Manuel de montage

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E4) Connect E4) E5) the fuel line to the engine. hood electric wiring. Connect screws on each side following drawing E5-1). together(2 372335 engine lower and 372334 hood engine upper the Assembly the hoods on the aircraft (E5-2), drill central hole n°1, then drill 3 holes on each side alternately. In case of Rotax 912 engine, it may be necessary to enlarge the hole for the propeller support in the upper hood (E5-3). Position E5-3 280 E5-1 60 KAR s.a. ASSEMBLY MANUAL XAIR HANUMAN 2009, July, 21 ©Randkar 2009 Prohibited reproduction / Reproduction interdite E5-2 RAND Connecter Page 58 / 85 E5) la durite d’alimentation au moteur. inférieur le circuit électrique au niveau du moteur. Connecter suivant E5-1). coté chaque de vis (2 ensemble 372335 et 372334 supérieur moteur capots les Assembler positionner sur la machine (E5-2), percer le trou central N°1, puis les 3 trous latéraux alternativement de chaque coté. Dans le cas d’une motorisation 912, il peut être nécessaire de retoucher le capot supérieur au niveau de la sortie d’hélice (E5-3). Les 1 30 130 130
A E6) E6) floor cover 377. under Fit E6 l’habillage composite sous plancher 377. Poser RAND KAR s.a. ASSEMBLY MANUAL XAIR HANUMAN 2009, July, 21 ©Randkar 2009 Prohibited reproduction / Reproduction interdite Page 59 / 85
Page 1 and 2:
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
Page 17 and 18: 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: E3) Install E2) the choke handle an
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 and 74: H2) H2) spats 379 wheel Install H3)
Page 75 and 76: alance Weighing operation must be d
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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