Manuel de montage

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I/ FINAL TUNING OF CONTROLS AND CONTROL SUR- FACES. is all too often neglected. Yet, these adjustments make all the difference between an aircraft that gives smooth, coherent response, and a cantankerous, even dangerous beast. 1) The elevator: This stage the pivot bolts are not too tight against the washers. .Elevator trim tab: first of all, check it responds in the right direction! Push the trim sure Make the tab should move up (so as to push the elevator down, for a nose down response). Second, adjust the cables so that the trim tab is in line with the elevator when the lever is vertical. The trim cables must be tight, but not in excess; forward: lever of wrapped on the pulley: 2 and half. Do not apply any lubricant: here, the more friction, the better! You also need a small screw to stop the cable from slipping. 2) The ailerons: number turns straight tubes or rulers, about 2m (6ft) long. Two helpers will make things easier. -The turnbuckles must be adjusted so that: The aileron tips are in contact with the two rulers held tight against the lead- -Get two ing trailing edge, lying parallel to the keel, level with the inboard, wider ends of the ailerons. (Caution: if you place the rulers elsewhere along the wing, aileron angle will be set differently due to wing twist). edge and sticks in vertical position. control Both It is not a good idea to have the cables too tight; a reasonable amount of NOTE: When Also play is preferable, so that the ailerons are not too « stiff », due to excessive friction. you are satisfied, do not forget to safety wire the turnbuckles and to torque the nuts of the rod ends. check that the sticks do not bind on the pitch axis: the bolts must be free. I4 interdite Reproduction / reproduction Prohibited 2009 ©Randkar 21 July, 2009, HANUMAN XAIR MANUAL ASSEMBLY s.a. KAR RAND First Page 74 / 85 THE RUDDER CABLES ARE CROSSED!! once again, because this bears repeating, make sure that: and all, of rudder: The 3) cables will be under slight tension when the rudder is centered; slack in all other positions is normal. To eliminate any possibility of the cables jamming over the bolt The the two rear support tubes, next to the stainless plate, it is a good idea to make two simple leads using plastic ties and pieces of gas hose, tied to the leading edge of the stabilizer. (D7A) that ties pedals are lined up, the rudder should be in line with the longitudinal axis of the aircraft: the easiest way to get this is to clamp the rudder between two cleats the When the adjustable links so that: - the nose wheel is in line with the longitudinal axis - the pedals are lined up - the cables are slightly taut and set those pulleys! The pulleys at the after end of the keel must be installed so that they cannot move off of their bearings: the red mark must be visible from out- out Watch (only this way will the bearing keep the pulley in place). 4) Rudder tab (N°146) it corrects engine torque effects. Mount it on the rudder after the first trial flights if necessary. side,
alance Weighing operation must be done with 3 similar weighing machines on an horizontal surface. The aircraft must be weighed with its complete equipment (instrument, radio and eventually parachute) without pilot and passenger and without fuel in the tank. 5)Weight WEIGHT FRONT WHEEL A RIGHT REAR WHEEL B LEFT REAR WHEEL C CG=150xA/A+B+C result must be located between 22 and 40,5 6) Lubrication: The ideal lubricant is a silicone spray (if unavailable, you can use a WD-40 equivalent, but it is not so clean); apply to all points likely to create un- The friction: control tube washers and pivots, elevator and rudder hinges, aileron and pedal bearings, all pivot bolts of sticks and parallelogram, as well as the fork main axle during assembly. In short, to obtain smooth, precise controls, you need: barely taut cables, barely tight bolts, and regular lubrication. 7) Preflight checks: wanted you are all done, sit in the cockpit, and make sure the control-to-control surfaces system works perfectly, and gives the right responses; this is nothing but vital common sense: it is no fun to find out during your first fly-around that the rudder cables have not been crossed. Some pilots never get over the surprise. When it’s imperative to make all the following controls: So - Stick back => elevator up - Stick forward => elevator down - Stick left => left aileron up and right aileron down - Stick right => right aileron up and left aileron down - Push right foot => rudder right - Push left foot => rudder left HAPPY FLYING ... Notice: during the first 10 minutes of engine run-in, some unburnt oil can be blown out by the exhaust muffler. To avoid the stain of the wing fabric, it is recommended to cover parts of the aircraft risking to be touched. Only use sweet soap and fresh water to clean the fabric. interdite Reproduction / reproduction Prohibited 2009 ©Randkar 21 July, 2009, HANUMAN XAIR MANUAL ASSEMBLY s.a. KAR RAND Page 75 / 85
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Assembly manual Manuel de montage *
Page 3 and 4:
IMPORTANTES RECOMMANDATIONS POUR L'
Page 5 and 6:
A/ AIRFRAME ASSEMBLY A/ MONTAGE DE
Page 7 and 8:
A3) the rear cockpit side tubes 341
Page 9 and 10:
A7) cockpit front horizontal tube 3
Page 11 and 12:
A10) rear under floor tube 362. Par
Page 13 and 14:
A14) nylon housings with silicon gr
Page 15 and 16:
A18 ) the plate 336 on the ground b
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A22) A22) aileron control system 35
Page 19 and 20:
A24) the frame one side on the floo
Page 21 and 22:
A26) A26) handles 337. throttle Ins
Page 23 and 24: A28) the wheel axels and install fr
Page 25 and 26: B2) frame 336 that bear the rudder
Page 27 and 28: B4) the stabilizer leading edge sup
Page 29 and 30: B7) longitudinal fuselage stiffener
Page 31 and 32: B9) longitudinal fuselage battens 3
Page 33 and 34: B11) the two plates from the tip of
Page 35 and 36: B13) B13) fork 319. Apply silicon g
Page 37 and 38: C B15) and torque all the bolts alr
Page 39 and 40: B17) sail 334377 with luggage rack
Page 41 and 42: C2) rudder horn on rudder (see draw
Page 43 and 44: C4) C4) if the aircraft must be equ
Page 45 and 46: D2) Position firewall 384 in front
Page 47 and 48: BC A D4) a stripe of 3cm wide of th
Page 49 and 50: B A D5-Jabiru RAND KAR s.a. ASSEMBL
Page 51 and 52: D8) D8) in its housing 386 Install
Page 53 and 54: D11) seats 380 in their railings. S
Page 55 and 56: ROTAX 582 RAND KAR s.a. ASSEMBLY MA
Page 57 and 58: E3) Install E2) the choke handle an
Page 59 and 60: A E6) E6) floor cover 377. under Fi
Page 61 and 62: F1C KAR s.a. ASSEMBLY MANUAL XAIR H
Page 63 and 64: F3) that the wing twist is similar
Page 65 and 66: F5) you have clean hands. Position
Page 67 and 68: F7) F7) sail tension at the wing ro
Page 69 and 70: F11) F11) cockpit sides 383 right a
Page 71 and 72: B G3) ailerons 306. Ailerons being
Page 73: H2) H2) spats 379 wheel Install H3)
Page 77 and 78: Page 77 / 85 Centrage L’appareil
Page 79 and 80: DÉMONTAGE ET TRANSPORT préparatio
Page 81 and 82: RAND KAR s.a. ASSEMBLY MANUAL XAIR
Page 83 and 84: RAND KAR s.a. ASSEMBLY MANUAL XAIR
Page 85: FORMULAIRE DE GARANTIE A RETOURNER
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Manuel de montage

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