm 24 28 Volt Type 1350 39 C 6 MAMENINE Guan 40 C 6 1 by the user operator MES 1 Ser No drawing page 44 45 40 C 6 2 Lubrication by the user operator MES 1 Ser No drawing Page 47 43 6 3 Scheduled work Page 48 49 e prex Dana 45 roop Maintenance Lover debe usia eden 47 C 6 5 Temporar
24. 123023 1 7 Hose band clip lock 106911 4 8 Tensioning belt 113079 4 EDP 13203 3 8 A2 3 Clamping pin 100138 10 Securing ring 100734 11 Grooved pin 201418 12 Identification plate 123140 1 C C 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 75 Center part mont compl Order No 109752 LEON td ZZR ESSA 12 Pos Description Order No Qty DIN No Dimension 1 Center part compl 109753 1 2 Eyecompl 108799 1 3 Sliding part 108262 1 4 Key 108272 1 5 Bolt 108274 1 6 Bolt 108787 1 8 Spingwashe 100456 Bam _ 79 Alensoew 00021 804762 M020 A2 _ 14 Steoringroler 10807 1 LPO206 15 Ds 0600 GPN900K4rOt 717 dewWcaionpae 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 76 Cross bar mont compl Order No 109751 Ansicht A 1 Crossbarcomp 1938 111 2 Locking bar compl emo 2 21 02 4 5 Bl 2 7 8 identifcation 1007 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 77 Brace mont compl Order No 109756
25. 18 Indification plate 108664 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 60 Rack extension compl Order No 108803 8 Ansicht X Order No Qty DIN No Dimension 108707 Rack 108709 7 7 Cover 1 Cynder 1939 2 Compression spring 106020 1 12 Notice plate 108553 1 13 Indification plate 108656 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 61 Rack extension compl Order No 108801 r lt lt pol sss u I 2 N Yn EVE gt lt Ansicht X 3 as iss Rectangular tube compl 108758 Extension compl 108706 Rack 108710 Cover 107929 Key 107932 Cylinder pin 107933 Compression spring 106020 Threaded pin 100492 ISO 4766 M8x10 A4D N O BWIN Allen screw 100620 DIN 6912 M8x20 A2 Countersunk screw 101705 ISO 10642 20 2 Grooved 201418 ISO 8746 3 5x6 St A3A 108554 Indification plate 108657 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 62 Bar left mont Order No 121956 P
26. 1848 1 24 Bushng 1886 2 28 Bearing ne L 26 Bearing 118831 1 27 _ Wheel carriage 118804 1 28 Plateright 118833 1 30 Frame 118835 1 31 Springleft 120424 58 cross beam a 33 Cross beam 118819 1 34 Washer 106040 3 GPN900K4rot 35 Shaftsealingring 101742 2 BASL 48x68x10 38 Taper roller bearing 106410 2 DIN 720 32007X 39 40 41 42 Axaldsc 100817 1 5460 43 Supporting disc i 45 Shim ring 120173 2 DIN 988 42x52x0 5 46 Allen screw 47 i 49 Allen screw 120175 6 ISO 4762 M10x40 10 9 A2P 50 52 53 54 DU Bushing 100963 1 18 20 25 55 Bushng 100967 2 GIYPG222520F none 5 Bushing 100976 2 30 34 20 58 59 s 61 Clamping pin 100186 2 ISO 8752 8x50 A 62 63 64 65 66 67 Securing ring 106479 2 471 18x1 2 A2 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 69 Crank compl Order No 108800 lt gt Pos Description OrderNo Gty DINNo Dimension 244 1 2 demicaionpate 108888 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 7O Crankcase mont Order No 108762 ll QHH
27. 8752 6 45 6 Grooved 201418 2 1150 8746 3 5x6 St A3A 7 Identification plate 109744 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 80 Steering lever compl Order No 123170 ATA 22 RA 177 L IN SHE N 174 lt GI 1 Colletcompl 12375 1 gt 1983 1 _ Umhpn 87 4 Intermediatepiece 108630 1 5 Adustingring 10632 _ 6 1 7 2 8 9 Washer 100442 1 1507093 6 4 140 2 10 Clamping pin 100143 1 ISO 8752 6 40 11 Clamping 101889 1 ISO 8752 10 40 12 Clamping 101883 1 ISO 8752 6 45 13 101890 1 ISO 8752 10 45 14 Grooved 201418 2 ISO 8746 3 5x6 St A3A 15 Identification plate 123183 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 81 Steering rod compl Order No 123614 Pos Description 6 o Washer 100442 5 150 7093 6 4 140HV A2 8 Clamping pin 100107 1 ISO 8752 4 40 9 Grooved pin 201418 2 1150 8746 3 5x6 St A3A 10 Allen screw 100065 4 ISO 4762 M6x12 A2 70 11 Identification plate 123681 1 Pin compl Order No 123615 Pos Description
28. Changing the bolt If the bolt 3 on the flattened surfaces displays excessive wear or if it has been bent by force it must be replaced Unscrew the threaded pin 1 Drive out the clamping pin 2 Unscrew the bolt 3 with the spring parts Unscrew the fillister head screws 4 Remove the stop 5 Mount a new stop 5 with a fillister head screw and lock washer 4 Push the bolt 3 through the first bearing When doing so thread on the washers 6 and spring 7 Drive the clamping pin 2 into the bolt 3 between the washers 6 Bring the bolt 3 into position and secure it with the threaded pin 1 to prevent it from turning Grease the bolt 3 Check the function g b a threaded pin b chain tensioner c engagement position Tensioning the chain Undo the threaded pin until the chain tensioner is free Turn the chain tensioner until the counter pressure of the chain can be felt Turn back the chain tensioner until one of the eight latching positions is reached noticeab le by screwing in the threaded pin Screw in the threaded pin fasten the chain tensioner 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 48 Wheel unit Changing the tyres hoses and rims If the profile depth becomes less than 4 mm change the tyres or the fitted running wheel 5
29. Fax 49 0 9375 8466 13 Attention This interchanged attachment method en sures that there is sufficient rolling on the aircraft ramp when the cabin is set down onto the horizontal aircraft ramp see picture C 4 1 On the second front side of the cabin the bars 7 8 are fitted in the same way as for standard setting down The boom supports 48 of the bars 7 8 are outside the cabin The retaining consoles 29 must be fitted for rolling The two wheel caster assembly is fitted to these retaining consoles 29 Locking and bolting the bars 1 1 Fitting the bars rolling B1 1 2 Fitting with mounting thread Operating Instructions 094047 enclosed The mounting thread consists of Boom arm 41 123796 Retaining bracket 40 123794 123793 If the cabins are on the truck use of the two part mounting thread simplifies fitting remo val of the bars The mounting thread can also be used to fit the boom 2 The boom arm 41 with the manual cable winch 42 is telescopic e Fit the retaining bar 40 on the longitudinal side of the cabin onto the top ISO corner and lock it by actuating the tie bolt 43 Extend the telescopic tube 47 to its maxi mum length Insert the telescopic tube 47 into the boom of the retaining bar 40 Lower the cable with the manual cable winch 42 Hook the bar 7 8 onto the support bracket Crank up the bar 7 8 until the boom of the bar
30. corner units bar boom rack gear unit set of wheels can be fitted e Fit the parts of the corner units The brakes are released and pinned on the sets of wheels Brakes out of action Wheel unit blocked to prevent rotation e With the crankcase 12 raise the set of wheels 10 of the fitted corner units sufficiently so that they take the load as rolling continues Attention The rollers of the roller ways must support the load during rolling out If necessary adjust the heights with the crankcase 12 Continue rolling out until the next two corner units can be fitted e Fit the corner units Sets of wheels blocked to prevent rotation Turn the corner units with the crankcase until all four corner units are supporting approxi mately equal loads Ensure that the contact surfaces of the tyres are equal e Fit the connecting shafts 14 15 on the left and right of the cabin Raise the cabin with the crankcase 12 until the roller ways of the aircraft ramp are free Attention Avoid impacting against the aircraft e Remove the cable and the deflection roller of the on board cable winch Continue rolling until just before the end of the ramp Lower to a rolling height of 460 mm Fit the two wheel caster assembly Roll the cabin away from the aircraft Attention A longer rolling distance requires changeover to narrow track operation C 4 3 Loading trials wheel units Loading test of the wh
31. on the longitudinal side of the cabin and bring it into the lok ked position Tighten with the a f 30 spanner The bars are correctly fitted when the boom holder 48 projects on the front side of the cabin 7 8 48 Rolling Hook the bar 7 8 into the upper corner mounts of the cabin Bring the lock 45 into the unlocked position Insert the lock 45 through the oval ope ning of the ISO corner on the front side of the cabin and bring it into the locked position The bars are correctly fitted when the boom holder 48 is parallel to the front side of the cabin Attention Tighten the lock 45 with the nut then fit the retaining bracket 26 See Point B Basic structure of the system for the bolting method for both locks 45 46 Move the lock 46 on the retaining bracket 26 into the unlocked position Insert the lock 46 of the retaining bracket 26 through the oval opening of the ISO corner on the longitudinal side of the cabin and bring it into the locked position Tighten the locks 45 46 on the front and longitudinal side of the cabin Note Bars 7 8 after setting down with the at tachment parts boom 2 rack 3 4 5 6 gear unit 1 set wheels 10 swivelled into the rolling position on the front side of the ca bin In this procedure the bar remains hoo ked into the top ISO corner of the cabin The bolt connection on the bottom ISO cor
32. that the cabin can be safely rolled into the aircraft additional parts must be fitted to the basic structure described under B 1 The illustrations shown on Page 20 apply The tow bar 27 is only used for rolling via the aircraft s inclined ramp The automatic brake of the set of wheels is activated with the tow bar This ensures that in the event of a cable breakage in the aircraft s on board cable winch the cabin does not roll back on the inclined ramp For safety reasons the bolt 56 assumes two functions Inactive brake Brake 55 pinned with bolt 56 Active brake Bolt 56 connects the tow bar 27 with the set of wheels 10 The cable bre akage brake is active when the tow bar 27 is fitted B 3 1 Fitting the tow bar and the after two wheel caster assembly Dic ct U rs a after steering rod b tow bar 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 18 Tow bar Insert the tow bar 27 between the wheel unit 10 Pin with the bolt 56 and secure with a spring connector after steering rod e Attach the steering lever 21 to the wheel unit 10 and connect with the bolt 54 Se
33. 22 Needle roller bearing 100828 2 HK 2018 RS 23 Needle roller bearing 100832 1 HK 2518 RS 24 25 26 27 28 Chaincomp 10367 1 29 30 3 32 73 Extension compl Order No 202222 Pos Description Order No Qty DIN No Dimension 1 Connection shank compl 116354 1 2 Shaft compl 108636 1 3 Clamping pin 100138 1 ISO 8752 6 28 4 Clamping pin 100094 1 1808752 3 5x26 5 Grooved pin 201418 2 150 8745 3 5x6 St A3A 6 identification plate 108659 1 Connecting shaft compl Order No 108804 2 j 2 5 j SITES ETT I HE EN lt NN WEE 4 EL BANS 27 ZZZ TNA JD 1 8 4 7 4 7 1 Pos Description J rderNo Gty DIN No Dimension 4 Connection shankcompl 10249 2 2 Smfcoecomi _ sms 1 100138 4 808752 628 9x0 5553018 Hose band clip lock 106911 Grovedpn 248 2 ISO8746 03556 5 3 9 Identification plate 108663 108755 2 77777777 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 74 Connecting shaft compl Order No 123022 12 CAE 8 7 11 Connection shankeomp 10729 1 gt Shftcoecomp Coupling 1 4 Sleeve 5 Axial dis 5
34. 66 84 Retaining bracket compl Order No 123688 Pos Description Order No Qty DIN No Dimension 1 Console compl 123648 1 Locngbot 1 2 0 nt gt Washer 1 2 0 Bushing 1 identification plate 12823 Retaining console compl Order No 123689 1 1 Consolecomp 123797 gt 1 3 123607 1 4 Washer 107925 1 5 Bushing 108806 1 6 Compression spring 101074 1 VD 264 34 5x2 5x71 5 A2 Clamping pin 100146 1 ISO 8752 6 50 8 Grooved 201418 2 150 8746 3 5x6 St A3A 9 Identification plate 123798 1 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 85 Electric drive compl Order No 209842 Ht 2 NTG 7 MEN 14 Schnitt 8 2 241 E LU ru x ISAT I9 amp 7 Pos Qt 4 1 212 2 ss 4 2 z 6 jDrivecable2 7 126257 8 Rubber strip 129685 4 GE 9 Washer 100402 2 1507090 2 DIN 137 0 2 12 2 9 6 DIN 985 M5 A2 8 Spring washer 100453 10035 101680 120515 150 4017 M6x35 8 8 A3P 201418 5
35. 919 penu e6euueo 99uM e u 9 JO q r 2 u e 2 uoneouqn opun L Auanoy 186 uoneubBisog jo Ko 159 aes L S3IN 5 2 9 3 43 haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 094216 h gb hrlsys s 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 44 esn 9J0J8q A esn Jaye u sujuoui 9 U s eaA g Jaye ou OOGG 491JVu se 1018 169M uooeeu uonoedsur ul91s Ss 1 Aljenuue 30UO 340 JO 01 G y ui 1018 EZ
36. Crankcase compl 1 489 1 Ds 2 10040 1 GPNS00K4rt Springloadedpn 1 10H72 23608 pite 108849 11 0 Identification plate 108649 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 71 Crankcase compl Order No 118020 64 02 22 9 7 72 6l 82 LE OL 9 lt t HIUYIS N Ne Ge 5 CC 7 9L 56 72 haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 094216 h gb hrlsys s Pos Description OrderNo ty DINNo Dimension 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 1 108688 2 y 2 Crankshaftcompl 108640 1 1 3 Driveshaftcompl 10354 1 4 Intermediatedrivecompl 103596 1 C 5 6 7 8 9 10 11 12 13 Allen screw 100611 DIN 6912 M6x12 A2 70 14 Allen screw 100607 DIN 6912 M5x12 A2 15 Allen screw 100615 DIN 6912 M6x16 A2 70 16 Spring ring 100466 DIN 7980 5 140HV A2 17 Spring ring 100468 2 DIN 7980 A6 A2 18 Clamping pin 100141 2 ISO 8752 6x35 A 19 Needle roller bearing 100844 1 HK 1712 20 Needle roller bearing 100845 1 HK 3516 21 Needle roller bearing 100824 2 HK 1212
37. OrderNe t DINNo Dimension 1 2996 1 2 1661 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 82 Base plate compl Order No 108712 1 Base plate 2 Grooved pin 3 Identification plate Extension mont compl Order No 123093 Hit ay Extension comp 12304 1 _ _ Mounting ink compl 1 Pincom 1 22 1 Washer Eu identification plate 12308 _ 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 83 Retaining bracket compl Order No 121954 Pos Description OrderNo t DINNo Dimension 4 Consolecomp 12088 1 2 tockngbot 267 1 397 1 4 War 1 5 Bushing 1 6 Compression spring 101074 1 VD 264 34 5 2 5 7L5 A2 8 Gmowdpn 508 2 60876 34 6 8 79 Tidentiication plate Tow bar compl Order No 123171 Pos Description Order No Qty DIN No Dimension Tow bar compl 123176 1 r 2 120239 1 23 25 201418 2 608746 3 5 6 St A3A 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 84
38. a E m 1840 Ln2337ETEQ 1 Su m 301 B nel on 8 25881123 5 m ars 8 PILIHbZ o 2 d oe m P rd a A 1 PT 20 B lee 885 Jes ER etm en Ole EE TE z HAG ES 2 a Tu amp 888888 DER le eoooaoaoao 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 39 19 8 6 1 0916 Jequunu 2045 1220 9109AJOIN Q aojeq A BUIYIOM 916 U 006 e o i SL 9105409 u 21 C vL 4901 seoeyuns 149 1 DuiurejeH I u aos v er peau erideseg u qo 6721 eiou z zL sued L zL og uesj pojBuueeis u qo t LL LL 8un4oo uea yeys I u 2 2 01 5 OL eyenbs apisul uea D oseoxuel3 01 u aee z G ernbsopsmow r6 epsureseeDop use wuosuepi 6 u que z 2 8 4 1 8 og ue O
39. a boom a rack a gear unit and a set of wheels two wheel caster assembly for roller operation A two wheel caster assembly consists of a center part a cross bar a brace a bolt and two steering levers A 2 Technical data Carrying force set 4 supports 100 kN Carrying force support on wheels Tyre pressure 6 bar 32 kN Carrying force support on base plate 50 kN an ae bottom edge of cabin to floor 1750 mm Crank force pair of supports N Stroke crank revolution 236 mm Rolling speed max mr Weight without options kg es Power E motors W Current type 24 28 Power consumption Lifting speed approx 260 mm min Weight kg max system incline Sion 106205 onthebar 2 max angle base plate max ground pressure base plate 25 N cm Ground composition en when setting down on base plate firm surface pay attention to max ground pressure when setting down on wheels and rolling operation Setting down permissible uo to wind 64 km h speed Temperature range 802980 6 surface similar to runway e g concrete or tarmac 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 5 Individual Ix 260 36 0 kg 72 0 kg 41 0 kg 82 0 kg 2 2 108803 14 0 kg 28 0 kg ER Bar left 121956 66 0 kg 132 0 kg Ls s pe 1707656 4 0
40. abin with the load Transport aircraft prerequisites The transport aircraft is lowered to the lowest loading position and is supported The ramp is flush with the aircraft floor The ramp is supported if necessary The ramp and aircraft floor have roller ways The aircraft s own cable winch is used to pull in the cabin A deflection roller should be used to halve the rolling in speed Attention Attention must be paid to the permissible load of the roller ways See GAF T O IC 160 9 Technical manual Loading the aircraft TRANSALL C 160 Cabin prerequisites The floor of the cabin must be rollable Flight pallets can also be used in the case of lower cabins The cabin may only be so long that it does not touch the narrowing upper rear part of the aircraft s fuselage when being raised horizontally Page 36 Rolling prerequisites Rolling distance to the aircraft 50 mm Wide track fitting of the lifting rolling and loading system Page 35 The cabin is aligned to the aircraft s axis Rolling distance to the aircraft gt 50 m Narrow track fitting of the lifting rolling and loading system Page 29 Attention So that the C 4 1 Loading procedure can be carried out the following work steps must also be carried out for wide track operation after rolling the cabin up to the horizontal aircraft ramp Replace corner units near to the aircraft on the front side and fit in the w
41. about the rotation point in the upper ISO corner on the front side of the cabin Insert the bar lock 45 into the oval ope ning of the ISO corner on the front side of the cabin Attach the retaining bracket 26 on the ISO corner of the cabin s longitudinal side and insert the retaining bracket 46 lock into the oval opening of the ISO corner on the front side of the cabin Close both locks 45 46 Attention B Pay attention to the basic structure of the system explanation of the bar lock The bars 7 8 can be changed from setting down to the rolling direction also without the attachment parts boom rack gear unit set of wheels 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 26 C 2 Narrow track rolling Rolling on the runway is possible up to max 6 km h sign on the boom and on the center part of the two wheel caster assembly Attention e Max rolling height 460 mm ground to lower edge of the cabin Sign on the boom Tyre pressure 6 bar for max admissible tyre pressure and loading into the aircraft e Max permissible speed 6 km h e When negotiating bends pay attention to the markings for the maximum steering angle If the red marked springs tilt to the side the permissible steering angle has been reached Avoid jerky braking Release all brakes for rolling pin and the reby keep them non functional
42. allverh tungsvorschriften Allgemeine Vorschriften D8 Unfallverh tungsvorschriften Winden Hub Zugger te DIN 1055 Blatt 4 Verkehrslasten Windlasten DIN 7355 Stahlwinden DIN VDE 0530 Teil 1 umlaufende elektrische Maschinen DIN VDE 0660 Teil 2 Niederspannungsger te Steuerger te Schaltelemente DIN VDE 0470 Schutzarten IP Freudenberg 27 06 07 2 _ 737222 i V Konrad Lazarus gb issue3 06 07 090053 dated 27 06 07 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 51 C 7 Spare parts Lifting rolling and loading system Order No 209841 7OLLOE J3SSNIYIS NDWUIJ 69S00 1 25 8909 02602 yY gt s Bus y gt s nap u j pliu3ssi mu H 09 000 q lJ un0J 331 3 10 8 5135 204 3 960000 Buniu3JiijsjoA q H IN 9151 5 ju21u u jjjpuju BupjunjJ j 1 wy 1 18437 Jndsjra g 8 JNASJDWYIS qa13qN0Y 499149421954 aqauuv EL 0515 7 2 52 haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 094216 h gb hrlsys s 129167 108764 108765 108803 121956 121955 109367 i 129166 1 2 13 Extension compl O AJOIN 202222 DIN No Dimension 108804 14 Con
43. and keep them in this sition Wheelsel nol locked gored side pulled side o 108570 5 130061 6 108557 123636 Fahrtrichtung Driving direction Sens de marche Q 106213 Caulion Use electrical motor drive only to upper and lower limits off to the main switch DC except during lifting or 24 28 Volt lowering process 123329 ERROR STOP OPERATION 2 DOWN bew 1 DOWN Er Lx 454 E Ee zj 17 90 20 marked otor manual ler i on each rack see label below and on each outrigger Be sure to swilch off molor drive when limil mark on the first of the 4 racks has been reached 4 2 lt GST 34 9 th eae m 4 1725 merce SSS 7 m et jl in 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 7 auc H 9 ee en ca 250 EEG i ue em epa rS VAS r 3 car TIT TI i vs gt A 4 Part designations and depiction em Bomam Boom Boo
44. cinity of the aircraft ramp are blocked to prevent rotation The connecting shafts 14 15 and crankcase 12 are fitted e With the crankcase 12 raise the cabin until the aircraft ramp can be safely rolled over The cabin can be rolled further across the ramp manually Alternatively the aircraft s cable winch can be used to secure the deflection roller with the cable to the bar 7 8 Attention Roll in slowly The roll in distance up until the corner units near to the aircraft are removed is very short During rolling in the booms 2 enter the angular opening between the bottom of the ramp and the aircraft s fuselage profile gt Page 36 21 15 14 10 12 a steering rod b aircraft ramp c roller way 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 33 he Typ C 141 oe Typ C 130 D j 3 5 E E me 22 2 22 ec Z 2 ME Z C cse T Bere 7 We Sasa
45. crankcase 12 B 5 1 Connecting shaft e Lift the cabin by cranking with the crankca se 12 until the carrier vehicle is free Carefully drive the carrier vehicle forwards guide in 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 23 Attention Impacting against the lifting rolling and loading system can cause toppling over Bring the cabin into the horizontal position and lower it onto the ground Attention Avoid cabin vibrations e g by rhythmical cranking Ensure that the cabin is lowered evenly Lower the cabin to rolling height The rolling height has been reached when the distance between the cabin bottom and the rolling surface is 460 mm Measure C 1 2 Loading from the ground to rolling height Basic structure B 1 Basic structure loading and unloading the carrier vehicle 1 1 Fitting the bars When the cabins are close one behind the other When the cabin is on the truck near to the tailgate During wide track rolling when loading is being carried out via the horizontal aircraft ramp B 1 2 Fitting boom rack and gear unit B 1 3 Fitting the wheel unit B 5 Fitting the control parts Ensure Tyre pressure 6 bar for a speed up to 6 km h and loading into the aircraft Tyre pressure 10 bar for a speed of more than 6 km h max 16 km h Loading and unloading is possib
46. cure with the linchpin Attach the steering rod 22 on the steering lever 21 and secure with the linchpin The steering levers 21 are designed so that the stand upright at the operator s level after they are attached to the wheel unit 10 The brakes remain out of action on the after stee ring rod side The bolt 56 is inserted into the wheel unit 10 22 21 B 4 Basic structure loading the horizontal ramp So that the cabin can be rolled on and via the horizontal ramp so that it can be safely placed down on the roller ways of the ramp it is necessary to pay attention to the following B 1 1 1 Fitting the bars under special conditions Wide track rollers when loading via the horizontal aircraft ramp B 1 2 Fitting booms racks and gear units B 1 3 Fitting the wheel unit 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 19 B 4 1 Fitting the two wheel caster assembly and the steering rod 63 19 10 21 25 61 22 25 63 54 10 21 ramp side This installation method enables wide track rolling Attention Wide track rolling The rolling distance is max 50m for loading over the horizontal ramp The cabin is aligned to the aircraft axis so that only slight steering angles slight direction corrections are required Two wheel caster assembly e Fit the steering lever 19 on the set of
47. d upwards sme 9 117980 106206 WARNING Do not attach and operate Ihe system before you have read and understood the operating instructions ATTENTION Do not raise Ihe container above 20 when winds exceed 40 mph inclinglion of the coniainer 2 Personnel are not allowed neither on nor in under the container when it is raised or when it is being towed or raised 106197 Caution Operale tow bar only wilhin red sleerng markers se Do not fix onylhing with o o o 02 chose 123336 The system has to be turned of the system Oben sum O 108559 Attention Turn wheel into dmg drechon bs before staring Driving direction LANE EE roll off o ATTENTION Tyre pressure 6 bar Check before operalion During use fires must have an even flattening Max rolling speed 6 km h Avoid jerkily brake and torque actions Rolling operation Max rolling height 460mm distance ground lo lower surface cabin To roll open all brakes then fasten them and keep them in this position Non guided wheels locked no gerela possible Load and wnlaod the transpor plane Rolling height according to application Stop during loading and correct height Brakes on Ihe pulled side in action wheelsets locked Open the brakes on the geared side lock them
48. e crankcase When rasing or lowering an empty cabin direct current electric drives can be faster and can cause the connecting shaft 14 15 to vibrate more By briefly stopping the gear motors allow the connecting shaft to come to rest Restart the gear motors If different drive speeds cause the cabin to be tilted by more than 1 the cabin must be brought back into the horizontal position The gear motors are fitted with adjustable sliding clutches The torque is set at the factory 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 38 C 5 3 Electrical wiring diagramm 24 28 Volt Type 1350 95920 4 Jan nero u aon ona ET 407 an elle en e pe 890 ixi 01 22 S 193 e 0 a un gt lu Jon dn 2 ang 5 a aano BHI 2170 hs DAEL 4 5 sine SM 3 m S e o T 2160 Em 5 tine e 1 M sino Gye 5 aum 210 z 3 amp eu HNO INI 81 092 071 I G 9 531 52H i Ag 8 8 i SNSISSNRASS 505 8 55528855808 798 5 A A gt zx 57 8 BE ZI 2 gzunreengP2zttrn A 2 rs r
49. e are two cable tongs on the power supply cable connection to the battery Tongs can be replaced with plugs corre sponding to the existing C 5 2 Operating stipulations To avoid any risk to persons and the lifting device before you raise the container ensure that a the power type corresponds with that stated on the notice plates of the switch box 71 an the gear motors 70 b the container has been released from the carrier vehicle C the lifting capacity has not been exeeded d Lift the cabin with the crank 11 ot the crankcase 12 approximately 25 mm e The corner units are connected to each other in pairs by connecting shafts 14 15 in or der to guarantee synchronous lifting or lowering Note In tempreatures of less than 22 C the gear drives should be allowed to run without a load for around two minutes 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 37 Operating Switch the main switch to ON You can now complete the following functions using the joystick Joystick up Both supports move upwards Joystick down Both supports move downwards Joystick up left The support 2 moves upwards and the support 1 does not move Joystick up right The right support 17 moves upwards the left support 2 does not move Joystick down left The support 2 moves downwards the support 1 does not move Joystick down r
50. e into the lower ISO corners for setting down 0 d A lock 45 is permanently fitted on all bars The second lock 46 is installed in the re taining brackets 26 28 and the retaining console 29 so that it cannot get lost and is required for rolling a locking piece b nut c bolt d spring locking bolt f edge locking bolt g slot shaped opening h unlocked i locked Structure and function of the lock In the unlocked position the bars are in serted into the ISO corners with the lock 45 or are removed for dismounting The lock 46 of the retaining bracket console 26 28 29 is inserted in the same position through the oval openings of the bars and into the ISO corners A spring ensures that the locking bolt is always pressed against the locking piece The nut is opened by turning it anticlockwise The locking bolt can be swivelled with the bolt When the edges of the locking bolt cover the slot shaped opening of the lo cking piece the locking bolt is pressed into the slot shaped opening of the locking piece with the aid of the spring The positive fit guarantees secure locking 094216 h gb hrlsys s 20 20 29 1 ZZA x L SH After the positive fit is obtained the nut is tightened The bar ISO corner connection forms a secure connection The bolt and t
51. ed easily in all direction DIP E zu T IN 13 FUN see rS kkk 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 36 Fitting The gear motors 70 are secured to the two diagonal corner units on which the latching disks of the gear unit 1 face outwards Pull of the spring cotter 75 on the front part of the unit Push the drive shaft 74 of the gear motor 70 through the latching disk of the gear unit 1 By swivwiling the gear motor 70 make the outer square of the gear motor 70 fit the inner square of the gear unit 1 Swivel the gear motor 70 until the faste ning bolt is above the flattened part of the latching disk Press the gear motor 70 onto the latching disk as far as it will go Secure with a spring cotter 75 75 Attention Before putting the electric drive into opera tion check that no crank 11 and or small crankcase 12 is fitted on one of the corner units accident hazard 72 Preparing the electric drive connect the drive cable 72 to the switch box 71 and secure it Attention 71 connect the drive cable 1 to connector 1 on the switch box 71 connect the drive cable 2 to connector 2 on the switch box 71 connect the drive cable to the gear motor 70 and secure it Connect the power supply When delivered ther
52. eel units at 6 bar tyre size 180 x 70 R8 IC 70 Wheel Surface pressing kg sm 893 600 Wheel2 Sinking dimension mm 37 00 42 00 Floor area cm 303 60 333 65 Surface pressing kg cm 180 70 R8 IC 70 Measured tyre diameter mm 451 0 Measured tyre width mm 172 0 Measured profile width mm 162 5 Measured wheel spacing outside mm 697 0 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 35 C 5 Electric drive C 5 1 General The electric drive consists of a mobile cart on which the switch box 71 the two drive cables 72 the power cable 73 and the two gear motors 70 are mounted This reduces the cycle time 71 72 73 70 Switch box Each motor has its own fuse To protect the semi conductors these fuses must only be replaced with equivalent types 10x 38 mm 25 A GOULD series aM for motor circuits rated voltage 500 V 120 kA switch rating The fuses for the limit switches are also inside the controller they measure 5 x 20 mm 1 A The controller houses a 4 way DIP switch using which the direction of rotation of the motors can be changed if necessary DIP 1 turns the first motor DIP 2 the second All the components in the controller are designed for operation in temperatures as low as 32 C Nevertheless in temperatures below 20 C before you start work with the controller you should check that the joystick can be mov
53. einforced rolling tracks in the aircraft Release the brakes of the sets of wheels 10 on the steering rod 22 with the steering lever 21 and pin Brake not active Page 31 The brakes on the sets of wheels 10 with the tow bar 27 are activated Page 31 Secure the deflection roller with the cable on the tow bar 27 Attention The cable must not scrape on the ramp joint Lower the front cabin side with the fitted tow bar 27 until a ground clearance of min ap proximately 50 mm is guaranteed 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 28 21 10 d 22 1 21 a steering rod b tow bar c deflection roller and cable d operator Attention When rolling in after steering is possible only on the rear side of the cabin Two operators perform after steering on the steering rod 22 on the left and right of the cabin The after steering must be adjusted when the ramp joint of the cabin is reached Pull up and hold the cabin over the wedge e Perform height adjustment on the cabin Roll further on the ramp into the aircraft If necessary stop and adjust the cabin height After reaching the ramp joint remove the steering rod 22 and block the sets of wheels to prevent rotation Attention If possible the cabin must be rolled in horizonta
54. guard is installed in the sequence The steering lever 21 required for after steering can only be fitted to the bottom holder The towing fixture 27 required during roiling over the inclined ramp can only be fitted on the top holder See C 6 4 Troop maintenance The tow bar 27 can only be pinned onto the top holder with the bolt 56 The brake is functional The brake is pinned and kept non functional with the bolt 56 This measure guarantees that the brake is functional during rolling across the inclined aircraft ramp and that the parts steering lever 21 and towing fixture 27 cannot be fitted incorrectly Attention Before every use Check the tyre pressure 6 bar Inspect the function of the automatic brake cable breakage safeguard See C 6 4 Brake adjustment After the bolt 56 is pulled the eccentric must be movable After a cable breakage of the on board cable winch Attention Check the wheels pay attention to the air pressure and any damage to the tyres and re place if necessary Check the function of the automatic brake See 6 4 Brake adjustment 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 31 C 4 Instructions for loading unloading an aircraft via the horizontal ramp The cabin is rolled via the on board roller ways to the location in the aircraft The precise location in the aircraft depends on the center of gravity of the c
55. he edges of the locking bolt have the same position This means Horizontal position lock closed Vertical position lock open If the nut is undone the locking bolt can be pressed in and the lock can be released by swivelling round the bolt haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 10 B 1 Basic structure for loading and unloading the carrier vehicle Fitthe bars 7 8 without the retaining brackets 26 28 The boom support 48 of the bars projects on the front wall of the cabin Fit the four booms 2 at 90 degrees to the cabin wall Insert the connecting shafts 14 15 into the gear unit 1 Operation is possible by 2 persons with the crankcase 12 or the cranks 11 11 14 15 12 Ver 1 bd Pai 2 48 48 A ud 8 7 i e p 7 8 a 48 E 48 NAAS 0 r lt 12 11 A longitudinal side container B front side container Wheel units swivelled about 90 11 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 B 1 1 Fitting the bars Setting down without retaining bracket Hook the bar 7 8 into the upper corner mounts of the cabin Insert the lock 45 through the oval ope ning of the ISO corner
56. ide track position See B 1 1 1 Remove the rack extension See B 1 2 Swivel corner units facing away from the aircraft on the front side into the wide track and mount e Lift all four corner units and ensure even load distribution tyres flatten out e Fit the connecting shafts Raise the cabin over the horizontal ramp 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 32 C 4 1 Loading Before rolling up to the aircraft ramp on the side facing the aircraft it is necessary to remove the rack extension according to the aircraft type see B 1 2 picture page 36 The cabin is now pushed via the two wheel caster assembly until it is close to the aircraft ramp Fitting B 4 Basic structure loading via the horizontal ramp B 4 1 Fitting the two wheel caster assembly and the steering rod When pushing the cabin into position the sets of wheels 10 on the side facing away from the two wheel caster assembly can be blocked to prevent rotation If positional correction of the cabin is required the connected sets of wheels 10 can be steered via the steering lever 21 and the steering rod 22 Page 35 Attention Risk of collision between operator and material in the vicinity of the aircraft ramp The cabin is pushed up to about 100 mm away from the ramp end The brakes are released on all sets of wheels 10 Brake function not active The sets of wheels 10 in the vi
57. ight The support 1 moves downwards the support 2 does not move The LED s on the control desk have the following functions GREEN Activation of the electric motors If the power consumption rises to over 55 A per motor the LED will flash and the motor current will be electronically limited ORANGE At least one drive cable is not connected RED Excess temperature on the power section in the controller If the green LED is also lit the drive has suffered an overload Operating stipulations In order to prevent damage to the gear motors 70 the boom 2 the gear unit 1 and the racks 3 5 4 6 the electric drive must not be used across the entire possible lifting range i e in the upper and lower lifting range the remaining lift must be performed manually with the crank 11 or crankcase 12 The red dots in the rack tubes mark the lifting limit for the electric drive Observe the notice sign for motor stop on the boom 2 See A 3 Technical infomation on the system During operation if the current voltage is too low if the temperature is too high or if the load is too high one or both gear motors may be swichted off INTERRUPT THE LIFTING OPERATION IMMEDIATELY Heason The maximum operating temperature of the motor s is exceeded Remedy a Interrupt the lifting operation until the motors have cooled down approx 15 30 minutes b Remove the gear motors and complete the lifting process manually ba using th
58. ircraft longer than 50 m and or if the cabin is not aligned with the aircraft only rolling in a narrow track set up is permissible In the case of wide track ope ration the bars and set pf wheels are fitted on the longitudinal side of the cabin see Page 21 B 2 1 Fitting the two wheel caster assembly 21 54 56 3 4 5 6 93 59 18 54 56 17 63 10 2 7 A longitudinal side B front side c narrow track operation Original state The booms 2 are fitted on the bars 7 8 in the rolling track wheel center spacing 1880 mm corresponding to the reinforced rolling track in the aircraft Likewise the rack 3 5 4 6 gear unit 1 and wheel unit 10 The brakes on all four sets of wheels 10 are not active The bolt 56 is pushed in e Fit the steering lever 21 to the sets of wheels 10 pin with the bolt 54 and se cure with the linchpin Insert the cross bar 17 between the bars 7 8 push the bolt 59 into the bars 7 8 and secure with the lock Push the center part 16 onto the cross bar 17 pin with the bolt 20 and secure with the spring connector Connect the brace 18 to the steering lever 21 pin with the bolt 63 and secure with the linchpin 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 Basic structure loading via the inclined ramp So
59. l Avoid banging the cabin and the lifting rolling and loading system against the aircraft Check the floor ceiling and side clearances during the entire loading process Attention If the cabin is horizontal in the aircraft it is possible that the brake is not released fully as the cable force diminishes push manually Release the brake with the lever 21 and hold it open Roll the cabin to the mounting place in the aircraft and set it down ash down the cabin Attention Lashing down to parts of the lifting rolling and loading system is not permissible Attention If the lifting rolling and loading system remains in the aircraft on the cabin the set of wheels must be turned freely The cabin set down only on the wheels is not permissible 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 29 C 3 2 Unloading Page 31 Page 32 Note Transport aircraft prerequisites see C 3 Undo the lashes Check that the tyre pressure is 6 bar Secure the deflection roller with cable on the tow bar 27 Position the wedges at the end of the ramp to the rolling track width Release and pin the brake on the sets of wheels 10 with the steering lever 21 Brakes inactive The steering rod 22 can only be fitted outside the aircraft The sets of wheels 10 are blocked on the steering rod side to pre vent rotation The brakes on the se
60. le for both 6 and 10 bar Attach the crankcase 12 to the gear unit 1 2 B 5 2 Crankcase e Cranking individually with the crankcase 12 until the crank pressure increases noticeably and the wheels of the set of wheels 10 flatten slightly Attention When all four corner units are brought into contact with the ground the contact surface of all tyres must be of equal size Ensure that the load on all four corner units is approximately the same Attach the extended connecting shaft 14 15 to the gear unit 1 and crankcase 12 B 5 1 Connecting shaft e Lift the cabin about 100 mm Check whether the cabin is horizontal If necessary remove the connecting shaft 14 15 and level out the cabin e Lift the cabin over the loading surface of the carrier vehicle Carefully drive the carrier vehicle under the cabin guide in Position the support bolts of the carrier vehicle precisely under the lower openings of the metal corner mounts of the cabin Lower the cabin until all four corner units of the lifting rolling and loading system are relieved Close the connection between the cabin and carrier vehicle Remove the lifting rolling and loading system B 1 3 1 1 1 1 1 B 5 1 B 5 2 but in reverse order 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 24 C 1 3 Swivelling the bars This is only possible if the bars 7 8 are at
61. ly inspect the wheels for wear and external damage and replace if necessary Check the function of the automatic brake see C 6 4 Brake adjustment The following is not permitted Remaining on in and below the raised cab ins as well as transporting persons Do not fix anything with lashing straps on parts of the system The unit conforms to the regulations of BGV D8 accident prevention regulations for winches lifting units and towing units Pay attention to the valid laws and regulations governing accident prevention 094216 h gb hrlsys s Inspection by an expert The lifting rolling and loading system must be inspected by an expert depending on the conditions under which it is used and the operational conditions but at least once annually annual operational safety inspection in accordance with the accident prevention regulations BGV D8 Section 23 Paragraph 2 In all cases before the lifting rolling and loa ding system is put back into operation ser vice the safety relevant parts e g the bar gear unit boom rack and set of wheels Experts are persons who by virtue of their specialist training and experience have sufficient knowledge in the field of winches lifting units and towing units and who are familiar with the relevant national work safety regulations accident prevention regulations directives and generally recognized technical regulations e g DIN EN standards to the extent that they a
62. m arm 3 Rak 92 6 Rackextension 45 lock bar ___ 7 Bar left 46 Lock retaining bracket _____ LB Bolt Boom support 10 M Crank ss 13 Extension Hub 18 20 Bolt Bolt 21 60 Lock 23 Bolt 24 Base plate Bolt Extension 29 Retaining console wide track gaude 1 68 r Smgecendopenemdedspameraj2t 70 31 Single end open ended spanner a f 24 Gear motor Electricdrive S 73 Power cable T4 Drive shaft Spring cotter Parts 1 33 are identical to the drawing 1350 10 012 see Page 10 Parts 40 75 see figure Option Mounting thread 209152 Cabin height 8 and 8 12 209153 Cabin height 7 and 7 72 Electric drive 209842 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 8 41 Buying
63. necting shaft compl 123022 15 shaft compl 109752 16 Center part mont compl 109751 17 Cross bar mont compl 18 Brace mont compl 109756 19 Steering lever compl 123173 20 Bolt mont compl 109146 21 Steering lever compl 123170 22 Steering rod 123614 23 Bolt compl 123615 24 4 25 2 26 27 28 29 30 3 32 33 34 35 094216 h gb hrlsys s DIN 3113 DIN 894 SW 30 SW 24 24V haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 53 Gear unit mont compl Order No 128031 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 54 i Gearuntcomp eos ft gt Lachngdskcomp 10958 1 3 10475 4 4 Gudepaes 7 Gmoedpn 2 2 o GPN 300 F2 i 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 55 Gear unit compl Order No 128035 lt G m N UM F NY KLA N n IX SI IV HAr DNS ODE LL 7 Gat Ie Lif te N SIN a m N D 9 m m m gt m m e m m M m N
64. ner is released see Point C1 3 Swivelling the bars 26 BE 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 12 B1 1 1 Fitting the bars under special conditions When the cabins are close one behind the other Cabin on the truck next to the tailgate Attention The bars are fitted interchanged on both longitudinal sides of the cabin The boom support 48 for fitting the boom 2 does not project on the front wall of the cabin With this attachment method it is not possi ble to change to rolling operation Wide track rolling for loading via the hori zontal aircraft ramp gt Attention Wide track rolling in walking speed is only permissible in the vicinity of the aircraft max rolling distance 50m cabin is aligned 2 towards the aircraft Avoid steering angle Fit the bars 7 8 interchanged on the front 28 side B of the cabin facing the aircraft The boom supports 48 of the bars 7 8 face inwards on the longitudinal side of the cabin 7 Picture The bar must also be bolted with the retaining E M brackets 28 setting down with retaining bracket and console 3529 interchanged 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0
65. os Description Order No Qty DIN No Dimension 1 Bar left compl 121929 1 2 Boom compl 121926 1 3 Bolt 108227 1 4 Folding pin compl 114716 1 5 Guide 108867 1 6 Locking bolt 121934 1 7 Bolt 121935 1 8 Washer 121936 1 9 Washer 107925 1 10 Bushing 107940 1 67 1 2 E I 15 16 18 19 20 22 23 _________ 094216 h gb 5 haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 63 Bar right mont Order No 121955 Pos Description Order No Qty Bar left compl 121918 Boom compl 121926 Bolt 108227 Folding pin compl 114716 Guide 108867 Locking bolt 121934 121935 121936 107925 107940 123607 42 Compression spring 101074 1 VD 264 34 5 2 5 7L5 A2 4 Menseew 10008 1 SO4762 2 270 44 Campngpn 10046 1 50852 Jos 718 Grasenppe 100307 1 DNTMI2 16 ssfeynut 400884 1 DINGBS M20 8 N AP Washer 1 60700 18 Washer 400448 1 SO7093 64 Spring 0846 2 3645 23 2998 1 2 3 4 5 6 7 8 9 a 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 64
66. re able to assess the ope rational state of the lifting rolling and loading system Manufacturer s and customer service address haacon hebetechnik gmbh Josef Haamann StraBe 6 D 97896 Freudenberg Main Phone 0049 0 9375 84 0 Fax 0049 0 9375 8466 Please state the following when ordering spare parts Type Year of construction Serial No Order No from the spare parts list in the Appendix Required quantity 1350 10 012 haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 4 A General description of the system An after steering rod with two steering levers A 1 System description Atow bar for rolling the cabin over the incli The lifting rolling and loading system ned ramp 1350 10 allows cabins to be loaded into and the cable of the on board aircraft cable unloaded from the aircraft Transall C 160 and winch is attached to the tow bar Hercules enables the cabins to be lifted onto _ Two separable connecting shafts Two cor and off the carrier vehicle without additional ner units can be connected in each case aids and permits cabins to be rolled on a flat Two crankcases and two cranks for single firm surface and paired drive The system consists of Linkage points for the lifting rolling and Swivel bars loading system are the ISO corners of the Four each of booms racks gear units sets Cabins of wheels and base plate A corner unit consists of a bar
67. set the eccentric part 6 by one tooth on the splined shaft 7 Remove the fillister head screw 8 Pull the eccentric 6 off the splined shaft 7 and reattach it having been turned by one tooth Check the space between the tyres 5 and the eccentric 6 Screw in the fillister head screw 8 LZ EE m 2 section A A 6 27 C 6 5 Temporary non use and long term storage Work for temporary non use of up to 6 months Only the scheduled care and maintenance work must be carried out Work for long term storage of up to 5 years The same measures apply as for non use of up to 6 months A functional inspection must be carried out before putting back into operation 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 50 E C Declaration of Conformity ii 5 1 to 98 37 EC D 97896 Freudenberg Main Name and address haacon hebetechnik gmbh Telefon 09375 84 0 Josef Haamann Stra e 6 Telefax 09375 8466 97896 Freudenberg Main Description Designation Shelter Lifting Rolling and Loading System electric drive Type 1350 10 1350 6 5 Capacities 101 6 5 Relevant Directives 98 37 EC EC machinery directive 73 23 EEC EC Low voltage directives Harmonised standards DIN EN ISO 12100 1 2 safety of machines National standards and technical specifications Al Unf
68. tached to the cabin in accordance with the method B 1 1 The boom support 48 of the bars projects on the longitudinal side of the cabin During setting down the bars 7 8 are bolted onto the longitudinal side of the cabin gt B 1 1 Fitting the bars The attachment parts bar 7 8 rack 8 4 gear unit 1 set of wheels 10 are at right an gles to the longitudinal wall of the cabin For rolling bolt the bars 7 8 to the front side of the cabin and also secure them with the retaining bracket 26 to the longitudinal side of the cabin gt Page 11 13 This attachment method is advantageous for rolling the cabins into the aircraft via the inclined ramp because in the critical free space area the ISO corner on the top of the cabin there is no attachment part of the lifting rolling and loading system at the side 1 C 3 4 10 er ground 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 25 Changing the bars from setting down to rolling The cabin has been set down on the ground Raise the rack 3 4 with the crankcase 12 until the set of wheels 10 loses its grip on the ground Release the bar lock 45 Swivel the corner unit bar boom rack gear unit set of wheels
69. the longitudinal side of the cabin Fitting By pulling or pushing the grooved sleeve 66 just behind the external square of the con necting shafts 14 15 itis possible to insert the connecting shafts into the inner square of the gear unit 1 the crankcase 12 and connecting shaft Attention Check the axial safeguard during every use by pulling manually 66 14 66 Connect both parts to get a long connection shaft B 5 2 Crankcase The crankcase 12 enables two hand cran king and adjustment of the crank height to suit the body Fitting Hold the crankcase 12 horizontally Guide the square pin 47 of the crankcase 12 into the latching disk of the gear unit 1 By slowly turning the crank allow the square pin 47 of the crankcase 12 to en gage in the inner square of the gear unit 1 Pull the crankcase 12 ball head 49 of the bolt against the spring and hold Press the crankcase 12 further onto the gear unit 1 until the stop hook 50 is behind the latching disk Swivel the crank case into the desired position and lock it by releasing the bolt 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 21 B 5 3 Wheel units wheels The wheels 51 of the wheel unit 10 can be individually removed from the wheel unit 10 Removal Use the open ended spanner a f 24 31 to undo and replace the screws 53
70. tic brake a The automatic cable breakage brake is used only when loading unloading via the inclined 56 ramp Each of the four identical wheel units N 10 is fitted with an automatic brake 55 The automatic brake is functioning When rolling the cabin over the inclined Hs aircraft ramp on the sets of wheels with b 56 the tow bar 27 and on board winch cable 22 attached 22 When setting down on the sets of wheels a holder top b holder bottom for brief periods The automatic brake is c tightening brake d release brake not functioning When rolling the cabin over the inclined aircraft ramp on the support side with the steering rod When rolling the cabin in front of the air craft on all four wheel units 10 During wide track rolling rolling over the horizontal ramp 3 4 5 6 d Attention When the lifting rolling and loading system is on level ground with the cabin raised the brakes functioning act on the front or rear wheel units depending on the rolling direction All other operating parts two wheel caster assembly must be removed form the set of wheels Attention The cabin can be set down on the sets of wheels on flat ground with the brakes released bra ke non functional On sloping ground the brake is required on all four sets of wheels 10 In order to achieve the operating states brake functional brake non functional a safe
71. ts of wheels 10 with the tow bar 27 are activated e With the tow bar 27 release the brake on the sets of wheels and keep them released until the sets of wheels are on the inclined ramp Roll the cabin onto the inclined ramp Slak ken the cable of the on board cable winch in a controlled manner Attention For safety reasons the winch cable must be kept taut during the entire unloading pro cess If the cabin is on the ramp the brake is released and applied automatically Roll the cabin further out of the aircraft on the ramp If necessary stop and correct the height Attention If possible the cabin must be rolled out of the aircraft horizontally Check the ground ceiling and side clearances during the entire unloading process Prevent the cabin and the lifting rolling and loading system from impacting against the aircraft Continue rolling until all sets of wheels have left the ramp Align the cabin to rolling height Remove the towing fixture 27 Keep the brakes of all four sets of wheels released 10 Brakes inactive Block the rear sets of wheels to prevent them rotating without two wheel caster assembly B 5 4 e Roll the cabin to the desired location and set it down a steering rod b tow bar c operator 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 30 C 3 3 Function of the automa
72. ure loading and unloading the carrier vehicle B 1 1 Fitting the bars B 1 1 1 Fitting under special conditions When the cabins are close one behind the other When the cabin is on the truck near to the tailgate During wide track rolling when loading is being carried out via the horizontal aircraft ramp B 1 2 Fitting boom rack and gear unit B 1 3 Fitting the wheel unit B 5 Fitting the control parts Ensure Tyre pressure 6 bar for a speed up to 6 km h and loading into the aircraft Tyre pressure 10 bar for a speed of more than 6 km h max 16 km h Loading and unloading is possible for both 6 and 10 bar The cabin is detached from the carrier vehicle Attention When all four corner units are brought into contact with the ground and the cabin has been slightly raised off the carrier vehicle the contact surface of all tyres must be of equal size Ensure that the load on all four corner units is approximately the same Attach the crankcase 12 to the gear unit 1 Setting down B 5 2 Crankcase 2 supports connected on the longitudinal side Crank individually on all four corner units 2 man operation visual contact until the sets of wheels 10 make contact with the ground Continue cranking with the crankcase 12 until the crank pressure increases noti ceably and the wheels of the set of wheels 10 flatten slightly Attach the extended connecting shaft 14 15 to the gear unit 1 and
73. wheels 10 pin with the bolt 54 and secure with the linchpin Insert the cross bar 17 vertically between the retaining console 29 push the bolt 59 into the retaining console 29 and secure with the lock 60 Push the center part 16 onto the cross bar 17 pin with the bolt 20 and secure with the spring connector Pin in the long part of the cross bar Attach the brace 18 under the center part 16 and secure with the spring connector Attach the brace extension 25 on the brace 18 pin with the bolt 61 and secure with the linchpin Connect the brace extension 25 to the steering lever 19 pin with the bolt 61 and secure with the linchpin Steering rod e Fit the steering lever 21 on the set of wheels 10 pin with the bolt 54 and secure with the linchpin Attach the steering rod 22 on the steering lever 21 and secure with the linchpin 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 20 B 5 Fitting the operating parts B 5 1 Connecting shaft 14 15 The connecting shafts connect two supports This enables two man operation It consists of two parts 1 The short part 14 which has two external squares on the end This connecting shaft 14 is used for rolling narrow track 2 The extension 15 a long part with a coupling piece The parts 14 15 connected produce a long connecting shaft that is used for setting down on
74. y non use and long term storage 50 C 7 Spare DAS ee i ee Ee Saree COLLES En 52 094216 h gb hrlsys s haacon hebetechnik gmbh Phone 49 0 9375 84 0 Fax 49 0 9375 8466 3 Instructions for safe working Before starting work with the lifting rolling and loading system for the first time it is ne cessary to have read and understood these operating instructions The unit may only be installed used and serviced by persons who are familiar with the assembly and operating instructions and who have received the appropriate specialist training The lifting rolling and loading system may only be used for its intended correct purpose Correct use is loading and unloading the aircraft Transall C 160 and Hercules with the lifting rolling and loading system as well as depositing and placing down cabins with ISO corners from a carrier vehicle Before lifting lowering and rolling the cabin install the unit correctly It is prohibited for persons to remain in the danger area Check every time before use Tyre pressure 6 bar Obligatory for loading into the aircraft and rolling speed 6 km h Tyre pressure 10 bar For rolling speed gt 6 km h Max speed 16 km h Only rolling in a nar row track set up is permissible e Function of the automatic brake cable breakage safeguard If the cable of the on board cable winch breaks Visual

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